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添加A24-A29,F11新算例；修改A13、A15参数、更新README

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hechao 2022-06-29 23:33:27 +08:00
parent edab4af668
commit 35fd719b7a
56 changed files with 12078 additions and 95 deletions
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A13_TwoD_BackwardStep_PressureOutlet_SA_Struct_4CPU/bin/boundary_condition.hypara
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# nBoundaryConditions : number of global boundary conditions.
# bcName : Boundary Condition Name.
# bcType(in PHengLEI): Boundary Condition Type.
# Account of how to set boundarycondition.
# string bcName = "Farfield";
# {
# int bcType = 4;
# int inflowParaType = 1;
# double attackd = 0;
# double refReNumber = 6.5e6;
# double refMachNumber = 3.5;
# double angleSlide = 0;
# }
int nBoundaryConditions = 4;
string bcName = "SOLID_SURFACE";
{
int bcType = 2;
}
string bcName = "SYMMETRY";
{
int bcType = 3;
}
string bcName = "FARFIELD";
{
int bcType = 4;
}
string bcName = "OUTFLOW";
{
int bcType = 6;
}
# 'bcType' is defined as following:
# 99: PERIODIC
# -2: WAKE
# -1: INTERFACE
# 0 : NO_BOUNDARY_CONDITION
# 1 : EXTRAPOLATION
# 2 : SOLID_SURFACE
# 3 : SYMMETRY
# 4 : FARFIELD
# 5 : INFLOW
# 6 : OUTFLOW
# 52: PRESSURE_INLET
# 62: PRESSURE_OUTLET
# 61: OUTFLOW_CONFINED
# 7 : POLE

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A15_ThreeD_ShockWave_PeriodicBoundary_SA_Struct_4CPU/bin/boundary_condition.hypara
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# nBoundaryConditions : number of global boundary conditions.
# bcName : Boundary Condition Name.
# bcType(in PHengLEI): Boundary Condition Type.
# Account of how to set boundarycondition.
# string bcName = "Farfield";
# {
# int bcType = 4;
# int inflowParaType = 1;
# double attackd = 0;
# double refReNumber = 6.5e6;
# double refMachNumber = 3.5;
# double angleSlide = 0;
# }
int nBoundaryConditions = 3;
string bcName = "Wall_viscous";
{
int bcType = 2;
}
string bcName = "Farfield";
{
int bcType = 4;
}
string bcName = "Outflow";
{
int bcType = 6;
}
# 'bcType' is defined as following:
# 99: PERIODIC
# -2: WAKE
# -1: INTERFACE
# 0 : NO_BOUNDARY_CONDITION
# 1 : EXTRAPOLATION
# 2 : SOLID_SURFACE
# 3 : SYMMETRY
# 4 : FARFIELD
# 5 : INFLOW
# 6 : OUTFLOW
# 52: PRESSURE_INLET
# 62: PRESSURE_OUTLET
# 61: OUTFLOW_CONFINED
# 7 : POLE

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A24_TwoD_30p30n_SA_MatrixLUSGS_Struct_4CPU/bin/cfd_para.hypara Normal file
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A24_TwoD_30p30n_SA_MatrixLUSGS_Struct_4CPU/bin/cfd_para_subsonic.hypara Normal file
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#########################################################################
# General Control Parameter #
#########################################################################
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual 'res.dat' saved.
int maxSimuStep = 60000;
int intervalStepFlow = 500;
int intervalStepPlot = 500;
int intervalStepForce = 50;
int intervalStepRes = 50;
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
// 0 -- no precondition process. (default, mach > 0.3)
// 1 -- carry out precondition process. (mach number <= 0.3)
int ifLowSpeedPrecon = 0;
#########################################################################
# Inflow Parameter #
#########################################################################
// refMachNumber: Mach number.
// attackd: Angle of attack.
// angleSlide: Angle of sideslip.
// inflowParaType: The type of inflow parameters.
// 0 -- the nondimensional conditions.
// 1 -- the flight conditions.
// 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions.
// 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.
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
// height: Fly height, unit of km.
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
// 1 dm = 0.1 m.
// 1 cm = 0.01 m.
// 1 mm = 0.001m.
// 1 inch = 0.0254m.
// 1 foot = 12 inches = 0.3048m.
// 1 yard = 3 feet = 0.9144m.
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit.
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
double refMachNumber = 0.2;
double attackd = 19.0;
double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 9.0e6;
double refDimensionalTemperature = 288.0;
//int inflowParaType = 1;
//double height = 0.001;
double gridScaleFactor = 1.0;
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 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 #
#########################################################################
// viscousType : Viscous model.
// 0 -- Euler.
// 1 -- Lamilar.
// 3 -- 1eq turbulent.
// 4 -- 2eq turbulent.
// viscousName: Laminar or tubulent model.
// -- "1eq-sa", when viscousType = 3.
// -- "2eq-kw-menter-sst", when viscousType = 4.
// DESType: Type of DES.
// 0 -- RANS.(default)
// 1 -- DES.
// 2 -- DDES.
// 3 -- IDDES.
//int viscousType = 0;
//string viscousName = "Euler";
//int viscousType = 1;
//string viscousName = "laminar";
int viscousType = 3;
string viscousName = "1eq-sa";
//int viscousType = 4;
//string viscousName = "2eq-kw-menter-sst";
int DESType = 0;
int roeEntropyFixMethod = 2;
double roeEntropyScale = 1.0;
#########################################################################
# Spatial Discretisation #
#########################################################################
#*******************************************************************
# Struct Solver *
#*******************************************************************
// str_limiter_name: Limiter of struct grid.
// -- "3rdsmooth", "smooth".
// -- "nolim", no limiter.
string str_limiter_name = "smooth";
double MUSCLCoefXk = 0.333333;
#*******************************************************************
# UnStruct Solver *
#*******************************************************************
// uns_limiter_name: Limiter of Unstruct grid.
// -- "vencat".
// -- "1st", meaning accuracy of first-order.
// -- "nolim", no limiter.
// 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;
#########################################################################
# Temporal Discretisation #
#########################################################################
// iunsteady: Steady or unsteady.
// 0 -- steady.
// 1 -- unsteay.
// CFLEnd: The CFL number, [0.1, 100].
// The bigger the value, the convergence faster but lower robustness.
// nLUSGSSweeps: Number of Sub-iteration of LU-SGS.
// 1 -- is recommended for structured solver.
// 1-3 -- is recommended for unstructured solver.
int iunsteady = 0;
double CFLEnd = 10.0;
int tscheme = 8;
int nLUSGSSweeps = 1;
#########################################################################
# Multi-Grid parameters #
#########################################################################
// nMGLevel: The number of Multi-Grid level.
// = 1 -- single-level.
// > 1 -- multi-level.
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
// 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;
#########################################################################
# File In or Out #
#########################################################################
// gridfile: The partitioned Grid file path, using relative path,
// which is relative to the working directory.
// IMPORTANT WARNING: The file index should be ignored,
// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
// Please use 'rae2822_hybrid2d__4.fts' here!
// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
string gridfile = "./grid/30p30n_str__4.fts";
int plotFieldType = 0;
// ----------------- Advanced Parameters, DO NOT care it ----------------
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables: Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
// -- viscosityLaminar(7), viscosityTurbulent(8),
// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12),
// -- strain_rate(13), Q_criteria(14), Cp(15), timeStep(16), volume(17),
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
// Variables order must from small to big.
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// limitVariables: Limit model (It is useful only if limitVector is 0).
// 0 -- limit only for pressure and denstiny, then get the min value.
// 1 -- limit for every variables, then get the min value.
// limitVector:
// 0 -- Each variable use the same limiter coefficient.
// 1 -- Each variable use the respective limiter coefficients.
// 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;

