forked from PHengLEI/PHengLEI-TestCases
239 lines
12 KiB
Plaintext
239 lines
12 KiB
Plaintext
|
#########################################################################
|
||
|
# General Control Parameter #
|
||
|
#########################################################################
|
||
|
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||
|
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||
|
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||
|
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||
|
// intervalStepRes: The step intervals for residual 'res.dat' saved.
|
||
|
|
||
|
int maxSimuStep = 30000;
|
||
|
|
||
|
int intervalStepFlow = 2000;
|
||
|
int intervalStepPlot = 2000;
|
||
|
int intervalStepForce = 100;
|
||
|
int intervalStepRes = 10;
|
||
|
|
||
|
#########################################################################
|
||
|
# Inflow Parameter #
|
||
|
#########################################################################
|
||
|
// refMachNumber: Mach number.
|
||
|
// attackd: Angle of attack.
|
||
|
// angleSlide: Angle of sideslip.
|
||
|
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||
|
// inflowParaType: The type of inflow parameters.
|
||
|
// 0 -- the nondimensional conditions.
|
||
|
// 1 -- the flight conditions.
|
||
|
// 2 -- the experiment conditions.
|
||
|
// 3 -- the subsonic boundary conditions.
|
||
|
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||
|
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||
|
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||
|
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||
|
// height: Fly height, unit of km.
|
||
|
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||
|
// 1 dm = 0.1 m.
|
||
|
// 1 cm = 0.01 m.
|
||
|
// 1 mm = 0.001m.
|
||
|
// 1 inch = 0.0254m.
|
||
|
// 1 foot = 12 inches = 0.3048m.
|
||
|
// 1 yard = 3 feet = 0.9144m.
|
||
|
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||
|
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||
|
|
||
|
double refMachNumber = 8.15;
|
||
|
double attackd = 0.00;
|
||
|
double angleSlide = 0.00;
|
||
|
|
||
|
double wallTemperature = 296.0;
|
||
|
|
||
|
int inflowParaType = 0;
|
||
|
double refReNumber = 1.6e7;
|
||
|
double refDimensionalTemperature = 56.0;
|
||
|
double freestream_vibration_temperature = 10000.0;
|
||
|
|
||
|
//int inflowParaType = 1;
|
||
|
//double height = 0.001;
|
||
|
|
||
|
//int inflowParaType = 2;
|
||
|
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||
|
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||
|
|
||
|
double gridScaleFactor = 0.01;
|
||
|
|
||
|
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||
|
double forceRefenenceLength = 1.0; // unit of meter.
|
||
|
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||
|
double TorqueRefX = 0.0; // unit of meter.
|
||
|
double TorqueRefY = 0.0; // unit of meter.
|
||
|
double TorqueRefZ = 0.0; // unit of meter.
|
||
|
|
||
|
#########################################################################
|
||
|
# Physical models #
|
||
|
#########################################################################
|
||
|
// viscousType: Viscous model.
|
||
|
// 0 -- Euler.
|
||
|
// 1 -- Lamilar.
|
||
|
// 3 -- 1eq turbulent.
|
||
|
// 4 -- 2eq turbulent.
|
||
|
// viscousName: Laminar or tubulent model.
|
||
|
// -- "1eq-sa", when viscousType = 3.
|
||
|
// -- "2eq-kw-menter-sst", when viscousType = 4.
|
||
|
// DESType: Type of DES.
|
||
|
// 0 -- RANS.(default)
|
||
|
// 1 -- DES.
|
||
|
// 2 -- DDES.
|
||
|
// 3 -- IDDES.
|
||
|
|
||
|
//int viscousType = 0;
|
||
|
//string viscousName = "Euler";
|
||
|
|
||
|
int viscousType = 1;
|
||
|
string viscousName = "laminar";
|
||
|
|
||
|
//int viscousType = 3;
|
||
|
//string viscousName = "1eq-sa";
|
||
|
|
||
|
//int viscousType = 4;
|
||
|
//string viscousName = "2eq-kw-menter-sst";
|
||
|
|
||
|
int DESType = 0;
|
||
|
|
||
|
int roeEntropyFixMethod = 3;
|
||
|
double roeEntropyScale = 1.0;
|
||
|
#########################################################################
|
||
|
# Spatial Discretisation #
|
||
|
#########################################################################
|
||
|
#*******************************************************************
|
||
|
# Struct Solver *
|
||
|
#*******************************************************************
|
||
|
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||
|
// Using this when solve structered grid or hybrid.
|
||
|
// -- "vanleer", "steger", "ausmpw".
|
||
|
// str_limiter_name: Limiter of struct grid.
|
||
|
// -- "minmod", "3rd_minmod_smooth".
|
||
|
|
||
|
string inviscidSchemeName = "steger";
|
||
|
string str_limiter_name = "minmod";
|
||
|
|
||
|
#*******************************************************************
|
||
|
# UnStruct Solver *
|
||
|
#*******************************************************************
|
||
|
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||
|
// Using this when solve Unstructered grid or hybrid.
