PHengLEI2112版本新添功能算例库更新
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# nBoundaryConditons : Number of global boundary conditions.
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# bcName : Boundary condition name.
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# bcType(in PHengLEI): Boundary condition type.
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# How to set boundary condition, for example:
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# string bcName = "Wall";
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# {
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# int bcType = 2;
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# int viscousType = 1;
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# double wallTemperature = -1.0;
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# double uWall = 0.0;
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# double vWall = 0.0;
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# double wWall = 0.0;
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# }
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# string bcName = "Inflow";
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# {
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# int bcType = 5;
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# int inflowParaType = 0;
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# double refMachNumber = 0.73;
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# double attackd = 2.79;
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# double angleSlide = 0.0;
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# double refReNumber = 6.5e6;
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# double refDimensionalTemperature = 288.15;
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# }
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# For more information, see examples/bin/boundary_condition.hypara file!!!
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int nBoundaryConditons = 6;
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string bcName = "Solid";
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{
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string bodyName = "body";
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int bcType = 2;
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}
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string bcName = "jet";
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{
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string bodyName = "body";
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int bcType = 5;
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int inflowParaType = 9;
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double primDensity = 41.45637;
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double primU = 0.0;
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double primV = 0.543918;
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double primW = 0.0;
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double primPressure = 8.76743560;
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}
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string bcName = "Symmetry";
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{
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int bcType = 3;
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}
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string bcName = "Farfield";
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{
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int bcType = 4;
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}
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string bcName = "Outflow";
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{
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int bcType = 6;
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}
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string bcName = "Pole";
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{
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int bcType = 73;
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}
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# 'bcType' is defined as following:
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# 99: PERIODIC
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# -2: WAKE
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# -1: INTERFACE
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# 0 : NO_BOUNDARY_CONDITION
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# 1 : EXTRAPOLATION
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# 2 : SOLID_SURFACE
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# 3 : SYMMETRY
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# 4 : FARFIELD
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# 5 : INFLOW
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# 6 : OUTFLOW
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# 52: PRESSURE_INLET
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# 62: PRESSURE_OUTLET
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# 61: OUTFLOW_CONFINED
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# 7 : POLE
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File diff suppressed because it is too large
Load Diff
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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 = 50000;
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int intervalStepFlow = 2000;
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int intervalStepPlot = 500;
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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.
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// attackd: Angle of attack.
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// angleSlide: Angle of sideslip.
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// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary 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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// 3 -- the subsonic boundary conditions.
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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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// height: Fly height, unit of km.
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// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
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// 1 dm = 0.1 m.
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// 1 cm = 0.01 m.
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// 1 mm = 0.001m.
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// 1 inch = 0.0254m.
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// 1 foot = 12 inches = 0.3048m.
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// 1 yard = 3 feet = 0.9144m.
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// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit.
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// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
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double refMachNumber = 3.33;
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double attackd = 0.00;
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double angleSlide = 0.00;
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double wallTemperature = -1.0;
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int inflowParaType = 0;
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double refReNumber = 8.22818e7;
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double refDimensionalTemperature = 84.22;
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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+(refGama-1)*M*M/2).
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//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
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double gridScaleFactor = 0.001;
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double forceReferenceLengthSpanWise = 0.415; // unit of meter.
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double forceReferenceLength = 0.415; // unit of meter.
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double forceReferenceArea = 0.00196; // 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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// viscousType : 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 viscousType = 3.
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// -- "2eq-kw-menter-sst", when viscousType = 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 viscousType = 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 viscousType = 3;
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//string viscousName = "1eq-sa";
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int viscousType = 4;
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string viscousName = "2eq-kw-menter-sst";
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int DESType = 0;
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int roeEntropyFixMethod = 3;
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double roeEntropyScale = 1.0;
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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", "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 = "minvan";
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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 = 5.0;
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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 WARNING: 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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// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
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string gridfile = "./grid/3D_jet__8.fts";
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int plotFieldType = 1;
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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),
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// -- strain_rate(13), Q_criteria(14), 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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// Variables order must from small to big.
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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 (It is useful only if limitVector is 0).
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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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#########################################################################
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# Grid data type #
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#########################################################################
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// gridtype: Grid type for generation, conversion, reconstruction, merging.
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// 0 -- Unstructured grid.
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// 1 -- Structured grid.
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// axisup: Type of Cartisien coordinates system, used in grid conversion.
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// 1 -- Y upward. (default)
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// 2 -- Z upward.
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// from_gtype: Type of grid data type in grid conversion process.
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// -1 -- MULTI_TYPE.
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// 1 -- PHengLEI, *.fts.
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// 2 -- CGNS, *.cgns.
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// 3 -- Plot3D type of structured grid, *.dat/*.grd.
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// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
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// 5 -- Fluent, *.cas/*.msh.
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// 6 -- Ustar, mgrid.in.
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// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
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// 8 -- GMSH, *.msh.
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int gridtype = 1;
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int axisup = 1;
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int from_gtype = 2;
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#########################################################################
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# File path #
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#########################################################################
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// from_gfile: path of original data file for unstructure grid convert from.
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// out_gfile: path of target file for grid convert to, *.fts type of file usually.
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string from_gfile = "./grid/3D_jet.cgns";
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string out_gfile = "./grid/3D_jet.fts";
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@ -0,0 +1,56 @@
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string title = "PHengLEI Main Parameter Control File";
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// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
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string defaultParaFile = "./bin/cfd_para.hypara";
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// ndim: Dimensional of the grid, 2 or 3.
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// nparafile: the number of parameter files.
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// nsimutask: simulation task type.
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// 0 -- CFD Solver of NS or Turbulation.
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// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
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// Grid conversion: from other format to PHengLEI format (.fts).
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// Grid reconstruction: such as grid adaptation.
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// Grid merging: merge two blocks into one block.
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// Grid repairing: repair the original grid in order to remove the negative volume cells.
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// 2 -- Wall distance computation for turb-solver.
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// 3 -- Grid partition.
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// 4 -- Knowledge repository / examples of PHengLEI-API.
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int ndim = 3;
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int nparafile = 1;
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int nsimutask = 0;
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//string parafilename = "./bin/cfd_para_subsonic.hypara";
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//string parafilename = "./bin/cfd_para_transonic.hypara";
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string parafilename = "./bin/cfd_para_supersonic.hypara";
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//string parafilename = "./bin/cfd_para_hypersonic.hypara";
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//string parafilename = "./bin/incompressible.hypara";
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//int nsimutask = 1;
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//string parafilename = "./bin/grid_para.hypara";
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//int nsimutask = 2;
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//string parafilename = "./bin/cfd_para.hypara";
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//int nsimutask = 3;
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//string parafilename = "./bin/partition.hypara";
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//int nsimutask = 4;
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//string parafilename = "./bin/repository.hypara";
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//int nsimutask = 5;
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//string parafilename = "./bin/overset_grid_view.hypara";
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//int nsimutask = 13;
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//string parafilename = "./bin/lbm_para.hypara";
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//int nsimutask = 14;
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//string parafilename = "./bin/integrative_solver.hypara";
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//int nsimutask = 99;
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//string parafilename = "./bin/post_processing.hypara";
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// ---------------- Advanced Parameters, DO NOT care it ----------------
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int numberOfGridProcessor = 0;
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// ATP read
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//@string parafilename1 = ""
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//@string parafilename2 = "";
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// pgridtype: The grid type.