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A24_TwoD_30p30n_SA_MatrixLUSGS_Struct_4CPU/bin/grid_para.hypara Normal file
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#########################################################################
# Grid data type #
#########################################################################
// gridtype: Grid type for generation, conversion, reconstruction, merging.
// 0 -- Unstructured grid.
// 1 -- Structured grid.
// axisup: Type of Cartisien coordinates system, used in grid conversion.
// 1 -- Y upward. (default)
// 2 -- Z upward.
// from_gtype: Type of grid data type in grid conversion process.
// -1 -- MULTI_TYPE.
// 1 -- PHengLEI, *.fts.
// 2 -- CGNS, *.cgns.
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
// 5 -- Fluent, *.cas/*.msh.
// 6 -- Ustar, mgrid.in.
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
// 8 -- GMSH, *.msh.
// 9 -- Gridgen type of structured grid, *.dat/*.grd.
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/30p30n_str.grd";
string out_gfile = "./grid/30p30n_str.fts";

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string title = "PHengLEI Main Parameter Control File";
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
string defaultParaFile = "./bin/cfd_para.hypara";
// ndim: Dimensional of the grid, 2 or 3.
// nparafile: the number of parameter files.
// nsimutask: simulation task type.
// 0 -- CFD Solver of NS or Turbulation.
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
// Grid conversion: from other format to PHengLEI format (.fts).
// Grid reconstruction: such as grid adaptation.
// Grid merging: merge two blocks into one block.
// Grid repairing: repair the original grid in order to remove the negative volume cells.
// 2 -- Wall distance computation for turb-solver.
// 3 -- Grid partition.
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/cfd_para_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 = 1;
//string parafilename = "./bin/grid_deform_para.hypara";
//int nsimutask = 1;
//string parafilename = "./bin/grid_refine_para.hypara";
//int nsimutask = 14;
//string parafilename = "./bin/integrative_solver.hypara";
//int nsimutask = 99;
//string parafilename = "./bin/post_processing.hypara";
// ---------------- Advanced Parameters, DO NOT care it ----------------
int numberOfGridProcessor = 0;
// ATP read
//@string parafilename1 = ""
//@string parafilename2 = "";

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// pgridtype: The grid type.
// 0 -- unstruct grid.
// 1 -- struct grid.
// maxproc: The number of partition zones that want to be divided into,
// which is equal to the number of CPU processors you want.
// Usually, 50~100 thousands structured cells per CPU-Core is suggested.
// 30~70 thousands unstructured cells per CPU-Core is suggested.
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
// numberOfMultifile: The number of partition grid files that want to be dumped out.
int pgridtype = 1;
int maxproc = 4;
string original_grid_file = "./grid/30p30n_str.fts";
string partition_grid_file = "./grid/30p30n_str__4.fts";
int numberOfMultifile = 1;
// numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid.
// 1 -- single level.
// 2 -- 2 level.
// N -- N level,..., et al.
int numberOfMultigrid = 1;

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1
8
81 617
A
21
1 41 1 1 4
1 1 65 1 -1
353 353 -65 -1 7
1 1 65 129 -1
281 281 -1 -65 6
1 1 189 129 -1
121 121 -61 -1 8
1 1 221 189 -1
121 121 -93 -61 8
1 1 221 245 -1
121 121 -93 -117 8
1 1 309 245 -1
41 41 65 1 2
1 1 309 341 -1
41 41 -65 -97 2
1 1 -481 -553 -1
41 41 -65 -137 5
1 1 -481 -449 -1
41 41 -65 -33 5
1 1 -373 -449 -1
121 121 -33 -109 4
1 1 -341 -373 -1
121 121 -1 -33 4
41 1 617 617 4
1 1 -553 -617 -1
1 1 -65 -1 7
81 81 553 617 4
81 41 617 617 4
81 81 341 553 4
81 81 245 341 4
81 81 65 245 4
81 81 65 1 4
41 81 1 1 4
41 97
B
6
41 41 65 1 -1
1 1 309 245 1
-1 -41 1 1 -1
81 121 117 117 8
1 1 65 1 2
41 41 -65 -97 -1
1 1 309 341 1
1 1 97 65 2
1 41 97 97 -1
81 121 1 1 4
81 49
C
6
81 49 49 49 -1
81 49 1 1 4
81 81 1 49 2
81 49 1 1 -1
81 49 117 117 8
-1 -49 49 49 -1
1 49 1 1 4
1 1 49 1 2
-49 -1 1 1 -1
49 1 117 117 8
121 141
D
14
121 121 -1 -33 -1
1 1 -341 -373 1
81 121 1 1 -1
1 41 97 97 2
81 49 1 1 -1
81 49 49 49 3
1 1 33 1 2
1 49 1 1 -1
-1 -49 49 49 3
121 121 -33 -109 -1
1 1 -373 -449 1
1 1 77 33 2
1 1 93 77 2
1 1 109 93 2
1 1 125 109 2
1 1 -125 -141 -1
1 1 -17 -1 8
49 1 141 141 -1
113 161 65 65 6
-121 -49 141 141 -1
41 113 65 65 6
121 121 141 109 -1
41 41 -1 -33 5
41 137
E
8
41 41 -1 -33 -1
121 121 141 109 4
1 1 33 1 2
1 41 1 1 -1
1 41 65 65 6
41 41 -65 -33 -1
1 1 -481 -449 1
1 1 65 33 2
41 41 -65 -137 -1
1 1 -481 -553 1
1 1 137 65 2
41 1 137 137 -1
1 41 65 65 7
281 65
F
8
1 1 65 1 2
1 161 1 1 -1
73 233 65 65 7
113 161 65 65 -1
49 1 141 141 4
41 113 65 65 -1
-121 -49 141 141 4
1 41 65 65 -1
1 41 1 1 5
161 281 65 65 -1
1 121 1 1 8
281 281 -1 -65 -1
1 1 65 129 1
161 281 1 1 -1
233 353 65 65 7
353 65
G
7
1 1 -65 -1 -1
1 1 -553 -617 1
1 41 65 65 -1
41 1 137 137 5
73 41 65 65 2
73 233 65 65 -1
1 161 1 1 6
233 353 65 65 -1
161 281 1 1 6
353 353 -65 -1 -1
1 1 65 1 1
1 353 1 1 4
121 117
H
11
1 1 61 17 2
1 1 -17 -1 -1
1 1 -125 -141 4
1 121 1 1 -1
161 281 65 65 6
121 121 -61 -1 -1
1 1 189 129 1
1 1 93 61 2
121 121 -93 -61 -1
1 1 221 189 1
1 1 117 93 2
81 49 117 117 -1
81 49 1 1 3
49 1 117 117 -1
-49 -1 1 1 3
81 121 117 117 -1
-1 -41 1 1 2
121 121 -93 -117 -1
1 1 221 245 1

