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PHengLEI-TestCases
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update v7628

This commit is contained in:
hechao 2021-04-15 09:34:10 +08:00
parent b7c800cbc0
commit e53764020a
39 changed files with 470 additions and 470 deletions
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24
ThreeD_Cylinder_LES_Re3900_Struct_120CPU/bin/cfd_para.hypara
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@ -264,11 +264,11 @@ int compressible = 1;
// condition is radiation equilibrium temperature, and 0.8 is the default value.
double refMachNumber = 0.20;
double attackd = 0.00;
double angleSlide = 0.00;
double attackd = 0.00;
double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 3900;
int inflowParaType = 0;
double refReNumber = 3900;
double refDimensionalTemperature = 288.15;
double freestream_vibration_temperature = 10000.00;
@ -288,9 +288,9 @@ double freestream_vibration_temperature = 10000.00;
//double refDimensionalPressure = 1.01313E05;
double wallTemperature = -1.0;
int dump_Q = 0;
int dump_Q = 0;
double radiationCoef = 0.8;
double radiationCoef = 0.8;
double gridScaleFactor = 1.0;
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
@ -316,7 +316,7 @@ double TorqueRefZ = 0.0; // unit of meter.
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
// -- "nolim", no limiter.
// -- "vanalbada_clz", clz supersonic version.
string inviscidSchemeName = "roe";
string inviscidSchemeName = "roe";
string str_limiter_name = "vanalbada";
#*******************************************************************
@ -383,7 +383,7 @@ string str_limiter_name = "vanalbada";
//string viscousName = "Euler";
int viscousType = 1;
string viscousName = "laminar";
string viscousName = "laminar";
//int viscousType = 3;
//string viscousName = "1eq-sa";
@ -399,9 +399,9 @@ string uns_vis_name = "test";
string gradientName = "ggnode";
int ivencat = 7;
double venkatCoeff = 5.0;
double venkatCoeff = 5.0;
int reconmeth = 1;
int limitVariables = 0;
int limitVariables = 0;
int limitVector = 0;
double limit_angle = 0;
double skewnessAngle = 60.0;
@ -474,14 +474,14 @@ int iSimplifyViscousTerm = 1;
int ifLocalTimeStep = 0;
double CFLStart = 0.01;
double CFLEnd = 10.0;
int CFLVaryStep = 500;
int CFLVaryStep = 500;
double ktmax = 1.0e10;
int swapDq = 1;
int nLUSGSSweeps = 1;
double LUSGSTolerance = 0.01;
double LUSGSTolerance = 0.01;
int order = 2;
double visl_min = 0.01;

10
ThreeD_DoubleEllipse_Laminar_HighOrder_Struct/ThreeD_DoubleEllipse_Laminar_HighOrder_Struct/bin/cfd_para_hypersonic.hypara
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@ -93,16 +93,16 @@ double TorqueRefZ = 0.0; // unit of meter.
// 3 -- IDDES.
//int viscousType = 0;
//string viscousName = "Euler";
//string viscousName = "Euler";
int viscousType = 1;
string viscousName = "laminar";
string viscousName = "laminar";
//int viscousType = 3;
//string viscousName = "1eq-sa";
//string viscousName = "1eq-sa";
//int viscousType = 4;
//string viscousName = "2eq-kw-menter-sst";
//string viscousName = "2eq-kw-menter-sst";
int DESType = 0;
@ -264,4 +264,4 @@ double catalyticCoef = 1.0;
string gasfile = "DK5";
string speciesName = "O, O2, NO, N, N2";
string initMassFraction = "0.07955, 0.134, 0.0509, 1.0e-9, 0.73555";
int ifStartFromPerfectGasResults = 0;
int ifStartFromPerfectGasResults = 0;

8
ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para_transonic.hypara
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@ -81,16 +81,16 @@ double TorqueRefZ = 0.0; // unit of meter.
// 3 -- IDDES.
//int viscousType = 0;
//string viscousName = "Euler";
//string viscousName = "Euler";
//int viscousType = 1;
//string viscousName = "laminar";
//string viscousName = "laminar";
//int viscousType = 3;
//string viscousName = "1eq-sa";
//string viscousName = "1eq-sa";
int viscousType = 4;
string viscousName = "2eq-kw-menter-sst";
string viscousName = "2eq-kw-menter-sst";
int DESType = 0;

8
ThreeD_M6_SST_Struct_MG2_4CPU/bin/key.hypara
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@ -15,10 +15,10 @@ string defaultParaFile = "./bin/cfd_para.hypara";
// 2 -- Wall distance computation for turb-solver.
// 3 -- Grid partition.
// 4 -- Knowledge repository / examples of PHengLEI-API.
int ndim = 3;
int nparafile = 1;
int ndim = 3;
int nparafile = 1;
int nsimutask = 0;
int nsimutask = 0;
string parafilename = "./bin/cfd_para_transonic.hypara";
//string parafilename = "./bin/cfd_para_transonic.hypara";
//string parafilename = "./bin/cfd_para_supersonic.hypara";
@ -38,7 +38,7 @@ string parafilename = "./bin/cfd_para_transonic.hypara";
//string parafilename = "./bin/post_processing.hypara";
// ---------------- Advanced Parameters, DO NOT care it ----------------
int iovrlap = 0;
int iovrlap = 0;
int numberOfGridProcessor = 0;
// ATP read
//@string parafilename1 = ""

8
ThreeD_M6_SST_Struct_MG2_4CPU/bin/partition.hypara
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@ -8,11 +8,11 @@
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
int pgridtype = 1;
int maxproc = 4;
int pgridtype = 1;
int maxproc = 4;
string original_grid_file = "./grid/m6_str.fts";
string partition_grid_file = "./grid/m6_str__4.fts";
string original_grid_file = "./grid/m6_str.fts";
string partition_grid_file = "./grid/m6_str__4.fts";
// numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid.
// 1 -- single level.

58
ThreeD_NACA0012_SA_Struct/bin/cfd_para_transonic.hypara
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@ -7,12 +7,12 @@
// intervalStepForce: the step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: the step intervals for residual 'res.dat' saved.
int maxSimuStep = 50000;
int maxSimuStep = 50000;
int intervalStepFlow = 1000;
int intervalStepPlot = 1000;
int intervalStepForce = 100;
int intervalStepRes = 10;
int intervalStepFlow = 1000;
int intervalStepPlot = 1000;
int intervalStepForce = 100;
int intervalStepRes = 10;
#########################################################################
# Inflow Parameter #
@ -33,17 +33,17 @@ int intervalStepRes = 10;
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent to grid scale.
double refMachNumber = 0.799;
double attackd = 2.26;
double angleSlide = 0.00;
double attackd = 2.26;
double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 9.0e6;
int inflowParaType = 0;
double refReNumber = 9.0e6;
double refDimensionalTemperature = 288.15;
//int inflowParaType = 1;
//double height = 0.001;
//int inflowParaType = 1;
//double height = 0.001;
//int inflowParaType = 2;
//int inflowParaType = 2;
//double refDimensionalTemperature = 6051.024; //the total temperature, T*(1+(gama0-1)*M*M/2).
//double refDimensionalPressure = 4.299696E09; //the total pressure, p*(T0/T)^(gama0/(gama0-1)).
@ -73,17 +73,17 @@ double TorqueRefZ = 0.0; // unit of meter.
// 2 - DDES;
// 3 - IDDES;
//int iviscous = 0;
//string viscousName = "Euler";
//int iviscous = 0;
//string viscousName = "Euler";
//int iviscous = 1;
//string viscousName = "laminar";
//int iviscous = 1;
//string viscousName = "laminar";
int viscousType = 3;
string viscousName = "1eq-sa";
int viscousType = 3;
string viscousName = "1eq-sa";
//int iviscous = 4;
//string viscousName = "2eq-kw-menter-sst";
//int iviscous = 4;
//string viscousName = "2eq-kw-menter-sst";
int DESType = 0;
@ -102,7 +102,7 @@ double roeEntropyScale = 1.0;
// - "3rdsmooth", "smooth"
// - "nolim" - no limiter
string inviscidSchemeName = "roe";
string inviscidSchemeName = "roe";
string str_limiter_name = "smooth";
#*******************************************************************
@ -121,7 +121,7 @@ string str_limiter_name = "smooth";
string uns_scheme_name = "roe";
string uns_limiter_name = "vencat";
double venkatCoeff = 5.0;
double venkatCoeff = 5.0;
#########################################################################
# Temporal Discretisation #
@ -135,11 +135,11 @@ double venkatCoeff = 5.0;
// 1 : is recommended for structured solver.
// 1-3: is recommended for unstructured solver.
int iunsteady = 0;
int iunsteady = 0;
double CFLEnd = 30.0;
double CFLEnd = 30.0;
int nLUSGSSweeps = 1;
int nLUSGSSweeps = 1;
#########################################################################
# Multi-Grid parameters #
@ -151,7 +151,7 @@ int nLUSGSSweeps = 1;
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
int nMGLevel = 1;
int nMGLevel = 1;
int flowInitStep = 100;
@ -166,7 +166,7 @@ int flowInitStep = 100;
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0/1.
string gridfile = "./grid/NACA0012__4.fts";
int isPlotVolumeField = 0;
int isPlotVolumeField = 0;
@ -192,6 +192,6 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// reconmeth:
// 0 - When reconstruct face value, Q+, Q- use respective limiter coefficients.
// 1 - Q+, Q- use the min limiter coefficients of left and right cell.
int reconmeth = 1;
int limitVariables = 0;
int reconmeth = 1;
int limitVariables = 0;
int limitVector = 0;