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// 0 -- unstruct grid
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// 1 -- struct grid
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// maxproc: The number of partition zones that want to be divided into,
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// which is equal to the number of CPU processors you want.
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// Usually, 50~100 thousands structured cells per CPU-Core is suggested.
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// 30~70 thousands unstructured cells per CPU-Core is suggested.
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// original_grid_file : original grid file that want to be divided(HyperFLOW/PHengLEI type, *.fts).
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// partition_grid_file : target partition grid file(HyperFLOW/PHengLEI type, *.fts).
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int pgridtype = 1;
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int maxproc = 8;
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string original_grid_file = "./grid/3D_jet.fts";
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string partition_grid_file = "./grid/3D_jet__8.fts";
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// Number of multi-grid levels, ONLY used for structured grid.
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// 1 -- single level, 2 -- 2 level, N -- N level, ..., et al.
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int numberOfMultigrid = 1;
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Binary file not shown.
Binary file not shown.
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# nBoundaryConditons : Number of global boundary conditions.
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# bcName : Boundary condition name.
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# bcType(in PHengLEI): Boundary condition type.
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# How to set boundary condition, for example:
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# string bcName = "Wall";
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# {
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# int bcType = 2;
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# int viscousType = 1;
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# double wallTemperature = -1.0;
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# double uWall = 0.0;
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# double vWall = 0.0;
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# double wWall = 0.0;
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# }
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# string bcName = "Inflow";
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# {
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# int bcType = 5;
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# int inflowParaType = 0;
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# double refMachNumber = 0.73;
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# double attackd = 2.79;
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# double angleSlide = 0.0;
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# double refReNumber = 6.5e6;
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# double refDimensionalTemperature = 288.15;
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# }
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# For more information, see examples/bin/boundary_condition.hypara file!!!
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int nBoundaryConditons = 5;
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string bcName = "BCWall";
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{
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string bodyName = "body";
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int bcType = 2;
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}
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string bcName = "BCSymmetryPlane";
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{
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int bcType = 3;
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}
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string bcName = "BCFarfield";
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{
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int bcType = 4;
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}
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string bcName = "BCInflow";
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{
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int bcType = 5;
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}
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string bcName = "BCOutflow";
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{
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int bcType = 6;
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}
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# 'bcType' is defined as following:
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# 99: PERIODIC
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# -2: WAKE
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# -1: INTERFACE
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# 0 : NO_BOUNDARY_CONDITION
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# 1 : EXTRAPOLATION
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# 2 : SOLID_SURFACE
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# 3 : SYMMETRY
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# 4 : FARFIELD
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# 5 : INFLOW
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# 6 : OUTFLOW
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# 52: PRESSURE_INLET
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# 62: PRESSURE_OUTLET
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# 61: OUTFLOW_CONFINED
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# 7 : POLE
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File diff suppressed because it is too large
Load Diff
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@ -0,0 +1,201 @@
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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.
|
||||
// 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 = 50000;
|
||||
int intervalStepFlow = 2000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
int ifLowSpeedPrecon = 1;
|
||||
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// 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.
|
||||
// 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.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
|
||||
double refMachNumber = 0.1467;
|
||||
double attackd = 0.0;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 3.34e6;
|
||||
double refDimensionalTemperature = 290.5;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
double wallTemperature = -300.0;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
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.
|
||||
|
||||
#########################################################################
|
||||
# Physical models #
|
||||
#########################################################################
|
||||
// iviscous: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "1eq-sa", when iviscous = 3.
|
||||
// -- "2eq-kw-menter-sst", when iviscous = 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 transitionType = 2;
|
||||
double turbIntensity = 0.18;
|
||||
double freeStreamViscosity = 5.0;
|
||||
int freeturbIntensitySRModify = 1;
|
||||
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
#########################################################################
|
||||
# Spatial Discretisation #
|
||||
#########################################################################
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "3rdsmooth", "smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "minvan";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "vencat".
|
||||
// -- "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_limiter_name = "vencat";
|
||||
double venkatCoeff = 1.0;
|
||||
|
||||
#########################################################################
|
||||
# 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.
|
||||
// nLUSGSSweeps: Number of Sub-iteration of LU-SGS.
|
||||
// 0 -- is recommended for structured solver.
|
||||
// 1-3 -- is recommended for unstructured solver.
|
||||
|
||||
int iunsteady = 0;
|
||||
double CFLEnd = 50.0;
|
||||
int nLUSGSSweeps = 3;
|
||||
|
||||
#########################################################################
|
||||
# Multi-Grid parameters #
|
||||
#########################################################################
|
||||
// nMGLevel: The number of Multi-Grid level.
|
||||
// = 1 -- single-level.
|
||||
// > 1 -- multi-level.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
|
||||
int nMGLevel = 4;
|
||||
int flowInitStep = 0;
|
||||
|
||||
#########################################################################
|
||||
# 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/sk-flat-2D_str__4.fts";
|
||||
int walldistMethod = 3;
|
||||
int plotFieldType = 1;
|
||||
|
||||
// ----------------- 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).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
||||
int nVisualVariables = 15;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 8, 15, 18, 19, 20, 21, 51, 52];
|
||||
|
||||
// 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 = 0;
|
||||
|
||||
|
||||
|
|
@ -0,0 +1,34 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE
|
||||
// 1 -- HyperFLOW( PHengLEI ), *.fts.
|
||||
// 2 -- CGNS, *.cgns.
|
||||
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
|
||||
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
|
||||
// 5 -- Fluent, *.cas/*.msh.
|
||||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
int gridtype = 1;
|
||||
int axisup = 1;
|
||||
int from_gtype = 2;
|
||||
|
||||
#########################################################################
|
||||
# File path #
|
||||
#########################################################################
|
||||
// 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.
|
||||
string from_gfile = "./grid/sk-flat-2D_str.cgns";
|
||||
string out_gfile = "./grid/sk-flat-2D_str.fts";
|
||||
|
||||
|
||||
|
||||
|
||||
|
|
@ -0,0 +1,59 @@
|
|||
string title = "PHengLEI Main Parameter Control File";
|
||||
|
||||
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
|
||||
string defaultParaFile = "./bin/cfd_para.hypara";
|
||||
|
||||
// ndim: Dimensional of the grid, 2 or 3.
|
||||
// nparafile: the number of parameter files.
|
||||
// nsimutask: simulation task type.
|
||||
// 0 -- CFD Solver of NS or Turbulation.
|
||||
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
|
||||
// Grid conversion: from other format to PHengLEI format (.fts).
