forked from PHengLEI/PHengLEI-TestCases
A23、B17、C01-C04、E01-E03、F07=F08算例参数及文档更新
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@ -1,65 +0,0 @@
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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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@ -24,6 +24,7 @@
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// 4 -- Grid deformation, achieve unstructured grid deformation.
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// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
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// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
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// 7 -- Grid type change, convert structured grid to unstructured grid.
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// multiblock: Multi-block grid or not, only for structured grid conversion.
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// 0 -- Not.
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// 1 -- Yes.
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@ -32,12 +33,23 @@
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// 0 -- X axis.
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// 1 -- Y axis.
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// 2 -- Z axis.
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// gridReorder: Reorder cell and face of grid or not, only for 3D unstructured grid conversion,
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// which is CGNS type.
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// 0 -- Not.
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// 1 -- Yes.
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// faceReorderMethod: the reorder method face of unstructured grid.
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// 0 -- BSFCELLFACEORG.
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// 1 -- BSFCELLFACELEFT.
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// 2 -- BSFCELLFACERIGHT.
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int gridtype = 0;
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int gridobj = 1;
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int multiblock = 0;
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int iadapt = 0;
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int SymmetryFaceVector = 1;
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int gridReorder = 0;
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int faceReorderMethod = 0;
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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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@ -61,6 +73,7 @@ int omit_no_bound_bc = 0;
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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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// dumpOldGrid: If dump out the old grid file.
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// 0 -- Not. (default)
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// 1 -- Yes.
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@ -82,7 +95,6 @@ string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
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// ----------------- some advanced choices ------------------------------
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// iunsteady: The Grid is for unsteady simulation or not.
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int iunsteady = 0;
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int codeOfAleModel = 0;
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// fileformat: Ustar Grid file format.
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// 0 -- BINARY.
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@ -102,12 +114,10 @@ string holeFullFileName = "./oversetGridView/holeFullFile.dat";
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string linkFileName = "./oversetGridView/topology.dat";
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string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
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// ----------------- Adaptive Mesh Refine -------------------------------
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// In this file, the original_grid_file is used of the partition part.
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// If use it dependently, abstract it here.
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string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
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string geometryFileName = "./grid/jsm.igs";
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// ----------------- Grid Refine Parameters -----------------------------
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// anisoRefine: If refine grid by anisoRefine type.
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// 0 -- Not. (default)
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// 1 -- Yes.
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// geometryUnit: Geometry unit.
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// 1 -- meter.
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// 2 -- millimeter.
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@ -117,14 +127,14 @@ string geometryFileName = "./grid/jsm.igs";
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// 1 -- JSM-C2-NPOFF case.
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// 2 -- CHNT.
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// projectOrgPoint: If the original wall points need to be projected or not.
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int geometryUnit = 1;
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int anisoRefine = 0;
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int geometryUnit = 1;
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int isProject = 0;
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int readDist = 0;
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int isDeform = 0;
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int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
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int projectOrgPoint = 0; // if project original wall points.
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int exclusiveCase = 0;
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int projectOrgPoint = 0;
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string geometryFileName = "./grid/jsm.igs";
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// ----------------- Grid Deform Parameters -----------------------------
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// deformationMethod: Grid Deform.
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@ -181,8 +191,11 @@ double rotationAngle = 0.0;
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// 1 -- struct grid.
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// 2 -- refine structured grid.
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// maxproc: The number of partition zones that want to be divided into.
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// numberOfMultifile: The number of partition grid files that want to be dumped out.
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int pgridtype = 0;
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int maxproc = 4;
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int numberOfMultifile = 1;
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// traceMark: Trace mark or not, only for structured grid partition.
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// 0 -- Not.
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@ -291,6 +304,7 @@ int compressible = 1;
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// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
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// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
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int directionMethod = 0;
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double refMachNumber = 0.73;
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double attackd = 2.79;
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double angleSlide = 0.00;
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@ -334,6 +348,7 @@ double wallTemperature = -1.0;
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double radiationCoef = 0.8;
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double gridScaleFactor = 1.0;
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double gridTranslationVector[] = [0.0, 0.0, 0.0];
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int numberOfAerodynamicForceComponents = 1;
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double forceReferenceLengthSpanWise = 1.0; // unit of meter.
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@ -355,11 +370,17 @@ double refMolecularWeight = 28.9644; // unit of g/mol.
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// -- "vanleer", "steger", "hlle", "lax_f".
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// -- "roe", "modified_roe".
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// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
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// isWennScheme: If using WENN Scheme of struct grid.
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// 0 -- NO. (default)
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// 1 -- Yes.
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// str_limiter_name: Limiter of struct grid.
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// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
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// -- "nolim", no limiter.
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// -- "vanalbada_clz", clz supersonic version.
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// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3"
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string inviscidSchemeName = "roe";
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int isWennScheme = 0;
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string str_limiter_name = "vanalbada";
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#*******************************************************************
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@ -421,6 +442,7 @@ string str_limiter_name = "vanalbada";
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// 3 -- Harten type, which is default used.
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// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
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// It is used to scale the default Roe entropy fix coefficients.
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// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0
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//int viscousType = 0;
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//string viscousName = "Euler";
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@ -451,6 +473,8 @@ double skewnessAngle = 60.0;
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int roeEntropyFixMethod = 3;
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double roeEntropyScale = 1.0;
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double AusmpwPlusLimiter = 1.0;
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//-----------------------------------------------------------------------
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# Temporal Discretisation #
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//-----------------------------------------------------------------------
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@ -466,8 +490,8 @@ double roeEntropyScale = 1.0;
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// statisticalTimePeriod: Used as time period of statistic analysis.
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// when the value is negative, time period is treated as infinite.
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// statisticMethod: Statistic reynolds stress method.
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0 --tau = <q^2> - <q>^2
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1 --tau = <u'u'>
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// 0 -- tau = <q^2> - <q>^2
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// 1 -- tau = <u'u'>
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// min_sub_iter: The min sub iteration of unsteady simulation.
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// max_sub_iter: The max sub iteration of unsteady simulation.
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// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
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@ -478,9 +502,8 @@ double roeEntropyScale = 1.0;
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// 4 -- LU-SGS.
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// 5 -- Block LU-SGS.
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// 6 -- Jacobian iteration.
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// 7 -- Lower G-S iteration.
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// 8 -- Upper G-S iteration.
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// 9 -- Lower/Upper G-S iteration.
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// 7 -- Line LU-SGS.
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// 8 -- Matrix LU-SGS.
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// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
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// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
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// CFLStart: Started cfl number.
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@ -493,6 +516,10 @@ double roeEntropyScale = 1.0;
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// ifLocalTimeStep: Time step method.
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// 0 --Local.
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// 1 --Global.
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// isUseLocalCFL: use variable number of CFL or not.
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// 0 -- global unified CFL number.
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// 1 -- local CFL number.
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// isUsePreTwall: use the previous temperatures on wall. 1 indicates yes, and 0 indicates no.
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// visl_min: Minimum value of laminar viscosity coefficient.
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// turbCFLScale: Turbulence model cfl number factor.
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// codeOfAleModel: Arbitrary Lagrangian-Eulerian method.
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@ -509,6 +536,7 @@ double roeEntropyScale = 1.0;
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int iunsteady = 0;
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double physicalTimeStep = 0.01;
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double physicalTimeStepDimensional = -0.001;
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int ifStartFromSteadyResults = 0;
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int ifStaticsFlowField = 0;
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int ifStaticsReynoldsStress = 0;
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@ -525,10 +553,18 @@ double tol_sub_iter = 0.01;
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int tscheme = 4;
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int iSimplifyViscousTerm = 1;
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int ifLocalTimeStep = 0;
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int isUseLocalCFL = 0;
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int isUsePreTwall = 0;
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double CFLStart = 0.01;
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double CFLEnd = 10.0;
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int CFLVaryStep = 500;
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double pMaxForCFL = 0.2;
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double pMinForCFL = 0.1;
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double deltaMaxForCFL = 0.2;
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double magnifyFactorForCFL = 1.1;
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double reduceFactorForCFL = 0.5;
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double ktmax = 1.0e10;
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int swapDq = 1;
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@ -548,7 +584,7 @@ double dtau = 0.001;
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int wallFunctionType = 0;
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int RKStage = 2;
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double lamda[] = 0.5, 1.0;
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double lamda[] = [0.5, 1.0];
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//int RKStage = 1;
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//double lamda[] = 1.0;
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@ -579,12 +615,20 @@ double lamda[] = 0.5, 1.0;
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// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
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// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux.
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// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux.
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// nIsComputeWallDist: Whether to compute the wall distance.
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// 0 -- Compute wall distance.
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// 1 -- Not compute.
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//
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// protectionFile0 and protectionFile1 : Two continuation file of the data protection mechanism.
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// wall_heatfluxfile : The file to output the MaxHeatFlux of wall.
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int numberOfGridGroups = 1;
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string gridfile = "./grid/rae2822_hybrid2d__4.fts";
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string wallTemperaturefile= "";
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int nIsComputeWallDist = 0;
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int walldistMethod = 1;
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int cellMethodOrNodeMethod = 0;
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string resSaveFile = "results/res.dat";
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string turbresfile = "results/turbres.dat";
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@ -597,6 +641,10 @@ string visualfile = "results/tecflow.plt";
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string wall_aircoefile = "results/wall_aircoef.dat";
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string samplefile = "results/sample.dat";
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string protectionFile0 = "results/flow0.dat";
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string protectionFile1 = "results/flow1.dat";
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string wall_heatfluxfile = "results/wall_heatflux.dat";
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int nDumpSurfaceInfo = 0;
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string wall_varfile = "";
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@ -648,7 +696,10 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
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// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
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// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
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// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
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// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), iblank(81).
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// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
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// -- transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
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// -- overlap iblank(iblank, 81)
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// -- specific heat ratio(gama, 56)
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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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@ -660,10 +711,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
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// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
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// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
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// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
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// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
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// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
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// -overlap iblank(iblank, 81)
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// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -Grid Reynolds number on wall(Re_w, 23)
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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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@ -691,7 +739,7 @@ int dumpStandardModel = 0;
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// 1 -- Real cell where the probe is located.
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// nProbeVariables: Number of variables want to be dumped for probes monitered.
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// probeVariables : Variable types dumped, listed as following:
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// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
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// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6).
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// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
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// probeVariables order must from small to big.
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// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables.
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@ -713,8 +761,8 @@ string probesDefineFile = "bin/probes_XYZ.dat";
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int searchCellsMethod = 0;
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int nProbeVariables = 6;
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int probeVariables[] = [0, 1, 2, 3, 4, 5];
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int nProbeVariables = 7;
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int probeVariables[] = [0, 1, 2, 3, 4, 5, 6];
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int probeVariablesInterpolationMethod = 0;
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//-----------------------------------------------------------------------
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# Turbulence Parameter #
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@ -722,9 +770,13 @@ int probeVariablesInterpolationMethod = 0;
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// turbInterval: Iteration number of turbulence.
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// kindOfTurbSource: Kinds of turbulent source.
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// 0 -- Original.
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// 1 -- Edwards.
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// 2 -- new.
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// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
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// transitionType: transition model type
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// 0 -- none.
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// 2 -- gama-re-theta.
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// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition
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// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not
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int turbInterval = 1;
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int turbOrderStruct = 2;
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@ -739,6 +791,7 @@ double turbIntensity = -1.0;
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int freeturbIntensitySRModify = 0;
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double freeDecayXLocation = 0.0;
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int compressibleCorrection = 0;
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int prandtlNumberCorrection = 0;
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int transitionMaFix = 1;
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# maximum eddy viscosity (myt/my) max.
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@ -749,7 +802,7 @@ int monitor_vistmax = 0;
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# LES Parameter #
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//-----------------------------------------------------------------------
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// iLES: Create LESSolver or not.
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// == 1 - Create LESSolver;
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// = 1 - Create LESSolver;
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// != 1 - not.
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// amplitudeofDisturb: Amplitude of adding disturb.
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// disturbstep: Unsteady time step or steady iteration of adding random disturb.
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@ -808,9 +861,10 @@ int monitorNegativeConstant = 0;
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// iapplication:
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// 0 -- gas model is fixed in the codes.
|
||||
// 1 -- gas model is imported from library files.
|
||||
// iCodeBranch:
|
||||
// 0 -- The old code version is used for Navier-Stokes.
|
||||
// 1 -- A new code version is active for Navier-Stokes solver.
|
||||
// isAdaptiveSolver: isAdaptiveSolver=0 indicates the generic Navier-Stokes solver,
|
||||
// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver.
|
||||
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
|
||||
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -824,7 +878,6 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
|
|
@ -860,9 +913,13 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nIdealState: whether take all gas species as ideal gas for gas-mixture process.
|
||||
// 0 -- No.
|
||||
// 1 -- Yes.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// 1 -- the energy term is computed using the polynomial fitting method.
|
||||
// 2 -- the energy term is computed using the piecewise polynomial fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
|
|
@ -875,6 +932,13 @@ int monitorNegativeConstant = 0;
|
|||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// nSurfGradMethod : the method to compute the surface heating ratio.
|
||||
// 0 -- the gradient of variable is computed with the first-order difference method.
|
||||
// 1 -- the gradient of variable is computed with the Green-Guass integral method.
|
||||
// nRapidFlowfield : initialize the flowfield using the rapid engineering method when it is greater than zero.
|
||||
// nSurfHeatMonitor : To exam the surface heating change or not. 0 is no, 1 is yes.
|
||||
// nInitPressureStep : the steps to initialize the boundary variables when the rapid method is used. 100 is the default value.
|
||||
// nDumpCFLNumber : 1 indicates dumping the CFL number to file, 0 denotes no dumping.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
|
|
@ -884,13 +948,17 @@ int monitorNegativeConstant = 0;
|
|||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// spectrumRadiusCoef: The value is in range of [0.0, 2.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
|
||||
//maxViscous: the maximum of Viscous.
|
||||
//trTemperatureMin: the minimum value of trTemperature.
|
||||
//veTemperatureMin: the minimum value of veTemperature.
|
||||
//densityMin: the minimum value of density.
|
||||
//tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0].
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
|
|
@ -903,9 +971,30 @@ int monitorNegativeConstant = 0;
|
|||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nViscosityPeModified: Pe Modified for ViscosityCoef
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceEsMethod: Modified on ChemcalSource
|
||||
// 0 -- approximation algorithm 1 (Ori.)
|
||||
// 1 -- approximation algorithm 2 (New)
|
||||
|
||||
// nMaxStepTemperature: the iterative steps of temperature.
|
||||
|
||||
// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs
|
||||
// 0 -- not used
|
||||
// 1 -- used
|
||||
|
||||
// nDiagonalModified: Modified on Diagonal
|
||||
// 0 -- not used
|
||||
// 1 -- Ori.
|
||||
// 2 -- new
|
||||
|
||||
//nGradPrimtiveMethod:
|
||||
// 0 -- Ori.
|
||||
// 1 -- new
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
|
|
@ -913,9 +1002,11 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// 0 -- Blottner fitting method(N89).
|
||||
// 1 -- Gupta fitting method(N90).
|
||||
// nContinueModel: The new continue model can switch different computation model.
|
||||
// 0 -- Not use the new continue model.
|
||||
// 1 -- use the new continue model.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
|
|
@ -925,20 +1016,54 @@ int monitorNegativeConstant = 0;
|
|||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// "Gas-Mixture" -- indicates the process of mixing gas without reacting.
|
||||
// for struct solver mixing two species£¨SpeciesA, SpeciesB£©.
|
||||
// for unstruct solver mixing multi-species£¨O2 NO CO CO2 H2 N2 Air CH4£©.
|
||||
// For self-definition model, the gasfile is used to indicate the file path of the new gas model.
|
||||
// speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma.
|
||||
// initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName.
|
||||
// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes.
|
||||
// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation.
|
||||
// nIterSecondStep : the maximum number of iteration in the second step for the self-adaptive calculation.
|
||||
// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation.
|
||||
// nEnergyAssembly : the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory.
|
||||
// 0 -- no,
|
||||
// 1 -- yes.
|
||||
// nControlVariable: the variable to computing the residual error that determines the convergence is meet or not in the one-temperature model.
|
||||
// 0 -- the density.
|
||||
// 1 -- the translation temperature.
|
||||
// 2 -- the vibration temperature.
|
||||
// 3 -- the electron temperature.
|
||||
// 4 -- the pressure.
|
||||
// 5 -- the mass fraction of oxygen.
|
||||
// 6 -- the mass fraction of nitrogen.
|
||||
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
|
||||
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
|
||||
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
|
||||
// useHyflowSetting : Setting for HyFLOW GUI.
|
||||
// 0 -- PHengLEI
|
||||
// 1 -- HyFLOW
|
||||
// nProtectData : Use the continuation file data protection mechanism.
|
||||
// 0 -- no
|
||||
// 1 -- yes
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int isAdaptiveSolver = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
int nIterFirstStep = 1000;
|
||||
int nIterSecondStep= 2000;
|
||||
int nIterThirdStep = 2000;
|
||||
int nEnergyAssembly = 0;
|
||||
int nControlVariable = 1;
|
||||
double firstStepError = 0.01;
|
||||
double secondStepError = 0.001;
|
||||
double thirdStepError = 0.001;
|
||||
double predictCFLError = 0.1;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -952,7 +1077,8 @@ int nchemsrc = 1;
|
|||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nIdealState = 0;
|
||||
int nEnergyRecycle = 1;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
|
|
@ -960,6 +1086,11 @@ int nMeanFreePathType = 0;
|
|||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
int nSurfGradMethod = 0;
|
||||
int nRapidFlowfield = 0;
|
||||
int nSurfHeatMonitor = 0;
|
||||
int nInitPressureStep = 100;
|
||||
int nDumpCFLNumber = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
|
|
@ -970,17 +1101,38 @@ double velocitySlipCorrectConstant = 1.0;
|
|||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.5;
|
||||
double inviscidSpectrumRadiusCoef = 1.5;
|
||||
double spectrumRadiusCoef = 0.5;
|
||||
double staticPressureRelaxCorf = 0.2;
|
||||
|
||||
double maxViscous = 10000.0;
|
||||
double trTemperatureMin = 10.0;
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
double maxTemperature = 50000.0;
|
||||
double densityMin = 1.0e-8;
|
||||
double densityMinFactor = 0.1;
|
||||
double tAdjustmentFactor = 10.0;
|
||||
double iniSpeedCoef = 1.0;
|
||||
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 1;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 1;
|
||||
int nViscosityPeModified = 0;
|
||||
int nChemcalSourceModified = 2;
|
||||
int nChemcalSourceEsMethod = 1;
|
||||
int nMaxStepTemperature = 5;
|
||||
int veTemperatureMinModified = 1;
|
||||
int nDiagonalModified = 0;
|
||||
int nGradPrimtiveMethod = 1;
|
||||
int nInviscidFluxModify = 1;
|
||||
int nQlLimitMethod = 2;
|
||||
int nSpeciesForWallMethod = 1;
|
||||
int nDensityForWallMethod = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1000,7 +1152,7 @@ string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
|||
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
|
||||
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string gasfile = "Pa";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
|
|
@ -1017,6 +1169,11 @@ double gamaSpeciesB = 1.3;
|
|||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName = "O2, N2";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
|
|
@ -1124,7 +1281,7 @@ int codeOfOversetGrid = 0;
|
|||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
int readInAuxiliaryInnerGrid = 0;
|
||||
int readInAuxiliaryOuterGrid = 0;
|
||||
int readInSklFileOrNot = 0;
|
||||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
|
|
@ -1137,13 +1294,18 @@ double toleranceForOversetBox = 1.0e-3;
|
|||
int twoOrderInterpolationOrNot = 0;
|
||||
int keyEnlargeOfActiveNodes = 0;
|
||||
int outTecplotOverset = 0;
|
||||
int outPutOversetVisualization = 0;
|
||||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
double referenceLength = 1.0;
|
||||
double referenceVelocity = 1.0;
|
||||
double referenceDensity = 1.0;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
|
|
@ -1187,6 +1349,11 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0
|
|||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//direction of rotation
|
||||
// 1 -- clockwise from the point of view along the positive x axis.
|
||||
// -1 -- anticlockwise from the point of view along the positive x axis.
|
||||
int direction_0 = -1;
|
||||
double rotateFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
|
|
@ -1218,3 +1385,12 @@ int integralOrder = 4;
|
|||
#########################################################################
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
|
||||
#########################################################################
|
||||
# Incompressible Parameter #
|
||||
#########################################################################
|
||||
|
||||
int isSolveEnergyEquation = 0;
|
||||
int isSolveTurbEquation = 0;
|
||||
int isSolveSpeciesEquation = 0;
|
||||
|
||||
|
|
|
|||
|
|
@ -23,7 +23,7 @@ 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";
|
||||
//string parafilename = "./bin/cfd_para_incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
|
@ -37,14 +37,8 @@ string parafilename = "./bin/cfd_para_subsonic.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 = 1;
|
||||
//string parafilename = "./bin/grid_refine_para.hypara";
|
||||
|
||||
//int nsimutask = 14;
|
||||
//string parafilename = "./bin/integrative_solver.hypara";
|
||||
|
|
|
|||
Binary file not shown.
|
|
@ -1,69 +0,0 @@
|
|||
# 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
|
||||
|
|
@ -24,6 +24,7 @@
|
|||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// 7 -- Grid type change, convert structured grid to unstructured grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
|
|
@ -32,12 +33,23 @@
|
|||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
// gridReorder: Reorder cell and face of grid or not, only for 3D unstructured grid conversion,
|
||||
// which is CGNS type.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// faceReorderMethod: the reorder method face of unstructured grid.
|
||||
// 0 -- BSFCELLFACEORG.
|
||||
// 1 -- BSFCELLFACELEFT.
|
||||
// 2 -- BSFCELLFACERIGHT.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int iadapt = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
int gridReorder = 0;
|
||||
int faceReorderMethod = 0;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
|
|
@ -61,6 +73,7 @@ int omit_no_bound_bc = 0;
|
|||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
// 9 -- Gridgen type of structured grid, *.dat/*.grd.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
|
|
@ -82,7 +95,6 @@ string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
|||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
|
|
@ -102,12 +114,10 @@ string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
|||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Refine Parameters -----------------------------
|
||||
// anisoRefine: If refine grid by anisoRefine type.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
|
|
@ -117,14 +127,14 @@ string geometryFileName = "./grid/jsm.igs";
|
|||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int geometryUnit = 1;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
int exclusiveCase = 0;
|
||||
int projectOrgPoint = 0;
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
|
|
@ -181,8 +191,11 @@ double rotationAngle = 0.0;
|
|||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
// numberOfMultifile: The number of partition grid files that want to be dumped out.
|
||||
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
int numberOfMultifile = 1;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
|
|
@ -291,6 +304,7 @@ int compressible = 1;
|
|||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
int directionMethod = 0;
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
|
@ -334,6 +348,7 @@ double wallTemperature = -1.0;
|
|||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
double gridTranslationVector[] = [0.0, 0.0, 0.0];
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
|
|
@ -355,11 +370,17 @@ double refMolecularWeight = 28.9644; // unit of g/mol.
|
|||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// isWennScheme: If using WENN Scheme of struct grid.
|
||||
// 0 -- NO. (default)
|
||||
// 1 -- Yes.
