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红山官方算例库，更新2406版本默认参数

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hechao 2024-06-28 15:38:48 +08:00
parent f674abb75a
commit 6cd9da73a0
108 changed files with 2123 additions and 5155 deletions
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69
A01_TwoD_Plate_Laminar_Struct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A02_TwoD_Plate_Laminar_Ma5_Struct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A03_TwoD_plate_SST_LowMach_Struct/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A04_TwoD_Plate_SST_Ma5_Struct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A05_TwoD_Cylinder_Laminar_Ma8d03_Struct/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A06_ThreeD_NACA0012_SA_Struct_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A07_TwoD_Rae2822_SST_Struct_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A08_TwoD_30p30n_SST_Struct_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A09_ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A10_ThreeD_CHNT_SST_Struct_16CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A11_ThreeD_Sphere_Laminar_Ma10_Struct/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A12_ThreeD_DoubleEllipse_Laminar_Struct_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A13_TwoD_BackwardStep_PressureOutlet_SA_Struct_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A14_TwoD_Plate_TotalPressTempBC_SA_Struct_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A15_ThreeD_ShockWave_PeriodicBoundary_SA_Struct_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A16_TwoD_NLR7301_SST_Struct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A17_ThreeD_Compression_Ramp-16_SA_Struct/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A18_ThreeD_Hollow_Cylinder_Flare_Laminar_Struct_16CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A19_ThreeD_BluntCone_Ma10d6_Laminar_Struct_64CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A20_ThreeD_OV102_Ma20_Laminar_H50_Struct_24CPU/bin/cfd_para.hypara
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@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A21_ThreeD_ShockwaveInteractionPlate_Ma2_Laminar_UDB_Struct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A22_ThreeD_Jet_Ma3d33_SST_Struct_8CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A23_TwoD_Plate_S-KSR_SST_Struct_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A24_TwoD_30p30n_SA_MatrixLUSGS_Struct_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A25_TwoD_Plate_SST_LowMach_MatrixLUSGS_Struct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A26_TwoD_Rae2822_SA_MatrixLUSGS_Struct_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
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@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A28_TwoD_Cylinder_Inv_Ma3d0_Entropyfix6_Struct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
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View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A30_TwoD_Cylinder_Inv_Ma10d0_Entropyfix6_Struct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A31_ThreeD_CHNT_SST_MatrixLUSGS_Struct_256CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
A32_TwoD_NACA0012_Inv_Ma0d2_Precondition_Struct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B01_TwoD_NACA0012_SA_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B02_TwoD_NACA4412_SA_Unstruct_2CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B03_TwoD_Rae2822_SA_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B04_ThreeD_DLR-F6_SA_Unstruct_60CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B05_ThreeD_x38_Laminar_Unstruct_128CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B06_ThreeD_Axisymmetric_SA_Unstruct_64CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B07_ThreeD_Sphere_Laminar_Unstruct_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B08_TwoD_Plate_Laminar_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B09_TwoD_plate_SA_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
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View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
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View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B12_ThreeD_DoubleEllipse_Laminar_Unstruct_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B13_ThreeD_Chnt_SA_Unstruct_100CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
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View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B15_TwoD_NLR7301_SA_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B16_ThreeD_Hollow_Cylinder_Flare_Laminar_Unstruct_16CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B17_TwoD_Plate_S-KSR_SST_Unstruct_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B18_ThreeD_CRM-HL_Level-B_SA_Unstruct_1024CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B19_ThreeD_TrapWing_SA_AoA13_256CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B20_TwoD_NACA0012_SA_GMRES_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B21_ThreeD_Sphere_Laminar_GMRES_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B22_ThreeD_Rotor67_SngleZone_RotatingFrame_6CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B23_ThreeD_Stage35_MultiZone_MixingPlane_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
B24_ThreeD_Aachen-row1_SngleZone_Periodicity_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

15
B25_TwoD_Cylinder_Laminar_LowSpeed_Steady_Unstruct_4CPU/bin/cfd_para.hypara
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@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -515,6 +515,9 @@ double AusmpwPlusLimiter = 1.0;
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
@ -672,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -710,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -727,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -1196,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1409,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.