|
||||
// Grid reconstruction: such as grid adaptation.
|
||||
// Grid merging: merge two blocks into one block.
|
||||
// Grid repairing: repair the original grid in order to remove the negative volume cells.
|
||||
// 2 -- Wall distance computation for turb-solver.
|
||||
// 3 -- Grid partition.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
int ndim = 2;
|
||||
int nparafile = 1;
|
||||
|
||||
int nsimutask = 0;
|
||||
string parafilename = "./bin/cfd_para_subsonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_transonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_supersonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_hypersonic.hypara";
|
||||
//string parafilename = "./bin/incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
||||
//int nsimutask = 2;
|
||||
//string parafilename = "./bin/cfd_para.hypara";
|
||||
|
||||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
|
||||
//int nsimutask = 13;
|
||||
//string parafilename = "./bin/lbm_para.hypara";
|
||||
|
||||
//int nsimutask = 14;
|
||||
//string parafilename = "./bin/integrative_solver.hypara";
|
||||
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
|
||||
// ---------------- Advanced Parameters, DO NOT care it ----------------
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
|
|
@ -0,0 +1,23 @@
|
|||
// 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(HyperFLOW/PHengLEI type, *.fts).
|
||||
// partition_grid_file : target partition grid file(HyperFLOW/PHengLEI type, *.fts).
|
||||
|
||||
int pgridtype = 1;
|
||||
int maxproc = 4;
|
||||
|
||||
string original_grid_file = "./grid/sk-flat-2D_str.fts";
|
||||
string partition_grid_file = "./grid/sk-flat-2D_str__4.fts";
|
||||
|
||||
|
||||
// Number of multi-grid levels, ONLY used for structured grid.
|
||||
// 1 -- single level, 2 -- 2 level, N -- N level, ..., et al.
|
||||
int numberOfMultigrid = 4;
|
||||
|
||||
|
||||
|
||||
Binary file not shown.
Binary file not shown.
|
|
@ -0,0 +1,69 @@
|
|||
# nBoundaryConditons : Number of global boundary conditions.
|
||||
# bcName : Boundary condition name.
|
||||
# bcType(in PHengLEI): Boundary condition type.
|
||||
|
||||
# How to set boundary condition, for example:
|
||||
# string bcName = "Wall";
|
||||
# {
|
||||
# int bcType = 2;
|
||||
# int viscousType = 1;
|
||||
# double wallTemperature = -1.0;
|
||||
# double uWall = 0.0;
|
||||
# double vWall = 0.0;
|
||||
# double wWall = 0.0;
|
||||
# }
|
||||
# string bcName = "Inflow";
|
||||
# {
|
||||
# int bcType = 5;
|
||||
# int inflowParaType = 0;
|
||||
# double refMachNumber = 0.73;
|
||||
# double attackd = 2.79;
|
||||
# double angleSlide = 0.0;
|
||||
# double refReNumber = 6.5e6;
|
||||
# double refDimensionalTemperature = 288.15;
|
||||
# }
|
||||
|
||||
# For more information, see examples/bin/boundary_condition.hypara file!!!
|
||||
|
||||
int nBoundaryConditons = 6;
|
||||
string bcName = "Wall";
|
||||
{
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
}
|
||||
string bcName = "Symmetry Plane";
|
||||
{
|
||||
int bcType = 3;
|
||||
}
|
||||
string bcName = "Farfield";
|
||||
{
|
||||
int bcType = 4;
|
||||
}
|
||||
string bcName = "Farfield2";
|
||||
{
|
||||
int bcType = 4;
|
||||
}
|
||||
string bcName = "Inflow";
|
||||
{
|
||||
int bcType = 5;
|
||||
}
|
||||
string bcName = "Outflow";
|
||||
{
|
||||
int bcType = 6;
|
||||
}
|
||||
|
||||
# 'bcType' is defined as following:
|
||||
# 99: PERIODIC
|
||||
# -2: WAKE
|
||||
# -1: INTERFACE
|
||||
# 0 : NO_BOUNDARY_CONDITION
|
||||
# 1 : EXTRAPOLATION
|
||||
# 2 : SOLID_SURFACE
|
||||
# 3 : SYMMETRY
|
||||
# 4 : FARFIELD
|
||||
# 5 : INFLOW
|
||||
# 6 : OUTFLOW
|
||||
# 52: PRESSURE_INLET
|
||||
# 62: PRESSURE_OUTLET
|
||||
# 61: OUTFLOW_CONFINED
|
||||
# 7 : POLE
|
||||
File diff suppressed because it is too large
Load Diff
|
|
@ -0,0 +1,201 @@
|
|||
#########################################################################
|
||||
# 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 = 20000;
|
||||
int intervalStepFlow = 2000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
int ifLowSpeedPrecon = 1;
|
||||
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// 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.
|
||||
// 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.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
|
||||
double refMachNumber = 0.1467;
|
||||
double attackd = 0.0;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 3.34e6;
|
||||
double refDimensionalTemperature = 290.5;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
double wallTemperature = -300.0;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
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.
|
||||
|
||||
#########################################################################
|
||||
# Physical models #
|
||||
#########################################################################
|
||||
// iviscous: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "1eq-sa", when iviscous = 3.
|
||||
// -- "2eq-kw-menter-sst", when iviscous = 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 transitionType = 2;
|
||||
double turbIntensity = 0.18;
|
||||
double freeStreamViscosity = 5.0;
|
||||
int freeturbIntensitySRModify = 1;
|
||||
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
#########################################################################
|
||||
# Spatial Discretisation #
|
||||
#########################################################################
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "3rdsmooth", "smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "minvan";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "vencat".
|
||||
// -- "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_limiter_name = "vencat";
|
||||
double venkatCoeff = 1.0;
|
||||
|
||||
#########################################################################
|
||||
# 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.
|
||||
// nLUSGSSweeps: Number of Sub-iteration of LU-SGS.
|
||||
// 0 -- is recommended for structured solver.
|
||||
// 1-3 -- is recommended for unstructured solver.
|
||||
|
||||
int iunsteady = 0;
|
||||
double CFLEnd = 50.0;
|
||||
int nLUSGSSweeps = 3;
|
||||
|
||||
#########################################################################
|
||||
# Multi-Grid parameters #
|
||||
#########################################################################
|
||||
// nMGLevel: The number of Multi-Grid level.
|
||||
// = 1 -- single-level.
|
||||
// > 1 -- multi-level.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
|
||||
int nMGLevel = 4;
|
||||
int flowInitStep = 1000;
|
||||
|
||||
#########################################################################
|
||||
# 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/sk-flat-2D_unstr__4.fts";
|
||||
int walldistMethod = 1;
|
||||
int plotFieldType = 1;
|
||||
|
||||
// ----------------- 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).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
||||
int nVisualVariables = 15;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 8, 15, 18, 19, 20, 21, 51, 52];
|
||||
|
||||
// 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 = 0;
|
||||
|
||||
|
||||
|
|
@ -0,0 +1,34 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE
|
||||
// 1 -- HyperFLOW( PHengLEI ), *.fts.