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A24_TwoD_30p30n_SA_MatrixLUSGS_Struct_4CPU/二维结构30p30n翼型低速绕流(Matrix LUSGS)算例说明文档.pdf Normal file
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#########################################################################
# General Control Parameter #
#########################################################################
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual 'res.dat' saved.
int maxSimuStep = 100000;
int intervalStepFlow = 5000;
int intervalStepPlot = 5000;
int intervalStepForce = 100;
int intervalStepRes = 100;
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
// 0 -- no precondition process. (default, mach > 0.3)
// 1 -- carry out precondition process. (mach number <= 0.3)
int ifLowSpeedPrecon = 0;
#########################################################################
# Inflow Parameter #
#########################################################################
// refMachNumber: Mach number.
// attackd: Angle of attack.
// angleSlide: Angle of sideslip.
// inflowParaType: The type of inflow parameters.
// 0 -- the nondimensional conditions.
// 1 -- the flight conditions.
// 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions.
// 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.
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
// height: Fly height, unit of km.
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
// 1 dm = 0.1 m.
// 1 cm = 0.01 m.
// 1 mm = 0.001m.
// 1 inch = 0.0254m.
// 1 foot = 12 inches = 0.3048m.
// 1 yard = 3 feet = 0.9144m.
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit.
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
double refMachNumber = 0.2;
double attackd = 0.00;
double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 5.0e6;
double refDimensionalTemperature = 288.15;
//int inflowParaType = 1;
//double height = 0.001;
double gridScaleFactor = 0.001;
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 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 #
#########################################################################
// viscousType : Viscous model.
// 0 -- Euler.
// 1 -- Lamilar.
// 3 -- 1eq turbulent.
// 4 -- 2eq turbulent.
// viscousName: Laminar or tubulent model.
// -- "1eq-sa", when viscousType = 3.
// -- "2eq-kw-menter-sst", when viscousType = 4.
// DESType: Type of DES.
// 0 -- RANS.(default)
// 1 -- DES.
// 2 -- DDES.
// 3 -- IDDES.
//int viscousType = 0;
//string viscousName = "Euler";
//int viscousType = 1;
//string viscousName = "laminar";
//int viscousType = 3;
//string viscousName = "1eq-sa";
int viscousType = 4;
string viscousName = "2eq-kw-menter-sst";
int DESType = 0;
int roeEntropyFixMethod = 2;
double roeEntropyScale = 1.0;
#########################################################################
# Spatial Discretisation #
#########################################################################
#*******************************************************************
# Struct Solver *
#*******************************************************************
// str_limiter_name: Limiter of struct grid.
// -- "3rdsmooth", "smooth".
// -- "nolim", no limiter.
string str_limiter_name = "nolim";
double MUSCLCoefXk =0.333333;
#*******************************************************************
# UnStruct Solver *
#*******************************************************************
// uns_limiter_name: Limiter of Unstruct grid.
// -- "vencat".
// -- "1st", meaning accuracy of first-order.
// -- "nolim", no limiter.
// 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;
#########################################################################
# Temporal Discretisation #
#########################################################################
// iunsteady: Steady or unsteady.
// 0 -- steady.
// 1 -- unsteay.
// CFLEnd: The CFL number, [0.1, 100].
// The bigger the value, the convergence faster but lower robustness.
// nLUSGSSweeps: Number of Sub-iteration of LU-SGS.
// 1 -- is recommended for structured solver.
// 1-3 -- is recommended for unstructured solver.
int iunsteady = 0;
double CFLEnd = 500.0;
int tscheme = 8;
int nLUSGSSweeps = 1;
#########################################################################
# Multi-Grid parameters #
#########################################################################
// nMGLevel: The number of Multi-Grid level.
// = 1 -- single-level.
// > 1 -- multi-level.
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
// 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;
#########################################################################
# File In or Out #
#########################################################################
// gridfile: The partitioned Grid file path, using relative path,
// which is relative to the working directory.
// IMPORTANT WARNING: The file index should be ignored,
// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
// Please use 'rae2822_hybrid2d__4.fts' here!
// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
string gridfile = "./grid/Mesh4_137_97.fts";
int plotFieldType = 0;
// ----------------- Advanced Parameters, DO NOT care it ----------------
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables: Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
// -- viscosityLaminar(7), viscosityTurbulent(8),
// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12),
// -- strain_rate(13), Q_criteria(14), Cp(15), timeStep(16), volume(17),
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
// Variables order must from small to big.
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// limitVariables: Limit model (It is useful only if limitVector is 0).
// 0 -- limit only for pressure and denstiny, then get the min value.
// 1 -- limit for every variables, then get the min value.
// limitVector:
// 0 -- Each variable use the same limiter coefficient.
// 1 -- Each variable use the respective limiter coefficients.
// 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;

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#########################################################################
# Grid data type #
#########################################################################
// gridtype: Grid type for generation, conversion, reconstruction, merging.
// 0 -- Unstructured grid.
// 1 -- Structured grid.
// axisup: Type of Cartisien coordinates system, used in grid conversion.
// 1 -- Y upward. (default)
// 2 -- Z upward.
// from_gtype: Type of grid data type in grid conversion process.
// -1 -- MULTI_TYPE.
// 1 -- PHengLEI, *.fts.
// 2 -- CGNS, *.cgns.
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
// 5 -- Fluent, *.cas/*.msh.
// 6 -- Ustar, mgrid.in.
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
// 8 -- GMSH, *.msh.
// 9 -- Gridgen type of structured grid, *.dat/*.grd.
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";

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string title = "PHengLEI Main Parameter Control File";
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
string defaultParaFile = "./bin/cfd_para.hypara";
// ndim: Dimensional of the grid, 2 or 3.
// nparafile: the number of parameter files.
// nsimutask: simulation task type.
// 0 -- CFD Solver of NS or Turbulation.
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
// Grid conversion: from other format to PHengLEI format (.fts).
// Grid reconstruction: such as grid adaptation.
// Grid merging: merge two blocks into one block.
// Grid repairing: repair the original grid in order to remove the negative volume cells.
// 2 -- Wall distance computation for turb-solver.
// 3 -- Grid partition.
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/cfd_para_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 = 1;
//string parafilename = "./bin/grid_deform_para.hypara";
//int nsimutask = 1;
//string parafilename = "./bin/grid_refine_para.hypara";
//int nsimutask = 14;
//string parafilename = "./bin/integrative_solver.hypara";
//int nsimutask = 99;
//string parafilename = "./bin/post_processing.hypara";
// ---------------- Advanced Parameters, DO NOT care it ----------------
int numberOfGridProcessor = 0;
// ATP read
//@string parafilename1 = ""
//@string parafilename2 = "";

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1
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137 97
A
5
1 25 1 1 3
25 137 1 1 2
137 137 1 97 6
1 137 97 97 4
1 1 1 97 4

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A25_TwoD_Plate_SST_LowMach_MatrixLUSGS_Struct_1CPU/二维结构低速湍流平板(Matrix LUSGS)算例说明文档.pdf Normal file
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#########################################################################
# General Control Parameter #
#########################################################################
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual 'res.dat' saved.
int maxSimuStep = 10000;
int intervalStepFlow = 500;
int intervalStepPlot = 500;
int intervalStepForce = 50;
int intervalStepRes = 50;
#########################################################################
# Inflow Parameter #
#########################################################################
// refMachNumber: Mach number.
// attackd: Angle of attack.
// angleSlide: Angle of sideslip.
// inflowParaType: The type of inflow parameters.
// 0 -- the nondimensional conditions.
// 1 -- the flight conditions.
// 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions.
// 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.
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
// height: Fly height, unit of km.
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
// 1 dm = 0.1 m.
// 1 cm = 0.01 m.
// 1 mm = 0.001m.
// 1 inch = 0.0254m.
// 1 foot = 12 inches = 0.3048m.
// 1 yard = 3 feet = 0.9144m.
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit.
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
double refMachNumber = 0.73;
double attackd = 2.31;
double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 6.5e6;
double refDimensionalTemperature = 288.15;
//int inflowParaType = 1;
//double height = 0.001;
//int inflowParaType = 2;
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
double gridScaleFactor = 1.0;
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 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 #
#########################################################################
// viscousType : Viscous model.
// 0 -- Euler.
// 1 -- Lamilar.
// 3 -- 1eq turbulent.
// 4 -- 2eq turbulent.
// viscousName: Laminar or tubulent model.
// -- "1eq-sa", when viscousType = 3.
// -- "2eq-kw-menter-sst", when viscousType = 4.
// DESType: Type of DES.
// 0 -- RANS.(default)
// 1 -- DES.
// 2 -- DDES.
// 3 -- IDDES.
//int viscousType = 0;
//string viscousName = "Euler";
//int viscousType = 1;
//string viscousName = "laminar";
int viscousType = 3;
string viscousName = "1eq-sa";
//int viscousType = 4;
//string viscousName = "2eq-kw-menter-sst";
int DESType = 0;
int roeEntropyFixMethod = 2;
double roeEntropyScale = 1.0;
#########################################################################
# Spatial Discretisation #
#########################################################################
#*******************************************************************
# Struct Solver *
#*******************************************************************
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
// Using this when solve structered grid or hybrid.
// -- "roe", "vanleer", "ausm+up", "ausmpw".
// str_limiter_name: Limiter of struct grid.
// -- "3rdsmooth", "smooth".
// -- "nolim", no limiter.
string inviscidSchemeName = "roe";
string str_limiter_name = "smooth";
double MUSCLCoefXk = 0.333333;
#*******************************************************************
# UnStruct Solver *
#*******************************************************************
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
// uns_limiter_name: Limiter of Unstruct grid.
// -- "vencat", "barth".
// -- "1st", meaning accuracy of first-order.
// -- "nolim", no limiter.
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'.
// The smaller the value, the more robust it is.
string uns_scheme_name = "roe";
string uns_limiter_name = "vencat";
double venkatCoeff = 5.0;
#########################################################################
# Temporal Discretisation #
#########################################################################
// iunsteady: Steady or unsteady.
// 0 -- steady.
// 1 -- unsteay.
// CFLEnd: The CFL number, [0.1, 100].
// The bigger the value, the convergence faster but lower robustness.
// nLUSGSSweeps: Number of Sub-iteration of LU-SGS.
// 1 -- is recommended for structured solver.
// 1-3 -- is recommended for unstructured solver.
int iunsteady = 0;
double CFLEnd = 10.0;
int tscheme = 8;
int nLUSGSSweeps = 1;
#########################################################################
# Multi-Grid parameters #
#########################################################################
// nMGLevel: The number of Multi-Grid level.
// = 1 -- single-level.
// > 1 -- multi-level.
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
// 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;
#########################################################################
# File In or Out #
#########################################################################
// gridfile: The partitioned Grid file path, using relative path,
// which is relative to the working directory.
// IMPORTANT WARNING: The file index should be ignored,
// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
// Please use 'rae2822_hybrid2d__4.fts' here!
// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
string gridfile = "./grid/rae2822_vis2d__4.fts";
int plotFieldType = 0;
// ----------------- Advanced Parameters, DO NOT care it ----------------
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables: Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
// -- viscosityLaminar(7), viscosityTurbulent(8),
// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12),
// -- strain_rate(13), Q_criteria(14), Cp(15), timeStep(16), volume(17),
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), iblank(81).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
// Variables order must from small to big.
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// limitVariables: Limit model (It is useful only if limitVector is 0).
// 0 -- limit only for pressure and denstiny, then get the min value.
// 1 -- limit for every variables, then get the min value.
// limitVector:
// 0 -- Each variable use the same limiter coefficient.
// 1 -- Each variable use the respective limiter coefficients.
// 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;