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3"
|
||||
|
||||
string inviscidSchemeName = "roe";
|
||||
int isWennScheme = 0;
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
|
|
@ -421,6 +442,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
|
@ -451,6 +473,8 @@ double skewnessAngle = 60.0;
|
|||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
double AusmpwPlusLimiter = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -466,8 +490,8 @@ double roeEntropyScale = 1.0;
|
|||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 0 -- tau = <q^2> - <q>^2
|
||||
// 1 -- tau = <u'u'>
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
|
|
@ -478,9 +502,8 @@ double roeEntropyScale = 1.0;
|
|||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// 7 -- Line LU-SGS.
|
||||
// 8 -- Matrix LU-SGS.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
|
|
@ -493,6 +516,10 @@ double roeEntropyScale = 1.0;
|
|||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// isUseLocalCFL: use variable number of CFL or not.
|
||||
// 0 -- global unified CFL number.
|
||||
// 1 -- local CFL number.
|
||||
// isUsePreTwall: use the previous temperatures on wall. 1 indicates yes, and 0 indicates no.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// codeOfAleModel: Arbitrary Lagrangian-Eulerian method.
|
||||
|
|
@ -509,6 +536,7 @@ double roeEntropyScale = 1.0;
|
|||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
double physicalTimeStepDimensional = -0.001;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
|
|
@ -525,10 +553,18 @@ double tol_sub_iter = 0.01;
|
|||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
int isUseLocalCFL = 0;
|
||||
int isUsePreTwall = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
double magnifyFactorForCFL = 1.1;
|
||||
double reduceFactorForCFL = 0.5;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
|
@ -548,7 +584,7 @@ double dtau = 0.001;
|
|||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
double lamda[] = [0.5, 1.0];
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
|
@ -579,12 +615,20 @@ double lamda[] = 0.5, 1.0;
|
|||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux.
|
||||
// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux.
|
||||
// nIsComputeWallDist: Whether to compute the wall distance.
|
||||
// 0 -- Compute wall distance.
|
||||
// 1 -- Not compute.
|
||||
//
|
||||
// protectionFile0 and protectionFile1 : Two continuation file of the data protection mechanism.
|
||||
// wall_heatfluxfile : The file to output the MaxHeatFlux of wall.
|
||||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int nIsComputeWallDist = 0;
|
||||
int walldistMethod = 1;
|
||||
int cellMethodOrNodeMethod = 0;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
|
|
@ -597,6 +641,10 @@ string visualfile = "results/tecflow.plt";
|
|||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
string protectionFile0 = "results/flow0.dat";
|
||||
string protectionFile1 = "results/flow1.dat";
|
||||
string wall_heatfluxfile = "results/wall_heatflux.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
|
|
@ -648,7 +696,10 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
|
||||
// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
|
||||
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), iblank(81).
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
|
||||
// -- transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -- overlap iblank(iblank, 81)
|
||||
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
|
@ -660,10 +711,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -Grid Reynolds number on wall(Re_w, 23)
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
|
|
@ -691,7 +739,7 @@ int dumpStandardModel = 0;
|
|||
// 1 -- Real cell where the probe is located.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables.
|
||||
|
|
@ -713,8 +761,8 @@ string probesDefineFile = "bin/probes_XYZ.dat";
|
|||
|
||||
int searchCellsMethod = 0;
|
||||
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
int nProbeVariables = 7;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5, 6];
|
||||
int probeVariablesInterpolationMethod = 0;
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
|
|
@ -722,9 +770,13 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
// transitionType: transition model type
|
||||
// 0 -- none.
|
||||
// 2 -- gama-re-theta.
|
||||
// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition
|
||||
// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not
|
||||
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
|
|
@ -739,6 +791,7 @@ double turbIntensity = -1.0;
|
|||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int prandtlNumberCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
|
|
@ -749,7 +802,7 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// == 1 - Create LESSolver;
|
||||
// = 1 - Create LESSolver;
|
||||
// != 1 - not.
|
||||
// amplitudeofDisturb: Amplitude of adding disturb.
|
||||
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
|
||||
|
|
@ -808,9 +861,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 1 -- gas model is imported from library files.
|
||||
// iCodeBranch:
|
||||
// 0 -- The old code version is used for Navier-Stokes.
|
||||
// 1 -- A new code version is active for Navier-Stokes solver.
|
||||
// isAdaptiveSolver: isAdaptiveSolver=0 indicates the generic Navier-Stokes solver,
|
||||
// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver.
|
||||
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
|
||||
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -824,7 +878,6 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
|
|
@ -860,9 +913,13 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nIdealState: whether take all gas species as ideal gas for gas-mixture process.
|
||||
// 0 -- No.
|
||||
// 1 -- Yes.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// 1 -- the energy term is computed using the polynomial fitting method.
|
||||
// 2 -- the energy term is computed using the piecewise polynomial fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
|
|
@ -875,6 +932,13 @@ int monitorNegativeConstant = 0;
|
|||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// nSurfGradMethod : the method to compute the surface heating ratio.
|
||||
// 0 -- the gradient of variable is computed with the first-order difference method.
|
||||
// 1 -- the gradient of variable is computed with the Green-Guass integral method.
|
||||
// nRapidFlowfield : initialize the flowfield using the rapid engineering method when it is greater than zero.
|
||||
// nSurfHeatMonitor : To exam the surface heating change or not. 0 is no, 1 is yes.
|
||||
// nInitPressureStep : the steps to initialize the boundary variables when the rapid method is used. 100 is the default value.
|
||||
// nDumpCFLNumber : 1 indicates dumping the CFL number to file, 0 denotes no dumping.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
|
|
@ -884,13 +948,17 @@ int monitorNegativeConstant = 0;
|
|||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// spectrumRadiusCoef: The value is in range of [0.0, 2.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
|
||||
//maxViscous: the maximum of Viscous.
|
||||
//trTemperatureMin: the minimum value of trTemperature.
|
||||
//veTemperatureMin: the minimum value of veTemperature.
|
||||
//densityMin: the minimum value of density.
|
||||
//tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0].
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
|
|
@ -903,9 +971,30 @@ int monitorNegativeConstant = 0;
|
|||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nViscosityPeModified: Pe Modified for ViscosityCoef
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceEsMethod: Modified on ChemcalSource
|
||||
// 0 -- approximation algorithm 1 (Ori.)
|
||||
// 1 -- approximation algorithm 2 (New)
|
||||
|
||||
// nMaxStepTemperature: the iterative steps of temperature.
|
||||
|
||||
// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs
|
||||
// 0 -- not used
|
||||
// 1 -- used
|
||||
|
||||
// nDiagonalModified: Modified on Diagonal
|
||||
// 0 -- not used
|
||||
// 1 -- Ori.
|
||||
// 2 -- new
|
||||
|
||||
//nGradPrimtiveMethod:
|
||||
// 0 -- Ori.
|
||||
// 1 -- new
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
|
|
@ -913,9 +1002,11 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// 0 -- Blottner fitting method(N89).
|
||||
// 1 -- Gupta fitting method(N90).
|
||||
// nContinueModel: The new continue model can switch different computation model.
|
||||
// 0 -- Not use the new continue model.
|
||||
// 1 -- use the new continue model.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
|
|
@ -925,20 +1016,54 @@ int monitorNegativeConstant = 0;
|
|||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// "Gas-Mixture" -- indicates the process of mixing gas without reacting.
|
||||
// for struct solver mixing two species£¨SpeciesA, SpeciesB£©.
|
||||
// for unstruct solver mixing multi-species£¨O2 NO CO CO2 H2 N2 Air CH4£©.
|
||||
// For self-definition model, the gasfile is used to indicate the file path of the new gas model.
|
||||
// speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma.
|
||||
// initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName.
|
||||
// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes.
|
||||
// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation.
|
||||
// nIterSecondStep : the maximum number of iteration in the second step for the self-adaptive calculation.
|
||||
// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation.
|
||||
// nEnergyAssembly : the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory.
|
||||
// 0 -- no,
|
||||
// 1 -- yes.
|
||||
// nControlVariable: the variable to computing the residual error that determines the convergence is meet or not in the one-temperature model.
|
||||
// 0 -- the density.
|
||||
// 1 -- the translation temperature.
|
||||
// 2 -- the vibration temperature.
|
||||
// 3 -- the electron temperature.
|
||||
// 4 -- the pressure.
|
||||
// 5 -- the mass fraction of oxygen.
|
||||
// 6 -- the mass fraction of nitrogen.
|
||||
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
|
||||
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
|
||||
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
|
||||
// useHyflowSetting : Setting for HyFLOW GUI.
|
||||
// 0 -- PHengLEI
|
||||
// 1 -- HyFLOW
|
||||
// nProtectData : Use the continuation file data protection mechanism.
|
||||
// 0 -- no
|
||||
// 1 -- yes
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int isAdaptiveSolver = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
int nIterFirstStep = 1000;
|
||||
int nIterSecondStep= 2000;
|
||||
int nIterThirdStep = 2000;
|
||||
int nEnergyAssembly = 0;
|
||||
int nControlVariable = 1;
|
||||
double firstStepError = 0.01;
|
||||
double secondStepError = 0.001;
|
||||
double thirdStepError = 0.001;
|
||||
double predictCFLError = 0.1;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -952,7 +1077,8 @@ int nchemsrc = 1;
|
|||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nIdealState = 0;
|
||||
int nEnergyRecycle = 1;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
|
|
@ -960,6 +1086,11 @@ int nMeanFreePathType = 0;
|
|||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
int nSurfGradMethod = 0;
|
||||
int nRapidFlowfield = 0;
|
||||
int nSurfHeatMonitor = 0;
|
||||
int nInitPressureStep = 100;
|
||||
int nDumpCFLNumber = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
|
|
@ -970,17 +1101,38 @@ double velocitySlipCorrectConstant = 1.0;
|
|||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.5;
|
||||
double inviscidSpectrumRadiusCoef = 1.5;
|
||||
double spectrumRadiusCoef = 0.5;
|
||||
double staticPressureRelaxCorf = 0.2;
|
||||
|
||||
double maxViscous = 10000.0;
|
||||
double trTemperatureMin = 10.0;
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
double maxTemperature = 50000.0;
|
||||
double densityMin = 1.0e-8;
|
||||
double densityMinFactor = 0.1;
|
||||
double tAdjustmentFactor = 10.0;
|
||||
double iniSpeedCoef = 1.0;
|
||||
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 1;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 1;
|
||||
int nViscosityPeModified = 0;
|
||||
int nChemcalSourceModified = 2;
|
||||
int nChemcalSourceEsMethod = 1;
|
||||
int nMaxStepTemperature = 5;
|
||||
int veTemperatureMinModified = 1;
|
||||
int nDiagonalModified = 0;
|
||||
int nGradPrimtiveMethod = 1;
|
||||
int nInviscidFluxModify = 1;
|
||||
int nQlLimitMethod = 2;
|
||||
int nSpeciesForWallMethod = 1;
|
||||
int nDensityForWallMethod = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1000,7 +1152,7 @@ string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
|||
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
|
||||
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string gasfile = "Pa";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
|
|
@ -1017,6 +1169,11 @@ double gamaSpeciesB = 1.3;
|
|||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName = "O2, N2";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
|
|
@ -1124,7 +1281,7 @@ int codeOfOversetGrid = 0;
|
|||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
int readInAuxiliaryInnerGrid = 0;
|
||||
int readInAuxiliaryOuterGrid = 0;
|
||||
int readInSklFileOrNot = 0;
|
||||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
|
|
@ -1137,13 +1294,18 @@ double toleranceForOversetBox = 1.0e-3;
|
|||
int twoOrderInterpolationOrNot = 0;
|
||||
int keyEnlargeOfActiveNodes = 0;
|
||||
int outTecplotOverset = 0;
|
||||
int outPutOversetVisualization = 0;
|
||||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
double referenceLength = 1.0;
|
||||
double referenceVelocity = 1.0;
|
||||
double referenceDensity = 1.0;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
|
|
@ -1187,6 +1349,11 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0
|
|||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//direction of rotation
|
||||
// 1 -- clockwise from the point of view along the positive x axis.
|
||||
// -1 -- anticlockwise from the point of view along the positive x axis.
|
||||
int direction_0 = -1;
|
||||
double rotateFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
|
|
@ -1218,3 +1385,12 @@ int integralOrder = 4;
|
|||
#########################################################################
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
|
||||
#########################################################################
|
||||
# Incompressible Parameter #
|
||||
#########################################################################
|
||||
|
||||
int isSolveEnergyEquation = 0;
|
||||
int isSolveTurbEquation = 0;
|
||||
int isSolveSpeciesEquation = 0;
|
||||
|
||||
|
|
|
|||
|
|
@ -23,7 +23,7 @@ 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";
|
||||
//string parafilename = "./bin/cfd_para_incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
|
@ -37,14 +37,8 @@ string parafilename = "./bin/cfd_para_subsonic.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 = 1;
|
||||
//string parafilename = "./bin/grid_refine_para.hypara";
|
||||
|
||||
//int nsimutask = 14;
|
||||
//string parafilename = "./bin/integrative_solver.hypara";
|
||||
|
|
|
|||
Binary file not shown.
|
|
@ -1,52 +0,0 @@
|
|||
# nBoundaryConditons : number of global boundary conditions.
|
||||
# bcName : Boundary Condition Name.
|
||||
# bcType(in PHengLEI): Boundary Condition Type.
|
||||
|
||||
# Account of how to set boundaryconditon.
|
||||
# string bcName = "Farfield";
|
||||
# {
|
||||
# int bcType = 4;
|
||||
# int inflowParaType = 1;
|
||||
# double attackd = 0;
|
||||
# double refReNumber = 6.5e6;
|
||||
# double refMachNumber = 3.5;
|
||||
# double angleSlide = 0;
|
||||
# }
|
||||
|
||||
int nBoundaryConditons = 5;
|
||||
string bcName = "Interface";
|
||||
{
|
||||
int bcType = -1;
|
||||
}
|
||||
string bcName = "mixgridinterior";
|
||||
{
|
||||
int bcType = -1;
|
||||
}
|
||||
string bcName = "wall";
|
||||
{
|
||||
int bcType = 2;
|
||||
}
|
||||
string bcName = "in";
|
||||
{
|
||||
int bcType = 5;
|
||||
}
|
||||
string bcName = "out";
|
||||
{
|
||||
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
|
||||
|
|
@ -24,6 +24,7 @@
|
|||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// 7 -- Grid type change, convert structured grid to unstructured grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
|
|
@ -32,12 +33,23 @@
|
|||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
// gridReorder: Reorder cell and face of grid or not, only for 3D unstructured grid conversion,
|
||||
// which is CGNS type.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// faceReorderMethod: the reorder method face of unstructured grid.
|
||||
// 0 -- BSFCELLFACEORG.
|
||||
// 1 -- BSFCELLFACELEFT.
|
||||
// 2 -- BSFCELLFACERIGHT.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int iadapt = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
int gridReorder = 0;
|
||||
int faceReorderMethod = 0;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
|
|
@ -61,6 +73,7 @@ int omit_no_bound_bc = 0;
|
|||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
// 9 -- Gridgen type of structured grid, *.dat/*.grd.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
|
|
@ -82,7 +95,6 @@ string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
|||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
|
|
@ -102,12 +114,10 @@ string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
|||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Refine Parameters -----------------------------
|
||||
// anisoRefine: If refine grid by anisoRefine type.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
|
|
@ -117,14 +127,14 @@ string geometryFileName = "./grid/jsm.igs";
|
|||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int geometryUnit = 1;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
int exclusiveCase = 0;
|
||||
int projectOrgPoint = 0;
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
|
|
@ -181,8 +191,11 @@ double rotationAngle = 0.0;
|
|||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
// numberOfMultifile: The number of partition grid files that want to be dumped out.
|
||||
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
int numberOfMultifile = 1;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
|
|
@ -291,6 +304,7 @@ int compressible = 1;
|
|||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
int directionMethod = 0;
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
|
@ -334,6 +348,7 @@ double wallTemperature = -1.0;
|
|||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
double gridTranslationVector[] = [0.0, 0.0, 0.0];
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
|
|
@ -355,11 +370,17 @@ double refMolecularWeight = 28.9644; // unit of g/mol.
|
|||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// isWennScheme: If using WENN Scheme of struct grid.
|
||||
// 0 -- NO. (default)
|
||||
// 1 -- Yes.
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3"
|
||||
|
||||
string inviscidSchemeName = "roe";
|
||||
int isWennScheme = 0;
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
|
|
@ -421,6 +442,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
|
@ -451,6 +473,8 @@ double skewnessAngle = 60.0;
|
|||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
double AusmpwPlusLimiter = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -466,8 +490,8 @@ double roeEntropyScale = 1.0;
|
|||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 0 -- tau = <q^2> - <q>^2
|
||||
// 1 -- tau = <u'u'>
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
|
|
@ -478,9 +502,8 @@ double roeEntropyScale = 1.0;
|
|||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// 7 -- Line LU-SGS.
|
||||
// 8 -- Matrix LU-SGS.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
|
|
@ -493,6 +516,10 @@ double roeEntropyScale = 1.0;
|
|||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// isUseLocalCFL: use variable number of CFL or not.
|
||||
// 0 -- global unified CFL number.
|
||||
// 1 -- local CFL number.
|
||||
// isUsePreTwall: use the previous temperatures on wall. 1 indicates yes, and 0 indicates no.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// codeOfAleModel: Arbitrary Lagrangian-Eulerian method.
|
||||
|
|
@ -509,6 +536,7 @@ double roeEntropyScale = 1.0;
|
|||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
double physicalTimeStepDimensional = -0.001;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
|
|
@ -525,10 +553,18 @@ double tol_sub_iter = 0.01;
|
|||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
int isUseLocalCFL = 0;
|
||||
int isUsePreTwall = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
double magnifyFactorForCFL = 1.1;
|
||||
double reduceFactorForCFL = 0.5;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
|
@ -548,7 +584,7 @@ double dtau = 0.001;
|
|||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
double lamda[] = [0.5, 1.0];
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
|
@ -579,12 +615,20 @@ double lamda[] = 0.5, 1.0;
|
|||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux.
|
||||
// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux.
|
||||
// nIsComputeWallDist: Whether to compute the wall distance.
|
||||
// 0 -- Compute wall distance.
|
||||
// 1 -- Not compute.
|
||||
//
|
||||
// protectionFile0 and protectionFile1 : Two continuation file of the data protection mechanism.
|
||||
// wall_heatfluxfile : The file to output the MaxHeatFlux of wall.
|
||||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int nIsComputeWallDist = 0;
|
||||
int walldistMethod = 1;
|
||||
int cellMethodOrNodeMethod = 0;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
|
|
@ -597,6 +641,10 @@ string visualfile = "results/tecflow.plt";
|
|||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
string protectionFile0 = "results/flow0.dat";
|
||||
string protectionFile1 = "results/flow1.dat";
|
||||
string wall_heatfluxfile = "results/wall_heatflux.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
|
|
@ -648,7 +696,10 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
|
||||
// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
|
||||
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), iblank(81).
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
|
||||
// -- transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -- overlap iblank(iblank, 81)
|
||||
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
|
@ -660,10 +711,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -Grid Reynolds number on wall(Re_w, 23)
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
|
|
@ -691,7 +739,7 @@ int dumpStandardModel = 0;
|
|||
// 1 -- Real cell where the probe is located.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables.
|
||||
|
|
@ -713,8 +761,8 @@ string probesDefineFile = "bin/probes_XYZ.dat";
|
|||
|
||||
int searchCellsMethod = 0;
|
||||
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
int nProbeVariables = 7;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5, 6];
|
||||
int probeVariablesInterpolationMethod = 0;
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
|
|
@ -722,9 +770,13 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
// transitionType: transition model type
|
||||
// 0 -- none.
|
||||
// 2 -- gama-re-theta.
|
||||
// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition
|
||||
// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not
|
||||
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
|
|
@ -739,6 +791,7 @@ double turbIntensity = -1.0;
|
|||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int prandtlNumberCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
|
|
@ -749,7 +802,7 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// == 1 - Create LESSolver;
|
||||
// = 1 - Create LESSolver;
|
||||
// != 1 - not.
|
||||
// amplitudeofDisturb: Amplitude of adding disturb.
|
||||
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
|
||||
|
|
@ -808,9 +861,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 1 -- gas model is imported from library files.
|
||||
// iCodeBranch:
|
||||
// 0 -- The old code version is used for Navier-Stokes.
|
||||
// 1 -- A new code version is active for Navier-Stokes solver.
|
||||
// isAdaptiveSolver: isAdaptiveSolver=0 indicates the generic Navier-Stokes solver,
|
||||
// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver.
|
||||
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
|
||||
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -824,7 +878,6 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
|
|
@ -860,9 +913,13 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nIdealState: whether take all gas species as ideal gas for gas-mixture process.
|
||||
// 0 -- No.
|
||||
// 1 -- Yes.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// 1 -- the energy term is computed using the polynomial fitting method.
|
||||
// 2 -- the energy term is computed using the piecewise polynomial fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
|
|
@ -875,6 +932,13 @@ int monitorNegativeConstant = 0;
|
|||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// nSurfGradMethod : the method to compute the surface heating ratio.
|
||||
// 0 -- the gradient of variable is computed with the first-order difference method.
|
||||
// 1 -- the gradient of variable is computed with the Green-Guass integral method.
|
||||
// nRapidFlowfield : initialize the flowfield using the rapid engineering method when it is greater than zero.
|
||||
// nSurfHeatMonitor : To exam the surface heating change or not. 0 is no, 1 is yes.
|
||||
// nInitPressureStep : the steps to initialize the boundary variables when the rapid method is used. 100 is the default value.
|
||||
// nDumpCFLNumber : 1 indicates dumping the CFL number to file, 0 denotes no dumping.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
|
|
@ -884,13 +948,17 @@ int monitorNegativeConstant = 0;
|
|||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// spectrumRadiusCoef: The value is in range of [0.0, 2.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
|
||||
//maxViscous: the maximum of Viscous.
|
||||
//trTemperatureMin: the minimum value of trTemperature.
|
||||
//veTemperatureMin: the minimum value of veTemperature.
|
||||
//densityMin: the minimum value of density.
|
||||
//tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0].