|
||
|
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||
|
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||
|
// uns_limiter_name: Limiter of Unstruct grid.
|
||
|
// -- "vencat", "barth".
|
||
|
// -- "1st", meaning accuracy of first-order.
|
||
|
// -- "nolim", no limiter.
|
||
|
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'.
|
||
|
// The smaller the value, the more robust it is.
|
||
|
|
||
|
string uns_scheme_name = "vanleer";
|
||
|
string uns_limiter_name = "vencat";
|
||
|
double venkatCoeff = 0.5;
|
||
|
|
||
|
#########################################################################
|
||
|
# Temporal Discretisation #
|
||
|
#########################################################################
|
||
|
// iunsteady: Steady or unsteady.
|
||
|
// 0 -- steady.
|
||
|
// 1 -- unsteay.
|
||
|
// CFLEnd: The CFL number, [0.1, 100].
|
||
|
// The bigger the value, the convergence faster but lower robustness.
|
||
|
// ktmax: The lower the value, the more robustness, 1.0e5 - 1.0e10.
|
||
|
|
||
|
int iunsteady = 0;
|
||
|
|
||
|
double CFLEnd = 1.0;
|
||
|
|
||
|
double ktmax = 1.0e10;
|
||
|
|
||
|
#########################################################################
|
||
|
# File In or Out #
|
||
|
#########################################################################
|
||
|
// gridfile: The partitioned Grid file path, using relative path,
|
||
|
// which is relative to the working directory.
|
||
|
// IMPORTANT WARNING: The file index should be ignored,
|
||
|
// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
|
||
|
// Please use 'rae2822_hybrid2d__4.fts' here!
|
||
|
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0 / 1.
|
||
|
|
||
|
string gridfile = "./grid/DoubleEllipse__4.fts";
|
||
|
int isPlotVolumeField = 0;
|
||
|
|
||
|
// ----------------- Advanced Parameters, DO NOT care it ----------------
|
||
|
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
|
||
|
// visualVariables: Variable types dumped, listed as following:
|
||
|
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
|
||
|
// -- viscosityLaminar(7), viscosityTurbulent(8),
|
||
|
// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12),
|
||
|
// -- strain_rate(13), Q_criteria(14), Cp(15), timeStep(16), volume(17),
|
||
|
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
|
||
|
// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
|
||
|
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40).
|
||
|
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||
|
// Variables order must from small to big.
|
||
|
|
||
|
int nVisualVariables = 8;
|
||
|
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||
|
|
||
|
// limitVariables: Limit model (It is useful only if limitVector is 0).
|
||
|
// 0 -- limit only for pressure and denstiny, then get the min value.
|
||
|
// 1 -- limit for every variables, then get the min value.
|
||
|
// limitVector:
|
||
|
// 0 -- Each variable use the same limiter coefficient.
|
||
|
// 1 -- Each variable use the respective limiter coefficients.
|
||
|
// reconmeth:
|
||
|
// 0 -- When reconstruct face value, Q+, Q- use respective limiter coefficients.
|
||
|
// 1 -- Q+, Q- use the min limiter coefficients of left and right cell.
|
||
|
|
||
|
int reconmeth = 0;
|
||
|
int limitVariables = 0;
|
||
|
int limitVector = 1;
|
||
|
|
||
|
#########################################################################
|
||
|
# Non-equilibrium gas #
|
||
|
#########################################################################
|
||
|
// nGasModel: The type of gas.
|
||
|
// 0 -- Earth gas.
|
||
|
// 1 -- Mars gas.
|
||
|
// nchem:
|
||
|
// 0 -- without chemical reaction flow.
|
||
|
// 1 -- the chemical reaction flow is considered.
|
||
|
// nchemsrc:
|
||
|
// 0 -- the source terms are not computed.
|
||
|
// 1 -- the source terms are computed.
|
||
|
// nchemrad:
|
||
|
// 0 -- compute the spectrum radius without considering chemical reaction flow.
|
||
|
// 1 -- compute the spectrum radius that need to count the contribution from chemical reaction flow.
|
||
|
// ntmodel: The thermodynamic temperature model.
|
||
|
// 1 -- One-temperature model.
|
||
|
// 2 -- Two-temperature model.
|
||
|
// 3 -- Three-temperature model.
|
||
|
// 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.
|
||
|
// 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.
|
||
|
// For self-definition model, the gasfile is used to indicate the file path of the new gas model.
|
||
|
// speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma.
|
||
|
// initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName.
|
||
|
// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes.
|
||
|
|
||
|
int nGasModel = 0;
|
||
|
int nchem = 0;
|
||
|
int ntmodel = 1;
|
||
|
int nchemsrc = 1;
|
||
|
int nchemrad = 1;
|
||
|
double catalyticCoef = 1.0;
|
||
|
string gasfile = "DK5";
|
||
|
string speciesName = "O, O2, NO, N, N2";
|
||
|
string initMassFraction = "0.07955, 0.134, 0.0509, 1.0e-9, 0.73555";
|
||
|
int ifStartFromPerfectGasResults = 0;
|