diff --git a/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/boundary_condition.hypara b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/boundary_condition.hypara new file mode 100644 index 0000000..3b2728f --- /dev/null +++ b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/boundary_condition.hypara @@ -0,0 +1,65 @@ +# 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 diff --git a/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/cfd_para.hypara b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/cfd_para.hypara new file mode 100644 index 0000000..df090b7 --- /dev/null +++ b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/cfd_para.hypara @@ -0,0 +1,923 @@ +//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ +// PPPPP H H EEEEE N N GGGGG L EEEEE III + +// P P H H E NN N G L E I + +// PPPPP HHHHH EEEEE N N N G GG L EEEEE I + +// P H H E N N N G G L E I + +// P H H EEEEE N N GGGGG LLLLL EEEEE III + +//------------------------------------------------------------------------+ +// Platform for Hybrid Engineering Simulation of Flows + +// China Aerodynamics Research and Development Center + +// (C) Copyright, Since 2010 + +//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ +########################################################################### +# Default parameters for Grid conversion # +########################################################################### +// gridtype: Grid type for generation, conversion, reconstruction, merging. +// 0 -- Unstructured grid. +// 1 -- Structured grid. +// 2 -- Hybrid grid, include both of unstructured and structured grid. +// gridobj: Task type of grid treatment. +// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc. +// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS. +// 2 -- Grid refinement. +// 3 -- Grid merging, merge two blocks into one block. +// 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. +// multiblock: Multi-block grid or not, only for structured grid conversion. +// 0 -- Not. +// 1 -- Yes. +// iadapt: Adaptation number for unstructure grid. +// SymmetryFaceVector: The vector of symmetry face. +// 0 -- X axis. +// 1 -- Y axis. +// 2 -- Z axis. +int gridtype = 0; +int gridobj = 1; +int multiblock = 0; +int iadapt = 0; +int SymmetryFaceVector = 1; + +// axisup: Type of Cartisien coordinates system, used in grid conversion. +// 1 -- Y upward. (default) +// 2 -- Z upward. +int axisup = 1; + +// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition". +// 0 -- Interface. (default) +// 1 -- Physical boundary condition, used in Hybrid solver. +int omit_no_bound_bc = 0; + +//----------------------------------------------------------------------- +# Grid data type # +//----------------------------------------------------------------------- +// from_gtype/to_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. +// dumpOldGrid: If dump out the old grid file. +// 0 -- Not. (default) +// 1 -- Yes. +int from_gtype = 2; +int to_gtype = 1; +int dumpOldGrid = 0; + +//----------------------------------------------------------------------- +# 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/rae2822_hybrid2d.cas"; +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 iale = 0; +int codeOfAleModel = 0; + +// fileformat: Ustar Grid file format. +// 0 -- BINARY. +// 1 -- ASCII. +int fileformat = 0; + +// Parameters for hybrid solver. +// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type. +// mixgrid_str: path of structure grid file for hybrid solver, *.fts type. +string mixgrid_uns = "./grid/rae2822_uns2d_4.fts"; +string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts"; + +// Some parameters for structured overlapping grid. +int codeOfDigHoles = 1; +string holeBasicFileName = "./oversetGridView/holeBasicFile.inp"; +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"; + +// geometryUnit: Geometry unit. +// 1 -- meter. +// 2 -- millimeter. +// 3 -- inch. +// exclusiveCase: Parallel projection exclusive case. +// 0 -- NON case. +// 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 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. + +// ----------------- RBF Parameters ------------------------------------- +// symmetryPlane: Which symmetry plane is used in the mesh. +// 0 -- without symmetry. +// 1 -- plane of x=0. +// 2 -- plane of y=0. +// 3 -- plane of z=0. +int numberOfReferenceCP = 10; +double influenceRadius = 20; +int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; + +// ----------------- Periodic Parameters -------------------------------- +// Notice: Rotational periodicity only support rotation along the X axis! +// periodicType: Which periodic boundary is used. +// 0 -- without Periodic Boundary. +// 1 -- Translational periodicity. +// 2 -- Rotational periodicity. +int periodicType = 0; +double translationLength[] = [0.0,0.0,0.0]; +double rotationAngle = 