forked from PHengLEI/PHengLEI-TestCases
红山官方算例库，更新2406版本默认参数
This commit is contained in:
hechao
parent
f674abb75a
commit
6cd9da73a0
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -515,6 +515,9 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
|
|
@ -672,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -727,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -1196,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1409,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -515,6 +515,9 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
|
|
@ -672,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -727,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -1196,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1409,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -515,6 +515,9 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
|
|
@ -8,7 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2312 +
|
||||
// PHengLEI 2406 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -295,8 +295,6 @@ int preconFarfieldBCMethod = 1;
|
|||
//flowInitMethod: Flow field initialization method.
|
||||
// 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.
|
||||
// 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.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
|
|
@ -421,7 +419,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// 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+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod",
|
||||
|
|
@ -515,14 +513,14 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line 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.
|
||||
// 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.
|
||||
// CFLEnd: End cfl number.
|
||||
// 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])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -571,8 +569,7 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 0;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -678,6 +675,7 @@ int plotFieldType = 0;
|
|||
// 1 -- Tecplot ASCII.
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
// 4 -- Paraview.
|
||||
int visualfileType = 1;
|
||||
|
||||
// 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),
|
||||
// -- 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),
|
||||
// -- 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),
|
||||
// -- 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!!!
|
||||
|
|
@ -733,8 +731,8 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
|
|
@ -877,7 +875,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 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.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -1053,6 +1054,9 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
|
|
@ -1151,6 +1155,7 @@ int nDensityForWallMethod = 0;
|
|||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1195,7 +1200,6 @@ double molecularWeightSpeciesB = 30.0;
|
|||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
|
@ -1408,6 +1412,8 @@ double rotateFrequency_0 = 0.0;
|
|||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
// dimensional physical time for additional force(s).
|
||||
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.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
|
|
@ -1418,41 +1424,6 @@ int morphing_0 = 0;
|
|||
// post indentify.
|
||||
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 --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
|
|||
Some files were not shown because too many files have changed in this diff Show More
Loading…
Reference in New Issue