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#########################################################################
# Grid data type #
#########################################################################
// gridtype: Grid type for generation, conversion, reconstruction, merging.
// 0 -- Unstructured grid.
// 1 -- Structured grid.
// axisup: Type of Cartisien coordinates system, used in grid conversion.
// 1 -- Y upward. (default)
// 2 -- Z upward.
// from_gtype: Type of grid data type in grid conversion process.
// -1 -- MULTI_TYPE.
// 1 -- PHengLEI, *.fts.
// 2 -- CGNS, *.cgns.
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
// 5 -- Fluent, *.cas/*.msh.
// 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;
#########################################################################
# 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";

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string title = "PHengLEI Main Parameter Control File";
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
string defaultParaFile = "./bin/cfd_para.hypara";
// ndim: Dimensional of the grid, 2 or 3.
// nparafile: the number of parameter files.
// nsimutask: simulation task type.
// 0 -- CFD Solver of NS or Turbulation.
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
// Grid conversion: from other format to PHengLEI format (.fts).
// Grid reconstruction: such as grid adaptation.
// Grid merging: merge two blocks into one block.
// Grid repairing: repair the original grid in order to remove the negative volume cells.
// 2 -- Wall distance computation for turb-solver.
// 3 -- Grid partition.
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/cfd_para_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 = 1;
//string parafilename = "./bin/grid_deform_para.hypara";
//int nsimutask = 1;
//string parafilename = "./bin/grid_refine_para.hypara";
//int nsimutask = 14;
//string parafilename = "./bin/integrative_solver.hypara";
//int nsimutask = 99;
//string parafilename = "./bin/post_processing.hypara";
// ---------------- Advanced Parameters, DO NOT care it ----------------
int numberOfGridProcessor = 0;
// ATP read
//@string parafilename1 = ""
//@string parafilename2 = "";

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// pgridtype: The grid type.
// 0 -- unstruct grid.
// 1 -- struct grid.
// maxproc: The number of partition zones that want to be divided into,
// which is equal to the number of CPU processors you want.
// Usually, 50~100 thousands structured cells per CPU-Core is suggested.
// 30~70 thousands unstructured cells per CPU-Core is suggested.
// 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;
string original_grid_file = "./grid/rae2822_vis2d.fts";
string partition_grid_file = "./grid/rae2822_vis2d__4.fts";
// numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid.
// 1 -- single level.
// 2 -- 2 level.
// N -- N level,..., et al.
int numberOfMultigrid = 1;

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1
369 65
A
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-33 -1 1 1 -1
-337 -369 1 1 1
33 337 1 1 2
-337 -369 1 1 -1
-33 -1 1 1 1
369 369 1 65 4
1 369 65 65 4
1 1 1 65 4

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A26_TwoD_Rae2822_SA_MatrixLUSGS_Struct_4CPU/二维结构Rae2822翼型跨声速绕流(Matrix LUSGS)算例说明文档.pdf Normal file
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#########################################################################
# General Control Parameter #
#########################################################################
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual 'res.dat' saved.
int maxSimuStep = 60000;
int intervalStepFlow = 500;
int intervalStepPlot = 500;
int intervalStepForce = 50;
int intervalStepRes = 50;
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
// 0 -- no precondition process. (default, mach > 0.3)
// 1 -- carry out precondition process. (mach number <= 0.3)
int ifLowSpeedPrecon = 0;
#########################################################################
# Inflow Parameter #
#########################################################################
// refMachNumber: Mach number.
// attackd: Angle of attack.
// angleSlide: Angle of sideslip.
// inflowParaType: The type of inflow parameters.
// 0 -- the nondimensional conditions.
// 1 -- the flight conditions.
// 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions.
// 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.
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
// height: Fly height, unit of km.
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
// 1 dm = 0.1 m.
// 1 cm = 0.01 m.
// 1 mm = 0.001m.
// 1 inch = 0.0254m.
// 1 foot = 12 inches = 0.3048m.
// 1 yard = 3 feet = 0.9144m.
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit.
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
double refMachNumber = 0.2;
double attackd = 19.0;
double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 9.0e6;
double refDimensionalTemperature = 288.0;
//int inflowParaType = 1;
//double height = 0.001;
double gridScaleFactor = 1.0;
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 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 #
#########################################################################
// viscousType : Viscous model.
// 0 -- Euler.
// 1 -- Lamilar.
// 3 -- 1eq turbulent.
// 4 -- 2eq turbulent.
// viscousName: Laminar or tubulent model.
// -- "1eq-sa", when viscousType = 3.
// -- "2eq-kw-menter-sst", when viscousType = 4.
// DESType: Type of DES.
// 0 -- RANS.(default)
// 1 -- DES.
// 2 -- DDES.
// 3 -- IDDES.
//int viscousType = 0;
//string viscousName = "Euler";
//int viscousType = 1;
//string viscousName = "laminar";
int viscousType = 3;
string viscousName = "1eq-sa";
//int viscousType = 4;
//string viscousName = "2eq-kw-menter-sst";
int DESType = 0;
int roeEntropyFixMethod = 6;
double roeEntropyScale = 1.0;
#########################################################################
# Spatial Discretisation #
#########################################################################
#*******************************************************************
# Struct Solver *
#*******************************************************************
// str_limiter_name: Limiter of struct grid.
// -- "3rdsmooth", "smooth".
// -- "nolim", no limiter.
string str_limiter_name = "smooth";
double MUSCLCoefXk = 0.333333;
#*******************************************************************
# UnStruct Solver *
#*******************************************************************
// uns_limiter_name: Limiter of Unstruct grid.
// -- "vencat".
// -- "1st", meaning accuracy of first-order.
// -- "nolim", no limiter.
// 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;
#########################################################################
# Temporal Discretisation #
#########################################################################
// iunsteady: Steady or unsteady.
// 0 -- steady.
// 1 -- unsteay.
// CFLEnd: The CFL number, [0.1, 100].
// The bigger the value, the convergence faster but lower robustness.
// nLUSGSSweeps: Number of Sub-iteration of LU-SGS.
// 1 -- is recommended for structured solver.
// 1-3 -- is recommended for unstructured solver.
int iunsteady = 0;
double CFLEnd = 10.0;
int nLUSGSSweeps = 1;
#########################################################################
# Multi-Grid parameters #
#########################################################################
// nMGLevel: The number of Multi-Grid level.
// = 1 -- single-level.
// > 1 -- multi-level.
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
// 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;
#########################################################################
# File In or Out #
#########################################################################
// gridfile: The partitioned Grid file path, using relative path,
// which is relative to the working directory.
// IMPORTANT WARNING: The file index should be ignored,
// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
// Please use 'rae2822_hybrid2d__4.fts' here!
// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
string gridfile = "./grid/30p30n_str__4.fts";
int plotFieldType = 0;
// ----------------- Advanced Parameters, DO NOT care it ----------------
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables: Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
// -- viscosityLaminar(7), viscosityTurbulent(8),
// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12),
// -- strain_rate(13), Q_criteria(14), Cp(15), timeStep(16), volume(17),
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
// Variables order must from small to big.
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// limitVariables: Limit model (It is useful only if limitVector is 0).
// 0 -- limit only for pressure and denstiny, then get the min value.
// 1 -- limit for every variables, then get the min value.
// limitVector:
// 0 -- Each variable use the same limiter coefficient.
// 1 -- Each variable use the respective limiter coefficients.
// 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;

