调整F03-F04;更新F09-F10、Z01-Z02；新增G05-G07、H01-H05
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hechao
parent
8d8748c38a
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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.
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// 1 -- gas model is imported from library files.
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// iCodeBranch:
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// 0 -- The old code version is used for Navier-Stokes.
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// 1 -- A new code version is active for Navier-Stokes solver.
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// isAdaptiveSolver: isAdaptiveSolver=0 indicates the generic Navier-Stokes solver,
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// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver.
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// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
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// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
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// nm: Equation number of the physics, but is out of commision now.
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// 4 -- for 2D.
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// 5 -- for 3D.
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@ -824,7 +878,6 @@ int monitorNegativeConstant = 0;
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// 0 -- not used .
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// 1 -- used.
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// nDensityModify: The type of densitymodify.
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// 0 -- not used.
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// 1 -- used.
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// nchem:
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@ -860,9 +913,13 @@ int monitorNegativeConstant = 0;
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// 1 -- One-temperature model.
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// 2 -- Two-temperature model.
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// 3 -- Three-temperature model.
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// nIdealState: whether take all gas species as ideal gas for gas-mixture process.
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// 0 -- No.
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// 1 -- Yes.
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// nTEnergyModel: the method to computing temperature energy model.
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// 0 -- the energy term is computed using the conventional method.
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// 1 -- the energy term is computed using the curve fitting method.
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// 1 -- the energy term is computed using the polynomial fitting method.
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// 2 -- the energy term is computed using the piecewise polynomial fitting method.
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// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
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// 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.
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// catalyticCoef:
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@ -875,6 +932,13 @@ int monitorNegativeConstant = 0;
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// nTemperatureJump : the method to calculate the temperature jump.
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// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
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// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
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// nSurfGradMethod : the method to compute the surface heating ratio.
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// 0 -- the gradient of variable is computed with the first-order difference method.
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// 1 -- the gradient of variable is computed with the Green-Guass integral method.
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// nRapidFlowfield : initialize the flowfield using the rapid engineering method when it is greater than zero.
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// 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;
|
||||
|
||||
|
|
@ -171,7 +171,6 @@ int flowInitStep = 100;
|
|||
// Please use 'rae2822_hybrid2d__4.fts' here!
|
||||
// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
|
||||
|
||||
string gridfile = "./grid/background__2.fts";
|
||||
int plotFieldType = 1;
|
||||
|
||||
// ----------------- Advanced Parameters, DO NOT care it ----------------
|
||||
|
|
@ -20,7 +20,6 @@
|
|||
int gridtype = 0;
|
||||
int axisup = 1;
|
||||
int from_gtype = 2;
|
||||
int dumpOldGrid = 0;
|
||||
|
||||
#########################################################################
|
||||
# File path #
|
||||
|
|
@ -28,17 +27,10 @@ int dumpOldGrid = 0;
|
|||
// from_gfile: path of original data file for unstructure grid convert from.
|
||||
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
|
||||
|
||||
//string from_gfile = "./grid/aux-lower.cgns";
|
||||
//string out_gfile = "./grid/aux-lower.fts";
|
||||
int numberOfGridFile = 5;
|
||||
string from_gfile = "./grid/aux-lower.cgns";
|
||||
string from_gfile1 = "./grid/aux-upper.cgns";
|
||||
string from_gfile2 = "./grid/background.cgns";
|
||||
string from_gfile3 = "./grid/lowerwing.cgns";
|
||||
string from_gfile4 = "./grid/upperwing.cgns";
|
||||
|
||||
//string from_gfile = "./grid/aux-upper.cgns";
|
||||
//string out_gfile = "./grid/aux-upper.fts";
|
||||
|
||||
//string from_gfile = "./grid/background.cgns";
|
||||
//string out_gfile = "./grid/background.fts";
|
||||
|
||||
//string from_gfile = "./grid/lowerwing.cgns";
|
||||
//string out_gfile = "./grid/lowerwing.fts";
|
||||
|
||||
string from_gfile = "./grid/upperwing.cgns";
|
||||
string out_gfile = "./grid/upperwing.fts";
|
||||
|
|
@ -23,8 +23,7 @@ int nparafile = 1;
|
|||
//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 parafilename1 = "./bin/overset_config.hypara";
|
||||
//string parafilename = "./bin/cfd_para_incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
|
@ -35,11 +34,11 @@ int nparafile = 1;
|
|||
//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 = 6;
|
||||
string parafilename = "./bin/overset_config.hypara";
|
||||
|
|
@ -1,8 +1,8 @@
|
|||
int parallelStrategy = 1;
|
||||
int numberOfGridGroups = 3;
|
||||
string gridfile = "./grid/background__2.fts";
|
||||
string gridfile1 = "./grid/upperwing__2.fts";
|
||||
string gridfile2 = "./grid/lowerwing__2.fts";
|
||||
string gridfile = "./grid/background__4.fts";
|
||||
string gridfile1 = "./grid/upperwing__4.fts";
|
||||
string gridfile2 = "./grid/lowerwing__4.fts";
|
||||
int codeOfOversetGrid = 1; // 0: 无重叠 1: 重叠;
|
||||
int codeOfOversetSlipGrid = 0; // 0: 无滑移 1: 滑移;
|
||||
int readOversetFileOrNot = 0; // 0: 适时装配 1: 读ovs文件
|
||||
|
|
@ -20,8 +20,5 @@ double toleranceForOversetBox = 1e-3;
|
|||
int twoOrderInterpolationOrNot = 1; //1-采用二阶插值（多一排插值点）；0-一阶插值
|
||||
int keyEnlargeOfActiveNodes = 1; //活跃区域扩展次数
|
||||
int outTecplotOverset = 1; //
|
||||
//kinetic
|
||||
int numberOfMovingBodies = 2;
|
||||
int morphing_0 = 0; //0-不变形；1-二维fish
|
||||
int morphing_1 = 0; //0-不变形；1-二维fish
|
||||
int morphing_2 = 0; //0-不变形；1-二维fish
|
||||
|
||||
|
||||
|
|
@ -8,17 +8,17 @@
|
|||
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||
|
||||
int numberOfGridFile = 3;
|
||||
int pgridtype = 0;
|
||||
int maxproc = 2;
|
||||
int pgridtype1 = 0;
|
||||
int pgridtype2 = 0;
|
||||
int maxproc = 4;
|
||||
int maxproc1 = 4;
|
||||
int maxproc2 = 4;
|
||||
|
||||
//string original_grid_file = "./grid/background.fts";
|
||||
//string partition_grid_file = "./grid/background__2.fts";
|
||||
|
||||
//string original_grid_file = "./grid/lowerwing.fts";
|
||||
//string partition_grid_file = "./grid/lowerwing__2.fts";
|
||||
|
||||
string original_grid_file = "./grid/upperwing.fts";
|
||||
string partition_grid_file = "./grid/upperwing__2.fts";
|
||||
string original_grid_file = "./grid/background.fts";
|
||||
string original_grid_file1 = "./grid/lowerwing.fts";
|
||||
string original_grid_file2 = "./grid/upperwing.fts";
|
||||
|
||||
// numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid.
|
||||
// 1 -- single level.
|
||||
Binary file not shown.
|
|
@ -1,65 +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 = 7;
|
||||
string bcName = "Wall";
|
||||
{
|
||||
int bcType = 2;
|
||||
}
|
||||
|
||||
string bcName = "Wall2";
|
||||
{
|
||||
int bcType = 2;
|
||||
}
|
||||
|
||||
string bcName = "UserDefined";
|
||||
{
|
||||
int bcType = 1000;
|
||||
}
|
||||
|
||||
string bcName = "Farfield";
|
||||
{
|
||||
int bcType = 4;
|
||||
}
|
||||
|
||||
string bcName = "Farfield2";
|
||||
{
|
||||
int bcType = 4;
|
||||
}
|
||||
|
||||
string bcName = "Farfield3";
|
||||
{
|
||||
int bcType = 4;
|
||||
}
|
||||
|
||||
string bcName = "Farfield4";
|
||||
{
|
||||
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
|
||||
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;
|
||||
|
||||
|
|
@ -171,7 +171,6 @@ int flowInitStep = 100;
|
|||
// Please use 'rae2822_hybrid2d__4.fts' here!
|
||||
// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
|
||||
|
||||
string gridfile = "./grid/background__2.fts";
|
||||
int plotFieldType = 1;
|
||||
|
||||
// ----------------- Advanced Parameters, DO NOT care it ----------------
|
||||
|
|
@ -20,7 +20,6 @@
|
|||
int gridtype = 0;
|
||||
int axisup = 1;
|
||||
int from_gtype = 2;
|
||||
int dumpOldGrid = 0;
|
||||
|
||||
#########################################################################
|
||||
# File path #
|
||||
|
|
@ -28,17 +27,10 @@ int dumpOldGrid = 0;
|
|||
// from_gfile: path of original data file for unstructure grid convert from.
|
||||
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
|
||||
|
||||
//string from_gfile = "./grid/aux-lower.cgns";
|
||||
//string out_gfile = "./grid/aux-lower.fts";
|
||||
int numberOfGridFile = 5;
|
||||
string from_gfile = "./grid/aux-lower.cgns";
|
||||
string from_gfile1 = "./grid/aux-upper.cgns";
|
||||
string from_gfile2 = "./grid/background.cgns";
|
||||
string from_gfile3 = "./grid/lowerwing.cgns";
|
||||
string from_gfile4 = "./grid/upperwing.cgns";
|
||||
|
||||
//string from_gfile = "./grid/aux-upper.cgns";
|
||||
//string out_gfile = "./grid/aux-upper.fts";
|
||||
|
||||
//string from_gfile = "./grid/background.cgns";
|
||||
//string out_gfile = "./grid/background.fts";
|
||||
|
||||
//string from_gfile = "./grid/lowerwing.cgns";
|
||||
//string out_gfile = "./grid/lowerwing.fts";
|
||||
|
||||
string from_gfile = "./grid/upperwing.cgns";
|
||||
string out_gfile = "./grid/upperwing.fts";
|
||||
|
|
@ -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";
|
||||
string parafilename1 = "./bin/overset_config.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
|
|
@ -35,11 +35,11 @@ string parafilename1 = "./bin/overset_config.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 = 6;
|
||||
//string parafilename = "./bin/overset_config.hypara";
|
||||
|
|
@ -1,8 +1,8 @@
|
|||
int parallelStrategy = 1;
|
||||
int numberOfGridGroups = 3;
|
||||
string gridfile = "./grid/background__2.fts";
|
||||
string gridfile1 = "./grid/upperwing__2.fts";
|
||||
string gridfile2 = "./grid/lowerwing__2.fts";
|
||||
string gridfile = "./grid/background__4.fts";
|
||||
string gridfile1 = "./grid/upperwing__4.fts";
|
||||
string gridfile2 = "./grid/lowerwing__4.fts";
|
||||
int codeOfOversetGrid = 1; // 0: 无重叠 1: 重叠;
|
||||
int codeOfOversetSlipGrid = 0; // 0: 无滑移 1: 滑移;
|
||||
int readOversetFileOrNot = 0; // 0: 适时装配 1: 读ovs文件
|
||||
|
|
@ -20,9 +20,4 @@ double toleranceForOversetBox = 1e-3;
|
|||
int twoOrderInterpolationOrNot = 1; //1-采用二阶插值（多一排插值点）；0-一阶插值
|
||||
int keyEnlargeOfActiveNodes = 1; //活跃区域扩展次数
|
||||
int outTecplotOverset = 1; //
|
||||
// kinetic
|
||||
int numberOfMovingBodies = 2;
|
||||
int morphing_0 = 0; //0-不变形；1-二维fish
|
||||
int morphing_1 = 0; //0-不变形；1-二维fish
|
||||
int morphing_2 = 0; //0-不变形；1-二维fish
|
||||
|
||||
|
|
@ -8,17 +8,17 @@
|
|||
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||
|
||||
int numberOfGridFile = 3;
|
||||
int pgridtype = 0;
|
||||
int maxproc = 2;
|
||||
int pgridtype1 = 0;
|
||||
int pgridtype2 = 0;
|
||||
int maxproc = 4;
|
||||
int maxproc1 = 4;
|
||||
int maxproc2 = 4;
|
||||
|
||||
//string original_grid_file = "./grid/background.fts";
|
||||
//string partition_grid_file = "./grid/background__2.fts";
|
||||
|
||||
//string original_grid_file = "./grid/lowerwing.fts";
|
||||
//string partition_grid_file = "./grid/lowerwing__2.fts";
|
||||
|
||||
string original_grid_file = "./grid/upperwing.fts";
|
||||
string partition_grid_file = "./grid/upperwing__2.fts";
|
||||
string original_grid_file = "./grid/background.fts";
|
||||
string original_grid_file1 = "./grid/lowerwing.fts";
|
||||
string original_grid_file2 = "./grid/upperwing.fts";
|
||||
|
||||
// numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid.
