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PHengLEI2112版本已有算例参数及文档更新

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hechao 2021-12-31 11:27:31 +08:00
parent 356ace3f2e
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B01_TwoD_NACA0012_SA_Unstruct_1CPU/bin/cfd_para.hypara
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@ -21,6 +21,7 @@
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
// 2 -- Grid refinement.
// 3 -- Grid merging, merge two blocks into one block.
// 4 -- Grid deformation, achieve unstructured grid deformation.
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
// multiblock: Multi-block grid or not, only for structured grid conversion.
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
//-----------------------------------------------------------------------
// from_gfile: path of original data file for unstructure grid convert from.
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
int numberOfGridFile = 1;
string from_gfile = "./grid/rae2822_hybrid2d.cas";
string from_gfile1= "";
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
// ----------------- some advanced choices ------------------------------
// iunsteady: The Grid is for unsteady simulation or not.
int iunsteady = 0;
int iale = 0;
int codeOfAleModel = 0;
// fileformat: Ustar Grid file format.
@ -122,15 +125,38 @@ int isDeform = 0;
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
int projectOrgPoint = 0; // if project original wall points.
// ----------------- Grid Deform Parameters -----------------------------
// deformationMethod: Grid Deform.
// 1 -- SPRING.
// 2 -- RBF.
// stationalGridFile: Original grid file.
// visualFileName : The visualization file path of deform grid.
// nDeformStep : The max deform step.
// flapAngle : The max flap angle.
// rotatePostionZ : Rotate postion.
// rotatePostionY : Rotate postion.
// gridSlice : If dump slice grid.
// sliceAxis : Grid slice axis.
// slicePosition : Grid slice position.
int nDeformStep = 40;
double flapAngle = 10.0;
double rotatePostionZ = 4.00003;
double rotatePostionY = 3.05;
int deformationMethod = 2;
string stationalGridFile = "./grid/Segment2Brid.fts";
string visualFileName = "./results/deformedGrid.dat"
int gridSlice = 1;
int sliceAxis = 1;
double slicePosition = 13;
// ----------------- RBF Parameters -------------------------------------
// symmetryPlane: Which symmetry plane is used in the mesh.
// 0 -- without symmetry.
// 1 -- plane of x=0.
// 2 -- plane of y=0.
// 3 -- plane of z=0.
int numberOfReferenceCP = 10;
double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// numberOfReferenceCP : Number of reference Control Points.
// influencePara : The RBF influence radius parameter.
int numberOfReferenceCP = 40;
double influencePara = 25.0;
// ----------------- Periodic Parameters --------------------------------
// Notice: Rotational periodicity only support rotation along the X axis!
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
// translationLength[]: The relative distance between two periodic face
which only support one direction.
// rotationAngle: The relative angle between two periodic face.
which is recorded in degrees.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
// 0 -- Interface. (default)
// 1 -- Physical boundary condition, used in Hybrid solver.
// 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.
// parallelPartitionMethod: 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.
// 2 -- Using Metis for homogeneous MPI.
// 3 -- using METIS partition for homogeneous OpenMP.
@ -238,6 +269,8 @@ int compressible = 1;
// 1 -- the flight conditions.
// 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions.
// 4 -- the condition that the velocity, temperature and density are given.
// 5 -- the condition that the velocity, temperature and pressure are given.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -251,10 +284,12 @@ int compressible = 1;
// 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.
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, 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
// condition is radiation equilibrium temperature, and 0.8 is the default value.
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
double refMachNumber = 0.73;
double attackd = 2.79;
@ -263,7 +298,7 @@ double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 6.5e6;
double refDimensionalTemperature = 288.15;
double freestream_vibration_temperature = 10000.00;
double freestream_vibration_temperature = 300.00;
//int inflowParaType = 1;
//double height = 0.001;
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
//double refDimensionalTemperature = 288.144;
//double refDimensionalPressure = 1.01313E05;
//The velocity, temperature and density are fixed.
//int inflowParaType = 4;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalDensity = 1.0e3;
//The velocity, temperature and pressure are fixed.
//int inflowParaType = 5;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalPressure = 1.0e5;
//The MachNumber, temperature and pressure are fixed.
//int inflowParaType = 6;
//double refDimensionalTemperature = 293;
//double refDimensionalPressure = 8886.06;
double wallTemperature = -1.0;
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.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.
double refMolecularWeight = 28.9644; // unit of g/mol.
//-----------------------------------------------------------------------
# Spatial Discretisation #
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
// Using this when solve structered grid or hybrid.
// -- "vanleer", "steger", "hlle", "lax_f".
// -- "roe", "modified_roe".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
// str_limiter_name: Limiter of struct grid.
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
// -- "nolim", no limiter.
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod".
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
// -- "nolim", no limiter.
// uns_vis_name: Discretisation method of viscous term.
// -- "std", "test", "aver", "new1", "new2".
// uns_gradient: Gradient reconstruction method.
// gradientName: Gradient reconstruction method.
// -- "default", "ggcell", "ggnode", "lsq".
// ivencat: Variation of vencat limiter.
// 0 -- org method, it is independent of grid scale.
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
// 1 -- unsteay.
// 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.
// ifStaticsFlowField: Statistical variables for DES simulation.
// ifStaticsFlowField: Statistical variables for unsteady simulation.
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
// startStatisticStep: Outer step when start statistics.
// when the value is larger than "maxSimuStep", it is useless.
// statisticalTimePeriod: Used as time period of statistic analysis.
// when the value is negative, time period is treated as infinite.
// statisticMethod: Statistic reynolds stress method.
0 --tau = <q^2> - <q>^2
1 --tau = <u'u'>
// min_sub_iter: The min sub iteration of unsteady simulation.
// max_sub_iter: The max sub iteration of unsteady simulation.
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
@ -454,7 +511,10 @@ int iunsteady = 0;
double physicalTimeStep = 0.01;
int ifStartFromSteadyResults = 0;
int ifStaticsFlowField = 0;
int ifStaticsReynoldsStress = 0;
int startStatisticStep = 800000;
double statisticalTimePeriod = -1.0;
int statisticMethod = 0;
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
int methodOfDualTime = 3;
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
double csrv = 2.0;
double timemax = 1.0e10;
double dtsave = -1.0;
int codeOfAleModel = 0;
int aleStartStrategy = -1;
int maxale = 10;
double dtau = 0.001;
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
int numberOfGridGroups = 1;
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
string wallTemperaturefile= "";
int walldistMethod = 1;
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt";
string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string samplefile = "results/sample.dat";
int nDumpSurfaceInfo = 0;
string wall_varfile = "";
string jetDefineFile = "bin/jet.hypara";
string overset_gridfile = "results/iblank.ovs";
string sixDofFileName = "results/sixDofInfo.dat";
string derivativeFileName = "results/identify.dat";
string hysteresisFileName = "results/force_beta.plt";
int plotFieldType = 0;
@ -554,6 +614,11 @@ int plotFieldType = 0;
int visualfileType = 1;
// samplefileMode: The dump mode of sample file.
// 0 -- dump out every probe/line/surface data for all step intervals.
// 1 -- dump out all probe/line/surface data for every step intervals.
int samplefileMode = 0;
// visualSlice: The slice of tecflow.
// 0 -- Do not save slice data.
// 1 -- comput and save it to sliceFile.
@ -567,11 +632,13 @@ int visualSlice = 0;
int sliceAxis = 1;
double slicePostion = -0.5;
string sliceFile = "results/Slice.plt";
int dumpWallFaceCenter = 0;
// min-max box of the visual block.
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
double upperPlotFieldBox[] = [1.0 1.0 1.0];
//-----------the optional parameters list for the flow field output----------------
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- 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), iblank(81).
// -- specific heat ratio(gama, 56)
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
// Variables order must from small to big.
//-----------the optional parameters list for the wall boundary condition----------------
// nVisualWallVariables: The number of visual variables on wall.
// visualWallVariables : dumped variable types, listed as following:
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -overlap iblank(iblank, 81)
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
// dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate.
int dumpStandardModel = 0;
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
int turbInterval = 1;
int turbOrderStruct = 2;
int kindOfTurbSource = 0;
int mod_turb_res = 0;
double turb_relax = 1.0;
@ -652,6 +736,10 @@ double muoo = 3.0;
double kwoo = 5.0;
int transitionType = 0;
double turbIntensity = -1.0;
int freeturbIntensitySRModify = 0;
double freeDecayXLocation = 0.0;
int compressibleCorrection = 0;
int transitionMaFix = 1;
# maximum eddy viscosity (myt/my) max.
double eddyViscosityLimit = 1.0e10;
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
# LES Parameter #
//-----------------------------------------------------------------------
// iLES: Create LESSolver or not.
// >= 1 - Create LESSolver;
// < 1 - not.
// == 1 - Create LESSolver;
// != 1 - not.
// amplitudeofDisturb: Amplitude of adding disturb.
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
// iterdisturb: Add random disturb in every sub-iter or only first sub-iter.
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
// utau: friction velocity, using in DNSDisturb.
// sgsmodel: subgrid scale model.
// = "smagorinsky";
// = "dsm";
// = "wale".
// = "dsmCom";
// = "wale";
// = "sigma".
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
// = 2 - pow(deltai * deltaj *deltak, 1/3);
// = 3 - Devloped by Scotti.
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
int deltaFunctionType = 2;
int wallDampingFunctionType = 1;
int turbViscousCutType = 2;
double smagConstant = 0.135;
double smagConstant = 0.1;
double isotropicConstant = 0.0;
double waleConstant = 0.6;
double sigmaConstant = 1.35;
int filterDirection[] = [1, 1, 0];
int averageDirection[] = [0, 0, 0];
double testFilterScale = 2.0;
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
// nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D.
// 5 -- for 3D.
// nGasModel: The type of gas.
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
// Otherwise, the pure gas with one component is used for perfect gas.
// 0 -- Earth gas.
// 1 -- Mars gas.
// 2 -- Argon.
// 3 -- Nitrogen.
// nEnergyRecycle: The type of EnergyModel Recycle.
// 0 -- not used .
// 1 -- used.
// nDensityModify: The type of densitymodify.
// 0 -- not used.
// 1 -- used.
// nchem:
// 0 -- without chemical reaction flow.
// 1 -- the chemical reaction flow is considered.
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
// 0 -- perfect gas.
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
// the value equals to or is greater than 1, and 3 is for default value.
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
// the value equals to or is greater than 1, and 3 is for default value.
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
// the value equals to or is greater than 1, and 3 is for default value.
// nSlipBCModel : The computational model of slip boundary conditions.
// 0 -- no slip.
// 1 -- the conventional Maxwell slip conditions.
// 2 -- the Gokcen slip conditions.
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
// 4 -- the Kogan simplified slip conditions.
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
// nchemsrc:
// 0 -- the source terms are not computed.
// 1 -- the source terms are computed.
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
// 1 -- One-temperature model.
// 2 -- Two-temperature model.
// 3 -- Three-temperature model.
// nTEnergyModel: the method to computing temperature energy model.
// 0 -- the energy term is computed using the conventional method.
// 1 -- the energy term is computed using the curve fitting method.
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
// catalyticCoef:
// 0.0 -- full non-catalytic wall boundary condition.
// 1.0 -- full catalytic wall boundary condition.
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
// nTemperatureJump : the method to calculate the temperature jump.
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
// 1.0 -- proposed by Maxwell.
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
// 1.146 -- proposed for an additional "fictitious" velocity slip.
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
// 0 -- not freeze, the chemical reaction sources will be calculated.
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
// nDebug: cout the Wrong place and abort
// 0 -- not used.
// 1 -- used.
// nSpeciesLimit: limitter of gas species
// 0 -- not used.
// 1 -- used.
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
// 0 -- method 0.
// 1 -- method 1.
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
// 0 -- not used.
// 1 -- used.
// nChemcalSourceModified: Modified on ChemcalSource
// 0 -- not used.
// 1 -- used.
// nAblation:
// 0 -- The wall ablation is not computed.
// 1 -- The wall ablation is computed.
// isInjection:
// 0 -- The injection velocity of ablation wall is not computed.
// 1 -- The injection velocity of ablation wall is computed.
// nViscosityModel:
// 0 -- Blottner fitting method.
// 1 -- Gupta fitting method.
// nSutherland:
// 0 -- stands for selecting the Blotter curve fits mode.
// 1 -- stands for Sutherland relation.
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
// "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.
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
// 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.
@ -758,6 +935,10 @@ int dg_high_order = 0;
int iapplication = 0;
int iCodeBranch = 0;
int nm = 5;
int nEquilibriumGas = 0;
int nPCWCycleStep = 3;
int nRETCycleStep = 3;
int nSLIPCycleStep= 3;
double refGama = 1.4;
double prl = 0.72;
@ -770,23 +951,73 @@ int nchem = 0;
int nchemsrc = 1;
int nchemrad = 1;
int ntmodel = 1;
int nChemicalFlowStep = 0;
int nEnergyRecycle = 0;
int nSlipBCModel = 0;
int nDensityModify = 1;
int nTEnergyModel = 0;
int nMeanFreePathType = 0;
int nIsChemicalFreeze = 0;
int nIsSuperCatalytic = 1;
int nTemperatureJump = 0;
double parkVDPower = 0.6;
double catalyticCoef = 0.0;
double sigmaVelocity = 1.0;
double sigmaTemperature = 1.0;
double sigmaMassFraction = 1.0;
double velocitySlipCorrectConstant = 1.0;
double chemicalRelaxCorf = 1.0;
double chemicalSpectrumRadiusCoef = 1.0;
double viscousSpectrumRadiusCoef = 1.0;
double inviscidSpectrumRadiusCoef = 1.0;
double staticPressureRelaxCorf = 1.0;
double veTemperatureMin = 30.0;
int nDebug = 0;
int nSpeciesLimit = 0;
int nTurblenceForChemical = 0;
int nViscosityFluxSublevelModified = 0 ;
int nChemcalSourceModified = 0;
int nAblation = 0;
int isInjection = 0;
int nViscosityModel = 0;
int nMarsModel = 0;
string gasfile = "DK5";
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
string speciesName = "O, O2, NO, N, N2";
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
//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, 0.233, 0.0, 0.0, 0.0, 0.767, 0.0";
//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, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Mars-Pa8";
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
//string gasfile = "DK7";
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Combustion-12";
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
//string gasfile = "Gas-Mixture";
//string speciesName ="SpeciesA, SpeciesB";
//string initMassFraction = "1.0, 0.0";
int nSutherland = 0;
double gamaSpeciesA = 1.4;
double gamaSpeciesB = 1.3;
double molecularWeightSpeciesA = 29.0;
double molecularWeightSpeciesB = 30.0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0;
#########################################################################
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
#########################################################################
# High Order Struct Solver #
#########################################################################
// ifvfd:
// isFVMOrFDM:
// 0 -- NSSolverStruct using Finite Volume Method.
// 1 -- NSSolverStruct using Finite Differ Method.
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// -- "roe", "steger".
// structhighordergradient:
// -- "conservation", "chain_rule".
int ifvfd = 0;
int isFVMOrFDM = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6;
@ -885,8 +1116,12 @@ int allReduceStep = 1;
// codeOfOversetGrid: Overlapping(overset) grid or not.
// 0 -- NON-overlapping grid.
// 1 -- Overlapping grid.
// oversetInterpolationMethod: the method of overset interpolation while field simulation
// 0 -- set the acceptor cell value by donor cell value.
// 1 -- set the acceptor cell value by distance weight of donor cell value.
int codeOfOversetGrid = 0;
int codeOfOversetSlipGrid = 0;
int oversetInterpolationMethod = 0;
int readOversetFileOrNot = 0;
int symetryOrNot = 0;
int readInAuxiliaryInnerGrid = 1;
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
string auxiliaryInnerGrid2 = "";
string oversetGridFileName = "./grid/overlap.ovs";
string oversetGridFileName = "./grid/iblank.ovs";
double walldistMainZone = 1.0
double toleranceForOversetSearch = 1.0e-3;
double toleranceForOversetBox = 1.0e-3;
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
int numberOfMovingBodies = 2;
// ----------------- ALE configuration ------------------------------
int codeOfAleModel = 1;
int aleStartStrategy = -1;
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
int strategyForGCLSource = 0; //0-present; 1-Ahn;
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
int methodForKineticEquation = 0;
double relaxParameterOfKinetic = 1.0;
#########################################################################
# motive information #
#########################################################################
int numberOfMovingBodies = 1;
############################## body0 ##############################
//mass of parts
double mass_0 = 1.0;
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
//initial six DOF position information of parts. xc yc zc
double massCenter_0[] = 0.0 , 0.0, 0.0;
//initial six DOF position information of parts. angleX angleY angleZ
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
//initial six DOF move information of parts. vc vy vz
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
//initial six DOF move information of parts. omigX omigY omigZ
double angularVelocity_0[] = 0.0, 0.0, 0.0;
//the object that the parts belong to.
int fartherIndex_0 = -1;
//the assembly position of the parts. xc yc zc angleX angleY angleZ
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
//the move pattern of the parts.
// -1 given motion partten.
// 0 still.
// 1 six DOF motion.
// 2 three DOF motion.
// 11 X-axis forced motion.
// 12 Y-axis forced motion.
// 13 Z-axis forced motion.
// 14 forced pitch motion.
// 15 forced yaw motion.
// 16 forced roll motion.
int RBDMethod_0 = 0;
double amplitude_0 = 0.0;
double reduceFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
//additional force (system axis) fX fY fZ
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
//additional moment of Force (system axis) mX mY mZ
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
//the deformation method of the parts.
int morphing_0 = 0;
// post indentify
int integralOrder = 4;
// ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0;
//@double refReNumber = 2.329418E08;
//@double refDimensionalTemperature = 288.144;
//@double refDimensionalPressure = 1.01313E05;
//@double height = -0.001;
//@double refReNumber = 6.5e6;
//@double refDimensionalTemperature = 288.15;
//@double freestream_vibration_temperature = 300.00;
//@double refDimensionalPressure = 0;
//@double height = 0;
//@int nsubsonicInlet = 0;
//@int nsubsonicOutlet = 0;
//@string inLetFileName = "./bin/subsonicInlet.hypara";
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
//@double refDimensionalVelocity = 0;
//@double refDimensionalDensity = 0;
#########################################################################
# Old Parameter #

6
B01_TwoD_NACA0012_SA_Unstruct_1CPU/bin/cfd_para_subsonic.hypara
View File

@ -57,9 +57,9 @@ double refDimensionalTemperature = 300.0;
double gridScaleFactor = 1.0;
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
double forceRefenenceLength = 1.0; // unit of meter.
double forceRefenenceArea = 1.0; // unit of meter^2.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.

379
B02_TwoD_NACA4412_SA_Unstruct_2CPU/bin/cfd_para.hypara
View File

@ -21,6 +21,7 @@
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
// 2 -- Grid refinement.
// 3 -- Grid merging, merge two blocks into one block.
// 4 -- Grid deformation, achieve unstructured grid deformation.
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
// multiblock: Multi-block grid or not, only for structured grid conversion.
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
//-----------------------------------------------------------------------
// from_gfile: path of original data file for unstructure grid convert from.
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
int numberOfGridFile = 1;
string from_gfile = "./grid/rae2822_hybrid2d.cas";
string from_gfile1= "";
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
// ----------------- some advanced choices ------------------------------
// iunsteady: The Grid is for unsteady simulation or not.
int iunsteady = 0;
int iale = 0;
int codeOfAleModel = 0;
// fileformat: Ustar Grid file format.
@ -122,15 +125,38 @@ int isDeform = 0;
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
int projectOrgPoint = 0; // if project original wall points.
// ----------------- Grid Deform Parameters -----------------------------
// deformationMethod: Grid Deform.
// 1 -- SPRING.
// 2 -- RBF.
// stationalGridFile: Original grid file.
// visualFileName : The visualization file path of deform grid.
// nDeformStep : The max deform step.
// flapAngle : The max flap angle.
// rotatePostionZ : Rotate postion.
// rotatePostionY : Rotate postion.
// gridSlice : If dump slice grid.
// sliceAxis : Grid slice axis.
// slicePosition : Grid slice position.
int nDeformStep = 40;
double flapAngle = 10.0;
double rotatePostionZ = 4.00003;
double rotatePostionY = 3.05;
int deformationMethod = 2;
string stationalGridFile = "./grid/Segment2Brid.fts";
string visualFileName = "./results/deformedGrid.dat"
int gridSlice = 1;
int sliceAxis = 1;
double slicePosition = 13;
// ----------------- RBF Parameters -------------------------------------
// symmetryPlane: Which symmetry plane is used in the mesh.
// 0 -- without symmetry.
// 1 -- plane of x=0.
// 2 -- plane of y=0.
// 3 -- plane of z=0.
int numberOfReferenceCP = 10;
double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// numberOfReferenceCP : Number of reference Control Points.
// influencePara : The RBF influence radius parameter.
int numberOfReferenceCP = 40;
double influencePara = 25.0;
// ----------------- Periodic Parameters --------------------------------
// Notice: Rotational periodicity only support rotation along the X axis!
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
// translationLength[]: The relative distance between two periodic face
which only support one direction.
// rotationAngle: The relative angle between two periodic face.
which is recorded in degrees.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
// 0 -- Interface. (default)
// 1 -- Physical boundary condition, used in Hybrid solver.
// 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.
// parallelPartitionMethod: 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.
// 2 -- Using Metis for homogeneous MPI.
// 3 -- using METIS partition for homogeneous OpenMP.
@ -238,6 +269,8 @@ int compressible = 1;
// 1 -- the flight conditions.
// 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions.
// 4 -- the condition that the velocity, temperature and density are given.
// 5 -- the condition that the velocity, temperature and pressure are given.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -251,10 +284,12 @@ int compressible = 1;
// 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.
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, 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
// condition is radiation equilibrium temperature, and 0.8 is the default value.
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
double refMachNumber = 0.73;
double attackd = 2.79;
@ -263,7 +298,7 @@ double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 6.5e6;
double refDimensionalTemperature = 288.15;
double freestream_vibration_temperature = 10000.00;
double freestream_vibration_temperature = 300.00;
//int inflowParaType = 1;
//double height = 0.001;
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
//double refDimensionalTemperature = 288.144;
//double refDimensionalPressure = 1.01313E05;
//The velocity, temperature and density are fixed.
//int inflowParaType = 4;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalDensity = 1.0e3;
//The velocity, temperature and pressure are fixed.
//int inflowParaType = 5;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalPressure = 1.0e5;
//The MachNumber, temperature and pressure are fixed.
//int inflowParaType = 6;
//double refDimensionalTemperature = 293;
//double refDimensionalPressure = 8886.06;
double wallTemperature = -1.0;
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.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.
double refMolecularWeight = 28.9644; // unit of g/mol.
//-----------------------------------------------------------------------
# Spatial Discretisation #
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
// Using this when solve structered grid or hybrid.
// -- "vanleer", "steger", "hlle", "lax_f".
// -- "roe", "modified_roe".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
// str_limiter_name: Limiter of struct grid.
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
// -- "nolim", no limiter.
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod".
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
// -- "nolim", no limiter.
// uns_vis_name: Discretisation method of viscous term.
// -- "std", "test", "aver", "new1", "new2".
// uns_gradient: Gradient reconstruction method.
// gradientName: Gradient reconstruction method.
// -- "default", "ggcell", "ggnode", "lsq".
// ivencat: Variation of vencat limiter.
// 0 -- org method, it is independent of grid scale.
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
// 1 -- unsteay.
// 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.
// ifStaticsFlowField: Statistical variables for DES simulation.
// ifStaticsFlowField: Statistical variables for unsteady simulation.
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
// startStatisticStep: Outer step when start statistics.
// when the value is larger than "maxSimuStep", it is useless.
// statisticalTimePeriod: Used as time period of statistic analysis.
// when the value is negative, time period is treated as infinite.
// statisticMethod: Statistic reynolds stress method.
0 --tau = <q^2> - <q>^2
1 --tau = <u'u'>
// min_sub_iter: The min sub iteration of unsteady simulation.
// max_sub_iter: The max sub iteration of unsteady simulation.
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
@ -454,7 +511,10 @@ int iunsteady = 0;
double physicalTimeStep = 0.01;
int ifStartFromSteadyResults = 0;
int ifStaticsFlowField = 0;
int ifStaticsReynoldsStress = 0;
int startStatisticStep = 800000;
double statisticalTimePeriod = -1.0;
int statisticMethod = 0;
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
int methodOfDualTime = 3;
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
double csrv = 2.0;
double timemax = 1.0e10;
double dtsave = -1.0;
int codeOfAleModel = 0;
int aleStartStrategy = -1;
int maxale = 10;
double dtau = 0.001;
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
int numberOfGridGroups = 1;
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
string wallTemperaturefile= "";
int walldistMethod = 1;
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt";
string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string samplefile = "results/sample.dat";
int nDumpSurfaceInfo = 0;
string wall_varfile = "";
string jetDefineFile = "bin/jet.hypara";
string overset_gridfile = "results/iblank.ovs";
string sixDofFileName = "results/sixDofInfo.dat";
string derivativeFileName = "results/identify.dat";
string hysteresisFileName = "results/force_beta.plt";
int plotFieldType = 0;
@ -554,6 +614,11 @@ int plotFieldType = 0;
int visualfileType = 1;
// samplefileMode: The dump mode of sample file.
// 0 -- dump out every probe/line/surface data for all step intervals.
// 1 -- dump out all probe/line/surface data for every step intervals.
int samplefileMode = 0;
// visualSlice: The slice of tecflow.
// 0 -- Do not save slice data.
// 1 -- comput and save it to sliceFile.
@ -567,11 +632,13 @@ int visualSlice = 0;
int sliceAxis = 1;
double slicePostion = -0.5;
string sliceFile = "results/Slice.plt";
int dumpWallFaceCenter = 0;
// min-max box of the visual block.
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
double upperPlotFieldBox[] = [1.0 1.0 1.0];
//-----------the optional parameters list for the flow field output----------------
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- 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), iblank(81).
// -- specific heat ratio(gama, 56)
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
// Variables order must from small to big.
//-----------the optional parameters list for the wall boundary condition----------------
// nVisualWallVariables: The number of visual variables on wall.
// visualWallVariables : dumped variable types, listed as following:
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -overlap iblank(iblank, 81)
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
// dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate.
int dumpStandardModel = 0;
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
int turbInterval = 1;
int turbOrderStruct = 2;
int kindOfTurbSource = 0;
int mod_turb_res = 0;
double turb_relax = 1.0;
@ -652,6 +736,10 @@ double muoo = 3.0;
double kwoo = 5.0;
int transitionType = 0;
double turbIntensity = -1.0;
int freeturbIntensitySRModify = 0;
double freeDecayXLocation = 0.0;
int compressibleCorrection = 0;
int transitionMaFix = 1;
# maximum eddy viscosity (myt/my) max.
double eddyViscosityLimit = 1.0e10;
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
# LES Parameter #
//-----------------------------------------------------------------------
// iLES: Create LESSolver or not.
// >= 1 - Create LESSolver;
// < 1 - not.
// == 1 - Create LESSolver;
// != 1 - not.
// amplitudeofDisturb: Amplitude of adding disturb.
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
// iterdisturb: Add random disturb in every sub-iter or only first sub-iter.
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
// utau: friction velocity, using in DNSDisturb.
// sgsmodel: subgrid scale model.
// = "smagorinsky";
// = "dsm";
// = "wale".
// = "dsmCom";
// = "wale";
// = "sigma".
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
// = 2 - pow(deltai * deltaj *deltak, 1/3);
// = 3 - Devloped by Scotti.
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
int deltaFunctionType = 2;
int wallDampingFunctionType = 1;
int turbViscousCutType = 2;
double smagConstant = 0.135;
double smagConstant = 0.1;
double isotropicConstant = 0.0;
double waleConstant = 0.6;
double sigmaConstant = 1.35;
int filterDirection[] = [1, 1, 0];
int averageDirection[] = [0, 0, 0];
double testFilterScale = 2.0;
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
// nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D.
// 5 -- for 3D.
// nGasModel: The type of gas.
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
// Otherwise, the pure gas with one component is used for perfect gas.
// 0 -- Earth gas.
// 1 -- Mars gas.
// 2 -- Argon.
// 3 -- Nitrogen.
// nEnergyRecycle: The type of EnergyModel Recycle.
// 0 -- not used .
// 1 -- used.
// nDensityModify: The type of densitymodify.
// 0 -- not used.
// 1 -- used.
// nchem:
// 0 -- without chemical reaction flow.
// 1 -- the chemical reaction flow is considered.
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
// 0 -- perfect gas.
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
// the value equals to or is greater than 1, and 3 is for default value.
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
// the value equals to or is greater than 1, and 3 is for default value.
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
// the value equals to or is greater than 1, and 3 is for default value.
// nSlipBCModel : The computational model of slip boundary conditions.
// 0 -- no slip.
// 1 -- the conventional Maxwell slip conditions.
// 2 -- the Gokcen slip conditions.
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
// 4 -- the Kogan simplified slip conditions.
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
// nchemsrc:
// 0 -- the source terms are not computed.
// 1 -- the source terms are computed.
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
// 1 -- One-temperature model.
// 2 -- Two-temperature model.
// 3 -- Three-temperature model.
// nTEnergyModel: the method to computing temperature energy model.
// 0 -- the energy term is computed using the conventional method.
// 1 -- the energy term is computed using the curve fitting method.
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
// catalyticCoef:
// 0.0 -- full non-catalytic wall boundary condition.
// 1.0 -- full catalytic wall boundary condition.
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
// nTemperatureJump : the method to calculate the temperature jump.
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
// 1.0 -- proposed by Maxwell.
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
// 1.146 -- proposed for an additional "fictitious" velocity slip.
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
// 0 -- not freeze, the chemical reaction sources will be calculated.
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
// nDebug: cout the Wrong place and abort
// 0 -- not used.
// 1 -- used.
// nSpeciesLimit: limitter of gas species
// 0 -- not used.
// 1 -- used.
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
// 0 -- method 0.
// 1 -- method 1.
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
// 0 -- not used.
// 1 -- used.
// nChemcalSourceModified: Modified on ChemcalSource
// 0 -- not used.
// 1 -- used.
// nAblation:
// 0 -- The wall ablation is not computed.
// 1 -- The wall ablation is computed.
// isInjection:
// 0 -- The injection velocity of ablation wall is not computed.
// 1 -- The injection velocity of ablation wall is computed.
// nViscosityModel:
// 0 -- Blottner fitting method.
// 1 -- Gupta fitting method.
// nSutherland:
// 0 -- stands for selecting the Blotter curve fits mode.
// 1 -- stands for Sutherland relation.
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
// "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.
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
// 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.
@ -758,6 +935,10 @@ int dg_high_order = 0;
int iapplication = 0;
int iCodeBranch = 0;
int nm = 5;
int nEquilibriumGas = 0;
int nPCWCycleStep = 3;
int nRETCycleStep = 3;
int nSLIPCycleStep= 3;
double refGama = 1.4;
double prl = 0.72;
@ -770,23 +951,73 @@ int nchem = 0;
int nchemsrc = 1;
int nchemrad = 1;
int ntmodel = 1;
int nChemicalFlowStep = 0;
int nEnergyRecycle = 0;
int nSlipBCModel = 0;
int nDensityModify = 1;
int nTEnergyModel = 0;
int nMeanFreePathType = 0;
int nIsChemicalFreeze = 0;
int nIsSuperCatalytic = 1;
int nTemperatureJump = 0;
double parkVDPower = 0.6;
double catalyticCoef = 0.0;
double sigmaVelocity = 1.0;
double sigmaTemperature = 1.0;
double sigmaMassFraction = 1.0;
double velocitySlipCorrectConstant = 1.0;
double chemicalRelaxCorf = 1.0;
double chemicalSpectrumRadiusCoef = 1.0;
double viscousSpectrumRadiusCoef = 1.0;
double inviscidSpectrumRadiusCoef = 1.0;
double staticPressureRelaxCorf = 1.0;
double veTemperatureMin = 30.0;
int nDebug = 0;
int nSpeciesLimit = 0;
int nTurblenceForChemical = 0;
int nViscosityFluxSublevelModified = 0 ;
int nChemcalSourceModified = 0;
int nAblation = 0;
int isInjection = 0;
int nViscosityModel = 0;
int nMarsModel = 0;
string gasfile = "DK5";
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
string speciesName = "O, O2, NO, N, N2";
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
//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, 0.233, 0.0, 0.0, 0.0, 0.767, 0.0";
//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, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Mars-Pa8";
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
//string gasfile = "DK7";
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Combustion-12";
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
//string gasfile = "Gas-Mixture";
//string speciesName ="SpeciesA, SpeciesB";
//string initMassFraction = "1.0, 0.0";
int nSutherland = 0;
double gamaSpeciesA = 1.4;
double gamaSpeciesB = 1.3;
double molecularWeightSpeciesA = 29.0;
double molecularWeightSpeciesB = 30.0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0;
#########################################################################
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
#########################################################################
# High Order Struct Solver #
#########################################################################
// ifvfd:
// isFVMOrFDM:
// 0 -- NSSolverStruct using Finite Volume Method.
// 1 -- NSSolverStruct using Finite Differ Method.
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// -- "roe", "steger".
// structhighordergradient:
// -- "conservation", "chain_rule".
int ifvfd = 0;
int isFVMOrFDM = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6;
@ -885,8 +1116,12 @@ int allReduceStep = 1;
// codeOfOversetGrid: Overlapping(overset) grid or not.
// 0 -- NON-overlapping grid.
// 1 -- Overlapping grid.
// oversetInterpolationMethod: the method of overset interpolation while field simulation
// 0 -- set the acceptor cell value by donor cell value.
// 1 -- set the acceptor cell value by distance weight of donor cell value.
int codeOfOversetGrid = 0;
int codeOfOversetSlipGrid = 0;
int oversetInterpolationMethod = 0;
int readOversetFileOrNot = 0;
int symetryOrNot = 0;
int readInAuxiliaryInnerGrid = 1;
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
string auxiliaryInnerGrid2 = "";
string oversetGridFileName = "./grid/overlap.ovs";
string oversetGridFileName = "./grid/iblank.ovs";
double walldistMainZone = 1.0
double toleranceForOversetSearch = 1.0e-3;
double toleranceForOversetBox = 1.0e-3;
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
int numberOfMovingBodies = 2;
// ----------------- ALE configuration ------------------------------
int codeOfAleModel = 1;
int aleStartStrategy = -1;
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
int strategyForGCLSource = 0; //0-present; 1-Ahn;
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
int methodForKineticEquation = 0;
double relaxParameterOfKinetic = 1.0;
#########################################################################
# motive information #
#########################################################################
int numberOfMovingBodies = 1;
############################## body0 ##############################
//mass of parts
double mass_0 = 1.0;
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
//initial six DOF position information of parts. xc yc zc
double massCenter_0[] = 0.0 , 0.0, 0.0;
//initial six DOF position information of parts. angleX angleY angleZ
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
//initial six DOF move information of parts. vc vy vz
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
//initial six DOF move information of parts. omigX omigY omigZ
double angularVelocity_0[] = 0.0, 0.0, 0.0;
//the object that the parts belong to.
int fartherIndex_0 = -1;
//the assembly position of the parts. xc yc zc angleX angleY angleZ
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
//the move pattern of the parts.
// -1 given motion partten.
// 0 still.
// 1 six DOF motion.
// 2 three DOF motion.
// 11 X-axis forced motion.
// 12 Y-axis forced motion.
// 13 Z-axis forced motion.
// 14 forced pitch motion.
// 15 forced yaw motion.
// 16 forced roll motion.
int RBDMethod_0 = 0;
double amplitude_0 = 0.0;
double reduceFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
//additional force (system axis) fX fY fZ
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
//additional moment of Force (system axis) mX mY mZ
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
//the deformation method of the parts.
int morphing_0 = 0;
// post indentify
int integralOrder = 4;
// ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0;
//@double refReNumber = 2.329418E08;
//@double refDimensionalTemperature = 288.144;
//@double refDimensionalPressure = 1.01313E05;
//@double height = -0.001;
//@double refReNumber = 6.5e6;
//@double refDimensionalTemperature = 288.15;
//@double freestream_vibration_temperature = 300.00;
//@double refDimensionalPressure = 0;
//@double height = 0;
//@int nsubsonicInlet = 0;
//@int nsubsonicOutlet = 0;
//@string inLetFileName = "./bin/subsonicInlet.hypara";
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
//@double refDimensionalVelocity = 0;
//@double refDimensionalDensity = 0;
#########################################################################
# Old Parameter #