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#########################################################################
# Grid data type #
#########################################################################
// gridtype: Grid type for generation, conversion, reconstruction, merging.
// 0 -- Unstructured grid.
// 1 -- Structured grid.
// axisup: Type of Cartisien coordinates system, used in grid conversion.
// 1 -- Y upward. (default)
// 2 -- Z upward.
// from_gtype: Type of grid data type in grid conversion process.
// -1 -- MULTI_TYPE.
// 1 -- PHengLEI, *.fts.
// 2 -- CGNS, *.cgns.
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
// 5 -- Fluent, *.cas/*.msh.
// 6 -- Ustar, mgrid.in.
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
// 8 -- GMSH, *.msh.
// 9 -- Gridgen type of structured grid, *.dat/*.grd.
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/30p30n_str.grd";
string out_gfile = "./grid/30p30n_str.fts";

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string title = "PHengLEI Main Parameter Control File";
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
string defaultParaFile = "./bin/cfd_para.hypara";
// ndim: Dimensional of the grid, 2 or 3.
// nparafile: the number of parameter files.
// nsimutask: simulation task type.
// 0 -- CFD Solver of NS or Turbulation.
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
// Grid conversion: from other format to PHengLEI format (.fts).
// Grid reconstruction: such as grid adaptation.
// Grid merging: merge two blocks into one block.
// Grid repairing: repair the original grid in order to remove the negative volume cells.
// 2 -- Wall distance computation for turb-solver.
// 3 -- Grid partition.
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/cfd_para_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 = 1;
//string parafilename = "./bin/grid_deform_para.hypara";
//int nsimutask = 1;
//string parafilename = "./bin/grid_refine_para.hypara";
//int nsimutask = 14;
//string parafilename = "./bin/integrative_solver.hypara";
//int nsimutask = 99;
//string parafilename = "./bin/post_processing.hypara";
// ---------------- Advanced Parameters, DO NOT care it ----------------
int numberOfGridProcessor = 0;
// ATP read
//@string parafilename1 = ""
//@string parafilename2 = "";

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// pgridtype: The grid type.
// 0 -- unstruct grid.
// 1 -- struct grid.
// maxproc: The number of partition zones that want to be divided into,
// which is equal to the number of CPU processors you want.
// Usually, 50~100 thousands structured cells per CPU-Core is suggested.
// 30~70 thousands unstructured cells per CPU-Core is suggested.
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
// numberOfMultifile: The number of partition grid files that want to be dumped out.
int pgridtype = 1;
int maxproc = 4;
string original_grid_file = "./grid/30p30n_str.fts";
string partition_grid_file = "./grid/30p30n_str__4.fts";
int numberOfMultifile = 1;
// numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid.
// 1 -- single level.
// 2 -- 2 level.
// N -- N level,..., et al.
int numberOfMultigrid = 1;

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1
8
81 617
A
21
1 41 1 1 4
1 1 65 1 -1
353 353 -65 -1 7
1 1 65 129 -1
281 281 -1 -65 6
1 1 189 129 -1
121 121 -61 -1 8
1 1 221 189 -1
121 121 -93 -61 8
1 1 221 245 -1
121 121 -93 -117 8
1 1 309 245 -1
41 41 65 1 2
1 1 309 341 -1
41 41 -65 -97 2
1 1 -481 -553 -1
41 41 -65 -137 5
1 1 -481 -449 -1
41 41 -65 -33 5
1 1 -373 -449 -1
121 121 -33 -109 4
1 1 -341 -373 -1
121 121 -1 -33 4
41 1 617 617 4
1 1 -553 -617 -1
1 1 -65 -1 7
81 81 553 617 4
81 41 617 617 4
81 81 341 553 4
81 81 245 341 4
81 81 65 245 4
81 81 65 1 4
41 81 1 1 4
41 97
B
6
41 41 65 1 -1
1 1 309 245 1
-1 -41 1 1 -1
81 121 117 117 8
1 1 65 1 2
41 41 -65 -97 -1
1 1 309 341 1
1 1 97 65 2
1 41 97 97 -1
81 121 1 1 4
81 49
C
6
81 49 49 49 -1
81 49 1 1 4
81 81 1 49 2
81 49 1 1 -1
81 49 117 117 8
-1 -49 49 49 -1
1 49 1 1 4
1 1 49 1 2
-49 -1 1 1 -1
49 1 117 117 8
121 141
D
14
121 121 -1 -33 -1
1 1 -341 -373 1
81 121 1 1 -1
1 41 97 97 2
81 49 1 1 -1
81 49 49 49 3
1 1 33 1 2
1 49 1 1 -1
-1 -49 49 49 3
121 121 -33 -109 -1
1 1 -373 -449 1
1 1 77 33 2
1 1 93 77 2
1 1 109 93 2
1 1 125 109 2
1 1 -125 -141 -1
1 1 -17 -1 8
49 1 141 141 -1
113 161 65 65 6
-121 -49 141 141 -1
41 113 65 65 6
121 121 141 109 -1
41 41 -1 -33 5
41 137
E
8
41 41 -1 -33 -1
121 121 141 109 4
1 1 33 1 2
1 41 1 1 -1
1 41 65 65 6
41 41 -65 -33 -1
1 1 -481 -449 1
1 1 65 33 2
41 41 -65 -137 -1
1 1 -481 -553 1
1 1 137 65 2
41 1 137 137 -1
1 41 65 65 7
281 65
F
8
1 1 65 1 2
1 161 1 1 -1
73 233 65 65 7
113 161 65 65 -1
49 1 141 141 4
41 113 65 65 -1
-121 -49 141 141 4
1 41 65 65 -1
1 41 1 1 5
161 281 65 65 -1
1 121 1 1 8
281 281 -1 -65 -1
1 1 65 129 1
161 281 1 1 -1
233 353 65 65 7
353 65
G
7
1 1 -65 -1 -1
1 1 -553 -617 1
1 41 65 65 -1
41 1 137 137 5
73 41 65 65 2
73 233 65 65 -1
1 161 1 1 6
233 353 65 65 -1
161 281 1 1 6
353 353 -65 -1 -1
1 1 65 1 1
1 353 1 1 4
121 117
H
11
1 1 61 17 2
1 1 -17 -1 -1
1 1 -125 -141 4
1 121 1 1 -1
161 281 65 65 6
121 121 -61 -1 -1
1 1 189 129 1
1 1 93 61 2
121 121 -93 -61 -1
1 1 221 189 1
1 1 117 93 2
81 49 117 117 -1
81 49 1 1 3
49 1 117 117 -1
-49 -1 1 1 3
81 121 117 117 -1
-1 -41 1 1 2
121 121 -93 -117 -1
1 1 221 245 1