|
||||
// 1 -- single level.
|
||||
Binary file not shown.
|
|
@ -1,59 +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 = 7;
|
||||
string bcName = "Wall";
|
||||
{
|
||||
int bcType = 2;
|
||||
}
|
||||
string bcName = "Wall2";
|
||||
{
|
||||
int bcType = 2;
|
||||
}
|
||||
string bcName = "UserDefined";
|
||||
{
|
||||
int bcType = 1000;
|
||||
}
|
||||
string bcName = "Farfield";
|
||||
{
|
||||
int bcType = 4;
|
||||
}
|
||||
string bcName = "Farfield2";
|
||||
{
|
||||
int bcType = 4;
|
||||
}
|
||||
string bcName = "Farfield3";
|
||||
{
|
||||
int bcType = 4;
|
||||
}
|
||||
string bcName = "Farfield4";
|
||||
{
|
||||
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
|
||||
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 = 4;
|
||||
int nBoundaryConditions = 4;
|
||||
string bcName = "BODY";
|
||||
{
|
||||
int isSecondSegment = 0;
|
||||
|
|
|
|||
|
|
@ -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 nparafile = 1;
|
|||
//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 @@ int nparafile = 1;
|
|||
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";
|
||||
|
|
|
|||
|
|
@ -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 = 4;
|
||||
int nBoundaryConditions = 4;
|
||||
string bcName = "BODY";
|
||||
{
|
||||
int isSecondSegment = 0;
|
||||
|
|
|
|||
|
|
@ -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 nparafile = 1;
|
|||
//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/grid_para.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";
|
||||
|
|
|
|||
File diff suppressed because it is too large
Load Diff
|
|
@ -0,0 +1,237 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual 'res.dat' saved.
|
||||
|
||||
int maxSimuStep = 20000;
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// 4 -- the condition that the velocity, temperature and density are given.
|
||||
// 5 -- the condition that the velocity, temperature and pressure are given.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
|
||||
double refMachNumber = 8.7569;
|
||||
double attackd = 0.00;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
double wallTemperature = 1000.0;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 4.7001e5;
|
||||
double refDimensionalTemperature = 694.0;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
//The velocity, temperature and density are fixed.
|
||||
//int inflowParaType = 4;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalDensity = 1.0e3;
|
||||
|
||||
//The velocity, temperature and pressure are fixed.
|
||||
//int inflowParaType = 5;
|
||||
//double refDimensionalVelocity = 10.0;
|
||||
//double refDimensionalPressure = 101325.0;
|
||||
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
#########################################################################
|
||||
# Physical models #
|
||||
#########################################################################
|
||||
// viscousType: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "1eq-sa", when viscousType = 3.
|
||||
// -- "2eq-kw-menter-sst", when viscousType = 4.
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS.(default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
int viscousType = 1;
|
||||
string viscousName = "laminar";
|
||||
|
||||
//int viscousType = 3;
|
||||
//string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
#########################################################################
|
||||
# Spatial Discretisation #
|
||||
#########################################################################
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "ausmpw", "ausmpw+".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "minmod", "3rd_minmod_smooth".
|
||||
|
||||
string inviscidSchemeName = "steger";
|
||||
string str_limiter_name = "minmod";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "vencat", "barth".
|
||||
// -- "1st", meaning accuracy of first-order.
|
||||
// -- "nolim", no limiter.
|
||||
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'.
|
||||
// The smaller the value, the more robust it is.
|
||||
|
||||
string uns_scheme_name = "steger";
|
||||
string uns_limiter_name = "vencat";
|
||||
double venkatCoeff = 0.5;
|
||||
|
||||
#########################################################################
|
||||
# Temporal Discretisation #
|
||||
#########################################################################
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// CFLEnd: The CFL number, [0.1, 100].
|
||||
// The bigger the value, the convergence faster but lower robustness.
|
||||
// ktmax: The lower the value, the more robustness, 1.0e5 - 1.0e10.
|
||||
|
||||
int iunsteady = 0;
|
||||
double CFLStart = 0.1;
|
||||
double CFLEnd = 1.0;
|
||||
int CFLVaryStep = 1000;
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
#########################################################################
|
||||
# File In or Out #
|
||||
#########################################################################
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// IMPORTANT WARNING: The file index should be ignored,
|
||||
// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
|
||||
// Please use 'rae2822_hybrid2d__4.fts' here!
|
||||
// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
|
||||
|
||||
string gridfile = "./grid/2D_Cylinder_Rn0d045_160X131_dy1d-5.fts";
|
||||
int plotFieldType = 0;
|
||||
|
||||
// ----------------- Advanced Parameters, DO NOT care it ----------------
|
||||
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
|
||||
// visualVariables: Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
|
||||
// -- viscosityLaminar(7), viscosityTurbulent(8),
|
||||
// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12),
|
||||
// -- strain_rate(13), Q_criteria(14), Cp(15), timeStep(16), volume(17),
|
||||
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
|
||||
// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
|
||||
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// limitVariables: Limit model (It is useful only if limitVector is 0).
|
||||
// 0 -- limit only for pressure and denstiny, then get the min value.
|
||||
// 1 -- limit for every variables, then get the min value.
|
||||
// limitVector:
|
||||
// 0 -- Each variable use the same limiter coefficient.
|
||||
// 1 -- Each variable use the respective limiter coefficients.
|
||||
// reconmeth:
|
||||
// 0 -- When reconstruct face value, Q+, Q- use respective limiter coefficients.
|
||||
// 1 -- Q+, Q- use the min limiter coefficients of left and right cell.
|
||||
|
||||
int reconmeth = 0;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 1;
|
||||
|
||||
#########################################################################
|
||||
# Non-equilibrium gas #
|
||||
#########################################################################
|
||||
// nGasModel: The type of gas.
|
||||
// 0 -- Earth gas.
|
||||
// 1 -- Mars gas.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
// nchemsrc:
|
||||
// 0 -- the source terms are not computed.
|
||||
// 1 -- the source terms are computed.
|
||||
// nchemrad:
|
||||
// 0 -- compute the spectrum radius without considering chemical reaction flow.
|
||||
// 1 -- compute the spectrum radius that need to count the contribution from chemical reaction flow.
|
||||
// ntmodel: The thermodynamic temperature model.
|
||||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes.
|
||||
int nchem = 1;
|
||||
int nIdealState = 1;
|
||||
int nchemsrc = 0;
|
||||
int nchemrad = 0;
|
||||
int ntmodel = 1;
|
||||
string gasfile = "Gas-Mixture";
|
||||
string speciesName = "O2, N2";
|
||||
string initMassFraction = "0.23, 0.77";
|
||||
|
|
@ -0,0 +1,29 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE.
|
||||
// 1 -- PHengLEI, *.fts.
|
||||
// 2 -- CGNS, *.cgns.
|
||||
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
|
||||
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
|
||||
// 5 -- Fluent, *.cas/*.msh.
|
||||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
int gridtype = 0;
|
||||
int axisup = 1;
|
||||
int from_gtype = 2;
|
||||
#########################################################################
|
||||
# File path #
|
||||
#########################################################################
|
||||
// from_gfile: path of original data file for unstructure grid convert from.
|
||||
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
|
||||
string from_gfile = "./grid/2D_Cylinder_Rn0d045_160X131_dy1d-5.cgns";
|
||||
string out_gfile = "./grid/2D_Cylinder_Rn0d045_160X131_dy1d-5.fts";
|
||||
|
|
@ -0,0 +1,52 @@
|
|||
string title = "PHengLEI Main Parameter Control File";
|
||||
|
||||
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
|
||||
string defaultParaFile = "./bin/cfd_para.hypara";
|
||||
|
||||
// ndim: Dimensional of the grid, 2 or 3.
|
||||
// nparafile: the number of parameter files.
|
||||
// nsimutask: simulation task type.
|
||||
// 0 -- CFD Solver of NS or Turbulation.
|
||||
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
|
||||
// Grid conversion: from other format to PHengLEI format (.fts).
|
||||
// Grid reconstruction: such as grid adaptation.
|
||||
// Grid merging: merge two blocks into one block.
|
||||
// Grid repairing: repair the original grid in order to remove the negative volume cells.
|
||||
// 2 -- Wall distance computation for turb-solver.
|
||||
// 3 -- Grid partition.
|
||||
int ndim = 2;
|
||||
int nparafile = 1;
|
||||
|
||||
int nsimutask = 0;
|
||||
//string parafilename = "./bin/cfd_para_subsonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_transonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_supersonic.hypara";
|
||||
string parafilename = "./bin/cfd_para_hypersonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
||||
//int nsimutask = 2;
|
||||
//string parafilename = "./bin/cfd_para.hypara";
|
||||
|
||||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 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 numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
Binary file not shown.
Binary file not shown.
File diff suppressed because it is too large
Load Diff
|
|
@ -0,0 +1,237 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual 'res.dat' saved.
|
||||
|
||||
int maxSimuStep = 50000;
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// 4 -- the condition that the velocity, temperature and density are given.
|
||||
// 5 -- the condition that the velocity, temperature and pressure are given.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
|
||||
//double refMachNumber = 8.7569;
|
||||
double attackd = 0.00;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
double wallTemperature = 2000.0;
|
||||
|
||||
//int inflowParaType = 0;
|
||||
//double refReNumber = 4.7001e5;
|
||||
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
//The velocity, temperature and density are fixed.
|
||||
//int inflowParaType = 4;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalDensity = 1.0e3;
|
||||
|
||||
//The velocity, temperature and pressure are fixed.
|
||||
int inflowParaType = 5;
|
||||
double refDimensionalVelocity = 5280.0;
|
||||
double refDimensionalPressure = 664.0;
|
||||
double refDimensionalTemperature = 293.0;
|
||||
double freestream_vibration_temperature = 293.0;
|
||||
|
||||
double gridScaleFactor = 0.001;
|
||||
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
#########################################################################
|
||||
# Physical models #
|
||||
#########################################################################
|
||||
// viscousType: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "1eq-sa", when viscousType = 3.
|
||||
// -- "2eq-kw-menter-sst", when viscousType = 4.
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS.(default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
int viscousType = 1;
|
||||
string viscousName = "laminar";
|
||||
|
||||
//int viscousType = 3;
|
||||
//string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
#########################################################################
|
||||
# Spatial Discretisation #
|
||||
#########################################################################
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "ausmpw", "ausmpw+".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "minmod", "3rd_minmod_smooth".
|
||||
|
||||
string inviscidSchemeName = "steger";
|
||||
string str_limiter_name = "minmod";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "vencat", "barth".
|
||||
// -- "1st", meaning accuracy of first-order.
|
||||
// -- "nolim", no limiter.
|
||||
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'.
|
||||
// The smaller the value, the more robust it is.
|
||||
|
||||
string uns_scheme_name = "steger";
|
||||
string uns_limiter_name = "vencat";
|
||||
double venkatCoeff = 0.1;
|
||||
|
||||
#########################################################################
|
||||
# Temporal Discretisation #
|
||||
#########################################################################
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// CFLEnd: The CFL number, [0.1, 100].
|
||||
// The bigger the value, the convergence faster but lower robustness.
|
||||
// ktmax: The lower the value, the more robustness, 1.0e5 - 1.0e10.
|
||||
|
||||
int iunsteady = 0;
|
||||
double CFLEnd = 0.5;
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
#########################################################################
|
||||
# File In or Out #
|
||||
#########################################################################
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// IMPORTANT WARNING: The file index should be ignored,
|
||||
// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
|
||||
// Please use 'rae2822_hybrid2d__4.fts' here!
|
||||
// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
|
||||
|
||||
string gridfile = "./grid/R6d35MM_HalfModel_DY6d25E-4MM.fts";
|
||||
int plotFieldType = 0;
|
||||
|
||||
// ----------------- Advanced Parameters, DO NOT care it ----------------
|
||||
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
|
||||
// visualVariables: Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
|
||||
// -- viscosityLaminar(7), viscosityTurbulent(8),
|
||||
// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12),
|
||||
// -- strain_rate(13), Q_criteria(14), Cp(15), timeStep(16), volume(17),
|
||||
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
|
||||
// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
|
||||
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// limitVariables: Limit model (It is useful only if limitVector is 0).
