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PHengLEI-TestCases
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hechao 2021-03-26 15:53:14 +08:00
parent 7f8e0990db
commit 7774cb2a9a
16 changed files with 731 additions and 600 deletions
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50
ThreeD_CHNT_SST_Struct_16CPU/bin/cfd_para.hypara
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@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
double influenceRadius = 20; double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// ----------------- Periodic Parameters --------------------------------
// Notice:Rotational periodicity only support rotation along the X axis!
// periodicType: Which periodic boundary is used.
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
######################################################################### #########################################################################
# Default parameters for Partition # # Default parameters for Partition #
######################################################################### #########################################################################
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
// maxSimuStep: The max simulation step, don't care simulation is restart or not. // maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. // intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual file 'res.dat' saved. // intervalStepRes: The step intervals for residual file 'res.dat' saved.
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. // ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
int intervalStepFlow = 1000; int intervalStepFlow = 1000;
int intervalStepPlot = 1000; int intervalStepPlot = 1000;
int intervalStepSample = 1000;
int intervalStepForce = 100; int intervalStepForce = 100;
int intervalStepRes = 10; int intervalStepRes = 10;
int ifLowSpeedPrecon = 0; int ifLowSpeedPrecon = 0;
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter.
// directionMethod: The method of determining direction.
// 1 -- using direciton.
// 2 -- using face normal.
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
// direction_inlet: The direction of inlet.
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
// direction_outlet: The direction of outlet.
int directionMethod = 2;
double subsonicInletTotalPressure = 1.2e6;
double subsonicInletTotalTemperature = 1300;
double direction_inlet[] = 1, 0, 0;
double subsonicOutletTotalPressure = 17.8571428;
double subsonicOutletTotalTemperature = 1.0;
double direction_outlet[] = 1, 0, 0;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Spatial Discretisation # # Spatial Discretisation #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
#******************************************************************* #*******************************************************************
# UnStruct Solver or Common * # UnStruct Solver or Common *
#******************************************************************* #*******************************************************************
// viscousType : Viscous model. // viscousType: Viscous model.
// 0 -- Euler. // 0 -- Euler.
// 1 -- Lamilar. // 1 -- Lamilar.
// 2 -- Algebraic. // 2 -- Algebraic.
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt"; string visualfile = "results/tecflow.plt";
string Qwall_file = "results/Qwall.dat"; string Qwall_file = "results/Qwall.dat";
string wall_aircoefile = "results/wall_aircoef.dat"; string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string surfacefile = ""; string surfacefile = "";
string wall_varfile = ""; string wall_varfile = "";
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
int dumpStandardModel = 0; int dumpStandardModel = 0;
// ifSetProbesToMonitor: Set probes location to Monitor.
// 0 -- Do not monitor.
// 1 -- To monitor and save data to files.
// probesDefineFile: probes location information file.
// nProbeVariables: Number of variables want to be dumped for probes monitered.
// probeVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
// probeVariables order must from small to big.
int ifSetProbesToMonitor = 0;
string probesDefineFile = "bin/probes_location.hypara";
int nProbeVariables = 6;
int probeVariables[] = [0, 1, 2, 3, 4, 5];
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Turbulence Parameter # # Turbulence Parameter #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// structhighordergradient: // structhighordergradient:
// -- "conservation", "chain_rule". // -- "conservation", "chain_rule".
int ifvfd = 0; int ifvfd = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0; int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6; double str_highorder_interpolation_epsilon = 1.0e-6;
string str_highorder_interpolation_type = "test"; string str_highorder_interpolation_type = "test";
string str_highorder_flux_name = "steger"; string str_highorder_flux_name = "steger";
string structhighordergradient = "conservation"; string structhighordergradient = "conservation";
double coefofstrflux = 0.5;
double limitcoefofinterface = 0.0;
// ----------------- Advanced choices ----------------------------------- // ----------------- Advanced choices -----------------------------------
// outtimesc: Time stepping scheme for the outer loop. // outtimesc: Time stepping scheme for the outer loop.