0.0; + +######################################################################### +# Default parameters for Partition # +######################################################################### +// pgridtype: The grid type. +// 0 -- unstruct grid. +// 1 -- struct grid. +// 2 -- refine structured grid. +// maxproc: The number of partition zones that want to be divided into. +int pgridtype = 0; +int maxproc = 4; + +// traceMark: Trace mark or not, only for structured grid partition. +// 0 -- Not. +// 1 -- Yes. +// blockIndexOfMark: the block index of mark, only for structured grid partition. +// cellIndexOfMark: the cell index of mark, only for structured grid partition. +int traceMark = 0; +int blockIndexOfMark = 0; +int cellIndexOfMark[] = [185,30,1]; + +// parallel Strategy: +//! -# 0 : each zone is assigned to the one that defined in grid partition procedure. +//! -# 1 : random assigned for each zone or by some else ways. +int parallelStrategy = 1; + +//----------------------------------------------------------------------- +# File path # +//----------------------------------------------------------------------- +// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts). +// partition_grid_file: Target partition grid file(PHengLEI type, *.fts). +string original_grid_file = "./grid/sphere_mixed.fts"; +string partition_grid_file = "./grid/sphere_mixed__4.fts"; + +// ------------------ Sompe advanced parameters ------------------------- +// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition". +// 0 -- Interface. (default) +// 1 -- Physical boundary condition, used in Hybrid solver. +// npartmethod: Method of interface reconstruction, default is 1. +// parallelPartMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition. +// 1 -- Using ParMetis for homogeneous MPI. +// 2 -- Using Metis for homogeneous MPI. +// 3 -- using METIS partition for homogeneous OpenMP. +// parmetisBalance: Used to specify the imbalance tolerance. +// 1 -- perfect balance. +// maxproc -- perfect imbalance. +// 1.05 -- recommended. + +int omit_no_bound_bc = 0; +int npartmethod = 1; +int parallelPartitionMethod = 2; +double parmetisBalance = 1.05; + +// numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. +// 1 -- single level. +// 2 -- 2 level. +// N -- N level, ..., et al. +int numberOfMultigrid = 1; + +######################################################################### +# Default parameters for CFD simulation # +######################################################################### +// 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. +// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved. +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +// 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 maxSimuStep = 20000; + +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; +int intervalStepSample = 1000; +int intervalStepForce = 100; +int intervalStepRes = 10; +int ifLowSpeedPrecon = 0; + +// compressible: +// 0 -- incompressible flow. +// 1 -- compressible flow. (default) +int compressible = 1; + +//----------------------------------------------------------------------- +# CFD Control Parameter # +//----------------------------------------------------------------------- +// refMachNumber: Mach number. +// attackd: Angle of attack. +// angleSlide: Angle of sideslip. +// inflowParaType: The type of inflow parameters. +// 0 -- the nondimensional conditions. +// 1 -- the flight conditions. +// 2 -- the experiment conditions. +// 3 -- the subsonic boundary conditions. +// refReNumber: Reynolds number, which is based unit length, unit of 1/m. +// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. +// 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. +// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition. +// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like: +// 1 dm = 0.1 m. +// 1 cm = 0.01 m. +// 1 mm = 0.001m. +// 1 inch = 0.0254m. +// 1 foot = 12 inches = 0.3048m. +// 1 yard = 3 feet = 0.9144m. +// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit. +// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit. +// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary +// condition is radiation equilibrium temperature, and 0.8 is the default value. + +double refMachNumber = 0.73; +double attackd = 2.79; +double angleSlide = 0.00; + +int inflowParaType = 0; +double refReNumber = 6.5e6; +double refDimensionalTemperature = 288.15; +double freestream_vibration_temperature = 10000.00; + +//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)). + +//int inflowParaType = 3; +//int nsubsonicInlet = 1; +//int nsubsonicOutlet = 1; +//string inLetFileName = "./bin/subsonicInlet.hypara"; +//string outLetFileName = "./bin/subsonicOutlet.hypara"; +//double refDimensionalTemperature = 288.144; +//double refDimensionalPressure = 1.01313E05; + +double wallTemperature = -1.0; + +double radiationCoef = 0.8; +double gridScaleFactor = 1.0; + +int numberOfAerodynamicForceComponents = 1; +double forceRefenenceLengthSpanWise = 1.0; // unit of meter. +double forceRefenenceLength = 1.0; // unit of meter. +double forceRefenenceArea = 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. + +//----------------------------------------------------------------------- +# Spatial Discretisation # +//----------------------------------------------------------------------- +#******************************************************************* +# Struct Solver * +#******************************************************************* +// inviscidSchemeName: Spatial discretisation scheme of struct grid. +// Using this when solve structered grid or hybrid. +// -- "vanleer", "steger", "hlle", "lax_f". +// -- "roe", "modified_roe". +// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw". +// str_limiter_name: Limiter of struct grid. +// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth". +// -- "nolim", no limiter. +// -- "vanalbada_clz", clz supersonic version. +string inviscidSchemeName = "roe"; +string str_limiter_name = "vanalbada"; + +#******************************************************************* +# UnStruct Solver or Common * +#******************************************************************* +// viscousType: Viscous model. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. +// viscousName: Laminar or tubulent model. +// -- "0eq-bl". +// -- "1eq-sa". +// -- "2eq-kw-menter-sst". +// -- "2eq-kw-menter-bsl". +// -- "2eq-kw-wilcox-1988". +// -- "2eq-kw-wilcox-1998". +// -- "2eq-kw-kok-tnt". +// -- "2eq-kw-wilcox-2006". +// -- "easm-kw-2003". +// -- "easm-kw-2005". +// DESType: Type of DES. +// 0 -- RANS. (default) +// 1 -- DES. +// 2 -- DDES. +// 3 -- IDDES. +// 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. +// -- "barth", "vencat", "vanleer", "minmod". +// -- "vanalbada", "smooth", "nnd", "lpz", "1st". +// -- "nolim", no limiter. +// uns_vis_name: Discretisation method of viscous term. +// -- "std", "test", "aver", "new1", "new2". +// uns_gradient: Gradient reconstruction method. +// -- "default", "ggcell", "ggnode", "lsq". +// ivencat: Variation of vencat limiter. +// 0 -- org method, it is independent of grid scale. +// 1 -- new method, it is dependent of grid scale. +// 4 -- Ustar limiter model, without grid size unitary. +// 7 -- default used. +// venkatCoeff: Cofficient of vencat, when using vencat limter. +// 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. +// skewnessAngle: The skewness angle of grid cells. +// roeEntropyFixMethod: Entropy fix (correction) method. +// 1 -- direct fix, which limits the minimum eigenvalue directly. +// 2 -- multi-dimensional fix, which is derived from structured solver and now is only valid for struct solver. +// 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. + +//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; + +string uns_scheme_name = "roe"; +string uns_limiter_name = "vencat"; +string uns_vis_name = "test"; +string gradientName = "ggnode"; + +int ivencat = 7; +double venkatCoeff = 5.0; +int reconmeth = 1; +int limitVariables = 0; +int limitVector = 0; +double skewnessAngle = 60.0; + +int roeEntropyFixMethod = 3; +double roeEntropyScale = 1.0; + +//----------------------------------------------------------------------- +# Temporal Discretisation # +//----------------------------------------------------------------------- +// iunsteady: Steady or unsteady. +// 0 -- steady. +// 1 -- unsteay. +// physicalTimeStep: The nondimensional physical time step. +// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes. +// ifStaticsFlowField: Statistical variables for DES simulation. +// startStatisticStep: Outer step when start statistics. +// when the value is larger than "maxSimuStep", it is useless. +// 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. +// tscheme: Temporal Discretisation method. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 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. +// 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. +// CFLEnd: End cfl number. +// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. +// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) +// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. +// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. +// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS. +// ifLocalTimeStep: Time step method. +// 0 --Local. +// 1 --Global. +// visl_min: Minimum value of laminar viscosity coefficient. +// turbCFLScale: Turbulence model cfl number factor. +// codeOfAleModel: Arbitrary Lagrangian-Eulerian method. +// 0 -- no ALE method. +// 1 -- ALE method for non-moving grids. +// 2 -- ALE method for moving grids. +// 3 -- ALE method for deforming grids. +// wallFunctionType: The type of wall