|
||||
// 0 -- limit only for pressure and denstiny, then get the min value.
|
||||
// 1 -- limit for every variables, then get the min value.
|
||||
// limitVector:
|
||||
// 0 -- Each variable use the same limiter coefficient.
|
||||
// 1 -- Each variable use the respective limiter coefficients.
|
||||
// reconmeth:
|
||||
// 0 -- When reconstruct face value, Q+, Q- use respective limiter coefficients.
|
||||
// 1 -- Q+, Q- use the min limiter coefficients of left and right cell.
|
||||
|
||||
int reconmeth = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 1;
|
||||
|
||||
#########################################################################
|
||||
# Non-equilibrium gas #
|
||||
#########################################################################
|
||||
// nGasModel: The type of gas.
|
||||
// 0 -- Earth gas.
|
||||
// 1 -- Mars gas.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
// nchemsrc:
|
||||
// 0 -- the source terms are not computed.
|
||||
// 1 -- the source terms are computed.
|
||||
// nchemrad:
|
||||
// 0 -- compute the spectrum radius without considering chemical reaction flow.
|
||||
// 1 -- compute the spectrum radius that need to count the contribution from chemical reaction flow.
|
||||
// ntmodel: The thermodynamic temperature model.
|
||||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes.
|
||||
int nchem = 1;
|
||||
int nIdealState = 1;
|
||||
int nchemsrc = 0;
|
||||
int nchemrad = 0;
|
||||
int ntmodel = 1;
|
||||
string gasfile = "Gas-Mixture";
|
||||
string speciesName = " O2, N2";
|
||||
string initMassFraction = "0.23, 0.77";
|
||||
|
|
@ -0,0 +1,29 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE.
|
||||
// 1 -- PHengLEI, *.fts.
|
||||
// 2 -- CGNS, *.cgns.
|
||||
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
|
||||
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
|
||||
// 5 -- Fluent, *.cas/*.msh.
|
||||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
int gridtype = 0;
|
||||
int axisup = 1;
|
||||
int from_gtype = 2;
|
||||
#########################################################################
|
||||
# File path #
|
||||
#########################################################################
|
||||
// from_gfile: path of original data file for unstructure grid convert from.
|
||||
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
|
||||
string from_gfile = "./grid/R6d35MM_HalfModel_DY6d25E-4MM.cgns";
|
||||
string out_gfile = "./grid/R6d35MM_HalfModel_DY6d25E-4MM.fts";
|
||||
|
|
@ -0,0 +1,52 @@
|
|||
string title = "PHengLEI Main Parameter Control File";
|
||||
|
||||
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
|
||||
string defaultParaFile = "./bin/cfd_para.hypara";
|
||||
|
||||
// ndim: Dimensional of the grid, 2 or 3.
|
||||
// nparafile: the number of parameter files.
|
||||
// nsimutask: simulation task type.
|
||||
// 0 -- CFD Solver of NS or Turbulation.
|
||||
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
|
||||
// Grid conversion: from other format to PHengLEI format (.fts).
|
||||
// Grid reconstruction: such as grid adaptation.
|
||||
// Grid merging: merge two blocks into one block.
|
||||
// Grid repairing: repair the original grid in order to remove the negative volume cells.
|
||||
// 2 -- Wall distance computation for turb-solver.
|
||||
// 3 -- Grid partition.
|
||||
int ndim = 3;
|
||||
int nparafile = 1;
|
||||
|
||||
int nsimutask = 0;
|
||||
//string parafilename = "./bin/cfd_para_subsonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_transonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_supersonic.hypara";
|
||||
string parafilename = "./bin/cfd_para_hypersonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
||||
//int nsimutask = 2;
|
||||
//string parafilename = "./bin/cfd_para.hypara";
|
||||
|
||||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 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 numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
Binary file not shown.
Binary file not shown.
|
|
@ -0,0 +1,79 @@
|
|||
# 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 nBoundaryConditions = 6;
|
||||
string bcName = "jetwall";
|
||||
{
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
}
|
||||
string bcName = "pipelinetop";
|
||||
{
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
}
|
||||
string bcName = "symmetry";
|
||||
{
|
||||
int bcType = 3;
|
||||
}
|
||||
string bcName = "inlet";
|
||||
{
|
||||
int bcType = 5;
|
||||
int inflowParaType = 5;
|
||||
double refDimensionalVelocity = 9.2;
|
||||
double refDimensionalPressure = 101325.0;
|
||||
string speciesName ="Air, CH4";
|
||||
double initMassFraction[2] = [1.0, 0.0];
|
||||
}
|
||||
string bcName = "jet";
|
||||
{
|
||||
int bcType = 5;
|
||||
int inflowParaType = 5;
|
||||
double refDimensionalVelocity = 68.9;
|
||||
double refDimensionalPressure = 101325.0;
|
||||
string speciesName ="Air, CH4";
|
||||
double initMassFraction[2] = [0.0, 1.0];
|
||||
}
|
||||
string bcName = "outlet";
|
||||
{
|
||||
int bcType = 6;
|
||||
}
|
||||
|
||||
# 'bcType' is defined as following:
|
||||
# -2: WAKE
|
||||
# -1: INTERFACE
|
||||
# 0 : NO_BOUNDARY_CONDITION
|
||||
# 1 : EXTRAPOLATION
|
||||
# 2 : SOLID_SURFACE
|
||||
# 3 : SYMMETRY
|
||||
# 4 : FARFIELD
|
||||
# 5 : INFLOW
|
||||
# 6 : OUTFLOW
|
||||
# 52: PRESSURE_INLET
|
||||
# 62: PRESSURE_OUTLET
|
||||
# 61: OUTFLOW_CONFINED
|
||||
# 7 : POLE
|
||||
File diff suppressed because it is too large
Load Diff
|
|
@ -0,0 +1,256 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual 'res.dat' saved.
|
||||
|
||||
int maxSimuStep = 50000;
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
int ifLowSpeedPrecon = 0;
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// 4 -- the condition that the velocity, temperature and density are given.
|
||||
// 5 -- the condition that the velocity, temperature and pressure are given.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
|
||||
//double refMachNumber = 0.2;
|
||||
double attackd = 0.00;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
|
||||
//int inflowParaType = 0;
|
||||
//double refReNumber = 1.0e5;
|
||||
double refDimensionalTemperature = 300.0;
|
||||
double freestream_vibration_temperature = 300.0;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
//The velocity, temperature and density are fixed.
|
||||
//int inflowParaType = 4;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalDensity = 1.0e3;
|
||||
|
||||
//The velocity, temperature and pressure are fixed.
|
||||
int inflowParaType = 5;
|
||||
double refDimensionalVelocity = 9.2;
|
||||
double refDimensionalPressure = 101325.0;
|
||||
|
||||
double gridScaleFactor = 0.001;
|
||||
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
#########################################################################
|
||||
# Physical models #
|
||||
#########################################################################
|
||||
// viscousType: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "1eq-sa", when viscousType = 3.
|
||||
// -- "2eq-kw-menter-sst", when viscousType = 4.
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS.(default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
int viscousType = 1;
|
||||
string viscousName = "laminar";
|
||||
|
||||
//int viscousType = 3;
|
||||
//string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
#########################################################################
|
||||
# Spatial Discretisation #
|
||||
#########################################################################
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "ausmpw", "ausmpw+".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "minmod", "3rd_minmod_smooth".
|
||||
|
||||
string inviscidSchemeName = "steger";
|
||||
string str_limiter_name = "minmod";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "vencat", "barth".
|
||||
// -- "1st", meaning accuracy of first-order.
|
||||
// -- "nolim", no limiter.
|
||||
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'.
|
||||
// The smaller the value, the more robust it is.
|
||||
|
||||
string uns_scheme_name = "steger";
|
||||
string uns_limiter_name = "vencat";
|
||||
double venkatCoeff = 0.5;
|
||||
|
||||
#########################################################################
|
||||
# Temporal Discretisation #
|
||||
#########################################################################
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// CFLEnd: The CFL number, [0.1, 100].
|
||||
// The bigger the value, the convergence faster but lower robustness.
|
||||
// nLUSGSSweeps: Number of Sub-iteration of LU-SGS.
|
||||
// 1 -- is recommended for structured solver.
|
||||
// 1-3 -- is recommended for unstructured solver.
|
||||
|
||||
int iunsteady = 0;
|
||||
double CFLEnd = 50.0;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
|
||||
#########################################################################
|
||||
# Multi-Grid parameters #
|
||||
#########################################################################
|
||||
// nMGLevel: The number of Multi-Grid level.
|
||||
// = 1 -- single-level.
|
||||
// > 1 -- multi-level.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int flowInitStep = 100;
|
||||
|
||||
#########################################################################
|
||||
# File In or Out #
|
||||
#########################################################################
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// IMPORTANT WARNING: The file index should be ignored,
|
||||
// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
|
||||
// Please use 'rae2822_hybrid2d__4.fts' here!
|
||||
// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
|
||||
|
||||
string gridfile = "./grid/multi-species.fts";
|
||||
int plotFieldType = 0;
|
||||
|
||||
// ----------------- Advanced Parameters, DO NOT care it ----------------
|
||||
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
|
||||
// visualVariables: Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
|
||||
// -- viscosityLaminar(7), viscosityTurbulent(8),
|
||||
// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12),
|
||||
// -- strain_rate(13), Q_criteria(14), Cp(15), timeStep(16), volume(17),
|
||||
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
|
||||
// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
|
||||
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 6;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
|
||||
// limitVariables: Limit model (It is useful only if limitVector is 0).
|
||||
// 0 -- limit only for pressure and denstiny, then get the min value.
|
||||
// 1 -- limit for every variables, then get the min value.
|
||||
// limitVector:
|
||||
// 0 -- Each variable use the same limiter coefficient.
|
||||
// 1 -- Each variable use the respective limiter coefficients.
|
||||
// reconmeth:
|
||||
// 0 -- When reconstruct face value, Q+, Q- use respective limiter coefficients.
|
||||
// 1 -- Q+, Q- use the min limiter coefficients of left and right cell.
|
||||
|
||||
int reconmeth = 0;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 1;
|
||||
|
||||
#########################################################################
|
||||
# Non-equilibrium gas #
|
||||
#########################################################################
|
||||
// nGasModel: The type of gas.
|
||||
// 0 -- Earth gas.
|
||||
// 1 -- Mars gas.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
// nchemsrc:
|
||||
// 0 -- the source terms are not computed.
|
||||
// 1 -- the source terms are computed.
|
||||
// nchemrad:
|
||||
// 0 -- compute the spectrum radius without considering chemical reaction flow.
|
||||
// 1 -- compute the spectrum radius that need to count the contribution from chemical reaction flow.
|
||||
// ntmodel: The thermodynamic temperature model.
|
||||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes.
|
||||
int nchem = 1;
|
||||
int nIdealState = 1;
|
||||
int nchemsrc = 0;
|
||||
int nchemrad = 0;
|
||||
int ntmodel = 1;
|
||||
string gasfile = "Gas-Mixture";
|
||||
string speciesName ="Air, CH4";
|
||||
string initMassFraction = "1.0, 0.0";
|
||||
|
|
@ -0,0 +1,30 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE.
|
||||
// 1 -- PHengLEI, *.fts.
|
||||
// 2 -- CGNS, *.cgns.
|
||||
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
|
||||
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
|
||||
// 5 -- Fluent, *.cas/*.msh.
|
||||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
int gridtype = 0;
|
||||
int axisup = 1;
|
||||
int from_gtype = 2;
|
||||
|
||||
#########################################################################
|
||||
# File path #
|
||||
#########################################################################
|
||||
// from_gfile: path of original data file for unstructure grid convert from.
|
||||
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
|
||||
string from_gfile = "./grid/multi-species.cgns";
|
||||
string out_gfile = "./grid/multi-species.fts";
|
||||
|
|
@ -0,0 +1,52 @@
|
|||
string title = "PHengLEI Main Parameter Control File";
|
||||
|
||||
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
|
||||
string defaultParaFile = "./bin/cfd_para.hypara";
|
||||
|
||||
// ndim: Dimensional of the grid, 2 or 3.
|
||||
// nparafile: the number of parameter files.
|
||||
// nsimutask: simulation task type.
|
||||
// 0 -- CFD Solver of NS or Turbulation.
|
||||
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
|
||||
// Grid conversion: from other format to PHengLEI format (.fts).
|
||||
// Grid reconstruction: such as grid adaptation.
|
||||
// Grid merging: merge two blocks into one block.
|
||||
// Grid repairing: repair the original grid in order to remove the negative volume cells.
|
||||
// 2 -- Wall distance computation for turb-solver.
|
||||
// 3 -- Grid partition.
|
||||
int ndim = 2;
|
||||
int nparafile = 1;
|
||||
|
||||
int nsimutask = 0;
|
||||
string parafilename = "./bin/cfd_para_subsonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_transonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_supersonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_hypersonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
||||
//int nsimutask = 2;
|
||||
//string parafilename = "./bin/cfd_para.hypara";
|
||||
|
||||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 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 numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
Binary file not shown.