|
||||
// 2 -- CGNS, *.cgns.
|
||||
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
|
||||
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
|
||||
// 5 -- Fluent, *.cas/*.msh.
|
||||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
int gridtype = 0;
|
||||
int axisup = 1;
|
||||
int from_gtype = 2;
|
||||
|
||||
#########################################################################
|
||||
# File path #
|
||||
#########################################################################
|
||||
// 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.
|
||||
string from_gfile = "./grid/sk-flat-2D_unstr.cgns";
|
||||
string out_gfile = "./grid/sk-flat-2D_unstr.fts";
|
||||
|
||||
|
||||
|
||||
|
||||
|
|
@ -0,0 +1,59 @@
|
|||
string title = "PHengLEI Main Parameter Control File";
|
||||
|
||||
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
|
||||
string defaultParaFile = "./bin/cfd_para.hypara";
|
||||
|
||||
// ndim: Dimensional of the grid, 2 or 3.
|
||||
// nparafile: the number of parameter files.
|
||||
// nsimutask: simulation task type.
|
||||
// 0 -- CFD Solver of NS or Turbulation.
|
||||
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
|
||||
// Grid conversion: from other format to PHengLEI format (.fts).
|
||||
// Grid reconstruction: such as grid adaptation.
|
||||
// Grid merging: merge two blocks into one block.
|
||||
// Grid repairing: repair the original grid in order to remove the negative volume cells.
|
||||
// 2 -- Wall distance computation for turb-solver.
|
||||
// 3 -- Grid partition.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
int ndim = 2;
|
||||
int nparafile = 1;
|
||||
|
||||
int nsimutask = 0;
|
||||
string parafilename = "./bin/cfd_para_subsonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_transonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_supersonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_hypersonic.hypara";
|
||||
//string parafilename = "./bin/incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
||||
//int nsimutask = 2;
|
||||
//string parafilename = "./bin/cfd_para.hypara";
|
||||
|
||||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
|
||||
//int nsimutask = 13;
|
||||
//string parafilename = "./bin/lbm_para.hypara";
|
||||
|
||||
//int nsimutask = 14;
|
||||
//string parafilename = "./bin/integrative_solver.hypara";
|
||||
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
|
||||
// ---------------- Advanced Parameters, DO NOT care it ----------------
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
|
|
@ -0,0 +1,23 @@
|
|||
// 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(HyperFLOW/PHengLEI type, *.fts).
|
||||
// partition_grid_file : target partition grid file(HyperFLOW/PHengLEI type, *.fts).
|
||||
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
|
||||
string original_grid_file = "./grid/sk-flat-2D_unstr.fts";
|
||||
string partition_grid_file = "./grid/sk-flat-2D_unstr__4.fts";
|
||||
|
||||
|
||||
// Number of multi-grid levels, ONLY used for structured grid.
|
||||
// 1 -- single level, 2 -- 2 level, N -- N level, ..., et al.
|
||||
int numberOfMultigrid = 1;
|
||||
|
||||
|
||||
|
||||
Binary file not shown.
Binary file not shown.
File diff suppressed because it is too large
Load Diff
|
|
@ -0,0 +1,300 @@
|
|||
#########################################################################
|
||||
# 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 = 400;
|
||||
|
||||
int intervalStepFlow = 100;
|
||||
int intervalStepPlot = 100;
|
||||
int intervalStepForce = 10;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice:Periodic boundary only support translation or rotation along the X axis!
|
||||
// periodicType: Which symmetry plane is used in the mesh.
|
||||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
int periodicType = 1;
|
||||
double translationLength[] = [0.0,0.0,0.5];
|
||||
double rotationAngle = 0;
|
||||
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// 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.
|
||||
// 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.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
|
||||
double refMachNumber = 0.4;
|
||||
double attackd = 9.29;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 50000.0;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
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.
|
||||
|
||||
#########################################################################
|
||||
# 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 *
|
||||
#*******************************************************************
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "3rdsmooth", "smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "3rdsmooth";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "vencat".
|
||||
// -- "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_limiter_name = "vencat";
|
||||
double venkatCoeff = 50.0;
|
||||
|
||||
#########################################################################
|
||||
# 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.
|
||||
// nLUSGSSweeps: Number of Sub-iteration of LU-SGS.
|
||||
// 1 -- is recommended for structured solver.
|
||||
// 1-3 -- is recommended for unstructured solver.
|
||||
|
||||
int iunsteady = 1;
|
||||
double physicalTimeStep = 0.002;
|
||||
int ifStaticsFlowField = 1;
|
||||
int ifStaticsReynoldsStress = 1;
|
||||
int startStatisticStep = 30010;
|
||||
double statisticalTimePeriod = -1.0;
|
||||
int statisticMethod = 0;
|
||||
|
||||
int min_sub_iter = 20;
|
||||
int max_sub_iter = 20;
|
||||
|
||||
double CFLStart = 10.0;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 1;
|
||||
|
||||
int nLUSGSSweeps = 4;
|
||||
double LUSGSTolerance = 1.0e-20;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or 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.
|
||||
// = 0 - in only first sub-iter;
|
||||
// != 0 - in every sub-iter.
|
||||
// ipraddisturb: Add density and pressure disturb or not.
|
||||
// ibodyforce: Add body force in source flux of NS equations or not.
|
||||
// = 0 - not;
|
||||
// != 0 - Add body force.
|
||||
// bodyforce: Body force in source flux of NS equations or not.
|
||||
// utau: friction velocity, using in DNSDisturb.
|
||||
// sgsmodel: subgrid scale model.
|
||||
// = "smagorinsky";
|
||||
// = "dsm";
|
||||
// = "wale".
|
||||
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
|
||||
// = 2 - pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 - Devloped by Scotti.
|
||||
// wallDampingFunctionType: = 0 - no wall function;
|
||||
// = 1 - van Driest;
|
||||
// = 2 - developed by Dr. Deng Xiaobing;
|
||||
// = 3 - developed by Piomelli.
|
||||
// turbViscousCutType: turbulent viscosity cut type.
|
||||
// = 0 - mu_total = mut + mul;
|
||||
// = 1 - mu_total = max(mut-mul,0)+ mul;
|
||||
// = 2 - mu_total = max(mut ,0)+ mul.
|
||||
// smagConstant: constant of smagorinsky model.
|
||||
// waleConstant: constant of wale model.
|
||||
// filterDirection[3]: filter variables in i, j, k direction or not.
|
||||
// averageDirection[3]: average variables in i, j, k direction or not.
|
||||
// isotropicConstant: constant of isotropic part of SGS stress.