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A27_TwoD_30p30n_SA_Entropyfix6_Struct_4CPU/二维结构30p30n翼型低速绕流(熵修正)算例说明文档.pdf Normal file
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#########################################################################
# General Control Parameter #
#########################################################################
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual 'res.dat' saved.
int maxSimuStep = 5000;
int intervalStepFlow = 500;
int intervalStepPlot = 500;
int intervalStepForce = 50;
int intervalStepRes = 10;
#########################################################################
# Inflow Parameter #
#########################################################################
// refMachNumber: Mach number.
// attackd: Angle of attack.
// angleSlide: Angle of sideslip.
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
// inflowParaType: The type of inflow parameters.
// 0 -- the nondimensional conditions.
// 1 -- the flight conditions.
// 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions.
// 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.
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
// height: Fly height, unit of km.
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
// 1 dm = 0.1 m.
// 1 cm = 0.01 m.
// 1 mm = 0.001m.
// 1 inch = 0.0254m.
// 1 foot = 12 inches = 0.3048m.
// 1 yard = 3 feet = 0.9144m.
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit.
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
double refMachNumber = 3.0;
double attackd = 0.00;
double angleSlide = 0.00;
double wallTemperature = -1.0;
int inflowParaType = 0;
double refReNumber = 1.0e5;
double refDimensionalTemperature = 293;
//int inflowParaType = 1;
//double height = 0.001;
//int inflowParaType = 2;
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
double gridScaleFactor = 1.0;
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 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 #
#########################################################################
// viscousType : Viscous model.
// 0 -- Euler.
// 1 -- Lamilar.
// 3 -- 1eq turbulent.
// 4 -- 2eq turbulent.
// viscousName: Laminar or tubulent model.
// -- "1eq-sa", when viscousType = 3.
// -- "2eq-kw-menter-sst", when viscousType = 4.
// DESType: Type of DES.
// 0 -- RANS.(default)
// 1 -- DES.
// 2 -- DDES.
// 3 -- IDDES.
int viscousType = 0;
string viscousName = "Euler";
//int viscousType = 1;
//string viscousName = "laminar";
//int viscousType = 3;
//string viscousName = "1eq-sa";
//int viscousType = 4;
//string viscousName = "2eq-kw-menter-sst";
int DESType = 0;
int roeEntropyFixMethod = 6;
double roeEntropyScale = 1.0;
#########################################################################
# Spatial Discretisation #
#########################################################################
#*******************************************************************
# Struct Solver *
#*******************************************************************
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
// Using this when solve structered grid or hybrid.
// -- "vanleer", "steger", "ausmpw", "ausmpw+".
// str_limiter_name: Limiter of struct grid.
// -- "minmod", "3rd_minmod_smooth".
string inviscidSchemeName = "roe";
string str_limiter_name = "minvan";
#*******************************************************************
# UnStruct Solver *
#*******************************************************************
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
// uns_limiter_name: Limiter of Unstruct grid.
// -- "vencat", "barth".
// -- "1st", meaning accuracy of first-order.
// -- "nolim", no limiter.
// 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;
#########################################################################
# Temporal Discretisation #
#########################################################################
// iunsteady: Steady or unsteady.
// 0 -- steady.
// 1 -- unsteay.
// CFLEnd: The CFL number, [0.1, 100].
// 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;
double CFLStart = 0.1;
double CFLEnd = 20.0;
int CFLVaryStep = 100;
double ktmax = 1.0e10;
double LUSGSTolerance = 0.1;
#########################################################################
# File In or Out #
#########################################################################
// gridfile: The partitioned Grid file path, using relative path,
// which is relative to the working directory.
// IMPORTANT WARNING: The file index should be ignored,
// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
// Please use 'rae2822_hybrid2d__4.fts' here!
// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
string gridfile = "./grid/cylinder.fts";
int plotFieldType = 0;
// ----------------- Advanced Parameters, DO NOT care it ----------------
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables: Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
// -- viscosityLaminar(7), viscosityTurbulent(8),
// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12),
// -- strain_rate(13), Q_criteria(14), Cp(15), timeStep(16), volume(17),
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
// Variables order must from small to big.
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// limitVariables: Limit model (It is useful only if limitVector is 0).
// 0 -- limit only for pressure and denstiny, then get the min value.
// 1 -- limit for every variables, then get the min value.
// limitVector:
// 0 -- Each variable use the same limiter coefficient.
// 1 -- Each variable use the respective limiter coefficients.
// 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;

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#########################################################################
# Grid data type #
#########################################################################
// gridtype: Grid type for generation, conversion, reconstruction, merging.
// 0 -- Unstructured grid.
// 1 -- Structured grid.
// axisup: Type of Cartisien coordinates system, used in grid conversion.
// 1 -- Y upward. (default)
// 2 -- Z upward.
// from_gtype: Type of grid data type in grid conversion process.
// -1 -- MULTI_TYPE.
// 1 -- PHengLEI, *.fts.
// 2 -- CGNS, *.cgns.
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
// 5 -- Fluent, *.cas/*.msh.
// 6 -- Ustar, mgrid.in.
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
// 8 -- GMSH, *.msh.
// 9 -- Gridgen type of structured grid, *.dat/*.grd.
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/cylinder.grd";
string out_gfile = "./grid/cylinder.fts";

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string title = "PHengLEI Main Parameter Control File";
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
string defaultParaFile = "./bin/cfd_para.hypara";
// ndim: Dimensional of the grid, 2 or 3.
// nparafile: the number of parameter files.
// nsimutask: simulation task type.
// 0 -- CFD Solver of NS or Turbulation.
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
// Grid conversion: from other format to PHengLEI format (.fts).
// Grid reconstruction: such as grid adaptation.
// Grid merging: merge two blocks into one block.
// Grid repairing: repair the original grid in order to remove the negative volume cells.
// 2 -- Wall distance computation for turb-solver.
// 3 -- Grid partition.
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/cfd_para_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 = 1;
//string parafilename = "./bin/grid_deform_para.hypara";
//int nsimutask = 1;
//string parafilename = "./bin/grid_refine_para.hypara";
//int nsimutask = 14;
//string parafilename = "./bin/integrative_solver.hypara";
//int nsimutask = 99;
//string parafilename = "./bin/post_processing.hypara";
// ---------------- Advanced Parameters, DO NOT care it ----------------
int numberOfGridProcessor = 0;
// ATP read
//@string parafilename1 = ""
//@string parafilename2 = "";