Binary file not shown.
Binary file not shown.
Binary file not shown.
|
|
@ -0,0 +1,61 @@
|
|||
# nBoundaryConditions: 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 nBoundaryConditions = 3;
|
||||
string bcName = "wall";
|
||||
{
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
string flowType = "FLOW_SOLID_SURFACE";
|
||||
}
|
||||
string bcName = "inlet";
|
||||
{
|
||||
int bcType = 5;
|
||||
string flowType = "FLOW_VELOCITY_INLET";
|
||||
double flowU =0.9191874;
|
||||
}
|
||||
string bcName = "outlet";
|
||||
{
|
||||
int bcType = 6;
|
||||
string flowType = "FLOW_PRESSURE_OUTLET";
|
||||
double flowP =0;
|
||||
}
|
||||
|
||||
# 'bcType' is defined as following:
|
||||
# -2: WAKE
|
||||
# -1: INTERFACE
|
||||
# 0 : NO_BOUNDARY_CONDITION
|
||||
# 1 : EXTRAPOLATION
|
||||
# 2 : SOLID_SURFACE
|
||||
# 3 : SYMMETRY
|
||||
# 4 : FARFIELD
|
||||
# 5 : INFLOW
|
||||
# 6 : OUTFLOW
|
||||
# 52: PRESSURE_INLET
|
||||
# 62: PRESSURE_OUTLET
|
||||
# 61: OUTFLOW_CONFINED
|
||||
# 7 : POLE
|
||||
File diff suppressed because it is too large
Load Diff
|
|
@ -0,0 +1,215 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// nIsComputeWallDist: Whether to compute the wall distance.
|
||||
// 0 -- Compute wall distance.
|
||||
// 1 -- Not compute.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual 'res.dat' saved.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// compressible: An indicator that distinguishes density base from pressure base. 0-incompressible, 1-compressible
|
||||
// isUnsteady: An indicator that distinguishes unsteady problem from steady problem. 0-steady, 1-unsteady
|
||||
// startTime: The initial time of the unsteady simulation.
|
||||
// endTime: The end time of the unsteady simulation.
|
||||
// dt: The time interval of the unsteady simulation.
|
||||
// innerIter: The number of step for current time.
|
||||
// OutputTimeStep: The interval step of output for unsteady simulation.
|
||||
|
||||
int nIsComputeWallDist = 1;
|
||||
string gridfile = "./grid/back.fts";
|
||||
int maxSimuStep = 2000;
|
||||
int intervalStepFlow = 2000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
int compressible = 0;
|
||||
int iunsteady = 0;
|
||||
double startTime = 0.0;
|
||||
double endTime = 30;
|
||||
double dt = 0.1;
|
||||
int innerIter = 10;
|
||||
int OutputTimeStep = 5;
|
||||
|
||||
#########################################################################
|
||||
# Post-Processing #
|
||||
#########################################################################
|
||||
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
|
||||
// visualVariables : Variable types dumped, listed as following:
|
||||
// -- U(22), V(23), W(24), P(25), CP(26), T(27), DEN(28), VIS(29), TE(31), ED(32), enthalpy(70)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
||||
int nVisualVariables = 4;
|
||||
int visualVariables[] = [22, 23, 24, 25];
|
||||
|
||||
#########################################################################
|
||||
# Flow Parameter #
|
||||
#########################################################################
|
||||
string FLOW[] = "FLOW";
|
||||
|
||||
// Initial value of variables or constant
|
||||
double initRho = 1.0;
|
||||
double initMu = 0.0001;
|
||||
double initU = 0.9191874;
|
||||
double initV = 0;
|
||||
double initW = 0;
|
||||
double initP = 0;
|
||||
|
||||
// Relaxing factor
|
||||
double urfU = 0.4;
|
||||
double urfV = 0.4;
|
||||
double urfW = 0.4;
|
||||
double urfP = 0.3;
|
||||
double urfFlux = 0.4;
|
||||
|
||||
// Tolerance for governing equations
|
||||
double resU = 1e-6;
|
||||
double resV = 1e-6;
|
||||
double resW = 1e-5;
|
||||
double resP = 1e-5;
|
||||
|
||||
// Solver for solving linear system
|
||||
// : CGS/GMRES/BiCGSTAB/AMG
|
||||
string iterSolvU = "BiCGSTAB";
|
||||
string iterSolvV = "BiCGSTAB";
|
||||
string iterSolvW = "BiCGSTAB";
|
||||
string iterSolvP = "AMG";
|
||||
|
||||
// Max Iter for solving linear system
|
||||
int maxSweepU = 30;
|
||||
int maxSweepV = 30;
|
||||
int maxSweepW = 30;
|
||||
int maxSweepP = 30;
|
||||
|
||||
// Tolerance for solving linear system
|
||||
double iterSolvTolU = 1e-3;
|
||||
double iterSolvTolV = 1e-3;
|
||||
double iterSolvTolW = 1e-3;
|
||||
double iterSolvTolP = 1e-2;
|
||||
|
||||
// Gradient Calculation
|
||||
// : GAUSS/LSQ
|
||||
string UGradCalc = "GAUSS";
|
||||
string VGradCalc = "GAUSS";
|
||||
string WGradCalc = "GAUSS";
|
||||
string PGradCalc = "GAUSS";
|
||||
|
||||
// Convection scheme
|
||||
// : UPWIND/CDS/QUICK/SUDS
|
||||
string flowConvCalc = "UPWIND";
|
||||
|
||||
// Diffusion scheme(central difference)
|
||||
// : NON_ORTHOGONAL
|
||||
string flowDiffCalc = "NON_ORTHOGONAL";
|
||||
|
||||
// Transient scheme
|
||||
// : CRANK_NICOLSON/IMPLICIT_2ND_ORDER/IMPLICIT_EULER
|
||||
string flowTranCalc = "IMPLICIT_EULER";
|
||||
|
||||
// Source for flow
|
||||
// : FLOW_DEFAULT/FLOW_GRAVITY
|
||||
string flowSourceCalc[] = "FLOW_DEFAULT";
|
||||
|
||||
//string flowSourceCalc[] = "FLOW_DEFAULT FLOW_GRAVITY";
|
||||
int bodyForceFlag = 0;
|
||||
//double gravityX = 0.0;
|
||||
//double gravityY = -9.81;
|
||||
//double gravityZ = 0.0;
|
||||
int isBoussinesq = 0;
|
||||
#########################################################################
|
||||
# Turbulence Parameter #
|
||||
#########################################################################
|
||||
// turb SA
|
||||
//int viscousType = 11; //SPALART_ALLMARAS = 11, KEPSILON = 13
|
||||
string TURB_SA[] = ["TURB_SA"];
|
||||
string TURB_SA_SCALAR_NAME[] = ["kinetic"];
|
||||
double urfMu = 1.0;
|
||||
|
||||
double kineticInitValue = 1.0;
|
||||
string kineticConvCalc = "UPWIND";
|
||||
string kineticDiffCalc = "NON_ORTHOGONAL";
|
||||
string kineticSourceCalc[] = "TURB_SA_DEFAULT";
|
||||
double kineticUrf = 1.0;
|
||||
double kineticRes = 1e-6;
|
||||
|
||||
string turbIterSolv = "BiCGSTAB";
|
||||
int turbMaxSweep = 30;
|
||||
double turbIterSolvTol = 1e-12;
|
||||
|
||||
|
||||
// turb K-EPSILON
|
||||
//int viscousType = 13; //SPALART_ALLMARAS = 11, KEPSILON = 13
|
||||
string TURB_K_EPSILON[] = ["TURB_K","TURB_EPSILON"];
|
||||
string TURB_K_EPSILON_SCALAR_NAME[] = ["kinetic", "epsilon
|
||||
|
||||
string turbIterSolv = "BiCGSTAB";
|
||||
int turbMaxSweep = 30;
|
||||
double turbIterSolvTol = 1e-12;
|
||||
|
||||
string TURB_K[] = ["TURB_K"];
|
||||
string TURB_K_SCALAR_NAME[] = ["kinetic"];
|
||||
string TURB_EPSILON[] = ["TURB_EPSILON"];
|
||||
string TURB_EPSILON_SCALAR_NAME[] = ["epsilon"];
|
||||
double urfMu = 1.0;
|
||||
|
||||
// turb k
|
||||
double kineticInitValue = 15.48;
|
||||
string kineticConvCalc = "UPWIND";
|
||||
string kineticDiffCalc = "NON_ORTHOGONAL";
|
||||
string kineticSourceCalc[] = "TURB_K_DEFAULT";
|
||||
double kineticUrf = 0.6;
|
||||
double kineticRes = 1e-6;
|
||||
|
||||
// turb epsilon
|
||||
double epsilonInitValue = 200.3;
|
||||
string epsilonConvCalc = "UPWIND";
|
||||
string epsilonDiffCalc = "NON_ORTHOGONAL";
|
||||
string epsilonSourceCalc[] = "TURB_EPSILON_DEFAULT";
|
||||
double epsilonUrf = 0.6;
|
||||
double epsilonRes = 1e-6;
|
||||
|
||||
#########################################################################
|
||||
# Energy Parameter #
|
||||
#########################################################################
|
||||
// energyType: The energy solver switch. 0-off, 1-on
|
||||
// ENERGY[]: Solver binding for factory mode.
|
||||
// ENERGY_SCALAR_NAME[]: The name of variable to be solved in energy equation.
|
||||
// energyPrintName[]: The output on the screen during the solution.
|
||||
|
||||
int energyType = 0;
|
||||
string ENERGY[] = ["ENERGY"];
|
||||
string ENERGY_SCALAR_NAME[] = "enthalpy";
|
||||
string energyPrintName[] = ["H"];
|
||||
|
||||
// Initial value of variables or constant
|
||||
double initT = 273.0;
|
||||
double initK = 0.026;
|
||||
double initCPg = 1007.0;
|
||||
double urfT = 0.8;
|
||||
double urfH = 0.7;
|
||||
double enthalpyInitValue = 0.21;
|
||||
|
||||
// Discrete schemes
|
||||
string energyConvCalc = "UPWIND";
|
||||
string energyDiffCalc = "NON_ORTHOGONAL";
|
||||
string energySourceCalc[] = ["EMPTY"];
|
||||
string energyGradCalc = "GAUSS";
|
||||
string energyTranCalc = "IMPLICIT_EULER";
|
||||
|
||||
// Set for solving linear equations
|
||||
string enthalpyIterSolv = "BiCGSTAB";
|
||||
int enthalpyMaxSweep = 30;
|
||||
double enthalpyIterSolvTol = 1e-12;
|
||||
double enthalpyRes = 1e-6;
|
||||
|
|
@ -0,0 +1,30 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE.
|
||||
// 1 -- PHengLEI, *.fts.
|
||||
// 2 -- CGNS, *.cgns.
|
||||
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
|
||||
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
|
||||
// 5 -- Fluent, *.cas/*.msh.
|
||||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
int gridtype = 0;
|
||||
int axisup = 1;
|
||||
int from_gtype = 5;
|
||||
|
||||
#########################################################################
|
||||
# File path #
|
||||
#########################################################################
|
||||
// from_gfile: path of original data file for unstructure grid convert from.
|
||||
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
|
||||
string from_gfile = "./grid/back.cas";
|
||||
string out_gfile = "./grid/back.fts";
|
||||
|
|
@ -0,0 +1,52 @@
|
|||
string title = "PHengLEI Main Parameter Control File";
|
||||
|
||||
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
|
||||
string defaultParaFile = "./bin/cfd_para.hypara";
|
||||
|
||||
// ndim: Dimensional of the grid, 2 or 3.
|
||||
// nparafile: the number of parameter files.
|
||||
// nsimutask: simulation task type.
|
||||
// 0 -- CFD Solver of NS or Turbulation.
|
||||
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
|
||||
// Grid conversion: from other format to PHengLEI format (.fts).
|
||||
// Grid reconstruction: such as grid adaptation.
|
||||
// Grid merging: merge two blocks into one block.
|
||||
// Grid repairing: repair the original grid in order to remove the negative volume cells.
|
||||
// 2 -- Wall distance computation for turb-solver.