6
B02_TwoD_NACA4412_SA_Unstruct_2CPU/bin/cfd_para_subsonic.hypara
View File

@ -57,9 +57,9 @@ double refDimensionalTemperature = 297.78;
double gridScaleFactor = 1.0;
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
double forceRefenenceLength = 1.0; // unit of meter.
double forceRefenenceArea = 1.0; // unit of meter^2.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.

379
B03_TwoD_Rae2822_SA_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -21,6 +21,7 @@
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
// 2 -- Grid refinement.
// 3 -- Grid merging, merge two blocks into one block.
// 4 -- Grid deformation, achieve unstructured grid deformation.
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
// multiblock: Multi-block grid or not, only for structured grid conversion.
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
//-----------------------------------------------------------------------
// from_gfile: path of original data file for unstructure grid convert from.
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
int numberOfGridFile = 1;
string from_gfile = "./grid/rae2822_hybrid2d.cas";
string from_gfile1= "";
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
// ----------------- some advanced choices ------------------------------
// iunsteady: The Grid is for unsteady simulation or not.
int iunsteady = 0;
int iale = 0;
int codeOfAleModel = 0;
// fileformat: Ustar Grid file format.
@ -122,15 +125,38 @@ int isDeform = 0;
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
int projectOrgPoint = 0; // if project original wall points.
// ----------------- Grid Deform Parameters -----------------------------
// deformationMethod: Grid Deform.
// 1 -- SPRING.
// 2 -- RBF.
// stationalGridFile: Original grid file.
// visualFileName : The visualization file path of deform grid.
// nDeformStep : The max deform step.
// flapAngle : The max flap angle.
// rotatePostionZ : Rotate postion.
// rotatePostionY : Rotate postion.
// gridSlice : If dump slice grid.
// sliceAxis : Grid slice axis.
// slicePosition : Grid slice position.
int nDeformStep = 40;
double flapAngle = 10.0;
double rotatePostionZ = 4.00003;
double rotatePostionY = 3.05;
int deformationMethod = 2;
string stationalGridFile = "./grid/Segment2Brid.fts";
string visualFileName = "./results/deformedGrid.dat"
int gridSlice = 1;
int sliceAxis = 1;
double slicePosition = 13;
// ----------------- RBF Parameters -------------------------------------
// symmetryPlane: Which symmetry plane is used in the mesh.
// 0 -- without symmetry.
// 1 -- plane of x=0.
// 2 -- plane of y=0.
// 3 -- plane of z=0.
int numberOfReferenceCP = 10;
double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// numberOfReferenceCP : Number of reference Control Points.
// influencePara : The RBF influence radius parameter.
int numberOfReferenceCP = 40;
double influencePara = 25.0;
// ----------------- Periodic Parameters --------------------------------
// Notice: Rotational periodicity only support rotation along the X axis!
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
// translationLength[]: The relative distance between two periodic face
which only support one direction.
// rotationAngle: The relative angle between two periodic face.
which is recorded in degrees.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
// 0 -- Interface. (default)
// 1 -- Physical boundary condition, used in Hybrid solver.
// 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.
// parallelPartitionMethod: 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.
// 2 -- Using Metis for homogeneous MPI.
// 3 -- using METIS partition for homogeneous OpenMP.
@ -238,6 +269,8 @@ int compressible = 1;
// 1 -- the flight conditions.
// 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions.
// 4 -- the condition that the velocity, temperature and density are given.
// 5 -- the condition that the velocity, temperature and pressure are given.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -251,10 +284,12 @@ int compressible = 1;
// 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.
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, 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
// condition is radiation equilibrium temperature, and 0.8 is the default value.
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
double refMachNumber = 0.73;
double attackd = 2.79;
@ -263,7 +298,7 @@ double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 6.5e6;
double refDimensionalTemperature = 288.15;
double freestream_vibration_temperature = 10000.00;
double freestream_vibration_temperature = 300.00;
//int inflowParaType = 1;
//double height = 0.001;
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
//double refDimensionalTemperature = 288.144;
//double refDimensionalPressure = 1.01313E05;
//The velocity, temperature and density are fixed.
//int inflowParaType = 4;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalDensity = 1.0e3;
//The velocity, temperature and pressure are fixed.
//int inflowParaType = 5;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalPressure = 1.0e5;
//The MachNumber, temperature and pressure are fixed.
//int inflowParaType = 6;
//double refDimensionalTemperature = 293;
//double refDimensionalPressure = 8886.06;
double wallTemperature = -1.0;
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.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.
double refMolecularWeight = 28.9644; // unit of g/mol.
//-----------------------------------------------------------------------
# Spatial Discretisation #
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
// Using this when solve structered grid or hybrid.
// -- "vanleer", "steger", "hlle", "lax_f".
// -- "roe", "modified_roe".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
// str_limiter_name: Limiter of struct grid.
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
// -- "nolim", no limiter.
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod".
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
// -- "nolim", no limiter.
// uns_vis_name: Discretisation method of viscous term.
// -- "std", "test", "aver", "new1", "new2".
// uns_gradient: Gradient reconstruction method.
// gradientName: Gradient reconstruction method.
// -- "default", "ggcell", "ggnode", "lsq".
// ivencat: Variation of vencat limiter.
// 0 -- org method, it is independent of grid scale.
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
// 1 -- unsteay.
// 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.
// ifStaticsFlowField: Statistical variables for DES simulation.
// ifStaticsFlowField: Statistical variables for unsteady simulation.
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
// startStatisticStep: Outer step when start statistics.
// when the value is larger than "maxSimuStep", it is useless.
// statisticalTimePeriod: Used as time period of statistic analysis.
// when the value is negative, time period is treated as infinite.
// statisticMethod: Statistic reynolds stress method.
0 --tau = <q^2> - <q>^2
1 --tau = <u'u'>
// min_sub_iter: The min sub iteration of unsteady simulation.
// max_sub_iter: The max sub iteration of unsteady simulation.
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
@ -454,7 +511,10 @@ int iunsteady = 0;
double physicalTimeStep = 0.01;
int ifStartFromSteadyResults = 0;
int ifStaticsFlowField = 0;
int ifStaticsReynoldsStress = 0;
int startStatisticStep = 800000;
double statisticalTimePeriod = -1.0;
int statisticMethod = 0;
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
int methodOfDualTime = 3;
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
double csrv = 2.0;
double timemax = 1.0e10;
double dtsave = -1.0;
int codeOfAleModel = 0;
int aleStartStrategy = -1;
int maxale = 10;
double dtau = 0.001;
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
int numberOfGridGroups = 1;
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
string wallTemperaturefile= "";
int walldistMethod = 1;
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt";
string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string samplefile = "results/sample.dat";
int nDumpSurfaceInfo = 0;
string wall_varfile = "";
string jetDefineFile = "bin/jet.hypara";
string overset_gridfile = "results/iblank.ovs";
string sixDofFileName = "results/sixDofInfo.dat";
string derivativeFileName = "results/identify.dat";
string hysteresisFileName = "results/force_beta.plt";
int plotFieldType = 0;
@ -554,6 +614,11 @@ int plotFieldType = 0;
int visualfileType = 1;
// samplefileMode: The dump mode of sample file.
// 0 -- dump out every probe/line/surface data for all step intervals.
// 1 -- dump out all probe/line/surface data for every step intervals.
int samplefileMode = 0;
// visualSlice: The slice of tecflow.
// 0 -- Do not save slice data.
// 1 -- comput and save it to sliceFile.
@ -567,11 +632,13 @@ int visualSlice = 0;
int sliceAxis = 1;
double slicePostion = -0.5;
string sliceFile = "results/Slice.plt";
int dumpWallFaceCenter = 0;
// min-max box of the visual block.
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
double upperPlotFieldBox[] = [1.0 1.0 1.0];
//-----------the optional parameters list for the flow field output----------------
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- 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), iblank(81).
// -- specific heat ratio(gama, 56)
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
// Variables order must from small to big.
//-----------the optional parameters list for the wall boundary condition----------------
// nVisualWallVariables: The number of visual variables on wall.
// visualWallVariables : dumped variable types, listed as following:
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -overlap iblank(iblank, 81)
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
// dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate.
int dumpStandardModel = 0;
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
int turbInterval = 1;
int turbOrderStruct = 2;
int kindOfTurbSource = 0;
int mod_turb_res = 0;
double turb_relax = 1.0;
@ -652,6 +736,10 @@ double muoo = 3.0;
double kwoo = 5.0;
int transitionType = 0;
double turbIntensity = -1.0;
int freeturbIntensitySRModify = 0;
double freeDecayXLocation = 0.0;
int compressibleCorrection = 0;
int transitionMaFix = 1;
# maximum eddy viscosity (myt/my) max.
double eddyViscosityLimit = 1.0e10;
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
# LES Parameter #
//-----------------------------------------------------------------------
// iLES: Create LESSolver or not.
// >= 1 - Create LESSolver;
// < 1 - not.
// == 1 - Create LESSolver;
// != 1 - not.
// amplitudeofDisturb: Amplitude of adding disturb.
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
// iterdisturb: Add random disturb in every sub-iter or only first sub-iter.
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
// utau: friction velocity, using in DNSDisturb.
// sgsmodel: subgrid scale model.
// = "smagorinsky";
// = "dsm";
// = "wale".
// = "dsmCom";
// = "wale";
// = "sigma".
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
// = 2 - pow(deltai * deltaj *deltak, 1/3);
// = 3 - Devloped by Scotti.
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
int deltaFunctionType = 2;
int wallDampingFunctionType = 1;
int turbViscousCutType = 2;
double smagConstant = 0.135;
double smagConstant = 0.1;
double isotropicConstant = 0.0;
double waleConstant = 0.6;
double sigmaConstant = 1.35;
int filterDirection[] = [1, 1, 0];
int averageDirection[] = [0, 0, 0];
double testFilterScale = 2.0;
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
// nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D.
// 5 -- for 3D.
// nGasModel: The type of gas.
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
// Otherwise, the pure gas with one component is used for perfect gas.
// 0 -- Earth gas.
// 1 -- Mars gas.
// 2 -- Argon.
// 3 -- Nitrogen.
// nEnergyRecycle: The type of EnergyModel Recycle.
// 0 -- not used .
// 1 -- used.
// nDensityModify: The type of densitymodify.
// 0 -- not used.
// 1 -- used.
// nchem:
// 0 -- without chemical reaction flow.
// 1 -- the chemical reaction flow is considered.
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
// 0 -- perfect gas.
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
// the value equals to or is greater than 1, and 3 is for default value.
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
// the value equals to or is greater than 1, and 3 is for default value.
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
// the value equals to or is greater than 1, and 3 is for default value.
// nSlipBCModel : The computational model of slip boundary conditions.
// 0 -- no slip.
// 1 -- the conventional Maxwell slip conditions.
// 2 -- the Gokcen slip conditions.
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
// 4 -- the Kogan simplified slip conditions.
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
// nchemsrc:
// 0 -- the source terms are not computed.
// 1 -- the source terms are computed.
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
// 1 -- One-temperature model.
// 2 -- Two-temperature model.
// 3 -- Three-temperature model.
// nTEnergyModel: the method to computing temperature energy model.
// 0 -- the energy term is computed using the conventional method.
// 1 -- the energy term is computed using the curve fitting method.
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
// catalyticCoef:
// 0.0 -- full non-catalytic wall boundary condition.
// 1.0 -- full catalytic wall boundary condition.
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
// nTemperatureJump : the method to calculate the temperature jump.
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
// 1.0 -- proposed by Maxwell.
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
// 1.146 -- proposed for an additional "fictitious" velocity slip.
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
// 0 -- not freeze, the chemical reaction sources will be calculated.
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
// nDebug: cout the Wrong place and abort
// 0 -- not used.
// 1 -- used.
// nSpeciesLimit: limitter of gas species
// 0 -- not used.
// 1 -- used.
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
// 0 -- method 0.
// 1 -- method 1.
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
// 0 -- not used.
// 1 -- used.
// nChemcalSourceModified: Modified on ChemcalSource
// 0 -- not used.
// 1 -- used.
// nAblation:
// 0 -- The wall ablation is not computed.
// 1 -- The wall ablation is computed.
// isInjection:
// 0 -- The injection velocity of ablation wall is not computed.
// 1 -- The injection velocity of ablation wall is computed.
// nViscosityModel:
// 0 -- Blottner fitting method.
// 1 -- Gupta fitting method.
// nSutherland:
// 0 -- stands for selecting the Blotter curve fits mode.
// 1 -- stands for Sutherland relation.
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
// "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.
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
// 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.
@ -758,6 +935,10 @@ int dg_high_order = 0;
int iapplication = 0;
int iCodeBranch = 0;
int nm = 5;
int nEquilibriumGas = 0;
int nPCWCycleStep = 3;
int nRETCycleStep = 3;
int nSLIPCycleStep= 3;
double refGama = 1.4;
double prl = 0.72;
@ -770,23 +951,73 @@ int nchem = 0;
int nchemsrc = 1;
int nchemrad = 1;
int ntmodel = 1;
int nChemicalFlowStep = 0;
int nEnergyRecycle = 0;
int nSlipBCModel = 0;
int nDensityModify = 1;
int nTEnergyModel = 0;
int nMeanFreePathType = 0;
int nIsChemicalFreeze = 0;
int nIsSuperCatalytic = 1;
int nTemperatureJump = 0;
double parkVDPower = 0.6;
double catalyticCoef = 0.0;
double sigmaVelocity = 1.0;
double sigmaTemperature = 1.0;
double sigmaMassFraction = 1.0;
double velocitySlipCorrectConstant = 1.0;
double chemicalRelaxCorf = 1.0;
double chemicalSpectrumRadiusCoef = 1.0;
double viscousSpectrumRadiusCoef = 1.0;
double inviscidSpectrumRadiusCoef = 1.0;
double staticPressureRelaxCorf = 1.0;
double veTemperatureMin = 30.0;
int nDebug = 0;
int nSpeciesLimit = 0;
int nTurblenceForChemical = 0;
int nViscosityFluxSublevelModified = 0 ;
int nChemcalSourceModified = 0;
int nAblation = 0;
int isInjection = 0;
int nViscosityModel = 0;
int nMarsModel = 0;
string gasfile = "DK5";
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
string speciesName = "O, O2, NO, N, N2";
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
//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, 0.233, 0.0, 0.0, 0.0, 0.767, 0.0";
//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, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Mars-Pa8";
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
//string gasfile = "DK7";
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Combustion-12";
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
//string gasfile = "Gas-Mixture";
//string speciesName ="SpeciesA, SpeciesB";
//string initMassFraction = "1.0, 0.0";
int nSutherland = 0;
double gamaSpeciesA = 1.4;
double gamaSpeciesB = 1.3;
double molecularWeightSpeciesA = 29.0;
double molecularWeightSpeciesB = 30.0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0;
#########################################################################
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
#########################################################################
# High Order Struct Solver #
#########################################################################
// ifvfd:
// isFVMOrFDM:
// 0 -- NSSolverStruct using Finite Volume Method.
// 1 -- NSSolverStruct using Finite Differ Method.
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// -- "roe", "steger".
// structhighordergradient:
// -- "conservation", "chain_rule".
int ifvfd = 0;
int isFVMOrFDM = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6;
@ -885,8 +1116,12 @@ int allReduceStep = 1;
// codeOfOversetGrid: Overlapping(overset) grid or not.
// 0 -- NON-overlapping grid.
// 1 -- Overlapping grid.
// oversetInterpolationMethod: the method of overset interpolation while field simulation
// 0 -- set the acceptor cell value by donor cell value.
// 1 -- set the acceptor cell value by distance weight of donor cell value.
int codeOfOversetGrid = 0;
int codeOfOversetSlipGrid = 0;
int oversetInterpolationMethod = 0;
int readOversetFileOrNot = 0;
int symetryOrNot = 0;
int readInAuxiliaryInnerGrid = 1;
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
string auxiliaryInnerGrid2 = "";
string oversetGridFileName = "./grid/overlap.ovs";
string oversetGridFileName = "./grid/iblank.ovs";
double walldistMainZone = 1.0
double toleranceForOversetSearch = 1.0e-3;
double toleranceForOversetBox = 1.0e-3;
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
int numberOfMovingBodies = 2;
// ----------------- ALE configuration ------------------------------
int codeOfAleModel = 1;
int aleStartStrategy = -1;
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
int strategyForGCLSource = 0; //0-present; 1-Ahn;
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
int methodForKineticEquation = 0;
double relaxParameterOfKinetic = 1.0;
#########################################################################
# motive information #
#########################################################################
int numberOfMovingBodies = 1;
############################## body0 ##############################
//mass of parts
double mass_0 = 1.0;
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
//initial six DOF position information of parts. xc yc zc
double massCenter_0[] = 0.0 , 0.0, 0.0;
//initial six DOF position information of parts. angleX angleY angleZ
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
//initial six DOF move information of parts. vc vy vz
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
//initial six DOF move information of parts. omigX omigY omigZ
double angularVelocity_0[] = 0.0, 0.0, 0.0;
//the object that the parts belong to.
int fartherIndex_0 = -1;
//the assembly position of the parts. xc yc zc angleX angleY angleZ
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
//the move pattern of the parts.
// -1 given motion partten.
// 0 still.
// 1 six DOF motion.
// 2 three DOF motion.
// 11 X-axis forced motion.
// 12 Y-axis forced motion.
// 13 Z-axis forced motion.
// 14 forced pitch motion.
// 15 forced yaw motion.
// 16 forced roll motion.
int RBDMethod_0 = 0;
double amplitude_0 = 0.0;
double reduceFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
//additional force (system axis) fX fY fZ
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
//additional moment of Force (system axis) mX mY mZ
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
//the deformation method of the parts.
int morphing_0 = 0;
// post indentify
int integralOrder = 4;
// ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0;
//@double refReNumber = 2.329418E08;
//@double refDimensionalTemperature = 288.144;
//@double refDimensionalPressure = 1.01313E05;
//@double height = -0.001;
//@double refReNumber = 6.5e6;
//@double refDimensionalTemperature = 288.15;
//@double freestream_vibration_temperature = 300.00;
//@double refDimensionalPressure = 0;
//@double height = 0;
//@int nsubsonicInlet = 0;
//@int nsubsonicOutlet = 0;
//@string inLetFileName = "./bin/subsonicInlet.hypara";
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
//@double refDimensionalVelocity = 0;
//@double refDimensionalDensity = 0;
#########################################################################
# Old Parameter #

6
B03_TwoD_Rae2822_SA_Unstruct_1CPU/bin/cfd_para_transonic.hypara
View File

@ -56,9 +56,9 @@ double refDimensionalTemperature = 288.15;
double gridScaleFactor = 1.0;
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
double forceRefenenceLength = 1.0; // unit of meter.
double forceRefenenceArea = 1.0; // unit of meter^2.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.

21
B03_TwoD_Rae2822_SA_Unstruct_1CPU/bin/partition.hypara Normal file
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@ -0,0 +1,21 @@
// pgridtype: The grid type.
// 0 -- unstruct grid.
// 1 -- struct grid.
// maxproc: The number of partition zones that want to be divided into,
// which is equal to the number of CPU processors you want.
// Usually, 50~100 thousands structured cells per CPU-Core is suggested.
// 30~70 thousands unstructured cells per CPU-Core is suggested.
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
int pgridtype = 0;
int maxproc = 1;
string original_grid_file = "./grid/rae2822_hybrid2d_fine.fts";
string partition_grid_file = "./grid/rae2822_hybrid2d_fine.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;