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121 121 61 1 6
1 121 1 1 2
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#########################################################################
# General Control Parameter #
#########################################################################
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual 'res.dat' saved.
int maxSimuStep = 10000;
int intervalStepFlow = 500;
int intervalStepPlot = 500;
int intervalStepForce = 50;
int intervalStepRes = 50;
#########################################################################
# Inflow Parameter #
#########################################################################
// refMachNumber: Mach number.
// attackd: Angle of attack.
// angleSlide: Angle of sideslip.
// inflowParaType: The type of inflow parameters.
// 0 -- the nondimensional conditions.
// 1 -- the flight conditions.
// 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions.
// 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.
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
// height: Fly height, unit of km.
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
// 1 dm = 0.1 m.
// 1 cm = 0.01 m.
// 1 mm = 0.001m.
// 1 inch = 0.0254m.
// 1 foot = 12 inches = 0.3048m.
// 1 yard = 3 feet = 0.9144m.
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit.
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
double refMachNumber = 0.73;
double attackd = 2.31;
double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 6.5e6;
double refDimensionalTemperature = 288.15;
//int inflowParaType = 1;
//double height = 0.001;
//int inflowParaType = 2;
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
double gridScaleFactor = 1.0;
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 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 #
#########################################################################
// viscousType : Viscous model.
// 0 -- Euler.
// 1 -- Lamilar.
// 3 -- 1eq turbulent.
// 4 -- 2eq turbulent.
// viscousName: Laminar or tubulent model.
// -- "1eq-sa", when viscousType = 3.
// -- "2eq-kw-menter-sst", when viscousType = 4.
// DESType: Type of DES.
// 0 -- RANS.(default)
// 1 -- DES.
// 2 -- DDES.
// 3 -- IDDES.
//int viscousType = 0;
//string viscousName = "Euler";
//int viscousType = 1;
//string viscousName = "laminar";
int viscousType = 3;
string viscousName = "1eq-sa";
//int viscousType = 4;
//string viscousName = "2eq-kw-menter-sst";
int DESType = 0;
int roeEntropyFixMethod = 6;
double roeEntropyScale = 1.0;
#########################################################################
# Spatial Discretisation #
#########################################################################
#*******************************************************************
# Struct Solver *
#*******************************************************************
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
// Using this when solve structered grid or hybrid.
// -- "roe", "vanleer", "ausm+up", "ausmpw".
// str_limiter_name: Limiter of struct grid.
// -- "3rdsmooth", "smooth".
// -- "nolim", no limiter.
string inviscidSchemeName = "roe";
string str_limiter_name = "smooth";
double MUSCLCoefXk = 0.333333;
#*******************************************************************
# UnStruct Solver *
#*******************************************************************
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
// uns_limiter_name: Limiter of Unstruct grid.
// -- "vencat", "barth".
// -- "1st", meaning accuracy of first-order.
// -- "nolim", no limiter.
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'.
// The smaller the value, the more robust it is.
string uns_scheme_name = "roe";
string uns_limiter_name = "vencat";
double venkatCoeff = 5.0;
#########################################################################
# Temporal Discretisation #
#########################################################################
// iunsteady: Steady or unsteady.
// 0 -- steady.
// 1 -- unsteay.
// CFLEnd: The CFL number, [0.1, 100].
// The bigger the value, the convergence faster but lower robustness.
// nLUSGSSweeps: Number of Sub-iteration of LU-SGS.
// 1 -- is recommended for structured solver.
// 1-3 -- is recommended for unstructured solver.
int iunsteady = 0;
double CFLEnd = 10.0;
int nLUSGSSweeps = 1;
#########################################################################
# Multi-Grid parameters #
#########################################################################
// nMGLevel: The number of Multi-Grid level.
// = 1 -- single-level.
// > 1 -- multi-level.
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
// 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;
#########################################################################
# File In or Out #
#########################################################################
// gridfile: The partitioned Grid file path, using relative path,
// which is relative to the working directory.
// IMPORTANT WARNING: The file index should be ignored,
// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
// Please use 'rae2822_hybrid2d__4.fts' here!
// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
string gridfile = "./grid/rae2822_vis2d__4.fts";
int plotFieldType = 0;
// ----------------- Advanced Parameters, DO NOT care it ----------------
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables: Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
// -- viscosityLaminar(7), viscosityTurbulent(8),
// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12),
// -- strain_rate(13), Q_criteria(14), Cp(15), timeStep(16), volume(17),
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), iblank(81).
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
// Variables order must from small to big.
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// limitVariables: Limit model (It is useful only if limitVector is 0).
// 0 -- limit only for pressure and denstiny, then get the min value.
// 1 -- limit for every variables, then get the min value.
// limitVector:
// 0 -- Each variable use the same limiter coefficient.
// 1 -- Each variable use the respective limiter coefficients.
// 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;

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#########################################################################
# Grid data type #
#########################################################################
// gridtype: Grid type for generation, conversion, reconstruction, merging.
// 0 -- Unstructured grid.
// 1 -- Structured grid.
// axisup: Type of Cartisien coordinates system, used in grid conversion.
// 1 -- Y upward. (default)
// 2 -- Z upward.
// from_gtype: Type of grid data type in grid conversion process.
// -1 -- MULTI_TYPE.
// 1 -- PHengLEI, *.fts.
// 2 -- CGNS, *.cgns.
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
// 5 -- Fluent, *.cas/*.msh.
// 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;
#########################################################################
# 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";

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string title = "PHengLEI Main Parameter Control File";
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
string defaultParaFile = "./bin/cfd_para.hypara";
// ndim: Dimensional of the grid, 2 or 3.
// nparafile: the number of parameter files.
// nsimutask: simulation task type.
// 0 -- CFD Solver of NS or Turbulation.
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
// Grid conversion: from other format to PHengLEI format (.fts).
// Grid reconstruction: such as grid adaptation.
// Grid merging: merge two blocks into one block.
// Grid repairing: repair the original grid in order to remove the negative volume cells.
// 2 -- Wall distance computation for turb-solver.
// 3 -- Grid partition.
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/cfd_para_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 = 1;
//string parafilename = "./bin/grid_deform_para.hypara";
//int nsimutask = 1;
//string parafilename = "./bin/grid_refine_para.hypara";
//int nsimutask = 14;
//string parafilename = "./bin/integrative_solver.hypara";
//int nsimutask = 99;
//string parafilename = "./bin/post_processing.hypara";
// ---------------- Advanced Parameters, DO NOT care it ----------------
int numberOfGridProcessor = 0;
// ATP read
//@string parafilename1 = ""
//@string parafilename2 = "";

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// pgridtype: The grid type.
// 0 -- unstruct grid.
// 1 -- struct grid.
// maxproc: The number of partition zones that want to be divided into,
// which is equal to the number of CPU processors you want.
// Usually, 50~100 thousands structured cells per CPU-Core is suggested.
// 30~70 thousands unstructured cells per CPU-Core is suggested.
// 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;
string original_grid_file = "./grid/rae2822_vis2d.fts";
string partition_grid_file = "./grid/rae2822_vis2d__4.fts";
// numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid.
// 1 -- single level.
// 2 -- 2 level.
// N -- N level,..., et al.
int numberOfMultigrid = 1;

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1
1
369 65
A
6
-33 -1 1 1 -1
-337 -369 1 1 1
33 337 1 1 2
-337 -369 1 1 -1
-33 -1 1 1 1
369 369 1 65 4
1 369 65 65 4
1 1 1 65 4

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#########################################################################
# Grid data type #
#########################################################################
// gridtype: Grid type for generation, conversion, reconstruction, merging.
// 0 -- Unstructured grid.
// 1 -- Structured grid.
// axisup: Type of Cartisien coordinates system, used in grid conversion.
// 1 -- Y upward. (default)
// 2 -- Z upward.
// from_gtype: Type of grid data type in grid conversion process.
// -1 -- MULTI_TYPE.
// 1 -- PHengLEI, *.fts.
// 2 -- CGNS, *.cgns.
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
// 5 -- Fluent, *.cas/*.msh.
// 6 -- Ustar, mgrid.in.
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
// 8 -- GMSH, *.msh.
// 9 -- Gridgen type of structured grid, *.dat/*.grd.
int gridtype = 0;
int axisup = 1;
int from_gtype = 2;
#########################################################################
# 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/M6_unstr.cgns";
string out_gfile = "./grid/M6_unstr.fts";

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@ -0,0 +1,31 @@
#########################################################################
# Grid data type #
#########################################################################
// gridtype: Grid type for generation, conversion, reconstruction, merging.
// 0 -- Unstructured grid.
// 1 -- Structured grid.
// gridobj: Task type of grid treatment.
// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc.
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
// 2 -- Grid refinement.
// 3 -- Grid merging, merge two blocks into one block.
// 4 -- Grid deformation, achieve unstructured grid deformation.
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
// 7 -- Grid type change, convert structured grid to unstructured grid.
// anisoRefine: If refine grid by anisoRefine type.
// 0 -- Not. (default)
// 1 -- Yes.
int gridtype = 0;
int gridobj = 2;
int anisoRefine = 0;
#########################################################################
# 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/M6_unstr__4.fts";
string out_gfile = "./grid/M6_unstr_refined__4.fts";

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string title = "PHengLEI Main Parameter Control File";
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
string defaultParaFile = "./bin/cfd_para.hypara";
// ndim: Dimensional of the grid, 2 or 3.
// nparafile: the number of parameter files.
// nsimutask: simulation task type.
// 0 -- CFD Solver of NS or Turbulation.
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
// Grid conversion: from other format to PHengLEI format (.fts).
// Grid reconstruction: such as grid adaptation.
// Grid merging: merge two blocks into one block.
// Grid repairing: repair the original grid in order to remove the negative volume cells.
// 2 -- Wall distance computation for turb-solver.
// 3 -- Grid partition.
int ndim = 3;
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/cfd_para_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 = 1;
//string parafilename = "./bin/grid_deform_para.hypara";
//int nsimutask = 1;
//string parafilename = "./bin/grid_refine_para.hypara";
//int nsimutask = 14;
//string parafilename = "./bin/integrative_solver.hypara";
//int nsimutask = 99;
//string parafilename = "./bin/post_processing.hypara";
// ---------------- Advanced Parameters, DO NOT care it ----------------
int numberOfGridProcessor = 0;
// ATP read
//@string parafilename1 = ""
//@string parafilename2 = "";

