V2171 D01
This commit is contained in:
parent
7990d4276b
commit
303c629844
|
|
@ -26,15 +26,7 @@
|
|||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// grid_database_index: Case of typical case, only for gridobj=0.
|
||||
// 1 -- Laminar flat plate of subsonic flow.
|
||||
// 2 -- Laminar flat plate of supersonic flow.
|
||||
// 3 -- Turbulent flat plate of subsonic flow.
|
||||
// 4 -- Turbulent flat plate of supersonic flow.
|
||||
// iadapt: Adaptation number for unstructure grid.
|
||||
// iovrlap: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// SymmetryFaceVector: The vector of symmetry face.
|
||||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
|
|
@ -42,9 +34,7 @@
|
|||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int grid_database_index = 3;
|
||||
int iadapt = 0;
|
||||
int iovrlap = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
|
|
@ -89,22 +79,18 @@ string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
|||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int iale = 0;
|
||||
int codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
// 1 -- ASCII.
|
||||
int fileformat = 0;
|
||||
|
||||
// .skl meaning skeleton.
|
||||
string original_grid_info_file = "./grid/FLUENT_test.skl";
|
||||
|
||||
// Parameters for hybrid solver.
|
||||
// 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_bc: path of structure grid boundary condition file for hybrid solver.
|
||||
string mixgrid_uns = "./grid/rae2822_uns2d_4.fts";
|
||||
string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts";
|
||||
string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp";
|
||||
|
||||
// Some parameters for structured overlapping grid.
|
||||
int codeOfDigHoles = 1;
|
||||
|
|
@ -176,6 +162,11 @@ int traceMark = 0;
|
|||
int blockIndexOfMark = 0;
|
||||
int cellIndexOfMark[] = [185,30,1];
|
||||
|
||||
// parallel Strategy:
|
||||
//! -# 0 : each zone is assigned to the one that defined in grid partition procedure.
|
||||
//! -# 1 : random assigned for each zone or by some else ways.
|
||||
int parallelStrategy = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File path #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -253,12 +244,6 @@ int compressible = 1;
|
|||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 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.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
|
|
@ -296,11 +281,11 @@ double freestream_vibration_temperature = 10000.00;
|
|||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
int dump_Q = 0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
|
|
@ -410,7 +395,6 @@ double venkatCoeff = 5.0;
|
|||
int reconmeth = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
double limit_angle = 0;
|
||||
double skewnessAngle = 60.0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
|
|
@ -454,7 +438,7 @@ double roeEntropyScale = 1.0;
|
|||
// 1 --Global.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// iale: Arbitrary Lagrangian-Eulerian method.
|
||||
// codeOfAleModel: Arbitrary Lagrangian-Eulerian method.
|
||||
// 0 -- no ALE method.
|
||||
// 1 -- ALE method for non-moving grids.
|
||||
// 2 -- ALE method for moving grids.
|
||||
|
|
@ -471,7 +455,9 @@ double physicalTimeStep = 0.01;
|
|||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int startStatisticStep = 800000;
|
||||
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
|
||||
|
||||
int methodOfDualTime = 3;
|
||||
int min_sub_iter = 50;
|
||||
int max_sub_iter = 50;
|
||||
double tol_sub_iter = 0.01;
|
||||
|
|
@ -493,14 +479,13 @@ int order = 2;
|
|||
|
||||
double visl_min = 0.01;
|
||||
double turbCFLScale = 1.0;
|
||||
|
||||
double csrv = 2.0;
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int iale = 0;
|
||||
int ialetype = 2;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
double dtau_max = 1E-01;
|
||||
|
||||
int wallFunctionType = 0;
|
||||
|
||||
|
|
@ -522,7 +507,7 @@ double lamda[] = 0.5, 1.0;
|
|||
// IMPORTANT WARNING: The file index should be ignored,
|
||||
// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
|
||||
// please use 'rae2822_hybrid2d__4.fts' here!
|
||||
// isPlotVolumeField: If dump out the field results to visulization.
|
||||
// plotFieldType: If dump out the field results to visulization.
|
||||
// walldistMethod: The method to compute wall distance.
|
||||
// 0 -- accurate but not fast enough.
|
||||
// 1 -- fast but not accurate enough.