379
B04_ThreeD_DLR-F6_SA_Unstruct_60CPU/bin/cfd_para.hypara
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@ -21,6 +21,7 @@
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
// 2 -- Grid refinement.
// 3 -- Grid merging, merge two blocks into one block.
// 4 -- Grid deformation, achieve unstructured grid deformation.
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
// multiblock: Multi-block grid or not, only for structured grid conversion.
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
//-----------------------------------------------------------------------
// from_gfile: path of original data file for unstructure grid convert from.
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
int numberOfGridFile = 1;
string from_gfile = "./grid/rae2822_hybrid2d.cas";
string from_gfile1= "";
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
// ----------------- some advanced choices ------------------------------
// iunsteady: The Grid is for unsteady simulation or not.
int iunsteady = 0;
int iale = 0;
int codeOfAleModel = 0;
// fileformat: Ustar Grid file format.
@ -122,15 +125,38 @@ int isDeform = 0;
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
int projectOrgPoint = 0; // if project original wall points.
// ----------------- Grid Deform Parameters -----------------------------
// deformationMethod: Grid Deform.
// 1 -- SPRING.
// 2 -- RBF.
// stationalGridFile: Original grid file.
// visualFileName : The visualization file path of deform grid.
// nDeformStep : The max deform step.
// flapAngle : The max flap angle.
// rotatePostionZ : Rotate postion.
// rotatePostionY : Rotate postion.
// gridSlice : If dump slice grid.
// sliceAxis : Grid slice axis.
// slicePosition : Grid slice position.
int nDeformStep = 40;
double flapAngle = 10.0;
double rotatePostionZ = 4.00003;
double rotatePostionY = 3.05;
int deformationMethod = 2;
string stationalGridFile = "./grid/Segment2Brid.fts";
string visualFileName = "./results/deformedGrid.dat"
int gridSlice = 1;
int sliceAxis = 1;
double slicePosition = 13;
// ----------------- RBF Parameters -------------------------------------
// symmetryPlane: Which symmetry plane is used in the mesh.
// 0 -- without symmetry.
// 1 -- plane of x=0.
// 2 -- plane of y=0.
// 3 -- plane of z=0.
int numberOfReferenceCP = 10;
double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// numberOfReferenceCP : Number of reference Control Points.
// influencePara : The RBF influence radius parameter.
int numberOfReferenceCP = 40;
double influencePara = 25.0;
// ----------------- Periodic Parameters --------------------------------
// Notice: Rotational periodicity only support rotation along the X axis!
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
// translationLength[]: The relative distance between two periodic face
which only support one direction.
// rotationAngle: The relative angle between two periodic face.
which is recorded in degrees.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
// 0 -- Interface. (default)
// 1 -- Physical boundary condition, used in Hybrid solver.
// 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.
// parallelPartitionMethod: 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.
// 2 -- Using Metis for homogeneous MPI.
// 3 -- using METIS partition for homogeneous OpenMP.
@ -238,6 +269,8 @@ int compressible = 1;
// 1 -- the flight conditions.
// 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions.
// 4 -- the condition that the velocity, temperature and density are given.
// 5 -- the condition that the velocity, temperature and pressure are given.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -251,10 +284,12 @@ int compressible = 1;
// 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.
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, 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
// condition is radiation equilibrium temperature, and 0.8 is the default value.
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
double refMachNumber = 0.73;
double attackd = 2.79;
@ -263,7 +298,7 @@ double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 6.5e6;
double refDimensionalTemperature = 288.15;
double freestream_vibration_temperature = 10000.00;
double freestream_vibration_temperature = 300.00;
//int inflowParaType = 1;
//double height = 0.001;
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
//double refDimensionalTemperature = 288.144;
//double refDimensionalPressure = 1.01313E05;
//The velocity, temperature and density are fixed.
//int inflowParaType = 4;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalDensity = 1.0e3;
//The velocity, temperature and pressure are fixed.
//int inflowParaType = 5;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalPressure = 1.0e5;
//The MachNumber, temperature and pressure are fixed.
//int inflowParaType = 6;
//double refDimensionalTemperature = 293;
//double refDimensionalPressure = 8886.06;
double wallTemperature = -1.0;
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.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.
double refMolecularWeight = 28.9644; // unit of g/mol.
//-----------------------------------------------------------------------
# Spatial Discretisation #
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
// Using this when solve structered grid or hybrid.
// -- "vanleer", "steger", "hlle", "lax_f".
// -- "roe", "modified_roe".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
// str_limiter_name: Limiter of struct grid.
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
// -- "nolim", no limiter.
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod".
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
// -- "nolim", no limiter.
// uns_vis_name: Discretisation method of viscous term.
// -- "std", "test", "aver", "new1", "new2".
// uns_gradient: Gradient reconstruction method.
// gradientName: Gradient reconstruction method.
// -- "default", "ggcell", "ggnode", "lsq".
// ivencat: Variation of vencat limiter.
// 0 -- org method, it is independent of grid scale.
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
// 1 -- unsteay.
// 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.
// ifStaticsFlowField: Statistical variables for DES simulation.
// ifStaticsFlowField: Statistical variables for unsteady simulation.
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
// startStatisticStep: Outer step when start statistics.
// when the value is larger than "maxSimuStep", it is useless.
// statisticalTimePeriod: Used as time period of statistic analysis.
// when the value is negative, time period is treated as infinite.
// statisticMethod: Statistic reynolds stress method.
0 --tau = <q^2> - <q>^2
1 --tau = <u'u'>
// min_sub_iter: The min sub iteration of unsteady simulation.
// max_sub_iter: The max sub iteration of unsteady simulation.
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
@ -454,7 +511,10 @@ int iunsteady = 0;
double physicalTimeStep = 0.01;
int ifStartFromSteadyResults = 0;
int ifStaticsFlowField = 0;
int ifStaticsReynoldsStress = 0;
int startStatisticStep = 800000;
double statisticalTimePeriod = -1.0;
int statisticMethod = 0;
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
int methodOfDualTime = 3;
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
double csrv = 2.0;
double timemax = 1.0e10;
double dtsave = -1.0;
int codeOfAleModel = 0;
int aleStartStrategy = -1;
int maxale = 10;
double dtau = 0.001;
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
int numberOfGridGroups = 1;
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
string wallTemperaturefile= "";
int walldistMethod = 1;
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt";
string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string samplefile = "results/sample.dat";
int nDumpSurfaceInfo = 0;
string wall_varfile = "";
string jetDefineFile = "bin/jet.hypara";
string overset_gridfile = "results/iblank.ovs";
string sixDofFileName = "results/sixDofInfo.dat";
string derivativeFileName = "results/identify.dat";
string hysteresisFileName = "results/force_beta.plt";
int plotFieldType = 0;
@ -554,6 +614,11 @@ int plotFieldType = 0;
int visualfileType = 1;
// samplefileMode: The dump mode of sample file.
// 0 -- dump out every probe/line/surface data for all step intervals.
// 1 -- dump out all probe/line/surface data for every step intervals.
int samplefileMode = 0;
// visualSlice: The slice of tecflow.
// 0 -- Do not save slice data.
// 1 -- comput and save it to sliceFile.
@ -567,11 +632,13 @@ int visualSlice = 0;
int sliceAxis = 1;
double slicePostion = -0.5;
string sliceFile = "results/Slice.plt";
int dumpWallFaceCenter = 0;
// min-max box of the visual block.
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
double upperPlotFieldBox[] = [1.0 1.0 1.0];
//-----------the optional parameters list for the flow field output----------------
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- 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), iblank(81).
// -- specific heat ratio(gama, 56)
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
// Variables order must from small to big.
//-----------the optional parameters list for the wall boundary condition----------------
// nVisualWallVariables: The number of visual variables on wall.
// visualWallVariables : dumped variable types, listed as following:
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -overlap iblank(iblank, 81)
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
// dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate.
int dumpStandardModel = 0;
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
int turbInterval = 1;
int turbOrderStruct = 2;
int kindOfTurbSource = 0;
int mod_turb_res = 0;
double turb_relax = 1.0;
@ -652,6 +736,10 @@ double muoo = 3.0;
double kwoo = 5.0;
int transitionType = 0;
double turbIntensity = -1.0;
int freeturbIntensitySRModify = 0;
double freeDecayXLocation = 0.0;
int compressibleCorrection = 0;
int transitionMaFix = 1;
# maximum eddy viscosity (myt/my) max.
double eddyViscosityLimit = 1.0e10;
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
# LES Parameter #
//-----------------------------------------------------------------------
// iLES: Create LESSolver or not.
// >= 1 - Create LESSolver;
// < 1 - not.
// == 1 - Create LESSolver;
// != 1 - not.
// amplitudeofDisturb: Amplitude of adding disturb.
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
// iterdisturb: Add random disturb in every sub-iter or only first sub-iter.
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
// utau: friction velocity, using in DNSDisturb.
// sgsmodel: subgrid scale model.
// = "smagorinsky";
// = "dsm";
// = "wale".
// = "dsmCom";
// = "wale";
// = "sigma".
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
// = 2 - pow(deltai * deltaj *deltak, 1/3);
// = 3 - Devloped by Scotti.
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
int deltaFunctionType = 2;
int wallDampingFunctionType = 1;
int turbViscousCutType = 2;
double smagConstant = 0.135;
double smagConstant = 0.1;
double isotropicConstant = 0.0;
double waleConstant = 0.6;
double sigmaConstant = 1.35;
int filterDirection[] = [1, 1, 0];
int averageDirection[] = [0, 0, 0];
double testFilterScale = 2.0;
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
// nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D.
// 5 -- for 3D.
// nGasModel: The type of gas.
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
// Otherwise, the pure gas with one component is used for perfect gas.
// 0 -- Earth gas.
// 1 -- Mars gas.
// 2 -- Argon.
// 3 -- Nitrogen.
// nEnergyRecycle: The type of EnergyModel Recycle.
// 0 -- not used .
// 1 -- used.
// nDensityModify: The type of densitymodify.
// 0 -- not used.
// 1 -- used.
// nchem:
// 0 -- without chemical reaction flow.
// 1 -- the chemical reaction flow is considered.
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
// 0 -- perfect gas.
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
// the value equals to or is greater than 1, and 3 is for default value.
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
// the value equals to or is greater than 1, and 3 is for default value.
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
// the value equals to or is greater than 1, and 3 is for default value.
// nSlipBCModel : The computational model of slip boundary conditions.
// 0 -- no slip.
// 1 -- the conventional Maxwell slip conditions.
// 2 -- the Gokcen slip conditions.
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
// 4 -- the Kogan simplified slip conditions.
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
// nchemsrc:
// 0 -- the source terms are not computed.
// 1 -- the source terms are computed.
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
// 1 -- One-temperature model.
// 2 -- Two-temperature model.
// 3 -- Three-temperature model.
// nTEnergyModel: the method to computing temperature energy model.
// 0 -- the energy term is computed using the conventional method.
// 1 -- the energy term is computed using the curve fitting method.
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
// catalyticCoef:
// 0.0 -- full non-catalytic wall boundary condition.
// 1.0 -- full catalytic wall boundary condition.
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
// nTemperatureJump : the method to calculate the temperature jump.
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
// 1.0 -- proposed by Maxwell.
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
// 1.146 -- proposed for an additional "fictitious" velocity slip.
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
// 0 -- not freeze, the chemical reaction sources will be calculated.
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
// nDebug: cout the Wrong place and abort
// 0 -- not used.
// 1 -- used.
// nSpeciesLimit: limitter of gas species
// 0 -- not used.
// 1 -- used.
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
// 0 -- method 0.
// 1 -- method 1.
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
// 0 -- not used.
// 1 -- used.
// nChemcalSourceModified: Modified on ChemcalSource
// 0 -- not used.
// 1 -- used.
// nAblation:
// 0 -- The wall ablation is not computed.
// 1 -- The wall ablation is computed.
// isInjection:
// 0 -- The injection velocity of ablation wall is not computed.
// 1 -- The injection velocity of ablation wall is computed.
// nViscosityModel:
// 0 -- Blottner fitting method.
// 1 -- Gupta fitting method.
// nSutherland:
// 0 -- stands for selecting the Blotter curve fits mode.
// 1 -- stands for Sutherland relation.
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
// "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.
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
// 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.
@ -758,6 +935,10 @@ int dg_high_order = 0;
int iapplication = 0;
int iCodeBranch = 0;
int nm = 5;
int nEquilibriumGas = 0;
int nPCWCycleStep = 3;
int nRETCycleStep = 3;
int nSLIPCycleStep= 3;
double refGama = 1.4;
double prl = 0.72;
@ -770,23 +951,73 @@ int nchem = 0;
int nchemsrc = 1;
int nchemrad = 1;
int ntmodel = 1;
int nChemicalFlowStep = 0;
int nEnergyRecycle = 0;
int nSlipBCModel = 0;
int nDensityModify = 1;
int nTEnergyModel = 0;
int nMeanFreePathType = 0;
int nIsChemicalFreeze = 0;
int nIsSuperCatalytic = 1;
int nTemperatureJump = 0;
double parkVDPower = 0.6;
double catalyticCoef = 0.0;
double sigmaVelocity = 1.0;
double sigmaTemperature = 1.0;
double sigmaMassFraction = 1.0;
double velocitySlipCorrectConstant = 1.0;
double chemicalRelaxCorf = 1.0;
double chemicalSpectrumRadiusCoef = 1.0;
double viscousSpectrumRadiusCoef = 1.0;
double inviscidSpectrumRadiusCoef = 1.0;
double staticPressureRelaxCorf = 1.0;
double veTemperatureMin = 30.0;
int nDebug = 0;
int nSpeciesLimit = 0;
int nTurblenceForChemical = 0;
int nViscosityFluxSublevelModified = 0 ;
int nChemcalSourceModified = 0;
int nAblation = 0;
int isInjection = 0;
int nViscosityModel = 0;
int nMarsModel = 0;
string gasfile = "DK5";
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
string speciesName = "O, O2, NO, N, N2";
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
//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, 0.233, 0.0, 0.0, 0.0, 0.767, 0.0";
//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, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Mars-Pa8";
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
//string gasfile = "DK7";
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Combustion-12";
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
//string gasfile = "Gas-Mixture";
//string speciesName ="SpeciesA, SpeciesB";
//string initMassFraction = "1.0, 0.0";
int nSutherland = 0;
double gamaSpeciesA = 1.4;
double gamaSpeciesB = 1.3;
double molecularWeightSpeciesA = 29.0;
double molecularWeightSpeciesB = 30.0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0;
#########################################################################
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
#########################################################################
# High Order Struct Solver #
#########################################################################
// ifvfd:
// isFVMOrFDM:
// 0 -- NSSolverStruct using Finite Volume Method.
// 1 -- NSSolverStruct using Finite Differ Method.
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// -- "roe", "steger".
// structhighordergradient:
// -- "conservation", "chain_rule".
int ifvfd = 0;
int isFVMOrFDM = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6;
@ -885,8 +1116,12 @@ int allReduceStep = 1;
// codeOfOversetGrid: Overlapping(overset) grid or not.
// 0 -- NON-overlapping grid.
// 1 -- Overlapping grid.
// oversetInterpolationMethod: the method of overset interpolation while field simulation
// 0 -- set the acceptor cell value by donor cell value.
// 1 -- set the acceptor cell value by distance weight of donor cell value.
int codeOfOversetGrid = 0;
int codeOfOversetSlipGrid = 0;
int oversetInterpolationMethod = 0;
int readOversetFileOrNot = 0;
int symetryOrNot = 0;
int readInAuxiliaryInnerGrid = 1;
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
string auxiliaryInnerGrid2 = "";
string oversetGridFileName = "./grid/overlap.ovs";
string oversetGridFileName = "./grid/iblank.ovs";
double walldistMainZone = 1.0
double toleranceForOversetSearch = 1.0e-3;
double toleranceForOversetBox = 1.0e-3;
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
int numberOfMovingBodies = 2;
// ----------------- ALE configuration ------------------------------
int codeOfAleModel = 1;
int aleStartStrategy = -1;
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
int strategyForGCLSource = 0; //0-present; 1-Ahn;
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
int methodForKineticEquation = 0;
double relaxParameterOfKinetic = 1.0;
#########################################################################
# motive information #
#########################################################################
int numberOfMovingBodies = 1;
############################## body0 ##############################
//mass of parts
double mass_0 = 1.0;
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
//initial six DOF position information of parts. xc yc zc
double massCenter_0[] = 0.0 , 0.0, 0.0;
//initial six DOF position information of parts. angleX angleY angleZ
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
//initial six DOF move information of parts. vc vy vz
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
//initial six DOF move information of parts. omigX omigY omigZ
double angularVelocity_0[] = 0.0, 0.0, 0.0;
//the object that the parts belong to.
int fartherIndex_0 = -1;
//the assembly position of the parts. xc yc zc angleX angleY angleZ
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
//the move pattern of the parts.
// -1 given motion partten.
// 0 still.
// 1 six DOF motion.
// 2 three DOF motion.
// 11 X-axis forced motion.
// 12 Y-axis forced motion.
// 13 Z-axis forced motion.
// 14 forced pitch motion.
// 15 forced yaw motion.
// 16 forced roll motion.
int RBDMethod_0 = 0;
double amplitude_0 = 0.0;
double reduceFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
//additional force (system axis) fX fY fZ
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
//additional moment of Force (system axis) mX mY mZ
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
//the deformation method of the parts.
int morphing_0 = 0;
// post indentify
int integralOrder = 4;
// ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0;
//@double refReNumber = 2.329418E08;
//@double refDimensionalTemperature = 288.144;
//@double refDimensionalPressure = 1.01313E05;
//@double height = -0.001;
//@double refReNumber = 6.5e6;
//@double refDimensionalTemperature = 288.15;
//@double freestream_vibration_temperature = 300.00;
//@double refDimensionalPressure = 0;
//@double height = 0;
//@int nsubsonicInlet = 0;
//@int nsubsonicOutlet = 0;
//@string inLetFileName = "./bin/subsonicInlet.hypara";
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
//@double refDimensionalVelocity = 0;
//@double refDimensionalDensity = 0;
#########################################################################
# Old Parameter #

6
B04_ThreeD_DLR-F6_SA_Unstruct_60CPU/bin/cfd_para_subsonic.hypara
View File

@ -57,9 +57,9 @@ double refDimensionalTemperature = 274.1;
double gridScaleFactor = 0.001;
double forceRefenenceLengthSpanWise = 0.58565; // unit of meter.
double forceRefenenceLength = 0.1412; // unit of meter.
double forceRefenenceArea = 0.0727; // unit of meter^2.
double forceReferenceLengthSpanWise = 0.58565; // unit of meter.
double forceReferenceLength = 0.1412; // unit of meter.
double forceReferenceArea = 0.0727; // unit of meter^2.
double TorqueRefX = 0.1579; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = -0.03392; // unit of meter.

379
B05_ThreeD_x38_Laminar_Unstruct_128CPU/bin/cfd_para.hypara
View File

@ -21,6 +21,7 @@
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
// 2 -- Grid refinement.
// 3 -- Grid merging, merge two blocks into one block.
// 4 -- Grid deformation, achieve unstructured grid deformation.
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
// multiblock: Multi-block grid or not, only for structured grid conversion.
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
//-----------------------------------------------------------------------
// from_gfile: path of original data file for unstructure grid convert from.
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
int numberOfGridFile = 1;
string from_gfile = "./grid/rae2822_hybrid2d.cas";
string from_gfile1= "";
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
// ----------------- some advanced choices ------------------------------
// iunsteady: The Grid is for unsteady simulation or not.
int iunsteady = 0;
int iale = 0;
int codeOfAleModel = 0;
// fileformat: Ustar Grid file format.
@ -122,15 +125,38 @@ int isDeform = 0;
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
int projectOrgPoint = 0; // if project original wall points.
// ----------------- Grid Deform Parameters -----------------------------
// deformationMethod: Grid Deform.
// 1 -- SPRING.
// 2 -- RBF.
// stationalGridFile: Original grid file.
// visualFileName : The visualization file path of deform grid.
// nDeformStep : The max deform step.
// flapAngle : The max flap angle.
// rotatePostionZ : Rotate postion.
// rotatePostionY : Rotate postion.
// gridSlice : If dump slice grid.
// sliceAxis : Grid slice axis.
// slicePosition : Grid slice position.
int nDeformStep = 40;
double flapAngle = 10.0;
double rotatePostionZ = 4.00003;
double rotatePostionY = 3.05;
int deformationMethod = 2;
string stationalGridFile = "./grid/Segment2Brid.fts";
string visualFileName = "./results/deformedGrid.dat"
int gridSlice = 1;
int sliceAxis = 1;
double slicePosition = 13;
// ----------------- RBF Parameters -------------------------------------
// symmetryPlane: Which symmetry plane is used in the mesh.
// 0 -- without symmetry.
// 1 -- plane of x=0.
// 2 -- plane of y=0.
// 3 -- plane of z=0.
int numberOfReferenceCP = 10;
double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// numberOfReferenceCP : Number of reference Control Points.
// influencePara : The RBF influence radius parameter.
int numberOfReferenceCP = 40;
double influencePara = 25.0;
// ----------------- Periodic Parameters --------------------------------
// Notice: Rotational periodicity only support rotation along the X axis!
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
// translationLength[]: The relative distance between two periodic face
which only support one direction.
// rotationAngle: The relative angle between two periodic face.
which is recorded in degrees.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
// 0 -- Interface. (default)
// 1 -- Physical boundary condition, used in Hybrid solver.
// 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.
// parallelPartitionMethod: 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.
// 2 -- Using Metis for homogeneous MPI.
// 3 -- using METIS partition for homogeneous OpenMP.
@ -238,6 +269,8 @@ int compressible = 1;
// 1 -- the flight conditions.
// 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions.
// 4 -- the condition that the velocity, temperature and density are given.
// 5 -- the condition that the velocity, temperature and pressure are given.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -251,10 +284,12 @@ int compressible = 1;
// 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.
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, 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
// condition is radiation equilibrium temperature, and 0.8 is the default value.
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
double refMachNumber = 0.73;
double attackd = 2.79;
@ -263,7 +298,7 @@ double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 6.5e6;
double refDimensionalTemperature = 288.15;
double freestream_vibration_temperature = 10000.00;
double freestream_vibration_temperature = 300.00;
//int inflowParaType = 1;
//double height = 0.001;
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
//double refDimensionalTemperature = 288.144;
//double refDimensionalPressure = 1.01313E05;
//The velocity, temperature and density are fixed.
//int inflowParaType = 4;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalDensity = 1.0e3;
//The velocity, temperature and pressure are fixed.
//int inflowParaType = 5;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalPressure = 1.0e5;
//The MachNumber, temperature and pressure are fixed.
//int inflowParaType = 6;
//double refDimensionalTemperature = 293;
//double refDimensionalPressure = 8886.06;
double wallTemperature = -1.0;
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.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.
double refMolecularWeight = 28.9644; // unit of g/mol.
//-----------------------------------------------------------------------
# Spatial Discretisation #
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
// Using this when solve structered grid or hybrid.
// -- "vanleer", "steger", "hlle", "lax_f".
// -- "roe", "modified_roe".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
// str_limiter_name: Limiter of struct grid.
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
// -- "nolim", no limiter.
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod".
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
// -- "nolim", no limiter.
// uns_vis_name: Discretisation method of viscous term.
// -- "std", "test", "aver", "new1", "new2".
// uns_gradient: Gradient reconstruction method.
// gradientName: Gradient reconstruction method.
// -- "default", "ggcell", "ggnode", "lsq".
// ivencat: Variation of vencat limiter.
// 0 -- org method, it is independent of grid scale.
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
// 1 -- unsteay.
// 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.
// ifStaticsFlowField: Statistical variables for DES simulation.
// ifStaticsFlowField: Statistical variables for unsteady simulation.
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
// startStatisticStep: Outer step when start statistics.
// when the value is larger than "maxSimuStep", it is useless.
// statisticalTimePeriod: Used as time period of statistic analysis.
// when the value is negative, time period is treated as infinite.
// statisticMethod: Statistic reynolds stress method.
0 --tau = <q^2> - <q>^2
1 --tau = <u'u'>
// min_sub_iter: The min sub iteration of unsteady simulation.
// max_sub_iter: The max sub iteration of unsteady simulation.
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
@ -454,7 +511,10 @@ int iunsteady = 0;
double physicalTimeStep = 0.01;
int ifStartFromSteadyResults = 0;
int ifStaticsFlowField = 0;
int ifStaticsReynoldsStress = 0;
int startStatisticStep = 800000;
double statisticalTimePeriod = -1.0;
int statisticMethod = 0;
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
int methodOfDualTime = 3;
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
double csrv = 2.0;
double timemax = 1.0e10;
double dtsave = -1.0;
int codeOfAleModel = 0;
int aleStartStrategy = -1;
int maxale = 10;
double dtau = 0.001;
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
int numberOfGridGroups = 1;
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
string wallTemperaturefile= "";
int walldistMethod = 1;
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt";
string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string samplefile = "results/sample.dat";
int nDumpSurfaceInfo = 0;
string wall_varfile = "";
string jetDefineFile = "bin/jet.hypara";
string overset_gridfile = "results/iblank.ovs";
string sixDofFileName = "results/sixDofInfo.dat";
string derivativeFileName = "results/identify.dat";
string hysteresisFileName = "results/force_beta.plt";
int plotFieldType = 0;
@ -554,6 +614,11 @@ int plotFieldType = 0;
int visualfileType = 1;
// samplefileMode: The dump mode of sample file.
// 0 -- dump out every probe/line/surface data for all step intervals.
// 1 -- dump out all probe/line/surface data for every step intervals.
int samplefileMode = 0;
// visualSlice: The slice of tecflow.
// 0 -- Do not save slice data.
// 1 -- comput and save it to sliceFile.
@ -567,11 +632,13 @@ int visualSlice = 0;
int sliceAxis = 1;
double slicePostion = -0.5;
string sliceFile = "results/Slice.plt";
int dumpWallFaceCenter = 0;
// min-max box of the visual block.
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
double upperPlotFieldBox[] = [1.0 1.0 1.0];
//-----------the optional parameters list for the flow field output----------------
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- 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), iblank(81).
// -- specific heat ratio(gama, 56)
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
// Variables order must from small to big.
//-----------the optional parameters list for the wall boundary condition----------------
// nVisualWallVariables: The number of visual variables on wall.
// visualWallVariables : dumped variable types, listed as following:
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -overlap iblank(iblank, 81)
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
// dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate.
int dumpStandardModel = 0;
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
int turbInterval = 1;
int turbOrderStruct = 2;
int kindOfTurbSource = 0;
int mod_turb_res = 0;
double turb_relax = 1.0;
@ -652,6 +736,10 @@ double muoo = 3.0;
double kwoo = 5.0;
int transitionType = 0;
double turbIntensity = -1.0;
int freeturbIntensitySRModify = 0;
double freeDecayXLocation = 0.0;
int compressibleCorrection = 0;
int transitionMaFix = 1;
# maximum eddy viscosity (myt/my) max.
double eddyViscosityLimit = 1.0e10;
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
# LES Parameter #
//-----------------------------------------------------------------------
// iLES: Create LESSolver or not.
// >= 1 - Create LESSolver;
// < 1 - not.
// == 1 - Create LESSolver;
// != 1 - not.
// amplitudeofDisturb: Amplitude of adding disturb.
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
// iterdisturb: Add random disturb in every sub-iter or only first sub-iter.
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
// utau: friction velocity, using in DNSDisturb.
// sgsmodel: subgrid scale model.
// = "smagorinsky";
// = "dsm";
// = "wale".
// = "dsmCom";
// = "wale";
// = "sigma".
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
// = 2 - pow(deltai * deltaj *deltak, 1/3);
// = 3 - Devloped by Scotti.
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
int deltaFunctionType = 2;
int wallDampingFunctionType = 1;
int turbViscousCutType = 2;
double smagConstant = 0.135;
double smagConstant = 0.1;
double isotropicConstant = 0.0;
double waleConstant = 0.6;
double sigmaConstant = 1.35;
int filterDirection[] = [1, 1, 0];
int averageDirection[] = [0, 0, 0];
double testFilterScale = 2.0;
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
// nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D.
// 5 -- for 3D.
// nGasModel: The type of gas.
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
// Otherwise, the pure gas with one component is used for perfect gas.
// 0 -- Earth gas.
// 1 -- Mars gas.
// 2 -- Argon.
// 3 -- Nitrogen.
// nEnergyRecycle: The type of EnergyModel Recycle.
// 0 -- not used .
// 1 -- used.
// nDensityModify: The type of densitymodify.
// 0 -- not used.
// 1 -- used.
// nchem:
// 0 -- without chemical reaction flow.
// 1 -- the chemical reaction flow is considered.
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
// 0 -- perfect gas.
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
// the value equals to or is greater than 1, and 3 is for default value.
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
// the value equals to or is greater than 1, and 3 is for default value.
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
// the value equals to or is greater than 1, and 3 is for default value.
// nSlipBCModel : The computational model of slip boundary conditions.
// 0 -- no slip.
// 1 -- the conventional Maxwell slip conditions.
// 2 -- the Gokcen slip conditions.
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
// 4 -- the Kogan simplified slip conditions.
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
// nchemsrc:
// 0 -- the source terms are not computed.
// 1 -- the source terms are computed.
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
// 1 -- One-temperature model.
// 2 -- Two-temperature model.
// 3 -- Three-temperature model.
// nTEnergyModel: the method to computing temperature energy model.
// 0 -- the energy term is computed using the conventional method.
// 1 -- the energy term is computed using the curve fitting method.
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
// catalyticCoef:
// 0.0 -- full non-catalytic wall boundary condition.
// 1.0 -- full catalytic wall boundary condition.
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
// nTemperatureJump : the method to calculate the temperature jump.
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
// 1.0 -- proposed by Maxwell.
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
// 1.146 -- proposed for an additional "fictitious" velocity slip.
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
// 0 -- not freeze, the chemical reaction sources will be calculated.
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
// nDebug: cout the Wrong place and abort
// 0 -- not used.
// 1 -- used.
// nSpeciesLimit: limitter of gas species
// 0 -- not used.
// 1 -- used.
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
// 0 -- method 0.
// 1 -- method 1.
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
// 0 -- not used.
// 1 -- used.
// nChemcalSourceModified: Modified on ChemcalSource
// 0 -- not used.
// 1 -- used.
// nAblation:
// 0 -- The wall ablation is not computed.
// 1 -- The wall ablation is computed.
// isInjection:
// 0 -- The injection velocity of ablation wall is not computed.
// 1 -- The injection velocity of ablation wall is computed.
// nViscosityModel:
// 0 -- Blottner fitting method.
// 1 -- Gupta fitting method.
// nSutherland:
// 0 -- stands for selecting the Blotter curve fits mode.
// 1 -- stands for Sutherland relation.
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
// "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.
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
// 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.
@ -758,6 +935,10 @@ int dg_high_order = 0;
int iapplication = 0;
int iCodeBranch = 0;
int nm = 5;
int nEquilibriumGas = 0;
int nPCWCycleStep = 3;
int nRETCycleStep = 3;
int nSLIPCycleStep= 3;
double refGama = 1.4;
double prl = 0.72;
@ -770,23 +951,73 @@ int nchem = 0;
int nchemsrc = 1;
int nchemrad = 1;
int ntmodel = 1;
int nChemicalFlowStep = 0;
int nEnergyRecycle = 0;
int nSlipBCModel = 0;
int nDensityModify = 1;
int nTEnergyModel = 0;
int nMeanFreePathType = 0;
int nIsChemicalFreeze = 0;
int nIsSuperCatalytic = 1;
int nTemperatureJump = 0;
double parkVDPower = 0.6;
double catalyticCoef = 0.0;
double sigmaVelocity = 1.0;
double sigmaTemperature = 1.0;
double sigmaMassFraction = 1.0;
double velocitySlipCorrectConstant = 1.0;
double chemicalRelaxCorf = 1.0;
double chemicalSpectrumRadiusCoef = 1.0;
double viscousSpectrumRadiusCoef = 1.0;
double inviscidSpectrumRadiusCoef = 1.0;
double staticPressureRelaxCorf = 1.0;
double veTemperatureMin = 30.0;
int nDebug = 0;
int nSpeciesLimit = 0;
int nTurblenceForChemical = 0;
int nViscosityFluxSublevelModified = 0 ;
int nChemcalSourceModified = 0;
int nAblation = 0;
int isInjection = 0;
int nViscosityModel = 0;
int nMarsModel = 0;
string gasfile = "DK5";
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
string speciesName = "O, O2, NO, N, N2";
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
//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, 0.233, 0.0, 0.0, 0.0, 0.767, 0.0";
//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, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Mars-Pa8";
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
//string gasfile = "DK7";
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Combustion-12";
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
//string gasfile = "Gas-Mixture";
//string speciesName ="SpeciesA, SpeciesB";
//string initMassFraction = "1.0, 0.0";
int nSutherland = 0;
double gamaSpeciesA = 1.4;
double gamaSpeciesB = 1.3;
double molecularWeightSpeciesA = 29.0;
double molecularWeightSpeciesB = 30.0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0;
#########################################################################
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
#########################################################################
# High Order Struct Solver #
#########################################################################
// ifvfd:
// isFVMOrFDM:
// 0 -- NSSolverStruct using Finite Volume Method.
// 1 -- NSSolverStruct using Finite Differ Method.
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// -- "roe", "steger".
// structhighordergradient:
// -- "conservation", "chain_rule".
int ifvfd = 0;
int isFVMOrFDM = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6;
@ -885,8 +1116,12 @@ int allReduceStep = 1;
// codeOfOversetGrid: Overlapping(overset) grid or not.
// 0 -- NON-overlapping grid.
// 1 -- Overlapping grid.
// oversetInterpolationMethod: the method of overset interpolation while field simulation
// 0 -- set the acceptor cell value by donor cell value.
// 1 -- set the acceptor cell value by distance weight of donor cell value.
int codeOfOversetGrid = 0;
int codeOfOversetSlipGrid = 0;
int oversetInterpolationMethod = 0;
int readOversetFileOrNot = 0;
int symetryOrNot = 0;
int readInAuxiliaryInnerGrid = 1;
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
string auxiliaryInnerGrid2 = "";
string oversetGridFileName = "./grid/overlap.ovs";
string oversetGridFileName = "./grid/iblank.ovs";
double walldistMainZone = 1.0
double toleranceForOversetSearch = 1.0e-3;
double toleranceForOversetBox = 1.0e-3;
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
int numberOfMovingBodies = 2;
// ----------------- ALE configuration ------------------------------
int codeOfAleModel = 1;
int aleStartStrategy = -1;
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
int strategyForGCLSource = 0; //0-present; 1-Ahn;
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
int methodForKineticEquation = 0;
double relaxParameterOfKinetic = 1.0;
#########################################################################
# motive information #
#########################################################################
int numberOfMovingBodies = 1;
############################## body0 ##############################
//mass of parts
double mass_0 = 1.0;
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
//initial six DOF position information of parts. xc yc zc
double massCenter_0[] = 0.0 , 0.0, 0.0;
//initial six DOF position information of parts. angleX angleY angleZ
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
//initial six DOF move information of parts. vc vy vz
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
//initial six DOF move information of parts. omigX omigY omigZ
double angularVelocity_0[] = 0.0, 0.0, 0.0;
//the object that the parts belong to.
int fartherIndex_0 = -1;
//the assembly position of the parts. xc yc zc angleX angleY angleZ
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
//the move pattern of the parts.
// -1 given motion partten.
// 0 still.
// 1 six DOF motion.
// 2 three DOF motion.
// 11 X-axis forced motion.
// 12 Y-axis forced motion.
// 13 Z-axis forced motion.
// 14 forced pitch motion.
// 15 forced yaw motion.
// 16 forced roll motion.
int RBDMethod_0 = 0;
double amplitude_0 = 0.0;
double reduceFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
//additional force (system axis) fX fY fZ
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
//additional moment of Force (system axis) mX mY mZ
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
//the deformation method of the parts.
int morphing_0 = 0;
// post indentify
int integralOrder = 4;
// ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0;
//@double refReNumber = 2.329418E08;
//@double refDimensionalTemperature = 288.144;
//@double refDimensionalPressure = 1.01313E05;
//@double height = -0.001;
//@double refReNumber = 6.5e6;
//@double refDimensionalTemperature = 288.15;
//@double freestream_vibration_temperature = 300.00;
//@double refDimensionalPressure = 0;
//@double height = 0;
//@int nsubsonicInlet = 0;
//@int nsubsonicOutlet = 0;
//@string inLetFileName = "./bin/subsonicInlet.hypara";
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
//@double refDimensionalVelocity = 0;
//@double refDimensionalDensity = 0;
#########################################################################
# Old Parameter #

6
B05_ThreeD_x38_Laminar_Unstruct_128CPU/bin/cfd_para_hypersonic.hypara
View File

@ -61,9 +61,9 @@ double freestream_vibration_temperature = 10000.0;
double gridScaleFactor = 0.001;
double forceRefenenceLengthSpanWise = 0.0847; // unit of meter.
double forceRefenenceLength = 0.2805; // unit of meter.
double forceRefenenceArea = 0.0121; // unit of meter^2.
double forceReferenceLengthSpanWise = 0.0847; // unit of meter.
double forceReferenceLength = 0.2805; // unit of meter.
double forceReferenceArea = 0.0121; // unit of meter^2.
double TorqueRefX = 0.16; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.