|
||||
// 3 -- Grid partition.
|
||||
int ndim = 2;
|
||||
int nparafile = 1;
|
||||
|
||||
int nsimutask = 0;
|
||||
string parafilename = "./bin/cfd_para_incompressible.hypara"
|
||||
//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";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
||||
//int nsimutask = 2;
|
||||
//string parafilename = "./bin/cfd_para.hypara";
|
||||
|
||||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 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 numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
File diff suppressed because one or more lines are too long
|
|
@ -0,0 +1,73 @@
|
|||
# nBoundaryConditions: 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 nBoundaryConditions = 4;
|
||||
string bcName = "bottomwall";
|
||||
{
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
string flowType = "FLOW_SOLID_SURFACE";
|
||||
string energyBoundaryType = "ENERGY_WALL";
|
||||
}
|
||||
string bcName = "coldwall";
|
||||
{
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
string flowType = "FLOW_SOLID_SURFACE";
|
||||
string energyBoundaryType = "ENERGY_WALL";
|
||||
double T = 290.0;
|
||||
}
|
||||
string bcName = "hotwall";
|
||||
{
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
string flowType = "FLOW_SOLID_SURFACE";
|
||||
string energyBoundaryType = "ENERGY_WALL";
|
||||
double T = 305.0;
|
||||
}
|
||||
string bcName = "topwall";
|
||||
{
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
string flowType = "FLOW_SOLID_SURFACE";
|
||||
string energyBoundaryType = "ENERGY_WALL";
|
||||
}
|
||||
|
||||
# 'bcType' is defined as following:
|
||||
# -2: WAKE
|
||||
# -1: INTERFACE
|
||||
# 0 : NO_BOUNDARY_CONDITION
|
||||
# 1 : EXTRAPOLATION
|
||||
# 2 : SOLID_SURFACE
|
||||
# 3 : SYMMETRY
|
||||
# 4 : FARFIELD
|
||||
# 5 : INFLOW
|
||||
# 6 : OUTFLOW
|
||||
# 52: PRESSURE_INLET
|
||||
# 62: PRESSURE_OUTLET
|
||||
# 61: OUTFLOW_CONFINED
|
||||
# 7 : POLE
|
||||
File diff suppressed because it is too large
Load Diff
|
|
@ -0,0 +1,214 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// nIsComputeWallDist: Whether to compute the wall distance.
|
||||
// 0 -- Compute wall distance.
|
||||
// 1 -- Not compute.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual 'res.dat' saved.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// compressible: An indicator that distinguishes density base from pressure base. 0-incompressible, 1-compressible
|
||||
// isUnsteady: An indicator that distinguishes unsteady problem from steady problem. 0-steady, 1-unsteady
|
||||
// startTime: The initial time of the unsteady simulation.
|
||||
// endTime: The end time of the unsteady simulation.
|
||||
// dt: The time interval of the unsteady simulation.
|
||||
// innerIter: The number of step for current time.
|
||||
// OutputTimeStep: The interval step of output for unsteady simulation.
|
||||
|
||||
int nIsComputeWallDist = 1;
|
||||
string gridfile = "./grid/run.fts";
|
||||
int maxSimuStep = 10000;
|
||||
int intervalStepFlow = 2000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
int compressible = 0;
|
||||
int iunsteady = 0;
|
||||
double startTime = 0.0;
|
||||
double endTime = 20.0;
|
||||
double dt = 0.1;
|
||||
int innerIter = 10;
|
||||
int OutputTimeStep = 5;
|
||||
|
||||
#########################################################################
|
||||
# Post-Processing #
|
||||
#########################################################################
|
||||
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
|
||||
// visualVariables : Variable types dumped, listed as following:
|
||||
// -- U(22), V(23), W(24), P(25), CP(26), T(27), DEN(28), VIS(29), TE(31), ED(32), enthalpy(70)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
||||
int nVisualVariables = 6;
|
||||
int visualVariables[] = [22, 23, 24, 25, 27, 70];
|
||||
|
||||
#########################################################################
|
||||
# Flow Parameter #
|
||||
#########################################################################
|
||||
string FLOW[] = "FLOW";
|
||||
|
||||
// Initial value of variables or constant
|
||||
double initRho = 1.1405;
|
||||
double initMu = 1.7894e-5;
|
||||
double initU = 0;
|
||||
double initV = 0;
|
||||
double initW = 0;
|
||||
double initP = 0;
|
||||
|
||||
// Relaxing factor
|
||||
double urfU = 0.7;
|
||||
double urfV = 0.7;
|
||||
double urfW = 0.7;
|
||||
double urfP = 0.3;
|
||||
double urfFlux = 0.0;
|
||||
|
||||
// Tolerance for governing equations
|
||||
double resU = 1e-6;
|
||||
double resV = 1e-6;
|
||||
double resW = 1e-5;
|
||||
double resP = 1e-5;
|
||||
|
||||
// Solver for solving linear system
|
||||
// : CGS/GMRES/BiCGSTAB/AMG
|
||||
string iterSolvU = "BiCGSTAB";
|
||||
string iterSolvV = "BiCGSTAB";
|
||||
string iterSolvW = "BiCGSTAB";
|
||||
string iterSolvP = "GMRES";
|
||||
|
||||
// Max Iter for solving linear system
|
||||
int maxSweepU = 30;
|
||||
int maxSweepV = 30;
|
||||
int maxSweepW = 30;
|
||||
int maxSweepP = 30;
|
||||
|
||||
// Tolerance for solving linear system
|
||||
double iterSolvTolU = 1e-3;
|
||||
double iterSolvTolV = 1e-3;
|
||||
double iterSolvTolW = 1e-3;
|
||||
double iterSolvTolP = 1e-2;
|
||||
|
||||
// Gradient Calculation
|
||||
// : GAUSS/LSQ
|
||||
string UGradCalc = "GAUSS";
|
||||
string VGradCalc = "GAUSS";
|
||||
string WGradCalc = "GAUSS";
|
||||
string PGradCalc = "GAUSS";
|
||||
|
||||
// Convection scheme
|
||||
// : UPWIND/CDS/QUICK/SUDS
|
||||
string flowConvCalc = "UPWIND";
|
||||
|
||||
// Diffusion scheme(central difference)
|
||||
// : NON_ORTHOGONAL
|
||||
string flowDiffCalc = "NON_ORTHOGONAL";
|
||||
|
||||
// Transient scheme
|
||||
// : CRANK_NICOLSON/IMPLICIT_2ND_ORDER/IMPLICIT_EULER
|
||||
string flowTranCalc = "IMPLICIT_EULER";
|
||||
|
||||
// Source for flow
|
||||
// : FLOW_DEFAULT/FLOW_GRAVITY
|
||||
//string flowSourceCalc[] = "FLOW_DEFAULT";
|
||||
|
||||
string flowSourceCalc[] = "FLOW_DEFAULT FLOW_GRAVITY";
|
||||
int bodyForceFlag = 1;
|
||||
double gravityX = 0.0;
|
||||
double gravityY = -9.81;
|
||||
double gravityZ = 0.0;
|
||||
int isBoussinesq = 1;
|
||||
double thermalExpansion = 3.44827e-3;
|
||||
double refT = 290;
|
||||
|
||||
#########################################################################
|
||||
# Turbulence Parameter #
|
||||
#########################################################################
|
||||
//int viscousType = 13; //SPALART_ALLMARAS = 11, KEPSILON = 13
|
||||
|
||||
//turb SA
|
||||
string TURB_SA[] = ["TURB_SA"];
|
||||
string TURB_SA_SCALAR_NAME[] = ["kinetic"];
|
||||
double urfMu = 1.0;
|
||||
|
||||
double kineticInitValue = 1.0;
|
||||
string kineticConvCalc = "UPWIND";
|
||||
string kineticDiffCalc = "NON_ORTHOGONAL";
|
||||
string kineticSourceCalc[] = "TURB_SA_DEFAULT";
|
||||
double kineticUrf = 1.0;
|
||||
double kineticRes = 1e-6;
|
||||
|
||||
string turbIterSolv = "BiCGSTAB";
|
||||
int turbMaxSweep = 30;
|
||||
double turbIterSolvTol = 1e-12;
|
||||
|
||||
|
||||
//turb KEPSILON
|
||||
string TURB_K_EPSILON[] = ["TURB_K","TURB_EPSILON"];
|
||||
string TURB_K_EPSILON_SCALAR_NAME[] = ["kinetic", "epsilon"];
|
||||
|
||||
string TURB_K[] = ["TURB_K"];
|
||||
string TURB_K_SCALAR_NAME[] = ["kinetic"];
|
||||
string TURB_EPSILON[] = ["TURB_EPSILON"];
|
||||
string TURB_EPSILON_SCALAR_NAME[] = ["epsilon"];
|
||||
double urfMu = 1.0;
|
||||
|
||||
// turb k
|
||||
double kineticInitValue = 1.0;
|
||||
string kineticConvCalc = "UPWIND";
|
||||
string kineticDiffCalc = "NON_ORTHOGONAL";
|
||||
string kineticSourceCalc[] = "TURB_K_DEFAULT";
|
||||
double kineticUrf = 1.0;
|
||||
double kineticRes = 1e-6;
|
||||
|
||||
// turb epsilon
|
||||
double epsilonInitValue = 1.0;
|
||||
string epsilonConvCalc = "UPWIND";
|
||||
string epsilonDiffCalc = "NON_ORTHOGONAL";
|
||||
string epsilonSourceCalc[] = "TURB_EPSILON_DEFAULT";
|
||||
double epsilonUrf = 1.0;
|
||||
double epsilonRes = 1e-6;
|
||||
|
||||
#########################################################################
|
||||
# Energy Parameter #
|
||||
#########################################################################
|
||||
// energyType: The energy solver switch. 0-off, 1-on
|
||||
// ENERGY[]: Solver binding for factory mode.
|
||||
// ENERGY_SCALAR_NAME[]: The name of variable to be solved in energy equation.
|
||||
// energyPrintName[]: The output on the screen during the solution.
|
||||
|
||||
int energyType = 1;
|
||||
string ENERGY[] = ["ENERGY"];
|
||||
string ENERGY_SCALAR_NAME[] = "enthalpy";
|
||||
string energyPrintName[] = ["H"];
|
||||
|
||||
// Initial value of variables or constant
|
||||
double initT = 295;
|
||||
double initK = 0.0242;
|
||||
double initCPg = 1006.43;
|
||||
double urfT = 0.2;
|
||||
double urfH = 0.2;
|
||||
double enthalpyInitValue = 0.21;
|
||||
|
||||
// Discrete schemes
|
||||
string energyConvCalc = "UPWIND";
|
||||
string energyDiffCalc = "NON_ORTHOGONAL";
|
||||
string energySourceCalc[] = ["EMPTY"];
|
||||
string energyGradCalc = "GAUSS";
|
||||
string energyTranCalc = "IMPLICIT_EULER";
|
||||
|
||||
// Set for solving linear equations
|
||||
string enthalpyIterSolv = "BiCGSTAB";
|
||||
int enthalpyMaxSweep = 30;
|
||||
double enthalpyIterSolvTol = 1e-12;
|
||||
double enthalpyRes = 1e-6;
|
||||
|
|
@ -0,0 +1,30 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE.
|
||||
// 1 -- PHengLEI, *.fts.
|
||||
// 2 -- CGNS, *.cgns.
|
||||
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
|
||||
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
|
||||
// 5 -- Fluent, *.cas/*.msh.
|
||||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
int gridtype = 0;
|
||||
int axisup = 1;
|
||||
int from_gtype = 5;
|
||||
|
||||
#########################################################################
|
||||
# File path #
|
||||
#########################################################################
|
||||
// from_gfile: path of original data file for unstructure grid convert from.
|
||||
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
|
||||
string from_gfile = "./grid/run.cas";
|
||||
string out_gfile = "./grid/run.fts";
|
||||
|
|
@ -0,0 +1,52 @@
|
|||
string title = "PHengLEI Main Parameter Control File";
|
||||
|
||||
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
|
||||
string defaultParaFile = "./bin/cfd_para.hypara";
|
||||
|
||||
// ndim: Dimensional of the grid, 2 or 3.
|
||||
// nparafile: the number of parameter files.
|
||||
// nsimutask: simulation task type.
|
||||
// 0 -- CFD Solver of NS or Turbulation.
|
||||
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
|
||||
// Grid conversion: from other format to PHengLEI format (.fts).
|
||||
// Grid reconstruction: such as grid adaptation.
|
||||
// Grid merging: merge two blocks into one block.