583
ThreeD_Cylinder_LES_Re3900_Struct/bin/cfd_para.hypara
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@ -10,22 +10,22 @@
// (C) Copyright, Since 2010 + // (C) Copyright, Since 2010 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
########################################################################### ###########################################################################
# Default parameters for Grid conversion # # Default parameters for Grid conversion #
########################################################################### ###########################################################################
// gridtype: Grid type for generation, conversion, reconstruction, merging. // gridtype: Grid type for generation, conversion, reconstruction, merging.
// 0 -- Unstructured grid. // 0 -- Unstructured grid.
// 1 -- Structured grid. // 1 -- Structured grid.
// 2 -- Hybrid grid, include both of unstructured and structured grid. // 2 -- Hybrid grid, include both of unstructured and structured grid.
// gridobj: Task type of grid treatment. // gridobj: Task type of grid treatment.
// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc. // 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. // 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
// 2 -- Grid refinement. // 2 -- Grid refinement.
// 3 -- Grid merging, merge two blocks into one block. // 3 -- Grid merging, merge two blocks into one block.
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells. // 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. // 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
// multiblock: Multi-block grid or not, only for structured grid conversion. // multiblock: Multi-block grid or not, only for structured grid conversion.
// 0 -- Not. // 0 -- Not.
// 1 -- Yes. // 1 -- Yes.
// grid_database_index: Case of typical case, only for gridobj=0. // grid_database_index: Case of typical case, only for gridobj=0.
// 1 -- Laminar flat plate of subsonic flow. // 1 -- Laminar flat plate of subsonic flow.
// 2 -- Laminar flat plate of supersonic flow. // 2 -- Laminar flat plate of supersonic flow.
@ -33,28 +33,28 @@
// 4 -- Turbulent flat plate of supersonic flow. // 4 -- Turbulent flat plate of supersonic flow.
// iadapt: Adaptation number for unstructure grid. // iadapt: Adaptation number for unstructure grid.
// iovrlap: Overlapping(overset) grid or not. // iovrlap: Overlapping(overset) grid or not.
// 0 -- NON-overlapping grid. // 0 -- NON-overlapping grid.
// 1 -- Overlapping grid. // 1 -- Overlapping grid.
// SymmetryFaceVector: The vector of symmetry face. // SymmetryFaceVector: The vector of symmetry face.
// 0 -- X axis. // 0 -- X axis.
// 1 -- Y axis. // 1 -- Y axis.
// 2 -- Z axis. // 2 -- Z axis.
int gridtype = 0; int gridtype = 0;
int gridobj = 1; int gridobj = 1;
int multiblock = 0; int multiblock = 0;
int grid_database_index = 3; int grid_database_index = 3;
int iadapt = 0; int iadapt = 0;
int iovrlap = 0; int iovrlap = 0;
int SymmetryFaceVector = 1; int SymmetryFaceVector = 1;
// axisup: Type of Cartisien coordinates system, used in grid conversion. // axisup: Type of Cartisien coordinates system, used in grid conversion.
// 1 -- Y upward. (default) // 1 -- Y upward. (default)
// 2 -- Z upward. // 2 -- Z upward.
int axisup = 1; int axisup = 1;
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition". // omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
// 0 -- Interface. (default) // 0 -- Interface. (default)
// 1 -- Physical boundary condition, used in Hybrid solver. // 1 -- Physical boundary condition, used in Hybrid solver.
int omit_no_bound_bc = 0; int omit_no_bound_bc = 0;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -63,19 +63,19 @@ int omit_no_bound_bc = 0;
// from_gtype/to_gtype: Type of grid data type in grid conversion process. // from_gtype/to_gtype: Type of grid data type in grid conversion process.
// -1 -- MULTI_TYPE. // -1 -- MULTI_TYPE.
// 1 -- PHengLEI, *.fts. // 1 -- PHengLEI, *.fts.
// 2 -- CGNS, *.cgns. // 2 -- CGNS, *.cgns.
// 3 -- Plot3D type of structured grid, *.dat/*.grd. // 3 -- Plot3D type of structured grid, *.dat/*.grd.
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp. // 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
// 5 -- Fluent, *.cas/*.msh. // 5 -- Fluent, *.cas/*.msh.
// 6 -- Ustar, mgrid.in. // 6 -- Ustar, mgrid.in.
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts. // 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
// 8 -- GMSH, *.msh. // 8 -- GMSH, *.msh.
// dumpOldGrid: If dump out the old grid file. // dumpOldGrid: If dump out the old grid file.
// 0 -- Not. (default) // 0 -- Not. (default)
// 1 -- Yes. // 1 -- Yes.
int from_gtype = 2; int from_gtype = 2;
int to_gtype = 1; int to_gtype = 1;
int dumpOldGrid = 0; int dumpOldGrid = 0;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# File path # # File path #
@ -87,13 +87,13 @@ string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
// ----------------- some advanced choices ------------------------------ // ----------------- some advanced choices ------------------------------
// iunsteady: The Grid is for unsteady simulation or not. // iunsteady: The Grid is for unsteady simulation or not.
int iunsteady = 0; int iunsteady = 0;
int iale = 0; int iale = 0;
// fileformat: Ustar Grid file format. // fileformat: Ustar Grid file format.
// 0 -- BINARY. // 0 -- BINARY.
// 1 -- ASCII. // 1 -- ASCII.
int fileformat = 0; int fileformat = 0;
// .skl meaning skeleton. // .skl meaning skeleton.
string original_grid_info_file = "./grid/FLUENT_test.skl"; string original_grid_info_file = "./grid/FLUENT_test.skl";
@ -102,22 +102,22 @@ string original_grid_info_file = "./grid/FLUENT_test.skl";
// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type. // mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type.
// mixgrid_str: path of structure grid file for hybrid solver, *.fts type. // mixgrid_str: path of structure grid file for hybrid solver, *.fts type.
// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver. // mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver.
string mixgrid_uns = "./grid/rae2822_uns2d_4.fts"; string mixgrid_uns = "./grid/rae2822_uns2d_4.fts";
string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts"; string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts";
string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp"; string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp";
// Some parameters for structured overlapping grid. // Some parameters for structured overlapping grid.
int codeOfDigHoles = 1; int codeOfDigHoles = 1;
string holeBasicFileName = "./oversetGridView/holeBasicFile.inp"; string holeBasicFileName = "./oversetGridView/holeBasicFile.inp";
string holeFullFileName = "./oversetGridView/holeFullFile.dat"; string holeFullFileName = "./oversetGridView/holeFullFile.dat";
string linkFileName = "./oversetGridView/topology.dat"; string linkFileName = "./oversetGridView/topology.dat";
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp"; string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
// ----------------- Adaptive Mesh Refine ------------------------------- // ----------------- Adaptive Mesh Refine -------------------------------
// In this file, the original_grid_file is used of the partition part. // In this file, the original_grid_file is used of the partition part.
// If use it dependently, abstract it here. // If use it dependently, abstract it here.
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts"; string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
string geometryFileName = "./grid/jsm.igs"; string geometryFileName = "./grid/jsm.igs";
// geometryUnit: Geometry unit. // geometryUnit: Geometry unit.
// 1 -- meter. // 1 -- meter.
@ -130,11 +130,11 @@ string geometryFileName = "./grid/jsm.igs";
// projectOrgPoint: If the original wall points need to be projected or not. // projectOrgPoint: If the original wall points need to be projected or not.
int geometryUnit = 1; int geometryUnit = 1;
int anisoRefine = 0; int anisoRefine = 0;
int isProject = 0; int isProject = 0;
int readDist = 0; int readDist = 0;
int isDeform = 0; int isDeform = 0;
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT. int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
int projectOrgPoint = 0; // if project original wall points. int projectOrgPoint = 0; // if project original wall points.
// ----------------- RBF Parameters ------------------------------------- // ----------------- RBF Parameters -------------------------------------
// symmetryPlane: Which symmetry plane is used in the mesh. // symmetryPlane: Which symmetry plane is used in the mesh.
@ -146,24 +146,34 @@ int numberOfReferenceCP = 10;
double influenceRadius = 20; double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// ----------------- Periodic Parameters --------------------------------
// Notice:Rotational periodicity only support rotation along the X axis!
// periodicType: Which periodic boundary is used.
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
######################################################################### #########################################################################
# Default parameters for Partition # # Default parameters for Partition #
######################################################################### #########################################################################
// pgridtype: The grid type. // pgridtype: The grid type.
// 0 -- unstruct grid. // 0 -- unstruct grid.
// 1 -- struct grid. // 1 -- struct grid.
// 2 -- refine structured grid. // 2 -- refine structured grid.
// maxproc: The number of partition zones that want to be divided into. // maxproc: The number of partition zones that want to be divided into.
int pgridtype = 0; int pgridtype = 0;
int maxproc = 4; int maxproc = 4;
// traceMark: Trace mark or not, only for structured grid partition. // traceMark: Trace mark or not, only for structured grid partition.
// 0 -- Not. // 0 -- Not.
// 1 -- Yes. // 1 -- Yes.
// blockIndexOfMark: the block index of mark, only for structured grid partition. // blockIndexOfMark: the block index of mark, only for structured grid partition.
// cellIndexOfMark: the cell index of mark, only for structured grid partition. // cellIndexOfMark: the cell index of mark, only for structured grid partition.
int traceMark = 0; int traceMark = 0;
int blockIndexOfMark = 0; int blockIndexOfMark = 0;
int cellIndexOfMark[] = [185,30,1]; int cellIndexOfMark[] = [185,30,1];
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -171,22 +181,22 @@ int cellIndexOfMark[] = [185,30,1];
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts). // original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts). // partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
string original_grid_file = "./grid/sphere_mixed.fts"; string original_grid_file = "./grid/sphere_mixed.fts";
string partition_grid_file = "./grid/sphere_mixed__4.fts"; string partition_grid_file = "./grid/sphere_mixed__4.fts";
// ------------------ Sompe advanced parameters ------------------------- // ------------------ Sompe advanced parameters -------------------------
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition". // omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
// 0 -- Interface. (default) // 0 -- Interface. (default)
// 1 -- Physical boundary condition, used in Hybrid solver. // 1 -- Physical boundary condition, used in Hybrid solver.
// npartmethod: Method of interface reconstruction, default is 1. // npartmethod: Method of interface reconstruction, default is 1.
// parallelPartMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition. // parallelPartMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition.
// 1 -- Using ParMetis for homogeneous MPI. // 1 -- Using ParMetis for homogeneous MPI.
// 2 -- Using Metis for homogeneous MPI. // 2 -- Using Metis for homogeneous MPI.
// 3 -- using METIS partition for homogeneous OpenMP. // 3 -- using METIS partition for homogeneous OpenMP.
// parmetisBalance: Used to specify the imbalance tolerance. // parmetisBalance: Used to specify the imbalance tolerance.
// 1 -- perfect balance. // 1 -- perfect balance.
// maxproc -- perfect imbalance. // maxproc -- perfect imbalance.
// 1.05 -- recommended. // 1.05 -- recommended.
int omit_no_bound_bc = 0; int omit_no_bound_bc = 0;
int npartmethod = 1; int npartmethod = 1;
@ -197,7 +207,7 @@ double parmetisBalance = 1.05;
// 1 -- single level. // 1 -- single level.
// 2 -- 2 level. // 2 -- 2 level.
// N -- N level, ..., et al. // N -- N level, ..., et al.
int numberOfMultigrid = 1; int numberOfMultigrid = 1;
######################################################################### #########################################################################
# Default parameters for CFD simulation # # Default parameters for CFD simulation #
@ -205,80 +215,88 @@ int numberOfMultigrid = 1;
// maxSimuStep: The max simulation step, don't care simulation is restart or not. // maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. // intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual 'res.dat' saved. // intervalStepRes: The step intervals for residual file 'res.dat' saved.
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. // ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
// 0 -- no precondition process. (default, mach > 0.3) // 0 -- no precondition process. (default, mach > 0.3)
// 1 -- carry out precondition process. (mach number <= 0.3) // 1 -- carry out precondition process. (mach number <= 0.3)
int maxSimuStep = 3000; int maxSimuStep = 20000;
int intervalStepFlow = 100; int intervalStepFlow = 1000;
int intervalStepPlot = 100; int intervalStepPlot = 1000;
int intervalStepForce = 1; int intervalStepSample = 1000;
int intervalStepRes = 1; int intervalStepForce = 100;
int ifLowSpeedPrecon = 0; int intervalStepRes = 10;
int ifLowSpeedPrecon = 0;
// compressible: // compressible:
// 0 -- incompressible flow. // 0 -- incompressible flow.
// 1 -- compressible flow. (default) // 1 -- compressible flow. (default)
int compressible = 1; int compressible = 1;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# CFD Control Parameter # # CFD Control Parameter #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
// refMachNumber: Mach number. // refMachNumber: Mach number.
// attackd: Angle of attack. // attackd: Angle of attack.
// angleSlide: Angle of sideslip. // angleSlide: Angle of sideslip.
// inflowParaType: The type of inflow parameters. // inflowParaType: The type of inflow parameters.
// 0 -- the nondimensional conditions. // 0 -- the nondimensional conditions.
// 1 -- the flight conditions. // 1 -- the flight conditions.
// 2 -- the experiment conditions. // 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions. // 3 -- the subsonic boundary conditions.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature. // freestream_vibration_temperature: Dimensional freestream vibration temperature.
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition. // refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
// height: Fly height, unit of km. // height: Fly height, unit of km.
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition. // wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
// dump_Q: Dump out thermal flux Q of solid wall. // dump_Q: Dump out thermal flux Q of solid wall.
// 0 -- no dump out. // 0 -- no dump out.
// 1 -- dump out wall Q only. // 1 -- dump out wall Q only.
// 2 -- dump out wall Q & the typical position Q of ball. // 2 -- dump out wall Q & the typical position Q of ball.
// 3 -- dump out wall Q & the typical position Q of cone. // 3 -- dump out wall Q & the typical position Q of cone.
// 4 -- dump out wall Q & the typical position Q of double sphere. // 4 -- dump out wall Q & the typical position Q of double sphere.
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter. // 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.
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit. // forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit. // TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
// radiationCoef: the radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary // radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary
// condition is radiation equilibrium temperature, and 0.8 is the default value. // condition is radiation equilibrium temperature, and 0.8 is the default value.
double refMachNumber = 0.20; double refMachNumber = 0.73;
double attackd = 0.00; double attackd = 2.79;
double angleSlide = 0.00; double angleSlide = 0.00;
int inflowParaType = 0; int inflowParaType = 0;
double refReNumber = 3900; double refReNumber = 6.5e6;
double refDimensionalTemperature = 288.15; double refDimensionalTemperature = 288.15;
double freestream_vibration_temperature = 10000.00; double freestream_vibration_temperature = 10000.00;
//int inflowParaType = 1; //int inflowParaType = 1;
//double height = 0.001; //double height = 0.001;
//int inflowParaType = 2; //int inflowParaType = 2;
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/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 refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
//int inflowParaType = 3; //int inflowParaType = 3;
//int nsubsonicInlet = 1; //int nsubsonicInlet = 1;
//int nsubsonicOutlet = 1; //int nsubsonicOutlet = 1;
//string inLetFileName = "./bin/subsonicInlet.hypara"; //string inLetFileName = "./bin/subsonicInlet.hypara";
//string outLetFileName = "./bin/subsonicOutlet.hypara"; //string outLetFileName = "./bin/subsonicOutlet.hypara";
//double refDimensionalTemperature = 288.144; //double refDimensionalTemperature = 288.144;
//double refDimensionalPressure = 1.01313E05; //double refDimensionalPressure = 1.01313E05;
double wallTemperature = -1.0; 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 gridScaleFactor = 1.0;
@ -290,29 +308,11 @@ double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter.
// directionMethod: The method of determining direction.
// 1 -- using direciton.
// 2 -- using face normal.
// subsonicInletTotalPressure: The total pressure of subsonic inlet.
// subsonicInletTotalTemperature: The total temperature of subsonic inlet.
// direction_inlet: The direction of inlet.
// subsonicOutletTotalPressure: The total pressure of subsonic outlet.
// subsonicOutletTotalTemperature: The total temperature of subsonic outlet.
// direction_outlet: The direction of outlet.
int directionMethod = 2;
double subsonicInletTotalPressure = 1.2e6;
double subsonicInletTotalTemperature = 1300;
double direction_inlet[] = 1, 0, 0;
double subsonicOutletTotalPressure = 17.8571428;
double subsonicOutletTotalTemperature = 1.0;
double direction_outlet[] = 1, 0, 0;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Spatial Discretisation # # Spatial Discretisation #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
#******************************************************************* #*******************************************************************
# Struct Solver * # Struct Solver *
#******************************************************************* #*******************************************************************
// inviscidSchemeName: Spatial discretisation scheme of struct grid. // inviscidSchemeName: Spatial discretisation scheme of struct grid.
// Using this when solve structered grid or hybrid. // Using this when solve structered grid or hybrid.
@ -323,13 +323,13 @@ double direction_outlet[] = 1, 0, 0;
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth". // -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
// -- "nolim", no limiter. // -- "nolim", no limiter.
// -- "vanalbada_clz", clz supersonic version. // -- "vanalbada_clz", clz supersonic version.
string inviscidSchemeName = "roe"; string inviscidSchemeName = "roe";
string str_limiter_name = "vanalbada"; string str_limiter_name = "vanalbada";
#******************************************************************* #*******************************************************************
# UnStruct Solver or Common * # UnStruct Solver or Common *
#******************************************************************* #*******************************************************************
// iviscous: Viscous model. // viscousType: Viscous model.
// 0 -- Euler. // 0 -- Euler.
// 1 -- Lamilar. // 1 -- Lamilar.
// 2 -- Algebraic. // 2 -- Algebraic.
@ -352,14 +352,14 @@ string str_limiter_name = "vanalbada";
// 2 -- DDES. // 2 -- DDES.
// 3 -- IDDES. // 3 -- IDDES.
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid. // Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle". // -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus". // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
// uns_limiter_name: Limiter of Unstruct grid. // uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod". // -- "barth", "vencat", "vanleer", "minmod".
// -- "vanalbada", "smooth", "nnd", "lpz", "1st". // -- "vanalbada", "smooth", "nnd", "lpz", "1st".
// -- "nolim", no limiter. // -- "nolim", no limiter.
// uns_vis_name: Discretisation method of viscous term. // uns_vis_name: Discretisation method of viscous term.
// -- "std", "test", "aver", "new1", "new2". // -- "std", "test", "aver", "new1", "new2".
// uns_gradient: Gradient reconstruction method. // uns_gradient: Gradient reconstruction method.
// -- "default", "ggcell", "ggnode", "lsq". // -- "default", "ggcell", "ggnode", "lsq".
@ -369,7 +369,7 @@ string str_limiter_name = "vanalbada";