379
B06_ThreeD_Axisymmetric_SA_Unstruct_64CPU/bin/cfd_para.hypara
View File

@ -21,6 +21,7 @@
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
// 2 -- Grid refinement.
// 3 -- Grid merging, merge two blocks into one block.
// 4 -- Grid deformation, achieve unstructured grid deformation.
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
// multiblock: Multi-block grid or not, only for structured grid conversion.
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
//-----------------------------------------------------------------------
// from_gfile: path of original data file for unstructure grid convert from.
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
int numberOfGridFile = 1;
string from_gfile = "./grid/rae2822_hybrid2d.cas";
string from_gfile1= "";
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
// ----------------- some advanced choices ------------------------------
// iunsteady: The Grid is for unsteady simulation or not.
int iunsteady = 0;
int iale = 0;
int codeOfAleModel = 0;
// fileformat: Ustar Grid file format.
@ -122,15 +125,38 @@ int isDeform = 0;
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
int projectOrgPoint = 0; // if project original wall points.
// ----------------- Grid Deform Parameters -----------------------------
// deformationMethod: Grid Deform.
// 1 -- SPRING.
// 2 -- RBF.
// stationalGridFile: Original grid file.
// visualFileName : The visualization file path of deform grid.
// nDeformStep : The max deform step.
// flapAngle : The max flap angle.
// rotatePostionZ : Rotate postion.
// rotatePostionY : Rotate postion.
// gridSlice : If dump slice grid.
// sliceAxis : Grid slice axis.
// slicePosition : Grid slice position.
int nDeformStep = 40;
double flapAngle = 10.0;
double rotatePostionZ = 4.00003;
double rotatePostionY = 3.05;
int deformationMethod = 2;
string stationalGridFile = "./grid/Segment2Brid.fts";
string visualFileName = "./results/deformedGrid.dat"
int gridSlice = 1;
int sliceAxis = 1;
double slicePosition = 13;
// ----------------- RBF Parameters -------------------------------------
// symmetryPlane: Which symmetry plane is used in the mesh.
// 0 -- without symmetry.
// 1 -- plane of x=0.
// 2 -- plane of y=0.
// 3 -- plane of z=0.
int numberOfReferenceCP = 10;
double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// numberOfReferenceCP : Number of reference Control Points.
// influencePara : The RBF influence radius parameter.
int numberOfReferenceCP = 40;
double influencePara = 25.0;
// ----------------- Periodic Parameters --------------------------------
// Notice: Rotational periodicity only support rotation along the X axis!
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
// translationLength[]: The relative distance between two periodic face
which only support one direction.
// rotationAngle: The relative angle between two periodic face.
which is recorded in degrees.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
// 0 -- Interface. (default)
// 1 -- Physical boundary condition, used in Hybrid solver.
// 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.
// parallelPartitionMethod: 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.
// 2 -- Using Metis for homogeneous MPI.
// 3 -- using METIS partition for homogeneous OpenMP.
@ -238,6 +269,8 @@ int compressible = 1;
// 1 -- the flight conditions.
// 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions.
// 4 -- the condition that the velocity, temperature and density are given.
// 5 -- the condition that the velocity, temperature and pressure are given.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -251,10 +284,12 @@ int compressible = 1;
// 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.
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, 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
// condition is radiation equilibrium temperature, and 0.8 is the default value.
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
double refMachNumber = 0.73;
double attackd = 2.79;
@ -263,7 +298,7 @@ double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 6.5e6;
double refDimensionalTemperature = 288.15;
double freestream_vibration_temperature = 10000.00;
double freestream_vibration_temperature = 300.00;
//int inflowParaType = 1;
//double height = 0.001;
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
//double refDimensionalTemperature = 288.144;
//double refDimensionalPressure = 1.01313E05;
//The velocity, temperature and density are fixed.
//int inflowParaType = 4;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalDensity = 1.0e3;
//The velocity, temperature and pressure are fixed.
//int inflowParaType = 5;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalPressure = 1.0e5;
//The MachNumber, temperature and pressure are fixed.
//int inflowParaType = 6;
//double refDimensionalTemperature = 293;
//double refDimensionalPressure = 8886.06;
double wallTemperature = -1.0;
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.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.
double refMolecularWeight = 28.9644; // unit of g/mol.
//-----------------------------------------------------------------------
# Spatial Discretisation #
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
// Using this when solve structered grid or hybrid.
// -- "vanleer", "steger", "hlle", "lax_f".
// -- "roe", "modified_roe".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
// str_limiter_name: Limiter of struct grid.
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
// -- "nolim", no limiter.
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod".
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
// -- "nolim", no limiter.
// uns_vis_name: Discretisation method of viscous term.
// -- "std", "test", "aver", "new1", "new2".
// uns_gradient: Gradient reconstruction method.
// gradientName: Gradient reconstruction method.
// -- "default", "ggcell", "ggnode", "lsq".
// ivencat: Variation of vencat limiter.
// 0 -- org method, it is independent of grid scale.
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
// 1 -- unsteay.
// 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.
// ifStaticsFlowField: Statistical variables for DES simulation.
// ifStaticsFlowField: Statistical variables for unsteady simulation.
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
// startStatisticStep: Outer step when start statistics.
// when the value is larger than "maxSimuStep", it is useless.
// statisticalTimePeriod: Used as time period of statistic analysis.
// when the value is negative, time period is treated as infinite.
// statisticMethod: Statistic reynolds stress method.
0 --tau = <q^2> - <q>^2
1 --tau = <u'u'>
// min_sub_iter: The min sub iteration of unsteady simulation.
// max_sub_iter: The max sub iteration of unsteady simulation.
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
@ -454,7 +511,10 @@ int iunsteady = 0;
double physicalTimeStep = 0.01;
int ifStartFromSteadyResults = 0;
int ifStaticsFlowField = 0;
int ifStaticsReynoldsStress = 0;
int startStatisticStep = 800000;
double statisticalTimePeriod = -1.0;
int statisticMethod = 0;
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
int methodOfDualTime = 3;
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
double csrv = 2.0;
double timemax = 1.0e10;
double dtsave = -1.0;
int codeOfAleModel = 0;
int aleStartStrategy = -1;
int maxale = 10;
double dtau = 0.001;
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
int numberOfGridGroups = 1;
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
string wallTemperaturefile= "";
int walldistMethod = 1;
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt";
string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string samplefile = "results/sample.dat";
int nDumpSurfaceInfo = 0;
string wall_varfile = "";
string jetDefineFile = "bin/jet.hypara";
string overset_gridfile = "results/iblank.ovs";
string sixDofFileName = "results/sixDofInfo.dat";
string derivativeFileName = "results/identify.dat";
string hysteresisFileName = "results/force_beta.plt";
int plotFieldType = 0;
@ -554,6 +614,11 @@ int plotFieldType = 0;
int visualfileType = 1;
// samplefileMode: The dump mode of sample file.
// 0 -- dump out every probe/line/surface data for all step intervals.
// 1 -- dump out all probe/line/surface data for every step intervals.
int samplefileMode = 0;
// visualSlice: The slice of tecflow.
// 0 -- Do not save slice data.
// 1 -- comput and save it to sliceFile.
@ -567,11 +632,13 @@ int visualSlice = 0;
int sliceAxis = 1;
double slicePostion = -0.5;
string sliceFile = "results/Slice.plt";
int dumpWallFaceCenter = 0;
// min-max box of the visual block.
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
double upperPlotFieldBox[] = [1.0 1.0 1.0];
//-----------the optional parameters list for the flow field output----------------
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- 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), iblank(81).
// -- specific heat ratio(gama, 56)
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
// Variables order must from small to big.
//-----------the optional parameters list for the wall boundary condition----------------
// nVisualWallVariables: The number of visual variables on wall.
// visualWallVariables : dumped variable types, listed as following:
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -overlap iblank(iblank, 81)
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
// dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate.
int dumpStandardModel = 0;
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
int turbInterval = 1;
int turbOrderStruct = 2;
int kindOfTurbSource = 0;
int mod_turb_res = 0;
double turb_relax = 1.0;
@ -652,6 +736,10 @@ double muoo = 3.0;
double kwoo = 5.0;
int transitionType = 0;
double turbIntensity = -1.0;
int freeturbIntensitySRModify = 0;
double freeDecayXLocation = 0.0;
int compressibleCorrection = 0;
int transitionMaFix = 1;
# maximum eddy viscosity (myt/my) max.
double eddyViscosityLimit = 1.0e10;
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
# LES Parameter #
//-----------------------------------------------------------------------
// iLES: Create LESSolver or not.
// >= 1 - Create LESSolver;
// < 1 - not.
// == 1 - Create LESSolver;
// != 1 - not.
// amplitudeofDisturb: Amplitude of adding disturb.
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
// iterdisturb: Add random disturb in every sub-iter or only first sub-iter.
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
// utau: friction velocity, using in DNSDisturb.
// sgsmodel: subgrid scale model.
// = "smagorinsky";
// = "dsm";
// = "wale".
// = "dsmCom";
// = "wale";
// = "sigma".
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
// = 2 - pow(deltai * deltaj *deltak, 1/3);
// = 3 - Devloped by Scotti.
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
int deltaFunctionType = 2;
int wallDampingFunctionType = 1;
int turbViscousCutType = 2;
double smagConstant = 0.135;
double smagConstant = 0.1;
double isotropicConstant = 0.0;
double waleConstant = 0.6;
double sigmaConstant = 1.35;
int filterDirection[] = [1, 1, 0];
int averageDirection[] = [0, 0, 0];
double testFilterScale = 2.0;
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
// nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D.
// 5 -- for 3D.
// nGasModel: The type of gas.
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
// Otherwise, the pure gas with one component is used for perfect gas.
// 0 -- Earth gas.
// 1 -- Mars gas.
// 2 -- Argon.
// 3 -- Nitrogen.
// nEnergyRecycle: The type of EnergyModel Recycle.
// 0 -- not used .
// 1 -- used.
// nDensityModify: The type of densitymodify.
// 0 -- not used.
// 1 -- used.
// nchem:
// 0 -- without chemical reaction flow.
// 1 -- the chemical reaction flow is considered.
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
// 0 -- perfect gas.
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
// the value equals to or is greater than 1, and 3 is for default value.
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
// the value equals to or is greater than 1, and 3 is for default value.
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
// the value equals to or is greater than 1, and 3 is for default value.
// nSlipBCModel : The computational model of slip boundary conditions.
// 0 -- no slip.
// 1 -- the conventional Maxwell slip conditions.
// 2 -- the Gokcen slip conditions.
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
// 4 -- the Kogan simplified slip conditions.
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
// nchemsrc:
// 0 -- the source terms are not computed.
// 1 -- the source terms are computed.
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
// 1 -- One-temperature model.
// 2 -- Two-temperature model.
// 3 -- Three-temperature model.
// nTEnergyModel: the method to computing temperature energy model.
// 0 -- the energy term is computed using the conventional method.
// 1 -- the energy term is computed using the curve fitting method.
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
// catalyticCoef:
// 0.0 -- full non-catalytic wall boundary condition.
// 1.0 -- full catalytic wall boundary condition.
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
// nTemperatureJump : the method to calculate the temperature jump.
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
// 1.0 -- proposed by Maxwell.
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
// 1.146 -- proposed for an additional "fictitious" velocity slip.
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
// 0 -- not freeze, the chemical reaction sources will be calculated.
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
// nDebug: cout the Wrong place and abort
// 0 -- not used.
// 1 -- used.
// nSpeciesLimit: limitter of gas species
// 0 -- not used.
// 1 -- used.
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
// 0 -- method 0.
// 1 -- method 1.
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
// 0 -- not used.
// 1 -- used.
// nChemcalSourceModified: Modified on ChemcalSource
// 0 -- not used.
// 1 -- used.
// nAblation:
// 0 -- The wall ablation is not computed.
// 1 -- The wall ablation is computed.
// isInjection:
// 0 -- The injection velocity of ablation wall is not computed.
// 1 -- The injection velocity of ablation wall is computed.
// nViscosityModel:
// 0 -- Blottner fitting method.
// 1 -- Gupta fitting method.
// nSutherland:
// 0 -- stands for selecting the Blotter curve fits mode.
// 1 -- stands for Sutherland relation.
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
// "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.
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
// 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.
@ -758,6 +935,10 @@ int dg_high_order = 0;
int iapplication = 0;
int iCodeBranch = 0;
int nm = 5;
int nEquilibriumGas = 0;
int nPCWCycleStep = 3;
int nRETCycleStep = 3;
int nSLIPCycleStep= 3;
double refGama = 1.4;
double prl = 0.72;
@ -770,23 +951,73 @@ int nchem = 0;
int nchemsrc = 1;
int nchemrad = 1;
int ntmodel = 1;
int nChemicalFlowStep = 0;
int nEnergyRecycle = 0;
int nSlipBCModel = 0;
int nDensityModify = 1;
int nTEnergyModel = 0;
int nMeanFreePathType = 0;
int nIsChemicalFreeze = 0;
int nIsSuperCatalytic = 1;
int nTemperatureJump = 0;
double parkVDPower = 0.6;
double catalyticCoef = 0.0;
double sigmaVelocity = 1.0;
double sigmaTemperature = 1.0;
double sigmaMassFraction = 1.0;
double velocitySlipCorrectConstant = 1.0;
double chemicalRelaxCorf = 1.0;
double chemicalSpectrumRadiusCoef = 1.0;
double viscousSpectrumRadiusCoef = 1.0;
double inviscidSpectrumRadiusCoef = 1.0;
double staticPressureRelaxCorf = 1.0;
double veTemperatureMin = 30.0;
int nDebug = 0;
int nSpeciesLimit = 0;
int nTurblenceForChemical = 0;
int nViscosityFluxSublevelModified = 0 ;
int nChemcalSourceModified = 0;
int nAblation = 0;
int isInjection = 0;
int nViscosityModel = 0;
int nMarsModel = 0;
string gasfile = "DK5";
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
string speciesName = "O, O2, NO, N, N2";
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
//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, 0.233, 0.0, 0.0, 0.0, 0.767, 0.0";
//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, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Mars-Pa8";
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
//string gasfile = "DK7";
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Combustion-12";
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
//string gasfile = "Gas-Mixture";
//string speciesName ="SpeciesA, SpeciesB";
//string initMassFraction = "1.0, 0.0";
int nSutherland = 0;
double gamaSpeciesA = 1.4;
double gamaSpeciesB = 1.3;
double molecularWeightSpeciesA = 29.0;
double molecularWeightSpeciesB = 30.0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0;
#########################################################################
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
#########################################################################
# High Order Struct Solver #
#########################################################################
// ifvfd:
// isFVMOrFDM:
// 0 -- NSSolverStruct using Finite Volume Method.
// 1 -- NSSolverStruct using Finite Differ Method.
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// -- "roe", "steger".
// structhighordergradient:
// -- "conservation", "chain_rule".
int ifvfd = 0;
int isFVMOrFDM = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6;
@ -885,8 +1116,12 @@ int allReduceStep = 1;
// codeOfOversetGrid: Overlapping(overset) grid or not.
// 0 -- NON-overlapping grid.
// 1 -- Overlapping grid.
// oversetInterpolationMethod: the method of overset interpolation while field simulation
// 0 -- set the acceptor cell value by donor cell value.
// 1 -- set the acceptor cell value by distance weight of donor cell value.
int codeOfOversetGrid = 0;
int codeOfOversetSlipGrid = 0;
int oversetInterpolationMethod = 0;
int readOversetFileOrNot = 0;
int symetryOrNot = 0;
int readInAuxiliaryInnerGrid = 1;
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
string auxiliaryInnerGrid2 = "";
string oversetGridFileName = "./grid/overlap.ovs";
string oversetGridFileName = "./grid/iblank.ovs";
double walldistMainZone = 1.0
double toleranceForOversetSearch = 1.0e-3;
double toleranceForOversetBox = 1.0e-3;
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
int numberOfMovingBodies = 2;
// ----------------- ALE configuration ------------------------------
int codeOfAleModel = 1;
int aleStartStrategy = -1;
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
int strategyForGCLSource = 0; //0-present; 1-Ahn;
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
int methodForKineticEquation = 0;
double relaxParameterOfKinetic = 1.0;
#########################################################################
# motive information #
#########################################################################
int numberOfMovingBodies = 1;
############################## body0 ##############################
//mass of parts
double mass_0 = 1.0;
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
//initial six DOF position information of parts. xc yc zc
double massCenter_0[] = 0.0 , 0.0, 0.0;
//initial six DOF position information of parts. angleX angleY angleZ
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
//initial six DOF move information of parts. vc vy vz
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
//initial six DOF move information of parts. omigX omigY omigZ
double angularVelocity_0[] = 0.0, 0.0, 0.0;
//the object that the parts belong to.
int fartherIndex_0 = -1;
//the assembly position of the parts. xc yc zc angleX angleY angleZ
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
//the move pattern of the parts.
// -1 given motion partten.
// 0 still.
// 1 six DOF motion.
// 2 three DOF motion.
// 11 X-axis forced motion.
// 12 Y-axis forced motion.
// 13 Z-axis forced motion.
// 14 forced pitch motion.
// 15 forced yaw motion.
// 16 forced roll motion.
int RBDMethod_0 = 0;
double amplitude_0 = 0.0;
double reduceFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
//additional force (system axis) fX fY fZ
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
//additional moment of Force (system axis) mX mY mZ
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
//the deformation method of the parts.
int morphing_0 = 0;
// post indentify
int integralOrder = 4;
// ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0;
//@double refReNumber = 2.329418E08;
//@double refDimensionalTemperature = 288.144;
//@double refDimensionalPressure = 1.01313E05;
//@double height = -0.001;
//@double refReNumber = 6.5e6;
//@double refDimensionalTemperature = 288.15;
//@double freestream_vibration_temperature = 300.00;
//@double refDimensionalPressure = 0;
//@double height = 0;
//@int nsubsonicInlet = 0;
//@int nsubsonicOutlet = 0;
//@string inLetFileName = "./bin/subsonicInlet.hypara";
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
//@double refDimensionalVelocity = 0;
//@double refDimensionalDensity = 0;
#########################################################################
# Old Parameter #

6
B06_ThreeD_Axisymmetric_SA_Unstruct_64CPU/bin/cfd_para_transonic.hypara
View File

@ -56,9 +56,9 @@ double refDimensionalTemperature = 300;
double gridScaleFactor = 0.01;
double forceRefenenceLengthSpanWise = 0.0381; // unit of meter.
double forceRefenenceLength = 0.0381; // unit of meter.
double forceRefenenceArea = 0.00456; // unit of meter^2.
double forceReferenceLengthSpanWise = 0.0381; // unit of meter.
double forceReferenceLength = 0.0381; // unit of meter.
double forceReferenceArea = 0.00456; // unit of meter^2.
double TorqueRefX = 0.29845; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.

379
B07_ThreeD_Sphere_Laminar_Unstruct_4CPU/bin/cfd_para.hypara
View File

@ -21,6 +21,7 @@
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
// 2 -- Grid refinement.
// 3 -- Grid merging, merge two blocks into one block.
// 4 -- Grid deformation, achieve unstructured grid deformation.
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
// multiblock: Multi-block grid or not, only for structured grid conversion.
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
//-----------------------------------------------------------------------
// from_gfile: path of original data file for unstructure grid convert from.
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
int numberOfGridFile = 1;
string from_gfile = "./grid/rae2822_hybrid2d.cas";
string from_gfile1= "";
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
// ----------------- some advanced choices ------------------------------
// iunsteady: The Grid is for unsteady simulation or not.
int iunsteady = 0;
int iale = 0;
int codeOfAleModel = 0;
// fileformat: Ustar Grid file format.
@ -122,15 +125,38 @@ int isDeform = 0;
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
int projectOrgPoint = 0; // if project original wall points.
// ----------------- Grid Deform Parameters -----------------------------
// deformationMethod: Grid Deform.
// 1 -- SPRING.
// 2 -- RBF.
// stationalGridFile: Original grid file.
// visualFileName : The visualization file path of deform grid.
// nDeformStep : The max deform step.
// flapAngle : The max flap angle.
// rotatePostionZ : Rotate postion.
// rotatePostionY : Rotate postion.
// gridSlice : If dump slice grid.
// sliceAxis : Grid slice axis.
// slicePosition : Grid slice position.
int nDeformStep = 40;
double flapAngle = 10.0;
double rotatePostionZ = 4.00003;
double rotatePostionY = 3.05;
int deformationMethod = 2;
string stationalGridFile = "./grid/Segment2Brid.fts";
string visualFileName = "./results/deformedGrid.dat"
int gridSlice = 1;
int sliceAxis = 1;
double slicePosition = 13;
// ----------------- RBF Parameters -------------------------------------
// symmetryPlane: Which symmetry plane is used in the mesh.
// 0 -- without symmetry.
// 1 -- plane of x=0.
// 2 -- plane of y=0.
// 3 -- plane of z=0.
int numberOfReferenceCP = 10;
double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// numberOfReferenceCP : Number of reference Control Points.
// influencePara : The RBF influence radius parameter.
int numberOfReferenceCP = 40;
double influencePara = 25.0;
// ----------------- Periodic Parameters --------------------------------
// Notice: Rotational periodicity only support rotation along the X axis!
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
// translationLength[]: The relative distance between two periodic face
which only support one direction.
// rotationAngle: The relative angle between two periodic face.
which is recorded in degrees.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
// 0 -- Interface. (default)
// 1 -- Physical boundary condition, used in Hybrid solver.
// 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.
// parallelPartitionMethod: 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.
// 2 -- Using Metis for homogeneous MPI.
// 3 -- using METIS partition for homogeneous OpenMP.
@ -238,6 +269,8 @@ int compressible = 1;
// 1 -- the flight conditions.
// 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions.
// 4 -- the condition that the velocity, temperature and density are given.
// 5 -- the condition that the velocity, temperature and pressure are given.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -251,10 +284,12 @@ int compressible = 1;
// 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.
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, 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
// condition is radiation equilibrium temperature, and 0.8 is the default value.
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
double refMachNumber = 0.73;
double attackd = 2.79;
@ -263,7 +298,7 @@ double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 6.5e6;
double refDimensionalTemperature = 288.15;
double freestream_vibration_temperature = 10000.00;
double freestream_vibration_temperature = 300.00;
//int inflowParaType = 1;
//double height = 0.001;
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
//double refDimensionalTemperature = 288.144;
//double refDimensionalPressure = 1.01313E05;
//The velocity, temperature and density are fixed.
//int inflowParaType = 4;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalDensity = 1.0e3;
//The velocity, temperature and pressure are fixed.
//int inflowParaType = 5;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalPressure = 1.0e5;
//The MachNumber, temperature and pressure are fixed.
//int inflowParaType = 6;
//double refDimensionalTemperature = 293;
//double refDimensionalPressure = 8886.06;
double wallTemperature = -1.0;
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.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.
double refMolecularWeight = 28.9644; // unit of g/mol.
//-----------------------------------------------------------------------
# Spatial Discretisation #
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
// Using this when solve structered grid or hybrid.
// -- "vanleer", "steger", "hlle", "lax_f".
// -- "roe", "modified_roe".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
// str_limiter_name: Limiter of struct grid.
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
// -- "nolim", no limiter.
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod".
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
// -- "nolim", no limiter.
// uns_vis_name: Discretisation method of viscous term.
// -- "std", "test", "aver", "new1", "new2".
// uns_gradient: Gradient reconstruction method.
// gradientName: Gradient reconstruction method.
// -- "default", "ggcell", "ggnode", "lsq".
// ivencat: Variation of vencat limiter.
// 0 -- org method, it is independent of grid scale.
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
// 1 -- unsteay.
// 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.
// ifStaticsFlowField: Statistical variables for DES simulation.
// ifStaticsFlowField: Statistical variables for unsteady simulation.
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
// startStatisticStep: Outer step when start statistics.
// when the value is larger than "maxSimuStep", it is useless.
// statisticalTimePeriod: Used as time period of statistic analysis.
// when the value is negative, time period is treated as infinite.
// statisticMethod: Statistic reynolds stress method.
0 --tau = <q^2> - <q>^2
1 --tau = <u'u'>
// min_sub_iter: The min sub iteration of unsteady simulation.
// max_sub_iter: The max sub iteration of unsteady simulation.
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
@ -454,7 +511,10 @@ int iunsteady = 0;
double physicalTimeStep = 0.01;
int ifStartFromSteadyResults = 0;
int ifStaticsFlowField = 0;
int ifStaticsReynoldsStress = 0;
int startStatisticStep = 800000;
double statisticalTimePeriod = -1.0;
int statisticMethod = 0;
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
int methodOfDualTime = 3;
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
double csrv = 2.0;
double timemax = 1.0e10;
double dtsave = -1.0;
int codeOfAleModel = 0;
int aleStartStrategy = -1;
int maxale = 10;
double dtau = 0.001;
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
int numberOfGridGroups = 1;
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
string wallTemperaturefile= "";
int walldistMethod = 1;
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt";
string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string samplefile = "results/sample.dat";
int nDumpSurfaceInfo = 0;
string wall_varfile = "";
string jetDefineFile = "bin/jet.hypara";
string overset_gridfile = "results/iblank.ovs";
string sixDofFileName = "results/sixDofInfo.dat";
string derivativeFileName = "results/identify.dat";
string hysteresisFileName = "results/force_beta.plt";
int plotFieldType = 0;
@ -554,6 +614,11 @@ int plotFieldType = 0;
int visualfileType = 1;
// samplefileMode: The dump mode of sample file.
// 0 -- dump out every probe/line/surface data for all step intervals.
// 1 -- dump out all probe/line/surface data for every step intervals.
int samplefileMode = 0;
// visualSlice: The slice of tecflow.
// 0 -- Do not save slice data.
// 1 -- comput and save it to sliceFile.
@ -567,11 +632,13 @@ int visualSlice = 0;
int sliceAxis = 1;
double slicePostion = -0.5;
string sliceFile = "results/Slice.plt";
int dumpWallFaceCenter = 0;
// min-max box of the visual block.
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
double upperPlotFieldBox[] = [1.0 1.0 1.0];
//-----------the optional parameters list for the flow field output----------------
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- 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), iblank(81).
// -- specific heat ratio(gama, 56)
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
// Variables order must from small to big.
//-----------the optional parameters list for the wall boundary condition----------------
// nVisualWallVariables: The number of visual variables on wall.
// visualWallVariables : dumped variable types, listed as following:
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -overlap iblank(iblank, 81)
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
// dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate.
int dumpStandardModel = 0;
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
int turbInterval = 1;
int turbOrderStruct = 2;
int kindOfTurbSource = 0;
int mod_turb_res = 0;
double turb_relax = 1.0;
@ -652,6 +736,10 @@ double muoo = 3.0;
double kwoo = 5.0;
int transitionType = 0;
double turbIntensity = -1.0;
int freeturbIntensitySRModify = 0;
double freeDecayXLocation = 0.0;
int compressibleCorrection = 0;
int transitionMaFix = 1;
# maximum eddy viscosity (myt/my) max.
double eddyViscosityLimit = 1.0e10;
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
# LES Parameter #
//-----------------------------------------------------------------------
// iLES: Create LESSolver or not.
// >= 1 - Create LESSolver;
// < 1 - not.
// == 1 - Create LESSolver;
// != 1 - not.
// amplitudeofDisturb: Amplitude of adding disturb.
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
// iterdisturb: Add random disturb in every sub-iter or only first sub-iter.
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
// utau: friction velocity, using in DNSDisturb.
// sgsmodel: subgrid scale model.
// = "smagorinsky";
// = "dsm";
// = "wale".
// = "dsmCom";
// = "wale";
// = "sigma".
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
// = 2 - pow(deltai * deltaj *deltak, 1/3);
// = 3 - Devloped by Scotti.
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
int deltaFunctionType = 2;
int wallDampingFunctionType = 1;
int turbViscousCutType = 2;
double smagConstant = 0.135;
double smagConstant = 0.1;
double isotropicConstant = 0.0;
double waleConstant = 0.6;
double sigmaConstant = 1.35;
int filterDirection[] = [1, 1, 0];
int averageDirection[] = [0, 0, 0];
double testFilterScale = 2.0;
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
// nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D.
// 5 -- for 3D.
// nGasModel: The type of gas.
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
// Otherwise, the pure gas with one component is used for perfect gas.
// 0 -- Earth gas.
// 1 -- Mars gas.
// 2 -- Argon.
// 3 -- Nitrogen.
// nEnergyRecycle: The type of EnergyModel Recycle.
// 0 -- not used .
// 1 -- used.
// nDensityModify: The type of densitymodify.
// 0 -- not used.
// 1 -- used.
// nchem:
// 0 -- without chemical reaction flow.
// 1 -- the chemical reaction flow is considered.
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
// 0 -- perfect gas.
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
// the value equals to or is greater than 1, and 3 is for default value.
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
// the value equals to or is greater than 1, and 3 is for default value.
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
// the value equals to or is greater than 1, and 3 is for default value.
// nSlipBCModel : The computational model of slip boundary conditions.
// 0 -- no slip.
// 1 -- the conventional Maxwell slip conditions.
// 2 -- the Gokcen slip conditions.
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
// 4 -- the Kogan simplified slip conditions.
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
// nchemsrc:
// 0 -- the source terms are not computed.
// 1 -- the source terms are computed.
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
// 1 -- One-temperature model.
// 2 -- Two-temperature model.
// 3 -- Three-temperature model.
// nTEnergyModel: the method to computing temperature energy model.
// 0 -- the energy term is computed using the conventional method.
// 1 -- the energy term is computed using the curve fitting method.
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
// catalyticCoef:
// 0.0 -- full non-catalytic wall boundary condition.
// 1.0 -- full catalytic wall boundary condition.
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
// nTemperatureJump : the method to calculate the temperature jump.
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
// 1.0 -- proposed by Maxwell.
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
// 1.146 -- proposed for an additional "fictitious" velocity slip.
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
// 0 -- not freeze, the chemical reaction sources will be calculated.
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
// nDebug: cout the Wrong place and abort
// 0 -- not used.
// 1 -- used.
// nSpeciesLimit: limitter of gas species
// 0 -- not used.
// 1 -- used.
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
// 0 -- method 0.
// 1 -- method 1.
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
// 0 -- not used.
// 1 -- used.
// nChemcalSourceModified: Modified on ChemcalSource
// 0 -- not used.
// 1 -- used.
// nAblation:
// 0 -- The wall ablation is not computed.
// 1 -- The wall ablation is computed.
// isInjection:
// 0 -- The injection velocity of ablation wall is not computed.
// 1 -- The injection velocity of ablation wall is computed.
// nViscosityModel:
// 0 -- Blottner fitting method.
// 1 -- Gupta fitting method.
// nSutherland:
// 0 -- stands for selecting the Blotter curve fits mode.
// 1 -- stands for Sutherland relation.
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
// "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.
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
// 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.
@ -758,6 +935,10 @@ int dg_high_order = 0;
int iapplication = 0;
int iCodeBranch = 0;
int nm = 5;
int nEquilibriumGas = 0;
int nPCWCycleStep = 3;
int nRETCycleStep = 3;
int nSLIPCycleStep= 3;
double refGama = 1.4;
double prl = 0.72;
@ -770,23 +951,73 @@ int nchem = 0;
int nchemsrc = 1;
int nchemrad = 1;
int ntmodel = 1;
int nChemicalFlowStep = 0;
int nEnergyRecycle = 0;
int nSlipBCModel = 0;
int nDensityModify = 1;
int nTEnergyModel = 0;
int nMeanFreePathType = 0;
int nIsChemicalFreeze = 0;
int nIsSuperCatalytic = 1;
int nTemperatureJump = 0;
double parkVDPower = 0.6;
double catalyticCoef = 0.0;
double sigmaVelocity = 1.0;
double sigmaTemperature = 1.0;
double sigmaMassFraction = 1.0;
double velocitySlipCorrectConstant = 1.0;
double chemicalRelaxCorf = 1.0;
double chemicalSpectrumRadiusCoef = 1.0;
double viscousSpectrumRadiusCoef = 1.0;
double inviscidSpectrumRadiusCoef = 1.0;
double staticPressureRelaxCorf = 1.0;
double veTemperatureMin = 30.0;
int nDebug = 0;
int nSpeciesLimit = 0;
int nTurblenceForChemical = 0;
int nViscosityFluxSublevelModified = 0 ;
int nChemcalSourceModified = 0;
int nAblation = 0;
int isInjection = 0;
int nViscosityModel = 0;
int nMarsModel = 0;
string gasfile = "DK5";
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
string speciesName = "O, O2, NO, N, N2";
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
//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, 0.233, 0.0, 0.0, 0.0, 0.767, 0.0";
//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, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Mars-Pa8";
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
//string gasfile = "DK7";
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Combustion-12";
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
//string gasfile = "Gas-Mixture";
//string speciesName ="SpeciesA, SpeciesB";
//string initMassFraction = "1.0, 0.0";
int nSutherland = 0;
double gamaSpeciesA = 1.4;
double gamaSpeciesB = 1.3;
double molecularWeightSpeciesA = 29.0;
double molecularWeightSpeciesB = 30.0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0;
#########################################################################
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
#########################################################################
# High Order Struct Solver #
#########################################################################
// ifvfd:
// isFVMOrFDM:
// 0 -- NSSolverStruct using Finite Volume Method.
// 1 -- NSSolverStruct using Finite Differ Method.
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// -- "roe", "steger".
// structhighordergradient:
// -- "conservation", "chain_rule".
int ifvfd = 0;
int isFVMOrFDM = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6;
@ -885,8 +1116,12 @@ int allReduceStep = 1;
// codeOfOversetGrid: Overlapping(overset) grid or not.
// 0 -- NON-overlapping grid.
// 1 -- Overlapping grid.
// oversetInterpolationMethod: the method of overset interpolation while field simulation
// 0 -- set the acceptor cell value by donor cell value.
// 1 -- set the acceptor cell value by distance weight of donor cell value.
int codeOfOversetGrid = 0;
int codeOfOversetSlipGrid = 0;
int oversetInterpolationMethod = 0;
int readOversetFileOrNot = 0;
int symetryOrNot = 0;
int readInAuxiliaryInnerGrid = 1;
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
string auxiliaryInnerGrid2 = "";
string oversetGridFileName = "./grid/overlap.ovs";
string oversetGridFileName = "./grid/iblank.ovs";
double walldistMainZone = 1.0
double toleranceForOversetSearch = 1.0e-3;
double toleranceForOversetBox = 1.0e-3;
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
int numberOfMovingBodies = 2;
// ----------------- ALE configuration ------------------------------
int codeOfAleModel = 1;
int aleStartStrategy = -1;
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
int strategyForGCLSource = 0; //0-present; 1-Ahn;
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
int methodForKineticEquation = 0;
double relaxParameterOfKinetic = 1.0;
#########################################################################
# motive information #
#########################################################################
int numberOfMovingBodies = 1;
############################## body0 ##############################
//mass of parts
double mass_0 = 1.0;
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
//initial six DOF position information of parts. xc yc zc
double massCenter_0[] = 0.0 , 0.0, 0.0;
//initial six DOF position information of parts. angleX angleY angleZ
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
//initial six DOF move information of parts. vc vy vz
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
//initial six DOF move information of parts. omigX omigY omigZ
double angularVelocity_0[] = 0.0, 0.0, 0.0;
//the object that the parts belong to.
int fartherIndex_0 = -1;
//the assembly position of the parts. xc yc zc angleX angleY angleZ
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
//the move pattern of the parts.
// -1 given motion partten.
// 0 still.
// 1 six DOF motion.
// 2 three DOF motion.
// 11 X-axis forced motion.
// 12 Y-axis forced motion.
// 13 Z-axis forced motion.
// 14 forced pitch motion.
// 15 forced yaw motion.
// 16 forced roll motion.
int RBDMethod_0 = 0;
double amplitude_0 = 0.0;
double reduceFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
//additional force (system axis) fX fY fZ
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
//additional moment of Force (system axis) mX mY mZ
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
//the deformation method of the parts.
int morphing_0 = 0;
// post indentify
int integralOrder = 4;
// ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0;
//@double refReNumber = 2.329418E08;
//@double refDimensionalTemperature = 288.144;
//@double refDimensionalPressure = 1.01313E05;
//@double height = -0.001;
//@double refReNumber = 6.5e6;
//@double refDimensionalTemperature = 288.15;
//@double freestream_vibration_temperature = 300.00;
//@double refDimensionalPressure = 0;
//@double height = 0;
//@int nsubsonicInlet = 0;
//@int nsubsonicOutlet = 0;
//@string inLetFileName = "./bin/subsonicInlet.hypara";
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
//@double refDimensionalVelocity = 0;
//@double refDimensionalDensity = 0;
#########################################################################
# Old Parameter #