|
||||
|
|
@ -550,22 +535,18 @@ string restartNSFile = "results/flow.dat";
|
|||
string turbfile = "results/turb.dat";
|
||||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string surfacefile = "";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
string componentDefineFile = "bin/component.hypara";
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string componentforcefile = "results/component_aircoef.dat";
|
||||
string overset_gridfile = "results/iblank.ovs";
|
||||
string sixDofFileName = "results/sixDofInfo.dat";
|
||||
|
||||
string overset_gridfile = "iblank.ovs";
|
||||
|
||||
int isPlotVolumeField = 0;
|
||||
int plotFieldType = 0;
|
||||
|
||||
// visualfileType: The file type of visualfile.
|
||||
// 0 -- Tecplot binary.
|
||||
|
|
@ -600,7 +581,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
|
||||
// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
|
||||
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44).
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), iblank(81).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
int nVisualVariables = 8;
|
||||
|
|
@ -610,19 +591,48 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
|||
// 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.
|
||||
// ifSetDataMonitor: Whether to set the data monitor.
|
||||
// 0 -- No.
|
||||
// 1 -- Yes.
|
||||
// dataMonitorType: The type of data Monitor.
|
||||
// 0 -- Probes data monitor.
|
||||
// 1 -- Lines data monitor.
|
||||
// 2 -- Surfaces data monitor.
|
||||
// probesDefineFile: Probes location information file.
|
||||
// nLines: The number of lines need to be monitored.
|
||||
// linesDefineFile: Lines location information file.
|
||||
// nSurfaces: The number of surfaces need to be monitored.
|
||||
// surfacesDefineFile: Surfaces location information file.
|
||||
// searchCellsMethod: method to search the cell of each probe.
|
||||
// 0 -- Nearest cell to the probe.
|
||||
// 1 -- Real cell where the probe is located.
|
||||
// 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";
|
||||
// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables.
|
||||
// 0 -- Take the value of probe's cell as probe real value.
|
||||
// 1 -- Interpolation from probe's and neighbouring cell to probe.
|
||||
// 2 -- Interpolation from probe's cell nodes to probe.
|
||||
int ifSetDataMonitor = 0;
|
||||
|
||||
int dataMonitorType = 0;
|
||||
string probesDefineFile = "bin/probes_XYZ.dat";
|
||||
|
||||
//int dataMonitorType = 1;
|
||||
//int nLines = 1;
|
||||
//string linesDefineFile = "bin/lines_XYZ.dat";
|
||||
|
||||
//int dataMonitorType = 2;
|
||||
//int nSurfaces = 4;
|
||||
//string surfacesDefineFile = "bin/surfaces_XYZ.dat";
|
||||
|
||||
int searchCellsMethod = 0;
|
||||
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
int probeVariablesInterpolationMethod = 0;
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -634,19 +644,17 @@ int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
|||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turb_vis_kind = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
double turb_min_coef = 1.0e-1;
|
||||
double freeStreamViscosity = 1.0e-3;
|
||||
double muoo = 1.0e-1;
|
||||
double kwoo = 1.0;
|
||||
double muoo = 3.0;
|
||||
double kwoo = 5.0;
|
||||
int transitionType = 0;
|
||||
double turbIntensity = -1.0;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
double sdilim = 1.0e20;
|
||||
double coef_kvist = 1.0;
|
||||
int monitor_vistmax = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -751,11 +759,6 @@ int iapplication = 0;
|
|||
int iCodeBranch = 0;
|
||||
int nm = 5;
|
||||
|
||||
// MHD
|
||||
double bxoo = 0.0;
|
||||
double byoo = 0.0;
|
||||
double bzoo = 0.0;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
double prt = 0.90;
|
||||
|
|
@ -878,6 +881,30 @@ double MUSCLCoefXk = -1;
|
|||
double MUSCLCoefXb = 1.0;
|
||||
int allReduceStep = 1;
|
||||
|
||||
// ----------------- overlap configuration ------------------------------
|
||||
// codeOfOversetGrid: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
int codeOfOversetGrid = 0;
|
||||
int codeOfOversetSlipGrid = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
int readInAuxiliaryOuterGrid = 0;
|
||||
int readInSklFileOrNot = 0;
|
||||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
|
||||
string auxiliaryInnerGrid2 = "";
|
||||
string oversetGridFileName = "./grid/overlap.ovs";
|
||||
double walldistMainZone = 1.0
|
||||
double toleranceForOversetSearch = 1.0e-3;
|
||||
double toleranceForOversetBox = 1.0e-3;
|
||||
int twoOrderInterpolationOrNot = 0;
|
||||
int keyEnlargeOfActiveNodes = 0;
|
||||
int outTecplotOverset = 0;
|
||||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
|
|
@ -888,3 +915,9 @@ int allReduceStep = 1;
|
|||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
|
||||
#########################################################################
|
||||
# Old Parameter #
|
||||
#########################################################################
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
|
|
@ -21,12 +21,6 @@ int intervalStepRes = 10;
|
|||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
|
|
@ -52,12 +46,10 @@ double attackd = 0.00;
|
|||
double angleSlide = 0.00;
|
||||
|
||||
double wallTemperature = 294.44;
|
||||
int dump_Q = 1;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 1.835e5;
|
||||
double refDimensionalTemperature = 124.94;
|
||||
double freestream_vibration_temperature = 10000.0;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
|
@ -78,7 +70,7 @@ double TorqueRefZ = 0.0; // unit of meter.