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
|
|
@ -903,9 +971,30 @@ int monitorNegativeConstant = 0;
|
|||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nViscosityPeModified: Pe Modified for ViscosityCoef
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceEsMethod: Modified on ChemcalSource
|
||||
// 0 -- approximation algorithm 1 (Ori.)
|
||||
// 1 -- approximation algorithm 2 (New)
|
||||
|
||||
// nMaxStepTemperature: the iterative steps of temperature.
|
||||
|
||||
// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs
|
||||
// 0 -- not used
|
||||
// 1 -- used
|
||||
|
||||
// nDiagonalModified: Modified on Diagonal
|
||||
// 0 -- not used
|
||||
// 1 -- Ori.
|
||||
// 2 -- new
|
||||
|
||||
//nGradPrimtiveMethod:
|
||||
// 0 -- Ori.
|
||||
// 1 -- new
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
|
|
@ -913,9 +1002,11 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// 0 -- Blottner fitting method(N89).
|
||||
// 1 -- Gupta fitting method(N90).
|
||||
// nContinueModel: The new continue model can switch different computation model.
|
||||
// 0 -- Not use the new continue model.
|
||||
// 1 -- use the new continue model.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
|
|
@ -925,20 +1016,54 @@ int monitorNegativeConstant = 0;
|
|||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// "Gas-Mixture" -- indicates the process of mixing gas without reacting.
|
||||
// for struct solver mixing two species£¨SpeciesA, SpeciesB£©.
|
||||
// for unstruct solver mixing multi-species£¨O2 NO CO CO2 H2 N2 Air CH4£©.
|
||||
// For self-definition model, the gasfile is used to indicate the file path of the new gas model.
|
||||
// speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma.
|
||||
// initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName.
|
||||
// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes.
|
||||
// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation.
|
||||
// nIterSecondStep : the maximum number of iteration in the second step for the self-adaptive calculation.
|
||||
// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation.
|
||||
// nEnergyAssembly : the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory.
|
||||
// 0 -- no,
|
||||
// 1 -- yes.
|
||||
// nControlVariable: the variable to computing the residual error that determines the convergence is meet or not in the one-temperature model.
|
||||
// 0 -- the density.
|
||||
// 1 -- the translation temperature.
|
||||
// 2 -- the vibration temperature.
|
||||
// 3 -- the electron temperature.
|
||||
// 4 -- the pressure.
|
||||
// 5 -- the mass fraction of oxygen.
|
||||
// 6 -- the mass fraction of nitrogen.
|
||||
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
|
||||
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
|
||||
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
|
||||
// useHyflowSetting : Setting for HyFLOW GUI.
|
||||
// 0 -- PHengLEI
|
||||
// 1 -- HyFLOW
|
||||
// nProtectData : Use the continuation file data protection mechanism.
|
||||
// 0 -- no
|
||||
// 1 -- yes
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int isAdaptiveSolver = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
int nIterFirstStep = 1000;
|
||||
int nIterSecondStep= 2000;
|
||||
int nIterThirdStep = 2000;
|
||||
int nEnergyAssembly = 0;
|
||||
int nControlVariable = 1;
|
||||
double firstStepError = 0.01;
|
||||
double secondStepError = 0.001;
|
||||
double thirdStepError = 0.001;
|
||||
double predictCFLError = 0.1;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -952,7 +1077,8 @@ int nchemsrc = 1;
|
|||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nIdealState = 0;
|
||||
int nEnergyRecycle = 1;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
|
|
@ -960,6 +1086,11 @@ int nMeanFreePathType = 0;
|
|||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
int nSurfGradMethod = 0;
|
||||
int nRapidFlowfield = 0;
|
||||
int nSurfHeatMonitor = 0;
|
||||
int nInitPressureStep = 100;
|
||||
int nDumpCFLNumber = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
|
|
@ -970,17 +1101,38 @@ double velocitySlipCorrectConstant = 1.0;
|
|||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.5;
|
||||
double inviscidSpectrumRadiusCoef = 1.5;
|
||||
double spectrumRadiusCoef = 0.5;
|
||||
double staticPressureRelaxCorf = 0.2;
|
||||
|
||||
double maxViscous = 10000.0;
|
||||
double trTemperatureMin = 10.0;
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
double maxTemperature = 50000.0;
|
||||
double densityMin = 1.0e-8;
|
||||
double densityMinFactor = 0.1;
|
||||
double tAdjustmentFactor = 10.0;
|
||||
double iniSpeedCoef = 1.0;
|
||||
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 1;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 1;
|
||||
int nViscosityPeModified = 0;
|
||||
int nChemcalSourceModified = 2;
|
||||
int nChemcalSourceEsMethod = 1;
|
||||
int nMaxStepTemperature = 5;
|
||||
int veTemperatureMinModified = 1;
|
||||
int nDiagonalModified = 0;
|
||||
int nGradPrimtiveMethod = 1;
|
||||
int nInviscidFluxModify = 1;
|
||||
int nQlLimitMethod = 2;
|
||||
int nSpeciesForWallMethod = 1;
|
||||
int nDensityForWallMethod = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1000,7 +1152,7 @@ string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
|||
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
|
||||
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string gasfile = "Pa";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
|
|
@ -1017,6 +1169,11 @@ double gamaSpeciesB = 1.3;
|
|||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName = "O2, N2";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
|
|
@ -1124,7 +1281,7 @@ int codeOfOversetGrid = 0;
|
|||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
int readInAuxiliaryInnerGrid = 0;
|
||||
int readInAuxiliaryOuterGrid = 0;
|
||||
int readInSklFileOrNot = 0;
|
||||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
|
|
@ -1137,13 +1294,18 @@ double toleranceForOversetBox = 1.0e-3;
|
|||
int twoOrderInterpolationOrNot = 0;
|
||||
int keyEnlargeOfActiveNodes = 0;
|
||||
int outTecplotOverset = 0;
|
||||
int outPutOversetVisualization = 0;
|
||||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
double referenceLength = 1.0;
|
||||
double referenceVelocity = 1.0;
|
||||
double referenceDensity = 1.0;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
|
|
@ -1187,6 +1349,11 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0
|
|||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//direction of rotation
|
||||
// 1 -- clockwise from the point of view along the positive x axis.
|
||||
// -1 -- anticlockwise from the point of view along the positive x axis.
|
||||
int direction_0 = -1;
|
||||
double rotateFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
|
|
@ -1218,3 +1385,12 @@ int integralOrder = 4;
|
|||
#########################################################################
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
|
||||
#########################################################################
|
||||
# Incompressible Parameter #
|
||||
#########################################################################
|
||||
|
||||
int isSolveEnergyEquation = 0;
|
||||
int isSolveTurbEquation = 0;
|
||||
int isSolveSpeciesEquation = 0;
|
||||
|
||||
|
|
|
|||
|
|
@ -23,7 +23,7 @@ int nsimutask = 0;
|
|||
//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";
|
||||
//string parafilename = "./bin/cfd_para_incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
|
@ -34,11 +34,11 @@ string parafilename = "./bin/cfd_para_hypersonic.hypara";
|
|||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_refine_para.hypara";
|
||||
|
||||
//int nsimutask = 14;
|
||||
//string parafilename = "./bin/integrative_solver.hypara";
|
||||
|
|
|
|||
Binary file not shown.
|
|
@ -1,48 +0,0 @@
|
|||
# nBoundaryConditons : number of global boundary conditions.
|
||||
# bcName : Boundary Condition Name.
|
||||
# bcType(in PHengLEI): Boundary Condition Type.
|
||||
|
||||
# Account of how to set boundaryconditon.
|
||||
# string bcName = "Farfield";
|
||||
# {
|
||||
# int bcType = 4;
|
||||
# int inflowParaType = 1;
|
||||
# double attackd = 0;
|
||||
# double refReNumber = 6.5e6;
|
||||
# double refMachNumber = 3.5;
|
||||
# double angleSlide = 0;
|
||||
# }
|
||||
|
||||
int nBoundaryConditons = 4;
|
||||
string bcName = "Interface";
|
||||
{
|
||||
int bcType = -1;
|
||||
}
|
||||
string bcName = "mixbc";
|
||||
{
|
||||
int bcType = -1;
|
||||
}
|
||||
string bcName = "wall";
|
||||
{
|
||||
int bcType = 2;
|
||||
}
|
||||
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
|
||||
|
|
@ -24,6 +24,7 @@
|
|||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// 7 -- Grid type change, convert structured grid to unstructured grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
|
|
@ -32,12 +33,23 @@
|
|||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
// gridReorder: Reorder cell and face of grid or not, only for 3D unstructured grid conversion,
|
||||
// which is CGNS type.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// faceReorderMethod: the reorder method face of unstructured grid.
|
||||
// 0 -- BSFCELLFACEORG.
|
||||
// 1 -- BSFCELLFACELEFT.
|
||||
// 2 -- BSFCELLFACERIGHT.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int iadapt = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
int gridReorder = 0;
|
||||
int faceReorderMethod = 0;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
|
|
@ -61,6 +73,7 @@ int omit_no_bound_bc = 0;
|
|||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
// 9 -- Gridgen type of structured grid, *.dat/*.grd.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
|
|
@ -82,7 +95,6 @@ string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
|||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
|
|
@ -102,12 +114,10 @@ string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
|||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Refine Parameters -----------------------------
|
||||
// anisoRefine: If refine grid by anisoRefine type.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
|
|
@ -117,14 +127,14 @@ string geometryFileName = "./grid/jsm.igs";
|
|||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int geometryUnit = 1;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
int exclusiveCase = 0;
|
||||
int projectOrgPoint = 0;
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
|
|
@ -181,8 +191,11 @@ double rotationAngle = 0.0;
|
|||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
// numberOfMultifile: The number of partition grid files that want to be dumped out.
|
||||
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
int numberOfMultifile = 1;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
|
|
@ -291,6 +304,7 @@ int compressible = 1;
|
|||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
int directionMethod = 0;
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
|
@ -334,6 +348,7 @@ double wallTemperature = -1.0;
|
|||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
double gridTranslationVector[] = [0.0, 0.0, 0.0];
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
|
|
@ -355,11 +370,17 @@ double refMolecularWeight = 28.9644; // unit of g/mol.
|
|||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// isWennScheme: If using WENN Scheme of struct grid.
|
||||
// 0 -- NO. (default)
|
||||
// 1 -- Yes.
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3"
|
||||
|
||||
string inviscidSchemeName = "roe";
|
||||
int isWennScheme = 0;
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
|
|
@ -421,6 +442,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
|
@ -451,6 +473,8 @@ double skewnessAngle = 60.0;
|
|||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
double AusmpwPlusLimiter = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -466,8 +490,8 @@ double roeEntropyScale = 1.0;
|
|||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 0 -- tau = <q^2> - <q>^2
|
||||
// 1 -- tau = <u'u'>
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
|
|
@ -478,9 +502,8 @@ double roeEntropyScale = 1.0;
|
|||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// 7 -- Line LU-SGS.
|
||||
// 8 -- Matrix LU-SGS.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
|
|
@ -493,6 +516,10 @@ double roeEntropyScale = 1.0;
|
|||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// isUseLocalCFL: use variable number of CFL or not.
|
||||
// 0 -- global unified CFL number.
|
||||
// 1 -- local CFL number.
|
||||
// isUsePreTwall: use the previous temperatures on wall. 1 indicates yes, and 0 indicates no.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// codeOfAleModel: Arbitrary Lagrangian-Eulerian method.
|
||||
|
|
@ -509,6 +536,7 @@ double roeEntropyScale = 1.0;
|
|||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
double physicalTimeStepDimensional = -0.001;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
|
|
@ -525,10 +553,18 @@ double tol_sub_iter = 0.01;
|
|||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
int isUseLocalCFL = 0;
|
||||
int isUsePreTwall = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
double magnifyFactorForCFL = 1.1;
|
||||
double reduceFactorForCFL = 0.5;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
|
@ -548,7 +584,7 @@ double dtau = 0.001;
|
|||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
double lamda[] = [0.5, 1.0];
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
|
@ -579,12 +615,20 @@ double lamda[] = 0.5, 1.0;
|
|||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux.
|
||||
// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux.
|
||||
// nIsComputeWallDist: Whether to compute the wall distance.
|
||||
// 0 -- Compute wall distance.
|
||||
// 1 -- Not compute.
|
||||
//
|
||||
// protectionFile0 and protectionFile1 : Two continuation file of the data protection mechanism.
|
||||
// wall_heatfluxfile : The file to output the MaxHeatFlux of wall.
|
||||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int nIsComputeWallDist = 0;
|
||||
int walldistMethod = 1;
|
||||
int cellMethodOrNodeMethod = 0;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
|
|
@ -597,6 +641,10 @@ string visualfile = "results/tecflow.plt";
|
|||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
string protectionFile0 = "results/flow0.dat";
|
||||
string protectionFile1 = "results/flow1.dat";
|
||||
string wall_heatfluxfile = "results/wall_heatflux.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
|
|
@ -648,7 +696,10 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
|
||||
// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
|
||||
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), iblank(81).
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
|
||||
// -- transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -- overlap iblank(iblank, 81)
|
||||
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
|
@ -660,10 +711,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -Grid Reynolds number on wall(Re_w, 23)
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
|
|
@ -691,7 +739,7 @@ int dumpStandardModel = 0;
|
|||
// 1 -- Real cell where the probe is located.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables.
|
||||
|
|
@ -713,8 +761,8 @@ string probesDefineFile = "bin/probes_XYZ.dat";
|
|||
|
||||
int searchCellsMethod = 0;
|
||||
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
int nProbeVariables = 7;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5, 6];
|
||||
int probeVariablesInterpolationMethod = 0;
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
|
|
@ -722,9 +770,13 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
// transitionType: transition model type
|
||||
// 0 -- none.
|
||||
// 2 -- gama-re-theta.
|
||||
// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition
|
||||
// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not
|
||||
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
|
|
@ -739,6 +791,7 @@ double turbIntensity = -1.0;
|
|||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int prandtlNumberCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
|
|
@ -749,7 +802,7 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// == 1 - Create LESSolver;
|
||||
// = 1 - Create LESSolver;
|
||||
// != 1 - not.
|
||||
// amplitudeofDisturb: Amplitude of adding disturb.
|
||||
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
|
||||
|
|
@ -808,9 +861,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 1 -- gas model is imported from library files.
|
||||
// iCodeBranch:
|
||||
// 0 -- The old code version is used for Navier-Stokes.
|
||||
// 1 -- A new code version is active for Navier-Stokes solver.
|
||||
// isAdaptiveSolver: isAdaptiveSolver=0 indicates the generic Navier-Stokes solver,
|
||||
// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver.
|
||||
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
|
||||
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -824,7 +878,6 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
|
|
@ -860,9 +913,13 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nIdealState: whether take all gas species as ideal gas for gas-mixture process.
|
||||
// 0 -- No.
|
||||
// 1 -- Yes.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// 1 -- the energy term is computed using the polynomial fitting method.
|
||||
// 2 -- the energy term is computed using the piecewise polynomial fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
|
|
@ -875,6 +932,13 @@ int monitorNegativeConstant = 0;
|
|||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// nSurfGradMethod : the method to compute the surface heating ratio.
|
||||
// 0 -- the gradient of variable is computed with the first-order difference method.
|
||||
// 1 -- the gradient of variable is computed with the Green-Guass integral method.
|
||||
// nRapidFlowfield : initialize the flowfield using the rapid engineering method when it is greater than zero.
|
||||
// nSurfHeatMonitor : To exam the surface heating change or not. 0 is no, 1 is yes.
|
||||
// nInitPressureStep : the steps to initialize the boundary variables when the rapid method is used. 100 is the default value.
|
||||
// nDumpCFLNumber : 1 indicates dumping the CFL number to file, 0 denotes no dumping.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
|
|
@ -884,13 +948,17 @@ int monitorNegativeConstant = 0;
|
|||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// spectrumRadiusCoef: The value is in range of [0.0, 2.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
|
||||
//maxViscous: the maximum of Viscous.
|
||||
//trTemperatureMin: the minimum value of trTemperature.
|
||||
//veTemperatureMin: the minimum value of veTemperature.
|
||||
//densityMin: the minimum value of density.
|
||||
//tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0].
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
|
|
@ -903,9 +971,30 @@ int monitorNegativeConstant = 0;
|
|||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nViscosityPeModified: Pe Modified for ViscosityCoef
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceEsMethod: Modified on ChemcalSource
|
||||
// 0 -- approximation algorithm 1 (Ori.)
|
||||
// 1 -- approximation algorithm 2 (New)
|
||||
|
||||
// nMaxStepTemperature: the iterative steps of temperature.
|
||||
|
||||
// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs
|
||||
// 0 -- not used
|
||||
// 1 -- used
|
||||
|
||||
// nDiagonalModified: Modified on Diagonal
|
||||
// 0 -- not used
|
||||
// 1 -- Ori.
|
||||
// 2 -- new
|
||||
|
||||
//nGradPrimtiveMethod:
|
||||
// 0 -- Ori.
|
||||
// 1 -- new
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
|
|
@ -913,9 +1002,11 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// 0 -- Blottner fitting method(N89).
|
||||
// 1 -- Gupta fitting method(N90).
|
||||
// nContinueModel: The new continue model can switch different computation model.
|
||||
// 0 -- Not use the new continue model.
|
||||
// 1 -- use the new continue model.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
|
|
@ -925,20 +1016,54 @@ int monitorNegativeConstant = 0;
|
|||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// "Gas-Mixture" -- indicates the process of mixing gas without reacting.
|
||||
// for struct solver mixing two species£¨SpeciesA, SpeciesB£©.
|
||||
// for unstruct solver mixing multi-species£¨O2 NO CO CO2 H2 N2 Air CH4£©.
|
||||
// For self-definition model, the gasfile is used to indicate the file path of the new gas model.
|
||||
// speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma.
|
||||
// initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName.
|
||||
// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes.
|
||||
// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation.
|
||||
// nIterSecondStep : the maximum number of iteration in the second step for the self-adaptive calculation.
|
||||
// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation.
|
||||
// nEnergyAssembly : the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory.
|
||||
// 0 -- no,
|
||||
// 1 -- yes.
|
||||
// nControlVariable: the variable to computing the residual error that determines the convergence is meet or not in the one-temperature model.
|
||||
// 0 -- the density.
|
||||
// 1 -- the translation temperature.
|
||||
// 2 -- the vibration temperature.
|
||||
// 3 -- the electron temperature.
|
||||
// 4 -- the pressure.
|
||||
// 5 -- the mass fraction of oxygen.
|
||||
// 6 -- the mass fraction of nitrogen.
|
||||
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
|
||||
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
|
||||
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
|
||||
// useHyflowSetting : Setting for HyFLOW GUI.
|
||||
// 0 -- PHengLEI
|
||||
// 1 -- HyFLOW
|
||||
// nProtectData : Use the continuation file data protection mechanism.
|
||||
// 0 -- no
|
||||
// 1 -- yes
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int isAdaptiveSolver = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
int nIterFirstStep = 1000;
|
||||
int nIterSecondStep= 2000;
|
||||
int nIterThirdStep = 2000;
|
||||
int nEnergyAssembly = 0;
|
||||
int nControlVariable = 1;
|
||||
double firstStepError = 0.01;
|
||||
double secondStepError = 0.001;
|
||||
double thirdStepError = 0.001;
|
||||
double predictCFLError = 0.1;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -952,7 +1077,8 @@ int nchemsrc = 1;
|
|||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nIdealState = 0;
|
||||
int nEnergyRecycle = 1;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
|
|
@ -960,6 +1086,11 @@ int nMeanFreePathType = 0;
|
|||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
int nSurfGradMethod = 0;
|
||||
int nRapidFlowfield = 0;
|
||||
int nSurfHeatMonitor = 0;
|
||||
int nInitPressureStep = 100;
|
||||
int nDumpCFLNumber = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
|
|
@ -970,17 +1101,38 @@ double velocitySlipCorrectConstant = 1.0;
|
|||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.5;
|
||||
double inviscidSpectrumRadiusCoef = 1.5;
|
||||
double spectrumRadiusCoef = 0.5;
|
||||
double staticPressureRelaxCorf = 0.2;
|
||||
|
||||
double maxViscous = 10000.0;
|
||||
double trTemperatureMin = 10.0;
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
double maxTemperature = 50000.0;
|
||||
double densityMin = 1.0e-8;
|
||||
double densityMinFactor = 0.1;
|
||||
double tAdjustmentFactor = 10.0;
|
||||
double iniSpeedCoef = 1.0;
|
||||
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 1;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 1;
|
||||
int nViscosityPeModified = 0;
|
||||
int nChemcalSourceModified = 2;
|
||||
int nChemcalSourceEsMethod = 1;
|
||||
int nMaxStepTemperature = 5;
|
||||
int veTemperatureMinModified = 1;
|
||||
int nDiagonalModified = 0;
|
||||
int nGradPrimtiveMethod = 1;
|
||||
int nInviscidFluxModify = 1;
|
||||
int nQlLimitMethod = 2;
|
||||
int nSpeciesForWallMethod = 1;
|
||||
int nDensityForWallMethod = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1000,7 +1152,7 @@ string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
|||
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
|
||||
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string gasfile = "Pa";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
|
|
@ -1017,6 +1169,11 @@ double gamaSpeciesB = 1.3;
|
|||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName = "O2, N2";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
|
|
@ -1124,7 +1281,7 @@ int codeOfOversetGrid = 0;
|
|||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
int readInAuxiliaryInnerGrid = 0;
|
||||
int readInAuxiliaryOuterGrid = 0;
|
||||
int readInSklFileOrNot = 0;
|
||||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
|
|
@ -1137,13 +1294,18 @@ double toleranceForOversetBox = 1.0e-3;
|
|||
int twoOrderInterpolationOrNot = 0;
|
||||
int keyEnlargeOfActiveNodes = 0;
|
||||
int outTecplotOverset = 0;
|
||||
int outPutOversetVisualization = 0;
|
||||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
double referenceLength = 1.0;
|
||||
double referenceVelocity = 1.0;
|
||||
double referenceDensity = 1.0;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
|
|
@ -1187,6 +1349,11 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0
|
|||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//direction of rotation
|
||||
// 1 -- clockwise from the point of view along the positive x axis.