10
ThreeD_NACA0012_SA_Struct/bin/grid_para.hypara
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@ -17,17 +17,17 @@
// 6 -- Ustar, mgrid.in.
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
// 8 -- GMSH, *.msh.
int gridtype = 1;
int axisup = 1;
int from_gtype = 3;
int gridtype = 1;
int axisup = 1;
int from_gtype = 3;
#########################################################################
# File path #
#########################################################################
// from_gfile: path of original data file for unstructure grid convert from.
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
string from_gfile = "./grid/NACA0012.grd";
string out_gfile = "./grid/NACA0012.fts";
string from_gfile = "./grid/NACA0012.grd";
string out_gfile = "./grid/NACA0012.fts";

4
ThreeD_NACA0012_SA_Struct/bin/key.hypara
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@ -15,8 +15,8 @@ string defaultParaFile = "./bin/cfd_para.hypara";
// 2 -- Wall distance computation for turb-solver.
// 3 -- Grid partition.
// 4 -- Knowledge repository / examples of PHengLEI-API.
int ndim = 3;
int nparafile = 1;
int ndim = 3;
int nparafile = 1;
int nsimutask = 0;
string parafilename = "./bin/cfd_para_transonic.hypara";

10
ThreeD_NACA0012_SA_Struct/bin/partition.hypara
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@ -8,16 +8,16 @@
// original_grid_file : original grid file that want to be divided(HyperFLOW/PHengLEI type, *.fts).
// partition_grid_file : target partition grid file(HyperFLOW/PHengLEI type, *.fts).
int pgridtype = 1;
int maxproc = 4;
int pgridtype = 1;
int maxproc = 4;
string original_grid_file = "./grid/NACA0012.fts";
string partition_grid_file = "./grid/NACA0012__4.fts";
string original_grid_file = "./grid/NACA0012.fts";
string partition_grid_file = "./grid/NACA0012__4.fts";
// Number of multi-grid levels, ONLY used for structured grid.
// 1 -- single level, 2 -- 2 level, N -- N level, ..., et al.
int numberOfMultigrid = 1;
int numberOfMultigrid = 1;

24
ThreeD_ShockWave_PeriodicBoundary_SA_Struct_4CPU/bin/cfd_para.hypara
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@ -222,14 +222,14 @@ int numberOfMultigrid = 1;
// 0 -- no precondition process. (default, mach > 0.3)
// 1 -- carry out precondition process. (mach number <= 0.3)
int maxSimuStep = 20000;
int maxSimuStep = 20000;
int intervalStepFlow = 1000;
int intervalStepPlot = 1000;
int intervalStepFlow = 1000;
int intervalStepPlot = 1000;
int intervalStepSample = 1000;
int intervalStepForce = 100;
int intervalStepRes = 10;
int ifLowSpeedPrecon = 0;
int intervalStepForce = 100;
int intervalStepRes = 10;
int ifLowSpeedPrecon = 0;
// compressible:
// 0 -- incompressible flow.
@ -296,7 +296,7 @@ double freestream_vibration_temperature = 10000.00;
//double refDimensionalPressure = 1.01313E05;
double wallTemperature = -1.0;
int dump_Q = 0;
int dump_Q = 0;
double radiationCoef = 0.8;
double gridScaleFactor = 1.0;
@ -387,16 +387,16 @@ string str_limiter_name = "vanalbada";
// It is used to scale the default Roe entropy fix coefficients.
//int viscousType = 0;
//string viscousName = "Euler";
//string viscousName = "Euler";
//int viscousType = 1;
//string viscousName = "laminar";
//string viscousName = "laminar";
int viscousType = 3;
string viscousName = "1eq-sa";
int viscousType = 3;
string viscousName = "1eq-sa";
//int viscousType = 4;
//string viscousName = "2eq-kw-menter-sst";
//string viscousName = "2eq-kw-menter-sst";
int DESType = 0;

4
ThreeD_ShockWave_PeriodicBoundary_SA_Struct_4CPU/bin/cfd_para_hypersonic.hypara
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@ -198,7 +198,7 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// 0 -- When reconstruct face value, Q+, Q- use respective limiter coefficients.
// 1 -- Q+, Q- use the min limiter coefficients of left and right cell.
int reconmeth = 1;
int reconmeth = 1;
int limitVariables = 0;
int limitVector = 0;
int limitVector = 0;
double MUSCLCoefXk = 0.333333;

58
ThreeD_Sphere_Laminar_Ma10_Struct/bin/cfd_para_hypersonic.hypara
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@ -7,12 +7,12 @@
// intervalStepForce: the step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: the step intervals for residual 'res.dat' saved.
int maxSimuStep = 25000;
int maxSimuStep = 25000;
int intervalStepFlow = 1000;
int intervalStepPlot = 1000;
int intervalStepForce = 100;
int intervalStepRes = 10;
int intervalStepFlow = 1000;
int intervalStepPlot = 1000;
int intervalStepForce = 100;
int intervalStepRes = 10;
#########################################################################
# Inflow Parameter #
@ -40,15 +40,15 @@ int intervalStepRes = 10;
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent to grid scale.
double refMachNumber = 10.00;
double attackd = 0.00;
double angleSlide = 0.00;
double attackd = 0.00;
double angleSlide = 0.00;
double wallTemperature = 294.0 ;
int dump_Q = 2;
double wallTemperature = 294.0 ;
int dump_Q = 2;
int inflowParaType = 0;
double refReNumber = 1.0e5;
double refDimensionalTemperature = 79.0;
int inflowParaType = 0;
double refReNumber = 1.0e5;
double refDimensionalTemperature = 79.0;
//int inflowParaType = 1;
//double height = 0.001;
@ -84,18 +84,18 @@ double TorqueRefZ = 0.0; // unit of meter.
// 3 - IDDES;
//int iviscous = 0;
//string viscousName = "Euler";
//string viscousName = "Euler";
int viscousType = 1;
string viscousName = "laminar";
int viscousType = 1;
string viscousName = "laminar";
//int iviscous = 3;
//string viscousName = "1eq-sa";
//string viscousName = "1eq-sa";
//int iviscous = 4;
//string viscousName = "2eq-kw-menter-sst";
//string viscousName = "2eq-kw-menter-sst";
int DESType = 0;
int DESType = 0;
int roeEntropyFixMethod = 2;
double roeEntropyScale = 0.0001;
@ -111,7 +111,7 @@ double roeEntropyScale = 0.0001;
// str_limiter_name: Limiter of struct grid
// - "minmod", "3rd_minmod_smooth"
string inviscidSchemeName = "steger";
string inviscidSchemeName = "steger";
string str_limiter_name = "minmod";
#*******************************************************************
@ -142,11 +142,11 @@ double venkatCoeff = 0.5;
// The bigger the value, the convergence faster but lower robustness.
// ktmax: The lower the value, the more robustness, 1.0e5 ~ 1.0e10.
int iunsteady = 0;
int iunsteady = 0;
double CFLEnd = 10.0;
int CFLVaryStep = 100;
double ktmax = 1.0e10;
double CFLEnd = 10.0;
int CFLVaryStep = 100;
double ktmax = 1.0e10;
#########################################################################
@ -160,7 +160,7 @@ double ktmax = 1.0e10;
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0/1.
string gridfile = "./grid/3dball.fts";
int isPlotVolumeField = 0;
int isPlotVolumeField = 0;
@ -174,8 +174,8 @@ int isPlotVolumeField = 0;
// -- modeledTKE(18),modeleddissipationrate(19), SSTF1(20), SSTF2(21)
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!.
// Arriables order must from small to larger.
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// limitVariables: limit model.
// 0 - limit only for pressure and denstiny, then get the min value
@ -186,6 +186,6 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// reconmeth:
// 0 - When reconstruct face value, Q+, Q- use respective limiter coefficients.
// 1 - Q+, Q- use the min limiter coefficients of left and right cell.
int reconmeth = 0;
int limitVariables = 0;
int limitVector = 1;
int reconmeth = 0;
int limitVariables = 0;
int limitVector = 1;