|
||||
// Grid repairing: repair the original grid in order to remove the negative volume cells.
|
||||
// 2 -- Wall distance computation for turb-solver.
|
||||
// 3 -- Grid partition.
|
||||
int ndim = 2;
|
||||
int nparafile = 1;
|
||||
|
||||
int nsimutask = 0;
|
||||
string parafilename = "./bin/cfd_para_incompressible.hypara"
|
||||
//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";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
||||
//int nsimutask = 2;
|
||||
//string parafilename = "./bin/cfd_para.hypara";
|
||||
|
||||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 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 numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
File diff suppressed because one or more lines are too long
|
|
@ -0,0 +1,68 @@
|
|||
# nBoundaryConditions: 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 nBoundaryConditions = 4;
|
||||
string bcName = "bottom";
|
||||
{
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
string flowType = "FLOW_SOLID_SURFACE";
|
||||
}
|
||||
string bcName = "left";
|
||||
{
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
string flowType = "FLOW_SOLID_SURFACE";
|
||||
}
|
||||
string bcName = "right";
|
||||
{
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
string flowType = "FLOW_SOLID_SURFACE";
|
||||
}
|
||||
string bcName = "top";
|
||||
{
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
string flowType = "FLOW_SOLID_SURFACE";
|
||||
double flowU = 1.0;
|
||||
}
|
||||
|
||||
# 'bcType' is defined as following:
|
||||
# -2: WAKE
|
||||
# -1: INTERFACE
|
||||
# 0 : NO_BOUNDARY_CONDITION
|
||||
# 1 : EXTRAPOLATION
|
||||
# 2 : SOLID_SURFACE
|
||||
# 3 : SYMMETRY
|
||||
# 4 : FARFIELD
|
||||
# 5 : INFLOW
|
||||
# 6 : OUTFLOW
|
||||
# 52: PRESSURE_INLET
|
||||
# 62: PRESSURE_OUTLET
|
||||
# 61: OUTFLOW_CONFINED
|
||||
# 7 : POLE
|
||||
File diff suppressed because it is too large
Load Diff
|
|
@ -0,0 +1,197 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// nIsComputeWallDist: Whether to compute the wall distance.
|
||||
// 0 -- Compute wall distance.
|
||||
// 1 -- Not compute.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual 'res.dat' saved.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// compressible: An indicator that distinguishes density base from pressure base. 0-incompressible, 1-compressible
|
||||
// isUnsteady: An indicator that distinguishes unsteady problem from steady problem. 0-steady, 1-unsteady
|
||||
// startTime: The initial time of the unsteady simulation.
|
||||
// endTime: The end time of the unsteady simulation.
|
||||
// dt: The time interval of the unsteady simulation.
|
||||
// innerIter: The number of step for current time.
|
||||
// OutputTimeStep: The interval step of output for unsteady simulation.
|
||||
|
||||
int nIsComputeWallDist = 1;
|
||||
string gridfile = "./grid/cavity.fts";
|
||||
int maxSimuStep = 10000;
|
||||
int intervalStepFlow = 2000;
|
||||
int intervalStepPlot = 2000;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
int compressible = 0;
|
||||
int iunsteady = 0;
|
||||
double startTime = 0.0;
|
||||
double endTime = 30;
|
||||
double dt = 0.1;
|
||||
int innerIter = 10;
|
||||
int OutputTimeStep = 5;
|
||||
|
||||
#########################################################################
|
||||
# Post-Processing #
|
||||
#########################################################################
|
||||
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
|
||||
// visualVariables : Variable types dumped, listed as following:
|
||||
// -- U(22), V(23), W(24), P(25), CP(26), T(27), DEN(28), VIS(29), TE(31), ED(32), enthalpy(70)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
||||
int nVisualVariables = 4;
|
||||
int visualVariables[] = [22, 23, 24, 25];
|
||||
#########################################################################
|
||||
# Flow Parameter #
|
||||
#########################################################################
|
||||
string FLOW[] = "FLOW";
|
||||
|
||||
// Initial value of variables or constant
|
||||
double initRho = 1.0;
|
||||
double initMu = 0.001;
|
||||
double initU = 0;
|
||||
double initV = 0;
|
||||
double initW = 0;
|
||||
double initP = 0;
|
||||
|
||||
// Relaxing factor
|
||||
double urfU = 0.4;
|
||||
double urfV = 0.4;
|
||||
double urfW = 0.4;
|
||||
double urfP = 0.7;
|
||||
double urfFlux = 0.4;
|
||||
|
||||
// Tolerance for governing equations
|
||||
double resU = 1e-6;
|
||||
double resV = 1e-6;
|
||||
double resW = 1e-5;
|
||||
double resP = 1e-5;
|
||||
|
||||
// Solver for solving linear system
|
||||
// : CGS/GMRES/BiCGSTAB/AMG
|
||||
string iterSolvU = "BiCGSTAB";
|
||||
string iterSolvV = "BiCGSTAB";
|
||||
string iterSolvW = "BiCGSTAB";
|
||||
string iterSolvP = "GMRES";
|
||||
|
||||
// Max Iter for solving linear system
|
||||
int maxSweepU = 30;
|
||||
int maxSweepV = 30;
|
||||
int maxSweepW = 30;
|
||||
int maxSweepP = 30;
|
||||
|
||||
// Tolerance for solving linear system
|
||||
double iterSolvTolU = 1e-3;
|
||||
double iterSolvTolV = 1e-3;
|
||||
double iterSolvTolW = 1e-3;
|
||||
double iterSolvTolP = 1e-2;
|
||||
|
||||
// Gradient Calculation
|
||||
// : GAUSS/LSQ
|
||||
string UGradCalc = "GAUSS";
|
||||
string VGradCalc = "GAUSS";
|
||||
string WGradCalc = "GAUSS";
|
||||
string PGradCalc = "GAUSS";
|
||||
|
||||
// Convection scheme
|
||||
// : UPWIND/CDS/QUICK/SUDS
|
||||
string flowConvCalc = "UPWIND";
|
||||
|
||||
// Diffusion scheme(central difference)
|
||||
// : NON_ORTHOGONAL
|
||||
string flowDiffCalc = "NON_ORTHOGONAL";
|
||||
|
||||
// Transient scheme
|
||||
// : CRANK_NICOLSON/IMPLICIT_2ND_ORDER/IMPLICIT_EULER
|
||||
string flowTranCalc = "IMPLICIT_EULER";
|
||||
|
||||
// Source for flow
|
||||
// : FLOW_DEFAULT/FLOW_GRAVITY
|
||||
string flowSourceCalc[] = "FLOW_DEFAULT";
|
||||
|
||||
// string flowSourceCalc[] = "FLOW_DEFAULT FLOW_GRAVITY";
|
||||
int bodyForceFlag = 0;
|
||||
int isBoussinesq = 0;
|
||||
//double gravityX = 0.0;
|
||||
//double gravityY = -9.81;
|
||||
//double gravityZ = 0.0;
|
||||
|
||||
#########################################################################
|
||||
# Turbulence Parameter #
|
||||
#########################################################################
|
||||
// turb K-EPSILON
|
||||
//int viscousType = 13; //SPALART_ALLMARAS = 11, KEPSILON = 13
|
||||
string TURB_K_EPSILON[] = ["TURB_K","TURB_EPSILON"];
|
||||
string TURB_K_EPSILON_SCALAR_NAME[] = ["kinetic", "epsilon"];
|
||||
|
||||
string turbIterSolv = "BiCGSTAB";
|
||||
int turbMaxSweep = 30;
|
||||
double turbIterSolvTol = 1e-12;
|
||||
|
||||
string TURB_K[] = ["TURB_K"];
|
||||
string TURB_K_SCALAR_NAME[] = ["kinetic"];
|
||||
string TURB_EPSILON[] = ["TURB_EPSILON"];
|
||||
string TURB_EPSILON_SCALAR_NAME[] = ["epsilon"];
|
||||
double urfMu = 1.0;
|
||||
|
||||
// turb k
|
||||
double kineticInitValue = 1.0;
|
||||
string kineticConvCalc = "UPWIND";
|
||||
string kineticDiffCalc = "NON_ORTHOGONAL";
|
||||
string kineticSourceCalc[] = "TURB_K_DEFAULT";
|
||||
double kineticUrf = 1.0;
|
||||
double kineticRes = 1e-6;
|
||||
|
||||
// turb epsilon
|
||||
double epsilonInitValue = 1.0;
|
||||
string epsilonConvCalc = "UPWIND";
|
||||
string epsilonDiffCalc = "NON_ORTHOGONAL";
|
||||
string epsilonSourceCalc[] = "TURB_EPSILON_DEFAULT";
|
||||
double epsilonUrf = 1.0;
|
||||
double epsilonRes = 1e-6;
|
||||
|
||||
#########################################################################
|
||||
# Energy Parameter #
|
||||
#########################################################################
|
||||
// energyType: The energy solver switch. 0-off, 1-on
|
||||
// ENERGY[]: Solver binding for factory mode.
|
||||
// ENERGY_SCALAR_NAME[]: The name of variable to be solved in energy equation.
|
||||
// energyPrintName[]: The output on the screen during the solution.
|
||||
|
||||
int energyType = 0;
|
||||
string ENERGY[] = ["ENERGY"];
|
||||
string ENERGY_SCALAR_NAME[] = "enthalpy";
|
||||
string energyPrintName[] = ["H"];
|
||||
|
||||
// Initial value of variables or constant
|
||||
double initT = 273.0;
|
||||
double initK = 0.026;
|
||||
double initCPg = 1007.0;
|
||||
double urfT = 0.8;
|
||||
double urfH = 0.7;
|
||||
double enthalpyInitValue = 0.21;
|
||||
|
||||
// Discrete schemes
|
||||
string energyConvCalc = "UPWIND";
|
||||
string energyDiffCalc = "NON_ORTHOGONAL";
|
||||
string energySourceCalc[] = ["EMPTY"];
|
||||
string energyGradCalc = "GAUSS";
|
||||
string energyTranCalc = "IMPLICIT_EULER";
|
||||
|
||||
// Set for solving linear equations
|
||||
string enthalpyIterSolv = "BiCGSTAB";
|
||||
int enthalpyMaxSweep = 30;
|
||||
double enthalpyIterSolvTol = 1e-12;
|
||||
double enthalpyRes = 1e-6;
|
||||
|
|
@ -0,0 +1,30 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE.
|
||||
// 1 -- PHengLEI, *.fts.
|
||||
// 2 -- CGNS, *.cgns.
|
||||
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
|
||||
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
|
||||
// 5 -- Fluent, *.cas/*.msh.
|
||||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
int gridtype = 0;
|
||||
int axisup = 1;
|
||||
int from_gtype = 5;
|
||||
|
||||
#########################################################################
|
||||
# File path #
|
||||
#########################################################################
|
||||
// from_gfile: path of original data file for unstructure grid convert from.
|
||||
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
|
||||
string from_gfile = "./grid/cavity.cas";
|
||||
string out_gfile = "./grid/cavity.fts";
|
||||
|
|
@ -0,0 +1,52 @@
|
|||
string title = "PHengLEI Main Parameter Control File";
|
||||
|
||||
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
|
||||
string defaultParaFile = "./bin/cfd_para.hypara";
|
||||
|
||||
// ndim: Dimensional of the grid, 2 or 3.
|
||||
// nparafile: the number of parameter files.
|
||||
// nsimutask: simulation task type.
|
||||
// 0 -- CFD Solver of NS or Turbulation.
|
||||
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
|
||||
// Grid conversion: from other format to PHengLEI format (.fts).
|
||||
// Grid reconstruction: such as grid adaptation.
|
||||
// Grid merging: merge two blocks into one block.
|
||||
// Grid repairing: repair the original grid in order to remove the negative volume cells.
|
||||
// 2 -- Wall distance computation for turb-solver.
|
||||
// 3 -- Grid partition.