|
||||
// -1 -- anticlockwise from the point of view along the positive x axis.
|
||||
int direction_0 = -1;
|
||||
double rotateFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
|
|
@ -1218,3 +1385,12 @@ int integralOrder = 4;
|
|||
#########################################################################
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
|
||||
#########################################################################
|
||||
# Incompressible Parameter #
|
||||
#########################################################################
|
||||
|
||||
int isSolveEnergyEquation = 0;
|
||||
int isSolveTurbEquation = 0;
|
||||
int isSolveSpeciesEquation = 0;
|
||||
|
||||
|
|
|
|||
|
|
@ -23,7 +23,7 @@ int nsimutask = 0;
|
|||
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";
|
||||
//string parafilename = "./bin/cfd_para_incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
|
@ -34,11 +34,11 @@ string parafilename = "./bin/cfd_para_transonic.hypara";
|
|||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_refine_para.hypara";
|
||||
|
||||
//int nsimutask = 14;
|
||||
//string parafilename = "./bin/integrative_solver.hypara";
|
||||
|
|
|
|||
Binary file not shown.
|
|
@ -1,52 +0,0 @@
|
|||
# nBoundaryConditons : number of global boundary conditions.
|
||||
# bcName : Boundary Condition Name.
|
||||
# bcType(in PHengLEI): Boundary Condition Type.
|
||||
|
||||
# Account of how to set boundaryconditon.
|
||||
# string bcName = "Farfield";
|
||||
# {
|
||||
# int bcType = 4;
|
||||
# int inflowParaType = 1;
|
||||
# double attackd = 0;
|
||||
# double refReNumber = 6.5e6;
|
||||
# double refMachNumber = 3.5;
|
||||
# double angleSlide = 0;
|
||||
# }
|
||||
|
||||
int nBoundaryConditons = 5;
|
||||
string bcName = "Interface";
|
||||
{
|
||||
int bcType = -1;
|
||||
}
|
||||
string bcName = "mixbc";
|
||||
{
|
||||
int bcType = -1;
|
||||
}
|
||||
string bcName = "wall";
|
||||
{
|
||||
int bcType = 2;
|
||||
}
|
||||
string bcName = "sym";
|
||||
{
|
||||
int bcType = 3;
|
||||
}
|
||||
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
|
||||
|
|
@ -24,6 +24,7 @@
|
|||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// 7 -- Grid type change, convert structured grid to unstructured grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
|
|
@ -32,12 +33,23 @@
|
|||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
// gridReorder: Reorder cell and face of grid or not, only for 3D unstructured grid conversion,
|
||||
// which is CGNS type.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// faceReorderMethod: the reorder method face of unstructured grid.
|
||||
// 0 -- BSFCELLFACEORG.
|
||||
// 1 -- BSFCELLFACELEFT.
|
||||
// 2 -- BSFCELLFACERIGHT.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int iadapt = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
int gridReorder = 0;
|
||||
int faceReorderMethod = 0;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
|
|
@ -61,6 +73,7 @@ int omit_no_bound_bc = 0;
|
|||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
// 9 -- Gridgen type of structured grid, *.dat/*.grd.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
|
|
@ -82,7 +95,6 @@ string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
|||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
|
|
@ -102,12 +114,10 @@ string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
|||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Refine Parameters -----------------------------
|
||||
// anisoRefine: If refine grid by anisoRefine type.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
|
|
@ -117,14 +127,14 @@ string geometryFileName = "./grid/jsm.igs";
|
|||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int geometryUnit = 1;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
int exclusiveCase = 0;
|
||||
int projectOrgPoint = 0;
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
|
|
@ -181,8 +191,11 @@ double rotationAngle = 0.0;
|
|||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
// numberOfMultifile: The number of partition grid files that want to be dumped out.
|
||||
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
int numberOfMultifile = 1;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
|
|
@ -291,6 +304,7 @@ int compressible = 1;
|
|||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
int directionMethod = 0;
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
|
@ -334,6 +348,7 @@ double wallTemperature = -1.0;
|
|||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
double gridTranslationVector[] = [0.0, 0.0, 0.0];
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
|
|
@ -355,11 +370,17 @@ double refMolecularWeight = 28.9644; // unit of g/mol.
|
|||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// isWennScheme: If using WENN Scheme of struct grid.
|
||||
// 0 -- NO. (default)
|
||||
// 1 -- Yes.
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3"
|
||||
|
||||
string inviscidSchemeName = "roe";
|
||||
int isWennScheme = 0;
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
|
|
@ -421,6 +442,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
|
@ -451,6 +473,8 @@ double skewnessAngle = 60.0;
|
|||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
double AusmpwPlusLimiter = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -466,8 +490,8 @@ double roeEntropyScale = 1.0;
|
|||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 0 -- tau = <q^2> - <q>^2
|
||||
// 1 -- tau = <u'u'>
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
|
|
@ -478,9 +502,8 @@ double roeEntropyScale = 1.0;
|
|||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// 7 -- Line LU-SGS.
|
||||
// 8 -- Matrix LU-SGS.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
|
|
@ -493,6 +516,10 @@ double roeEntropyScale = 1.0;
|
|||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// isUseLocalCFL: use variable number of CFL or not.
|
||||
// 0 -- global unified CFL number.
|
||||
// 1 -- local CFL number.
|
||||
// isUsePreTwall: use the previous temperatures on wall. 1 indicates yes, and 0 indicates no.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// codeOfAleModel: Arbitrary Lagrangian-Eulerian method.
|
||||
|
|
@ -509,6 +536,7 @@ double roeEntropyScale = 1.0;
|
|||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
double physicalTimeStepDimensional = -0.001;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
|
|
@ -525,10 +553,18 @@ double tol_sub_iter = 0.01;
|
|||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
int isUseLocalCFL = 0;
|
||||
int isUsePreTwall = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
double magnifyFactorForCFL = 1.1;
|
||||
double reduceFactorForCFL = 0.5;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
|
@ -548,7 +584,7 @@ double dtau = 0.001;
|
|||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
double lamda[] = [0.5, 1.0];
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
|
@ -579,12 +615,20 @@ double lamda[] = 0.5, 1.0;
|
|||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux.
|
||||
// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux.
|
||||
// nIsComputeWallDist: Whether to compute the wall distance.
|
||||
// 0 -- Compute wall distance.
|
||||
// 1 -- Not compute.
|
||||
//
|
||||
// protectionFile0 and protectionFile1 : Two continuation file of the data protection mechanism.
|
||||
// wall_heatfluxfile : The file to output the MaxHeatFlux of wall.
|
||||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int nIsComputeWallDist = 0;
|
||||
int walldistMethod = 1;
|
||||
int cellMethodOrNodeMethod = 0;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
|
|
@ -597,6 +641,10 @@ string visualfile = "results/tecflow.plt";
|
|||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
string protectionFile0 = "results/flow0.dat";
|
||||
string protectionFile1 = "results/flow1.dat";
|
||||
string wall_heatfluxfile = "results/wall_heatflux.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
|
|
@ -648,7 +696,10 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
|
||||
// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
|
||||
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), iblank(81).
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
|
||||
// -- transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -- overlap iblank(iblank, 81)
|
||||
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
|
@ -660,10 +711,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -Grid Reynolds number on wall(Re_w, 23)
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
|
|
@ -691,7 +739,7 @@ int dumpStandardModel = 0;
|
|||
// 1 -- Real cell where the probe is located.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables.
|
||||
|
|
@ -713,8 +761,8 @@ string probesDefineFile = "bin/probes_XYZ.dat";
|
|||
|
||||
int searchCellsMethod = 0;
|
||||
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
int nProbeVariables = 7;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5, 6];
|
||||
int probeVariablesInterpolationMethod = 0;
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
|
|
@ -722,9 +770,13 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
// transitionType: transition model type
|
||||
// 0 -- none.
|
||||
// 2 -- gama-re-theta.
|
||||
// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition
|
||||
// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not
|
||||
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
|
|
@ -739,6 +791,7 @@ double turbIntensity = -1.0;
|
|||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int prandtlNumberCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
|
|
@ -749,7 +802,7 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// == 1 - Create LESSolver;
|
||||
// = 1 - Create LESSolver;
|
||||
// != 1 - not.
|
||||
// amplitudeofDisturb: Amplitude of adding disturb.
|
||||
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
|
||||
|
|
@ -808,9 +861,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 1 -- gas model is imported from library files.
|
||||
// iCodeBranch:
|
||||
// 0 -- The old code version is used for Navier-Stokes.
|
||||
// 1 -- A new code version is active for Navier-Stokes solver.
|
||||
// isAdaptiveSolver: isAdaptiveSolver=0 indicates the generic Navier-Stokes solver,
|
||||
// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver.
|
||||
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
|
||||
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -824,7 +878,6 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
|
|
@ -860,9 +913,13 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nIdealState: whether take all gas species as ideal gas for gas-mixture process.
|
||||
// 0 -- No.
|
||||
// 1 -- Yes.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// 1 -- the energy term is computed using the polynomial fitting method.
|
||||
// 2 -- the energy term is computed using the piecewise polynomial fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
|
|
@ -875,6 +932,13 @@ int monitorNegativeConstant = 0;
|
|||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// nSurfGradMethod : the method to compute the surface heating ratio.
|
||||
// 0 -- the gradient of variable is computed with the first-order difference method.
|
||||
// 1 -- the gradient of variable is computed with the Green-Guass integral method.
|
||||
// nRapidFlowfield : initialize the flowfield using the rapid engineering method when it is greater than zero.
|
||||
// nSurfHeatMonitor : To exam the surface heating change or not. 0 is no, 1 is yes.
|
||||
// nInitPressureStep : the steps to initialize the boundary variables when the rapid method is used. 100 is the default value.
|
||||
// nDumpCFLNumber : 1 indicates dumping the CFL number to file, 0 denotes no dumping.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
|
|
@ -884,13 +948,17 @@ int monitorNegativeConstant = 0;
|
|||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// spectrumRadiusCoef: The value is in range of [0.0, 2.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
|
||||
//maxViscous: the maximum of Viscous.
|
||||
//trTemperatureMin: the minimum value of trTemperature.
|
||||
//veTemperatureMin: the minimum value of veTemperature.
|
||||
//densityMin: the minimum value of density.
|
||||
//tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0].
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
|
|
@ -903,9 +971,30 @@ int monitorNegativeConstant = 0;
|
|||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nViscosityPeModified: Pe Modified for ViscosityCoef
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceEsMethod: Modified on ChemcalSource
|
||||
// 0 -- approximation algorithm 1 (Ori.)
|
||||
// 1 -- approximation algorithm 2 (New)
|
||||
|
||||
// nMaxStepTemperature: the iterative steps of temperature.
|
||||
|
||||
// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs
|
||||
// 0 -- not used
|
||||
// 1 -- used
|
||||
|
||||
// nDiagonalModified: Modified on Diagonal
|
||||
// 0 -- not used
|
||||
// 1 -- Ori.
|
||||
// 2 -- new
|
||||
|
||||
//nGradPrimtiveMethod:
|
||||
// 0 -- Ori.
|
||||
// 1 -- new
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
|
|
@ -913,9 +1002,11 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// 0 -- Blottner fitting method(N89).
|
||||
// 1 -- Gupta fitting method(N90).
|
||||
// nContinueModel: The new continue model can switch different computation model.
|
||||
// 0 -- Not use the new continue model.
|
||||
// 1 -- use the new continue model.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
|
|
@ -925,20 +1016,54 @@ int monitorNegativeConstant = 0;
|
|||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// "Gas-Mixture" -- indicates the process of mixing gas without reacting.
|
||||
// for struct solver mixing two species£¨SpeciesA, SpeciesB£©.
|
||||
// for unstruct solver mixing multi-species£¨O2 NO CO CO2 H2 N2 Air CH4£©.
|
||||
// For self-definition model, the gasfile is used to indicate the file path of the new gas model.
|
||||
// speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma.
|
||||
// initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName.
|
||||
// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes.
|
||||
// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation.
|
||||
// nIterSecondStep : the maximum number of iteration in the second step for the self-adaptive calculation.
|
||||
// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation.
|
||||
// nEnergyAssembly : the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory.
|
||||
// 0 -- no,
|
||||
// 1 -- yes.
|
||||
// nControlVariable: the variable to computing the residual error that determines the convergence is meet or not in the one-temperature model.
|
||||
// 0 -- the density.
|
||||
// 1 -- the translation temperature.
|
||||
// 2 -- the vibration temperature.
|
||||
// 3 -- the electron temperature.
|
||||
// 4 -- the pressure.
|
||||
// 5 -- the mass fraction of oxygen.
|
||||
// 6 -- the mass fraction of nitrogen.
|
||||
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
|
||||
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
|
||||
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
|
||||
// useHyflowSetting : Setting for HyFLOW GUI.
|
||||
// 0 -- PHengLEI
|
||||
// 1 -- HyFLOW
|
||||
// nProtectData : Use the continuation file data protection mechanism.
|
||||
// 0 -- no
|
||||
// 1 -- yes
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int isAdaptiveSolver = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
int nIterFirstStep = 1000;
|
||||
int nIterSecondStep= 2000;
|
||||
int nIterThirdStep = 2000;
|
||||
int nEnergyAssembly = 0;
|
||||
int nControlVariable = 1;
|
||||
double firstStepError = 0.01;
|
||||
double secondStepError = 0.001;
|
||||
double thirdStepError = 0.001;
|
||||
double predictCFLError = 0.1;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -952,7 +1077,8 @@ int nchemsrc = 1;
|
|||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nIdealState = 0;
|
||||
int nEnergyRecycle = 1;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
|
|
@ -960,6 +1086,11 @@ int nMeanFreePathType = 0;
|
|||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
int nSurfGradMethod = 0;
|
||||
int nRapidFlowfield = 0;
|
||||
int nSurfHeatMonitor = 0;
|
||||
int nInitPressureStep = 100;
|
||||
int nDumpCFLNumber = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
|
|
@ -970,17 +1101,38 @@ double velocitySlipCorrectConstant = 1.0;
|
|||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.5;
|
||||
double inviscidSpectrumRadiusCoef = 1.5;
|
||||
double spectrumRadiusCoef = 0.5;
|
||||
double staticPressureRelaxCorf = 0.2;
|
||||
|
||||
double maxViscous = 10000.0;
|
||||
double trTemperatureMin = 10.0;
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
double maxTemperature = 50000.0;
|
||||
double densityMin = 1.0e-8;
|
||||
double densityMinFactor = 0.1;
|
||||
double tAdjustmentFactor = 10.0;
|
||||
double iniSpeedCoef = 1.0;
|
||||
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 1;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 1;
|
||||
int nViscosityPeModified = 0;
|
||||
int nChemcalSourceModified = 2;
|
||||
int nChemcalSourceEsMethod = 1;
|
||||
int nMaxStepTemperature = 5;
|
||||
int veTemperatureMinModified = 1;
|
||||
int nDiagonalModified = 0;
|
||||
int nGradPrimtiveMethod = 1;
|
||||
int nInviscidFluxModify = 1;
|
||||
int nQlLimitMethod = 2;
|
||||
int nSpeciesForWallMethod = 1;
|
||||
int nDensityForWallMethod = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1000,7 +1152,7 @@ string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
|||
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
|
||||
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string gasfile = "Pa";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
|
|
@ -1017,6 +1169,11 @@ double gamaSpeciesB = 1.3;
|
|||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName = "O2, N2";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
|
|
@ -1124,7 +1281,7 @@ int codeOfOversetGrid = 0;
|
|||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
int readInAuxiliaryInnerGrid = 0;
|
||||
int readInAuxiliaryOuterGrid = 0;
|
||||
int readInSklFileOrNot = 0;
|
||||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
|
|
@ -1137,13 +1294,18 @@ double toleranceForOversetBox = 1.0e-3;
|
|||
int twoOrderInterpolationOrNot = 0;
|
||||
int keyEnlargeOfActiveNodes = 0;
|
||||
int outTecplotOverset = 0;
|
||||
int outPutOversetVisualization = 0;
|
||||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
double referenceLength = 1.0;
|
||||
double referenceVelocity = 1.0;
|
||||
double referenceDensity = 1.0;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
|
|
@ -1187,6 +1349,11 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0
|
|||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//direction of rotation
|
||||
// 1 -- clockwise from the point of view along the positive x axis.
|
||||
// -1 -- anticlockwise from the point of view along the positive x axis.
|
||||
int direction_0 = -1;
|
||||
double rotateFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
|
|
@ -1218,3 +1385,12 @@ int integralOrder = 4;
|
|||
#########################################################################
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
|
||||
#########################################################################
|
||||
# Incompressible Parameter #
|
||||
#########################################################################
|
||||
|
||||
int isSolveEnergyEquation = 0;
|
||||
int isSolveTurbEquation = 0;
|
||||
int isSolveSpeciesEquation = 0;
|
||||
|
||||
|
|
|
|||
|
|
@ -23,7 +23,7 @@ int nsimutask = 0;
|
|||
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";
|
||||
//string parafilename = "./bin/cfd_para_incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
|
@ -34,11 +34,11 @@ string parafilename = "./bin/cfd_para_transonic.hypara";
|
|||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 4
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_refine_para.hypara";
|
||||
|
||||
//int nsimutask = 14;
|
||||
//string parafilename = "./bin/integrative_solver.hypara";
|
||||
|
|
|
|||
Binary file not shown.
|
|
@ -1,52 +0,0 @@
|
|||
# nBoundaryConditons : number of global boundary conditions.
|
||||
# bcName : Boundary Condition Name.
|
||||
# bcType(in PHengLEI): Boundary Condition Type.
|
||||
|
||||
# Account of how to set boundaryconditon.
|
||||
# string bcName = "Farfield";
|
||||
# {
|
||||
# int bcType = 4;
|
||||
# int inflowParaType = 1;
|
||||
# double attackd = 0;
|
||||
# double refReNumber = 6.5e6;
|
||||
# double refMachNumber = 3.5;
|
||||
# double angleSlide = 0;
|
||||
# }
|
||||
|
||||
int nBoundaryConditons = 5;
|
||||
string bcName = "Interface";
|
||||
{
|
||||
int bcType = -1;
|
||||
}
|
||||
string bcName = "mix_bc";
|
||||
{
|
||||
int bcType = -1;
|
||||
}
|
||||
string bcName = "wall";
|
||||
{
|
||||
int bcType = 2;
|
||||
}
|
||||
string bcName = "sym";
|
||||
{
|
||||
int bcType = 3;
|
||||
}
|
||||
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
|
||||
|
|
@ -24,6 +24,7 @@
|
|||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// 7 -- Grid type change, convert structured grid to unstructured grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
|
|
@ -32,12 +33,23 @@
|
|||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
// gridReorder: Reorder cell and face of grid or not, only for 3D unstructured grid conversion,
|
||||
// which is CGNS type.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// faceReorderMethod: the reorder method face of unstructured grid.
|
||||
// 0 -- BSFCELLFACEORG.
|
||||
// 1 -- BSFCELLFACELEFT.
|
||||
// 2 -- BSFCELLFACERIGHT.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int iadapt = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
int gridReorder = 0;
|
||||
int faceReorderMethod = 0;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
|
|
@ -61,6 +73,7 @@ int omit_no_bound_bc = 0;
|
|||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
// 9 -- Gridgen type of structured grid, *.dat/*.grd.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
|
|
@ -82,7 +95,6 @@ string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
|||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
|
|
@ -102,12 +114,10 @@ string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
|||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Refine Parameters -----------------------------
|
||||
// anisoRefine: If refine grid by anisoRefine type.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
|
|
@ -117,14 +127,14 @@ string geometryFileName = "./grid/jsm.igs";
|
|||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int geometryUnit = 1;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
int exclusiveCase = 0;
|
||||
int projectOrgPoint = 0;
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
|
|
@ -181,8 +191,11 @@ double rotationAngle = 0.0;
|
|||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
// numberOfMultifile: The number of partition grid files that want to be dumped out.
|
||||
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
int numberOfMultifile = 1;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
|
|
@ -291,6 +304,7 @@ int compressible = 1;
|
|||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
int directionMethod = 0;
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
|
@ -334,6 +348,7 @@ double wallTemperature = -1.0;
|
|||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
double gridTranslationVector[] = [0.0, 0.0, 0.0];
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
|
|
@ -355,11 +370,17 @@ double refMolecularWeight = 28.9644; // unit of g/mol.
|
|||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// isWennScheme: If using WENN Scheme of struct grid.
|
||||
// 0 -- NO. (default)
|
||||
// 1 -- Yes.