6
ThreeD_Sphere_Laminar_Ma10_Struct/bin/grid_para.hypara
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@ -17,9 +17,9 @@
// 6 -- Ustar, mgrid.in.
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
// 8 -- GMSH, *.msh.
int gridtype = 1;
int axisup = 1;
int from_gtype = 3;
int gridtype = 1;
int axisup = 1;
int from_gtype = 3;
#########################################################################
# File path #

6
ThreeD_Sphere_Laminar_Ma10_Struct/bin/key.hypara
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@ -15,7 +15,7 @@ string defaultParaFile = "./bin/cfd_para.hypara";
// 4 -- Knowledge repository / examples of PHengLEI-API.
int ndim = 3;
int nparafile = 1;
int nsimutask = 0;
int nsimutask = 0;
string parafilename = "./bin/cfd_para_hypersonic.hypara";
//string parafilename = "./bin/cfd_para_transonic.hypara";
//string parafilename = "./bin/cfd_para_supersonic.hypara";
@ -34,8 +34,8 @@ string parafilename = "./bin/cfd_para_hypersonic.hypara";
//int nsimutask = 99;
//string parafilename = "./bin/post_processing.hypara";
// ---------------- advanced Parameters, DO NOT care it -----------
int iovrlap = 0;
int numberOfGridProcessor = 0;
int iovrlap = 0;
int numberOfGridProcessor = 0;
// ATP read
string parafilename1 = ""
string parafilename2 = "";

2
ThreeD_Sphere_Laminar_Ma10_Struct/bin/partition.hypara
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@ -9,7 +9,7 @@
// partition_grid_file : target partition grid file(HyperFLOW/PHengLEI type, *.fts).
int pgridtype = 1;
int maxproc = 1;
int maxproc = 1;
string original_grid_file = "./grid/3dball.fts";
string partition_grid_file = "./grid/3dball.fts";

48
TwoD_30p30n_SST_Struct/bin/cfd_para_subsonic.hypara
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@ -39,15 +39,15 @@ int ifLowSpeedPrecon = 0;
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent to grid scale.
double refMachNumber = 0.2;
double attackd = 19.0;
double angleSlide = 0.00;
double attackd = 19.0;
double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 9.0e6;
double refDimensionalTemperature = 288.0;
int inflowParaType = 0;
double refReNumber = 9.0e6;
double refDimensionalTemperature = 288.0;
//int inflowParaType = 1;
//double height = 0.001;
//int inflowParaType = 1;
//double height = 0.001;
double gridScaleFactor = 1.0;
@ -76,21 +76,21 @@ double TorqueRefZ = 0.0; // unit of meter.
// 3 - IDDES;
//int iviscous = 0;
//string viscousName = "Euler";
//string viscousName = "Euler";
//int iviscous = 1;
//string viscousName = "laminar";
//string viscousName = "laminar";
//int iviscous = 3;
//string viscousName = "1eq-sa";
//string viscousName = "1eq-sa";
int viscousType = 4;
string viscousName = "2eq-kw-menter-sst";
string viscousName = "2eq-kw-menter-sst";
int DESType = 0;
int DESType = 0;
int roeEntropyFixMethod = 2;
double roeEntropyScale = 1.0;
double roeEntropyScale = 1.0;
#########################################################################
# Spatial Discretisation #
#########################################################################
@ -128,11 +128,11 @@ double venkatCoeff = 50.0;
// 1 : is recommended for structured solver.
// 1-3: is recommended for unstructured solver.
int iunsteady = 0;
int iunsteady = 0;
double CFLEnd = 10.0;
int nLUSGSSweeps = 1;
int nLUSGSSweeps = 1;
#########################################################################
# Multi-Grid parameters #
@ -144,8 +144,8 @@ int nLUSGSSweeps = 1;
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
int nMGLevel = 1;
int flowInitStep = 100;
int nMGLevel = 1;
int flowInitStep = 100;
#########################################################################
@ -158,8 +158,8 @@ int flowInitStep = 100;
// Please use 'rae2822_hybrid2d__4.fts' here!
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0/1.
string gridfile = "./grid/30p30n_str__4.fts";
int isPlotVolumeField = 0;
string gridfile = "./grid/30p30n_str__4.fts";
int isPlotVolumeField = 0;
// ---------------- advanced Parameters, DO NOT care it -----------
@ -172,8 +172,8 @@ int isPlotVolumeField = 0;
// -- modeledTKE(18),modeleddissipationrate(19), SSTF1(20), SSTF2(21)
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!.
// Arriables order must from small to larger.
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// limitVariables: limit model.
// 0 - limit only for pressure and denstiny, then get the min value
@ -184,6 +184,6 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// reconmeth:
// 0 - When reconstruct face value, Q+, Q- use respective limiter coefficients.
// 1 - Q+, Q- use the min limiter coefficients of left and right cell.
int reconmeth = 1;
int limitVariables = 0;
int limitVector = 0;
int reconmeth = 1;
int limitVariables = 0;
int limitVector = 0;

6
TwoD_30p30n_SST_Struct/bin/grid_para.hypara
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@ -17,9 +17,9 @@
// 6 -- Ustar, mgrid.in.
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
// 8 -- GMSH, *.msh.
int gridtype = 1;
int axisup = 1;
int from_gtype = 3;
int gridtype = 1;
int axisup = 1;
int from_gtype = 3;
#########################################################################
# File path #

6
TwoD_BackwardStep_PressureOutlet_SA_Struct_4CPU/bin/grid_para.hypara
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@ -17,9 +17,9 @@
// 6 -- Ustar, mgrid.in.
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
// 8 -- GMSH, *.msh.
int gridtype = 1;
int axisup = 1;
int from_gtype = 3;
int gridtype = 1;
int axisup = 1;
int from_gtype = 3;
#########################################################################
# File path #

2
TwoD_Cylinder_Laminar_HighOrder_Struct/TwoD_Cylinder_Laminar_HighOrder_Struct/bin/cfd_para_hypersonic.hypara
View File

@ -154,7 +154,7 @@ double venkatCoeff = 0.5;
int iunsteady = 0;
double CFLEnd = 10.0;
int CFLVaryStep = 100;
int CFLVaryStep = 100;
double ktmax = 1.0e10;