|
||||
int ndim = 2;
|
||||
int nparafile = 1;
|
||||
|
||||
int nsimutask = 0;
|
||||
string parafilename = "./bin/cfd_para_incompressible.hypara"
|
||||
//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";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
||||
//int nsimutask = 2;
|
||||
//string parafilename = "./bin/cfd_para.hypara";
|
||||
|
||||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 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 numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
File diff suppressed because one or more lines are too long
|
|
@ -0,0 +1,71 @@
|
|||
# nBoundaryConditions: 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 nBoundaryConditions = 3;
|
||||
string bcName = "in";
|
||||
{
|
||||
int bcType = 5;
|
||||
string flowType = "FLOW_VELOCITY_INLET";
|
||||
string kineticBoundaryType = "TURB_K_INLET";
|
||||
string epsilonBoundaryType = "TURB_EPSILON_INLET";
|
||||
double flowW = 50;
|
||||
double kinetic = 9.375004;
|
||||
double epsilon = 54151.86;
|
||||
}
|
||||
string bcName = "out";
|
||||
{
|
||||
int bcType = 6;
|
||||
string flowType = "FLOW_PRESSURE_OUTLET";
|
||||
string kineticBoundaryType = "TURB_K_PRESSUREOUTLET";
|
||||
string epsilonBoundaryType = "TURB_EPSILON_PRESSUREOUTLET";
|
||||
double flowP = 0;
|
||||
double kinetic = 9.375004;
|
||||
double epsilon = 54151.86;
|
||||
}
|
||||
string bcName = "wall";
|
||||
{
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
string flowType = "FLOW_SOLID_SURFACE";
|
||||
string kineticBoundaryType = "TURB_K_WALL";
|
||||
string epsilonBoundaryType = "TURB_EPSILON_WALL";
|
||||
}
|
||||
|
||||
# 'bcType' is defined as following:
|
||||
# -2: WAKE
|
||||
# -1: INTERFACE
|
||||
# 0 : NO_BOUNDARY_CONDITION
|
||||
# 1 : EXTRAPOLATION
|
||||
# 2 : SOLID_SURFACE
|
||||
# 3 : SYMMETRY
|
||||
# 4 : FARFIELD
|
||||
# 5 : INFLOW
|
||||
# 6 : OUTFLOW
|
||||
# 52: PRESSURE_INLET
|
||||
# 62: PRESSURE_OUTLET
|
||||
# 61: OUTFLOW_CONFINED
|
||||
# 7 : POLE
|
||||
File diff suppressed because it is too large
Load Diff
|
|
@ -0,0 +1,202 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// nIsComputeWallDist: Whether to compute the wall distance.
|
||||
// 0 -- Compute wall distance.
|
||||
// 1 -- Not compute.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual 'res.dat' saved.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// compressible: An indicator that distinguishes density base from pressure base. 0-incompressible, 1-compressible
|
||||
// isUnsteady: An indicator that distinguishes unsteady problem from steady problem. 0-steady, 1-unsteady
|
||||
// startTime: The initial time of the unsteady simulation.
|
||||
// endTime: The end time of the unsteady simulation.
|
||||
// dt: The time interval of the unsteady simulation.
|
||||
// innerIter: The number of step for current time.
|
||||
// OutputTimeStep: The interval step of output for unsteady simulation.
|
||||
|
||||
int nIsComputeWallDist = 1;
|
||||
string gridfile = "./grid/pipe.fts";
|
||||
int maxSimuStep = 10000;
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepRes = 1000;
|
||||
|
||||
double gridScaleFactor = 1;
|
||||
|
||||
int compressible = 0;
|
||||
int iunsteady = 0;
|
||||
double startTime = 0.0;
|
||||
double endTime = 5;
|
||||
double dt = 0.1;
|
||||
int innerIter = 10;
|
||||
int OutputTimeStep = 5;
|
||||
|
||||
#########################################################################
|
||||
# Post-Processing #
|
||||
#########################################################################
|
||||
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
|
||||
// visualVariables : Variable types dumped, listed as following:
|
||||
// -- U(22), V(23), W(24), P(25), CP(26), T(27), DEN(28), VIS(29), TE(31), ED(32), enthalpy(57)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
// plotFieldType: If dump out the field results to visulization.
|
||||
|
||||
int plotFieldType = 1;
|
||||
//int nVisualVariables = 4;
|
||||
//int visualVariables[] = [22, 23, 24, 25];
|
||||
|
||||
int nVisualVariables = 7;
|
||||
int visualVariables[] = [22, 23, 24, 25, 29,31,32];
|
||||
#########################################################################
|
||||
# Flow Parameter #
|
||||
#########################################################################
|
||||
string FLOW[] = "FLOW";
|
||||
|
||||
// Initial value of variables or constant
|
||||
double initRho = 1.225;
|
||||
double initMu = 1.7894e-05;
|
||||
double initU = 0;
|
||||
double initV = 0;
|
||||
double initW = 50;
|
||||
double initP = 0;
|
||||
|
||||
// Relaxing factor
|
||||
double urfU = 0.4;
|
||||
double urfV = 0.4;
|
||||
double urfW = 0.4;
|
||||
double urfP = 0.3;
|
||||
double urfFlux = 0.4;
|
||||
|
||||
// Tolerance for governing equations
|
||||
double resU = 1e-6;
|
||||
double resV = 1e-6;
|
||||
double resW = 1e-5;
|
||||
double resP = 1e-5;
|
||||
|
||||
// Solver for solving linear system
|
||||
// : CGS/GMRES/BiCGSTAB/AMG
|
||||
string iterSolvU = "BiCGSTAB";
|
||||
string iterSolvV = "BiCGSTAB";
|
||||
string iterSolvW = "BiCGSTAB";
|
||||
string iterSolvP = "AMG";
|
||||
|
||||
// Max Iter for solving linear system
|
||||
int maxSweepU = 30;
|
||||
int maxSweepV = 30;
|
||||
int maxSweepW = 30;
|
||||
int maxSweepP = 30;
|
||||
|
||||
// Tolerance for solving linear system
|
||||
double iterSolvTolU = 1e-4;
|
||||
double iterSolvTolV = 1e-4;
|
||||
double iterSolvTolW = 1e-4;
|
||||
double iterSolvTolP = 1e-3;
|
||||
|
||||
// Gradient Calculation
|
||||
// : GAUSS/LSQ
|
||||
string UGradCalc = "GAUSS";
|
||||
string VGradCalc = "GAUSS";
|
||||
string WGradCalc = "GAUSS";
|
||||
string PGradCalc = "GAUSS";
|
||||
|
||||
// Convection scheme
|
||||
// : UPWIND/CDS/QUICK/SUDS
|
||||
string flowConvCalc = "UPWIND";
|
||||
|
||||
// Diffusion scheme(central difference)
|
||||
// : NON_ORTHOGONAL
|
||||
string flowDiffCalc = "NON_ORTHOGONAL";
|
||||
|
||||
// Transient scheme
|
||||
// : CRANK_NICOLSON/IMPLICIT_2ND_ORDER/IMPLICIT_EULER
|
||||
string flowTranCalc = "IMPLICIT_EULER";
|
||||
|
||||
// Source for flow
|
||||
// : FLOW_DEFAULT/FLOW_GRAVITY
|
||||
string flowSourceCalc[] = "FLOW_DEFAULT";
|
||||
|
||||
//string flowSourceCalc[] = "FLOW_DEFAULT FLOW_GRAVITY";
|
||||
int bodyForceFlag = 0;
|
||||
double gravityX = 0.0;
|
||||
double gravityY = -9.81;
|
||||
double gravityZ = 0.0;
|
||||
|
||||
#########################################################################
|
||||
# Turbulence Parameter #
|
||||
#########################################################################
|
||||
int viscousType = 13; //SPALART_ALLMARAS = 11, KEPSILON = 13
|
||||
|
||||
//turb K-EPSILON
|
||||
string TURB_K_EPSILON[] = ["TURB_K","TURB_EPSILON"];
|
||||
string TURB_K_EPSILON_SCALAR_NAME[] = ["kinetic", "epsilon"];
|
||||
|
||||
string TURB_K[] = ["TURB_K"];
|
||||
string TURB_K_SCALAR_NAME[] = ["kinetic"];
|
||||
string TURB_EPSILON[] = ["TURB_EPSILON"];
|
||||
string TURB_EPSILON_SCALAR_NAME[] = ["epsilon"];
|
||||
double urfMu = 0.6;
|
||||
|
||||
string turbIterSolv = "BiCGSTAB";
|
||||
int turbMaxSweep = 30;
|
||||
double turbIterSolvTol = 1e-12;
|
||||
|
||||
// turb k
|
||||
double kineticInitValue = 9.375001;
|
||||
string kineticConvCalc = "UPWIND";
|
||||
string kineticDiffCalc = "NON_ORTHOGONAL";
|
||||
string kineticSourceCalc[] = "TURB_K_DEFAULT";
|
||||
double kineticUrf = 0.6;
|
||||
double kineticRes = 1e-6;
|
||||
|
||||
|
||||
// turb epsilon
|
||||
double epsilonInitValue = 54151.86;
|
||||
string epsilonConvCalc = "UPWIND";
|
||||
string epsilonDiffCalc = "NON_ORTHOGONAL";
|
||||
string epsilonSourceCalc[] = "TURB_EPSILON_DEFAULT";
|
||||
double epsilonUrf = 0.6;
|
||||
double epsilonRes = 1e-6;
|
||||
|
||||
#########################################################################
|
||||
# Energy Parameter #
|
||||
#########################################################################
|
||||
// energyType: The energy solver switch. 0-off, 1-on
|
||||
// ENERGY[]: Solver binding for factory mode.
|
||||
// ENERGY_SCALAR_NAME[]: The name of variable to be solved in energy equation.
|
||||
// energyPrintName[]: The output on the screen during the solution.
|
||||
int energyType = 0;
|
||||
string ENERGY[] = ["ENERGY"];
|
||||
string ENERGY_SCALAR_NAME[] = "enthalpy";
|
||||
string energyPrintName[] = ["H"];
|
||||
|
||||
// Initial value of variables or constant
|
||||
double initT = 273.0;
|
||||
double initK = 0.026;
|
||||
double initCPg = 1007.0;
|
||||
double urfT = 0.8;
|
||||
double urfH = 0.7;
|
||||
double enthalpyInitValue = 0.21;
|
||||
|
||||
// Discrete schemes
|
||||
string energyConvCalc = "UPWIND";
|
||||
string energyDiffCalc = "NON_ORTHOGONAL";
|
||||
string energySourceCalc[] = ["EMPTY"];
|
||||
string energyGradCalc = "GAUSS";
|
||||
string energyTranCalc = "IMPLICIT_EULER";
|
||||
|
||||
// Set for solving linear equations
|
||||
string enthalpyIterSolv = "BiCGSTAB";
|
||||
int enthalpyMaxSweep = 30;
|
||||
double enthalpyIterSolvTol = 1e-12;
|
||||
double enthalpyRes = 1e-6;
|
||||
|
|
@ -0,0 +1,30 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE.
|
||||
// 1 -- PHengLEI, *.fts.
|
||||
// 2 -- CGNS, *.cgns.
|
||||
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
|
||||
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
|
||||
// 5 -- Fluent, *.cas/*.msh.
|
||||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
int gridtype = 0;
|
||||
int axisup = 1;
|
||||
int from_gtype = 5;
|
||||
|
||||
#########################################################################
|
||||
# File path #
|
||||
#########################################################################
|
||||
// from_gfile: path of original data file for unstructure grid convert from.
|
||||
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
|
||||
string from_gfile = "./grid/pipe.cas";
|
||||
string out_gfile = "./grid/pipe.fts";
|
||||
|
|
@ -0,0 +1,52 @@
|
|||
string title = "PHengLEI Main Parameter Control File";
|
||||
|
||||
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
|
||||
string defaultParaFile = "./bin/cfd_para.hypara";
|
||||
|
||||
// ndim: Dimensional of the grid, 2 or 3.
|
||||
// nparafile: the number of parameter files.
|
||||
// nsimutask: simulation task type.
|
||||
// 0 -- CFD Solver of NS or Turbulation.
|
||||
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
|
||||
// Grid conversion: from other format to PHengLEI format (.fts).
|
||||
// Grid reconstruction: such as grid adaptation.
|
||||
// Grid merging: merge two blocks into one block.
|
||||
// Grid repairing: repair the original grid in order to remove the negative volume cells.
|
||||
// 2 -- Wall distance computation for turb-solver.
|
||||
// 3 -- Grid partition.