// 4 -- Ustar limiter model, without grid size unitary. // 4 -- Ustar limiter model, without grid size unitary.
// 7 -- default used. // 7 -- default used.
// venkatCoeff: Cofficient of vencat, when using vencat limter. // venkatCoeff: Cofficient of vencat, when using vencat limter.
// limitVariables: Limit model. // limitVariables: Limit model (It is useful only if limitVector is 0).
// 0 -- limit only for pressure and denstiny, then get the min value. // 0 -- limit only for pressure and denstiny, then get the min value.
// 1 -- limit for every variables, then get the min value. // 1 -- limit for every variables, then get the min value.
// limitVector: // limitVector:
@ -386,46 +386,46 @@ string str_limiter_name = "vanalbada";
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0. // roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
// It is used to scale the default Roe entropy fix coefficients. // It is used to scale the default Roe entropy fix coefficients.
//int iviscous = 0; //int viscousType = 0;
//string viscousName = "Euler"; //string viscousName = "Euler";
int viscousType = 1; //int viscousType = 1;
string viscousName = "laminar"; //string viscousName = "laminar";
//int iviscous = 3; int viscousType = 3;
//string viscousName = "1eq-sa"; string viscousName = "1eq-sa";
//int iviscous = 4; //int viscousType = 4;
//string viscousName = "2eq-kw-menter-sst"; //string viscousName = "2eq-kw-menter-sst";
int DESType = 0; int DESType = 0;
string uns_scheme_name = "roe"; string uns_scheme_name = "roe";
string uns_limiter_name = "vencat"; string uns_limiter_name = "vencat";
string uns_vis_name = "test"; string uns_vis_name = "test";
string gradientName = "ggnode"; string gradientName = "ggnode";
int ivencat = 7; int ivencat = 7;
double venkatCoeff = 5.0; double venkatCoeff = 5.0;
int reconmeth = 1; int reconmeth = 1;
int limitVariables = 0; int limitVariables = 0;
int limitVector = 0; int limitVector = 0;
double limit_angle = 0; double limit_angle = 0;
double skewnessAngle = 60.0; double skewnessAngle = 60.0;
int roeEntropyFixMethod = 3; int roeEntropyFixMethod = 3;
double roeEntropyScale = 1.0; double roeEntropyScale = 1.0;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Temporal Discretisation # # Temporal Discretisation #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
// iunsteady: Steady or unsteady. // iunsteady: Steady or unsteady.
// 0 -- steady. // 0 -- steady.
// 1 -- unsteay. // 1 -- unsteay.
// physicalTimeStep: The nondimensional physical time step. // physicalTimeStep: The nondimensional physical time step.
// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes. // ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes.
// ifStaticsFlowField: Statistical variables for DES simulation. // ifStaticsFlowField: Statistical variables for DES simulation.
// startStatisticStep: Outer step when start statistics. // startStatisticStep: Outer step when start statistics.
// when the value is larger than "maxSimuStep", it is useless. // when the value is larger than "maxSimuStep", it is useless.
// min_sub_iter: The min sub iteration of unsteady simulation. // min_sub_iter: The min sub iteration of unsteady simulation.
// max_sub_iter: The max sub iteration of unsteady simulation. // max_sub_iter: The max sub iteration of unsteady simulation.
@ -441,14 +441,14 @@ double roeEntropyScale = 1.0;
// 8 -- Upper G-S iteration. // 8 -- Upper G-S iteration.
// 9 -- Lower/Upper G-S iteration. // 9 -- Lower/Upper G-S iteration.
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
// CFLStart: Started cfl number. // CFLStart: Started cfl number.
// CFLEnd: End cfl number. // CFLEnd: End cfl number.
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS. // LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS.
// ifLocalTimeStep: Time step method. // ifLocalTimeStep: Time step method.
// 0 --Local. // 0 --Local.
// 1 --Global. // 1 --Global.
@ -466,64 +466,64 @@ double roeEntropyScale = 1.0;
// RKStage: The number of Runge-Kutta step. // RKStage: The number of Runge-Kutta step.
// lamda: Cofficient of Runge-Kutta step. // lamda: Cofficient of Runge-Kutta step.
int iunsteady = 1; int iunsteady = 0;
double physicalTimeStep = 0.005; double physicalTimeStep = 0.01;
int ifStartFromSteadyResults = 0; int ifStartFromSteadyResults = 0;
int ifStaticsFlowField = 0; int ifStaticsFlowField = 0;
int startStatisticStep = 0; int startStatisticStep = 800000;
int min_sub_iter = 20; int min_sub_iter = 50;
int max_sub_iter = 20; int max_sub_iter = 50;
double tol_sub_iter = 0.01; double tol_sub_iter = 0.01;
int tscheme = 4; int tscheme = 4;
int iSimplifyViscousTerm = 1; int iSimplifyViscousTerm = 1;
int ifLocalTimeStep = 0; int ifLocalTimeStep = 0;
double CFLStart = 0.01; double CFLStart = 0.01;
double CFLEnd = 10.0; double CFLEnd = 10.0;
int CFLVaryStep = 500; int CFLVaryStep = 500;
double ktmax = 1.0e10; double ktmax = 1.0e10;
int swapDq = 1; int swapDq = 1;
int nLUSGSSweeps = 1; int nLUSGSSweeps = 1;
double LUSGSTolerance = 0.01; double LUSGSTolerance = 0.01;
int order = 2; int order = 2;
double visl_min = 0.01; double visl_min = 0.01;
double turbCFLScale = 1.0; double turbCFLScale = 1.0;
double timemax = 1.0e10; double timemax = 1.0e10;
double dtsave = -1.0; double dtsave = -1.0;
int iale = 0; int iale = 0;
int ialetype = 2; int ialetype = 2;
int maxale = 10; int maxale = 10;
double dtau = 0.001; double dtau = 0.001;
double dtau_max = 1E-01; double dtau_max = 1E-01;
int wallFunctionType = 1; int wallFunctionType = 0;
int RKStage = 2; int RKStage = 2;
double [] = 0.5, 1.0; double lamda[] = 0.5, 1.0;
//int RKStage = 1; //int RKStage = 1;
//double lamda[] = 1.0; //double lamda[] = 1.0;
//int RKStage = 4; //int RKStage = 4;
//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; //double lamda[] = [0.25, 0.33333333333, 0.5, 1.0];
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# File In or Out # # File In or Out #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
// numberOfGridGroups: The number of grid groups. // numberOfGridGroups: The number of grid groups.
// gridfile: The partitioned Grid file path, using relative path, // gridfile: The partitioned Grid file path, using relative path,
// which is relative to the working directory. // which is relative to the working directory.
// IMPORTANT WARNING: The file index should be ignored, // IMPORTANT WARNING: The file index should be ignored,
// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts, // e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
// please use 'rae2822_hybrid2d__4.fts' here! // please use 'rae2822_hybrid2d__4.fts' here!
// isPlotVolumeField: If dump out the field results to visulization. // isPlotVolumeField: If dump out the field results to visulization.
// walldistMethod: The method to compute wall distance. // walldistMethod: The method to compute wall distance.
// 0 -- accurate but not fast enough. // 0 -- accurate but not fast enough.
// 1 -- fast but not accurate enough. // 1 -- fast but not accurate enough.
// 2 -- super fast but more non-accurate! // 2 -- super fast but more non-accurate!
@ -535,39 +535,39 @@ double [] = 0.5, 1.0;
// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps. // visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps.
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps. // wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
int numberOfGridGroups = 1; int numberOfGridGroups = 1;
string gridfile = "./grid/cylinder_Re3900_270w_split120.fts"; string gridfile = "./grid/rae2822_hybrid2d__4.fts";
int walldistMethod = 1; int walldistMethod = 1;
string resSaveFile = "results/res.dat"; string resSaveFile = "results/res.dat";
string turbresfile = "results/turbres.dat"; string turbresfile = "results/turbres.dat";
string aircoeffile = "results/aircoef.dat"; string aircoeffile = "results/aircoef.dat";
string restartNSFile = "results/flow.dat"; string restartNSFile = "results/flow.dat";
string turbfile = "results/turb.dat"; string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt"; string visualfile = "results/tecflow.plt";
string Qwall_file = "results/Qwall.dat"; string Qwall_file = "results/Qwall.dat";
string wall_aircoefile = "results/wall_aircoef.dat"; string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string surfacefile = ""; string surfacefile = "";
string wall_varfile = ""; string wall_varfile = "";
string componentDefineFile = "bin/component.hypara"; string componentDefineFile = "bin/component.hypara";
string jetDefineFile = "bin/jet.hypara"; string jetDefineFile = "bin/jet.hypara";
string componentforcefile = "results/component_aircoef.dat"; string componentforcefile = "results/component_aircoef.dat";
string overset_gridfile = "iblank.ovs"; string overset_gridfile = "iblank.ovs";
int isPlotVolumeField = 1; int isPlotVolumeField = 0;
// visualfileType: The file type of visualfile. // visualfileType: The file type of visualfile.
// 0 -- Tecplot binary. // 0 -- Tecplot binary.
// 1 -- Tecplot ASCII. // 1 -- Tecplot ASCII.
int visualfileType = 0; int visualfileType = 1;
// visualSlice: The slice of tecflow. // visualSlice: The slice of tecflow.
// 0 -- Do not save slice data. // 0 -- Do not save slice data.
@ -578,27 +578,45 @@ int visualfileType = 0;
// 3 -- Z_DIR. // 3 -- Z_DIR.
// slicePostion: Coordinate of slice. // slicePostion: Coordinate of slice.
int visualSlice = 0; int visualSlice = 0;
int sliceAxis = 1; int sliceAxis = 1;
double slicePostion = -0.5; double slicePostion = -0.5;
string sliceFile = "results/Slice.plt"; string sliceFile = "results/Slice.plt";
// min-max box of the visual block. // min-max box of the visual block.
double lowerPlotFieldBox[] = [0.0 0.0 0.0]; double lowerPlotFieldBox[] = [0.0 0.0 0.0];
double upperPlotFieldBox[] = [1.0 1.0 1.0]; double upperPlotFieldBox[] = [1.0 1.0 1.0];
// nVisualVariables: Number of variables want to be dumped for tecplot visualization. // nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables : variable types dumped, listed as following: // visualVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6) // -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
// -- viscosityLaminar(7), viscosityTurbulent(8), // -- viscosityLaminar(7), viscosityTurbulent(8),
// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12), strain_rate(13), Q_criteria(14) // -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12),
// -- Cp(15), timeStep(16), volume(17) // -- strain_rate(13), Q_criteria(14), Cp(15), timeStep(16), volume(17),
// -- modeledTKE(18),modeleddissipationrate(19), SSTF1(20), SSTF2(21) ,vibration temperature(33), electron temperature(34) // -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), vibration temperature(33), electron temperature(34),
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!. // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44).
// Arriables order must from small to larger. // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
int nVisualVariables = 10; // Variables order must from small to big.
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 11, 12, 15];; int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate.
int dumpStandardModel = 0;
// ifSetProbesToMonitor: Set probes location to Monitor.
// 0 -- Do not monitor.
// 1 -- To monitor and save data to files.
// probesDefineFile: probes location information file.
// nProbeVariables: Number of variables want to be dumped for probes monitered.
// probeVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
// probeVariables order must from small to big.
int ifSetProbesToMonitor = 0;
string probesDefineFile = "bin/probes_location.hypara";
int nProbeVariables = 6;
int probeVariables[] = [0, 1, 2, 3, 4, 5];
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Turbulence Parameter # # Turbulence Parameter #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -615,56 +633,16 @@ int kindOfTurbSource = 0;
int mod_turb_res = 0; int mod_turb_res = 0;
double turb_relax = 1.0; double turb_relax = 1.0;
double turb_min_coef = 1.0e-1; double turb_min_coef = 1.0e-1;
double freeStreamViscosity = 1.0e-3; double freeStreamViscosity = 1.0e-3;
double muoo = 1.0e-1; double muoo = 1.0e-1;
double kwoo = 1.0; double kwoo = 1.0;
# maximum eddy viscosity (myt/my) max. # maximum eddy viscosity (myt/my) max.
double eddyViscosityLimit = 1.0e5; double eddyViscosityLimit = 1.0e10;
double sdilim = 1.0e20; double sdilim = 1.0e20;
double coef_kvist = 1.0; double coef_kvist = 1.0;
int monitor_vistmax = 0; int monitor_vistmax = 0;
//-----------------------------------------------------------------------
# LES Parameter #
//-----------------------------------------------------------------------
// iLES : Create LESSolver or not.
// >= 1 - Create LESSolver;
// < 1 - not;
// sgsmodel : subgrid scale model
// = "smagorinsky" ;
// = "dsm" ;
// = "wale" ;
// deltaFunctionType : = 1 - MAX(deltai, deltaj, deltak)
// = 2 - pow(deltai * deltaj *deltak, 1/3)
// = 3 - Devloped by Scotti
// wallDampingFunctionType : = 0 - no wall function
// = 1 - van Driest
// = 2 - developed by Dr. Deng Xiaobing
// = 3 - developed by Piomelli
// turbViscousCutType : turbulent viscosity cut type
// = 0 - mu_total = mut + mul
// = 1 - mu_total = max(mut-mul,0)+ mul
// = 2 - mu_total = max(mut ,0)+ mul
// smagConstant : constant of smagorinsky model.
// waleConstant : constant of wale model
// filterDirection[3] : filter variables in i, j, k direction or not;
// averageDirection[3] : average variables in i, j, k direction or not;
// isotropicConstant : constant of isotropic part of SGS stress
int iLES = 1;
string sgsmodel = "smagorinsky";
int deltaFunctionType = 2;
int wallDampingFunctionType = 1;
int turbViscousCutType = 2;
double smagConstant = 0.135;
double isotropicConstant = 0.0;
double waleConstant = 0.6;
int filterDirection[] = [1, 1, 0];
int averageDirection[] = [1, 1, 0];
double testFilterScale = 2.0;
int averageWidth = 1;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Other Parameter # # Other Parameter #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -698,41 +676,41 @@ int averageWidth = 1;
// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. // "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions.
// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. // "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions.
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. // "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
// For self-definition model, the gasfile is used to indicate the file path of the new gas model. // For self-definition model, the gasfile is used to indicate the file path of the new gas model.
// speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma.
// initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName.
// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes. // ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes.
int dg_high_order = 0; int dg_high_order = 0;
int iapplication = 0; int iapplication = 0;
int nm = 5; int nm = 5;
// MHD // MHD
double bxoo = 0.0; double bxoo = 0.0;
double byoo = 0.0; double byoo = 0.0;
double bzoo = 0.0; double bzoo = 0.0;
double refGama = 1.4; double refGama = 1.4;
double prl = 0.72; double prl = 0.72;
double prt = 0.90; double prt = 0.90;
double sc_l = 0.5; double sc_l = 0.5;
double sc_t = 0.5; double sc_t = 0.5;
int nchem = 0; int nchem = 0;
int nchemsrc = 1; int nchemsrc = 1;
int nchemrad = 1; int nchemrad = 1;
int ntmodel = 1; int ntmodel = 1;
int nChemicalFlowStep = 0; int nChemicalFlowStep = 0;
double catalyticCoef = 0.0; double catalyticCoef = 0.0;
string gasfile = "DK5"; string gasfile = "DK5";
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; //string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
string speciesName = "O, O2, NO, N, N2"; string speciesName = "O, O2, NO, N, N2";
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77"; string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
//string speciesName = "O, O2, NO, N, NO+, N2, e-"; //string speciesName = "O, O2, NO, N, NO+, N2, e-";
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.77, 0.0"; //string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.77, 0.0";
//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-"; //string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-";
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.77, 0.0"; //string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.77, 0.0";
int ifStartFromPerfectGasResults = 0; int ifStartFromPerfectGasResults = 0;
@ -749,22 +727,22 @@ int ifStartFromPerfectGasResults = 0;
// 1 -- V-multi cycle. // 1 -- V-multi cycle.
// 2 -- W-multi cycle. // 2 -- W-multi cycle.
// flowInitStep: Flow initialization step, 0 - 500 is suggested. // flowInitStep: Flow initialization step, 0 - 500 is suggested.
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization. // 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. // Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
// mgCFLScale: CFL number enlarge times for coarse grid. // mgCFLScale: CFL number enlarge times for coarse grid.
// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid. // mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid.
// 1 -- zero order. // 1 -- zero order.
// 2 -- first-order. (default) // 2 -- first-order. (default)
// mgCorrectionLimit: Multi-grid correction limit. // mgCorrectionLimit: Multi-grid correction limit.
int nMGLevel = 1; int nMGLevel = 1;
int MGCoarsestIteration = 1; int MGCoarsestIteration = 1;
int MGPreIteration = 1; int MGPreIteration = 1;
int MGFasType = 1; int MGFasType = 1;
int n_post = 0; int n_post = 0;
int flowInitStep = 100; int flowInitStep = 100;
int mprol = 2; int mprol = 2;
double mgCFLScale = 1.0; double mgCFLScale = 1.0;
double mgCorrectionLimit = 0.01; double mgCorrectionLimit = 0.01;
//--------------- Some parameter for turbulent model -------------------- //--------------- Some parameter for turbulent model --------------------
@ -778,16 +756,16 @@ int ismooth_turb = 0;
int SAProductType = 2; int SAProductType = 2;
// ----------------- Overset Grid parameter ----------------------------- // ----------------- Overset Grid parameter -----------------------------
int codeOfDigHoles = 1; int codeOfDigHoles = 1;
int codeOfTurbulentModel = 0; int codeOfTurbulentModel = 0;
string masterFileName = "./grid/searchFile.inp"; string masterFileName = "./grid/searchFile.inp";
string holeBasicFileName = "./grid/holeBasicFile.inp"; string holeBasicFileName = "./grid/holeBasicFile.inp";
string holeFullFileName = "./grid/holeFullFile.dat"; string holeFullFileName = "./grid/holeFullFile.dat";
string linkFileName = "./grid/topology.dat"; string linkFileName = "./grid/topology.dat";
string zoneInverseFileName = "./grid/zoneInverseMapping.inp"; string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
######################################################################### #########################################################################
# High Order Struct Solver # # High Order Struct Solver #
######################################################################### #########################################################################
// ifvfd: // ifvfd:
// 0 -- NSSolverStruct using Finite Volume Method. // 0 -- NSSolverStruct using Finite Volume Method.
@ -805,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// structhighordergradient: // structhighordergradient:
// -- "conservation", "chain_rule". // -- "conservation", "chain_rule".
int ifvfd = 0; int ifvfd = 0;
int SolverStructOrder = 0; string str_highorder_solver = "WCNS";
int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6; double str_highorder_interpolation_epsilon = 1.0e-6;
string str_highorder_interpolation_type = "test"; string str_highorder_interpolation_type = "test";
string str_highorder_flux_name = "steger"; string str_highorder_flux_name = "steger";
string structhighordergradient = "conservation"; string structhighordergradient = "conservation";
double coefofstrflux = 0.5;
double limitcoefofinterface = 0.0;
// ----------------- Advanced choices ----------------------------------- // ----------------- Advanced choices -----------------------------------
// outtimesc: Time stepping scheme for the outer loop. // outtimesc: Time stepping scheme for the outer loop.
@ -822,17 +803,17 @@ string structhighordergradient = "conservation";
// 0 -- the effect of the limiter is cancelled, means the first-order interpolations. // 0 -- the effect of the limiter is cancelled, means the first-order interpolations.
// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1. // allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1.
string outtimesc = "impbd2"; string outtimesc = "impbd2";
double MUSCLCoefXk = 0.8; double MUSCLCoefXk = -1;
double MUSCLCoefXb = 1.0; double MUSCLCoefXb = 1.0;
int allReduceStep = 1; int allReduceStep = 1;
// ---------------- ATP read -------------------------------------------- // ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0; //@int inflowParaType = 0;
//@double refReNumber = 2.329418E08; //@double refReNumber = 2.329418E08;
//@double refDimensionalTemperature = 288.144; //@double refDimensionalTemperature = 288.144;
//@double refDimensionalPressure = 1.01313E05; //@double refDimensionalPressure = 1.01313E05;
//@double height = -0.001; //@double height = -0.001;
//@int nsubsonicInlet = 0; //@int nsubsonicInlet = 0;
//@int nsubsonicOutlet = 0; //@int nsubsonicOutlet = 0;
//@string inLetFileName = "./bin/subsonicInlet.hypara"; //@string inLetFileName = "./bin/subsonicInlet.hypara";
//@string outLetFileName = "./bin/subsonicOutlet.hypara"; //@string outLetFileName = "./bin/subsonicOutlet.hypara";