function to implement. +// 0 -- no wall function. (default) +// 1 -- standard wall function. +// 2 -- Pab3D wall function. +// RKStage: The number of Runge-Kutta step. +// lamda: Cofficient of Runge-Kutta step. + +int iunsteady = 0; +double physicalTimeStep = 0.01; +int ifStartFromSteadyResults = 0; +int ifStaticsFlowField = 0; +int startStatisticStep = 800000; +int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2; + +int methodOfDualTime = 3; +int min_sub_iter = 50; +int max_sub_iter = 50; +double tol_sub_iter = 0.01; + +int tscheme = 4; +int iSimplifyViscousTerm = 1; +int ifLocalTimeStep = 0; +double CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; + +double ktmax = 1.0e10; + +int swapDq = 1; + +int nLUSGSSweeps = 1; +double LUSGSTolerance = 0.01; +int order = 2; + +double visl_min = 0.01; +double turbCFLScale = 1.0; +double csrv = 2.0; +double timemax = 1.0e10; +double dtsave = -1.0; +int codeOfAleModel = 0; +int aleStartStrategy = -1; +int maxale = 10; +double dtau = 0.001; + +int wallFunctionType = 0; + +int RKStage = 2; +double lamda[] = 0.5, 1.0; + +//int RKStage = 1; +//double lamda[] = 1.0; + +//int RKStage = 4; +//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; + +//----------------------------------------------------------------------- +# File In or Out # +//----------------------------------------------------------------------- +// numberOfGridGroups: The number of grid groups. +// 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 field results to visulization. +// walldistMethod: The method to compute wall distance. +// 0 -- accurate but not fast enough. +// 1 -- fast but not accurate enough. +// 2 -- super fast but more non-accurate! +// resSaveFile: The file path to save the residual convergence process, write data for every default (intervalStepRes) steps. +// turbresfile: The file path to save the residual convergence process of turbulence, write data for every default (intervalStepRes) steps. +// aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps. +// restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps. +// turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps. +// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps. +// 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. + +int numberOfGridGroups = 1; +string gridfile = "./grid/rae2822_hybrid2d__4.fts"; + +int walldistMethod = 1; + +string resSaveFile = "results/res.dat"; +string turbresfile = "results/turbres.dat"; +string aircoeffile = "results/aircoef.dat"; + +string restartNSFile = "results/flow.dat"; +string turbfile = "results/turb.dat"; + +string visualfile = "results/tecflow.plt"; +string wall_aircoefile = "results/wall_aircoef.dat"; +string probesflowfile = "results/sample.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; + +string jetDefineFile = "bin/jet.hypara"; + +string overset_gridfile = "results/iblank.ovs"; +string sixDofFileName = "results/sixDofInfo.dat"; + +int plotFieldType = 0; + +// visualfileType: The file type of visualfile. +// 0 -- Tecplot binary. +// 1 -- Tecplot ASCII. + +int visualfileType = 1; + +// visualSlice: The slice of tecflow. +// 0 -- Do not save slice data. +// 1 -- comput and save it to sliceFile. +// sliceAxis: Normal vector of slice. +// 1 -- X_DIR. +// 2 -- Y_DIR. +// 3 -- Z_DIR. +// slicePostion: Coordinate of slice. + +int visualSlice = 0; +int sliceAxis = 1; +double slicePostion = -0.5; +string sliceFile = "results/Slice.plt"; + +// min-max box of the visual block. +double lowerPlotFieldBox[] = [0.0 0.0 0.0]; +double upperPlotFieldBox[] = [1.0 1.0 1.0]; + +// 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), +// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), iblank(81). +// 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]; + +// dumpStandardModel: Dump many standard model data. +// 1 -- Turbulent flat plate. +int dumpStandardModel = 0; + +// ifSetDataMonitor: Whether to set the data monitor. +// 0 -- No. +// 1 -- Yes. +// dataMonitorType: The type of data Monitor. +// 0 -- Probes data monitor. +// 1 -- Lines data monitor. +// 2 -- Surfaces data monitor. +// probesDefineFile: Probes location information file. +// nLines: The number of lines need to be monitored. +// linesDefineFile: Lines location information file. +// nSurfaces: The number of surfaces need to be monitored. +// surfacesDefineFile: Surfaces location information file. +// searchCellsMethod: method to search the cell of each probe. +// 0 -- Nearest cell to the probe. +// 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). +// 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. +// 0 -- Take the value of probe's cell as probe real value. +// 1 -- Interpolation from probe's and neighbouring cell to probe. +// 2 -- Interpolation from probe's cell nodes to probe. +int ifSetDataMonitor = 0; + +int dataMonitorType = 0; +string probesDefineFile = "bin/probes_XYZ.dat"; + +//int dataMonitorType = 1; +//int nLines = 1; +//string linesDefineFile = "bin/lines_XYZ.dat"; + +//int dataMonitorType = 2; +//int nSurfaces = 4; +//string surfacesDefineFile = "bin/surfaces_XYZ.dat"; + +int searchCellsMethod = 0; + +int nProbeVariables = 6; +int probeVariables[] = [0, 1, 2, 3, 4, 5]; +int probeVariablesInterpolationMethod = 0; +//----------------------------------------------------------------------- +# Turbulence Parameter # +//----------------------------------------------------------------------- +// 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. + +int turbInterval = 1; +int kindOfTurbSource = 0; +int mod_turb_res = 0; +double turb_relax = 1.0; +double freeStreamViscosity = 1.0e-3; +double muoo = 3.0; +double kwoo = 5.0; +int transitionType = 0; +double turbIntensity = -1.0; + +# maximum eddy viscosity (myt/my) max. +double eddyViscosityLimit = 1.0e10; +int monitor_vistmax = 0; + +//----------------------------------------------------------------------- +# LES Parameter # +//----------------------------------------------------------------------- +// iLES: Create LESSolver or not. +// >= 1 - Create LESSolver; +// < 1 - not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 - in only first sub-iter; +// != 0 - in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 - not; +// != 0 - Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// sgsmodel: subgrid scale model. +// = "smagorinsky"; +// = "dsm"; +// = "wale". +// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak); +// = 2 - pow(deltai * deltaj *deltak, 1/3); +// = 3 - Devloped by Scotti. +// wallDampingFunctionType: = 0 - no wall function; +// = 1 - van Driest; +// = 2 - developed by Dr. Deng Xiaobing; +// = 3 - developed by Piomelli. +// turbViscousCutType: turbulent viscosity cut type. +// = 0 - mu_total = mut + mul; +// = 1 - mu_total = max(mut-mul,0)+ mul; +// = 2 - mu_total = max(mut ,0)+ mul. +// smagConstant: constant of smagorinsky model. +// waleConstant: constant of wale model. +// filterDirection[3]: filter variables in i, j, k direction or not. +// averageDirection[3]: average variables in i, j, k direction or not. +// isotropicConstant: constant of isotropic part of SGS stress. + +int iLES = 0; +string sgsmodel = "smagorinsky"; +int deltaFunctionType = 2; +int wallDampingFunctionType = 1; +int turbViscousCutType = 2; +double smagConstant = 0.135; +double isotropicConstant = 0.0; +double waleConstant = 0.6; +int filterDirection[] = [1, 1, 0]; +int averageDirection[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +//----------------------------------------------------------------------- +# Other Parameters for Hypersonic Non-equilibrium Gas # +//----------------------------------------------------------------------- +// dg_high_order: +// 0 -- generic order accuracy. +// 1 -- high order accuracy. +// 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. +// nm: Equation number of the physics, but is out of commision now. +// 4 -- for 2D. +// 5 -- for 3D. +// 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. +// catalyticCoef: +// 0.0 -- full non-catalytic wall boundary condition. +// 1.0 -- full catalytic wall boundary condition. +// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient. +// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11". +// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. +// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. +// "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. +// 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. + +int dg_high_order = 0; +int iapplication = 0; +int iCodeBranch = 0; +int nm = 5; + +double refGama = 1.4; +double prl = 0.72; +double prt = 0.90; +double sc_l = 0.5; +double sc_t = 0.5; + +int nGasModel = 0; +int nchem = 0; +int nchemsrc = 1; +int nchemrad = 1; +int ntmodel = 1; +int nChemicalFlowStep = 0; +double catalyticCoef = 0.0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +string speciesName = "O, O2, NO, N, N2"; +string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77"; + +//string speciesName = "O, O2, NO, N, NO+, N2, e-"; +//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.77, 0.0"; + +//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-"; +//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.77, 0.0"; + +//string gasfile = "Mars-Pa8"; +//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"; + +int ifStartFromPerfectGasResults = 0; + +######################################################################### +// Multi-Grid parameters. +// nMGLevel: The number of level of Multi-Grid. +// <= 1 -- Single-level. +// > 1 -- multi-level. +// MGPreIteration: For each grid, the number of pre-smoothing steps. +// n_post: For each grid, the number of post-smoothing steps. +// MGCoarsestIteration: For the coarest grid the number of smoothing