forked from PHengLEI/PHengLEI-TestCases
192 lines
9.3 KiB
Plaintext
192 lines
9.3 KiB
Plaintext
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#########################################################################
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# General Control Parameter #
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#########################################################################
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// maxsimustep: the max simulation step, don't care simulation is restart or not.
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// intervalStepFlow: the step intervals for flow variables file 'flow.dat' saved.
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// intervalStepPlot: the step intervals for tecplot visual file 'tecflow.dat' saved.
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// intervalStepForce: the step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
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// intervalStepRes: the step intervals for residual 'res.dat' saved.
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int maxSimuStep = 25000;
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int intervalStepFlow = 1000;
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int intervalStepPlot = 1000;
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int intervalStepForce = 100;
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int intervalStepRes = 10;
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#########################################################################
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# Inflow Parameter #
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#########################################################################
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// refMachNumber: Mach number per meter.
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// attackd: Angle of attack.
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// angleSlide: Angle of sideslip.
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// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
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// refDimensionalTemperature: dimensional reference temperature, or the total temperature only for the experiment condition.
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// refDimensionalPressure: dimensional reference pressure , or the total pressure only for the experiment condition.
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// inflowParaType: the type of inflow parameters.
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// 0 - the nondimensional conditions.
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// 1 - the flight conditions.
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// 2 - the experiment conditions.
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// height: Fly height, unit of km.
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// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
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// dump_Q: Dump out thermal flux Q of solid wall.
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// 0 - no dump out.
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// 1 - dump out wall Q only.
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// 2 - dump out wall Q & the typical position Q of ball.
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// 3 - dump out wall Q & the typical position Q of cone.
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// 4 - dump out wall Q & the typical position Q of double sphere.
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// gridScaleFactor: The customizable unit of the grid, default value 1.0 metre.
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// forceRefenenceLength, forceRefenenceArea: Reference length and area, independent to grid scale.
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// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent to grid scale.
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double refMachNumber = 10.00;
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double attackd = 0.00;
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double angleSlide = 0.00;
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double wallTemperature = 294.0 ;
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int dump_Q = 2;
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int inflowParaType = 0;
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double refReNumber = 1.0e5;
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double refDimensionalTemperature = 79.0;
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//int inflowParaType = 1;
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//double height = 0.001;
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//int inflowParaType = 2;
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//double refDimensionalTemperature = 6051.024; //the total temperature, T*(1+(gama0-1)*M*M/2).
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//double refDimensionalPressure = 4.299696E09; //the total pressure, p*(T0/T)^(gama0/(gama0-1)).
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double gridScaleFactor = 1.0;
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double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
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double forceRefenenceLength = 1.0; // unit of meter.
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double forceRefenenceArea = 1.0; // unit of meter^2
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double TorqueRefX = 0.0; // unit of meter.
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double TorqueRefY = 0.0; // unit of meter.
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double TorqueRefZ = 0.0; // unit of meter.
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#*******************************************************************
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# Physical models *
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#*******************************************************************
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// iviscous: Viscous model
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// 0 - Euler
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// 1 - Lamilar
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// 3 - 1eq turbulent
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// 4 - 2eq turbulent
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// viscousName : Laminar or tubulent model
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// - "1eq-sa", when iviscous = 3
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// - "2eq-kw-menter-sst", when iviscous = 4
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// DESType : Type of DES
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// 0 - RANS (default);
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// 1 - DES;
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// 2 - DDES;
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// 3 - IDDES;
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//int iviscous = 0;
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//string viscousName = "Euler";
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int viscousType = 1;
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string viscousName = "laminar";
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//int iviscous = 3;
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//string viscousName = "1eq-sa";
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//int iviscous = 4;
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//string viscousName = "2eq-kw-menter-sst";
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int DESType = 0;
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int roeEntropyFixMethod = 2;
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double roeEntropyScale = 0.0001;
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#########################################################################
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# Spatial Discretisation #
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#########################################################################
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#*******************************************************************
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# Struct Solver *
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#*******************************************************************
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// inviscidSchemeName: Spatial discretisation scheme of struct grid
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// Using this when solve structered grid or hybrid.
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// - "vanleer", "steger", "ausmpw"
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// str_limiter_name: Limiter of struct grid
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// - "minmod", "3rd_minmod_smooth"
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string inviscidSchemeName = "steger";
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string str_limiter_name = "minmod";
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#*******************************************************************
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# UnStruct Solver *
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#*******************************************************************
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// uns_scheme_name: Spatial discretisation scheme of Unstruct grid
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// Using this when solve Unstructered grid or hybrid.
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// - "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle"
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// - "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus"
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// uns_limiter_name: Limiter of Unstruct grid
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// - "vencat", "barth"
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// - "1st", meaning accuracy of first-order.
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// - "nolim", no limiter.
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// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'
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// The smaller the value, the more robust it is.
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string uns_scheme_name = "vanleer";
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string uns_limiter_name = "vencat";
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double venkatCoeff = 0.5;
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#########################################################################
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# Temporal Discretisation #
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#########################################################################
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// iunsteady: Steady or unsteady.
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// 0 - steady
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// 1 - unsteay
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// CFLEnd: The CFL number, [0.1, 100]
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// The bigger the value, the convergence faster but lower robustness.
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// ktmax: The lower the value, the more robustness, 1.0e5 ~ 1.0e10.
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int iunsteady = 0;
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double CFLEnd = 10.0;
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int CFLVaryStep = 100;
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double ktmax = 1.0e10;
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#########################################################################
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# File In or Out #
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#########################################################################
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// gridfile: The partitioned Grid file path, using relative path,
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// which is relative to the working directory.
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// IMPORTANT WARNNING: the file index should be ignored,
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// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
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// Please use 'rae2822_hybrid2d__4.fts' here!
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// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0/1.
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string gridfile = "./grid/3dball.fts";
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int isPlotVolumeField = 0;
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// ---------------- advanced Parameters, DO NOT care it -----------
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// nVisualVariables: number of variables want to be dumped for tecplot visualization.
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// visualVariables : variable types dumped, listed as following:
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// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6)
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// -- viscosityLaminar(7), viscosityTurbulent(8)
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// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12), strain_rate(13), Q_criteria(14)
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// -- Cp(15), timeStep(16), volume(17)
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// -- modeledTKE(18),modeleddissipationrate(19), SSTF1(20), SSTF2(21)
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// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!.
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// Arriables order must from small to larger.
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int nVisualVariables = 8;
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int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
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// limitVariables: limit model.
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// 0 - limit only for pressure and denstiny, then get the min value
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// 1 - limit for every variables, then get the min value
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// limitVector:
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// 0 - Each variable use the same limiter coefficient.
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// 1 - Each variable use the respective limiter coefficients.
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// reconmeth:
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// 0 - When reconstruct face value, Q+, Q- use respective limiter coefficients.
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// 1 - Q+, Q- use the min limiter coefficients of left and right cell.
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int reconmeth = 0;
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int limitVariables = 0;
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int limitVector = 1;
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