6
B07_ThreeD_Sphere_Laminar_Unstruct_4CPU/bin/cfd_para_hypersonic.hypara
View File

@ -60,9 +60,9 @@ double refDimensionalTemperature = 79;
double gridScaleFactor = 1.0;
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
double forceRefenenceLength = 1.0; // unit of meter.
double forceRefenenceArea = 1.0; // unit of meter^2.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.

379
B08_TwoD_Plate_Laminar_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -21,6 +21,7 @@
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
// 2 -- Grid refinement.
// 3 -- Grid merging, merge two blocks into one block.
// 4 -- Grid deformation, achieve unstructured grid deformation.
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
// multiblock: Multi-block grid or not, only for structured grid conversion.
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
//-----------------------------------------------------------------------
// from_gfile: path of original data file for unstructure grid convert from.
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
int numberOfGridFile = 1;
string from_gfile = "./grid/rae2822_hybrid2d.cas";
string from_gfile1= "";
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
// ----------------- some advanced choices ------------------------------
// iunsteady: The Grid is for unsteady simulation or not.
int iunsteady = 0;
int iale = 0;
int codeOfAleModel = 0;
// fileformat: Ustar Grid file format.
@ -122,15 +125,38 @@ int isDeform = 0;
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
int projectOrgPoint = 0; // if project original wall points.
// ----------------- Grid Deform Parameters -----------------------------
// deformationMethod: Grid Deform.
// 1 -- SPRING.
// 2 -- RBF.
// stationalGridFile: Original grid file.
// visualFileName : The visualization file path of deform grid.
// nDeformStep : The max deform step.
// flapAngle : The max flap angle.
// rotatePostionZ : Rotate postion.
// rotatePostionY : Rotate postion.
// gridSlice : If dump slice grid.
// sliceAxis : Grid slice axis.
// slicePosition : Grid slice position.
int nDeformStep = 40;
double flapAngle = 10.0;
double rotatePostionZ = 4.00003;
double rotatePostionY = 3.05;
int deformationMethod = 2;
string stationalGridFile = "./grid/Segment2Brid.fts";
string visualFileName = "./results/deformedGrid.dat"
int gridSlice = 1;
int sliceAxis = 1;
double slicePosition = 13;
// ----------------- RBF Parameters -------------------------------------
// symmetryPlane: Which symmetry plane is used in the mesh.
// 0 -- without symmetry.
// 1 -- plane of x=0.
// 2 -- plane of y=0.
// 3 -- plane of z=0.
int numberOfReferenceCP = 10;
double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// numberOfReferenceCP : Number of reference Control Points.
// influencePara : The RBF influence radius parameter.
int numberOfReferenceCP = 40;
double influencePara = 25.0;
// ----------------- Periodic Parameters --------------------------------
// Notice: Rotational periodicity only support rotation along the X axis!
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
// translationLength[]: The relative distance between two periodic face
which only support one direction.
// rotationAngle: The relative angle between two periodic face.
which is recorded in degrees.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
// 0 -- Interface. (default)
// 1 -- Physical boundary condition, used in Hybrid solver.
// 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.
// parallelPartitionMethod: 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.
// 2 -- Using Metis for homogeneous MPI.
// 3 -- using METIS partition for homogeneous OpenMP.
@ -238,6 +269,8 @@ int compressible = 1;
// 1 -- the flight conditions.
// 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions.
// 4 -- the condition that the velocity, temperature and density are given.
// 5 -- the condition that the velocity, temperature and pressure are given.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -251,10 +284,12 @@ int compressible = 1;
// 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.
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, 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
// condition is radiation equilibrium temperature, and 0.8 is the default value.
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
double refMachNumber = 0.73;
double attackd = 2.79;
@ -263,7 +298,7 @@ double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 6.5e6;
double refDimensionalTemperature = 288.15;
double freestream_vibration_temperature = 10000.00;
double freestream_vibration_temperature = 300.00;
//int inflowParaType = 1;
//double height = 0.001;
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
//double refDimensionalTemperature = 288.144;
//double refDimensionalPressure = 1.01313E05;
//The velocity, temperature and density are fixed.
//int inflowParaType = 4;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalDensity = 1.0e3;
//The velocity, temperature and pressure are fixed.
//int inflowParaType = 5;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalPressure = 1.0e5;
//The MachNumber, temperature and pressure are fixed.
//int inflowParaType = 6;
//double refDimensionalTemperature = 293;
//double refDimensionalPressure = 8886.06;
double wallTemperature = -1.0;
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.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.
double refMolecularWeight = 28.9644; // unit of g/mol.
//-----------------------------------------------------------------------
# Spatial Discretisation #
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
// Using this when solve structered grid or hybrid.
// -- "vanleer", "steger", "hlle", "lax_f".
// -- "roe", "modified_roe".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
// str_limiter_name: Limiter of struct grid.
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
// -- "nolim", no limiter.
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod".
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
// -- "nolim", no limiter.
// uns_vis_name: Discretisation method of viscous term.
// -- "std", "test", "aver", "new1", "new2".
// uns_gradient: Gradient reconstruction method.
// gradientName: Gradient reconstruction method.
// -- "default", "ggcell", "ggnode", "lsq".
// ivencat: Variation of vencat limiter.
// 0 -- org method, it is independent of grid scale.
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
// 1 -- unsteay.
// 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.
// ifStaticsFlowField: Statistical variables for DES simulation.
// ifStaticsFlowField: Statistical variables for unsteady simulation.
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
// startStatisticStep: Outer step when start statistics.
// when the value is larger than "maxSimuStep", it is useless.
// statisticalTimePeriod: Used as time period of statistic analysis.
// when the value is negative, time period is treated as infinite.
// statisticMethod: Statistic reynolds stress method.
0 --tau = <q^2> - <q>^2
1 --tau = <u'u'>
// min_sub_iter: The min sub iteration of unsteady simulation.
// max_sub_iter: The max sub iteration of unsteady simulation.
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
@ -454,7 +511,10 @@ int iunsteady = 0;
double physicalTimeStep = 0.01;
int ifStartFromSteadyResults = 0;
int ifStaticsFlowField = 0;
int ifStaticsReynoldsStress = 0;
int startStatisticStep = 800000;
double statisticalTimePeriod = -1.0;
int statisticMethod = 0;
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
int methodOfDualTime = 3;
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
double csrv = 2.0;
double timemax = 1.0e10;
double dtsave = -1.0;
int codeOfAleModel = 0;
int aleStartStrategy = -1;
int maxale = 10;
double dtau = 0.001;
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
int numberOfGridGroups = 1;
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
string wallTemperaturefile= "";
int walldistMethod = 1;
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt";
string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string samplefile = "results/sample.dat";
int nDumpSurfaceInfo = 0;
string wall_varfile = "";
string jetDefineFile = "bin/jet.hypara";
string overset_gridfile = "results/iblank.ovs";
string sixDofFileName = "results/sixDofInfo.dat";
string derivativeFileName = "results/identify.dat";
string hysteresisFileName = "results/force_beta.plt";
int plotFieldType = 0;
@ -554,6 +614,11 @@ int plotFieldType = 0;
int visualfileType = 1;
// samplefileMode: The dump mode of sample file.
// 0 -- dump out every probe/line/surface data for all step intervals.
// 1 -- dump out all probe/line/surface data for every step intervals.
int samplefileMode = 0;
// visualSlice: The slice of tecflow.
// 0 -- Do not save slice data.
// 1 -- comput and save it to sliceFile.
@ -567,11 +632,13 @@ int visualSlice = 0;
int sliceAxis = 1;
double slicePostion = -0.5;
string sliceFile = "results/Slice.plt";
int dumpWallFaceCenter = 0;
// min-max box of the visual block.
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
double upperPlotFieldBox[] = [1.0 1.0 1.0];
//-----------the optional parameters list for the flow field output----------------
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- 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), iblank(81).
// -- specific heat ratio(gama, 56)
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
// Variables order must from small to big.
//-----------the optional parameters list for the wall boundary condition----------------
// nVisualWallVariables: The number of visual variables on wall.
// visualWallVariables : dumped variable types, listed as following:
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -overlap iblank(iblank, 81)
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
// dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate.
int dumpStandardModel = 0;
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
int turbInterval = 1;
int turbOrderStruct = 2;
int kindOfTurbSource = 0;
int mod_turb_res = 0;
double turb_relax = 1.0;
@ -652,6 +736,10 @@ double muoo = 3.0;
double kwoo = 5.0;
int transitionType = 0;
double turbIntensity = -1.0;
int freeturbIntensitySRModify = 0;
double freeDecayXLocation = 0.0;
int compressibleCorrection = 0;
int transitionMaFix = 1;
# maximum eddy viscosity (myt/my) max.
double eddyViscosityLimit = 1.0e10;
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
# LES Parameter #
//-----------------------------------------------------------------------
// iLES: Create LESSolver or not.
// >= 1 - Create LESSolver;
// < 1 - not.
// == 1 - Create LESSolver;
// != 1 - not.
// amplitudeofDisturb: Amplitude of adding disturb.
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
// iterdisturb: Add random disturb in every sub-iter or only first sub-iter.
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
// utau: friction velocity, using in DNSDisturb.
// sgsmodel: subgrid scale model.
// = "smagorinsky";
// = "dsm";
// = "wale".
// = "dsmCom";
// = "wale";
// = "sigma".
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
// = 2 - pow(deltai * deltaj *deltak, 1/3);
// = 3 - Devloped by Scotti.
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
int deltaFunctionType = 2;
int wallDampingFunctionType = 1;
int turbViscousCutType = 2;
double smagConstant = 0.135;
double smagConstant = 0.1;
double isotropicConstant = 0.0;
double waleConstant = 0.6;
double sigmaConstant = 1.35;
int filterDirection[] = [1, 1, 0];
int averageDirection[] = [0, 0, 0];
double testFilterScale = 2.0;
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
// nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D.
// 5 -- for 3D.
// nGasModel: The type of gas.
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
// Otherwise, the pure gas with one component is used for perfect gas.
// 0 -- Earth gas.
// 1 -- Mars gas.
// 2 -- Argon.
// 3 -- Nitrogen.
// nEnergyRecycle: The type of EnergyModel Recycle.
// 0 -- not used .
// 1 -- used.
// nDensityModify: The type of densitymodify.
// 0 -- not used.
// 1 -- used.
// nchem:
// 0 -- without chemical reaction flow.
// 1 -- the chemical reaction flow is considered.
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
// 0 -- perfect gas.
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
// the value equals to or is greater than 1, and 3 is for default value.
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
// the value equals to or is greater than 1, and 3 is for default value.
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
// the value equals to or is greater than 1, and 3 is for default value.
// nSlipBCModel : The computational model of slip boundary conditions.
// 0 -- no slip.
// 1 -- the conventional Maxwell slip conditions.
// 2 -- the Gokcen slip conditions.
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
// 4 -- the Kogan simplified slip conditions.
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
// nchemsrc:
// 0 -- the source terms are not computed.
// 1 -- the source terms are computed.
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
// 1 -- One-temperature model.
// 2 -- Two-temperature model.
// 3 -- Three-temperature model.
// nTEnergyModel: the method to computing temperature energy model.
// 0 -- the energy term is computed using the conventional method.
// 1 -- the energy term is computed using the curve fitting method.
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
// catalyticCoef:
// 0.0 -- full non-catalytic wall boundary condition.
// 1.0 -- full catalytic wall boundary condition.
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
// nTemperatureJump : the method to calculate the temperature jump.
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
// 1.0 -- proposed by Maxwell.
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
// 1.146 -- proposed for an additional "fictitious" velocity slip.
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
// 0 -- not freeze, the chemical reaction sources will be calculated.
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
// nDebug: cout the Wrong place and abort
// 0 -- not used.
// 1 -- used.
// nSpeciesLimit: limitter of gas species
// 0 -- not used.
// 1 -- used.
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
// 0 -- method 0.
// 1 -- method 1.
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
// 0 -- not used.
// 1 -- used.
// nChemcalSourceModified: Modified on ChemcalSource
// 0 -- not used.
// 1 -- used.
// nAblation:
// 0 -- The wall ablation is not computed.
// 1 -- The wall ablation is computed.
// isInjection:
// 0 -- The injection velocity of ablation wall is not computed.
// 1 -- The injection velocity of ablation wall is computed.
// nViscosityModel:
// 0 -- Blottner fitting method.
// 1 -- Gupta fitting method.
// nSutherland:
// 0 -- stands for selecting the Blotter curve fits mode.
// 1 -- stands for Sutherland relation.
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
// "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.
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
// 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.
@ -758,6 +935,10 @@ int dg_high_order = 0;
int iapplication = 0;
int iCodeBranch = 0;
int nm = 5;
int nEquilibriumGas = 0;
int nPCWCycleStep = 3;
int nRETCycleStep = 3;
int nSLIPCycleStep= 3;
double refGama = 1.4;
double prl = 0.72;
@ -770,23 +951,73 @@ int nchem = 0;
int nchemsrc = 1;
int nchemrad = 1;
int ntmodel = 1;
int nChemicalFlowStep = 0;
int nEnergyRecycle = 0;
int nSlipBCModel = 0;
int nDensityModify = 1;
int nTEnergyModel = 0;
int nMeanFreePathType = 0;
int nIsChemicalFreeze = 0;
int nIsSuperCatalytic = 1;
int nTemperatureJump = 0;
double parkVDPower = 0.6;
double catalyticCoef = 0.0;
double sigmaVelocity = 1.0;
double sigmaTemperature = 1.0;
double sigmaMassFraction = 1.0;
double velocitySlipCorrectConstant = 1.0;
double chemicalRelaxCorf = 1.0;
double chemicalSpectrumRadiusCoef = 1.0;
double viscousSpectrumRadiusCoef = 1.0;
double inviscidSpectrumRadiusCoef = 1.0;
double staticPressureRelaxCorf = 1.0;
double veTemperatureMin = 30.0;
int nDebug = 0;
int nSpeciesLimit = 0;
int nTurblenceForChemical = 0;
int nViscosityFluxSublevelModified = 0 ;
int nChemcalSourceModified = 0;
int nAblation = 0;
int isInjection = 0;
int nViscosityModel = 0;
int nMarsModel = 0;
string gasfile = "DK5";
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
string speciesName = "O, O2, NO, N, N2";
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
//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, 0.233, 0.0, 0.0, 0.0, 0.767, 0.0";
//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, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Mars-Pa8";
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
//string gasfile = "DK7";
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Combustion-12";
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
//string gasfile = "Gas-Mixture";
//string speciesName ="SpeciesA, SpeciesB";
//string initMassFraction = "1.0, 0.0";
int nSutherland = 0;
double gamaSpeciesA = 1.4;
double gamaSpeciesB = 1.3;
double molecularWeightSpeciesA = 29.0;
double molecularWeightSpeciesB = 30.0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0;
#########################################################################
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
#########################################################################
# High Order Struct Solver #
#########################################################################
// ifvfd:
// isFVMOrFDM:
// 0 -- NSSolverStruct using Finite Volume Method.
// 1 -- NSSolverStruct using Finite Differ Method.
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// -- "roe", "steger".
// structhighordergradient:
// -- "conservation", "chain_rule".
int ifvfd = 0;
int isFVMOrFDM = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6;
@ -885,8 +1116,12 @@ int allReduceStep = 1;
// codeOfOversetGrid: Overlapping(overset) grid or not.
// 0 -- NON-overlapping grid.
// 1 -- Overlapping grid.
// oversetInterpolationMethod: the method of overset interpolation while field simulation
// 0 -- set the acceptor cell value by donor cell value.
// 1 -- set the acceptor cell value by distance weight of donor cell value.
int codeOfOversetGrid = 0;
int codeOfOversetSlipGrid = 0;
int oversetInterpolationMethod = 0;
int readOversetFileOrNot = 0;
int symetryOrNot = 0;
int readInAuxiliaryInnerGrid = 1;
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
string auxiliaryInnerGrid2 = "";
string oversetGridFileName = "./grid/overlap.ovs";
string oversetGridFileName = "./grid/iblank.ovs";
double walldistMainZone = 1.0
double toleranceForOversetSearch = 1.0e-3;
double toleranceForOversetBox = 1.0e-3;
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
int numberOfMovingBodies = 2;
// ----------------- ALE configuration ------------------------------
int codeOfAleModel = 1;
int aleStartStrategy = -1;
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
int strategyForGCLSource = 0; //0-present; 1-Ahn;
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
int methodForKineticEquation = 0;
double relaxParameterOfKinetic = 1.0;
#########################################################################
# motive information #
#########################################################################
int numberOfMovingBodies = 1;
############################## body0 ##############################
//mass of parts
double mass_0 = 1.0;
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
//initial six DOF position information of parts. xc yc zc
double massCenter_0[] = 0.0 , 0.0, 0.0;
//initial six DOF position information of parts. angleX angleY angleZ
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
//initial six DOF move information of parts. vc vy vz
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
//initial six DOF move information of parts. omigX omigY omigZ
double angularVelocity_0[] = 0.0, 0.0, 0.0;
//the object that the parts belong to.
int fartherIndex_0 = -1;
//the assembly position of the parts. xc yc zc angleX angleY angleZ
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
//the move pattern of the parts.
// -1 given motion partten.
// 0 still.
// 1 six DOF motion.
// 2 three DOF motion.
// 11 X-axis forced motion.
// 12 Y-axis forced motion.
// 13 Z-axis forced motion.
// 14 forced pitch motion.
// 15 forced yaw motion.
// 16 forced roll motion.
int RBDMethod_0 = 0;
double amplitude_0 = 0.0;
double reduceFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
//additional force (system axis) fX fY fZ
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
//additional moment of Force (system axis) mX mY mZ
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
//the deformation method of the parts.
int morphing_0 = 0;
// post indentify
int integralOrder = 4;
// ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0;
//@double refReNumber = 2.329418E08;
//@double refDimensionalTemperature = 288.144;
//@double refDimensionalPressure = 1.01313E05;
//@double height = -0.001;
//@double refReNumber = 6.5e6;
//@double refDimensionalTemperature = 288.15;
//@double freestream_vibration_temperature = 300.00;
//@double refDimensionalPressure = 0;
//@double height = 0;
//@int nsubsonicInlet = 0;
//@int nsubsonicOutlet = 0;
//@string inLetFileName = "./bin/subsonicInlet.hypara";
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
//@double refDimensionalVelocity = 0;
//@double refDimensionalDensity = 0;
#########################################################################
# Old Parameter #

6
B08_TwoD_Plate_Laminar_Unstruct_1CPU/bin/cfd_para_subsonic.hypara
View File

@ -57,9 +57,9 @@ double refDimensionalTemperature = 293;
double gridScaleFactor = 1.0;
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
double forceRefenenceLength = 1.0; // unit of meter.
double forceRefenenceArea = 1.0; // unit of meter^2.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.