50
ThreeD_DoubleEllipse_Laminar_HighOrder_Struct/ThreeD_DoubleEllipse_Laminar_HighOrder_Struct/bin/cfd_para.hypara
View File

@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
double influenceRadius = 20; double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// ----------------- Periodic Parameters --------------------------------
// Notice:Rotational periodicity only support rotation along the X axis!
// periodicType: Which periodic boundary is used.
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
######################################################################### #########################################################################
# Default parameters for Partition # # Default parameters for Partition #
######################################################################### #########################################################################
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
// maxSimuStep: The max simulation step, don't care simulation is restart or not. // maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. // intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual file 'res.dat' saved. // intervalStepRes: The step intervals for residual file 'res.dat' saved.
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. // ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
int intervalStepFlow = 1000; int intervalStepFlow = 1000;
int intervalStepPlot = 1000; int intervalStepPlot = 1000;
int intervalStepSample = 1000;
int intervalStepForce = 100; int intervalStepForce = 100;
int intervalStepRes = 10; int intervalStepRes = 10;
int ifLowSpeedPrecon = 0; int ifLowSpeedPrecon = 0;
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter.
// directionMethod: The method of determining direction.
// 1 -- using direciton.
// 2 -- using face normal.
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
// direction_inlet: The direction of inlet.
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
// direction_outlet: The direction of outlet.
int directionMethod = 2;
double subsonicInletTotalPressure = 1.2e6;
double subsonicInletTotalTemperature = 1300;
double direction_inlet[] = 1, 0, 0;
double subsonicOutletTotalPressure = 17.8571428;
double subsonicOutletTotalTemperature = 1.0;
double direction_outlet[] = 1, 0, 0;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Spatial Discretisation # # Spatial Discretisation #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
#******************************************************************* #*******************************************************************
# UnStruct Solver or Common * # UnStruct Solver or Common *
#******************************************************************* #*******************************************************************
// viscousType : Viscous model. // viscousType: Viscous model.
// 0 -- Euler. // 0 -- Euler.
// 1 -- Lamilar. // 1 -- Lamilar.
// 2 -- Algebraic. // 2 -- Algebraic.
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt"; string visualfile = "results/tecflow.plt";
string Qwall_file = "results/Qwall.dat"; string Qwall_file = "results/Qwall.dat";
string wall_aircoefile = "results/wall_aircoef.dat"; string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string surfacefile = ""; string surfacefile = "";
string wall_varfile = ""; string wall_varfile = "";
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
int dumpStandardModel = 0; int dumpStandardModel = 0;
// ifSetProbesToMonitor: Set probes location to Monitor.
// 0 -- Do not monitor.
// 1 -- To monitor and save data to files.
// probesDefineFile: probes location information file.
// nProbeVariables: Number of variables want to be dumped for probes monitered.
// probeVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
// probeVariables order must from small to big.
int ifSetProbesToMonitor = 0;
string probesDefineFile = "bin/probes_location.hypara";
int nProbeVariables = 6;
int probeVariables[] = [0, 1, 2, 3, 4, 5];
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Turbulence Parameter # # Turbulence Parameter #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// structhighordergradient: // structhighordergradient:
// -- "conservation", "chain_rule". // -- "conservation", "chain_rule".
int ifvfd = 0; int ifvfd = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0; int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6; double str_highorder_interpolation_epsilon = 1.0e-6;
string str_highorder_interpolation_type = "test"; string str_highorder_interpolation_type = "test";
string str_highorder_flux_name = "steger"; string str_highorder_flux_name = "steger";
string structhighordergradient = "conservation"; string structhighordergradient = "conservation";
double coefofstrflux = 0.5;
double limitcoefofinterface = 0.0;
// ----------------- Advanced choices ----------------------------------- // ----------------- Advanced choices -----------------------------------
// outtimesc: Time stepping scheme for the outer loop. // outtimesc: Time stepping scheme for the outer loop.