54
TwoD_Cylinder_Laminar_Ma8d03_Struct/bin/cfd_para_hypersonic.hypara
View File

@ -7,12 +7,12 @@
// intervalStepForce: the step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: the step intervals for residual 'res.dat' saved.
int maxSimuStep = 30000;
int maxSimuStep = 30000;
int intervalStepFlow = 1000;
int intervalStepPlot = 1000;
int intervalStepForce = 100;
int intervalStepRes = 10;
int intervalStepFlow = 1000;
int intervalStepPlot = 1000;
int intervalStepForce = 100;
int intervalStepRes = 10;
#########################################################################
# Inflow Parameter #
@ -40,24 +40,24 @@ int intervalStepRes = 10;
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent to grid scale.
double refMachNumber = 8.03;
double attackd = 0.00;
double angleSlide = 0.00;
double attackd = 0.00;
double angleSlide = 0.00;
double wallTemperature = 294.0 ;
int dump_Q = 0;
double wallTemperature = 294.0 ;
int dump_Q = 0;
int inflowParaType = 0;
double refReNumber = 3.67e5;
int inflowParaType = 0;
double refReNumber = 3.67e5;
double refDimensionalTemperature = 125.0;
//int inflowParaType = 1;
//double height = 0.001;
//int inflowParaType = 1;
//double height = 0.001;
//int inflowParaType = 2;
//double refDimensionalTemperature = 6051.024; //the total temperature, T*(1+(gama0-1)*M*M/2).
//double refDimensionalPressure = 4.299696E09; //the total pressure, p*(T0/T)^(gama0/(gama0-1)).
double gridScaleFactor = 1.0;
double gridScaleFactor = 1.0;
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
double forceRefenenceLength = 1.0; // unit of meter.
@ -84,18 +84,18 @@ double TorqueRefZ = 0.0; // unit of meter.
// 3 - IDDES;
//int iviscous = 0;
//string viscousName = "Euler";
//string viscousName = "Euler";
int viscousType = 1;
string viscousName = "laminar";
int viscousType = 1;
string viscousName = "laminar";
//int iviscous = 3;
//string viscousName = "1eq-sa";
//string viscousName = "1eq-sa";
//int iviscous = 4;
//string viscousName = "2eq-kw-menter-sst";
//string viscousName = "2eq-kw-menter-sst";
int DESType = 0;
int DESType = 0;
int roeEntropyFixMethod = 2;
double roeEntropyScale = 0.0001;
@ -111,7 +111,7 @@ double roeEntropyScale = 0.0001;
// str_limiter_name: Limiter of struct grid
// - "minmod", "3rd_minmod_smooth"
string inviscidSchemeName = "roe";
string inviscidSchemeName = "roe";
string str_limiter_name = "vanleer";
#*******************************************************************
@ -130,7 +130,7 @@ string str_limiter_name = "vanleer";
string uns_scheme_name = "vanleer";
string uns_limiter_name = "vencat";
double venkatCoeff = 0.5;
double venkatCoeff = 0.5;
#########################################################################
# Temporal Discretisation #
@ -142,11 +142,11 @@ double venkatCoeff = 0.5;
// The bigger the value, the convergence faster but lower robustness.
// ktmax: The lower the value, the more robustness, 1.0e5 ~ 1.0e10.
int iunsteady = 0;
int iunsteady = 0;
double CFLEnd = 3.0;
double CFLEnd = 3.0;
double ktmax = 1.0e10;
double ktmax = 1.0e10;
#########################################################################
@ -159,8 +159,8 @@ double ktmax = 1.0e10;
// Please use 'rae2822_hybrid2d__4.fts' here!
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0/1.
string gridfile = "./grid/input.fts";
int isPlotVolumeField = 0;
string gridfile = "./grid/input.fts";
int isPlotVolumeField = 0;

6
TwoD_Cylinder_Laminar_Ma8d03_Struct/bin/grid_para.hypara
View File

@ -17,9 +17,9 @@
// 6 -- Ustar, mgrid.in.
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
// 8 -- GMSH, *.msh.
int gridtype = 1;
int axisup = 1;
int from_gtype = 3;
int gridtype = 1;
int axisup = 1;
int from_gtype = 3;
#########################################################################
# File path #

10
TwoD_Cylinder_Laminar_OneTemperMode_FCW_Struct/bin/cfd_para_hypersonic.hypara
View File

@ -92,16 +92,16 @@ double TorqueRefZ = 0.0; // unit of meter.
// 2 -- DDES.
// 3 -- IDDES.
//int viscousType = 0;
//int viscousType = 0;
//string viscousName = "Euler";
int viscousType = 1;
int viscousType = 1;
string viscousName = "laminar";
//int viscousType = 3;
//int viscousType = 3;
//string viscousName = "1eq-sa";
//int viscousType = 4;
//int viscousType = 4;
//string viscousName = "2eq-kw-menter-sst";
int DESType = 0;
@ -235,4 +235,4 @@ double catalyticCoef = 1.0;
string gasfile = "DK11";
string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-";
string initMassFraction = "0.07955,0.134,0.0509,1.0e-9,0.0,0.0,0.0,0.0,0.0,0.73555,0.0";
int ifStartFromPerfectGasResults = 0;
int ifStartFromPerfectGasResults = 0;

82
TwoD_Plate_Laminar_Ma5_Struct_1CPU/bin/cfd_para_hypersonic.hypara
View File

@ -7,12 +7,12 @@
// intervalStepForce: the step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: the step intervals for residual 'res.dat' saved.
int maxSimuStep = 50000;
int maxSimuStep = 50000;
int intervalStepFlow = 1000;
int intervalStepPlot = 1000;
int intervalStepForce = 100;
int intervalStepRes = 10;
int intervalStepFlow = 1000;
int intervalStepPlot = 1000;
int intervalStepForce = 100;
int intervalStepRes = 10;
#########################################################################
# Inflow Parameter #
@ -39,25 +39,25 @@ int intervalStepRes = 10;
// forceRefenenceLength, forceRefenenceArea: Reference length and area, independent to grid scale.
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent to grid scale.
double refMachNumber = 5.00;
double attackd = 0.00;
double angleSlide = 0.00;
double refMachNumber = 5.00;
double attackd = 0.00;
double angleSlide = 0.00;
double wallTemperature = 327.36;
int dump_Q = 0;
double wallTemperature = 327.36;
int dump_Q = 0;
int inflowParaType = 0;
double refReNumber = 1.5e7;
double refDimensionalTemperature = 300.33;
int inflowParaType = 0;
double refReNumber = 1.5e7;
double refDimensionalTemperature = 300.33;
//int inflowParaType = 1;
//double height = 0.001;
//int inflowParaType = 1;
//double height = 0.001;
//int inflowParaType = 2;
//double refDimensionalTemperature = 6051.024; //the total temperature, T*(1+(gama0-1)*M*M/2).
//double refDimensionalPressure = 4.299696E09; //the total pressure, p*(T0/T)^(gama0/(gama0-1)).
//int inflowParaType = 2;
//double refDimensionalTemperature = 6051.024; //the total temperature, T*(1+(gama0-1)*M*M/2).
//double refDimensionalPressure = 4.299696E09; //the total pressure, p*(T0/T)^(gama0/(gama0-1)).
double gridScaleFactor = 0.001;
double gridScaleFactor = 0.001;
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
double forceRefenenceLength = 1.0; // unit of meter.
@ -69,7 +69,7 @@ double TorqueRefZ = 0.0; // unit of meter.
#*******************************************************************
# Physical models *
#*******************************************************************
// iviscous: Viscous model
// viscousType: Viscous model
// 0 - Euler
// 1 - Lamilar
// 3 - 1eq turbulent
@ -83,22 +83,22 @@ double TorqueRefZ = 0.0; // unit of meter.
// 2 - DDES;
// 3 - IDDES;
//int iviscous = 0;
//string viscousName = "Euler";
//int viscousType = 0;
//string viscousName = "Euler";
int viscousType = 1;
string viscousName = "laminar";
string viscousName = "laminar";
//int iviscous = 3;
//string viscousName = "1eq-sa";
//int viscousType = 3;
//string viscousName = "1eq-sa";
//int iviscous = 4;
//string viscousName = "2eq-kw-menter-sst";
//int viscousType = 4;
//string viscousName = "2eq-kw-menter-sst";
int DESType = 0;
int DESType = 0;
int roeEntropyFixMethod = 2;
double roeEntropyScale = 0.0002;
int roeEntropyFixMethod = 2;
double roeEntropyScale = 0.0002;
#########################################################################
# Spatial Discretisation #
#########################################################################
@ -111,7 +111,7 @@ double roeEntropyScale = 0.0002;
// str_limiter_name: Limiter of struct grid
// - "minmod", "3rd_minmod_smooth"
string inviscidSchemeName = "roe";
string inviscidSchemeName = "roe";
string str_limiter_name = "smooth";
#*******************************************************************
@ -130,7 +130,7 @@ string str_limiter_name = "smooth";
string uns_scheme_name = "vanleer";
string uns_limiter_name = "vencat";
double venkatCoeff = 0.5;
double venkatCoeff = 0.5;
#########################################################################
# Temporal Discretisation #
@ -142,11 +142,11 @@ double venkatCoeff = 0.5;
// The bigger the value, the convergence faster but lower robustness.
// ktmax: The lower the value, the more robustness, 1.0e5 ~ 1.0e10.
int iunsteady = 0;
int iunsteady = 0;
double CFLEnd = 100;
int CFLVaryStep = 500;
double ktmax = 1.0e10;
int CFLVaryStep = 500;
double ktmax = 1.0e10;
#########################################################################
@ -159,8 +159,8 @@ double ktmax = 1.0e10;
// Please use 'rae2822_hybrid2d__4.fts' here!
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0/1.
string gridfile = "./grid/plate_137_97.fts";
int isPlotVolumeField = 0;
string gridfile = "./grid/plate_137_97.fts";
int isPlotVolumeField = 0;
@ -175,7 +175,7 @@ int isPlotVolumeField = 0;
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!.
// Arriables order must from small to larger.
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// limitVariables: limit model.
// 0 - limit only for pressure and denstiny, then get the min value
@ -186,8 +186,8 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// reconmeth:
// 0 - When reconstruct face value, Q+, Q- use respective limiter coefficients.
// 1 - Q+, Q- use the min limiter coefficients of left and right cell.
int reconmeth = 0;
int limitVariables = 0;
int limitVector = 1;
int reconmeth = 0;
int limitVariables = 0;
int limitVector = 1;
double MUSCLCoefXk = 0.333333;