379
B09_TwoD_plate_SA_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -21,6 +21,7 @@
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
// 2 -- Grid refinement.
// 3 -- Grid merging, merge two blocks into one block.
// 4 -- Grid deformation, achieve unstructured grid deformation.
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
// multiblock: Multi-block grid or not, only for structured grid conversion.
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
//-----------------------------------------------------------------------
// from_gfile: path of original data file for unstructure grid convert from.
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
int numberOfGridFile = 1;
string from_gfile = "./grid/rae2822_hybrid2d.cas";
string from_gfile1= "";
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
// ----------------- some advanced choices ------------------------------
// iunsteady: The Grid is for unsteady simulation or not.
int iunsteady = 0;
int iale = 0;
int codeOfAleModel = 0;
// fileformat: Ustar Grid file format.
@ -122,15 +125,38 @@ int isDeform = 0;
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
int projectOrgPoint = 0; // if project original wall points.
// ----------------- Grid Deform Parameters -----------------------------
// deformationMethod: Grid Deform.
// 1 -- SPRING.
// 2 -- RBF.
// stationalGridFile: Original grid file.
// visualFileName : The visualization file path of deform grid.
// nDeformStep : The max deform step.
// flapAngle : The max flap angle.
// rotatePostionZ : Rotate postion.
// rotatePostionY : Rotate postion.
// gridSlice : If dump slice grid.
// sliceAxis : Grid slice axis.
// slicePosition : Grid slice position.
int nDeformStep = 40;
double flapAngle = 10.0;
double rotatePostionZ = 4.00003;
double rotatePostionY = 3.05;
int deformationMethod = 2;
string stationalGridFile = "./grid/Segment2Brid.fts";
string visualFileName = "./results/deformedGrid.dat"
int gridSlice = 1;
int sliceAxis = 1;
double slicePosition = 13;
// ----------------- RBF Parameters -------------------------------------
// symmetryPlane: Which symmetry plane is used in the mesh.
// 0 -- without symmetry.
// 1 -- plane of x=0.
// 2 -- plane of y=0.
// 3 -- plane of z=0.
int numberOfReferenceCP = 10;
double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// numberOfReferenceCP : Number of reference Control Points.
// influencePara : The RBF influence radius parameter.
int numberOfReferenceCP = 40;
double influencePara = 25.0;
// ----------------- Periodic Parameters --------------------------------
// Notice: Rotational periodicity only support rotation along the X axis!
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
// translationLength[]: The relative distance between two periodic face
which only support one direction.
// rotationAngle: The relative angle between two periodic face.
which is recorded in degrees.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
// 0 -- Interface. (default)
// 1 -- Physical boundary condition, used in Hybrid solver.
// 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.
// parallelPartitionMethod: 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.
// 2 -- Using Metis for homogeneous MPI.
// 3 -- using METIS partition for homogeneous OpenMP.
@ -238,6 +269,8 @@ int compressible = 1;
// 1 -- the flight conditions.
// 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions.
// 4 -- the condition that the velocity, temperature and density are given.
// 5 -- the condition that the velocity, temperature and pressure are given.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -251,10 +284,12 @@ int compressible = 1;
// 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.
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, 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
// condition is radiation equilibrium temperature, and 0.8 is the default value.
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
double refMachNumber = 0.73;
double attackd = 2.79;
@ -263,7 +298,7 @@ double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 6.5e6;
double refDimensionalTemperature = 288.15;
double freestream_vibration_temperature = 10000.00;
double freestream_vibration_temperature = 300.00;
//int inflowParaType = 1;
//double height = 0.001;
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
//double refDimensionalTemperature = 288.144;
//double refDimensionalPressure = 1.01313E05;
//The velocity, temperature and density are fixed.
//int inflowParaType = 4;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalDensity = 1.0e3;
//The velocity, temperature and pressure are fixed.
//int inflowParaType = 5;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalPressure = 1.0e5;
//The MachNumber, temperature and pressure are fixed.
//int inflowParaType = 6;
//double refDimensionalTemperature = 293;
//double refDimensionalPressure = 8886.06;
double wallTemperature = -1.0;
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.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.
double refMolecularWeight = 28.9644; // unit of g/mol.
//-----------------------------------------------------------------------
# Spatial Discretisation #
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
// Using this when solve structered grid or hybrid.
// -- "vanleer", "steger", "hlle", "lax_f".
// -- "roe", "modified_roe".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
// str_limiter_name: Limiter of struct grid.
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
// -- "nolim", no limiter.
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod".
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
// -- "nolim", no limiter.
// uns_vis_name: Discretisation method of viscous term.
// -- "std", "test", "aver", "new1", "new2".
// uns_gradient: Gradient reconstruction method.
// gradientName: Gradient reconstruction method.
// -- "default", "ggcell", "ggnode", "lsq".
// ivencat: Variation of vencat limiter.
// 0 -- org method, it is independent of grid scale.
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
// 1 -- unsteay.
// 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.
// ifStaticsFlowField: Statistical variables for DES simulation.
// ifStaticsFlowField: Statistical variables for unsteady simulation.
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
// startStatisticStep: Outer step when start statistics.
// when the value is larger than "maxSimuStep", it is useless.
// statisticalTimePeriod: Used as time period of statistic analysis.
// when the value is negative, time period is treated as infinite.
// statisticMethod: Statistic reynolds stress method.
0 --tau = <q^2> - <q>^2
1 --tau = <u'u'>
// min_sub_iter: The min sub iteration of unsteady simulation.
// max_sub_iter: The max sub iteration of unsteady simulation.
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
@ -454,7 +511,10 @@ int iunsteady = 0;
double physicalTimeStep = 0.01;
int ifStartFromSteadyResults = 0;
int ifStaticsFlowField = 0;
int ifStaticsReynoldsStress = 0;
int startStatisticStep = 800000;
double statisticalTimePeriod = -1.0;
int statisticMethod = 0;
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
int methodOfDualTime = 3;
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
double csrv = 2.0;
double timemax = 1.0e10;
double dtsave = -1.0;
int codeOfAleModel = 0;
int aleStartStrategy = -1;
int maxale = 10;
double dtau = 0.001;
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
int numberOfGridGroups = 1;
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
string wallTemperaturefile= "";
int walldistMethod = 1;
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt";
string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string samplefile = "results/sample.dat";
int nDumpSurfaceInfo = 0;
string wall_varfile = "";
string jetDefineFile = "bin/jet.hypara";
string overset_gridfile = "results/iblank.ovs";
string sixDofFileName = "results/sixDofInfo.dat";
string derivativeFileName = "results/identify.dat";
string hysteresisFileName = "results/force_beta.plt";
int plotFieldType = 0;
@ -554,6 +614,11 @@ int plotFieldType = 0;
int visualfileType = 1;
// samplefileMode: The dump mode of sample file.
// 0 -- dump out every probe/line/surface data for all step intervals.
// 1 -- dump out all probe/line/surface data for every step intervals.
int samplefileMode = 0;
// visualSlice: The slice of tecflow.
// 0 -- Do not save slice data.
// 1 -- comput and save it to sliceFile.
@ -567,11 +632,13 @@ int visualSlice = 0;
int sliceAxis = 1;
double slicePostion = -0.5;
string sliceFile = "results/Slice.plt";
int dumpWallFaceCenter = 0;
// min-max box of the visual block.
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
double upperPlotFieldBox[] = [1.0 1.0 1.0];
//-----------the optional parameters list for the flow field output----------------
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- 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), iblank(81).
// -- specific heat ratio(gama, 56)
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
// Variables order must from small to big.
//-----------the optional parameters list for the wall boundary condition----------------
// nVisualWallVariables: The number of visual variables on wall.
// visualWallVariables : dumped variable types, listed as following:
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -overlap iblank(iblank, 81)
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
// dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate.
int dumpStandardModel = 0;
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
int turbInterval = 1;
int turbOrderStruct = 2;
int kindOfTurbSource = 0;
int mod_turb_res = 0;
double turb_relax = 1.0;
@ -652,6 +736,10 @@ double muoo = 3.0;
double kwoo = 5.0;
int transitionType = 0;
double turbIntensity = -1.0;
int freeturbIntensitySRModify = 0;
double freeDecayXLocation = 0.0;
int compressibleCorrection = 0;
int transitionMaFix = 1;
# maximum eddy viscosity (myt/my) max.
double eddyViscosityLimit = 1.0e10;
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
# LES Parameter #
//-----------------------------------------------------------------------
// iLES: Create LESSolver or not.
// >= 1 - Create LESSolver;
// < 1 - not.
// == 1 - Create LESSolver;
// != 1 - not.
// amplitudeofDisturb: Amplitude of adding disturb.
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
// iterdisturb: Add random disturb in every sub-iter or only first sub-iter.
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
// utau: friction velocity, using in DNSDisturb.
// sgsmodel: subgrid scale model.
// = "smagorinsky";
// = "dsm";
// = "wale".
// = "dsmCom";
// = "wale";
// = "sigma".
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
// = 2 - pow(deltai * deltaj *deltak, 1/3);
// = 3 - Devloped by Scotti.
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
int deltaFunctionType = 2;
int wallDampingFunctionType = 1;
int turbViscousCutType = 2;
double smagConstant = 0.135;
double smagConstant = 0.1;
double isotropicConstant = 0.0;
double waleConstant = 0.6;
double sigmaConstant = 1.35;
int filterDirection[] = [1, 1, 0];
int averageDirection[] = [0, 0, 0];
double testFilterScale = 2.0;
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
// nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D.
// 5 -- for 3D.
// nGasModel: The type of gas.
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
// Otherwise, the pure gas with one component is used for perfect gas.
// 0 -- Earth gas.
// 1 -- Mars gas.
// 2 -- Argon.
// 3 -- Nitrogen.
// nEnergyRecycle: The type of EnergyModel Recycle.
// 0 -- not used .
// 1 -- used.
// nDensityModify: The type of densitymodify.
// 0 -- not used.
// 1 -- used.
// nchem:
// 0 -- without chemical reaction flow.
// 1 -- the chemical reaction flow is considered.
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
// 0 -- perfect gas.
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
// the value equals to or is greater than 1, and 3 is for default value.
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
// the value equals to or is greater than 1, and 3 is for default value.
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
// the value equals to or is greater than 1, and 3 is for default value.
// nSlipBCModel : The computational model of slip boundary conditions.
// 0 -- no slip.
// 1 -- the conventional Maxwell slip conditions.
// 2 -- the Gokcen slip conditions.
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
// 4 -- the Kogan simplified slip conditions.
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
// nchemsrc:
// 0 -- the source terms are not computed.
// 1 -- the source terms are computed.
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
// 1 -- One-temperature model.
// 2 -- Two-temperature model.
// 3 -- Three-temperature model.
// nTEnergyModel: the method to computing temperature energy model.
// 0 -- the energy term is computed using the conventional method.
// 1 -- the energy term is computed using the curve fitting method.
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
// catalyticCoef:
// 0.0 -- full non-catalytic wall boundary condition.
// 1.0 -- full catalytic wall boundary condition.
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
// nTemperatureJump : the method to calculate the temperature jump.
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
// 1.0 -- proposed by Maxwell.
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
// 1.146 -- proposed for an additional "fictitious" velocity slip.
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
// 0 -- not freeze, the chemical reaction sources will be calculated.
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
// nDebug: cout the Wrong place and abort
// 0 -- not used.
// 1 -- used.
// nSpeciesLimit: limitter of gas species
// 0 -- not used.
// 1 -- used.
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
// 0 -- method 0.
// 1 -- method 1.
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
// 0 -- not used.
// 1 -- used.
// nChemcalSourceModified: Modified on ChemcalSource
// 0 -- not used.
// 1 -- used.
// nAblation:
// 0 -- The wall ablation is not computed.
// 1 -- The wall ablation is computed.
// isInjection:
// 0 -- The injection velocity of ablation wall is not computed.
// 1 -- The injection velocity of ablation wall is computed.
// nViscosityModel:
// 0 -- Blottner fitting method.
// 1 -- Gupta fitting method.
// nSutherland:
// 0 -- stands for selecting the Blotter curve fits mode.
// 1 -- stands for Sutherland relation.
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
// "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.
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
// 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.
@ -758,6 +935,10 @@ int dg_high_order = 0;
int iapplication = 0;
int iCodeBranch = 0;
int nm = 5;
int nEquilibriumGas = 0;
int nPCWCycleStep = 3;
int nRETCycleStep = 3;
int nSLIPCycleStep= 3;
double refGama = 1.4;
double prl = 0.72;
@ -770,23 +951,73 @@ int nchem = 0;
int nchemsrc = 1;
int nchemrad = 1;
int ntmodel = 1;
int nChemicalFlowStep = 0;
int nEnergyRecycle = 0;
int nSlipBCModel = 0;
int nDensityModify = 1;
int nTEnergyModel = 0;
int nMeanFreePathType = 0;
int nIsChemicalFreeze = 0;
int nIsSuperCatalytic = 1;
int nTemperatureJump = 0;
double parkVDPower = 0.6;
double catalyticCoef = 0.0;
double sigmaVelocity = 1.0;
double sigmaTemperature = 1.0;
double sigmaMassFraction = 1.0;
double velocitySlipCorrectConstant = 1.0;
double chemicalRelaxCorf = 1.0;
double chemicalSpectrumRadiusCoef = 1.0;
double viscousSpectrumRadiusCoef = 1.0;
double inviscidSpectrumRadiusCoef = 1.0;
double staticPressureRelaxCorf = 1.0;
double veTemperatureMin = 30.0;
int nDebug = 0;
int nSpeciesLimit = 0;
int nTurblenceForChemical = 0;
int nViscosityFluxSublevelModified = 0 ;
int nChemcalSourceModified = 0;
int nAblation = 0;
int isInjection = 0;
int nViscosityModel = 0;
int nMarsModel = 0;
string gasfile = "DK5";
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
string speciesName = "O, O2, NO, N, N2";
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
//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, 0.233, 0.0, 0.0, 0.0, 0.767, 0.0";
//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, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Mars-Pa8";
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
//string gasfile = "DK7";
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Combustion-12";
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
//string gasfile = "Gas-Mixture";
//string speciesName ="SpeciesA, SpeciesB";
//string initMassFraction = "1.0, 0.0";
int nSutherland = 0;
double gamaSpeciesA = 1.4;
double gamaSpeciesB = 1.3;
double molecularWeightSpeciesA = 29.0;
double molecularWeightSpeciesB = 30.0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0;
#########################################################################
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
#########################################################################
# High Order Struct Solver #
#########################################################################
// ifvfd:
// isFVMOrFDM:
// 0 -- NSSolverStruct using Finite Volume Method.
// 1 -- NSSolverStruct using Finite Differ Method.
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// -- "roe", "steger".
// structhighordergradient:
// -- "conservation", "chain_rule".
int ifvfd = 0;
int isFVMOrFDM = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6;
@ -885,8 +1116,12 @@ int allReduceStep = 1;
// codeOfOversetGrid: Overlapping(overset) grid or not.
// 0 -- NON-overlapping grid.
// 1 -- Overlapping grid.
// oversetInterpolationMethod: the method of overset interpolation while field simulation
// 0 -- set the acceptor cell value by donor cell value.
// 1 -- set the acceptor cell value by distance weight of donor cell value.
int codeOfOversetGrid = 0;
int codeOfOversetSlipGrid = 0;
int oversetInterpolationMethod = 0;
int readOversetFileOrNot = 0;
int symetryOrNot = 0;
int readInAuxiliaryInnerGrid = 1;
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
string auxiliaryInnerGrid2 = "";
string oversetGridFileName = "./grid/overlap.ovs";
string oversetGridFileName = "./grid/iblank.ovs";
double walldistMainZone = 1.0
double toleranceForOversetSearch = 1.0e-3;
double toleranceForOversetBox = 1.0e-3;
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
int numberOfMovingBodies = 2;
// ----------------- ALE configuration ------------------------------
int codeOfAleModel = 1;
int aleStartStrategy = -1;
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
int strategyForGCLSource = 0; //0-present; 1-Ahn;
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
int methodForKineticEquation = 0;
double relaxParameterOfKinetic = 1.0;
#########################################################################
# motive information #
#########################################################################
int numberOfMovingBodies = 1;
############################## body0 ##############################
//mass of parts
double mass_0 = 1.0;
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
//initial six DOF position information of parts. xc yc zc
double massCenter_0[] = 0.0 , 0.0, 0.0;
//initial six DOF position information of parts. angleX angleY angleZ
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
//initial six DOF move information of parts. vc vy vz
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
//initial six DOF move information of parts. omigX omigY omigZ
double angularVelocity_0[] = 0.0, 0.0, 0.0;
//the object that the parts belong to.
int fartherIndex_0 = -1;
//the assembly position of the parts. xc yc zc angleX angleY angleZ
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
//the move pattern of the parts.
// -1 given motion partten.
// 0 still.
// 1 six DOF motion.
// 2 three DOF motion.
// 11 X-axis forced motion.
// 12 Y-axis forced motion.
// 13 Z-axis forced motion.
// 14 forced pitch motion.
// 15 forced yaw motion.
// 16 forced roll motion.
int RBDMethod_0 = 0;
double amplitude_0 = 0.0;
double reduceFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
//additional force (system axis) fX fY fZ
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
//additional moment of Force (system axis) mX mY mZ
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
//the deformation method of the parts.
int morphing_0 = 0;
// post indentify
int integralOrder = 4;
// ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0;
//@double refReNumber = 2.329418E08;
//@double refDimensionalTemperature = 288.144;
//@double refDimensionalPressure = 1.01313E05;
//@double height = -0.001;
//@double refReNumber = 6.5e6;
//@double refDimensionalTemperature = 288.15;
//@double freestream_vibration_temperature = 300.00;
//@double refDimensionalPressure = 0;
//@double height = 0;
//@int nsubsonicInlet = 0;
//@int nsubsonicOutlet = 0;
//@string inLetFileName = "./bin/subsonicInlet.hypara";
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
//@double refDimensionalVelocity = 0;
//@double refDimensionalDensity = 0;
#########################################################################
# Old Parameter #

6
B09_TwoD_plate_SA_Unstruct_1CPU/bin/cfd_para_subsonic.hypara
View File

@ -57,9 +57,9 @@ double refDimensionalTemperature = 293;
double gridScaleFactor = 1.0;
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
double forceRefenenceLength = 1.0; // unit of meter.
double forceRefenenceArea = 1.0; // unit of meter^2.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.

379
B10_ThreeD_CompRamp-16_SA_Unstruct_1CPU/bin/cfd_para.hypara
View File

@ -21,6 +21,7 @@
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
// 2 -- Grid refinement.
// 3 -- Grid merging, merge two blocks into one block.
// 4 -- Grid deformation, achieve unstructured grid deformation.
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
// multiblock: Multi-block grid or not, only for structured grid conversion.
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
//-----------------------------------------------------------------------
// from_gfile: path of original data file for unstructure grid convert from.
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
int numberOfGridFile = 1;
string from_gfile = "./grid/rae2822_hybrid2d.cas";
string from_gfile1= "";
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
// ----------------- some advanced choices ------------------------------
// iunsteady: The Grid is for unsteady simulation or not.
int iunsteady = 0;
int iale = 0;
int codeOfAleModel = 0;
// fileformat: Ustar Grid file format.
@ -122,15 +125,38 @@ int isDeform = 0;
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
int projectOrgPoint = 0; // if project original wall points.
// ----------------- Grid Deform Parameters -----------------------------
// deformationMethod: Grid Deform.
// 1 -- SPRING.
// 2 -- RBF.
// stationalGridFile: Original grid file.
// visualFileName : The visualization file path of deform grid.
// nDeformStep : The max deform step.
// flapAngle : The max flap angle.
// rotatePostionZ : Rotate postion.
// rotatePostionY : Rotate postion.
// gridSlice : If dump slice grid.
// sliceAxis : Grid slice axis.
// slicePosition : Grid slice position.
int nDeformStep = 40;
double flapAngle = 10.0;
double rotatePostionZ = 4.00003;
double rotatePostionY = 3.05;
int deformationMethod = 2;
string stationalGridFile = "./grid/Segment2Brid.fts";
string visualFileName = "./results/deformedGrid.dat"
int gridSlice = 1;
int sliceAxis = 1;
double slicePosition = 13;
// ----------------- RBF Parameters -------------------------------------
// symmetryPlane: Which symmetry plane is used in the mesh.
// 0 -- without symmetry.
// 1 -- plane of x=0.
// 2 -- plane of y=0.
// 3 -- plane of z=0.
int numberOfReferenceCP = 10;
double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// numberOfReferenceCP : Number of reference Control Points.
// influencePara : The RBF influence radius parameter.
int numberOfReferenceCP = 40;
double influencePara = 25.0;
// ----------------- Periodic Parameters --------------------------------
// Notice: Rotational periodicity only support rotation along the X axis!
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
// translationLength[]: The relative distance between two periodic face
which only support one direction.
// rotationAngle: The relative angle between two periodic face.
which is recorded in degrees.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
// 0 -- Interface. (default)
// 1 -- Physical boundary condition, used in Hybrid solver.
// 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.
// parallelPartitionMethod: 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.
// 2 -- Using Metis for homogeneous MPI.
// 3 -- using METIS partition for homogeneous OpenMP.
@ -238,6 +269,8 @@ int compressible = 1;
// 1 -- the flight conditions.
// 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions.
// 4 -- the condition that the velocity, temperature and density are given.
// 5 -- the condition that the velocity, temperature and pressure are given.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -251,10 +284,12 @@ int compressible = 1;
// 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.
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, 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
// condition is radiation equilibrium temperature, and 0.8 is the default value.
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
double refMachNumber = 0.73;
double attackd = 2.79;
@ -263,7 +298,7 @@ double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 6.5e6;
double refDimensionalTemperature = 288.15;
double freestream_vibration_temperature = 10000.00;
double freestream_vibration_temperature = 300.00;
//int inflowParaType = 1;
//double height = 0.001;
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
//double refDimensionalTemperature = 288.144;
//double refDimensionalPressure = 1.01313E05;
//The velocity, temperature and density are fixed.
//int inflowParaType = 4;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalDensity = 1.0e3;
//The velocity, temperature and pressure are fixed.
//int inflowParaType = 5;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalPressure = 1.0e5;
//The MachNumber, temperature and pressure are fixed.
//int inflowParaType = 6;
//double refDimensionalTemperature = 293;
//double refDimensionalPressure = 8886.06;
double wallTemperature = -1.0;
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.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.
double refMolecularWeight = 28.9644; // unit of g/mol.
//-----------------------------------------------------------------------
# Spatial Discretisation #
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
// Using this when solve structered grid or hybrid.
// -- "vanleer", "steger", "hlle", "lax_f".
// -- "roe", "modified_roe".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
// str_limiter_name: Limiter of struct grid.
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
// -- "nolim", no limiter.
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod".
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
// -- "nolim", no limiter.
// uns_vis_name: Discretisation method of viscous term.
// -- "std", "test", "aver", "new1", "new2".
// uns_gradient: Gradient reconstruction method.
// gradientName: Gradient reconstruction method.
// -- "default", "ggcell", "ggnode", "lsq".
// ivencat: Variation of vencat limiter.
// 0 -- org method, it is independent of grid scale.
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
// 1 -- unsteay.
// 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.
// ifStaticsFlowField: Statistical variables for DES simulation.
// ifStaticsFlowField: Statistical variables for unsteady simulation.
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
// startStatisticStep: Outer step when start statistics.
// when the value is larger than "maxSimuStep", it is useless.
// statisticalTimePeriod: Used as time period of statistic analysis.
// when the value is negative, time period is treated as infinite.
// statisticMethod: Statistic reynolds stress method.
0 --tau = <q^2> - <q>^2
1 --tau = <u'u'>
// min_sub_iter: The min sub iteration of unsteady simulation.
// max_sub_iter: The max sub iteration of unsteady simulation.
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
@ -454,7 +511,10 @@ int iunsteady = 0;
double physicalTimeStep = 0.01;
int ifStartFromSteadyResults = 0;
int ifStaticsFlowField = 0;
int ifStaticsReynoldsStress = 0;
int startStatisticStep = 800000;
double statisticalTimePeriod = -1.0;
int statisticMethod = 0;
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
int methodOfDualTime = 3;
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
double csrv = 2.0;
double timemax = 1.0e10;
double dtsave = -1.0;
int codeOfAleModel = 0;
int aleStartStrategy = -1;
int maxale = 10;
double dtau = 0.001;
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
int numberOfGridGroups = 1;
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
string wallTemperaturefile= "";
int walldistMethod = 1;
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt";
string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string samplefile = "results/sample.dat";
int nDumpSurfaceInfo = 0;
string wall_varfile = "";
string jetDefineFile = "bin/jet.hypara";
string overset_gridfile = "results/iblank.ovs";
string sixDofFileName = "results/sixDofInfo.dat";
string derivativeFileName = "results/identify.dat";
string hysteresisFileName = "results/force_beta.plt";
int plotFieldType = 0;
@ -554,6 +614,11 @@ int plotFieldType = 0;
int visualfileType = 1;
// samplefileMode: The dump mode of sample file.
// 0 -- dump out every probe/line/surface data for all step intervals.
// 1 -- dump out all probe/line/surface data for every step intervals.
int samplefileMode = 0;
// visualSlice: The slice of tecflow.
// 0 -- Do not save slice data.
// 1 -- comput and save it to sliceFile.
@ -567,11 +632,13 @@ int visualSlice = 0;
int sliceAxis = 1;
double slicePostion = -0.5;
string sliceFile = "results/Slice.plt";
int dumpWallFaceCenter = 0;
// min-max box of the visual block.
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
double upperPlotFieldBox[] = [1.0 1.0 1.0];
//-----------the optional parameters list for the flow field output----------------
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- 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), iblank(81).
// -- specific heat ratio(gama, 56)
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
// Variables order must from small to big.
//-----------the optional parameters list for the wall boundary condition----------------
// nVisualWallVariables: The number of visual variables on wall.
// visualWallVariables : dumped variable types, listed as following:
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -overlap iblank(iblank, 81)
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
// dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate.
int dumpStandardModel = 0;
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
int turbInterval = 1;
int turbOrderStruct = 2;
int kindOfTurbSource = 0;
int mod_turb_res = 0;
double turb_relax = 1.0;
@ -652,6 +736,10 @@ double muoo = 3.0;
double kwoo = 5.0;
int transitionType = 0;
double turbIntensity = -1.0;
int freeturbIntensitySRModify = 0;
double freeDecayXLocation = 0.0;
int compressibleCorrection = 0;
int transitionMaFix = 1;
# maximum eddy viscosity (myt/my) max.
double eddyViscosityLimit = 1.0e10;
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
# LES Parameter #
//-----------------------------------------------------------------------
// iLES: Create LESSolver or not.
// >= 1 - Create LESSolver;
// < 1 - not.
// == 1 - Create LESSolver;
// != 1 - not.
// amplitudeofDisturb: Amplitude of adding disturb.
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
// iterdisturb: Add random disturb in every sub-iter or only first sub-iter.
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
// utau: friction velocity, using in DNSDisturb.
// sgsmodel: subgrid scale model.
// = "smagorinsky";
// = "dsm";
// = "wale".
// = "dsmCom";
// = "wale";
// = "sigma".
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
// = 2 - pow(deltai * deltaj *deltak, 1/3);
// = 3 - Devloped by Scotti.
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
int deltaFunctionType = 2;
int wallDampingFunctionType = 1;
int turbViscousCutType = 2;
double smagConstant = 0.135;
double smagConstant = 0.1;
double isotropicConstant = 0.0;
double waleConstant = 0.6;
double sigmaConstant = 1.35;
int filterDirection[] = [1, 1, 0];
int averageDirection[] = [0, 0, 0];
double testFilterScale = 2.0;
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
// nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D.
// 5 -- for 3D.
// nGasModel: The type of gas.
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
// Otherwise, the pure gas with one component is used for perfect gas.
// 0 -- Earth gas.
// 1 -- Mars gas.
// 2 -- Argon.
// 3 -- Nitrogen.
// nEnergyRecycle: The type of EnergyModel Recycle.
// 0 -- not used .
// 1 -- used.
// nDensityModify: The type of densitymodify.
// 0 -- not used.
// 1 -- used.
// nchem:
// 0 -- without chemical reaction flow.
// 1 -- the chemical reaction flow is considered.
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
// 0 -- perfect gas.
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
// the value equals to or is greater than 1, and 3 is for default value.
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
// the value equals to or is greater than 1, and 3 is for default value.
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
// the value equals to or is greater than 1, and 3 is for default value.
// nSlipBCModel : The computational model of slip boundary conditions.
// 0 -- no slip.
// 1 -- the conventional Maxwell slip conditions.
// 2 -- the Gokcen slip conditions.
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
// 4 -- the Kogan simplified slip conditions.
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
// nchemsrc:
// 0 -- the source terms are not computed.
// 1 -- the source terms are computed.
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
// 1 -- One-temperature model.
// 2 -- Two-temperature model.
// 3 -- Three-temperature model.
// nTEnergyModel: the method to computing temperature energy model.
// 0 -- the energy term is computed using the conventional method.
// 1 -- the energy term is computed using the curve fitting method.
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
// catalyticCoef:
// 0.0 -- full non-catalytic wall boundary condition.
// 1.0 -- full catalytic wall boundary condition.
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
// nTemperatureJump : the method to calculate the temperature jump.
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
// 1.0 -- proposed by Maxwell.
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
// 1.146 -- proposed for an additional "fictitious" velocity slip.
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
// 0 -- not freeze, the chemical reaction sources will be calculated.
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
// nDebug: cout the Wrong place and abort
// 0 -- not used.
// 1 -- used.
// nSpeciesLimit: limitter of gas species
// 0 -- not used.
// 1 -- used.
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
// 0 -- method 0.
// 1 -- method 1.
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
// 0 -- not used.
// 1 -- used.
// nChemcalSourceModified: Modified on ChemcalSource
// 0 -- not used.
// 1 -- used.
// nAblation:
// 0 -- The wall ablation is not computed.
// 1 -- The wall ablation is computed.
// isInjection:
// 0 -- The injection velocity of ablation wall is not computed.
// 1 -- The injection velocity of ablation wall is computed.
// nViscosityModel:
// 0 -- Blottner fitting method.
// 1 -- Gupta fitting method.
// nSutherland:
// 0 -- stands for selecting the Blotter curve fits mode.
// 1 -- stands for Sutherland relation.
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
// "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.
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
// 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.
@ -758,6 +935,10 @@ int dg_high_order = 0;
int iapplication = 0;
int iCodeBranch = 0;
int nm = 5;
int nEquilibriumGas = 0;
int nPCWCycleStep = 3;
int nRETCycleStep = 3;
int nSLIPCycleStep= 3;
double refGama = 1.4;
double prl = 0.72;
@ -770,23 +951,73 @@ int nchem = 0;
int nchemsrc = 1;
int nchemrad = 1;
int ntmodel = 1;
int nChemicalFlowStep = 0;
int nEnergyRecycle = 0;
int nSlipBCModel = 0;
int nDensityModify = 1;
int nTEnergyModel = 0;
int nMeanFreePathType = 0;
int nIsChemicalFreeze = 0;
int nIsSuperCatalytic = 1;
int nTemperatureJump = 0;
double parkVDPower = 0.6;
double catalyticCoef = 0.0;
double sigmaVelocity = 1.0;
double sigmaTemperature = 1.0;
double sigmaMassFraction = 1.0;
double velocitySlipCorrectConstant = 1.0;
double chemicalRelaxCorf = 1.0;
double chemicalSpectrumRadiusCoef = 1.0;
double viscousSpectrumRadiusCoef = 1.0;
double inviscidSpectrumRadiusCoef = 1.0;
double staticPressureRelaxCorf = 1.0;
double veTemperatureMin = 30.0;
int nDebug = 0;
int nSpeciesLimit = 0;
int nTurblenceForChemical = 0;
int nViscosityFluxSublevelModified = 0 ;
int nChemcalSourceModified = 0;
int nAblation = 0;
int isInjection = 0;
int nViscosityModel = 0;
int nMarsModel = 0;
string gasfile = "DK5";
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
string speciesName = "O, O2, NO, N, N2";
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
//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, 0.233, 0.0, 0.0, 0.0, 0.767, 0.0";
//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, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Mars-Pa8";
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
//string gasfile = "DK7";
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Combustion-12";
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
//string gasfile = "Gas-Mixture";
//string speciesName ="SpeciesA, SpeciesB";
//string initMassFraction = "1.0, 0.0";
int nSutherland = 0;
double gamaSpeciesA = 1.4;
double gamaSpeciesB = 1.3;
double molecularWeightSpeciesA = 29.0;
double molecularWeightSpeciesB = 30.0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0;
#########################################################################
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
#########################################################################
# High Order Struct Solver #
#########################################################################
// ifvfd:
// isFVMOrFDM:
// 0 -- NSSolverStruct using Finite Volume Method.
// 1 -- NSSolverStruct using Finite Differ Method.
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// -- "roe", "steger".
// structhighordergradient:
// -- "conservation", "chain_rule".
int ifvfd = 0;
int isFVMOrFDM = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6;
@ -885,8 +1116,12 @@ int allReduceStep = 1;
// codeOfOversetGrid: Overlapping(overset) grid or not.
// 0 -- NON-overlapping grid.
// 1 -- Overlapping grid.
// oversetInterpolationMethod: the method of overset interpolation while field simulation
// 0 -- set the acceptor cell value by donor cell value.
// 1 -- set the acceptor cell value by distance weight of donor cell value.
int codeOfOversetGrid = 0;
int codeOfOversetSlipGrid = 0;
int oversetInterpolationMethod = 0;
int readOversetFileOrNot = 0;
int symetryOrNot = 0;
int readInAuxiliaryInnerGrid = 1;
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
string auxiliaryInnerGrid2 = "";
string oversetGridFileName = "./grid/overlap.ovs";
string oversetGridFileName = "./grid/iblank.ovs";
double walldistMainZone = 1.0
double toleranceForOversetSearch = 1.0e-3;
double toleranceForOversetBox = 1.0e-3;
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
int numberOfMovingBodies = 2;
// ----------------- ALE configuration ------------------------------
int codeOfAleModel = 1;
int aleStartStrategy = -1;
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
int strategyForGCLSource = 0; //0-present; 1-Ahn;
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
int methodForKineticEquation = 0;
double relaxParameterOfKinetic = 1.0;
#########################################################################
# motive information #
#########################################################################
int numberOfMovingBodies = 1;
############################## body0 ##############################
//mass of parts
double mass_0 = 1.0;
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
//initial six DOF position information of parts. xc yc zc
double massCenter_0[] = 0.0 , 0.0, 0.0;
//initial six DOF position information of parts. angleX angleY angleZ
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
//initial six DOF move information of parts. vc vy vz
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
//initial six DOF move information of parts. omigX omigY omigZ
double angularVelocity_0[] = 0.0, 0.0, 0.0;
//the object that the parts belong to.
int fartherIndex_0 = -1;
//the assembly position of the parts. xc yc zc angleX angleY angleZ
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
//the move pattern of the parts.
// -1 given motion partten.
// 0 still.
// 1 six DOF motion.
// 2 three DOF motion.
// 11 X-axis forced motion.
// 12 Y-axis forced motion.
// 13 Z-axis forced motion.
// 14 forced pitch motion.
// 15 forced yaw motion.
// 16 forced roll motion.
int RBDMethod_0 = 0;
double amplitude_0 = 0.0;
double reduceFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
//additional force (system axis) fX fY fZ
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
//additional moment of Force (system axis) mX mY mZ
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
//the deformation method of the parts.
int morphing_0 = 0;
// post indentify
int integralOrder = 4;
// ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0;
//@double refReNumber = 2.329418E08;
//@double refDimensionalTemperature = 288.144;
//@double refDimensionalPressure = 1.01313E05;
//@double height = -0.001;
//@double refReNumber = 6.5e6;
//@double refDimensionalTemperature = 288.15;
//@double freestream_vibration_temperature = 300.00;
//@double refDimensionalPressure = 0;
//@double height = 0;
//@int nsubsonicInlet = 0;
//@int nsubsonicOutlet = 0;
//@string inLetFileName = "./bin/subsonicInlet.hypara";
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
//@double refDimensionalVelocity = 0;
//@double refDimensionalDensity = 0;
#########################################################################
# Old Parameter #

6
B10_ThreeD_CompRamp-16_SA_Unstruct_1CPU/bin/cfd_para_supersonic.hypara
View File

@ -59,9 +59,9 @@ double refDimensionalTemperature = 102.1;
double gridScaleFactor = 1.0;
double forceRefenenceLengthSpanWise = 0.026; // unit of meter.
double forceRefenenceLength = 1.0; // unit of meter.
double forceRefenenceArea = 1.0; // unit of meter^2.
double forceReferenceLengthSpanWise = 0.026; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.