|
||||
|
||||
int iLES = 1;
|
||||
string sgsmodel = "sigma";
|
||||
int deltaFunctionType = 2;
|
||||
int wallDampingFunctionType = 0;
|
||||
int turbViscousCutType = 2;
|
||||
double smagConstant = 0.11;
|
||||
double isotropicConstant = 0.0;
|
||||
double waleConstant = 0.6;
|
||||
double sigmaConstant = 1.35;
|
||||
int filterDirection[] = [1, 1, 0];
|
||||
int averageDirection[] = [1, 1, 0];
|
||||
double testFilterScale = 2.0;
|
||||
int averageWidth = 1;
|
||||
int monitorNegativeConstant = 0;
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
// <= 2 -- finite volume method.
|
||||
// >= 3 -- finite difference order. (to be completed)
|
||||
// 0 -- default.
|
||||
// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence,
|
||||
// smaller epsilon, robuster for shock-detecting.
|
||||
// str_highorder_interpolation_type:
|
||||
// -- "classical", "test".
|
||||
// str_highorder_flux_name:
|
||||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 1;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-4;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "roe";
|
||||
string structhighordergradient = "conservation";
|
||||
|
||||
#########################################################################
|
||||
# Multi-Grid parameters #
|
||||
#########################################################################
|
||||
// nMGLevel: The number of Multi-Grid level.
|
||||
// = 1 -- single-level.
|
||||
// > 1 -- multi-level.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int flowInitStep = 0;
|
||||
|
||||
#########################################################################
|
||||
# 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!
|
||||
// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
|
||||
|
||||
string gridfile = "./grid/naca0012_str_26m_yup__400.fts";
|
||||
int plotFieldType = 1;
|
||||
|
||||
// ----------------- 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).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
||||
int nVisualVariables = 9;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 8, 12, 14];
|
||||
|
||||
// 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 = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
|
||||
double eddyViscosityLimit = 1.0e5;
|
||||
double MUSCLCoefXk = 0.8;
|
||||
|
|
@ -0,0 +1,40 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE.
|
||||
// 1 -- PHengLEI, *.fts.
|
||||
// 2 -- CGNS, *.cgns.
|
||||
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
|
||||
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
|
||||
// 5 -- Fluent, *.cas/*.msh.
|
||||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
int gridtype = 1;
|
||||
int axisup = 1;
|
||||
int from_gtype = 2;
|
||||
|
||||
#########################################################################
|
||||
# File path #
|
||||
#########################################################################
|
||||
// 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.
|
||||
string from_gfile = "./grid/naca0012_str_26m_yup.cgns";
|
||||
string out_gfile = "./grid/naca0012_str_26m_yup.fts";
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice:Periodic boundary only support translation or rotation along the X axis!
|
||||
// periodicType: Which symmetry plane is used in the mesh.
|
||||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
int periodicType = 1;
|
||||
double translationLength[] = [0.0,0.0,0.5];
|
||||
double rotationAngle = 0.0;
|
||||
|
|
@ -0,0 +1,53 @@
|
|||
string title = "PHengLEI Main Parameter Control File";
|
||||
|
||||
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
|
||||
string defaultParaFile = "./bin/cfd_para.hypara";
|
||||
|
||||
// ndim: Dimensional of the grid, 2 or 3.
|
||||
// nparafile: the number of parameter files.
|
||||
// nsimutask: simulation task type.
|
||||
// 0 -- CFD Solver of NS or Turbulation.
|
||||
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
|
||||
// Grid conversion: from other format to PHengLEI format (.fts).
|
||||
// Grid reconstruction: such as grid adaptation.
|
||||
// Grid merging: merge two blocks into one block.
|
||||
// Grid repairing: repair the original grid in order to remove the negative volume cells.
|
||||
// 2 -- Wall distance computation for turb-solver.
|
||||
// 3 -- Grid partition.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
int ndim = 3;
|
||||
int nparafile = 1;
|
||||
|
||||
int nsimutask = 0;
|
||||
string parafilename = "./bin/cfd_para_subsonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_transonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_supersonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_hypersonic.hypara";
|
||||
//string parafilename = "./bin/incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
||||
//int nsimutask = 2;
|
||||
//string parafilename = "./bin/cfd_para.hypara";
|
||||
|
||||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
|
||||
//int nsimutask = 14;
|
||||
//string parafilename = "./bin/integrative_solver.hypara";
|
||||
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
|
||||
// ---------------- Advanced Parameters, DO NOT care it ----------------
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
|
|
@ -0,0 +1,31 @@
|
|||
// pgridtype: The grid type.
|
||||
// 0 -- unstruct grid.
|
||||
// 1 -- struct grid.
|
||||
// maxproc: The number of partition zones that want to be divided into,
|
||||
// which is equal to the number of CPU processors you want.
|
||||
// Usually, 50~100 thousands structured cells per CPU-Core is suggested.
|
||||
// 30~70 thousands unstructured cells per CPU-Core is suggested.
|
||||
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||
|
||||
int pgridtype = 1;
|
||||
int maxproc = 400;
|
||||
|
||||
string original_grid_file = "./grid/naca0012_str_26m_yup.fts";
|
||||
string partition_grid_file = "./grid/naca0012_str_26m_yup__400.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;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice:Periodic boundary only support translation or rotation along the X axis!
|
||||
// periodicType: Which symmetry plane is used in the mesh.
|
||||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
int periodicType = 1;
|
||||
double translationLength[] = [0.0,0.0,0.5];
|
||||
double rotationAngle = 0.0;
|
||||
|
|
@ -0,0 +1 @@
|
|||
如需该算例网格，请通过邮箱phenglei@126.com联系风雷团队获取。
|
||||
Binary file not shown.