8
TwoD_Plate_Laminar_Ma5_Struct_1CPU/bin/grid_para.hypara
View File

@ -17,9 +17,9 @@
// 6 -- Ustar, mgrid.in.
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
// 8 -- GMSH, *.msh.
int gridtype = 1;
int axisup = 1;
int from_gtype = 3;
int gridtype = 1;
int axisup = 1;
int from_gtype = 3;
#########################################################################
# File path #
@ -27,7 +27,7 @@ int from_gtype = 3;
// from_gfile: path of original data file for unstructure grid convert from.
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
string from_gfile = "./grid/plate_137_97.grd";
string out_gfile = "./grid/plate_137_97.fts";
string out_gfile = "./grid/plate_137_97.fts";

48
TwoD_Plate_Laminar_Ma5_Struct_1CPU/bin/key.hypara
View File

@ -13,30 +13,30 @@ string defaultParaFile = "./bin/cfd_para.hypara";
// 2 -- Wall distance computation for turb-solver.
// 3 -- Grid partition.
// 4 -- Knowledge repository / examples of PHengLEI-API.
int ndim = 2;
int nparafile = 1;
int nsimutask = 0;
string parafilename = "./bin/cfd_para_hypersonic.hypara";
//string parafilename = "./bin/cfd_para_transonic.hypara";
//string parafilename = "./bin/cfd_para_supersonic.hypara";
//string parafilename = "./bin/cfd_para_hypersonic.hypara";
//string parafilename = "./bin/incompressible.hypara";
//int nsimutask = 1;
//string parafilename = "./bin/grid_para.hypara";
//int nsimutask = 2;
//string parafilename = "./bin/cfd_para.hypara";
//int nsimutask = 3;
//string parafilename = "./bin/partition.hypara";
//int nsimutask = 4;
//string parafilename = "./bin/repository.hypara";
//int nsimutask = 5;
//string parafilename = "./bin/overset_grid_view.hypara";
//int nsimutask = 99;
//string parafilename = "./bin/post_processing.hypara";
int ndim = 2;
int nparafile = 1;
int nsimutask = 0;
string parafilename = "./bin/cfd_para_hypersonic.hypara";
//string parafilename = "./bin/cfd_para_transonic.hypara";
//string parafilename = "./bin/cfd_para_supersonic.hypara";
//string parafilename = "./bin/cfd_para_hypersonic.hypara";
//string parafilename = "./bin/incompressible.hypara";
//int nsimutask = 1;
//string parafilename = "./bin/grid_para.hypara";
//int nsimutask = 2;
//string parafilename = "./bin/cfd_para.hypara";
//int nsimutask = 3;
//string parafilename = "./bin/partition.hypara";
//int nsimutask = 4;
//string parafilename = "./bin/repository.hypara";
//int nsimutask = 5;
//string parafilename = "./bin/overset_grid_view.hypara";
//int nsimutask = 99;
//string parafilename = "./bin/post_processing.hypara";
// ---------------- advanced Parameters, DO NOT care it -----------
int iovrlap = 0;
int numberOfGridProcessor = 0;
int iovrlap = 0;
int numberOfGridProcessor = 0;
// ATP read
string parafilename1 = ""
string parafilename2 = "";
string parafilename1 = ""
string parafilename2 = "";

10
TwoD_Plate_Laminar_Ma5_Struct_1CPU/bin/partition.hypara
View File

@ -8,16 +8,16 @@
// original_grid_file : original grid file that want to be divided(HyperFLOW/PHengLEI type, *.fts).
// partition_grid_file : target partition grid file(HyperFLOW/PHengLEI type, *.fts).
int pgridtype = 1;
int maxproc = 1;
int pgridtype = 1;
int maxproc = 1;
string original_grid_file = "./grid/plate_137_97.fts";
string partition_grid_file = "./grid/plate_137_97.fts";
string original_grid_file = "./grid/plate_137_97.fts";
string partition_grid_file = "./grid/plate_137_97.fts";
// Number of multi-grid levels, ONLY used for structured grid.
// 1 -- single level, 2 -- 2 level, N -- N level, ..., et al.
int numberOfMultigrid = 1;
int numberOfMultigrid = 1;