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// pgridtype: The grid type.
// 0 -- unstruct grid.
// 1 -- struct grid.
// maxproc: The number of partition zones that want to be divided into,
// which is equal to the number of CPU processors you want.
// Usually, 50~100 thousands structured cells per CPU-Core is suggested.
// 30~70 thousands unstructured cells per CPU-Core is suggested.
// 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 = 0;
int maxproc = 4;
string original_grid_file = "./grid/M6_unstr.fts";
string partition_grid_file = "./grid/M6_unstr__4.fts";
// numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid.
// 1 -- single level.
// 2 -- 2 level.
// N -- N level,..., et al.
int numberOfMultigrid = 1;

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29
README.md
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@ -43,6 +43,12 @@ A 结构
| 三维结构激波干扰超声速层流平板 | A21_ThreeD_ShockwaveInteractionPlate_Ma2_Laminar_UDB_Struct_1CPU | | 三维结构激波干扰超声速层流平板 | A21_ThreeD_ShockwaveInteractionPlate_Ma2_Laminar_UDB_Struct_1CPU |
| 三维结构弹体喷流（自定义边界） | A22_ThreeD_Jet_Ma3d33_SST_Struct_8CPU | | 三维结构弹体喷流（自定义边界） | A22_ThreeD_Jet_Ma3d33_SST_Struct_8CPU |
| 二维结构S-K低速平板转捩模拟 | A23_TwoD_Plate_S-KSR_SST_Struct_4CPU | | 二维结构S-K低速平板转捩模拟 | A23_TwoD_Plate_S-KSR_SST_Struct_4CPU |
| 二维结构30p30n翼型低速绕流(Matrix LUSGS) | A24_TwoD_30p30n_SA_MatrixLUSGS_Struct_4CPU |
| 二维结构低速湍流平板(Matrix LUSGS) | A25_TwoD_Plate_SST_LowMach_MatrixLUSGS_Struct_1CPU |
| 二维结构Rae2822翼型跨声速绕流(Matrix LUSGS) | A26_TwoD_Rae2822_SA_MatrixLUSGS_Struct_4CPU |
| 二维结构30p30n翼型低速绕流(熵修正) | A27_TwoD_30p30n_SA_Entropyfix6_Struct_4CPU |
| 二维结构圆柱超声速绕流(熵修正) | A28_TwoD_Cylinder_Inv_Ma3d0_Entropyfix6_Struct_1CPU |
| 二维结构Rae2822翼型跨声速绕流(熵修正) | A29_TwoD_Rae2822_SA_Entropyfix6_Struct_4CPU |
B 非结构 B 非结构
@ -81,6 +87,9 @@ D 高阶
| :------------------------- | :--------------------------------- | | :------------------------- | :--------------------------------- |
| 二维结构高阶圆柱 | D01_TwoD_Cylinder_Laminar_HighOrder_Struct_1CPU | | 二维结构高阶圆柱 | D01_TwoD_Cylinder_Laminar_HighOrder_Struct_1CPU |
| 三维结构高阶双椭球 | D02_ThreeD_DoubleEllipse_Laminar_HighOrder_Struct_48CPU | | 三维结构高阶双椭球 | D02_ThreeD_DoubleEllipse_Laminar_HighOrder_Struct_48CPU |
| 二维WENN结构高阶30P30N翼型 | D03_TwoD_30P30N_SST_HighOrderWENN_Struct_6CPU |
| 三维WENN结构高阶M6机翼 | D04_ThreeD_ONERA_M6_SST_HighOrderWENN_Struct_8CPU |
| 三维WENN结构高阶双椭球 | D05_ThreeD_DoubleEllipse_Laminar_HighOrderWENN_Struct_48CPU |
E LES E LES
@ -96,14 +105,15 @@ F 重叠网格、动网格
| :------------------------- | :--------------------------------- | | :------------------------- | :--------------------------------- |
| 三维结构30p30n重叠网格装配 | F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU | | 三维结构30p30n重叠网格装配 | F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU |
| 三维结构多弹体重叠网格装配 | F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU | | 三维结构多弹体重叠网格装配 | F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU |
| 二维非结构双0012重叠网格装配 | F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU | | 二维非结构双0012重叠网格装配 | F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU |
| 二维非结构双0012重叠网格计算 | F04_TwoD_Dual0012_OversetGrid_InvisCal_Unstruct_4CPU | | 二维非结构双0012重叠网格计算 | F04_TwoD_Dual0012_OversetGrid_InvisCal_Unstruct_4CPU |
| 三维非结构AEDC重叠网格装配 | F05_ThreeD_AEDC_OversetGrid_SST_Unstruct_8CPU | | 三维非结构AEDC吊舱分离重叠网格装配 | F05_ThreeD_AEDC_OversetConfig_Unstruct_8CPU |
| 三维非结构AEDC重叠网格计算 | F06_ThreeD_AEDC_OversetGrid_SSTCal_Unstruct_8CPU | | 三维非结构AEDC吊舱分离非定常计算 | F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU |
| 二维结构NACA0012翼型俯仰振荡 | F07_TwoD_NACA0012_PitchingMovement_SA_Struct_4CPU | | 二维结构NACA0012翼型俯仰振荡 | F07_TwoD_NACA0012_PitchingMovement_SA_Struct_4CPU |
| 三维结构Finner弹体俯仰振荡 | F08_ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU | | 三维结构Finner弹体俯仰振荡 | F08_ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU |
| 鸟类扑翼网格变形（弹簧法） | F09_ThreeD_Brid_GridDeformationSPRING_Unstruct_1CPU | | 鸟类扑翼网格变形（弹簧法） | F09_ThreeD_Brid_GridDeformationSPRING_Unstruct_1CPU |
| 鸟类扑翼网格变形（RBF方法） | F10_ThreeD_Brid_GridDeformationRBF_Unstruct_1CPU | | 鸟类扑翼网格变形（RBF方法） | F10_ThreeD_Brid_GridDeformationRBF_Unstruct_1CPU |
| 非结构三维M6机翼并行加密 | F11_ThreeD_M6_GridParallelRefine_Unstruct_4CPU |
G 非平衡 G 非平衡
@ -113,6 +123,19 @@ G 非平衡
| 三维结构钝锥化学非平衡 | G02_ThreeD_Electre_Laminar_OneTemperMode_NCW_Struct | | 三维结构钝锥化学非平衡 | G02_ThreeD_Electre_Laminar_OneTemperMode_NCW_Struct |
| 三维结构类返回舱化学非平衡 | G03_ | | 三维结构类返回舱化学非平衡 | G03_ |
| 三维结构类航天飞机化学非平衡 | G04_ | | 三维结构类航天飞机化学非平衡 | G04_ |
| 二维非结构高速圆柱两气体组分预混 | G05_TwoD_Cylinder_N2-O2_Premixing-Unstruct_1CPU |
| 三维非结构高速球头两气体组分预混 | G06_ThreeD_Sphere_N2-O2_Premixing-Unstruct_1CPU |
| 二维非结构管道喷流两气体组分预混 | G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU |
H 不可压
| 中文 | 英文 |
| :----------------------------------- | :-------------------------------------------------------- |
| 二维非结构不可压层流后台阶流动 | H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU |
| 二维非结构不可压层流方腔自然对流 | H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU |
| 二维非结构不可压层流方腔流动 | H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU |
| 三维非结构不可压圆管湍流压降模拟 | H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU |
| 三维非结构不可压AFF-1 半艇外流场模拟 | H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU |
X 用户分享算例 X 用户分享算例