steps. +// MGFasType: V-multi cycle or W-multi cycle. +// 1 -- V-multi cycle. +// 2 -- W-multi cycle. +// 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. +// mgCFLScale: CFL number enlarge times for coarse grid. +// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid. +// 1 -- zero order. +// 2 -- first-order. (default) +// mgCorrectionLimit: Multi-grid correction limit. + +int nMGLevel = 1; +int MGCoarsestIteration = 1; +int MGPreIteration = 1; +int MGFasType = 1; +int n_post = 0; +int flowInitStep = 100; +int mprol = 2; +double mgCFLScale = 1.0; +double mgCorrectionLimit = 0.01; + +//--------------- Some parameter for turbulent model -------------------- +// neasm: The variation of kw turbulent model. +// ismooth_turb: Residual smooth for turb or not. +// SSTProductType: The type of product term based on vorticity for SST. +// SAProductType: The type of product term based on vorticity for SA. +int neasm = -3; +int SSTProductType = 0; +int ismooth_turb = 0; +int SAProductType = 2; + +// ----------------- Overset Grid parameter ----------------------------- +int codeOfDigHoles = 1; +int codeOfTurbulentModel = 0; +string masterFileName = "./grid/searchFile.inp"; +string holeBasicFileName = "./grid/holeBasicFile.inp"; +string holeFullFileName = "./grid/holeFullFile.dat"; +string linkFileName = "./grid/topology.dat"; +string zoneInverseFileName = "./grid/zoneInverseMapping.inp"; + +######################################################################### +# High Order Struct Solver # +######################################################################### +// ifvfd: +// 0 -- NSSolverStruct using Finite Volume Method. +// 1 -- NSSolverStruct using Finite Differ Method. +// SolverStructOrder: Spatial discretisation order of NS equations with struct grid. +// <= 2 -- finite volume method. +// >= 3 -- finite difference order. (to be completed) +// 0 -- default. +// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence, +// smaller epsilon, robuster for shock-detecting. +// str_highorder_interpolation_type: +// -- "classical", "test". +// str_highorder_flux_name: +// -- "roe", "steger". +// structhighordergradient: +// -- "conservation", "chain_rule". +int ifvfd = 0; +string str_highorder_solver = "WCNS"; +int SolverStructOrder = 0; +double str_highorder_interpolation_epsilon = 1.0e-6; +string str_highorder_interpolation_type = "test"; +string str_highorder_flux_name = "steger"; +string structhighordergradient = "conservation"; +double coefofstrflux = 0.5; +double limitcoefofinterface = 0.0; + +// ----------------- Advanced choices ----------------------------------- +// outtimesc: Time stepping scheme for the outer loop. +// MUSCLCoefXk: The parameter of MUSCL interpolations, belongs to [-1, 1]. +// -1 -- seconde-order fully-upwind differencing. +// 0 -- seconde-order upwind-biased differencing. +// 0.333333 -- third-order upwind-biased differencing. +// 1 -- seconde-order central differencing. +// MUSCLCoefXb: The limiter parameter. +// 0 -- the effect of the limiter is cancelled, means the first-order interpolations. +// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1. +string outtimesc = "impbd2"; +double MUSCLCoefXk = -1; +double MUSCLCoefXb = 1.0; +int allReduceStep = 1; + +// ----------------- overlap configuration ------------------------------ +// codeOfOversetGrid: Overlapping(overset) grid or not. +// 0 -- NON-overlapping grid. +// 1 -- Overlapping grid. +int codeOfOversetGrid = 0; +int codeOfOversetSlipGrid = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 1; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/overlap.ovs"; +double walldistMainZone = 1.0 +double toleranceForOversetSearch = 1.0e-3; +double toleranceForOversetBox = 1.0e-3; +int twoOrderInterpolationOrNot = 0; +int keyEnlargeOfActiveNodes = 0; +int outTecplotOverset = 0; + +int numberOfMovingBodies = 2; + +// ---------------- ATP read -------------------------------------------- +//@int inflowParaType = 0; +//@double refReNumber = 2.329418E08; +//@double refDimensionalTemperature = 288.144; +//@double refDimensionalPressure = 1.01313E05; +//@double height = -0.001; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; + +######################################################################### +# Old Parameter # +######################################################################### +int isPlotVolumeField = 0; + diff --git a/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/cfd_para_transonic.hypara b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/cfd_para_transonic.hypara new file mode 100644 index 0000000..06d2d7c --- /dev/null +++ b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/cfd_para_transonic.hypara @@ -0,0 +1,204 @@ +######################################################################### +# 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 = 300; + +int intervalStepFlow = 