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3"
|
||||
|
||||
string inviscidSchemeName = "roe";
|
||||
int isWennScheme = 0;
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
|
|
@ -421,6 +442,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
|
@ -451,6 +473,8 @@ double skewnessAngle = 60.0;
|
|||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
double AusmpwPlusLimiter = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -466,8 +490,8 @@ double roeEntropyScale = 1.0;
|
|||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 0 -- tau = <q^2> - <q>^2
|
||||
// 1 -- tau = <u'u'>
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
|
|
@ -478,9 +502,8 @@ double roeEntropyScale = 1.0;
|
|||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// 7 -- Line LU-SGS.
|
||||
// 8 -- Matrix LU-SGS.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
|
|
@ -493,6 +516,10 @@ double roeEntropyScale = 1.0;
|
|||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// isUseLocalCFL: use variable number of CFL or not.
|
||||
// 0 -- global unified CFL number.
|
||||
// 1 -- local CFL number.
|
||||
// isUsePreTwall: use the previous temperatures on wall. 1 indicates yes, and 0 indicates no.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// codeOfAleModel: Arbitrary Lagrangian-Eulerian method.
|
||||
|
|
@ -509,6 +536,7 @@ double roeEntropyScale = 1.0;
|
|||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
double physicalTimeStepDimensional = -0.001;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
|
|
@ -525,10 +553,18 @@ double tol_sub_iter = 0.01;
|
|||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
int isUseLocalCFL = 0;
|
||||
int isUsePreTwall = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
double magnifyFactorForCFL = 1.1;
|
||||
double reduceFactorForCFL = 0.5;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
|
@ -548,7 +584,7 @@ double dtau = 0.001;
|
|||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
double lamda[] = [0.5, 1.0];
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
|
@ -579,12 +615,20 @@ double lamda[] = 0.5, 1.0;
|
|||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux.
|
||||
// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux.
|
||||
// nIsComputeWallDist: Whether to compute the wall distance.
|
||||
// 0 -- Compute wall distance.
|
||||
// 1 -- Not compute.
|
||||
//
|
||||
// protectionFile0 and protectionFile1 : Two continuation file of the data protection mechanism.
|
||||
// wall_heatfluxfile : The file to output the MaxHeatFlux of wall.
|
||||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int nIsComputeWallDist = 0;
|
||||
int walldistMethod = 1;
|
||||
int cellMethodOrNodeMethod = 0;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
|
|
@ -597,6 +641,10 @@ string visualfile = "results/tecflow.plt";
|
|||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
string protectionFile0 = "results/flow0.dat";
|
||||
string protectionFile1 = "results/flow1.dat";
|
||||
string wall_heatfluxfile = "results/wall_heatflux.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
|
|
@ -648,7 +696,10 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
|
||||
// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
|
||||
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), iblank(81).
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
|
||||
// -- transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -- overlap iblank(iblank, 81)
|
||||
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
|
@ -660,10 +711,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -Grid Reynolds number on wall(Re_w, 23)
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
|
|
@ -691,7 +739,7 @@ int dumpStandardModel = 0;
|
|||
// 1 -- Real cell where the probe is located.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables.
|
||||
|
|
@ -713,8 +761,8 @@ string probesDefineFile = "bin/probes_XYZ.dat";
|
|||
|
||||
int searchCellsMethod = 0;
|
||||
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
int nProbeVariables = 7;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5, 6];
|
||||
int probeVariablesInterpolationMethod = 0;
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
|
|
@ -722,9 +770,13 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
// transitionType: transition model type
|
||||
// 0 -- none.
|
||||
// 2 -- gama-re-theta.
|
||||
// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition
|
||||
// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not
|
||||
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
|
|
@ -739,6 +791,7 @@ double turbIntensity = -1.0;
|
|||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int prandtlNumberCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
|
|
@ -749,7 +802,7 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// == 1 - Create LESSolver;
|
||||
// = 1 - Create LESSolver;
|
||||
// != 1 - not.
|
||||
// amplitudeofDisturb: Amplitude of adding disturb.
|
||||
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
|
||||
|
|
@ -808,9 +861,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 1 -- gas model is imported from library files.
|
||||
// iCodeBranch:
|
||||
// 0 -- The old code version is used for Navier-Stokes.
|
||||
// 1 -- A new code version is active for Navier-Stokes solver.
|
||||
// isAdaptiveSolver: isAdaptiveSolver=0 indicates the generic Navier-Stokes solver,
|
||||
// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver.
|
||||
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
|
||||
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -824,7 +878,6 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
|
|
@ -860,9 +913,13 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nIdealState: whether take all gas species as ideal gas for gas-mixture process.
|
||||
// 0 -- No.
|
||||
// 1 -- Yes.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// 1 -- the energy term is computed using the polynomial fitting method.
|
||||
// 2 -- the energy term is computed using the piecewise polynomial fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
|
|
@ -875,6 +932,13 @@ int monitorNegativeConstant = 0;
|
|||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// nSurfGradMethod : the method to compute the surface heating ratio.
|
||||
// 0 -- the gradient of variable is computed with the first-order difference method.
|
||||
// 1 -- the gradient of variable is computed with the Green-Guass integral method.
|
||||
// nRapidFlowfield : initialize the flowfield using the rapid engineering method when it is greater than zero.
|
||||
// nSurfHeatMonitor : To exam the surface heating change or not. 0 is no, 1 is yes.
|
||||
// nInitPressureStep : the steps to initialize the boundary variables when the rapid method is used. 100 is the default value.
|
||||
// nDumpCFLNumber : 1 indicates dumping the CFL number to file, 0 denotes no dumping.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
|
|
@ -884,13 +948,17 @@ int monitorNegativeConstant = 0;
|
|||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// spectrumRadiusCoef: The value is in range of [0.0, 2.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
|
||||
//maxViscous: the maximum of Viscous.
|
||||
//trTemperatureMin: the minimum value of trTemperature.
|
||||
//veTemperatureMin: the minimum value of veTemperature.
|
||||
//densityMin: the minimum value of density.
|
||||
//tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0].
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
|
|
@ -903,9 +971,30 @@ int monitorNegativeConstant = 0;
|
|||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nViscosityPeModified: Pe Modified for ViscosityCoef
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceEsMethod: Modified on ChemcalSource
|
||||
// 0 -- approximation algorithm 1 (Ori.)
|
||||
// 1 -- approximation algorithm 2 (New)
|
||||
|
||||
// nMaxStepTemperature: the iterative steps of temperature.
|
||||
|
||||
// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs
|
||||
// 0 -- not used
|
||||
// 1 -- used
|
||||
|
||||
// nDiagonalModified: Modified on Diagonal
|
||||
// 0 -- not used
|
||||
// 1 -- Ori.
|
||||
// 2 -- new
|
||||
|
||||
//nGradPrimtiveMethod:
|
||||
// 0 -- Ori.
|
||||
// 1 -- new
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
|
|
@ -913,9 +1002,11 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// 0 -- Blottner fitting method(N89).
|
||||
// 1 -- Gupta fitting method(N90).
|
||||
// nContinueModel: The new continue model can switch different computation model.
|
||||
// 0 -- Not use the new continue model.
|
||||
// 1 -- use the new continue model.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
|
|
@ -925,20 +1016,54 @@ int monitorNegativeConstant = 0;
|
|||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// "Gas-Mixture" -- indicates the process of mixing gas without reacting.
|
||||
// for struct solver mixing two species£¨SpeciesA, SpeciesB£©.
|
||||
// for unstruct solver mixing multi-species£¨O2 NO CO CO2 H2 N2 Air CH4£©.
|
||||
// For self-definition model, the gasfile is used to indicate the file path of the new gas model.
|
||||
// speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma.
|
||||
// initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName.
|
||||
// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes.
|
||||
// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation.
|
||||
// nIterSecondStep : the maximum number of iteration in the second step for the self-adaptive calculation.
|
||||
// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation.
|
||||
// nEnergyAssembly : the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory.
|
||||
// 0 -- no,
|
||||
// 1 -- yes.
|
||||
// nControlVariable: the variable to computing the residual error that determines the convergence is meet or not in the one-temperature model.
|
||||
// 0 -- the density.
|
||||
// 1 -- the translation temperature.
|
||||
// 2 -- the vibration temperature.
|
||||
// 3 -- the electron temperature.
|
||||
// 4 -- the pressure.
|
||||
// 5 -- the mass fraction of oxygen.
|
||||
// 6 -- the mass fraction of nitrogen.
|
||||
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
|
||||
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
|
||||
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
|
||||
// useHyflowSetting : Setting for HyFLOW GUI.
|
||||
// 0 -- PHengLEI
|
||||
// 1 -- HyFLOW
|
||||
// nProtectData : Use the continuation file data protection mechanism.
|
||||
// 0 -- no
|
||||
// 1 -- yes
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int isAdaptiveSolver = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
int nIterFirstStep = 1000;
|
||||
int nIterSecondStep= 2000;
|
||||
int nIterThirdStep = 2000;
|
||||
int nEnergyAssembly = 0;
|
||||
int nControlVariable = 1;
|
||||
double firstStepError = 0.01;
|
||||
double secondStepError = 0.001;
|
||||
double thirdStepError = 0.001;
|
||||
double predictCFLError = 0.1;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -952,7 +1077,8 @@ int nchemsrc = 1;
|
|||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nIdealState = 0;
|
||||
int nEnergyRecycle = 1;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
|
|
@ -960,6 +1086,11 @@ int nMeanFreePathType = 0;
|
|||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
int nSurfGradMethod = 0;
|
||||
int nRapidFlowfield = 0;
|
||||
int nSurfHeatMonitor = 0;
|
||||
int nInitPressureStep = 100;
|
||||
int nDumpCFLNumber = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
|
|
@ -970,17 +1101,38 @@ double velocitySlipCorrectConstant = 1.0;
|
|||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.5;
|
||||
double inviscidSpectrumRadiusCoef = 1.5;
|
||||
double spectrumRadiusCoef = 0.5;
|
||||
double staticPressureRelaxCorf = 0.2;
|
||||
|
||||
double maxViscous = 10000.0;
|
||||
double trTemperatureMin = 10.0;
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
double maxTemperature = 50000.0;
|
||||
double densityMin = 1.0e-8;
|
||||
double densityMinFactor = 0.1;
|
||||
double tAdjustmentFactor = 10.0;
|
||||
double iniSpeedCoef = 1.0;
|
||||
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 1;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 1;
|
||||
int nViscosityPeModified = 0;
|
||||
int nChemcalSourceModified = 2;
|
||||
int nChemcalSourceEsMethod = 1;
|
||||
int nMaxStepTemperature = 5;
|
||||
int veTemperatureMinModified = 1;
|
||||
int nDiagonalModified = 0;
|
||||
int nGradPrimtiveMethod = 1;
|
||||
int nInviscidFluxModify = 1;
|
||||
int nQlLimitMethod = 2;
|
||||
int nSpeciesForWallMethod = 1;
|
||||
int nDensityForWallMethod = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1000,7 +1152,7 @@ string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
|||
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
|
||||
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string gasfile = "Pa";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
|
|
@ -1017,6 +1169,11 @@ double gamaSpeciesB = 1.3;
|
|||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName = "O2, N2";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
|
|
@ -1124,7 +1281,7 @@ int codeOfOversetGrid = 0;
|
|||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
int readInAuxiliaryInnerGrid = 0;
|
||||
int readInAuxiliaryOuterGrid = 0;
|
||||
int readInSklFileOrNot = 0;
|
||||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
|
|
@ -1137,13 +1294,18 @@ double toleranceForOversetBox = 1.0e-3;
|
|||
int twoOrderInterpolationOrNot = 0;
|
||||
int keyEnlargeOfActiveNodes = 0;
|
||||
int outTecplotOverset = 0;
|
||||
int outPutOversetVisualization = 0;
|
||||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
double referenceLength = 1.0;
|
||||
double referenceVelocity = 1.0;
|
||||
double referenceDensity = 1.0;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
|
|
@ -1187,6 +1349,11 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0
|
|||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//direction of rotation
|
||||
// 1 -- clockwise from the point of view along the positive x axis.
|
||||
// -1 -- anticlockwise from the point of view along the positive x axis.
|
||||
int direction_0 = -1;
|
||||
double rotateFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
|
|
@ -1218,3 +1385,12 @@ int integralOrder = 4;
|
|||
#########################################################################
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
|
||||
#########################################################################
|
||||
# Incompressible Parameter #
|
||||
#########################################################################
|
||||
|
||||
int isSolveEnergyEquation = 0;
|
||||
int isSolveTurbEquation = 0;
|
||||
int isSolveSpeciesEquation = 0;
|
||||
|
||||
|
|
|
|||
|
|
@ -23,7 +23,7 @@ int nsimutask = 0;
|
|||
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";
|
||||
//string parafilename = "./bin/cfd_para_incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
|
@ -34,11 +34,11 @@ string parafilename = "./bin/cfd_para_transonic.hypara";
|
|||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_refine_para.hypara";
|
||||
|
||||
//int nsimutask = 14;
|
||||
//string parafilename = "./bin/integrative_solver.hypara";
|
||||
|
|
|
|||
Binary file not shown.
|
|
@ -24,6 +24,7 @@
|
|||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// 7 -- Grid type change, convert structured grid to unstructured grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
|
|
@ -32,12 +33,23 @@
|
|||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
// gridReorder: Reorder cell and face of grid or not, only for 3D unstructured grid conversion,
|
||||
// which is CGNS type.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// faceReorderMethod: the reorder method face of unstructured grid.
|
||||
// 0 -- BSFCELLFACEORG.
|
||||
// 1 -- BSFCELLFACELEFT.
|
||||
// 2 -- BSFCELLFACERIGHT.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int iadapt = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
int gridReorder = 0;
|
||||
int faceReorderMethod = 0;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
|
|
@ -61,6 +73,7 @@ int omit_no_bound_bc = 0;
|
|||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
// 9 -- Gridgen type of structured grid, *.dat/*.grd.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
|
|
@ -82,7 +95,6 @@ string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
|||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
|
|
@ -102,12 +114,10 @@ string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
|||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Refine Parameters -----------------------------
|
||||
// anisoRefine: If refine grid by anisoRefine type.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
|
|
@ -117,14 +127,14 @@ string geometryFileName = "./grid/jsm.igs";
|
|||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int geometryUnit = 1;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
int exclusiveCase = 0;
|
||||
int projectOrgPoint = 0;
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
|
|
@ -181,8 +191,11 @@ double rotationAngle = 0.0;
|
|||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
// numberOfMultifile: The number of partition grid files that want to be dumped out.
|
||||
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
int numberOfMultifile = 1;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
|
|
@ -291,6 +304,7 @@ int compressible = 1;
|
|||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
int directionMethod = 0;
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
|
@ -334,6 +348,7 @@ double wallTemperature = -1.0;
|
|||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
double gridTranslationVector[] = [0.0, 0.0, 0.0];
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
|
|
@ -355,11 +370,17 @@ double refMolecularWeight = 28.9644; // unit of g/mol.
|
|||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// isWennScheme: If using WENN Scheme of struct grid.
|
||||
// 0 -- NO. (default)
|
||||
// 1 -- Yes.
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3"
|
||||
|
||||
string inviscidSchemeName = "roe";
|
||||
int isWennScheme = 0;
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
|
|
@ -421,6 +442,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
|
@ -451,6 +473,8 @@ double skewnessAngle = 60.0;
|
|||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
double AusmpwPlusLimiter = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -466,8 +490,8 @@ double roeEntropyScale = 1.0;
|
|||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 0 -- tau = <q^2> - <q>^2
|
||||
// 1 -- tau = <u'u'>
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
|
|
@ -478,9 +502,8 @@ double roeEntropyScale = 1.0;
|
|||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// 7 -- Line LU-SGS.
|
||||
// 8 -- Matrix LU-SGS.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
|
|
@ -493,6 +516,10 @@ double roeEntropyScale = 1.0;
|
|||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// isUseLocalCFL: use variable number of CFL or not.
|
||||
// 0 -- global unified CFL number.
|
||||
// 1 -- local CFL number.
|
||||
// isUsePreTwall: use the previous temperatures on wall. 1 indicates yes, and 0 indicates no.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// codeOfAleModel: Arbitrary Lagrangian-Eulerian method.
|
||||
|
|
@ -509,6 +536,7 @@ double roeEntropyScale = 1.0;
|
|||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
double physicalTimeStepDimensional = -0.001;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
|
|
@ -525,10 +553,18 @@ double tol_sub_iter = 0.01;
|
|||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
int isUseLocalCFL = 0;
|
||||
int isUsePreTwall = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
double magnifyFactorForCFL = 1.1;
|
||||
double reduceFactorForCFL = 0.5;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
|
@ -548,7 +584,7 @@ double dtau = 0.001;
|
|||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
double lamda[] = [0.5, 1.0];
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
|
@ -579,12 +615,20 @@ double lamda[] = 0.5, 1.0;
|
|||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux.
|
||||
// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux.
|
||||
// nIsComputeWallDist: Whether to compute the wall distance.
|
||||
// 0 -- Compute wall distance.
|
||||
// 1 -- Not compute.
|
||||
//
|
||||
// protectionFile0 and protectionFile1 : Two continuation file of the data protection mechanism.
|
||||
// wall_heatfluxfile : The file to output the MaxHeatFlux of wall.
|
||||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int nIsComputeWallDist = 0;
|
||||
int walldistMethod = 1;
|
||||
int cellMethodOrNodeMethod = 0;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
|
|
@ -597,6 +641,10 @@ string visualfile = "results/tecflow.plt";
|
|||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
string protectionFile0 = "results/flow0.dat";
|
||||
string protectionFile1 = "results/flow1.dat";
|
||||
string wall_heatfluxfile = "results/wall_heatflux.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
|
|
@ -648,7 +696,10 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
|
||||
// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
|
||||
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), iblank(81).
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
|
||||
// -- transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -- overlap iblank(iblank, 81)
|
||||
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
|
@ -660,10 +711,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -Grid Reynolds number on wall(Re_w, 23)
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
|
|
@ -691,7 +739,7 @@ int dumpStandardModel = 0;
|
|||
// 1 -- Real cell where the probe is located.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables.
|
||||
|
|
@ -713,8 +761,8 @@ string probesDefineFile = "bin/probes_XYZ.dat";
|
|||
|
||||
int searchCellsMethod = 0;
|
||||
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
int nProbeVariables = 7;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5, 6];
|
||||
int probeVariablesInterpolationMethod = 0;
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
|
|
@ -722,9 +770,13 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
// transitionType: transition model type
|
||||
// 0 -- none.
|
||||
// 2 -- gama-re-theta.
|
||||
// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition
|
||||
// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not
|
||||
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
|
|
@ -739,6 +791,7 @@ double turbIntensity = -1.0;
|
|||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int prandtlNumberCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
|
|
@ -749,7 +802,7 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// == 1 - Create LESSolver;
|
||||
// = 1 - Create LESSolver;
|
||||
// != 1 - not.
|
||||
// amplitudeofDisturb: Amplitude of adding disturb.
|
||||
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
|
||||
|
|
@ -808,9 +861,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 1 -- gas model is imported from library files.
|
||||
// iCodeBranch:
|
||||
// 0 -- The old code version is used for Navier-Stokes.
|
||||
// 1 -- A new code version is active for Navier-Stokes solver.
|
||||
// isAdaptiveSolver: isAdaptiveSolver=0 indicates the generic Navier-Stokes solver,
|
||||
// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver.
|
||||
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
|
||||
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -824,7 +878,6 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
|
|
@ -860,9 +913,13 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nIdealState: whether take all gas species as ideal gas for gas-mixture process.
|
||||
// 0 -- No.
|
||||
// 1 -- Yes.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// 1 -- the energy term is computed using the polynomial fitting method.
|
||||
// 2 -- the energy term is computed using the piecewise polynomial fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
|
|
@ -875,6 +932,13 @@ int monitorNegativeConstant = 0;
|
|||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// nSurfGradMethod : the method to compute the surface heating ratio.
|
||||
// 0 -- the gradient of variable is computed with the first-order difference method.
|
||||
// 1 -- the gradient of variable is computed with the Green-Guass integral method.
|
||||
// nRapidFlowfield : initialize the flowfield using the rapid engineering method when it is greater than zero.
|
||||
// nSurfHeatMonitor : To exam the surface heating change or not. 0 is no, 1 is yes.
|
||||
// nInitPressureStep : the steps to initialize the boundary variables when the rapid method is used. 100 is the default value.
|
||||
// nDumpCFLNumber : 1 indicates dumping the CFL number to file, 0 denotes no dumping.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
|
|
@ -884,13 +948,17 @@ int monitorNegativeConstant = 0;
|
|||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// spectrumRadiusCoef: The value is in range of [0.0, 2.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
|
||||
//maxViscous: the maximum of Viscous.
|
||||
//trTemperatureMin: the minimum value of trTemperature.
|
||||
//veTemperatureMin: the minimum value of veTemperature.
|
||||
//densityMin: the minimum value of density.
|
||||
//tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0].