15
B26_TwoD_Cylinder_Laminar_LowSpeed_Unsteady_Unstruct_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -515,6 +515,9 @@ double AusmpwPlusLimiter = 1.0;
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
@ -672,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -710,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -727,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -1196,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1409,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.

69
C01_TwoD_Cylinder_Laminar_Mix_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
C02_TwoD_Rae2822_SST_Mix_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
C03_ThreeD_M6_SST_Mix_64CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
C04_ThreeD_F6-WB_SST_Mix_256CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
D01_TwoD_Cylinder_Laminar_HighOrder_Struct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
D02_ThreeD_DoubleEllipse_Laminar_HighOrder_Struct_48CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
D03_TwoD_30P30N_SST_HighOrderWENN_Struct_6CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
D04_ThreeD_ONERA_M6_SST_HighOrderWENN_Struct_8CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
D05_ThreeD_DoubleEllipse_Laminar_HighOrderWENN_Struct_48CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
E01_ThreeD_Cylinder_LES_Re3900_Struct_120CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
E02_ThreeD_Cylinder_LES_Re3900_Unstruct_120CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
E03-ThreeD_NACA0012_LES_Struct_400CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
F04_TwoD_Dual0012_OversetGrid_InvisCal_Unstruct_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
F05_ThreeD_AEDC_OversetConfig_Unstruct_8CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU/bin/cfd_para.hypara
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@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
F07-TwoD_NACA0012_PitchingMovement_SA_Struct_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
F08-ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
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View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
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View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
F11_ThreeD_M6_GridParallelRefine_Unstruct_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

3
F12_ThreeD_NRELPhaseⅥ_Laminar_OversetGrid_LowSpeed_Unsteady_Unstruct_64CPU/bin/cfd_para.hypara
View File

@ -515,6 +515,9 @@ double AusmpwPlusLimiter = 1.0;
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.

69
G05_TwoD_Cylinder_N2-O2_Premixing-Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
G06_ThreeD_Sphere_N2-O2_Premixing-Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
H01_TwoD_BackStep_KE_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
H02_TwoD_Cavitity_Re100_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
H03_TwoD_GasLeakage_Steady_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
H04_TwoD_NACA0012_UPWIND_SA_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
H05_TwoD_NACA0012_SIMPLEC_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
H06_TwoD_NaturalConvection_CDS_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
H07_TwoD_Plate_Turb_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
H08_TwoD_Species_Turb_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
H09_ThreeD_Car_Turb_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
H10_ThreeD_Chnt_Lam_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
H11_ThreeD_GasLeakage_Unsteady_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
H12_ThreeD_Species_Transient_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
H13_ThreeD_SUBOFF_UPWIND_4CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