379
B11_ThreeD_DLR-GK01_Ma7_SA_Unstruct_8CPU/bin/cfd_para.hypara
View File

@ -21,6 +21,7 @@
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
// 2 -- Grid refinement.
// 3 -- Grid merging, merge two blocks into one block.
// 4 -- Grid deformation, achieve unstructured grid deformation.
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
// multiblock: Multi-block grid or not, only for structured grid conversion.
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
//-----------------------------------------------------------------------
// from_gfile: path of original data file for unstructure grid convert from.
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
int numberOfGridFile = 1;
string from_gfile = "./grid/rae2822_hybrid2d.cas";
string from_gfile1= "";
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
// ----------------- some advanced choices ------------------------------
// iunsteady: The Grid is for unsteady simulation or not.
int iunsteady = 0;
int iale = 0;
int codeOfAleModel = 0;
// fileformat: Ustar Grid file format.
@ -122,15 +125,38 @@ int isDeform = 0;
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
int projectOrgPoint = 0; // if project original wall points.
// ----------------- Grid Deform Parameters -----------------------------
// deformationMethod: Grid Deform.
// 1 -- SPRING.
// 2 -- RBF.
// stationalGridFile: Original grid file.
// visualFileName : The visualization file path of deform grid.
// nDeformStep : The max deform step.
// flapAngle : The max flap angle.
// rotatePostionZ : Rotate postion.
// rotatePostionY : Rotate postion.
// gridSlice : If dump slice grid.
// sliceAxis : Grid slice axis.
// slicePosition : Grid slice position.
int nDeformStep = 40;
double flapAngle = 10.0;
double rotatePostionZ = 4.00003;
double rotatePostionY = 3.05;
int deformationMethod = 2;
string stationalGridFile = "./grid/Segment2Brid.fts";
string visualFileName = "./results/deformedGrid.dat"
int gridSlice = 1;
int sliceAxis = 1;
double slicePosition = 13;
// ----------------- RBF Parameters -------------------------------------
// symmetryPlane: Which symmetry plane is used in the mesh.
// 0 -- without symmetry.
// 1 -- plane of x=0.
// 2 -- plane of y=0.
// 3 -- plane of z=0.
int numberOfReferenceCP = 10;
double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// numberOfReferenceCP : Number of reference Control Points.
// influencePara : The RBF influence radius parameter.
int numberOfReferenceCP = 40;
double influencePara = 25.0;
// ----------------- Periodic Parameters --------------------------------
// Notice: Rotational periodicity only support rotation along the X axis!
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
// translationLength[]: The relative distance between two periodic face
which only support one direction.
// rotationAngle: The relative angle between two periodic face.
which is recorded in degrees.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
// 0 -- Interface. (default)
// 1 -- Physical boundary condition, used in Hybrid solver.
// 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.
// parallelPartitionMethod: 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.
// 2 -- Using Metis for homogeneous MPI.
// 3 -- using METIS partition for homogeneous OpenMP.
@ -238,6 +269,8 @@ int compressible = 1;
// 1 -- the flight conditions.
// 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions.
// 4 -- the condition that the velocity, temperature and density are given.
// 5 -- the condition that the velocity, temperature and pressure are given.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -251,10 +284,12 @@ int compressible = 1;
// 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.
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, 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
// condition is radiation equilibrium temperature, and 0.8 is the default value.
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
double refMachNumber = 0.73;
double attackd = 2.79;
@ -263,7 +298,7 @@ double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 6.5e6;
double refDimensionalTemperature = 288.15;
double freestream_vibration_temperature = 10000.00;
double freestream_vibration_temperature = 300.00;
//int inflowParaType = 1;
//double height = 0.001;
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
//double refDimensionalTemperature = 288.144;
//double refDimensionalPressure = 1.01313E05;
//The velocity, temperature and density are fixed.
//int inflowParaType = 4;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalDensity = 1.0e3;
//The velocity, temperature and pressure are fixed.
//int inflowParaType = 5;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalPressure = 1.0e5;
//The MachNumber, temperature and pressure are fixed.
//int inflowParaType = 6;
//double refDimensionalTemperature = 293;
//double refDimensionalPressure = 8886.06;
double wallTemperature = -1.0;
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.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.
double refMolecularWeight = 28.9644; // unit of g/mol.
//-----------------------------------------------------------------------
# Spatial Discretisation #
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
// Using this when solve structered grid or hybrid.
// -- "vanleer", "steger", "hlle", "lax_f".
// -- "roe", "modified_roe".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
// str_limiter_name: Limiter of struct grid.
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
// -- "nolim", no limiter.
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod".
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
// -- "nolim", no limiter.
// uns_vis_name: Discretisation method of viscous term.
// -- "std", "test", "aver", "new1", "new2".
// uns_gradient: Gradient reconstruction method.
// gradientName: Gradient reconstruction method.
// -- "default", "ggcell", "ggnode", "lsq".
// ivencat: Variation of vencat limiter.
// 0 -- org method, it is independent of grid scale.
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
// 1 -- unsteay.
// 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.
// ifStaticsFlowField: Statistical variables for DES simulation.
// ifStaticsFlowField: Statistical variables for unsteady simulation.
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
// startStatisticStep: Outer step when start statistics.
// when the value is larger than "maxSimuStep", it is useless.
// statisticalTimePeriod: Used as time period of statistic analysis.
// when the value is negative, time period is treated as infinite.
// statisticMethod: Statistic reynolds stress method.
0 --tau = <q^2> - <q>^2
1 --tau = <u'u'>
// min_sub_iter: The min sub iteration of unsteady simulation.
// max_sub_iter: The max sub iteration of unsteady simulation.
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
@ -454,7 +511,10 @@ int iunsteady = 0;
double physicalTimeStep = 0.01;
int ifStartFromSteadyResults = 0;
int ifStaticsFlowField = 0;
int ifStaticsReynoldsStress = 0;
int startStatisticStep = 800000;
double statisticalTimePeriod = -1.0;
int statisticMethod = 0;
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
int methodOfDualTime = 3;
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
double csrv = 2.0;
double timemax = 1.0e10;
double dtsave = -1.0;
int codeOfAleModel = 0;
int aleStartStrategy = -1;
int maxale = 10;
double dtau = 0.001;
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
int numberOfGridGroups = 1;
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
string wallTemperaturefile= "";
int walldistMethod = 1;
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt";
string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string samplefile = "results/sample.dat";
int nDumpSurfaceInfo = 0;
string wall_varfile = "";
string jetDefineFile = "bin/jet.hypara";
string overset_gridfile = "results/iblank.ovs";
string sixDofFileName = "results/sixDofInfo.dat";
string derivativeFileName = "results/identify.dat";
string hysteresisFileName = "results/force_beta.plt";
int plotFieldType = 0;
@ -554,6 +614,11 @@ int plotFieldType = 0;
int visualfileType = 1;
// samplefileMode: The dump mode of sample file.
// 0 -- dump out every probe/line/surface data for all step intervals.
// 1 -- dump out all probe/line/surface data for every step intervals.
int samplefileMode = 0;
// visualSlice: The slice of tecflow.
// 0 -- Do not save slice data.
// 1 -- comput and save it to sliceFile.
@ -567,11 +632,13 @@ int visualSlice = 0;
int sliceAxis = 1;
double slicePostion = -0.5;
string sliceFile = "results/Slice.plt";
int dumpWallFaceCenter = 0;
// min-max box of the visual block.
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
double upperPlotFieldBox[] = [1.0 1.0 1.0];
//-----------the optional parameters list for the flow field output----------------
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- 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), iblank(81).
// -- specific heat ratio(gama, 56)
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
// Variables order must from small to big.
//-----------the optional parameters list for the wall boundary condition----------------
// nVisualWallVariables: The number of visual variables on wall.
// visualWallVariables : dumped variable types, listed as following:
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -overlap iblank(iblank, 81)
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
// dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate.
int dumpStandardModel = 0;
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
int turbInterval = 1;
int turbOrderStruct = 2;
int kindOfTurbSource = 0;
int mod_turb_res = 0;
double turb_relax = 1.0;
@ -652,6 +736,10 @@ double muoo = 3.0;
double kwoo = 5.0;
int transitionType = 0;
double turbIntensity = -1.0;
int freeturbIntensitySRModify = 0;
double freeDecayXLocation = 0.0;
int compressibleCorrection = 0;
int transitionMaFix = 1;
# maximum eddy viscosity (myt/my) max.
double eddyViscosityLimit = 1.0e10;
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
# LES Parameter #
//-----------------------------------------------------------------------
// iLES: Create LESSolver or not.
// >= 1 - Create LESSolver;
// < 1 - not.
// == 1 - Create LESSolver;
// != 1 - not.
// amplitudeofDisturb: Amplitude of adding disturb.
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
// iterdisturb: Add random disturb in every sub-iter or only first sub-iter.
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
// utau: friction velocity, using in DNSDisturb.
// sgsmodel: subgrid scale model.
// = "smagorinsky";
// = "dsm";
// = "wale".
// = "dsmCom";
// = "wale";
// = "sigma".
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
// = 2 - pow(deltai * deltaj *deltak, 1/3);
// = 3 - Devloped by Scotti.
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
int deltaFunctionType = 2;
int wallDampingFunctionType = 1;
int turbViscousCutType = 2;
double smagConstant = 0.135;
double smagConstant = 0.1;
double isotropicConstant = 0.0;
double waleConstant = 0.6;
double sigmaConstant = 1.35;
int filterDirection[] = [1, 1, 0];
int averageDirection[] = [0, 0, 0];
double testFilterScale = 2.0;
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
// nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D.
// 5 -- for 3D.
// nGasModel: The type of gas.
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
// Otherwise, the pure gas with one component is used for perfect gas.
// 0 -- Earth gas.
// 1 -- Mars gas.
// 2 -- Argon.
// 3 -- Nitrogen.
// nEnergyRecycle: The type of EnergyModel Recycle.
// 0 -- not used .
// 1 -- used.
// nDensityModify: The type of densitymodify.
// 0 -- not used.
// 1 -- used.
// nchem:
// 0 -- without chemical reaction flow.
// 1 -- the chemical reaction flow is considered.
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
// 0 -- perfect gas.
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
// the value equals to or is greater than 1, and 3 is for default value.
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
// the value equals to or is greater than 1, and 3 is for default value.
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
// the value equals to or is greater than 1, and 3 is for default value.
// nSlipBCModel : The computational model of slip boundary conditions.
// 0 -- no slip.
// 1 -- the conventional Maxwell slip conditions.
// 2 -- the Gokcen slip conditions.
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
// 4 -- the Kogan simplified slip conditions.
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
// nchemsrc:
// 0 -- the source terms are not computed.
// 1 -- the source terms are computed.
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
// 1 -- One-temperature model.
// 2 -- Two-temperature model.
// 3 -- Three-temperature model.
// nTEnergyModel: the method to computing temperature energy model.
// 0 -- the energy term is computed using the conventional method.
// 1 -- the energy term is computed using the curve fitting method.
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
// catalyticCoef:
// 0.0 -- full non-catalytic wall boundary condition.
// 1.0 -- full catalytic wall boundary condition.
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
// nTemperatureJump : the method to calculate the temperature jump.
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
// 1.0 -- proposed by Maxwell.
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
// 1.146 -- proposed for an additional "fictitious" velocity slip.
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
// 0 -- not freeze, the chemical reaction sources will be calculated.
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
// nDebug: cout the Wrong place and abort
// 0 -- not used.
// 1 -- used.
// nSpeciesLimit: limitter of gas species
// 0 -- not used.
// 1 -- used.
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
// 0 -- method 0.
// 1 -- method 1.
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
// 0 -- not used.
// 1 -- used.
// nChemcalSourceModified: Modified on ChemcalSource
// 0 -- not used.
// 1 -- used.
// nAblation:
// 0 -- The wall ablation is not computed.
// 1 -- The wall ablation is computed.
// isInjection:
// 0 -- The injection velocity of ablation wall is not computed.
// 1 -- The injection velocity of ablation wall is computed.
// nViscosityModel:
// 0 -- Blottner fitting method.
// 1 -- Gupta fitting method.
// nSutherland:
// 0 -- stands for selecting the Blotter curve fits mode.
// 1 -- stands for Sutherland relation.
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
// "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.
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
// 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.
@ -758,6 +935,10 @@ int dg_high_order = 0;
int iapplication = 0;
int iCodeBranch = 0;
int nm = 5;
int nEquilibriumGas = 0;
int nPCWCycleStep = 3;
int nRETCycleStep = 3;
int nSLIPCycleStep= 3;
double refGama = 1.4;
double prl = 0.72;
@ -770,23 +951,73 @@ int nchem = 0;
int nchemsrc = 1;
int nchemrad = 1;
int ntmodel = 1;
int nChemicalFlowStep = 0;
int nEnergyRecycle = 0;
int nSlipBCModel = 0;
int nDensityModify = 1;
int nTEnergyModel = 0;
int nMeanFreePathType = 0;
int nIsChemicalFreeze = 0;
int nIsSuperCatalytic = 1;
int nTemperatureJump = 0;
double parkVDPower = 0.6;
double catalyticCoef = 0.0;
double sigmaVelocity = 1.0;
double sigmaTemperature = 1.0;
double sigmaMassFraction = 1.0;
double velocitySlipCorrectConstant = 1.0;
double chemicalRelaxCorf = 1.0;
double chemicalSpectrumRadiusCoef = 1.0;
double viscousSpectrumRadiusCoef = 1.0;
double inviscidSpectrumRadiusCoef = 1.0;
double staticPressureRelaxCorf = 1.0;
double veTemperatureMin = 30.0;
int nDebug = 0;
int nSpeciesLimit = 0;
int nTurblenceForChemical = 0;
int nViscosityFluxSublevelModified = 0 ;
int nChemcalSourceModified = 0;
int nAblation = 0;
int isInjection = 0;
int nViscosityModel = 0;
int nMarsModel = 0;
string gasfile = "DK5";
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
string speciesName = "O, O2, NO, N, N2";
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
//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, 0.233, 0.0, 0.0, 0.0, 0.767, 0.0";
//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, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Mars-Pa8";
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
//string gasfile = "DK7";
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Combustion-12";
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
//string gasfile = "Gas-Mixture";
//string speciesName ="SpeciesA, SpeciesB";
//string initMassFraction = "1.0, 0.0";
int nSutherland = 0;
double gamaSpeciesA = 1.4;
double gamaSpeciesB = 1.3;
double molecularWeightSpeciesA = 29.0;
double molecularWeightSpeciesB = 30.0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0;
#########################################################################
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
#########################################################################
# High Order Struct Solver #
#########################################################################
// ifvfd:
// isFVMOrFDM:
// 0 -- NSSolverStruct using Finite Volume Method.
// 1 -- NSSolverStruct using Finite Differ Method.
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// -- "roe", "steger".
// structhighordergradient:
// -- "conservation", "chain_rule".
int ifvfd = 0;
int isFVMOrFDM = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6;
@ -885,8 +1116,12 @@ int allReduceStep = 1;
// codeOfOversetGrid: Overlapping(overset) grid or not.
// 0 -- NON-overlapping grid.
// 1 -- Overlapping grid.
// oversetInterpolationMethod: the method of overset interpolation while field simulation
// 0 -- set the acceptor cell value by donor cell value.
// 1 -- set the acceptor cell value by distance weight of donor cell value.
int codeOfOversetGrid = 0;
int codeOfOversetSlipGrid = 0;
int oversetInterpolationMethod = 0;
int readOversetFileOrNot = 0;
int symetryOrNot = 0;
int readInAuxiliaryInnerGrid = 1;
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
string auxiliaryInnerGrid2 = "";
string oversetGridFileName = "./grid/overlap.ovs";
string oversetGridFileName = "./grid/iblank.ovs";
double walldistMainZone = 1.0
double toleranceForOversetSearch = 1.0e-3;
double toleranceForOversetBox = 1.0e-3;
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
int numberOfMovingBodies = 2;
// ----------------- ALE configuration ------------------------------
int codeOfAleModel = 1;
int aleStartStrategy = -1;
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
int strategyForGCLSource = 0; //0-present; 1-Ahn;
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
int methodForKineticEquation = 0;
double relaxParameterOfKinetic = 1.0;
#########################################################################
# motive information #
#########################################################################
int numberOfMovingBodies = 1;
############################## body0 ##############################
//mass of parts
double mass_0 = 1.0;
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
//initial six DOF position information of parts. xc yc zc
double massCenter_0[] = 0.0 , 0.0, 0.0;
//initial six DOF position information of parts. angleX angleY angleZ
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
//initial six DOF move information of parts. vc vy vz
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
//initial six DOF move information of parts. omigX omigY omigZ
double angularVelocity_0[] = 0.0, 0.0, 0.0;
//the object that the parts belong to.
int fartherIndex_0 = -1;
//the assembly position of the parts. xc yc zc angleX angleY angleZ
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
//the move pattern of the parts.
// -1 given motion partten.
// 0 still.
// 1 six DOF motion.
// 2 three DOF motion.
// 11 X-axis forced motion.
// 12 Y-axis forced motion.
// 13 Z-axis forced motion.
// 14 forced pitch motion.
// 15 forced yaw motion.
// 16 forced roll motion.
int RBDMethod_0 = 0;
double amplitude_0 = 0.0;
double reduceFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
//additional force (system axis) fX fY fZ
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
//additional moment of Force (system axis) mX mY mZ
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
//the deformation method of the parts.
int morphing_0 = 0;
// post indentify
int integralOrder = 4;
// ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0;
//@double refReNumber = 2.329418E08;
//@double refDimensionalTemperature = 288.144;
//@double refDimensionalPressure = 1.01313E05;
//@double height = -0.001;
//@double refReNumber = 6.5e6;
//@double refDimensionalTemperature = 288.15;
//@double freestream_vibration_temperature = 300.00;
//@double refDimensionalPressure = 0;
//@double height = 0;
//@int nsubsonicInlet = 0;
//@int nsubsonicOutlet = 0;
//@string inLetFileName = "./bin/subsonicInlet.hypara";
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
//@double refDimensionalVelocity = 0;
//@double refDimensionalDensity = 0;
#########################################################################
# Old Parameter #

6
B11_ThreeD_DLR-GK01_Ma7_SA_Unstruct_8CPU/bin/cfd_para_hypersonic.hypara
View File

@ -61,9 +61,9 @@ double freestream_vibration_temperature = 10000.0;
double gridScaleFactor = 1.0;
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
double forceRefenenceLength = 1.0; // unit of meter.
double forceRefenenceArea = 1.0; // unit of meter^2.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.