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
|
|
@ -903,9 +971,30 @@ int monitorNegativeConstant = 0;
|
|||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nViscosityPeModified: Pe Modified for ViscosityCoef
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceEsMethod: Modified on ChemcalSource
|
||||
// 0 -- approximation algorithm 1 (Ori.)
|
||||
// 1 -- approximation algorithm 2 (New)
|
||||
|
||||
// nMaxStepTemperature: the iterative steps of temperature.
|
||||
|
||||
// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs
|
||||
// 0 -- not used
|
||||
// 1 -- used
|
||||
|
||||
// nDiagonalModified: Modified on Diagonal
|
||||
// 0 -- not used
|
||||
// 1 -- Ori.
|
||||
// 2 -- new
|
||||
|
||||
//nGradPrimtiveMethod:
|
||||
// 0 -- Ori.
|
||||
// 1 -- new
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
|
|
@ -913,9 +1002,11 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// 0 -- Blottner fitting method(N89).
|
||||
// 1 -- Gupta fitting method(N90).
|
||||
// nContinueModel: The new continue model can switch different computation model.
|
||||
// 0 -- Not use the new continue model.
|
||||
// 1 -- use the new continue model.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
|
|
@ -925,20 +1016,54 @@ int monitorNegativeConstant = 0;
|
|||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// "Gas-Mixture" -- indicates the process of mixing gas without reacting.
|
||||
// for struct solver mixing two species£¨SpeciesA, SpeciesB£©.
|
||||
// for unstruct solver mixing multi-species£¨O2 NO CO CO2 H2 N2 Air CH4£©.
|
||||
// For self-definition model, the gasfile is used to indicate the file path of the new gas model.
|
||||
// speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma.
|
||||
// initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName.
|
||||
// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes.
|
||||
// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation.
|
||||
// nIterSecondStep : the maximum number of iteration in the second step for the self-adaptive calculation.
|
||||
// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation.
|
||||
// nEnergyAssembly : the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory.
|
||||
// 0 -- no,
|
||||
// 1 -- yes.
|
||||
// nControlVariable: the variable to computing the residual error that determines the convergence is meet or not in the one-temperature model.
|
||||
// 0 -- the density.
|
||||
// 1 -- the translation temperature.
|
||||
// 2 -- the vibration temperature.
|
||||
// 3 -- the electron temperature.
|
||||
// 4 -- the pressure.
|
||||
// 5 -- the mass fraction of oxygen.
|
||||
// 6 -- the mass fraction of nitrogen.
|
||||
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
|
||||
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
|
||||
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
|
||||
// useHyflowSetting : Setting for HyFLOW GUI.
|
||||
// 0 -- PHengLEI
|
||||
// 1 -- HyFLOW
|
||||
// nProtectData : Use the continuation file data protection mechanism.
|
||||
// 0 -- no
|
||||
// 1 -- yes
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int isAdaptiveSolver = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
int nIterFirstStep = 1000;
|
||||
int nIterSecondStep= 2000;
|
||||
int nIterThirdStep = 2000;
|
||||
int nEnergyAssembly = 0;
|
||||
int nControlVariable = 1;
|
||||
double firstStepError = 0.01;
|
||||
double secondStepError = 0.001;
|
||||
double thirdStepError = 0.001;
|
||||
double predictCFLError = 0.1;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -952,7 +1077,8 @@ int nchemsrc = 1;
|
|||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nIdealState = 0;
|
||||
int nEnergyRecycle = 1;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
|
|
@ -960,6 +1086,11 @@ int nMeanFreePathType = 0;
|
|||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
int nSurfGradMethod = 0;
|
||||
int nRapidFlowfield = 0;
|
||||
int nSurfHeatMonitor = 0;
|
||||
int nInitPressureStep = 100;
|
||||
int nDumpCFLNumber = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
|
|
@ -970,17 +1101,38 @@ double velocitySlipCorrectConstant = 1.0;
|
|||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.5;
|
||||
double inviscidSpectrumRadiusCoef = 1.5;
|
||||
double spectrumRadiusCoef = 0.5;
|
||||
double staticPressureRelaxCorf = 0.2;
|
||||
|
||||
double maxViscous = 10000.0;
|
||||
double trTemperatureMin = 10.0;
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
double maxTemperature = 50000.0;
|
||||
double densityMin = 1.0e-8;
|
||||
double densityMinFactor = 0.1;
|
||||
double tAdjustmentFactor = 10.0;
|
||||
double iniSpeedCoef = 1.0;
|
||||
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 1;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 1;
|
||||
int nViscosityPeModified = 0;
|
||||
int nChemcalSourceModified = 2;
|
||||
int nChemcalSourceEsMethod = 1;
|
||||
int nMaxStepTemperature = 5;
|
||||
int veTemperatureMinModified = 1;
|
||||
int nDiagonalModified = 0;
|
||||
int nGradPrimtiveMethod = 1;
|
||||
int nInviscidFluxModify = 1;
|
||||
int nQlLimitMethod = 2;
|
||||
int nSpeciesForWallMethod = 1;
|
||||
int nDensityForWallMethod = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1000,7 +1152,7 @@ string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
|||
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
|
||||
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string gasfile = "Pa";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
|
|
@ -1017,6 +1169,11 @@ double gamaSpeciesB = 1.3;
|
|||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName = "O2, N2";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
|
|
@ -1124,7 +1281,7 @@ int codeOfOversetGrid = 0;
|
|||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
int readInAuxiliaryInnerGrid = 0;
|
||||
int readInAuxiliaryOuterGrid = 0;
|
||||
int readInSklFileOrNot = 0;
|
||||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
|
|
@ -1137,13 +1294,18 @@ double toleranceForOversetBox = 1.0e-3;
|
|||
int twoOrderInterpolationOrNot = 0;
|
||||
int keyEnlargeOfActiveNodes = 0;
|
||||
int outTecplotOverset = 0;
|
||||
int outPutOversetVisualization = 0;
|
||||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
double referenceLength = 1.0;
|
||||
double referenceVelocity = 1.0;
|
||||
double referenceDensity = 1.0;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
|
|
@ -1187,6 +1349,11 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0
|
|||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//direction of rotation
|
||||
// 1 -- clockwise from the point of view along the positive x axis.
|
||||
// -1 -- anticlockwise from the point of view along the positive x axis.
|
||||
int direction_0 = -1;
|
||||
double rotateFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
|
|
@ -1218,3 +1385,12 @@ int integralOrder = 4;
|
|||
#########################################################################
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
|
||||
#########################################################################
|
||||
# Incompressible Parameter #
|
||||
#########################################################################
|
||||
|
||||
int isSolveEnergyEquation = 0;
|
||||
int isSolveTurbEquation = 0;
|
||||
int isSolveSpeciesEquation = 0;
|
||||
|
||||
|
|
|
|||
|
|
@ -23,7 +23,7 @@ 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";
|
||||
//string parafilename = "./bin/cfd_para_incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
|
@ -34,11 +34,11 @@ string parafilename = "./bin/cfd_para_subsonic.hypara";
|
|||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_refine_para.hypara";
|
||||
|
||||
//int nsimutask = 14;
|
||||
//string parafilename = "./bin/integrative_solver.hypara";
|
||||
|
|
|
|||
Binary file not shown.
|
|
@ -24,6 +24,7 @@
|
|||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// 7 -- Grid type change, convert structured grid to unstructured grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
|
|
@ -32,12 +33,23 @@
|
|||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
// gridReorder: Reorder cell and face of grid or not, only for 3D unstructured grid conversion,
|
||||
// which is CGNS type.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// faceReorderMethod: the reorder method face of unstructured grid.
|
||||
// 0 -- BSFCELLFACEORG.
|
||||
// 1 -- BSFCELLFACELEFT.
|
||||
// 2 -- BSFCELLFACERIGHT.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int iadapt = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
int gridReorder = 0;
|
||||
int faceReorderMethod = 0;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
|
|
@ -61,6 +73,7 @@ int omit_no_bound_bc = 0;
|
|||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
// 9 -- Gridgen type of structured grid, *.dat/*.grd.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
|
|
@ -82,7 +95,6 @@ string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
|||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
|
|
@ -102,12 +114,10 @@ string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
|||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Refine Parameters -----------------------------
|
||||
// anisoRefine: If refine grid by anisoRefine type.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
|
|
@ -117,14 +127,14 @@ string geometryFileName = "./grid/jsm.igs";
|
|||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int geometryUnit = 1;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
int exclusiveCase = 0;
|
||||
int projectOrgPoint = 0;
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
|
|
@ -181,8 +191,11 @@ double rotationAngle = 0.0;
|
|||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
// numberOfMultifile: The number of partition grid files that want to be dumped out.
|
||||
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
int numberOfMultifile = 1;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
|
|
@ -291,6 +304,7 @@ int compressible = 1;
|
|||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
int directionMethod = 0;
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
|
@ -334,6 +348,7 @@ double wallTemperature = -1.0;
|
|||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
double gridTranslationVector[] = [0.0, 0.0, 0.0];
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
|
|
@ -355,11 +370,17 @@ double refMolecularWeight = 28.9644; // unit of g/mol.
|
|||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// isWennScheme: If using WENN Scheme of struct grid.
|
||||
// 0 -- NO. (default)
|
||||
// 1 -- Yes.
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3"
|
||||
|
||||
string inviscidSchemeName = "roe";
|
||||
int isWennScheme = 0;
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
|
|
@ -421,6 +442,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
|
@ -451,6 +473,8 @@ double skewnessAngle = 60.0;
|
|||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
double AusmpwPlusLimiter = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -466,8 +490,8 @@ double roeEntropyScale = 1.0;
|
|||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 0 -- tau = <q^2> - <q>^2
|
||||
// 1 -- tau = <u'u'>
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
|
|
@ -478,9 +502,8 @@ double roeEntropyScale = 1.0;
|
|||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// 7 -- Line LU-SGS.
|
||||
// 8 -- Matrix LU-SGS.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
|
|
@ -493,6 +516,10 @@ double roeEntropyScale = 1.0;
|
|||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// isUseLocalCFL: use variable number of CFL or not.
|
||||
// 0 -- global unified CFL number.
|
||||
// 1 -- local CFL number.
|
||||
// isUsePreTwall: use the previous temperatures on wall. 1 indicates yes, and 0 indicates no.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// codeOfAleModel: Arbitrary Lagrangian-Eulerian method.
|
||||
|
|
@ -509,6 +536,7 @@ double roeEntropyScale = 1.0;
|
|||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
double physicalTimeStepDimensional = -0.001;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
|
|
@ -525,10 +553,18 @@ double tol_sub_iter = 0.01;
|
|||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
int isUseLocalCFL = 0;
|
||||
int isUsePreTwall = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
double magnifyFactorForCFL = 1.1;
|
||||
double reduceFactorForCFL = 0.5;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
|
@ -548,7 +584,7 @@ double dtau = 0.001;
|
|||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
double lamda[] = [0.5, 1.0];
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
|
@ -579,12 +615,20 @@ double lamda[] = 0.5, 1.0;
|
|||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux.
|
||||
// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux.
|
||||
// nIsComputeWallDist: Whether to compute the wall distance.
|
||||
// 0 -- Compute wall distance.
|
||||
// 1 -- Not compute.
|
||||
//
|
||||
// protectionFile0 and protectionFile1 : Two continuation file of the data protection mechanism.
|
||||
// wall_heatfluxfile : The file to output the MaxHeatFlux of wall.
|
||||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int nIsComputeWallDist = 0;
|
||||
int walldistMethod = 1;
|
||||
int cellMethodOrNodeMethod = 0;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
|
|
@ -597,6 +641,10 @@ string visualfile = "results/tecflow.plt";
|
|||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
string protectionFile0 = "results/flow0.dat";
|
||||
string protectionFile1 = "results/flow1.dat";
|
||||
string wall_heatfluxfile = "results/wall_heatflux.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
|
|
@ -648,7 +696,10 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
|
||||
// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
|
||||
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), iblank(81).
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
|
||||
// -- transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -- overlap iblank(iblank, 81)
|
||||
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
|
@ -660,10 +711,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -Grid Reynolds number on wall(Re_w, 23)
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
|
|
@ -691,7 +739,7 @@ int dumpStandardModel = 0;
|
|||
// 1 -- Real cell where the probe is located.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables.
|
||||
|
|
@ -713,8 +761,8 @@ string probesDefineFile = "bin/probes_XYZ.dat";
|
|||
|
||||
int searchCellsMethod = 0;
|
||||
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
int nProbeVariables = 7;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5, 6];
|
||||
int probeVariablesInterpolationMethod = 0;
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
|
|
@ -722,9 +770,13 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
// transitionType: transition model type
|
||||
// 0 -- none.
|
||||
// 2 -- gama-re-theta.
|
||||
// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition
|
||||
// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not
|
||||
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
|
|
@ -739,6 +791,7 @@ double turbIntensity = -1.0;
|
|||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int prandtlNumberCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
|
|
@ -749,7 +802,7 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// == 1 - Create LESSolver;
|
||||
// = 1 - Create LESSolver;
|
||||
// != 1 - not.
|
||||
// amplitudeofDisturb: Amplitude of adding disturb.
|
||||
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
|
||||
|
|
@ -808,9 +861,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 1 -- gas model is imported from library files.
|
||||
// iCodeBranch:
|
||||
// 0 -- The old code version is used for Navier-Stokes.
|
||||
// 1 -- A new code version is active for Navier-Stokes solver.
|
||||
// isAdaptiveSolver: isAdaptiveSolver=0 indicates the generic Navier-Stokes solver,
|
||||
// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver.
|
||||
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
|
||||
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -824,7 +878,6 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
|
|
@ -860,9 +913,13 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nIdealState: whether take all gas species as ideal gas for gas-mixture process.
|
||||
// 0 -- No.
|
||||
// 1 -- Yes.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// 1 -- the energy term is computed using the polynomial fitting method.
|
||||
// 2 -- the energy term is computed using the piecewise polynomial fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
|
|
@ -875,6 +932,13 @@ int monitorNegativeConstant = 0;
|
|||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// nSurfGradMethod : the method to compute the surface heating ratio.
|
||||
// 0 -- the gradient of variable is computed with the first-order difference method.
|
||||
// 1 -- the gradient of variable is computed with the Green-Guass integral method.
|
||||
// nRapidFlowfield : initialize the flowfield using the rapid engineering method when it is greater than zero.
|
||||
// nSurfHeatMonitor : To exam the surface heating change or not. 0 is no, 1 is yes.
|
||||
// nInitPressureStep : the steps to initialize the boundary variables when the rapid method is used. 100 is the default value.
|
||||
// nDumpCFLNumber : 1 indicates dumping the CFL number to file, 0 denotes no dumping.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
|
|
@ -884,13 +948,17 @@ int monitorNegativeConstant = 0;
|
|||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// spectrumRadiusCoef: The value is in range of [0.0, 2.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
|
||||
//maxViscous: the maximum of Viscous.
|
||||
//trTemperatureMin: the minimum value of trTemperature.
|
||||
//veTemperatureMin: the minimum value of veTemperature.
|
||||
//densityMin: the minimum value of density.
|
||||
//tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0].
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
|
|
@ -903,9 +971,30 @@ int monitorNegativeConstant = 0;
|
|||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nViscosityPeModified: Pe Modified for ViscosityCoef
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceEsMethod: Modified on ChemcalSource
|
||||
// 0 -- approximation algorithm 1 (Ori.)
|
||||
// 1 -- approximation algorithm 2 (New)
|
||||
|
||||
// nMaxStepTemperature: the iterative steps of temperature.
|
||||
|
||||
// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs
|
||||
// 0 -- not used
|
||||
// 1 -- used
|
||||
|
||||
// nDiagonalModified: Modified on Diagonal
|
||||
// 0 -- not used
|
||||
// 1 -- Ori.
|
||||
// 2 -- new
|
||||
|
||||
//nGradPrimtiveMethod:
|
||||
// 0 -- Ori.
|
||||
// 1 -- new
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
|
|
@ -913,9 +1002,11 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// 0 -- Blottner fitting method(N89).
|
||||
// 1 -- Gupta fitting method(N90).
|
||||
// nContinueModel: The new continue model can switch different computation model.
|
||||
// 0 -- Not use the new continue model.
|
||||
// 1 -- use the new continue model.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
|
|
@ -925,20 +1016,54 @@ int monitorNegativeConstant = 0;
|
|||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// "Gas-Mixture" -- indicates the process of mixing gas without reacting.
|
||||
// for struct solver mixing two species£¨SpeciesA, SpeciesB£©.
|
||||
// for unstruct solver mixing multi-species£¨O2 NO CO CO2 H2 N2 Air CH4£©.
|
||||
// For self-definition model, the gasfile is used to indicate the file path of the new gas model.
|
||||
// speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma.
|
||||
// initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName.
|
||||
// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes.
|
||||
// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation.
|
||||
// nIterSecondStep : the maximum number of iteration in the second step for the self-adaptive calculation.
|
||||
// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation.
|
||||
// nEnergyAssembly : the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory.
|
||||
// 0 -- no,
|
||||
// 1 -- yes.
|
||||
// nControlVariable: the variable to computing the residual error that determines the convergence is meet or not in the one-temperature model.
|
||||
// 0 -- the density.
|
||||
// 1 -- the translation temperature.
|
||||
// 2 -- the vibration temperature.
|
||||
// 3 -- the electron temperature.
|
||||
// 4 -- the pressure.
|
||||
// 5 -- the mass fraction of oxygen.
|
||||
// 6 -- the mass fraction of nitrogen.
|
||||
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
|
||||
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
|
||||
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
|
||||
// useHyflowSetting : Setting for HyFLOW GUI.
|
||||
// 0 -- PHengLEI
|
||||
// 1 -- HyFLOW
|
||||
// nProtectData : Use the continuation file data protection mechanism.
|
||||
// 0 -- no
|
||||
// 1 -- yes
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int isAdaptiveSolver = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
int nIterFirstStep = 1000;
|
||||
int nIterSecondStep= 2000;
|
||||
int nIterThirdStep = 2000;
|
||||
int nEnergyAssembly = 0;
|
||||
int nControlVariable = 1;
|
||||
double firstStepError = 0.01;
|
||||
double secondStepError = 0.001;
|
||||
double thirdStepError = 0.001;
|
||||
double predictCFLError = 0.1;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -952,7 +1077,8 @@ int nchemsrc = 1;
|
|||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nIdealState = 0;
|
||||
int nEnergyRecycle = 1;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
|
|
@ -960,6 +1086,11 @@ int nMeanFreePathType = 0;
|
|||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
int nSurfGradMethod = 0;
|
||||
int nRapidFlowfield = 0;
|
||||
int nSurfHeatMonitor = 0;
|
||||
int nInitPressureStep = 100;
|
||||
int nDumpCFLNumber = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
|
|
@ -970,17 +1101,38 @@ double velocitySlipCorrectConstant = 1.0;
|
|||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.5;
|
||||
double inviscidSpectrumRadiusCoef = 1.5;
|
||||
double spectrumRadiusCoef = 0.5;
|
||||
double staticPressureRelaxCorf = 0.2;
|
||||
|
||||
double maxViscous = 10000.0;
|
||||
double trTemperatureMin = 10.0;
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
double maxTemperature = 50000.0;
|
||||
double densityMin = 1.0e-8;
|
||||
double densityMinFactor = 0.1;
|
||||
double tAdjustmentFactor = 10.0;
|
||||
double iniSpeedCoef = 1.0;
|
||||
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 1;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 1;
|
||||
int nViscosityPeModified = 0;
|
||||
int nChemcalSourceModified = 2;
|
||||
int nChemcalSourceEsMethod = 1;
|
||||
int nMaxStepTemperature = 5;
|
||||
int veTemperatureMinModified = 1;
|
||||
int nDiagonalModified = 0;
|
||||
int nGradPrimtiveMethod = 1;
|
||||
int nInviscidFluxModify = 1;
|
||||
int nQlLimitMethod = 2;
|
||||
int nSpeciesForWallMethod = 1;
|
||||
int nDensityForWallMethod = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1000,7 +1152,7 @@ string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
|||
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
|
||||
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string gasfile = "Pa";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
|
|
@ -1017,6 +1169,11 @@ double gamaSpeciesB = 1.3;
|
|||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName = "O2, N2";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
|
|
@ -1124,7 +1281,7 @@ int codeOfOversetGrid = 0;
|
|||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
int readInAuxiliaryInnerGrid = 0;
|
||||
int readInAuxiliaryOuterGrid = 0;
|
||||
int readInSklFileOrNot = 0;
|
||||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
|
|
@ -1137,13 +1294,18 @@ double toleranceForOversetBox = 1.0e-3;
|
|||
int twoOrderInterpolationOrNot = 0;
|
||||
int keyEnlargeOfActiveNodes = 0;
|
||||
int outTecplotOverset = 0;
|
||||
int outPutOversetVisualization = 0;
|
||||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
double referenceLength = 1.0;
|
||||
double referenceVelocity = 1.0;
|
||||
double referenceDensity = 1.0;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
|
|
@ -1187,6 +1349,11 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0
|
|||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//direction of rotation
|
||||
// 1 -- clockwise from the point of view along the positive x axis.
|
||||
// -1 -- anticlockwise from the point of view along the positive x axis.
|
||||
int direction_0 = -1;
|
||||
double rotateFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
|
|
@ -1218,3 +1385,12 @@ int integralOrder = 4;
|
|||
#########################################################################
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
|
||||
#########################################################################
|
||||
# Incompressible Parameter #
|
||||
#########################################################################
|
||||
|
||||
int isSolveEnergyEquation = 0;
|
||||
int isSolveTurbEquation = 0;
|
||||
int isSolveSpeciesEquation = 0;
|
||||
|
||||
|
|
|
|||
|
|
@ -23,7 +23,7 @@ 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";
|
||||
//string parafilename = "./bin/cfd_para_incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
|
@ -34,11 +34,11 @@ string parafilename = "./bin/cfd_para_subsonic.hypara";
|
|||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_refine_para.hypara";
|
||||
|
||||
//int nsimutask = 14;
|
||||
//string parafilename = "./bin/integrative_solver.hypara";
|
||||
|
|
|
|||
Binary file not shown.
|
|
@ -24,6 +24,7 @@
|
|||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// 7 -- Grid type change, convert structured grid to unstructured grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
|
|
@ -32,12 +33,23 @@
|
|||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
// gridReorder: Reorder cell and face of grid or not, only for 3D unstructured grid conversion,
|
||||
// which is CGNS type.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// faceReorderMethod: the reorder method face of unstructured grid.
|
||||
// 0 -- BSFCELLFACEORG.
|
||||
// 1 -- BSFCELLFACELEFT.
|
||||
// 2 -- BSFCELLFACERIGHT.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int iadapt = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
int gridReorder = 0;
|
||||
int faceReorderMethod = 0;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
|
|
@ -61,6 +73,7 @@ int omit_no_bound_bc = 0;
|
|||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
// 9 -- Gridgen type of structured grid, *.dat/*.grd.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
|
|
@ -82,7 +95,6 @@ string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
|||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
|
|
@ -102,12 +114,10 @@ string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
|||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Refine Parameters -----------------------------
|
||||
// anisoRefine: If refine grid by anisoRefine type.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
|
|
@ -117,14 +127,14 @@ string geometryFileName = "./grid/jsm.igs";
|
|||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int geometryUnit = 1;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
int exclusiveCase = 0;
|
||||
int projectOrgPoint = 0;
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
|
|
@ -181,8 +191,11 @@ double rotationAngle = 0.0;
|
|||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
// numberOfMultifile: The number of partition grid files that want to be dumped out.
|
||||
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
int numberOfMultifile = 1;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
|
|
@ -291,6 +304,7 @@ int compressible = 1;
|
|||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
int directionMethod = 0;
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
|
@ -334,6 +348,7 @@ double wallTemperature = -1.0;
|
|||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
double gridTranslationVector[] = [0.0, 0.0, 0.0];
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
|
|
@ -355,11 +370,17 @@ double refMolecularWeight = 28.9644; // unit of g/mol.
|
|||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// isWennScheme: If using WENN Scheme of struct grid.
|
||||
// 0 -- NO. (default)
|
||||
// 1 -- Yes.