48
ThreeD_Electre_Laminar_OneTemperMode_NCW_Struct/bin/cfd_para.hypara
View File

@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
double influenceRadius = 20; double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// ----------------- Periodic Parameters --------------------------------
// Notice:Rotational periodicity only support rotation along the X axis!
// periodicType: Which periodic boundary is used.
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
######################################################################### #########################################################################
# Default parameters for Partition # # Default parameters for Partition #
######################################################################### #########################################################################
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
// maxSimuStep: The max simulation step, don't care simulation is restart or not. // maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. // intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual file 'res.dat' saved. // intervalStepRes: The step intervals for residual file 'res.dat' saved.
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. // ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
int intervalStepFlow = 1000; int intervalStepFlow = 1000;
int intervalStepPlot = 1000; int intervalStepPlot = 1000;
int intervalStepSample = 1000;
int intervalStepForce = 100; int intervalStepForce = 100;
int intervalStepRes = 10; int intervalStepRes = 10;
int ifLowSpeedPrecon = 0; int ifLowSpeedPrecon = 0;
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter.
// directionMethod: The method of determining direction.
// 1 -- using direciton.
// 2 -- using face normal.
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
// direction_inlet: The direction of inlet.
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
// direction_outlet: The direction of outlet.
int directionMethod = 2;
double subsonicInletTotalPressure = 1.2e6;
double subsonicInletTotalTemperature = 1300;
double direction_inlet[] = 1, 0, 0;
double subsonicOutletTotalPressure = 17.8571428;
double subsonicOutletTotalTemperature = 1.0;
double direction_outlet[] = 1, 0, 0;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Spatial Discretisation # # Spatial Discretisation #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt"; string visualfile = "results/tecflow.plt";
string Qwall_file = "results/Qwall.dat"; string Qwall_file = "results/Qwall.dat";
string wall_aircoefile = "results/wall_aircoef.dat"; string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string surfacefile = ""; string surfacefile = "";
string wall_varfile = ""; string wall_varfile = "";
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
int dumpStandardModel = 0; int dumpStandardModel = 0;
// ifSetProbesToMonitor: Set probes location to Monitor.
// 0 -- Do not monitor.
// 1 -- To monitor and save data to files.
// probesDefineFile: probes location information file.
// nProbeVariables: Number of variables want to be dumped for probes monitered.
// probeVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
// probeVariables order must from small to big.
int ifSetProbesToMonitor = 0;
string probesDefineFile = "bin/probes_location.hypara";
int nProbeVariables = 6;
int probeVariables[] = [0, 1, 2, 3, 4, 5];
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Turbulence Parameter # # Turbulence Parameter #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// structhighordergradient: // structhighordergradient:
// -- "conservation", "chain_rule". // -- "conservation", "chain_rule".
int ifvfd = 0; int ifvfd = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0; int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6; double str_highorder_interpolation_epsilon = 1.0e-6;
string str_highorder_interpolation_type = "test"; string str_highorder_interpolation_type = "test";
string str_highorder_flux_name = "steger"; string str_highorder_flux_name = "steger";
string structhighordergradient = "conservation"; string structhighordergradient = "conservation";
double coefofstrflux = 0.5;
double limitcoefofinterface = 0.0;
// ----------------- Advanced choices ----------------------------------- // ----------------- Advanced choices -----------------------------------
// outtimesc: Time stepping scheme for the outer loop. // outtimesc: Time stepping scheme for the outer loop.

50
ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para.hypara
View File

@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
double influenceRadius = 20; double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// ----------------- Periodic Parameters --------------------------------
// Notice:Rotational periodicity only support rotation along the X axis!
// periodicType: Which periodic boundary is used.
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
######################################################################### #########################################################################
# Default parameters for Partition # # Default parameters for Partition #
######################################################################### #########################################################################
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
// maxSimuStep: The max simulation step, don't care simulation is restart or not. // maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. // intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual file 'res.dat' saved. // intervalStepRes: The step intervals for residual file 'res.dat' saved.
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. // ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
int intervalStepFlow = 1000; int intervalStepFlow = 1000;
int intervalStepPlot = 1000; int intervalStepPlot = 1000;
int intervalStepSample = 1000;
int intervalStepForce = 100; int intervalStepForce = 100;
int intervalStepRes = 10; int intervalStepRes = 10;
int ifLowSpeedPrecon = 0; int ifLowSpeedPrecon = 0;
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter.
// directionMethod: The method of determining direction.
// 1 -- using direciton.
// 2 -- using face normal.
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
// direction_inlet: The direction of inlet.
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
// direction_outlet: The direction of outlet.
int directionMethod = 2;
double subsonicInletTotalPressure = 1.2e6;
double subsonicInletTotalTemperature = 1300;
double direction_inlet[] = 1, 0, 0;
double subsonicOutletTotalPressure = 17.8571428;
double subsonicOutletTotalTemperature = 1.0;
double direction_outlet[] = 1, 0, 0;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Spatial Discretisation # # Spatial Discretisation #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
#******************************************************************* #*******************************************************************
# UnStruct Solver or Common * # UnStruct Solver or Common *
#******************************************************************* #*******************************************************************
// viscousType : Viscous model. // viscousType: Viscous model.
// 0 -- Euler. // 0 -- Euler.
// 1 -- Lamilar. // 1 -- Lamilar.
// 2 -- Algebraic. // 2 -- Algebraic.
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt"; string visualfile = "results/tecflow.plt";
string Qwall_file = "results/Qwall.dat"; string Qwall_file = "results/Qwall.dat";
string wall_aircoefile = "results/wall_aircoef.dat"; string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string surfacefile = ""; string surfacefile = "";
string wall_varfile = ""; string wall_varfile = "";
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
int dumpStandardModel = 0; int dumpStandardModel = 0;
// ifSetProbesToMonitor: Set probes location to Monitor.
// 0 -- Do not monitor.
// 1 -- To monitor and save data to files.
// probesDefineFile: probes location information file.
// nProbeVariables: Number of variables want to be dumped for probes monitered.
// probeVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
// probeVariables order must from small to big.
int ifSetProbesToMonitor = 0;
string probesDefineFile = "bin/probes_location.hypara";
int nProbeVariables = 6;
int probeVariables[] = [0, 1, 2, 3, 4, 5];
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Turbulence Parameter # # Turbulence Parameter #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// structhighordergradient: // structhighordergradient:
// -- "conservation", "chain_rule". // -- "conservation", "chain_rule".
int ifvfd = 0; int ifvfd = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0; int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6; double str_highorder_interpolation_epsilon = 1.0e-6;
string str_highorder_interpolation_type = "test"; string str_highorder_interpolation_type = "test";
string str_highorder_flux_name = "steger"; string str_highorder_flux_name = "steger";
string structhighordergradient = "conservation"; string structhighordergradient = "conservation";
double coefofstrflux = 0.5;
double limitcoefofinterface = 0.0;
// ----------------- Advanced choices ----------------------------------- // ----------------- Advanced choices -----------------------------------
// outtimesc: Time stepping scheme for the outer loop. // outtimesc: Time stepping scheme for the outer loop.

50
ThreeD_NACA0012_SA_Struct/bin/cfd_para.hypara
View File

@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
double influenceRadius = 20; double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// ----------------- Periodic Parameters --------------------------------
// Notice:Rotational periodicity only support rotation along the X axis!
// periodicType: Which periodic boundary is used.
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
######################################################################### #########################################################################
# Default parameters for Partition # # Default parameters for Partition #
######################################################################### #########################################################################
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
// maxSimuStep: The max simulation step, don't care simulation is restart or not. // maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. // intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual file 'res.dat' saved. // intervalStepRes: The step intervals for residual file 'res.dat' saved.
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. // ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
int intervalStepFlow = 1000; int intervalStepFlow = 1000;
int intervalStepPlot = 1000; int intervalStepPlot = 1000;
int intervalStepSample = 1000;
int intervalStepForce = 100; int intervalStepForce = 100;
int intervalStepRes = 10; int intervalStepRes = 10;
int ifLowSpeedPrecon = 0; int ifLowSpeedPrecon = 0;
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter.
// directionMethod: The method of determining direction.
// 1 -- using direciton.
// 2 -- using face normal.
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
// direction_inlet: The direction of inlet.
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
// direction_outlet: The direction of outlet.
int directionMethod = 2;
double subsonicInletTotalPressure = 1.2e6;
double subsonicInletTotalTemperature = 1300;
double direction_inlet[] = 1, 0, 0;
double subsonicOutletTotalPressure = 17.8571428;
double subsonicOutletTotalTemperature = 1.0;
double direction_outlet[] = 1, 0, 0;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Spatial Discretisation # # Spatial Discretisation #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
#******************************************************************* #*******************************************************************
# UnStruct Solver or Common * # UnStruct Solver or Common *
#******************************************************************* #*******************************************************************
// iviscous: Viscous model. // viscousType: Viscous model.
// 0 -- Euler. // 0 -- Euler.
// 1 -- Lamilar. // 1 -- Lamilar.
// 2 -- Algebraic. // 2 -- Algebraic.
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt"; string visualfile = "results/tecflow.plt";
string Qwall_file = "results/Qwall.dat"; string Qwall_file = "results/Qwall.dat";
string wall_aircoefile = "results/wall_aircoef.dat"; string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string surfacefile = ""; string surfacefile = "";
string wall_varfile = ""; string wall_varfile = "";
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
int dumpStandardModel = 0; int dumpStandardModel = 0;
// ifSetProbesToMonitor: Set probes location to Monitor.
// 0 -- Do not monitor.
// 1 -- To monitor and save data to files.
// probesDefineFile: probes location information file.
// nProbeVariables: Number of variables want to be dumped for probes monitered.
// probeVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
// probeVariables order must from small to big.
int ifSetProbesToMonitor = 0;
string probesDefineFile = "bin/probes_location.hypara";
int nProbeVariables = 6;
int probeVariables[] = [0, 1, 2, 3, 4, 5];
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Turbulence Parameter # # Turbulence Parameter #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// structhighordergradient: // structhighordergradient:
// -- "conservation", "chain_rule". // -- "conservation", "chain_rule".
int ifvfd = 0; int ifvfd = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0; int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6; double str_highorder_interpolation_epsilon = 1.0e-6;
string str_highorder_interpolation_type = "test"; string str_highorder_interpolation_type = "test";
string str_highorder_flux_name = "steger"; string str_highorder_flux_name = "steger";
string structhighordergradient = "conservation"; string structhighordergradient = "conservation";
double coefofstrflux = 0.5;
double limitcoefofinterface = 0.0;
// ----------------- Advanced choices ----------------------------------- // ----------------- Advanced choices -----------------------------------
// outtimesc: Time stepping scheme for the outer loop. // outtimesc: Time stepping scheme for the outer loop.