|
||||
int ndim = 3;
|
||||
int nparafile = 1;
|
||||
|
||||
int nsimutask = 0;
|
||||
string parafilename = "./bin/cfd_para_incompressible.hypara"
|
||||
//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";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
||||
//int nsimutask = 2;
|
||||
//string parafilename = "./bin/cfd_para.hypara";
|
||||
|
||||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 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 numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
File diff suppressed because one or more lines are too long
|
|
@ -0,0 +1,63 @@
|
|||
# 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 nBoundaryConditions = 5;
|
||||
string bcName = "sym";
|
||||
{
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
string flowType = "FLOW_SOLID_SURFACE";
|
||||
}
|
||||
string bcName = "symf";
|
||||
{
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
string flowType = "FLOW_SOLID_SURFACE";
|
||||
}
|
||||
string bcName = "wall";
|
||||
{
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
string flowType = "FLOW_SOLID_SURFACE";
|
||||
}
|
||||
string bcName = "in";
|
||||
{
|
||||
int bcType = 5;
|
||||
string flowType = "FLOW_VELOCITY_INLET";
|
||||
double flowU =0.1;
|
||||
}
|
||||
string bcName = "out";
|
||||
{
|
||||
int bcType = 6;
|
||||
string flowType = "FLOW_PRESSURE_OUTLET";
|
||||
double flowU =0.1;
|
||||
double flowP =0;
|
||||
}
|
||||
|
||||
# 'bcType' is defined as following:
|
||||
# 99: PERIODIC
|
||||
# -2: WAKE
|
||||
# -1: INTERFACE
|
||||
# 0 : NO_BOUNDARY_CONDITION
|
||||
# 1 : EXTRAPOLATION
|
||||
# 2 : SOLID_SURFACE
|
||||
# 3 : SYMMETRY
|
||||
# 4 : FARFIELD
|
||||
# 5 : INFLOW
|
||||
# 6 : OUTFLOW
|
||||
# 52: PRESSURE_INLET
|
||||
# 62: PRESSURE_OUTLET
|
||||
# 61: OUTFLOW_CONFINED
|
||||
# 7 : POLE
|
||||
File diff suppressed because it is too large
Load Diff
|
|
@ -0,0 +1,212 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// nIsComputeWallDist: Whether to compute the wall distance.
|
||||
// 0 -- Compute wall distance.
|
||||
// 1 -- Not compute.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual 'res.dat' saved.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// compressible: An indicator that distinguishes density base from pressure base. 0-incompressible, 1-compressible
|
||||
// isUnsteady: An indicator that distinguishes unsteady problem from steady problem. 0-steady, 1-unsteady
|
||||
// startTime: The initial time of the unsteady simulation.
|
||||
// endTime: The end time of the unsteady simulation.
|
||||
// dt: The time interval of the unsteady simulation.
|
||||
// innerIter: The number of step for current time.
|
||||
// OutputTimeStep: The interval step of output for unsteady simulation.
|
||||
|
||||
int nIsComputeWallDist = 1;
|
||||
string gridfile = "./grid/suboff.fts";
|
||||
iint maxSimuStep = 10000;
|
||||
int intervalStepFlow = 2000;
|
||||
int intervalStepPlot = 2000;
|
||||
int intervalStepRes = 2000;
|
||||
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
int compressible = 0;
|
||||
int iunsteady = 0;
|
||||
double startTime = 0.0;
|
||||
double endTime = 5;
|
||||
double dt = 0.1;
|
||||
int innerIter = 10;
|
||||
int OutputTimeStep = 5;
|
||||
|
||||
#########################################################################
|
||||
# Post-Processing #
|
||||
#########################################################################
|
||||
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
|
||||
// visualVariables : Variable types dumped, listed as following:
|
||||
// -- U(22), V(23), W(24), P(25), CP(26), T(27), DEN(28), VIS(29), TE(31), ED(32), enthalpy(57)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
// plotFieldType: If dump out the field results to visulization.
|
||||
|
||||
int plotFieldType = 1;
|
||||
int nVisualVariables = 4;
|
||||
int visualVariables[] = [22, 23, 24, 25];
|
||||
|
||||
#########################################################################
|
||||
# Flow Parameter #
|
||||
#########################################################################
|
||||
string FLOW[] = "FLOW";
|
||||
|
||||
// Initial value of variables or constant
|
||||
double initRho = 998.3;
|
||||
double initMu = 1.93345725;
|
||||
double initU = 0.1;
|
||||
double initV = 0;
|
||||
double initW = 0;
|
||||
double initP = 0;
|
||||
|
||||
// Relaxing factor
|
||||
double urfU = 0.4;
|
||||
double urfV = 0.4;
|
||||
double urfW = 0.4;
|
||||
double urfP = 0.3;
|
||||
double urfFlux = 0.4;
|
||||
|
||||
// Tolerance for governing equations
|
||||
double resU = 1e-6;
|
||||
double resV = 1e-6;
|
||||
double resW = 1e-5;
|
||||
double resP = 1e-5;
|
||||
|
||||
// Solver for solving linear system
|
||||
// : CGS/GMRES/BiCGSTAB/AMG
|
||||
string iterSolvU = "BiCGSTAB";
|
||||
string iterSolvV = "BiCGSTAB";
|
||||
string iterSolvW = "BiCGSTAB";
|
||||
string iterSolvP = "GMRES";
|
||||
|
||||
// Max Iter for solving linear system
|
||||
int maxSweepU = 30;
|
||||
int maxSweepV = 30;
|
||||
int maxSweepW = 30;
|
||||
int maxSweepP = 30;
|
||||
|
||||
// Tolerance for solving linear system
|
||||
double iterSolvTolU = 1e-4;
|
||||
double iterSolvTolV = 1e-4;
|
||||
double iterSolvTolW = 1e-4;
|
||||
double iterSolvTolP = 1e-3;
|
||||
|
||||
// Gradient Calculation
|
||||
// : GAUSS/LSQ
|
||||
string UGradCalc = "GAUSS";
|
||||
string VGradCalc = "GAUSS";
|
||||
string WGradCalc = "GAUSS";
|
||||
string PGradCalc = "GAUSS";
|
||||
|
||||
// Convection scheme
|
||||
// : UPWIND/CDS/QUICK/SUDS
|
||||
string flowConvCalc = "QUICK";
|
||||
|
||||
// Diffusion scheme(central difference)
|
||||
// : NON_ORTHOGONAL
|
||||
string flowDiffCalc = "NON_ORTHOGONAL";
|
||||
|
||||
// Transient scheme
|
||||
// : CRANK_NICOLSON/IMPLICIT_2ND_ORDER/IMPLICIT_EULER
|
||||
string flowTranCalc = "IMPLICIT_EULER";
|
||||
|
||||
// Source for flow
|
||||
// : FLOW_DEFAULT/FLOW_GRAVITY
|
||||
string flowSourceCalc[] = "FLOW_DEFAULT";
|
||||
|
||||
//string flowSourceCalc[] = "FLOW_DEFAULT FLOW_GRAVITY";
|
||||
int bodyForceFlag = 0;
|
||||
//double gravityX = 0.0;
|
||||
//double gravityY = -9.81;
|
||||
//double gravityZ = 0.0;
|
||||
|
||||
#########################################################################
|
||||
# Turbulence Parameter #
|
||||
#########################################################################
|
||||
//int viscousType = 13; //SPALART_ALLMARAS = 11, KEPSILON = 13
|
||||
|
||||
//turb SA
|
||||
//string TURB_SA[] = ["TURB_SA"];
|
||||
//string TURB_SA_SCALAR_NAME[] = ["kinetic"];
|
||||
//double urfMu = 1.0;
|
||||
|
||||
//double kineticInitValue = 1.0;
|
||||
//string kineticConvCalc = "UPWIND";
|
||||
//string kineticDiffCalc = "NON_ORTHOGONAL";
|
||||
//string kineticSourceCalc[] = "TURB_SA_DEFAULT";
|
||||
//double kineticUrf = 1.0
|
||||
//double kineticRes = 1e-6;
|
||||
|
||||
//string turbIterSolv = "BiCGSTAB";
|
||||
//int turbMaxSweep = 30;
|
||||
//double turbIterSolvTol = 1e-12;
|
||||
|
||||
|
||||
//turb K-EPSILON
|
||||
string TURB_K_EPSILON[] = ["TURB_K","TURB_EPSILON"];
|
||||
string TURB_K_EPSILON_SCALAR_NAME[] = ["kinetic", "epsilon"];
|
||||
|
||||
string TURB_K[] = ["TURB_K"];
|
||||
string TURB_K_SCALAR_NAME[] = ["kinetic"];
|
||||
string TURB_EPSILON[] = ["TURB_EPSILON"];
|
||||
string TURB_EPSILON_SCALAR_NAME[] = ["epsilon"];
|
||||
double urfMu = 0.4;
|
||||
|
||||
// turb k
|
||||
double kineticInitValue = 3.750003e-05;
|
||||
string kineticConvCalc = "UPWIND";
|
||||
string kineticDiffCalc = "NON_ORTHOGONAL";
|
||||
string kineticSourceCalc[] = "TURB_K_DEFAULT";
|
||||
double kineticUrf = 0.4;
|
||||
double kineticRes = 1e-6;
|
||||
|
||||
// turb epsilon
|
||||
double epsilonInitValue = 8.664311e-07;
|
||||
string epsilonConvCalc = "UPWIND";
|
||||
string epsilonDiffCalc = "NON_ORTHOGONAL";
|
||||
string epsilonSourceCalc[] = "TURB_EPSILON_DEFAULT";
|
||||
double epsilonUrf = 0.4;
|
||||
double epsilonRes = 1e-6;
|
||||
|
||||
#########################################################################
|
||||
# Energy Parameter #
|
||||
#########################################################################
|
||||
// energyType: The energy solver switch. 0-off, 1-on
|
||||
// ENERGY[]: Solver binding for factory mode.
|
||||
// ENERGY_SCALAR_NAME[]: The name of variable to be solved in energy equation.
|
||||
// energyPrintName[]: The output on the screen during the solution.
|
||||
int energyType = 0;
|
||||
string ENERGY[] = ["ENERGY"];
|
||||
string ENERGY_SCALAR_NAME[] = "enthalpy";
|
||||
string energyPrintName[] = ["H"];
|
||||
|
||||
// Initial value of variables or constant
|
||||
double initT = 273.0;
|
||||
double initK = 0.026;
|
||||
double initCPg = 1007.0;
|
||||
double urfT = 0.8;
|
||||
double urfH = 0.7;
|
||||
double enthalpyInitValue = 0.21;
|
||||
|
||||
// Discrete schemes
|
||||
string energyConvCalc = "UPWIND";
|
||||
string energyDiffCalc = "NON_ORTHOGONAL";
|
||||
string energySourceCalc[] = ["EMPTY"];
|
||||
string energyGradCalc = "GAUSS";
|
||||
string energyTranCalc = "IMPLICIT_EULER";
|
||||
|
||||
// Set for solving linear equations
|
||||
string enthalpyIterSolv = "BiCGSTAB";
|
||||
int enthalpyMaxSweep = 30;
|
||||
double enthalpyIterSolvTol = 1e-12;
|
||||
double enthalpyRes = 1e-6;
|
||||
|
|
@ -0,0 +1,30 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE.
|
||||
// 1 -- PHengLEI, *.fts.
|
||||
// 2 -- CGNS, *.cgns.
|
||||
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
|
||||
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
|
||||
// 5 -- Fluent, *.cas/*.msh.
|
||||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
int gridtype = 0;
|
||||
int axisup = 1;
|
||||
int from_gtype = 5;
|
||||
|
||||
#########################################################################
|
||||
# File path #
|
||||
#########################################################################
|
||||
// from_gfile: path of original data file for unstructure grid convert from.
|
||||
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
|
||||
string from_gfile = "./grid/suboff.cas";
|
||||
string out_gfile = "./grid/suboff.fts";
|
||||
|
|
@ -0,0 +1,52 @@
|
|||
string title = "PHengLEI Main Parameter Control File";
|
||||
|
||||
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
|
||||
string defaultParaFile = "./bin/cfd_para.hypara";
|
||||
|
||||
// ndim: Dimensional of the grid, 2 or 3.
|
||||
// nparafile: the number of parameter files.
|
||||
// nsimutask: simulation task type.
|
||||
// 0 -- CFD Solver of NS or Turbulation.
|
||||
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
|
||||
// Grid conversion: from other format to PHengLEI format (.fts).
|
||||
// Grid reconstruction: such as grid adaptation.
|
||||
// Grid merging: merge two blocks into one block.
|
||||
// Grid repairing: repair the original grid in order to remove the negative volume cells.
|
||||
// 2 -- Wall distance computation for turb-solver.
|
||||
// 3 -- Grid partition.
|
||||
int ndim = 3;
|
||||
int nparafile = 1;
|
||||
|
||||
int nsimutask = 0;
|
||||
string parafilename = "./bin/cfd_para_incompressible.hypara"
|
||||
//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";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
||||
//int nsimutask = 2;
|
||||
//string parafilename = "./bin/cfd_para.hypara";
|
||||
|
||||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 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 numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
File diff suppressed because one or more lines are too long
|
|
@ -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";
|
||||
|
|
|
|||
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Reference in New Issue