100; +int intervalStepPlot = 100; +int intervalStepForce = 100; +int intervalStepRes = 10; + +######################################################################### +# Inflow Parameter # +######################################################################### +// refMachNumber: Mach number. +// attackd: Angle of attack. +// angleSlide: Angle of sideslip. +// inflowParaType: The type of inflow parameters. +// 0 -- the nondimensional conditions. +// 1 -- the flight conditions. +// 2 -- the experiment conditions. +// 3 -- the subsonic boundary conditions. +// refReNumber: Reynolds number, which is based unit length, unit of 1/m. +// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. +// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition. +// height: Fly height, unit of km. +// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like: +// 1 dm = 0.1 m. +// 1 cm = 0.01 m. +// 1 mm = 0.001m. +// 1 inch = 0.0254m. +// 1 foot = 12 inches = 0.3048m. +// 1 yard = 3 feet = 0.9144m. +// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit. +// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit. + +double refMachNumber = 0.755; +double attackd = 0.016; +double angleSlide = 0.00; + +int inflowParaType = 0; +double refReNumber = 6.5e6; +double refDimensionalTemperature = 288.15; + +//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)). + +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. +// -- "roe", "vanleer", "ausm+up", "ausmpw". +// str_limiter_name: Limiter of struct grid. +// -- "3rdsmooth", "smooth". +// -- "nolim", no limiter. + +string inviscidSchemeName = "roe"; +string str_limiter_name = "smooth"; + +#******************************************************************* +# 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 = "roe"; +string uns_limiter_name = "vencat"; +double venkatCoeff = 5.0; + +######################################################################### +# Temporal Discretisation # +######################################################################### +// iunsteady: Steady or unsteady. +// 0 -- steady. +// 1 -- unsteay. +// CFLEnd: The CFL number, [0.1, 100]. +// The bigger the value, the convergence faster but lower robustness. +// nLUSGSSweeps: Number of Sub-iteration of LU-SGS. +// 1 -- is recommended for structured solver. +// 1-3 -- is recommended for unstructured solver. + +int iunsteady = 0; + +double CFLEnd = 30.0; + +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/background__2.fts"; +int plotFieldType = 1; +int visualfileType = 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), iblank(81). +// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! +// Variables order must from small to big. + +int nVisualVariables = 8; +int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; + +// limitVariables: Limit model (It is useful only if limitVector is 0). +// 0 -- limit only for pressure and denstiny, then get the min value. +// 1 -- limit for every variables, then get the min value. +// limitVector: +// 0 -- Each variable use the same limiter coefficient. +// 1 -- Each variable use the respective limiter coefficients. +// reconmeth: +// 0 -- When reconstruct face value, Q+, Q- use respective limiter coefficients. +// 1 -- Q+, Q- use the min limiter coefficients of left and right cell. + +int reconmeth = 1; +int limitVariables = 0; +int limitVector = 0; diff --git a/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/grid_para.hypara b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/grid_para.hypara new file mode 100644 index 0000000..b323632 --- /dev/null +++ b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/grid_para.hypara @@ -0,0 +1,44 @@ +######################################################################### +# 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; +int dumpOldGrid = 0; + +######################################################################### +# 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/aux-lower.cgns"; +//string out_gfile = "./grid/aux-lower.fts"; + +//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"; diff --git a/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/key.hypara b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/key.hypara new file mode 100644 index 0000000..7ba83ad --- /dev/null +++ b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/key.hypara @@ -0,0 +1,57 @@ +string title = "PHengLEI Main Parameter Control File"; + +// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE. +string defaultParaFile = "./bin/cfd_para.hypara"; + +// ndim: Dimensional of the grid, 2 or 3. +// nparafile: the number of parameter files. +// nsimutask: simulation task type. +// 0 -- CFD Solver of NS or Turbulation. +// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc. +// Grid conversion: from other format to PHengLEI format (.fts). +// Grid reconstruction: such as