69
L01_TwoD_Cavity_BGK_MPI_1CPU/bin/cfd_para.hypara
View File

@ -8,7 +8,7 @@
// Platform for Hybrid Engineering Simulation of Flows + // Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center + // China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
// PHengLEI 2312 + // PHengLEI 2406 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
//flowInitMethod: Flow field initialization method. //flowInitMethod: Flow field initialization method.
// 0 -- The entire flow field is initialized according to Infinite velocity. // 0 -- The entire flow field is initialized according to Infinite velocity.
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
// 2 -- The entire flow field is initialized by flowInitStep iterations of FirstOrder method.
// 3 -- The entire flow field is initialized by flowInitStep iterations of LUSGS method.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle",
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod", // -- "barth", "vencat", "vanleer", "minmod",
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
// 6 -- Jacobian iteration. // 6 -- Jacobian iteration.
// 7 -- Line LU-SGS. // 7 -- Line LU-SGS.
// 8 -- Matrix LU-SGS. // 8 -- Matrix LU-SGS.
// 9 -- GMRES.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLMethod: The method to compute cfl number.
// 0 -- Linear change.
// 1 -- Exponential change.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double GMRESCFLScale = 1.0;
int OriginalTscheme = 0;
double pMaxForCFL = 0.2; double pMaxForCFL = 0.2;
double pMinForCFL = 0.1; double pMinForCFL = 0.1;
double deltaMaxForCFL = 0.2; double deltaMaxForCFL = 0.2;
@ -678,6 +675,7 @@ int plotFieldType = 0;
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
// 2 -- Ensight binary. // 2 -- Ensight binary.
// 3 -- Ensight ASCII. // 3 -- Ensight ASCII.
// 4 -- Paraview.
int visualfileType = 1; int visualfileType = 1;
// samplefileMode: The dump mode of sample file. // samplefileMode: The dump mode of sample file.
@ -716,7 +714,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), // -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), // -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58)(the two parameters are related to CFL self-adaptive, only support struct grid)
// -- overlap iblank(iblank, 81), // -- overlap iblank(iblank, 81),
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
int nVisualVariables = 8; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9; int nVisualWallVariables = 6;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
// dumpStandardModel: Dump many standard model data. // dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
// iapplication: // iapplication:
// 0 -- gas model is fixed in the codes. // 0 -- gas model is fixed in the codes.
// 1 -- gas model is imported from library files. // 1 -- gas model is imported from library files.
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver. // isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
// isAdaptiveSolver > 0 indicates the HyFlow self-adaptive solver.
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
// nm: Equation number of the physics, but is out of commision now. // nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D. // 4 -- for 2D.
// 5 -- for 3D. // 5 -- for 3D.
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
// useHyflowSetting: Setting for HyFLOW GUI.
// 0 -- PHengLEI.
// 1 -- HyFLOW.
// nProtectData: Use the continuation file data protection mechanism. // nProtectData: Use the continuation file data protection mechanism.
// 0 -- no. // 0 -- no.
// 1 -- yes. // 1 -- yes.
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
int wallMultiTemperature = 0; int wallMultiTemperature = 0;
int nProtectData = 0; int nProtectData = 0;
int useHyflowSetting = 0;
int nAblation = 0; int nAblation = 0;
int isInjection = 0; int isInjection = 0;
int nViscosityModel = 0; int nViscosityModel = 0;
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
int nFraction = 0; int nFraction = 0;
int nContinueModel = 0; int nContinueModel = 0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
int isUseNoneqCond = 0; int isUseNoneqCond = 0;
double frozenCondition = 0.01; double frozenCondition = 0.01;
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; //string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
// dimensional physical time for additional force(s). // dimensional physical time for additional force(s).
double addedForceTime_0[] = 0.0; double addedForceTime_0[] = 0.0;
// dimensional massCenterPosition for additional force(s).
double addedForcePosition_0[] = 0.0, 0.0, 0.0;
// additional force(inertia system) fX fY fZ. // additional force(inertia system) fX fY fZ.
double addedForce_0[] = 0.0, 0.0, 0.0; double addedForce_0[] = 0.0, 0.0, 0.0;
// additional moment(inertia system) mX mY mZ. // additional moment(inertia system) mX mY mZ.
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
// post indentify. // post indentify.
int integralOrder = 4; int integralOrder = 4;
#************************************************************************
# TurboMachinery Parameter *
#************************************************************************
// ----------------- Rotating Frame --------------------------------
// referenceFrame: whether rotating reference frame used.
// 0 -- Stationary Frame.
// 1 -- Translational Frame.
// 2 -- Rotational Frame.
int referenceFrame = 0;
// nTurboZone: number of rows of TurboMachinery.
int nTurboZone = 0;
// Periodic_Name: a list of periodic boundary name, the number of name equals to 2*nZone
// "Periodic_up, Periodic_down" means a pair of name of one zone
string Periodic_Name[] = "Periodic_up, Periodic_down";
// PeriodicRotationAngle means rotating angle for each zone.
// PeriodicRotationAngle[] = [theta1, theta2...]
// theta1, theta2 means rotating angle for zone1,zone2.
double PeriodicRotationAngle[] = [16.363636363636];
// MixingPlane: a list of mixing plane name, the number of name equals to 2*nZone-2
// "MixOut, MixIn" the first is upstream zone outlet, the second is downstream zone inlet.
string MixingPlane[] = "";
// Omega: angular velocity(rad/s) of each zone.
double Omega[] = [-1680.0];
// shroud: define turbomachinery shroud of each zone, because shroud do not rotate.
string shroud[] = "shroud";
// nSpanSection: number of spanwise section used for mixing plane.
int nSpanSection = 0;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 6.5e6; //@double refReNumber = 6.5e6;

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