|
|||
#########################################################################
|
||||
# Physical models #
|
||||
#########################################################################
|
||||
// viscousType : Viscous model.
|
||||
// viscousType: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 3 -- 1eq turbulent.
|
||||
|
|
@ -156,8 +148,6 @@ int iunsteady = 0;
|
|||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 100;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int nLUSGSSweeps = 4;
|
||||
double LUSGSTolerance = 1.0e-20;
|
||||
|
||||
|
|
@ -169,10 +159,10 @@ double LUSGSTolerance = 1.0e-20;
|
|||
// IMPORTANT WARNING: The file index should be ignored,
|
||||
// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
|
||||
// Please use 'rae2822_hybrid2d__4.fts' here!
|
||||
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0 / 1.
|
||||
// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
|
||||
|
||||
string gridfile = "./grid/cylinder_str.fts";
|
||||
int isPlotVolumeField = 0;
|
||||
int plotFieldType = 0;
|
||||
|
||||
// ----------------- Advanced Parameters, DO NOT care it ----------------
|
||||
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
|
||||
|
|
@ -181,7 +171,9 @@ int isPlotVolumeField = 0;
|
|||
// -- viscosityLaminar(7), viscosityTurbulent(8),
|
||||
// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12),
|
||||
// -- strain_rate(13), Q_criteria(14), Cp(15), timeStep(16), volume(17),
|
||||
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21).
|
||||
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
|
||||
// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
|
||||
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
||||
|
|
@ -230,6 +222,9 @@ string structhighordergradient = "conservation";
|
|||
#########################################################################
|
||||
# Non-equilibrium gas #
|
||||
#########################################################################
|
||||
// nGasModel: The type of gas.
|
||||
// 0 -- Earth gas.
|
||||
// 1 -- Mars gas.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
|
|
@ -251,11 +246,13 @@ string structhighordergradient = "conservation";
|
|||
// "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.
|
||||
// "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.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int nGasModel = 0;
|
||||
int nchem = 0;
|
||||
int ntmodel = 1;
|
||||
int nchemsrc = 1;
|
||||
|
|
@ -40,11 +40,13 @@ string parafilename = "./bin/cfd_para_hypersonic.hypara";
|
|||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
|
||||
//int nsimutask = 14;
|
||||
//string parafilename = "./bin/integrative_solver.hypara";
|
||||
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
|
||||
// ---------------- Advanced Parameters, DO NOT care it ----------------
|
||||
int iovrlap = 0;
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
|
|
@ -1,21 +0,0 @@
|
|||
// pgridtype: The grid type.
|
||||
// 0 -- unstruct grid.
|
||||
// 1 -- struct grid.
|
||||
// maxproc: The number of partition zones that want to be divided into,
|
||||
// which is equal to the number of CPU processors you want.
|
||||
// Usually, 50~100 thousands structured cells per CPU-Core is suggested.
|
||||
// 30~70 thousands unstructured cells per CPU-Core is suggested.
|
||||
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||
|
||||
int pgridtype = 1;
|
||||
int maxproc = 4;
|
||||
|
||||
string original_grid_file = "./grid/cylinder_str.fts";
|
||||
string partition_grid_file = "./grid/cylinder_str__4.fts";
|
||||
|
||||
// numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid.
|
||||
// 1 -- single level.
|
||||
// 2 -- 2 level.
|
||||
// N -- N level,..., et al.
|
||||
int numberOfMultigrid = 1;
|
||||
Loading…
Reference in New Issue