379
B12_ThreeD_DoubleEllipse_Laminar_Unstruct_4CPU/bin/cfd_para.hypara
View File

@ -21,6 +21,7 @@
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
// 2 -- Grid refinement.
// 3 -- Grid merging, merge two blocks into one block.
// 4 -- Grid deformation, achieve unstructured grid deformation.
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
// multiblock: Multi-block grid or not, only for structured grid conversion.
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
//-----------------------------------------------------------------------
// from_gfile: path of original data file for unstructure grid convert from.
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
int numberOfGridFile = 1;
string from_gfile = "./grid/rae2822_hybrid2d.cas";
string from_gfile1= "";
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
// ----------------- some advanced choices ------------------------------
// iunsteady: The Grid is for unsteady simulation or not.
int iunsteady = 0;
int iale = 0;
int codeOfAleModel = 0;
// fileformat: Ustar Grid file format.
@ -122,15 +125,38 @@ int isDeform = 0;
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
int projectOrgPoint = 0; // if project original wall points.
// ----------------- Grid Deform Parameters -----------------------------
// deformationMethod: Grid Deform.
// 1 -- SPRING.
// 2 -- RBF.
// stationalGridFile: Original grid file.
// visualFileName : The visualization file path of deform grid.
// nDeformStep : The max deform step.
// flapAngle : The max flap angle.
// rotatePostionZ : Rotate postion.
// rotatePostionY : Rotate postion.
// gridSlice : If dump slice grid.
// sliceAxis : Grid slice axis.
// slicePosition : Grid slice position.
int nDeformStep = 40;
double flapAngle = 10.0;
double rotatePostionZ = 4.00003;
double rotatePostionY = 3.05;
int deformationMethod = 2;
string stationalGridFile = "./grid/Segment2Brid.fts";
string visualFileName = "./results/deformedGrid.dat"
int gridSlice = 1;
int sliceAxis = 1;
double slicePosition = 13;
// ----------------- RBF Parameters -------------------------------------
// symmetryPlane: Which symmetry plane is used in the mesh.
// 0 -- without symmetry.
// 1 -- plane of x=0.
// 2 -- plane of y=0.
// 3 -- plane of z=0.
int numberOfReferenceCP = 10;
double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// numberOfReferenceCP : Number of reference Control Points.
// influencePara : The RBF influence radius parameter.
int numberOfReferenceCP = 40;
double influencePara = 25.0;
// ----------------- Periodic Parameters --------------------------------
// Notice: Rotational periodicity only support rotation along the X axis!
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
// translationLength[]: The relative distance between two periodic face
which only support one direction.
// rotationAngle: The relative angle between two periodic face.
which is recorded in degrees.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
// 0 -- Interface. (default)
// 1 -- Physical boundary condition, used in Hybrid solver.
// 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.
// parallelPartitionMethod: 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.
// 2 -- Using Metis for homogeneous MPI.
// 3 -- using METIS partition for homogeneous OpenMP.
@ -238,6 +269,8 @@ int compressible = 1;
// 1 -- the flight conditions.
// 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions.
// 4 -- the condition that the velocity, temperature and density are given.
// 5 -- the condition that the velocity, temperature and pressure are given.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -251,10 +284,12 @@ int compressible = 1;
// 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.
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, 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
// condition is radiation equilibrium temperature, and 0.8 is the default value.
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
double refMachNumber = 0.73;
double attackd = 2.79;
@ -263,7 +298,7 @@ double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 6.5e6;
double refDimensionalTemperature = 288.15;
double freestream_vibration_temperature = 10000.00;
double freestream_vibration_temperature = 300.00;
//int inflowParaType = 1;
//double height = 0.001;
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
//double refDimensionalTemperature = 288.144;
//double refDimensionalPressure = 1.01313E05;
//The velocity, temperature and density are fixed.
//int inflowParaType = 4;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalDensity = 1.0e3;
//The velocity, temperature and pressure are fixed.
//int inflowParaType = 5;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalPressure = 1.0e5;
//The MachNumber, temperature and pressure are fixed.
//int inflowParaType = 6;
//double refDimensionalTemperature = 293;
//double refDimensionalPressure = 8886.06;
double wallTemperature = -1.0;
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.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.
double refMolecularWeight = 28.9644; // unit of g/mol.
//-----------------------------------------------------------------------
# Spatial Discretisation #
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
// Using this when solve structered grid or hybrid.
// -- "vanleer", "steger", "hlle", "lax_f".
// -- "roe", "modified_roe".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
// str_limiter_name: Limiter of struct grid.
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
// -- "nolim", no limiter.
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod".
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
// -- "nolim", no limiter.
// uns_vis_name: Discretisation method of viscous term.
// -- "std", "test", "aver", "new1", "new2".
// uns_gradient: Gradient reconstruction method.
// gradientName: Gradient reconstruction method.
// -- "default", "ggcell", "ggnode", "lsq".
// ivencat: Variation of vencat limiter.
// 0 -- org method, it is independent of grid scale.
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
// 1 -- unsteay.
// 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.
// ifStaticsFlowField: Statistical variables for DES simulation.
// ifStaticsFlowField: Statistical variables for unsteady simulation.
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
// startStatisticStep: Outer step when start statistics.
// when the value is larger than "maxSimuStep", it is useless.
// statisticalTimePeriod: Used as time period of statistic analysis.
// when the value is negative, time period is treated as infinite.
// statisticMethod: Statistic reynolds stress method.
0 --tau = <q^2> - <q>^2
1 --tau = <u'u'>
// min_sub_iter: The min sub iteration of unsteady simulation.
// max_sub_iter: The max sub iteration of unsteady simulation.
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
@ -454,7 +511,10 @@ int iunsteady = 0;
double physicalTimeStep = 0.01;
int ifStartFromSteadyResults = 0;
int ifStaticsFlowField = 0;
int ifStaticsReynoldsStress = 0;
int startStatisticStep = 800000;
double statisticalTimePeriod = -1.0;
int statisticMethod = 0;
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
int methodOfDualTime = 3;
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
double csrv = 2.0;
double timemax = 1.0e10;
double dtsave = -1.0;
int codeOfAleModel = 0;
int aleStartStrategy = -1;
int maxale = 10;
double dtau = 0.001;
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
int numberOfGridGroups = 1;
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
string wallTemperaturefile= "";
int walldistMethod = 1;
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt";
string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string samplefile = "results/sample.dat";
int nDumpSurfaceInfo = 0;
string wall_varfile = "";
string jetDefineFile = "bin/jet.hypara";
string overset_gridfile = "results/iblank.ovs";
string sixDofFileName = "results/sixDofInfo.dat";
string derivativeFileName = "results/identify.dat";
string hysteresisFileName = "results/force_beta.plt";
int plotFieldType = 0;
@ -554,6 +614,11 @@ int plotFieldType = 0;
int visualfileType = 1;
// samplefileMode: The dump mode of sample file.
// 0 -- dump out every probe/line/surface data for all step intervals.
// 1 -- dump out all probe/line/surface data for every step intervals.
int samplefileMode = 0;
// visualSlice: The slice of tecflow.
// 0 -- Do not save slice data.
// 1 -- comput and save it to sliceFile.
@ -567,11 +632,13 @@ int visualSlice = 0;
int sliceAxis = 1;
double slicePostion = -0.5;
string sliceFile = "results/Slice.plt";
int dumpWallFaceCenter = 0;
// min-max box of the visual block.
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
double upperPlotFieldBox[] = [1.0 1.0 1.0];
//-----------the optional parameters list for the flow field output----------------
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- 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), iblank(81).
// -- specific heat ratio(gama, 56)
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
// Variables order must from small to big.
//-----------the optional parameters list for the wall boundary condition----------------
// nVisualWallVariables: The number of visual variables on wall.
// visualWallVariables : dumped variable types, listed as following:
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -overlap iblank(iblank, 81)
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
// dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate.
int dumpStandardModel = 0;
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
int turbInterval = 1;
int turbOrderStruct = 2;
int kindOfTurbSource = 0;
int mod_turb_res = 0;
double turb_relax = 1.0;
@ -652,6 +736,10 @@ double muoo = 3.0;
double kwoo = 5.0;
int transitionType = 0;
double turbIntensity = -1.0;
int freeturbIntensitySRModify = 0;
double freeDecayXLocation = 0.0;
int compressibleCorrection = 0;
int transitionMaFix = 1;
# maximum eddy viscosity (myt/my) max.
double eddyViscosityLimit = 1.0e10;
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
# LES Parameter #
//-----------------------------------------------------------------------
// iLES: Create LESSolver or not.
// >= 1 - Create LESSolver;
// < 1 - not.
// == 1 - Create LESSolver;
// != 1 - not.
// amplitudeofDisturb: Amplitude of adding disturb.
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
// iterdisturb: Add random disturb in every sub-iter or only first sub-iter.
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
// utau: friction velocity, using in DNSDisturb.
// sgsmodel: subgrid scale model.
// = "smagorinsky";
// = "dsm";
// = "wale".
// = "dsmCom";
// = "wale";
// = "sigma".
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
// = 2 - pow(deltai * deltaj *deltak, 1/3);
// = 3 - Devloped by Scotti.
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
int deltaFunctionType = 2;
int wallDampingFunctionType = 1;
int turbViscousCutType = 2;
double smagConstant = 0.135;
double smagConstant = 0.1;
double isotropicConstant = 0.0;
double waleConstant = 0.6;
double sigmaConstant = 1.35;
int filterDirection[] = [1, 1, 0];
int averageDirection[] = [0, 0, 0];
double testFilterScale = 2.0;
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
// nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D.
// 5 -- for 3D.
// nGasModel: The type of gas.
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
// Otherwise, the pure gas with one component is used for perfect gas.
// 0 -- Earth gas.
// 1 -- Mars gas.
// 2 -- Argon.
// 3 -- Nitrogen.
// nEnergyRecycle: The type of EnergyModel Recycle.
// 0 -- not used .
// 1 -- used.
// nDensityModify: The type of densitymodify.
// 0 -- not used.
// 1 -- used.
// nchem:
// 0 -- without chemical reaction flow.
// 1 -- the chemical reaction flow is considered.
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
// 0 -- perfect gas.
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
// the value equals to or is greater than 1, and 3 is for default value.
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
// the value equals to or is greater than 1, and 3 is for default value.
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
// the value equals to or is greater than 1, and 3 is for default value.
// nSlipBCModel : The computational model of slip boundary conditions.
// 0 -- no slip.
// 1 -- the conventional Maxwell slip conditions.
// 2 -- the Gokcen slip conditions.
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
// 4 -- the Kogan simplified slip conditions.
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
// nchemsrc:
// 0 -- the source terms are not computed.
// 1 -- the source terms are computed.
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
// 1 -- One-temperature model.
// 2 -- Two-temperature model.
// 3 -- Three-temperature model.
// nTEnergyModel: the method to computing temperature energy model.
// 0 -- the energy term is computed using the conventional method.
// 1 -- the energy term is computed using the curve fitting method.
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
// catalyticCoef:
// 0.0 -- full non-catalytic wall boundary condition.
// 1.0 -- full catalytic wall boundary condition.
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
// nTemperatureJump : the method to calculate the temperature jump.
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
// 1.0 -- proposed by Maxwell.
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
// 1.146 -- proposed for an additional "fictitious" velocity slip.
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
// 0 -- not freeze, the chemical reaction sources will be calculated.
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
// nDebug: cout the Wrong place and abort
// 0 -- not used.
// 1 -- used.
// nSpeciesLimit: limitter of gas species
// 0 -- not used.
// 1 -- used.
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
// 0 -- method 0.
// 1 -- method 1.
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
// 0 -- not used.
// 1 -- used.
// nChemcalSourceModified: Modified on ChemcalSource
// 0 -- not used.
// 1 -- used.
// nAblation:
// 0 -- The wall ablation is not computed.
// 1 -- The wall ablation is computed.
// isInjection:
// 0 -- The injection velocity of ablation wall is not computed.
// 1 -- The injection velocity of ablation wall is computed.
// nViscosityModel:
// 0 -- Blottner fitting method.
// 1 -- Gupta fitting method.
// nSutherland:
// 0 -- stands for selecting the Blotter curve fits mode.
// 1 -- stands for Sutherland relation.
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
// "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.
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
// 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.
@ -758,6 +935,10 @@ int dg_high_order = 0;
int iapplication = 0;
int iCodeBranch = 0;
int nm = 5;
int nEquilibriumGas = 0;
int nPCWCycleStep = 3;
int nRETCycleStep = 3;
int nSLIPCycleStep= 3;
double refGama = 1.4;
double prl = 0.72;
@ -770,23 +951,73 @@ int nchem = 0;
int nchemsrc = 1;
int nchemrad = 1;
int ntmodel = 1;
int nChemicalFlowStep = 0;
int nEnergyRecycle = 0;
int nSlipBCModel = 0;
int nDensityModify = 1;
int nTEnergyModel = 0;
int nMeanFreePathType = 0;
int nIsChemicalFreeze = 0;
int nIsSuperCatalytic = 1;
int nTemperatureJump = 0;
double parkVDPower = 0.6;
double catalyticCoef = 0.0;
double sigmaVelocity = 1.0;
double sigmaTemperature = 1.0;
double sigmaMassFraction = 1.0;
double velocitySlipCorrectConstant = 1.0;
double chemicalRelaxCorf = 1.0;
double chemicalSpectrumRadiusCoef = 1.0;
double viscousSpectrumRadiusCoef = 1.0;
double inviscidSpectrumRadiusCoef = 1.0;
double staticPressureRelaxCorf = 1.0;
double veTemperatureMin = 30.0;
int nDebug = 0;
int nSpeciesLimit = 0;
int nTurblenceForChemical = 0;
int nViscosityFluxSublevelModified = 0 ;
int nChemcalSourceModified = 0;
int nAblation = 0;
int isInjection = 0;
int nViscosityModel = 0;
int nMarsModel = 0;
string gasfile = "DK5";
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
string speciesName = "O, O2, NO, N, N2";
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
//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, 0.233, 0.0, 0.0, 0.0, 0.767, 0.0";
//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, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Mars-Pa8";
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
//string gasfile = "DK7";
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Combustion-12";
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
//string gasfile = "Gas-Mixture";
//string speciesName ="SpeciesA, SpeciesB";
//string initMassFraction = "1.0, 0.0";
int nSutherland = 0;
double gamaSpeciesA = 1.4;
double gamaSpeciesB = 1.3;
double molecularWeightSpeciesA = 29.0;
double molecularWeightSpeciesB = 30.0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0;
#########################################################################
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
#########################################################################
# High Order Struct Solver #
#########################################################################
// ifvfd:
// isFVMOrFDM:
// 0 -- NSSolverStruct using Finite Volume Method.
// 1 -- NSSolverStruct using Finite Differ Method.
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// -- "roe", "steger".
// structhighordergradient:
// -- "conservation", "chain_rule".
int ifvfd = 0;
int isFVMOrFDM = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6;
@ -885,8 +1116,12 @@ int allReduceStep = 1;
// codeOfOversetGrid: Overlapping(overset) grid or not.
// 0 -- NON-overlapping grid.
// 1 -- Overlapping grid.
// oversetInterpolationMethod: the method of overset interpolation while field simulation
// 0 -- set the acceptor cell value by donor cell value.
// 1 -- set the acceptor cell value by distance weight of donor cell value.
int codeOfOversetGrid = 0;
int codeOfOversetSlipGrid = 0;
int oversetInterpolationMethod = 0;
int readOversetFileOrNot = 0;
int symetryOrNot = 0;
int readInAuxiliaryInnerGrid = 1;
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
string auxiliaryInnerGrid2 = "";
string oversetGridFileName = "./grid/overlap.ovs";
string oversetGridFileName = "./grid/iblank.ovs";
double walldistMainZone = 1.0
double toleranceForOversetSearch = 1.0e-3;
double toleranceForOversetBox = 1.0e-3;
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
int numberOfMovingBodies = 2;
// ----------------- ALE configuration ------------------------------
int codeOfAleModel = 1;
int aleStartStrategy = -1;
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
int strategyForGCLSource = 0; //0-present; 1-Ahn;
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
int methodForKineticEquation = 0;
double relaxParameterOfKinetic = 1.0;
#########################################################################
# motive information #
#########################################################################
int numberOfMovingBodies = 1;
############################## body0 ##############################
//mass of parts
double mass_0 = 1.0;
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
//initial six DOF position information of parts. xc yc zc
double massCenter_0[] = 0.0 , 0.0, 0.0;
//initial six DOF position information of parts. angleX angleY angleZ
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
//initial six DOF move information of parts. vc vy vz
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
//initial six DOF move information of parts. omigX omigY omigZ
double angularVelocity_0[] = 0.0, 0.0, 0.0;
//the object that the parts belong to.
int fartherIndex_0 = -1;
//the assembly position of the parts. xc yc zc angleX angleY angleZ
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
//the move pattern of the parts.
// -1 given motion partten.
// 0 still.
// 1 six DOF motion.
// 2 three DOF motion.
// 11 X-axis forced motion.
// 12 Y-axis forced motion.
// 13 Z-axis forced motion.
// 14 forced pitch motion.
// 15 forced yaw motion.
// 16 forced roll motion.
int RBDMethod_0 = 0;
double amplitude_0 = 0.0;
double reduceFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
//additional force (system axis) fX fY fZ
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
//additional moment of Force (system axis) mX mY mZ
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
//the deformation method of the parts.
int morphing_0 = 0;
// post indentify
int integralOrder = 4;
// ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0;
//@double refReNumber = 2.329418E08;
//@double refDimensionalTemperature = 288.144;
//@double refDimensionalPressure = 1.01313E05;
//@double height = -0.001;
//@double refReNumber = 6.5e6;
//@double refDimensionalTemperature = 288.15;
//@double freestream_vibration_temperature = 300.00;
//@double refDimensionalPressure = 0;
//@double height = 0;
//@int nsubsonicInlet = 0;
//@int nsubsonicOutlet = 0;
//@string inLetFileName = "./bin/subsonicInlet.hypara";
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
//@double refDimensionalVelocity = 0;
//@double refDimensionalDensity = 0;
#########################################################################
# Old Parameter #

6
B12_ThreeD_DoubleEllipse_Laminar_Unstruct_4CPU/bin/cfd_para_hypersonic.hypara
View File

@ -61,9 +61,9 @@ double freestream_vibration_temperature = 10000.0;
double gridScaleFactor = 1.0;
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
double forceRefenenceLength = 1.0; // unit of meter.
double forceRefenenceArea = 1.0; // unit of meter^2.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.

379
B13_ThreeD_Chnt_SA_Unstruct_100CPU/bin/cfd_para.hypara
View File

@ -21,6 +21,7 @@
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
// 2 -- Grid refinement.
// 3 -- Grid merging, merge two blocks into one block.
// 4 -- Grid deformation, achieve unstructured grid deformation.
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
// multiblock: Multi-block grid or not, only for structured grid conversion.
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
//-----------------------------------------------------------------------
// from_gfile: path of original data file for unstructure grid convert from.
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
int numberOfGridFile = 1;
string from_gfile = "./grid/rae2822_hybrid2d.cas";
string from_gfile1= "";
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
// ----------------- some advanced choices ------------------------------
// iunsteady: The Grid is for unsteady simulation or not.
int iunsteady = 0;
int iale = 0;
int codeOfAleModel = 0;
// fileformat: Ustar Grid file format.
@ -122,15 +125,38 @@ int isDeform = 0;
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
int projectOrgPoint = 0; // if project original wall points.
// ----------------- Grid Deform Parameters -----------------------------
// deformationMethod: Grid Deform.
// 1 -- SPRING.
// 2 -- RBF.
// stationalGridFile: Original grid file.
// visualFileName : The visualization file path of deform grid.
// nDeformStep : The max deform step.
// flapAngle : The max flap angle.
// rotatePostionZ : Rotate postion.
// rotatePostionY : Rotate postion.
// gridSlice : If dump slice grid.
// sliceAxis : Grid slice axis.
// slicePosition : Grid slice position.
int nDeformStep = 40;
double flapAngle = 10.0;
double rotatePostionZ = 4.00003;
double rotatePostionY = 3.05;
int deformationMethod = 2;
string stationalGridFile = "./grid/Segment2Brid.fts";
string visualFileName = "./results/deformedGrid.dat"
int gridSlice = 1;
int sliceAxis = 1;
double slicePosition = 13;
// ----------------- RBF Parameters -------------------------------------
// symmetryPlane: Which symmetry plane is used in the mesh.
// 0 -- without symmetry.
// 1 -- plane of x=0.
// 2 -- plane of y=0.
// 3 -- plane of z=0.
int numberOfReferenceCP = 10;
double influenceRadius = 20;
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
// numberOfReferenceCP : Number of reference Control Points.
// influencePara : The RBF influence radius parameter.
int numberOfReferenceCP = 40;
double influencePara = 25.0;
// ----------------- Periodic Parameters --------------------------------
// Notice: Rotational periodicity only support rotation along the X axis!
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
// 0 -- without Periodic Boundary.
// 1 -- Translational periodicity.
// 2 -- Rotational periodicity.
// translationLength[]: The relative distance between two periodic face
which only support one direction.
// rotationAngle: The relative angle between two periodic face.
which is recorded in degrees.
int periodicType = 0;
double translationLength[] = [0.0,0.0,0.0];
double rotationAngle = 0.0;
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
// 0 -- Interface. (default)
// 1 -- Physical boundary condition, used in Hybrid solver.
// 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.
// parallelPartitionMethod: 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.
// 2 -- Using Metis for homogeneous MPI.
// 3 -- using METIS partition for homogeneous OpenMP.
@ -238,6 +269,8 @@ int compressible = 1;
// 1 -- the flight conditions.
// 2 -- the experiment conditions.
// 3 -- the subsonic boundary conditions.
// 4 -- the condition that the velocity, temperature and density are given.
// 5 -- the condition that the velocity, temperature and pressure are given.
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
@ -251,10 +284,12 @@ int compressible = 1;
// 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.
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, 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
// condition is radiation equilibrium temperature, and 0.8 is the default value.
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
double refMachNumber = 0.73;
double attackd = 2.79;
@ -263,7 +298,7 @@ double angleSlide = 0.00;
int inflowParaType = 0;
double refReNumber = 6.5e6;
double refDimensionalTemperature = 288.15;
double freestream_vibration_temperature = 10000.00;
double freestream_vibration_temperature = 300.00;
//int inflowParaType = 1;
//double height = 0.001;
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
//double refDimensionalTemperature = 288.144;
//double refDimensionalPressure = 1.01313E05;
//The velocity, temperature and density are fixed.
//int inflowParaType = 4;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalDensity = 1.0e3;
//The velocity, temperature and pressure are fixed.
//int inflowParaType = 5;
//double refDimensionalVelocity = 1000.0;
//double refDimensionalPressure = 1.0e5;
//The MachNumber, temperature and pressure are fixed.
//int inflowParaType = 6;
//double refDimensionalTemperature = 293;
//double refDimensionalPressure = 8886.06;
double wallTemperature = -1.0;
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.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 1.0; // unit of meter.
double forceReferenceArea = 1.0; // unit of meter^2.
double TorqueRefX = 0.0; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.
double refMolecularWeight = 28.9644; // unit of g/mol.
//-----------------------------------------------------------------------
# Spatial Discretisation #
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
// Using this when solve structered grid or hybrid.
// -- "vanleer", "steger", "hlle", "lax_f".
// -- "roe", "modified_roe".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
// str_limiter_name: Limiter of struct grid.
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
// -- "nolim", no limiter.
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
// Using this when solve Unstructered grid or hybrid.
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
// uns_limiter_name: Limiter of Unstruct grid.
// -- "barth", "vencat", "vanleer", "minmod".
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
// -- "nolim", no limiter.
// uns_vis_name: Discretisation method of viscous term.
// -- "std", "test", "aver", "new1", "new2".
// uns_gradient: Gradient reconstruction method.
// gradientName: Gradient reconstruction method.
// -- "default", "ggcell", "ggnode", "lsq".
// ivencat: Variation of vencat limiter.
// 0 -- org method, it is independent of grid scale.
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
// 1 -- unsteay.
// 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.
// ifStaticsFlowField: Statistical variables for DES simulation.
// ifStaticsFlowField: Statistical variables for unsteady simulation.
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
// startStatisticStep: Outer step when start statistics.
// when the value is larger than "maxSimuStep", it is useless.
// statisticalTimePeriod: Used as time period of statistic analysis.
// when the value is negative, time period is treated as infinite.
// statisticMethod: Statistic reynolds stress method.
0 --tau = <q^2> - <q>^2
1 --tau = <u'u'>
// min_sub_iter: The min sub iteration of unsteady simulation.
// max_sub_iter: The max sub iteration of unsteady simulation.
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
@ -454,7 +511,10 @@ int iunsteady = 0;
double physicalTimeStep = 0.01;
int ifStartFromSteadyResults = 0;
int ifStaticsFlowField = 0;
int ifStaticsReynoldsStress = 0;
int startStatisticStep = 800000;
double statisticalTimePeriod = -1.0;
int statisticMethod = 0;
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
int methodOfDualTime = 3;
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
double csrv = 2.0;
double timemax = 1.0e10;
double dtsave = -1.0;
int codeOfAleModel = 0;
int aleStartStrategy = -1;
int maxale = 10;
double dtau = 0.001;
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
int numberOfGridGroups = 1;
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
string wallTemperaturefile= "";
int walldistMethod = 1;
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
string visualfile = "results/tecflow.plt";
string wall_aircoefile = "results/wall_aircoef.dat";
string probesflowfile = "results/sample.dat";
string samplefile = "results/sample.dat";
int nDumpSurfaceInfo = 0;
string wall_varfile = "";
string jetDefineFile = "bin/jet.hypara";
string overset_gridfile = "results/iblank.ovs";
string sixDofFileName = "results/sixDofInfo.dat";
string derivativeFileName = "results/identify.dat";
string hysteresisFileName = "results/force_beta.plt";
int plotFieldType = 0;
@ -554,6 +614,11 @@ int plotFieldType = 0;
int visualfileType = 1;
// samplefileMode: The dump mode of sample file.
// 0 -- dump out every probe/line/surface data for all step intervals.
// 1 -- dump out all probe/line/surface data for every step intervals.
int samplefileMode = 0;
// visualSlice: The slice of tecflow.
// 0 -- Do not save slice data.
// 1 -- comput and save it to sliceFile.
@ -567,11 +632,13 @@ int visualSlice = 0;
int sliceAxis = 1;
double slicePostion = -0.5;
string sliceFile = "results/Slice.plt";
int dumpWallFaceCenter = 0;
// min-max box of the visual block.
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
double upperPlotFieldBox[] = [1.0 1.0 1.0];
//-----------the optional parameters list for the flow field output----------------
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
// visualVariables : Variable types dumped, listed as following:
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
// -- 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), iblank(81).
// -- specific heat ratio(gama, 56)
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
// Variables order must from small to big.
//-----------the optional parameters list for the wall boundary condition----------------
// nVisualWallVariables: The number of visual variables on wall.
// visualWallVariables : dumped variable types, listed as following:
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
// -overlap iblank(iblank, 81)
int nVisualVariables = 8;
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
int nVisualWallVariables = 9;
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
// dumpStandardModel: Dump many standard model data.
// 1 -- Turbulent flat plate.
int dumpStandardModel = 0;
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
int turbInterval = 1;
int turbOrderStruct = 2;
int kindOfTurbSource = 0;
int mod_turb_res = 0;
double turb_relax = 1.0;
@ -652,6 +736,10 @@ double muoo = 3.0;
double kwoo = 5.0;
int transitionType = 0;
double turbIntensity = -1.0;
int freeturbIntensitySRModify = 0;
double freeDecayXLocation = 0.0;
int compressibleCorrection = 0;
int transitionMaFix = 1;
# maximum eddy viscosity (myt/my) max.
double eddyViscosityLimit = 1.0e10;
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
# LES Parameter #
//-----------------------------------------------------------------------
// iLES: Create LESSolver or not.
// >= 1 - Create LESSolver;
// < 1 - not.
// == 1 - Create LESSolver;
// != 1 - not.
// amplitudeofDisturb: Amplitude of adding disturb.
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
// iterdisturb: Add random disturb in every sub-iter or only first sub-iter.
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
// utau: friction velocity, using in DNSDisturb.
// sgsmodel: subgrid scale model.
// = "smagorinsky";
// = "dsm";
// = "wale".
// = "dsmCom";
// = "wale";
// = "sigma".
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
// = 2 - pow(deltai * deltaj *deltak, 1/3);
// = 3 - Devloped by Scotti.
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
int deltaFunctionType = 2;
int wallDampingFunctionType = 1;
int turbViscousCutType = 2;
double smagConstant = 0.135;
double smagConstant = 0.1;
double isotropicConstant = 0.0;
double waleConstant = 0.6;
double sigmaConstant = 1.35;
int filterDirection[] = [1, 1, 0];
int averageDirection[] = [0, 0, 0];
double testFilterScale = 2.0;
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
// nm: Equation number of the physics, but is out of commision now.
// 4 -- for 2D.
// 5 -- for 3D.
// nGasModel: The type of gas.
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
// Otherwise, the pure gas with one component is used for perfect gas.
// 0 -- Earth gas.
// 1 -- Mars gas.
// 2 -- Argon.
// 3 -- Nitrogen.
// nEnergyRecycle: The type of EnergyModel Recycle.
// 0 -- not used .
// 1 -- used.
// nDensityModify: The type of densitymodify.
// 0 -- not used.
// 1 -- used.
// nchem:
// 0 -- without chemical reaction flow.
// 1 -- the chemical reaction flow is considered.
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
// 0 -- perfect gas.
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
// the value equals to or is greater than 1, and 3 is for default value.
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
// the value equals to or is greater than 1, and 3 is for default value.
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
// the value equals to or is greater than 1, and 3 is for default value.
// nSlipBCModel : The computational model of slip boundary conditions.
// 0 -- no slip.
// 1 -- the conventional Maxwell slip conditions.
// 2 -- the Gokcen slip conditions.
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
// 4 -- the Kogan simplified slip conditions.
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
// nchemsrc:
// 0 -- the source terms are not computed.
// 1 -- the source terms are computed.
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
// 1 -- One-temperature model.
// 2 -- Two-temperature model.
// 3 -- Three-temperature model.
// nTEnergyModel: the method to computing temperature energy model.
// 0 -- the energy term is computed using the conventional method.
// 1 -- the energy term is computed using the curve fitting method.
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
// catalyticCoef:
// 0.0 -- full non-catalytic wall boundary condition.
// 1.0 -- full catalytic wall boundary condition.
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
// nTemperatureJump : the method to calculate the temperature jump.
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
// 1.0 -- proposed by Maxwell.
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
// 1.146 -- proposed for an additional "fictitious" velocity slip.
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
// 0 -- not freeze, the chemical reaction sources will be calculated.
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
// nDebug: cout the Wrong place and abort
// 0 -- not used.
// 1 -- used.
// nSpeciesLimit: limitter of gas species
// 0 -- not used.
// 1 -- used.
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
// 0 -- method 0.
// 1 -- method 1.
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
// 0 -- not used.
// 1 -- used.
// nChemcalSourceModified: Modified on ChemcalSource
// 0 -- not used.
// 1 -- used.
// nAblation:
// 0 -- The wall ablation is not computed.
// 1 -- The wall ablation is computed.
// isInjection:
// 0 -- The injection velocity of ablation wall is not computed.
// 1 -- The injection velocity of ablation wall is computed.
// nViscosityModel:
// 0 -- Blottner fitting method.
// 1 -- Gupta fitting method.
// nSutherland:
// 0 -- stands for selecting the Blotter curve fits mode.
// 1 -- stands for Sutherland relation.
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
// "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.
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
// 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.
@ -758,6 +935,10 @@ int dg_high_order = 0;
int iapplication = 0;
int iCodeBranch = 0;
int nm = 5;
int nEquilibriumGas = 0;
int nPCWCycleStep = 3;
int nRETCycleStep = 3;
int nSLIPCycleStep= 3;
double refGama = 1.4;
double prl = 0.72;
@ -770,23 +951,73 @@ int nchem = 0;
int nchemsrc = 1;
int nchemrad = 1;
int ntmodel = 1;
int nChemicalFlowStep = 0;
int nEnergyRecycle = 0;
int nSlipBCModel = 0;
int nDensityModify = 1;
int nTEnergyModel = 0;
int nMeanFreePathType = 0;
int nIsChemicalFreeze = 0;
int nIsSuperCatalytic = 1;
int nTemperatureJump = 0;
double parkVDPower = 0.6;
double catalyticCoef = 0.0;
double sigmaVelocity = 1.0;
double sigmaTemperature = 1.0;
double sigmaMassFraction = 1.0;
double velocitySlipCorrectConstant = 1.0;
double chemicalRelaxCorf = 1.0;
double chemicalSpectrumRadiusCoef = 1.0;
double viscousSpectrumRadiusCoef = 1.0;
double inviscidSpectrumRadiusCoef = 1.0;
double staticPressureRelaxCorf = 1.0;
double veTemperatureMin = 30.0;
int nDebug = 0;
int nSpeciesLimit = 0;
int nTurblenceForChemical = 0;
int nViscosityFluxSublevelModified = 0 ;
int nChemcalSourceModified = 0;
int nAblation = 0;
int isInjection = 0;
int nViscosityModel = 0;
int nMarsModel = 0;
string gasfile = "DK5";
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
string speciesName = "O, O2, NO, N, N2";
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
//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, 0.233, 0.0, 0.0, 0.0, 0.767, 0.0";
//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, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Mars-Pa8";
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
//string gasfile = "DK7";
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
//string gasfile = "Combustion-12";
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
//string gasfile = "Gas-Mixture";
//string speciesName ="SpeciesA, SpeciesB";
//string initMassFraction = "1.0, 0.0";
int nSutherland = 0;
double gamaSpeciesA = 1.4;
double gamaSpeciesB = 1.3;
double molecularWeightSpeciesA = 29.0;
double molecularWeightSpeciesB = 30.0;
int nChemicalFlowStep = 0;
int ifStartFromPerfectGasResults = 0;
#########################################################################
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
#########################################################################
# High Order Struct Solver #
#########################################################################
// ifvfd:
// isFVMOrFDM:
// 0 -- NSSolverStruct using Finite Volume Method.
// 1 -- NSSolverStruct using Finite Differ Method.
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
// -- "roe", "steger".
// structhighordergradient:
// -- "conservation", "chain_rule".
int ifvfd = 0;
int isFVMOrFDM = 0;
string str_highorder_solver = "WCNS";
int SolverStructOrder = 0;
double str_highorder_interpolation_epsilon = 1.0e-6;
@ -885,8 +1116,12 @@ int allReduceStep = 1;
// codeOfOversetGrid: Overlapping(overset) grid or not.
// 0 -- NON-overlapping grid.
// 1 -- Overlapping grid.
// oversetInterpolationMethod: the method of overset interpolation while field simulation
// 0 -- set the acceptor cell value by donor cell value.
// 1 -- set the acceptor cell value by distance weight of donor cell value.
int codeOfOversetGrid = 0;
int codeOfOversetSlipGrid = 0;
int oversetInterpolationMethod = 0;
int readOversetFileOrNot = 0;
int symetryOrNot = 0;
int readInAuxiliaryInnerGrid = 1;
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
string auxiliaryInnerGrid2 = "";
string oversetGridFileName = "./grid/overlap.ovs";
string oversetGridFileName = "./grid/iblank.ovs";
double walldistMainZone = 1.0
double toleranceForOversetSearch = 1.0e-3;
double toleranceForOversetBox = 1.0e-3;
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
int numberOfMovingBodies = 2;
// ----------------- ALE configuration ------------------------------
int codeOfAleModel = 1;
int aleStartStrategy = -1;
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
int strategyForGCLSource = 0; //0-present; 1-Ahn;
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
int methodForKineticEquation = 0;
double relaxParameterOfKinetic = 1.0;
#########################################################################
# motive information #
#########################################################################
int numberOfMovingBodies = 1;
############################## body0 ##############################
//mass of parts
double mass_0 = 1.0;
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
//initial six DOF position information of parts. xc yc zc
double massCenter_0[] = 0.0 , 0.0, 0.0;
//initial six DOF position information of parts. angleX angleY angleZ
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
//initial six DOF move information of parts. vc vy vz
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
//initial six DOF move information of parts. omigX omigY omigZ
double angularVelocity_0[] = 0.0, 0.0, 0.0;
//the object that the parts belong to.
int fartherIndex_0 = -1;
//the assembly position of the parts. xc yc zc angleX angleY angleZ
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
//the move pattern of the parts.
// -1 given motion partten.
// 0 still.
// 1 six DOF motion.
// 2 three DOF motion.
// 11 X-axis forced motion.
// 12 Y-axis forced motion.
// 13 Z-axis forced motion.
// 14 forced pitch motion.
// 15 forced yaw motion.
// 16 forced roll motion.
int RBDMethod_0 = 0;
double amplitude_0 = 0.0;
double reduceFrequency_0 = 0.0;
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
//additional force (system axis) fX fY fZ
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
//additional moment of Force (system axis) mX mY mZ
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
//the deformation method of the parts.
int morphing_0 = 0;
// post indentify
int integralOrder = 4;
// ---------------- ATP read --------------------------------------------
//@int inflowParaType = 0;
//@double refReNumber = 2.329418E08;
//@double refDimensionalTemperature = 288.144;
//@double refDimensionalPressure = 1.01313E05;
//@double height = -0.001;
//@double refReNumber = 6.5e6;
//@double refDimensionalTemperature = 288.15;
//@double freestream_vibration_temperature = 300.00;
//@double refDimensionalPressure = 0;
//@double height = 0;
//@int nsubsonicInlet = 0;
//@int nsubsonicOutlet = 0;
//@string inLetFileName = "./bin/subsonicInlet.hypara";
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
//@double refDimensionalVelocity = 0;
//@double refDimensionalDensity = 0;
#########################################################################
# Old Parameter #

6
B13_ThreeD_Chnt_SA_Unstruct_100CPU/bin/cfd_para_subsonic.hypara
View File

@ -57,9 +57,9 @@ double refDimensionalTemperature = 298.15;
double gridScaleFactor = 1.0;
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
double forceRefenenceLength = 0.1937; // unit of meter.
double forceRefenenceArea = 0.12937; // unit of meter^2.
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
double forceReferenceLength = 0.1937; // unit of meter.
double forceReferenceArea = 0.12937; // unit of meter^2.
double TorqueRefX = 0.66087; // unit of meter.
double TorqueRefY = 0.0; // unit of meter.
double TorqueRefZ = 0.0; // unit of meter.