96
TwoD_Plate_Laminar_Struct_1CPU/bin/cfd_para_subsonic.hypara
View File

@ -7,19 +7,19 @@
// intervalStepForce: the step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: the step intervals for residual 'res.dat' saved.
int maxSimuStep = 150000;
int maxSimuStep = 150000;
int intervalStepFlow = 1000;
int intervalStepPlot = 1000;
int intervalStepForce = 100;
int intervalStepRes = 10;
int intervalStepFlow = 1000;
int intervalStepPlot = 1000;
int intervalStepForce = 100;
int intervalStepRes = 10;
// ifLowSpeedPrecon: precondition to accelerate convergence for low speed flow.
// ONLY available for unstructured solver!
// 0 -- no precondition process (default, mach > 0.2).
// 1 -- carry out precondition process ( mach number < 0.2 ).
int ifLowSpeedPrecon = 0;
int ifLowSpeedPrecon = 0;
#########################################################################
# Inflow Parameter #
@ -38,30 +38,30 @@ int ifLowSpeedPrecon = 0;
// forceRefenenceLength, forceRefenenceArea: Reference length and area, independent to grid scale.
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent to grid scale.
double refMachNumber = 0.1;
double attackd = 0.00;
double angleSlide = 0.00;
double refMachNumber = 0.1;
double attackd = 0.00;
double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 2.0e5;
double refDimensionalTemperature = 288.15;
int inflowParaType = 0;
double refReNumber = 2.0e5;
double refDimensionalTemperature = 288.15;
//int inflowParaType = 1;
//double height = 0.001;
//int inflowParaType = 1;
//double height = 0.001;
double gridScaleFactor = 1.0;
double gridScaleFactor = 1.0;
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
double forceRefenenceLength = 1.0; // unit of meter.
double forceRefenenceArea = 1.0; // unit of meter^2
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.
double forceRefenenceLength = 1.0; // unit of meter.
double forceRefenenceArea = 1.0; // unit of meter^2
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.
#*******************************************************************
# Physical models *
#*******************************************************************
// iviscous: Viscous model
// viscousType: Viscous model
// 0 - Euler
// 1 - Lamilar
// 3 - 1eq turbulent
@ -75,22 +75,22 @@ double TorqueRefZ = 0.0; // unit of meter.
// 2 - DDES;
// 3 - IDDES;
//int iviscous = 0;
//string viscousName = "Euler";
//int viscousType = 0;
//string viscousName = "Euler";
int viscousType = 1;
string viscousName = "laminar";
int viscousType = 1;
string viscousName = "laminar";
//int iviscous = 3;
//string viscousName = "1eq-sa";
//int viscousType = 3;
//string viscousName = "1eq-sa";
//int iviscous = 4;
//string viscousName = "2eq-kw-menter-sst";
//int viscousType = 4;
//string viscousName = "2eq-kw-menter-sst";
int DESType = 0;
int DESType = 0;
int roeEntropyFixMethod = 2;
double roeEntropyScale = 1.0;
int roeEntropyFixMethod = 2;
double roeEntropyScale = 1.0;
#########################################################################
# Spatial Discretisation #
#########################################################################
@ -101,7 +101,7 @@ double roeEntropyScale = 1.0;
// - "3rdsmooth", "smooth"
// - "nolim" - no limiter
string str_limiter_name = "nolim";
string str_limiter_name = "nolim";
#*******************************************************************
# UnStruct Solver *
@ -113,8 +113,8 @@ string str_limiter_name = "nolim";
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'
// The smaller the value, the more robust it is.
string uns_limiter_name = "vencat";
double venkatCoeff = 50.0;
string uns_limiter_name = "vencat";
double venkatCoeff = 50.0;
#########################################################################
# Temporal Discretisation #
@ -128,11 +128,11 @@ double venkatCoeff = 50.0;
// 1 : is recommended for structured solver.
// 1-3: is recommended for unstructured solver.
int iunsteady = 0;
int iunsteady = 0;
double CFLEnd = 100.0;
double CFLEnd = 100.0;
int nLUSGSSweeps = 1;
int nLUSGSSweeps = 1;
#########################################################################
# Multi-Grid parameters #
@ -144,8 +144,8 @@ int nLUSGSSweeps = 1;
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
int nMGLevel = 1;
int flowInitStep = 100;
int nMGLevel = 1;
int flowInitStep = 100;
#########################################################################
@ -158,8 +158,8 @@ int flowInitStep = 100;
// Please use 'rae2822_hybrid2d__4.fts' here!
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0/1.
string gridfile = "./grid/flat_laminar_73_81.fts";
int isPlotVolumeField = 0;
string gridfile = "./grid/flat_laminar_73_81.fts";
int isPlotVolumeField = 0;
// ---------------- advanced Parameters, DO NOT care it -----------
@ -172,8 +172,8 @@ int isPlotVolumeField = 0;
// -- modeledTKE(18),modeleddissipationrate(19), SSTF1(20), SSTF2(21)
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!.
// Arriables order must from small to larger.
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// limitVariables: limit model.
// 0 - limit only for pressure and denstiny, then get the min value
@ -184,10 +184,10 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// reconmeth:
// 0 - When reconstruct face value, Q+, Q- use respective limiter coefficients.
// 1 - Q+, Q- use the min limiter coefficients of left and right cell.
int reconmeth = 1;
int limitVariables = 0;
int limitVector = 0;
int reconmeth = 1;
int limitVariables = 0;
int limitVector = 0;
double MUSCLCoefXk = 0.333333;
double MUSCLCoefXk = 0.333333;

10
TwoD_Plate_Laminar_Struct_1CPU/bin/grid_para.hypara
View File

@ -17,17 +17,17 @@
// 6 -- Ustar, mgrid.in.
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
// 8 -- GMSH, *.msh.
int gridtype = 1;
int axisup = 1;
int from_gtype = 3;
int gridtype = 1;
int axisup = 1;
int from_gtype = 3;
#########################################################################
# File path #
#########################################################################
// from_gfile: path of original data file for unstructure grid convert from.
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
string from_gfile = "./grid/flat_laminar_73_81.grd";
string out_gfile = "./grid/flat_laminar_73_81.fts";
string from_gfile = "./grid/flat_laminar_73_81.grd";
string out_gfile = "./grid/flat_laminar_73_81.fts";

48
TwoD_Plate_Laminar_Struct_1CPU/bin/key.hypara
View File

@ -13,29 +13,29 @@ string defaultParaFile = "./bin/cfd_para.hypara";
// 2 -- Wall distance computation for turb-solver.
// 3 -- Grid partition.
// 4 -- Knowledge repository / examples of PHengLEI-API.
int ndim = 2;
int nparafile = 1;
int nsimutask = 0;
string parafilename="./bin/cfd_para_subsonic.hypara";
//string parafilename = "./bin/cfd_para_transonic.hypara";
//string parafilename = "./bin/cfd_para_supersonic.hypara";
//string parafilename = "./bin/cfd_para_hypersonic.hypara";
//string parafilename = "./bin/incompressible.hypara";
//int nsimutask = 1;
//string parafilename = "./bin/grid_para.hypara";
//int nsimutask = 2;
//string parafilename = "./bin/cfd_para.hypara";
//int nsimutask = 3;
//string parafilename = "./bin/partition.hypara";
//int nsimutask = 4;
//string parafilename = "./bin/repository.hypara";
//int nsimutask = 5;
//string parafilename = "./bin/overset_grid_view.hypara";
//int nsimutask = 99;
//string parafilename = "./bin/post_processing.hypara";
int ndim = 2;
int nparafile = 1;
int nsimutask = 0;
string parafilename = "./bin/cfd_para_subsonic.hypara";
//string parafilename = "./bin/cfd_para_transonic.hypara";
//string parafilename = "./bin/cfd_para_supersonic.hypara";
//string parafilename = "./bin/cfd_para_hypersonic.hypara";
//string parafilename = "./bin/incompressible.hypara";
//int nsimutask = 1;
//string parafilename = "./bin/grid_para.hypara";
//int nsimutask = 2;
//string parafilename = "./bin/cfd_para.hypara";
//int nsimutask = 3;
//string parafilename = "./bin/partition.hypara";
//int nsimutask = 4;
//string parafilename = "./bin/repository.hypara";
//int nsimutask = 5;
//string parafilename = "./bin/overset_grid_view.hypara";
//int nsimutask = 99;
//string parafilename = "./bin/post_processing.hypara";
// ---------------- advanced Parameters, DO NOT care it -----------
int iovrlap = 0;
int numberOfGridProcessor = 0;
int iovrlap = 0;
int numberOfGridProcessor = 0;
// ATP read
string parafilename1 = "./bin/cfd_para.hypara"
string parafilename2 = "./bin/cfd_para.hypara";
string parafilename1 = "./bin/cfd_para.hypara"
string parafilename2 = "./bin/cfd_para.hypara";

10
TwoD_Plate_Laminar_Struct_1CPU/bin/partition.hypara
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@ -8,16 +8,16 @@
// original_grid_file : original grid file that want to be divided(HyperFLOW/PHengLEI type, *.fts).
// partition_grid_file : target partition grid file(HyperFLOW/PHengLEI type, *.fts).
int pgridtype = 1;
int maxproc = 1;
int pgridtype = 1;
int maxproc = 1;
string original_grid_file = "./grid/flat_laminar_73_81.fts";
string partition_grid_file = "./grid/flat_laminar_73_81.fts";
string original_grid_file = "./grid/flat_laminar_73_81.fts";
string partition_grid_file = "./grid/flat_laminar_73_81.fts";
// Number of multi-grid levels, ONLY used for structured grid.
// 1 -- single level, 2 -- 2 level, N -- N level, ..., et al.
int numberOfMultigrid = 1;
int numberOfMultigrid = 1;