|
|
@ -0,0 +1,69 @@
|
|||
# nBoundaryConditons : Number of global boundary conditions.
|
||||
# bcName : Boundary condition name.
|
||||
# bcType(in PHengLEI): Boundary condition type.
|
||||
|
||||
# How to set boundary condition, for example:
|
||||
# string bcName = "Wall";
|
||||
# {
|
||||
# int bcType = 2;
|
||||
# int viscousType = 1;
|
||||
# double wallTemperature = -1.0;
|
||||
# double uWall = 0.0;
|
||||
# double vWall = 0.0;
|
||||
# double wWall = 0.0;
|
||||
# }
|
||||
# string bcName = "Inflow";
|
||||
# {
|
||||
# int bcType = 5;
|
||||
# int inflowParaType = 0;
|
||||
# double refMachNumber = 0.73;
|
||||
# double attackd = 2.79;
|
||||
# double angleSlide = 0.0;
|
||||
# double refReNumber = 6.5e6;
|
||||
# double refDimensionalTemperature = 288.15;
|
||||
# }
|
||||
|
||||
# For more information, see examples/bin/boundary_condition.hypara file!!!
|
||||
|
||||
int nBoundaryConditons = 6;
|
||||
string bcName = "BCWall";
|
||||
{
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
}
|
||||
string bcName = "BCFarfield";
|
||||
{
|
||||
int bcType = 4;
|
||||
}
|
||||
string bcName = "BCInflow";
|
||||
{
|
||||
int bcType = 5;
|
||||
}
|
||||
string bcName = "BCOutflow";
|
||||
{
|
||||
int bcType = 6;
|
||||
}
|
||||
string bcName = "BCDegenerateLine";
|
||||
{
|
||||
int bcType = 71;
|
||||
}
|
||||
string bcName = "BCDegenerateLine";
|
||||
{
|
||||
int bcType = 73;
|
||||
}
|
||||
|
||||
# 'bcType' is defined as following:
|
||||
# 99: PERIODIC
|
||||
# -2: WAKE
|
||||
# -1: INTERFACE
|
||||
# 0 : NO_BOUNDARY_CONDITION
|
||||
# 1 : EXTRAPOLATION
|
||||
# 2 : SOLID_SURFACE
|
||||
# 3 : SYMMETRY
|
||||
# 4 : FARFIELD
|
||||
# 5 : INFLOW
|
||||
# 6 : OUTFLOW
|
||||
# 52: PRESSURE_INLET
|
||||
# 62: PRESSURE_OUTLET
|
||||
# 61: OUTFLOW_CONFINED
|
||||
# 7 : POLE
|
||||
File diff suppressed because it is too large
Load Diff
|
|
@ -0,0 +1,206 @@
|
|||
#########################################################################
|
||||
# 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 = 2000;
|
||||
|
||||
int intervalStepFlow = 50;
|
||||
int intervalStepPlot = 50;
|
||||
int intervalStepForce = 1;
|
||||
int intervalStepRes = 1;
|
||||
|
||||
#########################################################################
|
||||
# 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.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 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.
|
||||
// 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 = 2.50;
|
||||
double attackd = 0.0;
|
||||
double angleSlide = 0.0;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
int dump_Q = 0;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 4.8e6;
|
||||
double refDimensionalTemperature = 51.0;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temper ature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 0.7854; // unit of meter^2.
|
||||
double TorqueRefX = 5.0; // 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 = 2;
|
||||
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 = "minvan";
|
||||
|
||||
#*******************************************************************
|
||||
# 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 = 1;
|
||||
double physicalTimeStep = 0.05;
|
||||
int min_sub_iter = 15;
|
||||
int max_sub_iter = 31;
|
||||
double tol_sub_iter = 0.0001;
|
||||
int aleStartStrategy = 1;
|
||||
int ifStartFromSteadyResults = 1;
|
||||
|
||||
int ifLocalTimeStep = 0;
|
||||
double CFLStart = 0.1;
|
||||
double CFLEnd = 20.0;
|
||||
int CFLVaryStep = 10;
|
||||
|
||||
#########################################################################
|
||||
# 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!
|
||||
// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
|
||||
|
||||
string gridfile = "./grid/finner__16.fts";
|
||||
int plotFieldType = 1;
|
||||
int visualfileType = 1;
|
||||
int walldistMethod = 3;
|
||||
|
||||
// ----------------- 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).
|
||||
// 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 = 0;
|
||||
|
|
@ -0,0 +1,34 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE
|
||||
// 1 -- HyperFLOW( PHengLEI ), *.fts.
|
||||
// 2 -- CGNS, *.cgns.
|
||||
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
|
||||
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
|
||||
// 5 -- Fluent, *.cas/*.msh.
|
||||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
int gridtype = 1;
|
||||
int axisup = 1;
|
||||
int from_gtype = 2;
|
||||
|
||||
#########################################################################
|
||||
# File path #
|
||||
#########################################################################
|
||||
// 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.
|
||||
string from_gfile = "./grid/finner.cgns";
|
||||
string out_gfile = "./grid/finner.fts";
|
||||
|
||||
|
||||
|
||||
|
||||
|
|
@ -0,0 +1,49 @@
|
|||
string title = "PHengLEI Main Parameter Control File";
|
||||
// IMPORTANT NOTICE：DON NOT MODIFY THE FOWLLOWING LINE
|
||||
string defaultParaFile = "./bin/cfd_para.hypara";
|
||||
// ndim: Dimensional of the grid: 2 or 3.
|
||||
// nparafile: the number of the parameter file.
|
||||
// nsimutask: simulation task type.
|
||||
// 0 -- CFD Solver of NS or Turbulation.
|
||||
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
|
||||
// Grid conversion: from other format to HyperFLOW format (.fts).
|
||||
// Grid reconstruction: such as grid adaptation.
|
||||
// Grid merging: merge two blocks into one block.
|
||||
// Grid repairing: repair the original grid in order to remove the negative volume cells.
|
||||
// 2 -- Wall distance computation for turb-solver.
|
||||
// 3 -- Grid partition.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
int ndim = 3;
|
||||
int nparafile = 2;
|
||||
|
||||
int nsimutask = 0;
|
||||
//string parafilename = "./bin/cfd_para_subsonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_transonic.hypara";
|
||||
string parafilename = "./bin/cfd_para_supersonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_hypersonic.hypara";
|
||||
//string parafilename = "./bin/incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
||||
//int nsimutask = 2;
|
||||
//string parafilename = "./bin/cfd_para.hypara";
|
||||
|
||||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
// ---------------- advanced Parameters, DO NOT care it -----------
|
||||
int iovrlap = 0;
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
string parafilename1 = "./bin/kinetic_para.hypara"
|
||||
//string parafilename2 = "./bin/overset_config.hypara";
|
||||
|
||||
|
|
@ -0,0 +1,48 @@
|
|||
#########################################################################
|
||||
# Parameter for RBD #
|
||||
# *动力学基于有量纲的形式 #
|
||||
#########################################################################
|
||||
int codeOfAleModel = 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;
|
||||
|
||||
#########################################################################
|
||||
# 动力学方程计算相关参数 #
|
||||
#########################################################################
|
||||
//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;
|
||||
|
||||
#########################################################################
|
||||
# 物体刚体运动信息 #
|
||||
#########################################################################
|
||||
int numberOfMovingBodies = 1;
|
||||
|
||||
############################## body0 ##############################
|
||||
//部件的质量
|
||||
double mass_0 = 1.0;
|
||||
//部件的质量矩阵 Ixx Iyy Izz Ixy Ixz Iyz
|
||||
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
|
||||
//部件的初始六自由度位置信息 xc yc zc
|
||||
double massCenter_0[] = 5.0 , 0.0, 0.0;
|
||||
//部件的初始六自由度位置信息 angleX angleY angleZ
|
||||
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
|
||||
//部件的初始六自由度运动信息 vc vy vz
|
||||
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//部件的初始六自由度运动信息 omigX omigY omigZ
|
||||
double angularVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//部件所属的物体
|
||||
int fartherIndex_0 = -1;
|
||||
//部件的装配位置 xc yc zc angleX angleY angleZ
|
||||
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
|
||||
//部件运动方式
|
||||
int RBDMethod_0 = 14;
|
||||
double amplitude_0 = 5.0;
|
||||
double reduceFrequency_0 = 0.05;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//附加力 (体轴系) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//附加力矩(体轴系) mX mY mZ
|
||||
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//部件变形方式
|
||||
int morphing_0 = 0;
|
||||
|
|
@ -0,0 +1,23 @@
|
|||
// 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(HyperFLOW/PHengLEI type, *.fts).
|
||||
// partition_grid_file : target partition grid file(HyperFLOW/PHengLEI type, *.fts).
|
||||
|
||||
int pgridtype = 1;
|
||||
int maxproc = 16;
|
||||
|
||||
string original_grid_file = "./grid/finner.fts";
|
||||
string partition_grid_file = "./grid/finner__16.fts";
|
||||
|
||||
|
||||
// Number of multi-grid levels, ONLY used for structured grid.
|
||||
// 1 -- single level, 2 -- 2 level, N -- N level, ..., et al.
|
||||
int numberOfMultigrid = 1;
|
||||
|
||||
|
||||
|
||||
Binary file not shown.