50
ThreeD_Sphere_Laminar_Ma10_Struct/bin/cfd_para.hypara
View File

@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
double influenceRadius = 20; double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// ----------------- Periodic Parameters --------------------------------
// Notice:Rotational periodicity only support rotation along the X axis!
// periodicType: Which periodic boundary is used.
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
######################################################################### #########################################################################
# Default parameters for Partition # # Default parameters for Partition #
######################################################################### #########################################################################
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
// maxSimuStep: The max simulation step, don't care simulation is restart or not. // maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. // intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual file 'res.dat' saved. // intervalStepRes: The step intervals for residual file 'res.dat' saved.
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. // ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
int intervalStepFlow = 1000; int intervalStepFlow = 1000;
int intervalStepPlot = 1000; int intervalStepPlot = 1000;
int intervalStepSample = 1000;
int intervalStepForce = 100; int intervalStepForce = 100;
int intervalStepRes = 10; int intervalStepRes = 10;
int ifLowSpeedPrecon = 0; int ifLowSpeedPrecon = 0;
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter.
// directionMethod: The method of determining direction.
// 1 -- using direciton.
// 2 -- using face normal.
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
// direction_inlet: The direction of inlet.
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
// direction_outlet: The direction of outlet.
int directionMethod = 2;
double subsonicInletTotalPressure = 1.2e6;
double subsonicInletTotalTemperature = 1300;
double direction_inlet[] = 1, 0, 0;
double subsonicOutletTotalPressure = 17.8571428;
double subsonicOutletTotalTemperature = 1.0;
double direction_outlet[] = 1, 0, 0;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Spatial Discretisation # # Spatial Discretisation #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
#******************************************************************* #*******************************************************************
# UnStruct Solver or Common * # UnStruct Solver or Common *
#******************************************************************* #*******************************************************************
// iviscous: Viscous model. // viscousType: Viscous model.
// 0 -- Euler. // 0 -- Euler.
// 1 -- Lamilar. // 1 -- Lamilar.
// 2 -- Algebraic. // 2 -- Algebraic.
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt"; string visualfile = "results/tecflow.plt";
string Qwall_file = "results/Qwall.dat"; string Qwall_file = "results/Qwall.dat";
string wall_aircoefile = "results/wall_aircoef.dat"; string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string surfacefile = ""; string surfacefile = "";
string wall_varfile = ""; string wall_varfile = "";
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
int dumpStandardModel = 0; int dumpStandardModel = 0;
// ifSetProbesToMonitor: Set probes location to Monitor.
// 0 -- Do not monitor.
// 1 -- To monitor and save data to files.
// probesDefineFile: probes location information file.
// nProbeVariables: Number of variables want to be dumped for probes monitered.
// probeVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
// probeVariables order must from small to big.
int ifSetProbesToMonitor = 0;
string probesDefineFile = "bin/probes_location.hypara";
int nProbeVariables = 6;
int probeVariables[] = [0, 1, 2, 3, 4, 5];
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Turbulence Parameter # # Turbulence Parameter #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// structhighordergradient: // structhighordergradient:
// -- "conservation", "chain_rule". // -- "conservation", "chain_rule".
int ifvfd = 0; int ifvfd = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0; int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6; double str_highorder_interpolation_epsilon = 1.0e-6;
string str_highorder_interpolation_type = "test"; string str_highorder_interpolation_type = "test";
string str_highorder_flux_name = "steger"; string str_highorder_flux_name = "steger";
string structhighordergradient = "conservation"; string structhighordergradient = "conservation";
double coefofstrflux = 0.5;
double limitcoefofinterface = 0.0;
// ----------------- Advanced choices ----------------------------------- // ----------------- Advanced choices -----------------------------------
// outtimesc: Time stepping scheme for the outer loop. // outtimesc: Time stepping scheme for the outer loop.

50
TwoD_30p30n_SST_Struct/bin/cfd_para.hypara
View File

@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
double influenceRadius = 20; double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// ----------------- Periodic Parameters --------------------------------
// Notice:Rotational periodicity only support rotation along the X axis!
// periodicType: Which periodic boundary is used.
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
######################################################################### #########################################################################
# Default parameters for Partition # # Default parameters for Partition #
######################################################################### #########################################################################
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
// maxSimuStep: The max simulation step, don't care simulation is restart or not. // maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. // intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual file 'res.dat' saved. // intervalStepRes: The step intervals for residual file 'res.dat' saved.
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. // ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
int intervalStepFlow = 1000; int intervalStepFlow = 1000;
int intervalStepPlot = 1000; int intervalStepPlot = 1000;
int intervalStepSample = 1000;
int intervalStepForce = 100; int intervalStepForce = 100;
int intervalStepRes = 10; int intervalStepRes = 10;
int ifLowSpeedPrecon = 0; int ifLowSpeedPrecon = 0;
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter.
// directionMethod: The method of determining direction.
// 1 -- using direciton.
// 2 -- using face normal.
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
// direction_inlet: The direction of inlet.
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
// direction_outlet: The direction of outlet.
int directionMethod = 2;
double subsonicInletTotalPressure = 1.2e6;
double subsonicInletTotalTemperature = 1300;
double direction_inlet[] = 1, 0, 0;
double subsonicOutletTotalPressure = 17.8571428;
double subsonicOutletTotalTemperature = 1.0;
double direction_outlet[] = 1, 0, 0;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Spatial Discretisation # # Spatial Discretisation #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
#******************************************************************* #*******************************************************************
# UnStruct Solver or Common * # UnStruct Solver or Common *
#******************************************************************* #*******************************************************************
// iviscous: Viscous model. // viscousType: Viscous model.
// 0 -- Euler. // 0 -- Euler.
// 1 -- Lamilar. // 1 -- Lamilar.
// 2 -- Algebraic. // 2 -- Algebraic.
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt"; string visualfile = "results/tecflow.plt";
string Qwall_file = "results/Qwall.dat"; string Qwall_file = "results/Qwall.dat";
string wall_aircoefile = "results/wall_aircoef.dat"; string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string surfacefile = ""; string surfacefile = "";
string wall_varfile = ""; string wall_varfile = "";
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
int dumpStandardModel = 0; int dumpStandardModel = 0;
// ifSetProbesToMonitor: Set probes location to Monitor.
// 0 -- Do not monitor.
// 1 -- To monitor and save data to files.
// probesDefineFile: probes location information file.
// nProbeVariables: Number of variables want to be dumped for probes monitered.
// probeVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
// probeVariables order must from small to big.
int ifSetProbesToMonitor = 0;
string probesDefineFile = "bin/probes_location.hypara";
int nProbeVariables = 6;
int probeVariables[] = [0, 1, 2, 3, 4, 5];
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Turbulence Parameter # # Turbulence Parameter #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// structhighordergradient: // structhighordergradient:
// -- "conservation", "chain_rule". // -- "conservation", "chain_rule".
int ifvfd = 0; int ifvfd = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0; int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6; double str_highorder_interpolation_epsilon = 1.0e-6;
string str_highorder_interpolation_type = "test"; string str_highorder_interpolation_type = "test";
string str_highorder_flux_name = "steger"; string str_highorder_flux_name = "steger";
string structhighordergradient = "conservation"; string structhighordergradient = "conservation";
double coefofstrflux = 0.5;
double limitcoefofinterface = 0.0;
// ----------------- Advanced choices ----------------------------------- // ----------------- Advanced choices -----------------------------------
// outtimesc: Time stepping scheme for the outer loop. // outtimesc: Time stepping scheme for the outer loop.

50
TwoD_Cylinder_Laminar_HighOrder_Struct/TwoD_Cylinder_Laminar_HighOrder_Struct/bin/cfd_para.hypara
View File

@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
double influenceRadius = 20; double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// ----------------- Periodic Parameters --------------------------------
// Notice:Rotational periodicity only support rotation along the X axis!
// periodicType: Which periodic boundary is used.
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
######################################################################### #########################################################################
# Default parameters for Partition # # Default parameters for Partition #
######################################################################### #########################################################################
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
// maxSimuStep: The max simulation step, don't care simulation is restart or not. // maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. // intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual file 'res.dat' saved. // intervalStepRes: The step intervals for residual file 'res.dat' saved.
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. // ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
int intervalStepFlow = 1000; int intervalStepFlow = 1000;
int intervalStepPlot = 1000; int intervalStepPlot = 1000;
int intervalStepSample = 1000;
int intervalStepForce = 100; int intervalStepForce = 100;
int intervalStepRes = 10; int intervalStepRes = 10;
int ifLowSpeedPrecon = 0; int ifLowSpeedPrecon = 0;
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter.
// directionMethod: The method of determining direction.
// 1 -- using direciton.
// 2 -- using face normal.
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
// direction_inlet: The direction of inlet.
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
// direction_outlet: The direction of outlet.
int directionMethod = 2;
double subsonicInletTotalPressure = 1.2e6;
double subsonicInletTotalTemperature = 1300;
double direction_inlet[] = 1, 0, 0;
double subsonicOutletTotalPressure = 17.8571428;
double subsonicOutletTotalTemperature = 1.0;
double direction_outlet[] = 1, 0, 0;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Spatial Discretisation # # Spatial Discretisation #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
#******************************************************************* #*******************************************************************
# UnStruct Solver or Common * # UnStruct Solver or Common *
#******************************************************************* #*******************************************************************
// viscousType : Viscous model. // viscousType: Viscous model.
// 0 -- Euler. // 0 -- Euler.
// 1 -- Lamilar. // 1 -- Lamilar.
// 2 -- Algebraic. // 2 -- Algebraic.
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt"; string visualfile = "results/tecflow.plt";
string Qwall_file = "results/Qwall.dat"; string Qwall_file = "results/Qwall.dat";
string wall_aircoefile = "results/wall_aircoef.dat"; string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string surfacefile = ""; string surfacefile = "";
string wall_varfile = ""; string wall_varfile = "";
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
int dumpStandardModel = 0; int dumpStandardModel = 0;
// ifSetProbesToMonitor: Set probes location to Monitor.
// 0 -- Do not monitor.
// 1 -- To monitor and save data to files.
// probesDefineFile: probes location information file.
// nProbeVariables: Number of variables want to be dumped for probes monitered.
// probeVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
// probeVariables order must from small to big.
int ifSetProbesToMonitor = 0;
string probesDefineFile = "bin/probes_location.hypara";
int nProbeVariables = 6;
int probeVariables[] = [0, 1, 2, 3, 4, 5];
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Turbulence Parameter # # Turbulence Parameter #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// structhighordergradient: // structhighordergradient:
// -- "conservation", "chain_rule". // -- "conservation", "chain_rule".
int ifvfd = 0; int ifvfd = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0; int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6; double str_highorder_interpolation_epsilon = 1.0e-6;
string str_highorder_interpolation_type = "test"; string str_highorder_interpolation_type = "test";
string str_highorder_flux_name = "steger"; string str_highorder_flux_name = "steger";
string structhighordergradient = "conservation"; string structhighordergradient = "conservation";
double coefofstrflux = 0.5;
double limitcoefofinterface = 0.0;
// ----------------- Advanced choices ----------------------------------- // ----------------- Advanced choices -----------------------------------
// outtimesc: Time stepping scheme for the outer loop. // outtimesc: Time stepping scheme for the outer loop.

50
TwoD_Cylinder_Laminar_Ma8d03_Struct/bin/cfd_para.hypara
View File

@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
double influenceRadius = 20; double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// ----------------- Periodic Parameters --------------------------------
// Notice:Rotational periodicity only support rotation along the X axis!
// periodicType: Which periodic boundary is used.
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
######################################################################### #########################################################################
# Default parameters for Partition # # Default parameters for Partition #
######################################################################### #########################################################################
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
// maxSimuStep: The max simulation step, don't care simulation is restart or not. // maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. // intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual file 'res.dat' saved. // intervalStepRes: The step intervals for residual file 'res.dat' saved.
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. // ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
int intervalStepFlow = 1000; int intervalStepFlow = 1000;
int intervalStepPlot = 1000; int intervalStepPlot = 1000;
int intervalStepSample = 1000;
int intervalStepForce = 100; int intervalStepForce = 100;
int intervalStepRes = 10; int intervalStepRes = 10;
int ifLowSpeedPrecon = 0; int ifLowSpeedPrecon = 0;
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter.
// directionMethod: The method of determining direction.
// 1 -- using direciton.
// 2 -- using face normal.
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
// direction_inlet: The direction of inlet.
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
// direction_outlet: The direction of outlet.
int directionMethod = 2;
double subsonicInletTotalPressure = 1.2e6;
double subsonicInletTotalTemperature = 1300;
double direction_inlet[] = 1, 0, 0;
double subsonicOutletTotalPressure = 17.8571428;
double subsonicOutletTotalTemperature = 1.0;
double direction_outlet[] = 1, 0, 0;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Spatial Discretisation # # Spatial Discretisation #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
#******************************************************************* #*******************************************************************
# UnStruct Solver or Common * # UnStruct Solver or Common *
#******************************************************************* #*******************************************************************
// iviscous: Viscous model. // viscousType: Viscous model.
// 0 -- Euler. // 0 -- Euler.
// 1 -- Lamilar. // 1 -- Lamilar.
// 2 -- Algebraic. // 2 -- Algebraic.
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt"; string visualfile = "results/tecflow.plt";
string Qwall_file = "results/Qwall.dat"; string Qwall_file = "results/Qwall.dat";
string wall_aircoefile = "results/wall_aircoef.dat"; string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string surfacefile = ""; string surfacefile = "";
string wall_varfile = ""; string wall_varfile = "";
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
int dumpStandardModel = 0; int dumpStandardModel = 0;
// ifSetProbesToMonitor: Set probes location to Monitor.
// 0 -- Do not monitor.
// 1 -- To monitor and save data to files.
// probesDefineFile: probes location information file.
// nProbeVariables: Number of variables want to be dumped for probes monitered.
// probeVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
// probeVariables order must from small to big.
int ifSetProbesToMonitor = 0;
string probesDefineFile = "bin/probes_location.hypara";
int nProbeVariables = 6;
int probeVariables[] = [0, 1, 2, 3, 4, 5];
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Turbulence Parameter # # Turbulence Parameter #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// structhighordergradient: // structhighordergradient:
// -- "conservation", "chain_rule". // -- "conservation", "chain_rule".
int ifvfd = 0; int ifvfd = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0; int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6; double str_highorder_interpolation_epsilon = 1.0e-6;
string str_highorder_interpolation_type = "test"; string str_highorder_interpolation_type = "test";
string str_highorder_flux_name = "steger"; string str_highorder_flux_name = "steger";
string structhighordergradient = "conservation"; string structhighordergradient = "conservation";
double coefofstrflux = 0.5;
double limitcoefofinterface = 0.0;
// ----------------- Advanced choices ----------------------------------- // ----------------- Advanced choices -----------------------------------
// outtimesc: Time stepping scheme for the outer loop. // outtimesc: Time stepping scheme for the outer loop.