100
TwoD_Plate_SST_Ma5_Struct_1CPU/bin/cfd_para_supersonic.hypara
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@ -7,12 +7,12 @@
// intervalStepForce: the step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: the step intervals for residual 'res.dat' saved.
int maxSimuStep = 20000;
int maxSimuStep = 20000;
int intervalStepFlow = 2000;
int intervalStepPlot = 2000;
int intervalStepForce = 100;
int intervalStepRes = 10;
int intervalStepFlow = 2000;
int intervalStepPlot = 2000;
int intervalStepForce = 100;
int intervalStepRes = 10;
#########################################################################
# Inflow Parameter #
@ -39,37 +39,37 @@ int intervalStepRes = 10;
// forceRefenenceLength, forceRefenenceArea: Reference length and area, independent to grid scale.
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent to grid scale.
double refMachNumber = 5.00;
double attackd = 0.00;
double angleSlide = 0.00;
double refMachNumber = 5.00;
double attackd = 0.00;
double angleSlide = 0.00;
double wallTemperature = 327.36;
int dump_Q = 0;
double wallTemperature = 327.36;
int dump_Q = 0;
int inflowParaType = 0;
double refReNumber = 1.5e7;
double refDimensionalTemperature = 300.33;
int inflowParaType = 0;
double refReNumber = 1.5e7;
double refDimensionalTemperature = 300.33;
//int inflowParaType = 1;
//double height = 0.001;
//int inflowParaType = 1;
//double height = 0.001;
//int inflowParaType = 2;
//double refDimensionalTemperature = 6051.024; //the total temperature, T*(1+(gama0-1)*M*M/2).
//double refDimensionalPressure = 4.299696E09; //the total pressure, p*(T0/T)^(gama0/(gama0-1)).
//int inflowParaType = 2;
//double refDimensionalTemperature = 6051.024; //the total temperature, T*(1+(gama0-1)*M*M/2).
//double refDimensionalPressure = 4.299696E09; //the total pressure, p*(T0/T)^(gama0/(gama0-1)).
double gridScaleFactor = 0.001;
double gridScaleFactor = 0.001;
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
double forceRefenenceLength = 1.0; // unit of meter.
double forceRefenenceArea = 2.0; // unit of meter^2
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.
double forceRefenenceLength = 1.0; // unit of meter.
double forceRefenenceArea = 2.0; // unit of meter^2
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.
#*******************************************************************
# Physical models *
#*******************************************************************
// iviscous: Viscous model
// viscousType: Viscous model
// 0 - Euler
// 1 - Lamilar
// 3 - 1eq turbulent
@ -83,22 +83,22 @@ double TorqueRefZ = 0.0; // unit of meter.
// 2 - DDES;
// 3 - IDDES;
//int iviscous = 0;
//string viscousName = "Euler";
//int viscousType = 0;
//string viscousName = "Euler";
//int iviscous = 1;
//string viscousName = "laminar";
//int viscousType = 1;
//string viscousName = "laminar";
//int iviscous = 3;
//string viscousName = "1eq-sa";
//int viscousType = 3;
//string viscousName = "1eq-sa";
int viscousType = 4;
string viscousName = "2eq-kw-menter-sst";
string viscousName = "2eq-kw-menter-sst";
int DESType = 0;
int DESType = 0;
int roeEntropyFixMethod = 2;
double roeEntropyScale = 1.0;
int roeEntropyFixMethod = 2;
double roeEntropyScale = 1.0;
#########################################################################
# Spatial Discretisation #
#########################################################################
@ -111,8 +111,8 @@ double roeEntropyScale = 1.0;
// str_limiter_name: Limiter of struct grid
// - "minmod", "3rd_minmod_smooth"
string inviscidSchemeName = "roe";
string str_limiter_name = "smooth";
string inviscidSchemeName = "roe";
string str_limiter_name = "smooth";
#*******************************************************************
# UnStruct Solver *
@ -128,9 +128,9 @@ string str_limiter_name = "smooth";
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'
// The smaller the value, the more robust it is.
string uns_scheme_name = "vanleer";
string uns_limiter_name = "vencat";
double venkatCoeff = 0.5;
string uns_scheme_name = "vanleer";
string uns_limiter_name = "vencat";
double venkatCoeff = 0.5;
#########################################################################
# Temporal Discretisation #
@ -142,11 +142,11 @@ double venkatCoeff = 0.5;
// The bigger the value, the convergence faster but lower robustness.
// ktmax: The lower the value, the more robustness, 1.0e5 ~ 1.0e10.
int iunsteady = 0;
int iunsteady = 0;
double CFLEnd = 50.0;
double CFLEnd = 50.0;
double ktmax = 1.0e10;
double ktmax = 1.0e10;
#########################################################################
@ -159,8 +159,8 @@ double ktmax = 1.0e10;
// Please use 'rae2822_hybrid2d__4.fts' here!
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0/1.
string gridfile = "./grid/Mesh4_137_97.fts";
int isPlotVolumeField = 0;
string gridfile = "./grid/Mesh4_137_97.fts";
int isPlotVolumeField = 0;
@ -174,8 +174,8 @@ int isPlotVolumeField = 0;
// -- modeledTKE(18),modeleddissipationrate(19), SSTF1(20), SSTF2(21)
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!.
// Arriables order must from small to larger.
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// limitVariables: limit model.
// 0 - limit only for pressure and denstiny, then get the min value
@ -186,8 +186,8 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// reconmeth:
// 0 - When reconstruct face value, Q+, Q- use respective limiter coefficients.
// 1 - Q+, Q- use the min limiter coefficients of left and right cell.
int reconmeth = 0;
int limitVariables = 0;
int limitVector = 1;
int reconmeth = 0;
int limitVariables = 0;
int limitVector = 1;
double MUSCLCoefXk = 0.333333;

10
TwoD_Plate_SST_Ma5_Struct_1CPU/bin/grid_para.hypara
View File

@ -17,17 +17,17 @@
// 6 -- Ustar, mgrid.in.
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
// 8 -- GMSH, *.msh.
int gridtype = 1;
int axisup = 1;
int from_gtype = 3;
int gridtype = 1;
int axisup = 1;
int from_gtype = 3;
#########################################################################
# File path #
#########################################################################
// from_gfile: path of original data file for unstructure grid convert from.
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
string from_gfile = "./grid/Mesh4_137_97.grd";
string out_gfile = "./grid/Mesh4_137_97.fts";
string from_gfile = "./grid/Mesh4_137_97.grd";
string out_gfile = "./grid/Mesh4_137_97.fts";