grid adaptation. +// Grid merging: merge two blocks into one block. +// Grid repairing: repair the original grid in order to remove the negative volume cells. +// 2 -- Wall distance computation for turb-solver. +// 3 -- Grid partition. +// 4 -- Knowledge repository / examples of PHengLEI-API. +int ndim = 2; +int nparafile = 1; + +//int nsimutask = 0; +//string parafilename = "./bin/cfd_para_subsonic.hypara"; +//string parafilename = "./bin/cfd_para_transonic.hypara"; +//string parafilename = "./bin/cfd_para_supersonic.hypara"; +//string parafilename = "./bin/cfd_para_hypersonic.hypara"; +//string parafilename = "./bin/incompressible.hypara"; +//string parafilename1 = "./bin/overset_config.hypara"; + +//int nsimutask = 1; +//string parafilename = "./bin/grid_para.hypara"; + +//int nsimutask = 2; +//string parafilename = "./bin/cfd_para.hypara"; + +//int nsimutask = 3; +//string parafilename = "./bin/partition.hypara"; + +//int nsimutask = 4; +//string parafilename = "./bin/repository.hypara"; + +//int nsimutask = 5; +//string parafilename = "./bin/overset_grid_view.hypara"; + +int nsimutask = 6; +string parafilename = "./bin/overset_config.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 = ""; diff --git a/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/overset_config.hypara b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/overset_config.hypara new file mode 100644 index 0000000..db9da58 --- /dev/null +++ b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/overset_config.hypara @@ -0,0 +1,28 @@ +int parallelStrategy = 1; +int numberOfGridGroups = 3; +string gridfile = "./grid/background__2.fts"; +string gridfile1 = "./grid/upperwing__2.fts"; +string gridfile2 = "./grid/lowerwing__2.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 +int symetryOrNot = 1; //是否只进行半场计算 +int readInAuxiliaryInnerGrid = 1; //是否需要辅助网格（inner） +int readInAuxiliaryOuterGrid = 0; //是否需要辅助网格（outer） +int readInSklFileOrNot = 0; //读入skl文件有助于点属性的准确通讯，但是比较耗时 +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string oversetGridFileName = "./grid/overlap.ovs"; +double walldistMainZone = 1.0 +double gridScaleFactor = 0.001; +double toleranceForOversetSearch = 1e-3; +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 + diff --git a/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/partition.hypara b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/partition.hypara new file mode 100644 index 0000000..16478fe --- /dev/null +++ b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/bin/partition.hypara @@ -0,0 +1,27 @@ +// pgridtype: The grid type. +// 0 -- unstruct grid. +// 1 -- struct grid. +// maxproc: The number of partition zones that want to be divided into, +// which is equal to the number of CPU processors you want. +// Usually, 50~100 thousands structured cells per CPU-Core is suggested. +// 30~70 thousands unstructured cells per CPU-Core is suggested. +// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts). +// partition_grid_file: Target partition grid file(PHengLEI type, *.fts). + +int pgridtype = 0; +int maxproc = 2; + +//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"; + +// numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. +// 1 -- single level. +// 2 -- 2 level. +// N -- N level,..., et al. +int numberOfMultigrid = 1; diff --git a/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/grid/aux-lower.cgns b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/grid/aux-lower.cgns new file mode 100644 index 0000000..be05388 Binary files /dev/null and b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/grid/aux-lower.cgns differ diff --git a/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/grid/aux-upper.cgns b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/grid/aux-upper.cgns new file mode 100644 index 0000000..c32d42c Binary files /dev/null and b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/grid/aux-upper.cgns differ diff --git a/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/grid/background.cgns b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/grid/background.cgns new file mode 100644 index 0000000..11cf126 Binary files /dev/null and b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/grid/background.cgns differ diff --git a/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/grid/lowerwing.cgns b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/grid/lowerwing.cgns new file mode 100644 index 0000000..49b0227 Binary files /dev/null and b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/grid/lowerwing.cgns differ diff --git a/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/grid/upperwing.cgns b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/grid/upperwing.cgns new file mode 100644 index 0000000..8e96815 Binary files /dev/null and b/F03_TwoD_Dual0012_OversetGrid_Invis_Unstruct_4CPU/grid/upperwing.cgns differ