50
TwoD_Cylinder_Laminar_OneTemperMode_FCW_Struct/bin/cfd_para.hypara
View File

@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
double influenceRadius = 20; double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// ----------------- Periodic Parameters --------------------------------
// Notice:Rotational periodicity only support rotation along the X axis!
// periodicType: Which periodic boundary is used.
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
######################################################################### #########################################################################
# Default parameters for Partition # # Default parameters for Partition #
######################################################################### #########################################################################
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
// maxSimuStep: The max simulation step, don't care simulation is restart or not. // maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. // intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual file 'res.dat' saved. // intervalStepRes: The step intervals for residual file 'res.dat' saved.
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. // ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
int intervalStepFlow = 1000; int intervalStepFlow = 1000;
int intervalStepPlot = 1000; int intervalStepPlot = 1000;
int intervalStepSample = 1000;
int intervalStepForce = 100; int intervalStepForce = 100;
int intervalStepRes = 10; int intervalStepRes = 10;
int ifLowSpeedPrecon = 0; int ifLowSpeedPrecon = 0;
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter.
// directionMethod: The method of determining direction.
// 1 -- using direciton.
// 2 -- using face normal.
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
// direction_inlet: The direction of inlet.
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
// direction_outlet: The direction of outlet.
int directionMethod = 2;
double subsonicInletTotalPressure = 1.2e6;
double subsonicInletTotalTemperature = 1300;
double direction_inlet[] = 1, 0, 0;
double subsonicOutletTotalPressure = 17.8571428;
double subsonicOutletTotalTemperature = 1.0;
double direction_outlet[] = 1, 0, 0;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Spatial Discretisation # # Spatial Discretisation #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
#******************************************************************* #*******************************************************************
# UnStruct Solver or Common * # UnStruct Solver or Common *
#******************************************************************* #*******************************************************************
// viscousType : Viscous model. // viscousType: Viscous model.
// 0 -- Euler. // 0 -- Euler.
// 1 -- Lamilar. // 1 -- Lamilar.
// 2 -- Algebraic. // 2 -- Algebraic.
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt"; string visualfile = "results/tecflow.plt";
string Qwall_file = "results/Qwall.dat"; string Qwall_file = "results/Qwall.dat";
string wall_aircoefile = "results/wall_aircoef.dat"; string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string surfacefile = ""; string surfacefile = "";
string wall_varfile = ""; string wall_varfile = "";
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
int dumpStandardModel = 0; int dumpStandardModel = 0;
// ifSetProbesToMonitor: Set probes location to Monitor.
// 0 -- Do not monitor.
// 1 -- To monitor and save data to files.
// probesDefineFile: probes location information file.
// nProbeVariables: Number of variables want to be dumped for probes monitered.
// probeVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
// probeVariables order must from small to big.
int ifSetProbesToMonitor = 0;
string probesDefineFile = "bin/probes_location.hypara";
int nProbeVariables = 6;
int probeVariables[] = [0, 1, 2, 3, 4, 5];
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Turbulence Parameter # # Turbulence Parameter #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// structhighordergradient: // structhighordergradient:
// -- "conservation", "chain_rule". // -- "conservation", "chain_rule".
int ifvfd = 0; int ifvfd = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0; int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6; double str_highorder_interpolation_epsilon = 1.0e-6;
string str_highorder_interpolation_type = "test"; string str_highorder_interpolation_type = "test";
string str_highorder_flux_name = "steger"; string str_highorder_flux_name = "steger";
string structhighordergradient = "conservation"; string structhighordergradient = "conservation";
double coefofstrflux = 0.5;
double limitcoefofinterface = 0.0;
// ----------------- Advanced choices ----------------------------------- // ----------------- Advanced choices -----------------------------------
// outtimesc: Time stepping scheme for the outer loop. // outtimesc: Time stepping scheme for the outer loop.

50
TwoD_LowMach_plate_SST_Struct/bin/cfd_para.hypara
View File

@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
double influenceRadius = 20; double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// ----------------- Periodic Parameters --------------------------------
// Notice:Rotational periodicity only support rotation along the X axis!
// periodicType: Which periodic boundary is used.
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
######################################################################### #########################################################################
# Default parameters for Partition # # Default parameters for Partition #
######################################################################### #########################################################################
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
// maxSimuStep: The max simulation step, don't care simulation is restart or not. // maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. // intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual file 'res.dat' saved. // intervalStepRes: The step intervals for residual file 'res.dat' saved.
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. // ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
int intervalStepFlow = 1000; int intervalStepFlow = 1000;
int intervalStepPlot = 1000; int intervalStepPlot = 1000;
int intervalStepSample = 1000;
int intervalStepForce = 100; int intervalStepForce = 100;
int intervalStepRes = 10; int intervalStepRes = 10;
int ifLowSpeedPrecon = 0; int ifLowSpeedPrecon = 0;
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter.
// directionMethod: The method of determining direction.
// 1 -- using direciton.
// 2 -- using face normal.
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
// direction_inlet: The direction of inlet.
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
// direction_outlet: The direction of outlet.
int directionMethod = 2;
double subsonicInletTotalPressure = 1.2e6;
double subsonicInletTotalTemperature = 1300;
double direction_inlet[] = 1, 0, 0;
double subsonicOutletTotalPressure = 17.8571428;
double subsonicOutletTotalTemperature = 1.0;
double direction_outlet[] = 1, 0, 0;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Spatial Discretisation # # Spatial Discretisation #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
#******************************************************************* #*******************************************************************
# UnStruct Solver or Common * # UnStruct Solver or Common *
#******************************************************************* #*******************************************************************
// iviscous: Viscous model. // viscousType: Viscous model.
// 0 -- Euler. // 0 -- Euler.
// 1 -- Lamilar. // 1 -- Lamilar.
// 2 -- Algebraic. // 2 -- Algebraic.
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt"; string visualfile = "results/tecflow.plt";
string Qwall_file = "results/Qwall.dat"; string Qwall_file = "results/Qwall.dat";
string wall_aircoefile = "results/wall_aircoef.dat"; string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string surfacefile = ""; string surfacefile = "";
string wall_varfile = ""; string wall_varfile = "";
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
int dumpStandardModel = 0; int dumpStandardModel = 0;
// ifSetProbesToMonitor: Set probes location to Monitor.
// 0 -- Do not monitor.
// 1 -- To monitor and save data to files.
// probesDefineFile: probes location information file.
// nProbeVariables: Number of variables want to be dumped for probes monitered.
// probeVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
// probeVariables order must from small to big.
int ifSetProbesToMonitor = 0;
string probesDefineFile = "bin/probes_location.hypara";
int nProbeVariables = 6;
int probeVariables[] = [0, 1, 2, 3, 4, 5];
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Turbulence Parameter # # Turbulence Parameter #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// structhighordergradient: // structhighordergradient:
// -- "conservation", "chain_rule". // -- "conservation", "chain_rule".
int ifvfd = 0; int ifvfd = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0; int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6; double str_highorder_interpolation_epsilon = 1.0e-6;
string str_highorder_interpolation_type = "test"; string str_highorder_interpolation_type = "test";
string str_highorder_flux_name = "steger"; string str_highorder_flux_name = "steger";
string structhighordergradient = "conservation"; string structhighordergradient = "conservation";
double coefofstrflux = 0.5;
double limitcoefofinterface = 0.0;
// ----------------- Advanced choices ----------------------------------- // ----------------- Advanced choices -----------------------------------
// outtimesc: Time stepping scheme for the outer loop. // outtimesc: Time stepping scheme for the outer loop.

50
TwoD_Plate_Laminar_Ma5_Struct_1CPU/bin/cfd_para.hypara
View File

@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
double influenceRadius = 20; double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// ----------------- Periodic Parameters --------------------------------
// Notice:Rotational periodicity only support rotation along the X axis!
// periodicType: Which periodic boundary is used.
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
######################################################################### #########################################################################
# Default parameters for Partition # # Default parameters for Partition #
######################################################################### #########################################################################
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
// maxSimuStep: The max simulation step, don't care simulation is restart or not. // maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. // intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual file 'res.dat' saved. // intervalStepRes: The step intervals for residual file 'res.dat' saved.
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. // ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
int intervalStepFlow = 1000; int intervalStepFlow = 1000;
int intervalStepPlot = 1000; int intervalStepPlot = 1000;
int intervalStepSample = 1000;
int intervalStepForce = 100; int intervalStepForce = 100;
int intervalStepRes = 10; int intervalStepRes = 10;
int ifLowSpeedPrecon = 0; int ifLowSpeedPrecon = 0;
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter.
// directionMethod: The method of determining direction.
// 1 -- using direciton.
// 2 -- using face normal.
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
// direction_inlet: The direction of inlet.
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
// direction_outlet: The direction of outlet.
int directionMethod = 2;
double subsonicInletTotalPressure = 1.2e6;
double subsonicInletTotalTemperature = 1300;
double direction_inlet[] = 1, 0, 0;
double subsonicOutletTotalPressure = 17.8571428;
double subsonicOutletTotalTemperature = 1.0;
double direction_outlet[] = 1, 0, 0;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Spatial Discretisation # # Spatial Discretisation #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
#******************************************************************* #*******************************************************************
# UnStruct Solver or Common * # UnStruct Solver or Common *
#******************************************************************* #*******************************************************************
// iviscous: Viscous model. // viscousType: Viscous model.
// 0 -- Euler. // 0 -- Euler.
// 1 -- Lamilar. // 1 -- Lamilar.
// 2 -- Algebraic. // 2 -- Algebraic.
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt"; string visualfile = "results/tecflow.plt";
string Qwall_file = "results/Qwall.dat"; string Qwall_file = "results/Qwall.dat";
string wall_aircoefile = "results/wall_aircoef.dat"; string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string surfacefile = ""; string surfacefile = "";
string wall_varfile = ""; string wall_varfile = "";
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
int dumpStandardModel = 0; int dumpStandardModel = 0;
// ifSetProbesToMonitor: Set probes location to Monitor.
// 0 -- Do not monitor.
// 1 -- To monitor and save data to files.
// probesDefineFile: probes location information file.
// nProbeVariables: Number of variables want to be dumped for probes monitered.
// probeVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
// probeVariables order must from small to big.
int ifSetProbesToMonitor = 0;
string probesDefineFile = "bin/probes_location.hypara";
int nProbeVariables = 6;
int probeVariables[] = [0, 1, 2, 3, 4, 5];
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Turbulence Parameter # # Turbulence Parameter #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// structhighordergradient: // structhighordergradient:
// -- "conservation", "chain_rule". // -- "conservation", "chain_rule".
int ifvfd = 0; int ifvfd = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0; int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6; double str_highorder_interpolation_epsilon = 1.0e-6;
string str_highorder_interpolation_type = "test"; string str_highorder_interpolation_type = "test";
string str_highorder_flux_name = "steger"; string str_highorder_flux_name = "steger";
string structhighordergradient = "conservation"; string structhighordergradient = "conservation";
double coefofstrflux = 0.5;
double limitcoefofinterface = 0.0;
// ----------------- Advanced choices ----------------------------------- // ----------------- Advanced choices -----------------------------------
// outtimesc: Time stepping scheme for the outer loop. // outtimesc: Time stepping scheme for the outer loop.