48
TwoD_Plate_SST_Ma5_Struct_1CPU/bin/key.hypara
View File

@ -13,30 +13,30 @@ string defaultParaFile = "./bin/cfd_para.hypara";
// 2 -- Wall distance computation for turb-solver.
// 3 -- Grid partition.
// 4 -- Knowledge repository / examples of PHengLEI-API.
int ndim = 2;
int nparafile = 1;
int nsimutask = 0;
string parafilename = "./bin/cfd_para_supersonic.hypara";
//string parafilename = "./bin/cfd_para_transonic.hypara";
//string parafilename = "./bin/cfd_para_supersonic.hypara";
//string parafilename = "./bin/cfd_para_hypersonic.hypara";
//string parafilename = "./bin/incompressible.hypara";
//int nsimutask = 1;
//string parafilename = "./bin/grid_para.hypara";
//int nsimutask = 2;
//string parafilename = "./bin/cfd_para.hypara";
//int nsimutask = 3;
//string parafilename = "./bin/partition.hypara";
//int nsimutask = 4;
//string parafilename = "./bin/repository.hypara";
//int nsimutask = 5;
//string parafilename = "./bin/overset_grid_view.hypara";
//int nsimutask = 99;
//string parafilename = "./bin/post_processing.hypara";
int ndim = 2;
int nparafile = 1;
int nsimutask = 0;
string parafilename = "./bin/cfd_para_supersonic.hypara";
//string parafilename = "./bin/cfd_para_transonic.hypara";
//string parafilename = "./bin/cfd_para_supersonic.hypara";
//string parafilename = "./bin/cfd_para_hypersonic.hypara";
//string parafilename = "./bin/incompressible.hypara";
//int nsimutask = 1;
//string parafilename = "./bin/grid_para.hypara";
//int nsimutask = 2;
//string parafilename = "./bin/cfd_para.hypara";
//int nsimutask = 3;
//string parafilename = "./bin/partition.hypara";
//int nsimutask = 4;
//string parafilename = "./bin/repository.hypara";
//int nsimutask = 5;
//string parafilename = "./bin/overset_grid_view.hypara";
//int nsimutask = 99;
//string parafilename = "./bin/post_processing.hypara";
// ---------------- advanced Parameters, DO NOT care it -----------
int iovrlap = 0;
int numberOfGridProcessor = 0;
int iovrlap = 0;
int numberOfGridProcessor = 0;
// ATP read
string parafilename1 = ""
string parafilename2 = "";
string parafilename1 = ""
string parafilename2 = "";

10
TwoD_Plate_SST_Ma5_Struct_1CPU/bin/partition.hypara
View File

@ -8,16 +8,16 @@
// original_grid_file : original grid file that want to be divided(HyperFLOW/PHengLEI type, *.fts).
// partition_grid_file : target partition grid file(HyperFLOW/PHengLEI type, *.fts).
int pgridtype = 1;
int maxproc = 1;
int pgridtype = 1;
int maxproc = 1;
string original_grid_file = "./grid/Mesh4_137_97.fts";
string partition_grid_file = "./grid/Mesh4_137_97.fts";
string original_grid_file = "./grid/Mesh4_137_97.fts";
string partition_grid_file = "./grid/Mesh4_137_97.fts";
// Number of multi-grid levels, ONLY used for structured grid.
// 1 -- single level, 2 -- 2 level, N -- N level, ..., et al.
int numberOfMultigrid = 1;
int numberOfMultigrid = 1;

10
TwoD_Plate_Subsonic_TotalPressTempBC_Structure_SA_4CPU/bin/cfd_para_subsonic.hypara
View File

@ -84,16 +84,16 @@ double TorqueRefZ = 0.0; // unit of meter.
// 2 -- DDES.
// 3 -- IDDES.
//int viscousType = 0;
//int viscousType = 0;
//string viscousName = "Euler";
//int viscousType = 1;
//int viscousType = 1;
//string viscousName = "laminar";
int viscousType = 3;
int viscousType = 3;
string viscousName = "1eq-sa";
//int viscousType = 4;
//int viscousType = 4;
//string viscousName = "2eq-kw-menter-sst";
int DESType = 0;
@ -110,7 +110,7 @@ double roeEntropyScale = 1.0;
// -- "3rdsmooth", "smooth".
// -- "nolim", no limiter.
string str_limiter_name = "smooth";
string str_limiter_name = "smooth";
#*******************************************************************
# UnStruct Solver *

10
TwoD_Rae2822_SST_Struct/bin/cfd_para_transonic.hypara
View File

@ -80,17 +80,17 @@ double TorqueRefZ = 0.0; // unit of meter.
// 2 -- DDES.
// 3 -- IDDES.
//int viscousType = 0;
//int viscousType = 0;
//string viscousName = "Euler";
//int viscousType = 1;
//int viscousType = 1;
//string viscousName = "laminar";
//int viscousType = 3;
//int viscousType = 3;
//string viscousName = "1eq-sa";
int viscousType = 4;
string viscousName = "2eq-kw-menter-sst";
int viscousType = 4;
string viscousName = "2eq-kw-menter-sst";
int DESType = 0;

10
TwoD_Rae2822_SST_Struct/bin/grid_para.hypara
View File

@ -17,17 +17,17 @@
// 6 -- Ustar, mgrid.in.
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
// 8 -- GMSH, *.msh.
int gridtype = 1;
int axisup = 1;
int from_gtype = 3;
int gridtype = 1;
int axisup = 1;
int from_gtype = 3;
#########################################################################
# File path #
#########################################################################
// from_gfile: path of original data file for unstructure grid convert from.
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
string from_gfile = "./grid/rae2822_vis2d.grd";
string out_gfile = "./grid/rae2822_vis2d.fts";
string from_gfile = "./grid/rae2822_vis2d.grd";
string out_gfile = "./grid/rae2822_vis2d.fts";

48
TwoD_Rae2822_SST_Struct/bin/key.hypara
View File

@ -15,37 +15,37 @@ string defaultParaFile = "./bin/cfd_para.hypara";
// 2 -- Wall distance computation for turb-solver.
// 3 -- Grid partition.
// 4 -- Knowledge repository / examples of PHengLEI-API.
int ndim = 2;
int nparafile = 1;
int ndim = 2;
int nparafile = 1;
int nsimutask = 0;
string parafilename = "./bin/cfd_para_transonic.hypara";
//string parafilename = "./bin/cfd_para_transonic.hypara";
//string parafilename = "./bin/cfd_para_supersonic.hypara";
//string parafilename = "./bin/cfd_para_hypersonic.hypara";
//string parafilename = "./bin/incompressible.hypara";
int nsimutask = 0;
string parafilename = "./bin/cfd_para_transonic.hypara";
//string parafilename = "./bin/cfd_para_transonic.hypara";
//string parafilename = "./bin/cfd_para_supersonic.hypara";
//string parafilename = "./bin/cfd_para_hypersonic.hypara";
//string parafilename = "./bin/incompressible.hypara";
//int nsimutask = 1;
//string parafilename = "./bin/grid_para.hypara";
//int nsimutask = 1;
//string parafilename = "./bin/grid_para.hypara";
//int nsimutask = 2;
//string parafilename = "./bin/cfd_para.hypara";
//int nsimutask = 2;
//string parafilename = "./bin/cfd_para.hypara";
//int nsimutask = 3;
//string parafilename = "./bin/partition.hypara";
//int nsimutask = 3;
//string parafilename = "./bin/partition.hypara";
//int nsimutask = 4;
//string parafilename = "./bin/repository.hypara";
//int nsimutask = 4;
//string parafilename = "./bin/repository.hypara";
//int nsimutask = 5;
//string parafilename = "./bin/overset_grid_view.hypara";
//int nsimutask = 5;
//string parafilename = "./bin/overset_grid_view.hypara";
//int nsimutask = 99;
//string parafilename = "./bin/post_processing.hypara";
//int nsimutask = 99;
//string parafilename = "./bin/post_processing.hypara";
// ---------------- advanced Parameters, DO NOT care it -----------
int iovrlap = 0;
int numberOfGridProcessor = 0;
int iovrlap = 0;
int numberOfGridProcessor = 0;
// ATP read
//@string parafilename1 = ""
//@string parafilename2 = "";
//@string parafilename1 = ""
//@string parafilename2 = "";

10
TwoD_Rae2822_SST_Struct/bin/partition.hypara
View File

@ -8,16 +8,16 @@
// original_grid_file : original grid file that want to be divided(HyperFLOW/PHengLEI type, *.fts).
// partition_grid_file : target partition grid file(HyperFLOW/PHengLEI type, *.fts).
int pgridtype = 1;
int maxproc = 4;
int pgridtype = 1;
int maxproc = 4;
string original_grid_file = "./grid/rae2822_vis2d.fts";
string partition_grid_file = "./grid/rae2822_vis2d__4.fts";
string original_grid_file = "./grid/rae2822_vis2d.fts";
string partition_grid_file = "./grid/rae2822_vis2d__4.fts";
// Number of multi-grid levels, ONLY used for structured grid.
// 1 -- single level, 2 -- 2 level, N -- N level, ..., et al.
int numberOfMultigrid = 1;
int numberOfMultigrid = 1;