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3"
|
||||
|
||||
string inviscidSchemeName = "roe";
|
||||
int isWennScheme = 0;
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
|
|
@ -421,6 +442,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
|
@ -451,6 +473,8 @@ double skewnessAngle = 60.0;
|
|||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
double AusmpwPlusLimiter = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -466,8 +490,8 @@ double roeEntropyScale = 1.0;
|
|||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 0 -- tau = <q^2> - <q>^2
|
||||
// 1 -- tau = <u'u'>
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
|
|
@ -478,9 +502,8 @@ double roeEntropyScale = 1.0;
|
|||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// 7 -- Line LU-SGS.
|
||||
// 8 -- Matrix LU-SGS.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
|
|
@ -493,6 +516,10 @@ double roeEntropyScale = 1.0;
|
|||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// isUseLocalCFL: use variable number of CFL or not.
|
||||
// 0 -- global unified CFL number.
|
||||
// 1 -- local CFL number.
|
||||
// isUsePreTwall: use the previous temperatures on wall. 1 indicates yes, and 0 indicates no.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// codeOfAleModel: Arbitrary Lagrangian-Eulerian method.
|
||||
|
|
@ -509,6 +536,7 @@ double roeEntropyScale = 1.0;
|
|||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
double physicalTimeStepDimensional = -0.001;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
|
|
@ -525,10 +553,18 @@ double tol_sub_iter = 0.01;
|
|||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
int isUseLocalCFL = 0;
|
||||
int isUsePreTwall = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
double magnifyFactorForCFL = 1.1;
|
||||
double reduceFactorForCFL = 0.5;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
|
@ -548,7 +584,7 @@ double dtau = 0.001;
|
|||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
double lamda[] = [0.5, 1.0];
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
|
@ -579,12 +615,20 @@ double lamda[] = 0.5, 1.0;
|
|||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux.
|
||||
// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux.
|
||||
// nIsComputeWallDist: Whether to compute the wall distance.
|
||||
// 0 -- Compute wall distance.
|
||||
// 1 -- Not compute.
|
||||
//
|
||||
// protectionFile0 and protectionFile1 : Two continuation file of the data protection mechanism.
|
||||
// wall_heatfluxfile : The file to output the MaxHeatFlux of wall.
|
||||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int nIsComputeWallDist = 0;
|
||||
int walldistMethod = 1;
|
||||
int cellMethodOrNodeMethod = 0;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
|
|
@ -597,6 +641,10 @@ string visualfile = "results/tecflow.plt";
|
|||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
string protectionFile0 = "results/flow0.dat";
|
||||
string protectionFile1 = "results/flow1.dat";
|
||||
string wall_heatfluxfile = "results/wall_heatflux.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
|
|
@ -648,7 +696,10 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
|
||||
// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
|
||||
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), iblank(81).
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
|
||||
// -- transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -- overlap iblank(iblank, 81)
|
||||
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
|
@ -660,10 +711,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -Grid Reynolds number on wall(Re_w, 23)
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
|
|
@ -691,7 +739,7 @@ int dumpStandardModel = 0;
|
|||
// 1 -- Real cell where the probe is located.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables.
|
||||
|
|
@ -713,8 +761,8 @@ string probesDefineFile = "bin/probes_XYZ.dat";
|
|||
|
||||
int searchCellsMethod = 0;
|
||||
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
int nProbeVariables = 7;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5, 6];
|
||||
int probeVariablesInterpolationMethod = 0;
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
|
|
@ -722,9 +770,13 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
// transitionType: transition model type
|
||||
// 0 -- none.
|
||||
// 2 -- gama-re-theta.
|
||||
// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition
|
||||
// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not
|
||||
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
|
|
@ -739,6 +791,7 @@ double turbIntensity = -1.0;
|
|||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int prandtlNumberCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
|
|
@ -749,7 +802,7 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// == 1 - Create LESSolver;
|
||||
// = 1 - Create LESSolver;
|
||||
// != 1 - not.
|
||||
// amplitudeofDisturb: Amplitude of adding disturb.
|
||||
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
|
||||
|
|
@ -808,9 +861,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 1 -- gas model is imported from library files.
|
||||
// iCodeBranch:
|
||||
// 0 -- The old code version is used for Navier-Stokes.
|
||||
// 1 -- A new code version is active for Navier-Stokes solver.
|
||||
// isAdaptiveSolver: isAdaptiveSolver=0 indicates the generic Navier-Stokes solver,
|
||||
// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver.
|
||||
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
|
||||
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -824,7 +878,6 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
|
|
@ -860,9 +913,13 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nIdealState: whether take all gas species as ideal gas for gas-mixture process.
|
||||
// 0 -- No.
|
||||
// 1 -- Yes.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// 1 -- the energy term is computed using the polynomial fitting method.
|
||||
// 2 -- the energy term is computed using the piecewise polynomial fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
|
|
@ -875,6 +932,13 @@ int monitorNegativeConstant = 0;
|
|||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// nSurfGradMethod : the method to compute the surface heating ratio.
|
||||
// 0 -- the gradient of variable is computed with the first-order difference method.
|
||||
// 1 -- the gradient of variable is computed with the Green-Guass integral method.
|
||||
// nRapidFlowfield : initialize the flowfield using the rapid engineering method when it is greater than zero.
|
||||
// nSurfHeatMonitor : To exam the surface heating change or not. 0 is no, 1 is yes.
|
||||
// nInitPressureStep : the steps to initialize the boundary variables when the rapid method is used. 100 is the default value.
|
||||
// nDumpCFLNumber : 1 indicates dumping the CFL number to file, 0 denotes no dumping.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
|
|
@ -884,13 +948,17 @@ int monitorNegativeConstant = 0;
|
|||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// spectrumRadiusCoef: The value is in range of [0.0, 2.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
|
||||
//maxViscous: the maximum of Viscous.
|
||||
//trTemperatureMin: the minimum value of trTemperature.
|
||||
//veTemperatureMin: the minimum value of veTemperature.
|
||||
//densityMin: the minimum value of density.
|
||||
//tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0].
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
|
|
@ -903,9 +971,30 @@ int monitorNegativeConstant = 0;
|
|||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nViscosityPeModified: Pe Modified for ViscosityCoef
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceEsMethod: Modified on ChemcalSource
|
||||
// 0 -- approximation algorithm 1 (Ori.)
|
||||
// 1 -- approximation algorithm 2 (New)
|
||||
|
||||
// nMaxStepTemperature: the iterative steps of temperature.
|
||||
|
||||
// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs
|
||||
// 0 -- not used
|
||||
// 1 -- used
|
||||
|
||||
// nDiagonalModified: Modified on Diagonal
|
||||
// 0 -- not used
|
||||
// 1 -- Ori.
|
||||
// 2 -- new
|
||||
|
||||
//nGradPrimtiveMethod:
|
||||
// 0 -- Ori.
|
||||
// 1 -- new
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
|
|
@ -913,9 +1002,11 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// 0 -- Blottner fitting method(N89).
|
||||
// 1 -- Gupta fitting method(N90).
|
||||
// nContinueModel: The new continue model can switch different computation model.
|
||||
// 0 -- Not use the new continue model.
|
||||
// 1 -- use the new continue model.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
|
|
@ -925,20 +1016,54 @@ int monitorNegativeConstant = 0;
|
|||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// "Gas-Mixture" -- indicates the process of mixing gas without reacting.
|
||||
// for struct solver mixing two species£¨SpeciesA, SpeciesB£©.
|
||||
// for unstruct solver mixing multi-species£¨O2 NO CO CO2 H2 N2 Air CH4£©.
|
||||
// For self-definition model, the gasfile is used to indicate the file path of the new gas model.
|
||||
// speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma.
|
||||
// initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName.
|
||||
// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes.
|
||||
// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation.
|
||||
// nIterSecondStep : the maximum number of iteration in the second step for the self-adaptive calculation.
|
||||
// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation.
|
||||
// nEnergyAssembly : the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory.
|
||||
// 0 -- no,
|
||||
// 1 -- yes.
|
||||
// nControlVariable: the variable to computing the residual error that determines the convergence is meet or not in the one-temperature model.
|
||||
// 0 -- the density.
|
||||
// 1 -- the translation temperature.
|
||||
// 2 -- the vibration temperature.
|
||||
// 3 -- the electron temperature.
|
||||
// 4 -- the pressure.
|
||||
// 5 -- the mass fraction of oxygen.
|
||||
// 6 -- the mass fraction of nitrogen.
|
||||
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
|
||||
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
|
||||
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
|
||||
// useHyflowSetting : Setting for HyFLOW GUI.
|
||||
// 0 -- PHengLEI
|
||||
// 1 -- HyFLOW
|
||||
// nProtectData : Use the continuation file data protection mechanism.
|
||||
// 0 -- no
|
||||
// 1 -- yes
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int isAdaptiveSolver = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
int nIterFirstStep = 1000;
|
||||
int nIterSecondStep= 2000;
|
||||
int nIterThirdStep = 2000;
|
||||
int nEnergyAssembly = 0;
|
||||
int nControlVariable = 1;
|
||||
double firstStepError = 0.01;
|
||||
double secondStepError = 0.001;
|
||||
double thirdStepError = 0.001;
|
||||
double predictCFLError = 0.1;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -952,7 +1077,8 @@ int nchemsrc = 1;
|
|||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nIdealState = 0;
|
||||
int nEnergyRecycle = 1;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
|
|
@ -960,6 +1086,11 @@ int nMeanFreePathType = 0;
|
|||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
int nSurfGradMethod = 0;
|
||||
int nRapidFlowfield = 0;
|
||||
int nSurfHeatMonitor = 0;
|
||||
int nInitPressureStep = 100;
|
||||
int nDumpCFLNumber = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
|
|
@ -970,17 +1101,38 @@ double velocitySlipCorrectConstant = 1.0;
|
|||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.5;
|
||||
double inviscidSpectrumRadiusCoef = 1.5;
|
||||
double spectrumRadiusCoef = 0.5;
|
||||
double staticPressureRelaxCorf = 0.2;
|
||||
|
||||
double maxViscous = 10000.0;
|
||||
double trTemperatureMin = 10.0;
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
double maxTemperature = 50000.0;
|
||||
double densityMin = 1.0e-8;
|
||||
double densityMinFactor = 0.1;
|
||||
double tAdjustmentFactor = 10.0;
|
||||
double iniSpeedCoef = 1.0;
|
||||
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 1;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 1;
|
||||
int nViscosityPeModified = 0;
|
||||
int nChemcalSourceModified = 2;
|
||||
int nChemcalSourceEsMethod = 1;
|
||||
int nMaxStepTemperature = 5;
|
||||
int veTemperatureMinModified = 1;
|
||||
int nDiagonalModified = 0;
|
||||
int nGradPrimtiveMethod = 1;
|
||||
int nInviscidFluxModify = 1;
|
||||
int nQlLimitMethod = 2;
|
||||
int nSpeciesForWallMethod = 1;
|
||||
int nDensityForWallMethod = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1000,7 +1152,7 @@ string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
|||
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
|
||||
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string gasfile = "Pa";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
|
|
@ -1017,6 +1169,11 @@ double gamaSpeciesB = 1.3;
|
|||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName = "O2, N2";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
|
|
@ -1124,7 +1281,7 @@ int codeOfOversetGrid = 0;
|
|||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
int readInAuxiliaryInnerGrid = 0;
|
||||
int readInAuxiliaryOuterGrid = 0;
|
||||
int readInSklFileOrNot = 0;
|
||||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
|
|
@ -1137,13 +1294,18 @@ double toleranceForOversetBox = 1.0e-3;
|
|||
int twoOrderInterpolationOrNot = 0;
|
||||
int keyEnlargeOfActiveNodes = 0;
|
||||
int outTecplotOverset = 0;
|
||||
int outPutOversetVisualization = 0;
|
||||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
double referenceLength = 1.0;
|
||||
double referenceVelocity = 1.0;
|
||||
double referenceDensity = 1.0;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
|
|
@ -1187,6 +1349,11 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0
|
|||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//direction of rotation
|
||||
// 1 -- clockwise from the point of view along the positive x axis.
|
||||
// -1 -- anticlockwise from the point of view along the positive x axis.
|
||||
int direction_0 = -1;
|
||||
double rotateFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
|
|
@ -1218,3 +1385,12 @@ int integralOrder = 4;
|
|||
#########################################################################
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
|
||||
#########################################################################
|
||||
# Incompressible Parameter #
|
||||
#########################################################################
|
||||
|
||||
int isSolveEnergyEquation = 0;
|
||||
int isSolveTurbEquation = 0;
|
||||
int isSolveSpeciesEquation = 0;
|
||||
|
||||
|
|
|
|||
|
|
@ -23,7 +23,7 @@ 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";
|
||||
//string parafilename = "./bin/cfd_para_incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
|
@ -34,11 +34,11 @@ string parafilename = "./bin/cfd_para_subsonic.hypara";
|
|||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_refine_para.hypara";
|
||||
|
||||
//int nsimutask = 14;
|
||||
//string parafilename = "./bin/integrative_solver.hypara";
|
||||
|
|
|
|||
Binary file not shown.
|
|
@ -1,44 +0,0 @@
|
|||
# nBoundaryConditons : number of global boundary conditions.
|
||||
# bcName : Boundary Condition Name.
|
||||
# bcType(in PHengLEI): Boundary Condition Type.
|
||||
|
||||
# Account of how to set boundaryconditon.
|
||||
# string bcName = "Farfield";
|
||||
# {
|
||||
# int bcType = 4;
|
||||
# int inflowParaType = 1;
|
||||
# double attackd = 0;
|
||||
# double refReNumber = 6.5e6;
|
||||
# double refMachNumber = 3.5;
|
||||
# double angleSlide = 0;
|
||||
# }
|
||||
|
||||
int nBoundaryConditons = 3;
|
||||
string bcName = "BCWall";
|
||||
{
|
||||
int bcType = 2;
|
||||
}
|
||||
string bcName = "BCFarfield";
|
||||
{
|
||||
int bcType = 4;
|
||||
}
|
||||
string bcName = "BCOutflow";
|
||||
{
|
||||
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
|
||||
|
|
@ -24,6 +24,7 @@
|
|||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// 7 -- Grid type change, convert structured grid to unstructured grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
|
|
@ -32,12 +33,23 @@
|
|||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
// gridReorder: Reorder cell and face of grid or not, only for 3D unstructured grid conversion,
|
||||
// which is CGNS type.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// faceReorderMethod: the reorder method face of unstructured grid.
|
||||
// 0 -- BSFCELLFACEORG.
|
||||
// 1 -- BSFCELLFACELEFT.
|
||||
// 2 -- BSFCELLFACERIGHT.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int iadapt = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
int gridReorder = 0;
|
||||
int faceReorderMethod = 0;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
|
|
@ -61,6 +73,7 @@ int omit_no_bound_bc = 0;
|
|||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
// 9 -- Gridgen type of structured grid, *.dat/*.grd.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
|
|
@ -82,7 +95,6 @@ string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
|||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
|
|
@ -102,12 +114,10 @@ string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
|||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Refine Parameters -----------------------------
|
||||
// anisoRefine: If refine grid by anisoRefine type.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
|
|
@ -117,14 +127,14 @@ string geometryFileName = "./grid/jsm.igs";
|
|||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int geometryUnit = 1;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
int exclusiveCase = 0;
|
||||
int projectOrgPoint = 0;
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
|
|
@ -181,8 +191,11 @@ double rotationAngle = 0.0;
|
|||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
// numberOfMultifile: The number of partition grid files that want to be dumped out.
|
||||
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
int numberOfMultifile = 1;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
|
|
@ -291,6 +304,7 @@ int compressible = 1;
|
|||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
int directionMethod = 0;
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
|
@ -334,6 +348,7 @@ double wallTemperature = -1.0;
|
|||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
double gridTranslationVector[] = [0.0, 0.0, 0.0];
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
|
|
@ -355,11 +370,17 @@ double refMolecularWeight = 28.9644; // unit of g/mol.
|
|||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// isWennScheme: If using WENN Scheme of struct grid.
|
||||
// 0 -- NO. (default)
|
||||
// 1 -- Yes.
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3"
|
||||
|
||||
string inviscidSchemeName = "roe";
|
||||
int isWennScheme = 0;
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
|
|
@ -421,6 +442,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
|
@ -451,6 +473,8 @@ double skewnessAngle = 60.0;
|
|||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
double AusmpwPlusLimiter = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -466,8 +490,8 @@ double roeEntropyScale = 1.0;
|
|||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 0 -- tau = <q^2> - <q>^2
|
||||
// 1 -- tau = <u'u'>
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
|
|
@ -478,9 +502,8 @@ double roeEntropyScale = 1.0;
|
|||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// 7 -- Line LU-SGS.
|
||||
// 8 -- Matrix LU-SGS.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
|
|
@ -493,6 +516,10 @@ double roeEntropyScale = 1.0;
|
|||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// isUseLocalCFL: use variable number of CFL or not.
|
||||
// 0 -- global unified CFL number.
|
||||
// 1 -- local CFL number.
|
||||
// isUsePreTwall: use the previous temperatures on wall. 1 indicates yes, and 0 indicates no.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// codeOfAleModel: Arbitrary Lagrangian-Eulerian method.
|
||||
|
|
@ -509,6 +536,7 @@ double roeEntropyScale = 1.0;
|
|||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
double physicalTimeStepDimensional = -0.001;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
|
|
@ -525,10 +553,18 @@ double tol_sub_iter = 0.01;
|
|||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
int isUseLocalCFL = 0;
|
||||
int isUsePreTwall = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
double magnifyFactorForCFL = 1.1;
|
||||
double reduceFactorForCFL = 0.5;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
|
@ -548,7 +584,7 @@ double dtau = 0.001;
|
|||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
double lamda[] = [0.5, 1.0];
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
|
@ -579,12 +615,20 @@ double lamda[] = 0.5, 1.0;
|
|||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux.
|
||||
// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux.
|
||||
// nIsComputeWallDist: Whether to compute the wall distance.
|
||||
// 0 -- Compute wall distance.
|
||||
// 1 -- Not compute.
|
||||
//
|
||||
// protectionFile0 and protectionFile1 : Two continuation file of the data protection mechanism.
|
||||
// wall_heatfluxfile : The file to output the MaxHeatFlux of wall.
|
||||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int nIsComputeWallDist = 0;
|
||||
int walldistMethod = 1;
|
||||
int cellMethodOrNodeMethod = 0;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
|
|
@ -597,6 +641,10 @@ string visualfile = "results/tecflow.plt";
|
|||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
string protectionFile0 = "results/flow0.dat";
|
||||
string protectionFile1 = "results/flow1.dat";
|
||||
string wall_heatfluxfile = "results/wall_heatflux.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
|
|
@ -648,7 +696,10 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
|
||||
// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
|
||||
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), iblank(81).
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
|
||||
// -- transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -- overlap iblank(iblank, 81)
|
||||
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
|
@ -660,10 +711,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -Grid Reynolds number on wall(Re_w, 23)
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
|
|
@ -691,7 +739,7 @@ int dumpStandardModel = 0;
|
|||
// 1 -- Real cell where the probe is located.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables.
|
||||
|
|
@ -713,8 +761,8 @@ string probesDefineFile = "bin/probes_XYZ.dat";
|
|||
|
||||
int searchCellsMethod = 0;
|
||||
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
int nProbeVariables = 7;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5, 6];
|
||||
int probeVariablesInterpolationMethod = 0;
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
|
|
@ -722,9 +770,13 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
// transitionType: transition model type
|
||||
// 0 -- none.
|
||||
// 2 -- gama-re-theta.
|
||||
// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition
|
||||
// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not
|
||||
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
|
|
@ -739,6 +791,7 @@ double turbIntensity = -1.0;
|
|||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int prandtlNumberCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
|
|
@ -749,7 +802,7 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// == 1 - Create LESSolver;
|
||||
// = 1 - Create LESSolver;
|
||||
// != 1 - not.
|
||||
// amplitudeofDisturb: Amplitude of adding disturb.
|
||||
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
|
||||
|
|
@ -808,9 +861,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 1 -- gas model is imported from library files.
|
||||
// iCodeBranch:
|
||||
// 0 -- The old code version is used for Navier-Stokes.
|
||||
// 1 -- A new code version is active for Navier-Stokes solver.
|
||||
// isAdaptiveSolver: isAdaptiveSolver=0 indicates the generic Navier-Stokes solver,
|
||||
// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver.
|
||||
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
|
||||
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -824,7 +878,6 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
|
|
@ -860,9 +913,13 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nIdealState: whether take all gas species as ideal gas for gas-mixture process.
|
||||
// 0 -- No.
|
||||
// 1 -- Yes.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// 1 -- the energy term is computed using the polynomial fitting method.
|
||||
// 2 -- the energy term is computed using the piecewise polynomial fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
|
|
@ -875,6 +932,13 @@ int monitorNegativeConstant = 0;
|
|||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// nSurfGradMethod : the method to compute the surface heating ratio.
|
||||
// 0 -- the gradient of variable is computed with the first-order difference method.
|
||||
// 1 -- the gradient of variable is computed with the Green-Guass integral method.
|
||||
// nRapidFlowfield : initialize the flowfield using the rapid engineering method when it is greater than zero.
|
||||
// nSurfHeatMonitor : To exam the surface heating change or not. 0 is no, 1 is yes.
|
||||
// nInitPressureStep : the steps to initialize the boundary variables when the rapid method is used. 100 is the default value.
|
||||
// nDumpCFLNumber : 1 indicates dumping the CFL number to file, 0 denotes no dumping.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
|
|
@ -884,13 +948,17 @@ int monitorNegativeConstant = 0;
|
|||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// spectrumRadiusCoef: The value is in range of [0.0, 2.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
|
||||
//maxViscous: the maximum of Viscous.
|
||||
//trTemperatureMin: the minimum value of trTemperature.
|
||||
//veTemperatureMin: the minimum value of veTemperature.
|
||||
//densityMin: the minimum value of density.
|
||||
//tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0].