Binary file not shown.
|
|
@ -0,0 +1,69 @@
|
|||
# nBoundaryConditons : Number of global boundary conditions.
|
||||
# bcName : Boundary condition name.
|
||||
# bcType(in PHengLEI): Boundary condition type.
|
||||
|
||||
# How to set boundary condition, for example:
|
||||
# string bcName = "Wall";
|
||||
# {
|
||||
# int bcType = 2;
|
||||
# int viscousType = 1;
|
||||
# double wallTemperature = -1.0;
|
||||
# double uWall = 0.0;
|
||||
# double vWall = 0.0;
|
||||
# double wWall = 0.0;
|
||||
# }
|
||||
# string bcName = "Inflow";
|
||||
# {
|
||||
# int bcType = 5;
|
||||
# int inflowParaType = 0;
|
||||
# double refMachNumber = 0.73;
|
||||
# double attackd = 2.79;
|
||||
# double angleSlide = 0.0;
|
||||
# double refReNumber = 6.5e6;
|
||||
# double refDimensionalTemperature = 288.15;
|
||||
# }
|
||||
|
||||
# For more information, see examples/bin/boundary_condition.hypara file!!!
|
||||
|
||||
int nBoundaryConditons = 4;
|
||||
string bcName = "BODY";
|
||||
{
|
||||
int isSecondSegment = 0;
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
}
|
||||
string bcName = "Segment1";
|
||||
{
|
||||
int isSecondSegment = 0;
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
}
|
||||
string bcName = "Segment2";
|
||||
{
|
||||
int isSecondSegment = 1;
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
double secondSegmentRotatePostionX = 6.0200968;
|
||||
double secondSegmentRotatePostionY = 6.0266381;
|
||||
double secondSegmentRotatePostionZ = 19.680012;
|
||||
}
|
||||
string bcName = "FAR";
|
||||
{
|
||||
int bcType = 4;
|
||||
}
|
||||
|
||||
# 'bcType' is defined as following:
|
||||
# 99: PERIODIC
|
||||
# -2: WAKE
|
||||
# -1: INTERFACE
|
||||
# 0 : NO_BOUNDARY_CONDITION
|
||||
# 1 : EXTRAPOLATION
|
||||
# 2 : SOLID_SURFACE
|
||||
# 3 : SYMMETRY
|
||||
# 4 : FARFIELD
|
||||
# 5 : INFLOW
|
||||
# 6 : OUTFLOW
|
||||
# 52: PRESSURE_INLET
|
||||
# 62: PRESSURE_OUTLET
|
||||
# 61: OUTFLOW_CONFINED
|
||||
# 7 : POLE
|
||||
File diff suppressed because it is too large
Load Diff
|
|
@ -0,0 +1,195 @@
|
|||
#########################################################################
|
||||
# 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 = 0;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// 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.
|
||||
// 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.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
|
||||
double refMachNumber = 0.2;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
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.
|
||||
|
||||
#########################################################################
|
||||
# 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 *
|
||||
#*******************************************************************
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "3rdsmooth", "smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
||||
string str_limiter_name = "smooth";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "vencat".
|
||||
// -- "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_limiter_name = "vencat";
|
||||
double venkatCoeff = 50.0;
|
||||
|
||||
#########################################################################
|
||||
# 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.
|
||||
// nLUSGSSweeps: Number of Sub-iteration of LU-SGS.
|
||||
// 1 -- is recommended for structured solver.
|
||||
// 1-3 -- is recommended for unstructured solver.
|
||||
|
||||
int iunsteady = 0;
|
||||
|
||||
double CFLEnd = 100.0;
|
||||
|
||||
int nLUSGSSweeps = 5;
|
||||
|
||||
#########################################################################
|
||||
# Multi-Grid parameters #
|
||||
#########################################################################
|
||||
// nMGLevel: The number of Multi-Grid level.
|
||||
// = 1 -- single-level.
|
||||
// > 1 -- multi-level.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int flowInitStep = 100;
|
||||
|
||||
#########################################################################
|
||||
# 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!
|
||||
// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
|
||||
|
||||
string gridfile = "./grid/walldisttest1.fts";
|
||||
int plotFieldType = 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).
|
||||
// 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 = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
|
|
@ -0,0 +1,34 @@
|
|||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// gridobj: Task type of grid treatment.
|
||||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 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 gridobj = 4;
|
||||
int nDeformStep = 40;
|
||||
double flapAngle = 10.0;
|
||||
double rotatePostionZ = 4.00003;
|
||||
double rotatePostionY = 3.05;
|
||||
|
||||
int deformationMethod = 1;
|
||||
string stationalGridFile = "./grid/Segment2Brid.fts";
|
||||
string visualFileName = "./results/deformedGrid.dat"
|
||||
|
||||
int gridSlice = 1;
|
||||
int sliceAxis = 1;
|
||||
double slicePosition = 13;
|
||||
|
||||
// ----------------- RBF Parameters -------------------------------------
|
||||
// numberOfReferenceCP : Number of reference Control Points.
|
||||
// influencePara : The RBF influence radius parameter.
|
||||
int numberOfReferenceCP = 40;
|
||||
double influencePara = 25.0;
|
||||
|
|
@ -0,0 +1,31 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE.
|
||||
// 1 -- PHengLEI, *.fts.
|
||||
// 2 -- CGNS, *.cgns.
|
||||
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
|
||||
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
|
||||
// 5 -- Fluent, *.cas/*.msh.
|
||||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
int gridtype = 0;
|
||||
int axisup = 1;
|
||||
int from_gtype = 2;
|
||||
|
||||
#########################################################################
|
||||
# File path #
|
||||
#########################################################################
|
||||
// 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.
|
||||
string from_gfile = "./grid/Segment2Brid.cgns";
|
||||
string out_gfile = "./grid/Segment2Brid.fts";
|
||||
|
||||
|
|
@ -0,0 +1,59 @@
|
|||
string title = "PHengLEI Main Parameter Control File";
|
||||
|
||||
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
|
||||
string defaultParaFile = "./bin/cfd_para.hypara";
|
||||
|
||||
// ndim: Dimensional of the grid, 2 or 3.
|
||||
// nparafile: the number of parameter files.
