forked from PHengLEI/PHengLEI-TestCases
新增B18:CRM-HL高升力外形模拟算例
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本算例在定常状态下采用RANS方法模拟CRM-HL高升力外形标模(B型网格)在大攻角状态下的气动特性。
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网格下载地址:http://hiliftpw.larc.nasa.gov/Workshop4/grids_downloads.html
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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 = 1000;
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int intervalStepPlot = 1000;
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int intervalStepForce = 50;
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int intervalStepRes = 10;
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// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
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// 0 -- no precondition process. (default, mach > 0.3)
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// 1 -- carry out precondition process. (mach number <= 0.3)
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int ifLowSpeedPrecon = 0;
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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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// 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 = 0.2;
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double attackd = 17.05;
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double angleSlide = 0.00;
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int inflowParaType = 0;
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double refReNumber = 7.8369E05;
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double refDimensionalTemperature = 289.44;
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//int inflowParaType = 1;
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//double height = 0.001;
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double gridScaleFactor = 0.0254;
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double forceReferenceLengthSpanWise = 29.38145; // unit of meter.
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double forceReferenceLength = 7.00532; // unit of meter.
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double forceReferenceArea = 191.8488; // unit of meter^2.
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double TorqueRefX = 33.67786; // unit of meter.
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double TorqueRefY = 4.51993; // 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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// str_limiter_name: Limiter of struct grid.
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// -- "3rdsmooth", "smooth".
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// -- "nolim", no limiter.
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string str_limiter_name = "smooth";
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#*******************************************************************
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# UnStruct Solver *
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#*******************************************************************
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// uns_limiter_name: Limiter of Unstruct grid.
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// -- "vencat".
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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_limiter_name = "vencat";
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double venkatCoeff = 50.0;
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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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// nLUSGSSweeps: Number of Sub-iteration of LU-SGS.
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// 1 -- is recommended for structured solver.
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// 1-3 -- is recommended for unstructured solver.
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int iunsteady = 0;
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double CFLEnd = 100.0;
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int nLUSGSSweeps = 5;
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#########################################################################
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# Multi-Grid parameters #
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#########################################################################
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// nMGLevel: The number of Multi-Grid level.
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// = 1 -- single-level.
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// > 1 -- multi-level.
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// flowInitStep: Flow initialization step, 0 - 500 is suggested.
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// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
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// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
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int nMGLevel = 1;
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int flowInitStep = 100;
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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/CRM-HL_40-37__Level-B__1024.fts";
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int plotFieldType = 0;
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// ----------------- Advanced Parameters, DO NOT care it ----------------
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// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
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// visualVariables: Variable types dumped, listed as following:
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// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
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// -- viscosityLaminar(7), viscosityTurbulent(8),
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// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12),
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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 = 3;
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int visualVariables[] = [ 1, 8, 12];
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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 = 1;
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int limitVariables = 0;
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int limitVector = 0;
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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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// 9 -- Gridgen type of structured grid, *.dat/*.grd.
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int gridtype = 0;
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int axisup = 2;
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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/CRM-HL_40-37_Nominal_Unstr_LevelB_Q1.cgns";
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string out_gfile = "./grid/CRM-HL_40-37_Nominal_Unstr_LevelB_Q1.fts";
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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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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 = 1;
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//string parafilename = "./bin/grid_deform_para.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 = 15;
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//string parafilename = "./bin/gridcheck_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(PHengLEI type, *.fts).
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// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
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int pgridtype = 0;
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int maxproc = 1024;
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string original_grid_file = "./grid/CRM-HL_40-37_Nominal_Unstr_LevelB_Q1.fts";
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string partition_grid_file = "./grid/CRM-HL_40-37_Nominal_Unstr_LevelB_Q1__1024.fts";
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// numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid.
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// 1 -- single level.
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// 2 -- 2 level.
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// N -- N level,..., et al.
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int numberOfMultigrid = 1;
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@ -71,6 +71,7 @@ B 非结构
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| 二维非结构NLR7301翼型低速绕流 | B15_TwoD_NLR7301_SA_Unstruct_4CPU |
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| 二维非结构NLR7301翼型低速绕流 | B15_TwoD_NLR7301_SA_Unstruct_4CPU |
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| 三维非结构空心圆柱裙 | B16_ThreeD_Hollow_Cylinder_Flare_Laminar_Unstruct_16CPU |
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| 三维非结构空心圆柱裙 | B16_ThreeD_Hollow_Cylinder_Flare_Laminar_Unstruct_16CPU |
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| 二维非结构S-K低速平板转捩模拟 | B17_TwoD_Plate_S-KSR_SST_Unstruct_4CPU |
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| 二维非结构S-K低速平板转捩模拟 | B17_TwoD_Plate_S-KSR_SST_Unstruct_4CPU |
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| 三维非结构CRM-HL高升力外形模拟 | B18-ThreeD_CRM-HL_Level-B_SA_Unstruct_1024CPU |
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C 混合
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C 混合
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