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
|
|
@ -903,9 +971,30 @@ int monitorNegativeConstant = 0;
|
|||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nViscosityPeModified: Pe Modified for ViscosityCoef
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceEsMethod: Modified on ChemcalSource
|
||||
// 0 -- approximation algorithm 1 (Ori.)
|
||||
// 1 -- approximation algorithm 2 (New)
|
||||
|
||||
// nMaxStepTemperature: the iterative steps of temperature.
|
||||
|
||||
// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs
|
||||
// 0 -- not used
|
||||
// 1 -- used
|
||||
|
||||
// nDiagonalModified: Modified on Diagonal
|
||||
// 0 -- not used
|
||||
// 1 -- Ori.
|
||||
// 2 -- new
|
||||
|
||||
//nGradPrimtiveMethod:
|
||||
// 0 -- Ori.
|
||||
// 1 -- new
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
|
|
@ -913,9 +1002,11 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// 0 -- Blottner fitting method(N89).
|
||||
// 1 -- Gupta fitting method(N90).
|
||||
// nContinueModel: The new continue model can switch different computation model.
|
||||
// 0 -- Not use the new continue model.
|
||||
// 1 -- use the new continue model.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
|
|
@ -925,20 +1016,54 @@ int monitorNegativeConstant = 0;
|
|||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// "Gas-Mixture" -- indicates the process of mixing gas without reacting.
|
||||
// for struct solver mixing two species£¨SpeciesA, SpeciesB£©.
|
||||
// for unstruct solver mixing multi-species£¨O2 NO CO CO2 H2 N2 Air CH4£©.
|
||||
// For self-definition model, the gasfile is used to indicate the file path of the new gas model.
|
||||
// speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma.
|
||||
// initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName.
|
||||
// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes.
|
||||
// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation.
|
||||
// nIterSecondStep : the maximum number of iteration in the second step for the self-adaptive calculation.
|
||||
// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation.
|
||||
// nEnergyAssembly : the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory.
|
||||
// 0 -- no,
|
||||
// 1 -- yes.
|
||||
// nControlVariable: the variable to computing the residual error that determines the convergence is meet or not in the one-temperature model.
|
||||
// 0 -- the density.
|
||||
// 1 -- the translation temperature.
|
||||
// 2 -- the vibration temperature.
|
||||
// 3 -- the electron temperature.
|
||||
// 4 -- the pressure.
|
||||
// 5 -- the mass fraction of oxygen.
|
||||
// 6 -- the mass fraction of nitrogen.
|
||||
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
|
||||
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
|
||||
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
|
||||
// useHyflowSetting : Setting for HyFLOW GUI.
|
||||
// 0 -- PHengLEI
|
||||
// 1 -- HyFLOW
|
||||
// nProtectData : Use the continuation file data protection mechanism.
|
||||
// 0 -- no
|
||||
// 1 -- yes
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int isAdaptiveSolver = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
int nIterFirstStep = 1000;
|
||||
int nIterSecondStep= 2000;
|
||||
int nIterThirdStep = 2000;
|
||||
int nEnergyAssembly = 0;
|
||||
int nControlVariable = 1;
|
||||
double firstStepError = 0.01;
|
||||
double secondStepError = 0.001;
|
||||
double thirdStepError = 0.001;
|
||||
double predictCFLError = 0.1;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -952,7 +1077,8 @@ int nchemsrc = 1;
|
|||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nIdealState = 0;
|
||||
int nEnergyRecycle = 1;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
|
|
@ -960,6 +1086,11 @@ int nMeanFreePathType = 0;
|
|||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
int nSurfGradMethod = 0;
|
||||
int nRapidFlowfield = 0;
|
||||
int nSurfHeatMonitor = 0;
|
||||
int nInitPressureStep = 100;
|
||||
int nDumpCFLNumber = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
|
|
@ -970,17 +1101,38 @@ double velocitySlipCorrectConstant = 1.0;
|
|||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.5;
|
||||
double inviscidSpectrumRadiusCoef = 1.5;
|
||||
double spectrumRadiusCoef = 0.5;
|
||||
double staticPressureRelaxCorf = 0.2;
|
||||
|
||||
double maxViscous = 10000.0;
|
||||
double trTemperatureMin = 10.0;
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
double maxTemperature = 50000.0;
|
||||
double densityMin = 1.0e-8;
|
||||
double densityMinFactor = 0.1;
|
||||
double tAdjustmentFactor = 10.0;
|
||||
double iniSpeedCoef = 1.0;
|
||||
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 1;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 1;
|
||||
int nViscosityPeModified = 0;
|
||||
int nChemcalSourceModified = 2;
|
||||
int nChemcalSourceEsMethod = 1;
|
||||
int nMaxStepTemperature = 5;
|
||||
int veTemperatureMinModified = 1;
|
||||
int nDiagonalModified = 0;
|
||||
int nGradPrimtiveMethod = 1;
|
||||
int nInviscidFluxModify = 1;
|
||||
int nQlLimitMethod = 2;
|
||||
int nSpeciesForWallMethod = 1;
|
||||
int nDensityForWallMethod = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1000,7 +1152,7 @@ string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
|||
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
|
||||
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string gasfile = "Pa";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
|
|
@ -1017,6 +1169,11 @@ double gamaSpeciesB = 1.3;
|
|||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName = "O2, N2";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
|
|
@ -1124,7 +1281,7 @@ int codeOfOversetGrid = 0;
|
|||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
int readInAuxiliaryInnerGrid = 0;
|
||||
int readInAuxiliaryOuterGrid = 0;
|
||||
int readInSklFileOrNot = 0;
|
||||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
|
|
@ -1137,13 +1294,18 @@ double toleranceForOversetBox = 1.0e-3;
|
|||
int twoOrderInterpolationOrNot = 0;
|
||||
int keyEnlargeOfActiveNodes = 0;
|
||||
int outTecplotOverset = 0;
|
||||
int outPutOversetVisualization = 0;
|
||||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
double referenceLength = 1.0;
|
||||
double referenceVelocity = 1.0;
|
||||
double referenceDensity = 1.0;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
|
|
@ -1187,6 +1349,11 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0
|
|||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//direction of rotation
|
||||
// 1 -- clockwise from the point of view along the positive x axis.
|
||||
// -1 -- anticlockwise from the point of view along the positive x axis.
|
||||
int direction_0 = -1;
|
||||
double rotateFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
|
|
@ -1218,3 +1385,12 @@ int integralOrder = 4;
|
|||
#########################################################################
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
|
||||
#########################################################################
|
||||
# Incompressible Parameter #
|
||||
#########################################################################
|
||||
|
||||
int isSolveEnergyEquation = 0;
|
||||
int isSolveTurbEquation = 0;
|
||||
int isSolveSpeciesEquation = 0;
|
||||
|
||||
|
|
|
|||
|
|
@ -21,7 +21,7 @@ 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";
|
||||
//string parafilename = "./bin/cfd_para_incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
|
@ -32,16 +32,19 @@ string parafilename = "./bin/cfd_para_subsonic.hypara";
|
|||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_refine_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 iovrlap = 0;
|
||||
|
||||
// ---------------- Advanced Parameters, DO NOT care it ----------------
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
string parafilename1 = "./bin/kinetic_para.hypara"
|
||||
|
|
|
|||
Binary file not shown.
|
|
@ -1,4 +1,4 @@
|
|||
# nBoundaryConditons : Number of global boundary conditions.
|
||||
# nBoundaryConditions : Number of global boundary conditions.
|
||||
# bcName : Boundary condition name.
|
||||
# bcType(in PHengLEI): Boundary condition type.
|
||||
|
||||
|
|
@ -25,7 +25,7 @@
|
|||
|
||||
# For more information, see examples/bin/boundary_condition.hypara file!!!
|
||||
|
||||
int nBoundaryConditons = 6;
|
||||
int nBoundaryConditions = 6;
|
||||
string bcName = "BCWall";
|
||||
{
|
||||
string bodyName = "body";
|
||||
|
|
|
|||
|
|
@ -24,6 +24,7 @@
|
|||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// 7 -- Grid type change, convert structured grid to unstructured grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
|
|
@ -32,12 +33,23 @@
|
|||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
// gridReorder: Reorder cell and face of grid or not, only for 3D unstructured grid conversion,
|
||||
// which is CGNS type.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// faceReorderMethod: the reorder method face of unstructured grid.
|
||||
// 0 -- BSFCELLFACEORG.
|
||||
// 1 -- BSFCELLFACELEFT.
|
||||
// 2 -- BSFCELLFACERIGHT.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int iadapt = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
int gridReorder = 0;
|
||||
int faceReorderMethod = 0;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
|
|
@ -61,6 +73,7 @@ int omit_no_bound_bc = 0;
|
|||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
// 9 -- Gridgen type of structured grid, *.dat/*.grd.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
|
|
@ -82,7 +95,6 @@ string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
|||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
|
|
@ -102,12 +114,10 @@ string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
|||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Refine Parameters -----------------------------
|
||||
// anisoRefine: If refine grid by anisoRefine type.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
|
|
@ -117,14 +127,14 @@ string geometryFileName = "./grid/jsm.igs";
|
|||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int geometryUnit = 1;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
int exclusiveCase = 0;
|
||||
int projectOrgPoint = 0;
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
|
|
@ -181,8 +191,11 @@ double rotationAngle = 0.0;
|
|||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
// numberOfMultifile: The number of partition grid files that want to be dumped out.
|
||||
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
int numberOfMultifile = 1;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
|
|
@ -291,6 +304,7 @@ int compressible = 1;
|
|||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
int directionMethod = 0;
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
|
@ -334,6 +348,7 @@ double wallTemperature = -1.0;
|
|||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
double gridTranslationVector[] = [0.0, 0.0, 0.0];
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
|
|
@ -355,11 +370,17 @@ double refMolecularWeight = 28.9644; // unit of g/mol.
|
|||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// isWennScheme: If using WENN Scheme of struct grid.
|
||||
// 0 -- NO. (default)
|
||||
// 1 -- Yes.
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3"
|
||||
|
||||
string inviscidSchemeName = "roe";
|
||||
int isWennScheme = 0;
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
|
|
@ -421,6 +442,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
|
@ -451,6 +473,8 @@ double skewnessAngle = 60.0;
|
|||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
double AusmpwPlusLimiter = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -466,8 +490,8 @@ double roeEntropyScale = 1.0;
|
|||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 0 -- tau = <q^2> - <q>^2
|
||||
// 1 -- tau = <u'u'>
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
|
|
@ -478,9 +502,8 @@ double roeEntropyScale = 1.0;
|
|||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// 7 -- Line LU-SGS.
|
||||
// 8 -- Matrix LU-SGS.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
|
|
@ -493,6 +516,10 @@ double roeEntropyScale = 1.0;
|
|||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// isUseLocalCFL: use variable number of CFL or not.
|
||||
// 0 -- global unified CFL number.
|
||||
// 1 -- local CFL number.
|
||||
// isUsePreTwall: use the previous temperatures on wall. 1 indicates yes, and 0 indicates no.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// codeOfAleModel: Arbitrary Lagrangian-Eulerian method.
|
||||
|
|
@ -509,6 +536,7 @@ double roeEntropyScale = 1.0;
|
|||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
double physicalTimeStepDimensional = -0.001;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
|
|
@ -525,10 +553,18 @@ double tol_sub_iter = 0.01;
|
|||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
int isUseLocalCFL = 0;
|
||||
int isUsePreTwall = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
double magnifyFactorForCFL = 1.1;
|
||||
double reduceFactorForCFL = 0.5;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
|
@ -548,7 +584,7 @@ double dtau = 0.001;
|
|||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
double lamda[] = [0.5, 1.0];
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
|
@ -579,12 +615,20 @@ double lamda[] = 0.5, 1.0;
|
|||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux.
|
||||
// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux.
|
||||
// nIsComputeWallDist: Whether to compute the wall distance.
|
||||
// 0 -- Compute wall distance.
|
||||
// 1 -- Not compute.
|
||||
//
|
||||
// protectionFile0 and protectionFile1 : Two continuation file of the data protection mechanism.
|
||||
// wall_heatfluxfile : The file to output the MaxHeatFlux of wall.
|
||||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int nIsComputeWallDist = 0;
|
||||
int walldistMethod = 1;
|
||||
int cellMethodOrNodeMethod = 0;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
|
|
@ -597,6 +641,10 @@ string visualfile = "results/tecflow.plt";
|
|||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
string protectionFile0 = "results/flow0.dat";
|
||||
string protectionFile1 = "results/flow1.dat";
|
||||
string wall_heatfluxfile = "results/wall_heatflux.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
|
|
@ -648,7 +696,10 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
|
||||
// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
|
||||
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), iblank(81).
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47),
|
||||
// -- transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -- overlap iblank(iblank, 81)
|
||||
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
|
@ -660,10 +711,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -Grid Reynolds number on wall(Re_w, 23)
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
|
|
@ -691,7 +739,7 @@ int dumpStandardModel = 0;
|
|||
// 1 -- Real cell where the probe is located.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables.
|
||||
|
|
@ -713,8 +761,8 @@ string probesDefineFile = "bin/probes_XYZ.dat";
|
|||
|
||||
int searchCellsMethod = 0;
|
||||
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
int nProbeVariables = 7;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5, 6];
|
||||
int probeVariablesInterpolationMethod = 0;
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
|
|
@ -722,9 +770,13 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
// transitionType: transition model type
|
||||
// 0 -- none.
|
||||
// 2 -- gama-re-theta.
|
||||
// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition
|
||||
// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not
|
||||
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
|
|
@ -739,6 +791,7 @@ double turbIntensity = -1.0;
|
|||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int prandtlNumberCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
|
|
@ -749,7 +802,7 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// == 1 - Create LESSolver;
|
||||
// = 1 - Create LESSolver;
|
||||
// != 1 - not.
|
||||
// amplitudeofDisturb: Amplitude of adding disturb.
|
||||
// disturbstep: Unsteady time step or steady iteration of adding random disturb.
|
||||
|
|
@ -808,9 +861,10 @@ int monitorNegativeConstant = 0;
|
|||
// iapplication:
|
||||
// 0 -- gas model is fixed in the codes.
|
||||
// 1 -- gas model is imported from library files.
|
||||
// iCodeBranch:
|
||||
// 0 -- The old code version is used for Navier-Stokes.
|
||||
// 1 -- A new code version is active for Navier-Stokes solver.
|
||||
// isAdaptiveSolver: isAdaptiveSolver=0 indicates the generic Navier-Stokes solver,
|
||||
// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver.
|
||||
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
|
||||
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -824,7 +878,6 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
|
|
@ -860,9 +913,13 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nIdealState: whether take all gas species as ideal gas for gas-mixture process.
|
||||
// 0 -- No.
|
||||
// 1 -- Yes.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// 1 -- the energy term is computed using the polynomial fitting method.
|
||||
// 2 -- the energy term is computed using the piecewise polynomial fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
|
|
@ -875,6 +932,13 @@ int monitorNegativeConstant = 0;
|
|||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// nSurfGradMethod : the method to compute the surface heating ratio.
|
||||
// 0 -- the gradient of variable is computed with the first-order difference method.
|
||||
// 1 -- the gradient of variable is computed with the Green-Guass integral method.
|
||||
// nRapidFlowfield : initialize the flowfield using the rapid engineering method when it is greater than zero.
|
||||
// nSurfHeatMonitor : To exam the surface heating change or not. 0 is no, 1 is yes.
|
||||
// nInitPressureStep : the steps to initialize the boundary variables when the rapid method is used. 100 is the default value.
|
||||
// nDumpCFLNumber : 1 indicates dumping the CFL number to file, 0 denotes no dumping.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
|
|
@ -884,13 +948,17 @@ int monitorNegativeConstant = 0;
|
|||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// spectrumRadiusCoef: The value is in range of [0.0, 2.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
|
||||
//maxViscous: the maximum of Viscous.
|
||||
//trTemperatureMin: the minimum value of trTemperature.
|
||||
//veTemperatureMin: the minimum value of veTemperature.
|
||||
//densityMin: the minimum value of density.
|
||||
//tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0].
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
|
|
@ -903,9 +971,30 @@ int monitorNegativeConstant = 0;
|
|||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nViscosityPeModified: Pe Modified for ViscosityCoef
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceEsMethod: Modified on ChemcalSource
|
||||
// 0 -- approximation algorithm 1 (Ori.)
|
||||
// 1 -- approximation algorithm 2 (New)
|
||||
|
||||
// nMaxStepTemperature: the iterative steps of temperature.
|
||||
|
||||
// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs
|
||||
// 0 -- not used
|
||||
// 1 -- used
|
||||
|
||||
// nDiagonalModified: Modified on Diagonal
|
||||
// 0 -- not used
|
||||
// 1 -- Ori.
|
||||
// 2 -- new
|
||||
|
||||
//nGradPrimtiveMethod:
|
||||
// 0 -- Ori.
|
||||
// 1 -- new
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
|
|
@ -913,9 +1002,11 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// 0 -- Blottner fitting method(N89).
|
||||
// 1 -- Gupta fitting method(N90).
|
||||
// nContinueModel: The new continue model can switch different computation model.
|
||||
// 0 -- Not use the new continue model.
|
||||
// 1 -- use the new continue model.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
|
|
@ -925,20 +1016,54 @@ int monitorNegativeConstant = 0;
|
|||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// "Gas-Mixture" -- indicates the process of mixing gas without reacting.
|
||||
// for struct solver mixing two species£¨SpeciesA, SpeciesB£©.
|
||||
// for unstruct solver mixing multi-species£¨O2 NO CO CO2 H2 N2 Air CH4£©.
|
||||
// For self-definition model, the gasfile is used to indicate the file path of the new gas model.
|
||||
// speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma.
|
||||
// initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName.
|
||||
// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes.
|
||||
// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation.
|
||||
// nIterSecondStep : the maximum number of iteration in the second step for the self-adaptive calculation.
|
||||
// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation.
|
||||
// nEnergyAssembly : the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory.
|
||||
// 0 -- no,
|
||||
// 1 -- yes.
|
||||
// nControlVariable: the variable to computing the residual error that determines the convergence is meet or not in the one-temperature model.
|
||||
// 0 -- the density.
|
||||
// 1 -- the translation temperature.
|
||||
// 2 -- the vibration temperature.
|
||||
// 3 -- the electron temperature.
|
||||
// 4 -- the pressure.
|
||||
// 5 -- the mass fraction of oxygen.
|
||||
// 6 -- the mass fraction of nitrogen.
|
||||
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
|
||||
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
|
||||
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
|
||||
// useHyflowSetting : Setting for HyFLOW GUI.
|
||||
// 0 -- PHengLEI
|
||||
// 1 -- HyFLOW
|
||||
// nProtectData : Use the continuation file data protection mechanism.
|
||||
// 0 -- no
|
||||
// 1 -- yes
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int isAdaptiveSolver = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
int nIterFirstStep = 1000;
|
||||
int nIterSecondStep= 2000;
|
||||
int nIterThirdStep = 2000;
|
||||
int nEnergyAssembly = 0;
|
||||
int nControlVariable = 1;
|
||||
double firstStepError = 0.01;
|
||||
double secondStepError = 0.001;
|
||||
double thirdStepError = 0.001;
|
||||
double predictCFLError = 0.1;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -952,7 +1077,8 @@ int nchemsrc = 1;
|
|||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nIdealState = 0;
|
||||
int nEnergyRecycle = 1;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
|
|
@ -960,6 +1086,11 @@ int nMeanFreePathType = 0;
|
|||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
int nSurfGradMethod = 0;
|
||||
int nRapidFlowfield = 0;
|
||||
int nSurfHeatMonitor = 0;
|
||||
int nInitPressureStep = 100;
|
||||
int nDumpCFLNumber = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
|
|
@ -970,17 +1101,38 @@ double velocitySlipCorrectConstant = 1.0;
|
|||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.5;
|
||||
double inviscidSpectrumRadiusCoef = 1.5;
|
||||
double spectrumRadiusCoef = 0.5;
|
||||
double staticPressureRelaxCorf = 0.2;
|
||||
|
||||
double maxViscous = 10000.0;
|
||||
double trTemperatureMin = 10.0;
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
double maxTemperature = 50000.0;
|
||||
double densityMin = 1.0e-8;
|
||||
double densityMinFactor = 0.1;
|
||||
double tAdjustmentFactor = 10.0;
|
||||
double iniSpeedCoef = 1.0;
|
||||
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 1;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 1;
|
||||
int nViscosityPeModified = 0;
|
||||
int nChemcalSourceModified = 2;
|
||||
int nChemcalSourceEsMethod = 1;
|
||||
int nMaxStepTemperature = 5;
|
||||
int veTemperatureMinModified = 1;
|
||||
int nDiagonalModified = 0;
|
||||
int nGradPrimtiveMethod = 1;
|
||||
int nInviscidFluxModify = 1;
|
||||
int nQlLimitMethod = 2;
|
||||
int nSpeciesForWallMethod = 1;
|
||||
int nDensityForWallMethod = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
|
|
@ -1000,7 +1152,7 @@ string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
|||
//string speciesName = "O, O2, NO, N, N2, C, CO, CO2";
|
||||
//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string gasfile = "Pa";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
|
|
@ -1017,6 +1169,11 @@ double gamaSpeciesB = 1.3;
|
|||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName = "O2, N2";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
|
|
@ -1124,7 +1281,7 @@ int codeOfOversetGrid = 0;
|
|||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
int readInAuxiliaryInnerGrid = 0;
|
||||
int readInAuxiliaryOuterGrid = 0;
|
||||
int readInSklFileOrNot = 0;
|
||||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
|
|
@ -1137,13 +1294,18 @@ double toleranceForOversetBox = 1.0e-3;
|
|||
int twoOrderInterpolationOrNot = 0;
|
||||
int keyEnlargeOfActiveNodes = 0;
|
||||
int outTecplotOverset = 0;
|
||||
int outPutOversetVisualization = 0;
|
||||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
double referenceLength = 1.0;
|
||||
double referenceVelocity = 1.0;
|
||||
double referenceDensity = 1.0;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
|
|
@ -1187,6 +1349,11 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0
|
|||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//direction of rotation
|
||||
// 1 -- clockwise from the point of view along the positive x axis.
|
||||
// -1 -- anticlockwise from the point of view along the positive x axis.
|
||||
int direction_0 = -1;
|
||||
double rotateFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
|
|
@ -1218,3 +1385,12 @@ int integralOrder = 4;
|
|||
#########################################################################
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
|
||||
#########################################################################
|
||||
# Incompressible Parameter #
|
||||
#########################################################################
|
||||
|
||||
int isSolveEnergyEquation = 0;
|
||||
int isSolveTurbEquation = 0;
|
||||
int isSolveSpeciesEquation = 0;
|
||||
|
||||
|
|
|
|||
|
|
@ -21,7 +21,7 @@ int nsimutask = 0;
|
|||
//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";
|
||||
//string parafilename = "./bin/cfd_para_incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
|
@ -32,16 +32,19 @@ string parafilename = "./bin/cfd_para_supersonic.hypara";
|
|||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_refine_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 iovrlap = 0;
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
string parafilename1 = "./bin/kinetic_para.hypara"
|
||||
|
|
|
|||
Binary file not shown.
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Reference in New Issue