50
TwoD_Plate_Laminar_Struct_1CPU/bin/cfd_para.hypara
View File

@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
double influenceRadius = 20; double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// ----------------- Periodic Parameters --------------------------------
// Notice:Rotational periodicity only support rotation along the X axis!
// periodicType: Which periodic boundary is used.
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
######################################################################### #########################################################################
# Default parameters for Partition # # Default parameters for Partition #
######################################################################### #########################################################################
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
// maxSimuStep: The max simulation step, don't care simulation is restart or not. // maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. // intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual file 'res.dat' saved. // intervalStepRes: The step intervals for residual file 'res.dat' saved.
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. // ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
int intervalStepFlow = 1000; int intervalStepFlow = 1000;
int intervalStepPlot = 1000; int intervalStepPlot = 1000;
int intervalStepSample = 1000;
int intervalStepForce = 100; int intervalStepForce = 100;
int intervalStepRes = 10; int intervalStepRes = 10;
int ifLowSpeedPrecon = 0; int ifLowSpeedPrecon = 0;
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter.
// directionMethod: The method of determining direction.
// 1 -- using direciton.
// 2 -- using face normal.
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
// direction_inlet: The direction of inlet.
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
// direction_outlet: The direction of outlet.
int directionMethod = 2;
double subsonicInletTotalPressure = 1.2e6;
double subsonicInletTotalTemperature = 1300;
double direction_inlet[] = 1, 0, 0;
double subsonicOutletTotalPressure = 17.8571428;
double subsonicOutletTotalTemperature = 1.0;
double direction_outlet[] = 1, 0, 0;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Spatial Discretisation # # Spatial Discretisation #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
#******************************************************************* #*******************************************************************
# UnStruct Solver or Common * # UnStruct Solver or Common *
#******************************************************************* #*******************************************************************
// iviscous: Viscous model. // viscousType: Viscous model.
// 0 -- Euler. // 0 -- Euler.
// 1 -- Lamilar. // 1 -- Lamilar.
// 2 -- Algebraic. // 2 -- Algebraic.
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt"; string visualfile = "results/tecflow.plt";
string Qwall_file = "results/Qwall.dat"; string Qwall_file = "results/Qwall.dat";
string wall_aircoefile = "results/wall_aircoef.dat"; string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string surfacefile = ""; string surfacefile = "";
string wall_varfile = ""; string wall_varfile = "";
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
int dumpStandardModel = 0; int dumpStandardModel = 0;
// ifSetProbesToMonitor: Set probes location to Monitor.
// 0 -- Do not monitor.
// 1 -- To monitor and save data to files.
// probesDefineFile: probes location information file.
// nProbeVariables: Number of variables want to be dumped for probes monitered.
// probeVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
// probeVariables order must from small to big.
int ifSetProbesToMonitor = 0;
string probesDefineFile = "bin/probes_location.hypara";
int nProbeVariables = 6;
int probeVariables[] = [0, 1, 2, 3, 4, 5];
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Turbulence Parameter # # Turbulence Parameter #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// structhighordergradient: // structhighordergradient:
// -- "conservation", "chain_rule". // -- "conservation", "chain_rule".
int ifvfd = 0; int ifvfd = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0; int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6; double str_highorder_interpolation_epsilon = 1.0e-6;
string str_highorder_interpolation_type = "test"; string str_highorder_interpolation_type = "test";
string str_highorder_flux_name = "steger"; string str_highorder_flux_name = "steger";
string structhighordergradient = "conservation"; string structhighordergradient = "conservation";
double coefofstrflux = 0.5;
double limitcoefofinterface = 0.0;
// ----------------- Advanced choices ----------------------------------- // ----------------- Advanced choices -----------------------------------
// outtimesc: Time stepping scheme for the outer loop. // outtimesc: Time stepping scheme for the outer loop.

50
TwoD_Plate_SST_Ma5_Struct_1CPU/bin/cfd_para.hypara
View File

@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
double influenceRadius = 20; double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// ----------------- Periodic Parameters --------------------------------
// Notice:Rotational periodicity only support rotation along the X axis!
// periodicType: Which periodic boundary is used.
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
######################################################################### #########################################################################
# Default parameters for Partition # # Default parameters for Partition #
######################################################################### #########################################################################
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
// maxSimuStep: The max simulation step, don't care simulation is restart or not. // maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. // intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual file 'res.dat' saved. // intervalStepRes: The step intervals for residual file 'res.dat' saved.
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. // ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
int intervalStepFlow = 1000; int intervalStepFlow = 1000;
int intervalStepPlot = 1000; int intervalStepPlot = 1000;
int intervalStepSample = 1000;
int intervalStepForce = 100; int intervalStepForce = 100;
int intervalStepRes = 10; int intervalStepRes = 10;
int ifLowSpeedPrecon = 0; int ifLowSpeedPrecon = 0;
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter.
// directionMethod: The method of determining direction.
// 1 -- using direciton.
// 2 -- using face normal.
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
// direction_inlet: The direction of inlet.
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
// direction_outlet: The direction of outlet.
int directionMethod = 2;
double subsonicInletTotalPressure = 1.2e6;
double subsonicInletTotalTemperature = 1300;
double direction_inlet[] = 1, 0, 0;
double subsonicOutletTotalPressure = 17.8571428;
double subsonicOutletTotalTemperature = 1.0;
double direction_outlet[] = 1, 0, 0;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Spatial Discretisation # # Spatial Discretisation #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
#******************************************************************* #*******************************************************************
# UnStruct Solver or Common * # UnStruct Solver or Common *
#******************************************************************* #*******************************************************************
// iviscous: Viscous model. // viscousType: Viscous model.
// 0 -- Euler. // 0 -- Euler.
// 1 -- Lamilar. // 1 -- Lamilar.
// 2 -- Algebraic. // 2 -- Algebraic.
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt"; string visualfile = "results/tecflow.plt";
string Qwall_file = "results/Qwall.dat"; string Qwall_file = "results/Qwall.dat";
string wall_aircoefile = "results/wall_aircoef.dat"; string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string surfacefile = ""; string surfacefile = "";
string wall_varfile = ""; string wall_varfile = "";
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
int dumpStandardModel = 0; int dumpStandardModel = 0;
// ifSetProbesToMonitor: Set probes location to Monitor.
// 0 -- Do not monitor.
// 1 -- To monitor and save data to files.
// probesDefineFile: probes location information file.
// nProbeVariables: Number of variables want to be dumped for probes monitered.
// probeVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
// probeVariables order must from small to big.
int ifSetProbesToMonitor = 0;
string probesDefineFile = "bin/probes_location.hypara";
int nProbeVariables = 6;
int probeVariables[] = [0, 1, 2, 3, 4, 5];
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Turbulence Parameter # # Turbulence Parameter #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// structhighordergradient: // structhighordergradient:
// -- "conservation", "chain_rule". // -- "conservation", "chain_rule".
int ifvfd = 0; int ifvfd = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0; int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6; double str_highorder_interpolation_epsilon = 1.0e-6;
string str_highorder_interpolation_type = "test"; string str_highorder_interpolation_type = "test";
string str_highorder_flux_name = "steger"; string str_highorder_flux_name = "steger";
string structhighordergradient = "conservation"; string structhighordergradient = "conservation";
double coefofstrflux = 0.5;
double limitcoefofinterface = 0.0;
// ----------------- Advanced choices ----------------------------------- // ----------------- Advanced choices -----------------------------------
// outtimesc: Time stepping scheme for the outer loop. // outtimesc: Time stepping scheme for the outer loop.

50
TwoD_Rae2822_SST_Struct/bin/cfd_para.hypara
View File

@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
double influenceRadius = 20; double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// ----------------- Periodic Parameters --------------------------------
// Notice:Rotational periodicity only support rotation along the X axis!
// periodicType: Which periodic boundary is used.
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
######################################################################### #########################################################################
# Default parameters for Partition # # Default parameters for Partition #
######################################################################### #########################################################################
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
// maxSimuStep: The max simulation step, don't care simulation is restart or not. // maxSimuStep: The max simulation step, don't care simulation is restart or not.
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. // intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
// intervalStepRes: The step intervals for residual file 'res.dat' saved. // intervalStepRes: The step intervals for residual file 'res.dat' saved.
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. // ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
int intervalStepFlow = 1000; int intervalStepFlow = 1000;
int intervalStepPlot = 1000; int intervalStepPlot = 1000;
int intervalStepSample = 1000;
int intervalStepForce = 100; int intervalStepForce = 100;
int intervalStepRes = 10; int intervalStepRes = 10;
int ifLowSpeedPrecon = 0; int ifLowSpeedPrecon = 0;
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter.
// directionMethod: The method of determining direction.
// 1 -- using direciton.
// 2 -- using face normal.
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
// direction_inlet: The direction of inlet.
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
// direction_outlet: The direction of outlet.
int directionMethod = 2;
double subsonicInletTotalPressure = 1.2e6;
double subsonicInletTotalTemperature = 1300;
double direction_inlet[] = 1, 0, 0;
double subsonicOutletTotalPressure = 17.8571428;
double subsonicOutletTotalTemperature = 1.0;
double direction_outlet[] = 1, 0, 0;
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Spatial Discretisation # # Spatial Discretisation #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
#******************************************************************* #*******************************************************************
# UnStruct Solver or Common * # UnStruct Solver or Common *
#******************************************************************* #*******************************************************************
// iviscous: Viscous model. // viscousType: Viscous model.
// 0 -- Euler. // 0 -- Euler.
// 1 -- Lamilar. // 1 -- Lamilar.
// 2 -- Algebraic. // 2 -- Algebraic.
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt"; string visualfile = "results/tecflow.plt";
string Qwall_file = "results/Qwall.dat"; string Qwall_file = "results/Qwall.dat";
string wall_aircoefile = "results/wall_aircoef.dat"; string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string surfacefile = ""; string surfacefile = "";
string wall_varfile = ""; string wall_varfile = "";
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
// 1 -- Turbulent flat plate. // 1 -- Turbulent flat plate.
int dumpStandardModel = 0; int dumpStandardModel = 0;
// ifSetProbesToMonitor: Set probes location to Monitor.
// 0 -- Do not monitor.
// 1 -- To monitor and save data to files.
// probesDefineFile: probes location information file.
// nProbeVariables: Number of variables want to be dumped for probes monitered.
// probeVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
// probeVariables order must from small to big.
int ifSetProbesToMonitor = 0;
string probesDefineFile = "bin/probes_location.hypara";
int nProbeVariables = 6;
int probeVariables[] = [0, 1, 2, 3, 4, 5];
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
# Turbulence Parameter # # Turbulence Parameter #
//----------------------------------------------------------------------- //-----------------------------------------------------------------------
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// structhighordergradient: // structhighordergradient:
// -- "conservation", "chain_rule". // -- "conservation", "chain_rule".
int ifvfd = 0; int ifvfd = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0; int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6; double str_highorder_interpolation_epsilon = 1.0e-6;
string str_highorder_interpolation_type = "test"; string str_highorder_interpolation_type = "test";
string str_highorder_flux_name = "steger"; string str_highorder_flux_name = "steger";
string structhighordergradient = "conservation"; string structhighordergradient = "conservation";
double coefofstrflux = 0.5;
double limitcoefofinterface = 0.0;
// ----------------- Advanced choices ----------------------------------- // ----------------- Advanced choices -----------------------------------
// outtimesc: Time stepping scheme for the outer loop. // outtimesc: Time stepping scheme for the outer loop.