|
||||
// nsimutask: simulation task type.
|
||||
// 0 -- CFD Solver of NS or Turbulation.
|
||||
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
|
||||
// Grid conversion: from other format to PHengLEI format (.fts).
|
||||
// Grid reconstruction: such as grid adaptation.
|
||||
// Grid merging: merge two blocks into one block.
|
||||
// Grid repairing: repair the original grid in order to remove the negative volume cells.
|
||||
// 2 -- Wall distance computation for turb-solver.
|
||||
// 3 -- Grid partition.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
int ndim = 3;
|
||||
int nparafile = 1;
|
||||
|
||||
//int nsimutask = 0;
|
||||
//string parafilename = "./bin/cfd_para_subsonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_transonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_supersonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_hypersonic.hypara";
|
||||
//string parafilename = "./bin/incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
||||
//int nsimutask = 2;
|
||||
//string parafilename = "./bin/cfd_para.hypara";
|
||||
|
||||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
int nsimutask = 1;
|
||||
string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
|
||||
//int nsimutask = 13;
|
||||
//string parafilename = "./bin/lbm_para.hypara";
|
||||
|
||||
//int nsimutask = 14;
|
||||
//string parafilename = "./bin/integrative_solver.hypara";
|
||||
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
|
||||
// ---------------- Advanced Parameters, DO NOT care it ----------------
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
Binary file not shown.
Binary file not shown.
|
|
@ -0,0 +1,69 @@
|
|||
# nBoundaryConditons : Number of global boundary conditions.
|
||||
# bcName : Boundary condition name.
|
||||
# bcType(in PHengLEI): Boundary condition type.
|
||||
|
||||
# How to set boundary condition, for example:
|
||||
# string bcName = "Wall";
|
||||
# {
|
||||
# int bcType = 2;
|
||||
# int viscousType = 1;
|
||||
# double wallTemperature = -1.0;
|
||||
# double uWall = 0.0;
|
||||
# double vWall = 0.0;
|
||||
# double wWall = 0.0;
|
||||
# }
|
||||
# string bcName = "Inflow";
|
||||
# {
|
||||
# int bcType = 5;
|
||||
# int inflowParaType = 0;
|
||||
# double refMachNumber = 0.73;
|
||||
# double attackd = 2.79;
|
||||
# double angleSlide = 0.0;
|
||||
# double refReNumber = 6.5e6;
|
||||
# double refDimensionalTemperature = 288.15;
|
||||
# }
|
||||
|
||||
# For more information, see examples/bin/boundary_condition.hypara file!!!
|
||||
|
||||
int nBoundaryConditons = 4;
|
||||
string bcName = "BODY";
|
||||
{
|
||||
int isSecondSegment = 0;
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
}
|
||||
string bcName = "Segment1";
|
||||
{
|
||||
int isSecondSegment = 0;
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
}
|
||||
string bcName = "Segment2";
|
||||
{
|
||||
int isSecondSegment = 1;
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
double secondSegmentRotatePostionX = 6.0200968;
|
||||
double secondSegmentRotatePostionY = 6.0266381;
|
||||
double secondSegmentRotatePostionZ = 19.680012;
|
||||
}
|
||||
string bcName = "FAR";
|
||||
{
|
||||
int bcType = 4;
|
||||
}
|
||||
|
||||
# 'bcType' is defined as following:
|
||||
# 99: PERIODIC
|
||||
# -2: WAKE
|
||||
# -1: INTERFACE
|
||||
# 0 : NO_BOUNDARY_CONDITION
|
||||
# 1 : EXTRAPOLATION
|
||||
# 2 : SOLID_SURFACE
|
||||
# 3 : SYMMETRY
|
||||
# 4 : FARFIELD
|
||||
# 5 : INFLOW
|
||||
# 6 : OUTFLOW
|
||||
# 52: PRESSURE_INLET
|
||||
# 62: PRESSURE_OUTLET
|
||||
# 61: OUTFLOW_CONFINED
|
||||
# 7 : POLE
|
||||
File diff suppressed because it is too large
Load Diff
|
|
@ -0,0 +1,34 @@
|
|||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// gridobj: Task type of grid treatment.
|
||||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 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 gridobj = 4;
|
||||
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 -------------------------------------
|
||||
// numberOfReferenceCP : Number of reference Control Points.
|
||||
// influencePara : The RBF influence radius parameter.
|
||||
int numberOfReferenceCP = 40;
|
||||
double influencePara = 25.0;
|
||||
|
|
@ -0,0 +1,31 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE.
|
||||
// 1 -- PHengLEI, *.fts.
|
||||
// 2 -- CGNS, *.cgns.
|
||||
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
|
||||
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
|
||||
// 5 -- Fluent, *.cas/*.msh.
|
||||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
int gridtype = 0;
|
||||
int axisup = 1;
|
||||
int from_gtype = 2;
|
||||
|
||||
#########################################################################
|
||||
# File path #
|
||||
#########################################################################
|
||||
// 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.
|
||||
string from_gfile = "./grid/Segment2Brid.cgns";
|
||||
string out_gfile = "./grid/Segment2Brid.fts";
|
||||
|
||||
|
|
@ -0,0 +1,59 @@
|
|||
string title = "PHengLEI Main Parameter Control File";
|
||||
|
||||
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
|
||||
string defaultParaFile = "./bin/cfd_para.hypara";
|
||||
|
||||
// ndim: Dimensional of the grid, 2 or 3.
|
||||
// nparafile: the number of parameter files.
|
||||
// nsimutask: simulation task type.
|
||||
// 0 -- CFD Solver of NS or Turbulation.
|
||||
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
|
||||
// Grid conversion: from other format to PHengLEI format (.fts).
|
||||
// Grid reconstruction: such as grid adaptation.
|
||||
// Grid merging: merge two blocks into one block.
|
||||
// Grid repairing: repair the original grid in order to remove the negative volume cells.
|
||||
// 2 -- Wall distance computation for turb-solver.
|
||||
// 3 -- Grid partition.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
int ndim = 3;
|
||||
int nparafile = 1;
|
||||
|
||||
//int nsimutask = 0;
|
||||
//string parafilename = "./bin/cfd_para_subsonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_transonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_supersonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_hypersonic.hypara";
|
||||
//string parafilename = "./bin/incompressible.hypara";
|
||||
|
||||
int nsimutask = 1;
|
||||
string parafilename = "./bin/grid_para.hypara";
|
||||
|
||||
//int nsimutask = 2;
|
||||
//string parafilename = "./bin/cfd_para.hypara";
|
||||
|
||||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
|
||||
//int nsimutask = 13;
|
||||
//string parafilename = "./bin/lbm_para.hypara";
|
||||
|
||||
//int nsimutask = 14;
|
||||
//string parafilename = "./bin/integrative_solver.hypara";
|
||||
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
|
||||
// ---------------- Advanced Parameters, DO NOT care it ----------------
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
Binary file not shown.
Binary file not shown.
Loading…
Reference in New Issue