diff --git a/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/README.txt b/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/README.txt new file mode 100644 index 0000000..472a79c --- /dev/null +++ b/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/README.txt @@ -0,0 +1,2 @@ +本算例结构网格重叠装配过程在读网格阶段会在结构网格上重新构建非结构网格信息，然后按照非结构的方式进行重叠网格装配过程 +用户如需使用结构重叠，则需使用2171版本代码及相应算例库版本的F01结构重叠算例 \ No newline at end of file diff --git a/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/bin/cfd_para.hypara b/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/bin/cfd_para.hypara new file mode 100644 index 0000000..f903a5a --- /dev/null +++ b/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/bin/cfd_para.hypara @@ -0,0 +1,1467 @@ +//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ +// 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 + +// PHengLEI 2212 + +//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ +########################################################################### +# 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. +// 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. +// iadapt: Adaptation number for unstructure grid. +// SymmetryFaceVector: The vector of symmetry face. +// 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; + +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; + +// 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; +int omitRepeatInterface = 1; + +//----------------------------------------------------------------------- +# 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. +// 9 -- Gridgen type of structured grid, *.dat/*.grd. +// 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. +int numberOfGridFile = 1; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +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; + +// 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"; + +// ----------------- Grid Refine Parameters ----------------------------- +// anisoRefine: If refine grid by anisoRefine type. +// 0 -- Not. (default) +// 1 -- Yes. +// 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 anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; +int exclusiveCase = 0; +int projectOrgPoint = 0; +string geometryFileName = "./grid/jsm.igs"; + +// ----------------- Grid Deform Parameters ----------------------------- +// deformationMethod: Grid Deform. +// 1 -- SPRING. +// 2 -- RBF. +// stationalGridFile: Original grid file. +// visualFileName : The visualization file path of deform grid. +// nDeformStep : The max deform step. +// flapAngle : The max flap angle. +// rotatePostionZ : Rotate postion. +// rotatePostionY : Rotate postion. +// gridSlice : If dump slice grid. +// sliceAxis : Grid slice axis. +// slicePosition : Grid slice position. +int nDeformStep = 40; +double flapAngle = 10.0; +double rotatePostionZ = 4.00003; +double rotatePostionY = 3.05; + +int deformationMethod = 2; +string stationalGridFile = "./grid/Segment2Brid.fts"; +string visualFileName = "./results/deformedGrid.dat" + +int gridSlice = 1; +int sliceAxis = 1; +double slicePosition = 13; + +// ----------------- RBF Parameters ------------------------------------- +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. +int numberOfReferenceCP = 40; +double influencePara = 25.0; + +// ----------------- 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. +// translationLength[]: The relative distance between two periodic face + which only support one direction. +// rotationAngle: The relative angle between two periodic face. + which is recorded in degrees. +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. +// 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. +// 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]; + +// parallelStrategy: +// 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. +// parallelPartitionMethod: 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. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; +int intervalStepSample = 1000; +int intervalStepForce = 100; +int intervalStepRes = 10; + +// compressible: +// 0 -- incompressible flow. +// 1 -- compressible flow. (default) +int compressible = 1; + +// 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) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 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. (Useless!) +// 4 -- the condition that the velocity, temperature and density are given. +// 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. +// 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 = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. +// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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. +// 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; +int flowInitMethod = 0; + +int inflowParaType = 0; +double refReNumber = 6.5e6; +double refDimensionalTemperature = 288.15; +double freestream_vibration_temperature = 300.00; + +//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)). + +// 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 = 1000.0; +//double refDimensionalPressure = 1.0e5; + +// The MachNumber, temperature and pressure are fixed. +//int inflowParaType = 6; +//double refDimensionalTemperature = 293.0; +//double refDimensionalPressure = 8886.06; + +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; + +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. +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. +double knudsenLength = 1.0; // unit of meter. +double refMolecularWeight = 28.9644; // unit of g/mol. + +//----------------------------------------------------------------------- +# 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", "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"; + +#************************************************************************ +# 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", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", +// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". +// 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". +// gradientName: 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. +// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0. + +//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; + +double AusmpwPlusLimiter = 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 unsteady simulation. +// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation. +// startStatisticStep: Outer step when start statistics. +// when the value is larger than "maxSimuStep", it is useless. +// 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 = - ^2 +// 1 -- tau = +// 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 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. +// 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. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. +// 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. +// 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. +// 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; +double physicalTimeStepDimensional = -0.001; +int ifStartFromSteadyResults = 0; +int ifStaticsFlowField = 0; +int ifStaticsReynoldsStress = 0; +int startStatisticStep = 800000; +double statisticalTimePeriod = -1.0; +int statisticMethod = 0; +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; +int isUseLocalCFL = 0; +int isUsePreTwall = 0; +double CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; +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; + +int nLUSGSSweeps = 1; +double LUSGSTolerance = 0.01; +int order = 2; + +double visl_min = 0.01; +double turbCFLScale = 1.0; +double csrv = 1.0; +double timemax = 1.0e10; +double dtsave = -1.0; +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. +// 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"; +string transitionResFile = "results/transitionRes.dat"; +string aircoeffile = "results/aircoef.dat"; + +string restartNSFile = "results/flow.dat"; +string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; + +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"; + +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; + +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; + +string sixDofFileName = "results/sixDofInfo.dat"; +string derivativeFileName = "results/identify.dat"; +string hysteresisFileName = "results/force_beta.plt"; + +int plotFieldType = 0; + +// visualfileType: The file type of visualfile. +// 0 -- Tecplot binary. +// 1 -- Tecplot ASCII. +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. +int visualfileType = 1; + +// samplefileMode: The dump mode of sample file. +// 0 -- dump out every probe/line/surface data for all step intervals. +// 1 -- dump out all probe/line/surface data for every step intervals. +int samplefileMode = 0; + +// 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"; +int dumpWallFaceCenter = 0; + +// min-max box of the visual block. +double lowerPlotFieldBox[] = [0.0 0.0 0.0]; +double upperPlotFieldBox[] = [1.0 1.0 1.0]; + +//-----------the optional parameters list for the flow field output---------------- +// 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), streamline_u(45), streamline_v(46), streamline_w(47), +// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). +// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! +// Variables order must from small to big. +//-----------the optional parameters list for the wall boundary condition---------------- +// nVisualWallVariables: The number of visual variables on wall. +// visualWallVariables : dumped variable types, listed as following: +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- 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), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). +int nVisualVariables = 8; +int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; + +int nVisualWallVariables = 9; +int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; + +// 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), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). +// 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 = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +int probeVariablesInterpolationMethod = 0; + +#************************************************************************ +# Turbulence Parameter * +#************************************************************************ +// turbInterval: Iteration number of turbulence. +// kindOfTurbSource: Kinds of turbulent source. +// 0 -- Original. +// 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; +int kindOfTurbSource = 0; +int mod_turb_res = 0; +double freeStreamViscosity = 1.0e-3; +double muoo = 3.0; +double kwoo = 5.0; +int transitionType = 0; +double turbIntensity = -1.0; +int freeturbIntensitySRModify = 0; +double freeDecayXLocation = 0.0; +int compressibleCorrection = 0; +int transitionMaFix = 1; + +// 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"; +// = "dsmCom"; +// = "wale"; +// = "sigma". +// 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 = 0.1; +double isotropicConstant = 0.0; +double waleConstant = 0.6; +double sigmaConstant = 1.35; +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. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic 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. less than and equal to 1 represents the mixture gas. +// Otherwise, the pure gas with one component is used for perfect gas. +// 0 -- Earth gas. +// 1 -- Mars gas. +// 2 -- Argon. +// 3 -- Nitrogen. +// nEnergyRecycle: The type of EnergyModel Recycle. +// 0 -- not used. +// 1 -- used. +// nDensityModify: The type of densitymodify. +// 0 -- not used. +// 1 -- used. +// nchem: +// 0 -- without chemical reaction flow. +// 1 -- the chemical reaction flow is considered. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. +// 0 -- perfect gas. +// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). +// 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. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. +// 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 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: +// 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. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// 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]. +// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// 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. +// nSpeciesLimit: limitter of gas species +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// 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 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. +// nAblation: +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. +// isInjection: +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. +// nViscosityModel: +// 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. +// 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. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "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. +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. +int dg_high_order = 0; +int iapplication = 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; +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 nIdealState = 0; +int nEnergyRecycle = 1; +int nSlipBCModel = 0; +int nDensityModify = 1; +int nTEnergyModel = 0; +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; +double sigmaVelocity = 1.0; +double sigmaTemperature = 1.0; +double sigmaMassFraction = 1.0; +double velocitySlipCorrectConstant = 1.0; + +double chemicalRelaxCorf = 1.0; +double chemicalSpectrumRadiusCoef = 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; +double maxTemperature = 50000.0; +double densityMin = 1.0e-8; +double densityMinFactor = 0.1; +double tAdjustmentFactor = 10.0; +double iniSpeedCoef = 1.0; +int iniSpeedMode = 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 nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; + +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +string speciesName = "O, O2, NO, N, N2"; +string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; + +//string speciesName = "O, O2, NO, N, NO+, N2, e-"; +//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 0.0"; + +//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-"; +//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 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"; + +//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"; + +//string gasfile = "Combustion-12"; +//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; +//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; + +//string gasfile = "Gas-Mixture"; +//string speciesName = "SpeciesA, SpeciesB"; +//string initMassFraction = "1.0, 0.0"; +int nSutherland = 0; +double gamaSpeciesA = 1.4; +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 nFraction = 0; +int nContinueModel = 0; +int nChemicalFlowStep = 0; +int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; + +######################################################################### +// 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 * +#************************************************************************ +// isFVMOrFDM: +// 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 isFVMOrFDM = 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. +// oversetInterpolationMethod: the method of overset interpolation while field simulation. +// 0 -- set the acceptor cell value by donor cell value. +// 1 -- set the acceptor cell value by distance weight of donor cell value. +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; + +// ----------------- ALE configuration ------------------------------ +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. + +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. +int methodForKineticEquation = 0; +double relaxParameterOfKinetic = 1.0; + +#************************************************************************ +# motive information * +#************************************************************************ +int numberOfMovingBodies = 1; + +############################## body0 ############################## +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. +// -1 given motion partten. +// 0 still. +// 1 six DOF motion. +// 2 three DOF motion. +// 11 X-axis forced motion. +// 12 Y-axis forced motion. +// 13 Z-axis forced motion. +// 14 forced pitch motion. +// 15 forced yaw motion. +// 16 forced roll motion. +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"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; + +// post indentify. +int integralOrder = 4; + +// ---------------- ATP read -------------------------------------------- +//@int inflowParaType = 0; +//@double refReNumber = 6.5e6; +//@double refDimensionalTemperature = 288.15; +//@double freestream_vibration_temperature = 300.00; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalVelocity = 0; +//@double refDimensionalDensity = 0; +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ +int isPlotVolumeField = 0; + +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; + +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; + +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ +int isSolveEnergyEquation = 0; +int isSolveTurbEquation = 0; +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/bin/grid_para.hypara b/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/bin/grid_para.hypara new file mode 100644 index 0000000..3348a00 --- /dev/null +++ b/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/bin/grid_para.hypara @@ -0,0 +1,41 @@ +######################################################################### +# Grid data type # +######################################################################### +// gridtype: Grid type for generation, conversion, reconstruction, merging. +// 0 -- Unstructured grid. +// 1 -- Structured grid. +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +// from_gtype: Type of grid data type in grid conversion process. +// -1 -- MULTI_TYPE +// 1 -- HyperFLOW( PHengLEI ), *.fts. +// 2 -- CGNS, *.cgns. +// 3 -- Plot3D type of structured grid, *.dat/*.grd. +// 4 -- Fieldview type of unstructured grid, *.dat/*.inp. +// 5 -- Fluent, *.cas/*.msh. +// 6 -- Ustar, mgrid.in. +// 7 -- Hybrid, include both of unstructured and structured grid, *.fts. +// 8 -- GMSH, *.msh. +int gridtype = 1; +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; +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. +int numberOfGridFile = 4; +string from_gfile = "./grid/30p30n-background.cgns"; +string from_gfile1 = "./grid/30p30n-main.cgns"; +string from_gfile2 = "./grid/30p30n-flap.cgns"; +string from_gfile3 = "./grid/30p30n-slat.cgns"; + + + diff --git a/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/bin/key.hypara b/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/bin/key.hypara new file mode 100644 index 0000000..ff96e4c --- /dev/null +++ b/F01_TwoD_30p30n_OversetGrid_SA_Struct_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/cfd_para_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 = 1; +//string parafilename = "./bin/grid_deform_para.hypara"; + +//int nsimutask = 1; +//string parafilename = "./bin/grid_refine_para.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/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/bin/overset_config.hypara b/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/bin/overset_config.hypara new file mode 100644 index 0000000..45446ad --- /dev/null +++ b/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/bin/overset_config.hypara @@ -0,0 +1,35 @@ +// ----------------- overlap configuration ------------------------------ +// numberOfGridGroups: The number of grid groups. +// codeOfOversetGrid: Overlapping(overset) grid or not. +// 0 -- NON-overlapping grid. +// 1 -- Overlapping grid. +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in + the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid +// 0 -- no. +// 1 -- yes. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. + +int numberOfGridGroups = 4; +string gridfile = "./grid/30p30n-background__4.fts"; +string gridfile1 = "./grid/30p30n-main__4.fts"; +string gridfile2 = "./grid/30p30n-slat__4.fts"; +string gridfile3 = "./grid/30p30n-flap__4.fts"; +int codeOfOversetGrid = 1; +int twoOrderInterpolationOrNot = 1; +int keyEnlargeOfActiveNodes = 0; +double gridScaleFactor = 0.001; +int outTecplotOverset = 1; + + diff --git a/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/bin/partition.hypara b/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/bin/partition.hypara new file mode 100644 index 0000000..cad069c --- /dev/null +++ b/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/bin/partition.hypara @@ -0,0 +1,31 @@ +// pgridtype: The grid type. +// 0 -- unstruct grid +// 1 -- struct grid +// maxproc: The number of partition zones that want to be divided into, +// which is equal to the number of CPU processors you want. +// Usually, 50~100 thousands structured cells per CPU-Core is suggested. +// 30~70 thousands unstructured cells per CPU-Core is suggested. +// original_grid_file : original grid file that want to be divided(HyperFLOW/PHengLEI type, *.fts). +// partition_grid_file : target partition grid file(HyperFLOW/PHengLEI type, *.fts). + +int numberOfGridFile = 4; +int pgridtype = 1; +int pgridtype1 = 1; +int pgridtype2 = 1; +int pgridtype3 = 1; +int maxproc = 4; +int maxproc1 = 4; +int maxproc2 = 4; +int maxproc3 = 4; + +string original_grid_file = "./grid/30p30n-background.fts"; +string original_grid_file1 = "./grid/30p30n-main.fts"; +string original_grid_file2 = "./grid/30p30n-flap.fts"; +string original_grid_file3 = "./grid/30p30n-slat.fts"; + +// Number of multi-grid levels, ONLY used for structured grid. +// 1 -- single level, 2 -- 2 level, N -- N level, ..., et al. +int numberOfMultigrid = 1; + + + diff --git a/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/grid/网格地址.txt b/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/grid/网格地址.txt new file mode 100644 index 0000000..899f977 --- /dev/null +++ b/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/grid/网格地址.txt @@ -0,0 +1,5 @@ +红山开源风雷算例库原始网格获取百度网盘链接： +链接：http://pan.baidu.com/s/1aZ9cdkp6CkT9il4fEpnTcA +提取码：w47m + +注：plot3D格式网格需同时下载.grd和.inp文件 \ No newline at end of file diff --git a/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/结构二维30p30n网格重叠装配_算例说明文档.pdf b/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/结构二维30p30n网格重叠装配_算例说明文档.pdf new file mode 100644 index 0000000..ed186c8 Binary files /dev/null and b/F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU/结构二维30p30n网格重叠装配_算例说明文档.pdf differ diff --git a/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/README.txt b/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/README.txt new file mode 100644 index 0000000..472a79c --- /dev/null +++ b/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/README.txt @@ -0,0 +1,2 @@ +本算例结构网格重叠装配过程在读网格阶段会在结构网格上重新构建非结构网格信息，然后按照非结构的方式进行重叠网格装配过程 +用户如需使用结构重叠，则需使用2171版本代码及相应算例库版本的F01结构重叠算例 \ No newline at end of file diff --git a/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/boundary_condition.hypara b/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/boundary_condition.hypara deleted file mode 100644 index 6d30c51..0000000 --- a/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/boundary_condition.hypara +++ /dev/null @@ -1,64 +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 = 8; -string bcName = "SOLID_SURFACE"; -{ - int bcType = 2; -} -string bcName = "Wall_11"; -{ - int bcType = 11; -} -string bcName = "Wall_12"; -{ - int bcType = 12; -} -string bcName = "Wall_13"; -{ - int bcType = 13; -} -string bcName = "Wall_8"; -{ - int bcType = 8; -} -string bcName = "SYMMETRY"; -{ - int bcType = 3; -} -string bcName = "FARFIELD"; -{ - int bcType = 4; -} -string bcName = "POLE"; -{ - int bcType = 7; -} - -# '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/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/cfd_para.hypara b/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/cfd_para.hypara index b17970c..f903a5a 100644 --- a/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/cfd_para.hypara +++ b/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/cfd_para.hypara @@ -8,22 +8,24 @@ // Platform for Hybrid Engineering Simulation of Flows + // China Aerodynamics Research and Development Center + // (C) Copyright, Since 2010 + +// PHengLEI 2212 + //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ########################################################################### # 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. -// 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. +// 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. +// 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. @@ -32,21 +34,37 @@ // 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. -int axisup = 1; +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; // 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; +int omitRepeatInterface = 1; //----------------------------------------------------------------------- # Grid data type # @@ -61,6 +79,7 @@ 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. @@ -74,15 +93,13 @@ 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. int numberOfGridFile = 1; -string from_gfile = "./grid/rae2822_hybrid2d.cas"; -string from_gfile1= ""; - -string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +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. @@ -91,9 +108,9 @@ 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"; +// 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; @@ -102,38 +119,36 @@ 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. -// 3 -- inch. +// 1 -- meter. +// 2 -- millimeter. +// 3 -- inch. // exclusiveCase: Parallel projection exclusive case. -// 0 -- NON case. -// 1 -- JSM-C2-NPOFF case. -// 2 -- CHNT. +// 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. - +int anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; +int exclusiveCase = 0; +int projectOrgPoint = 0; +string geometryFileName = "./grid/jsm.igs"; // ----------------- Grid Deform Parameters ----------------------------- // deformationMethod: Grid Deform. -// 1 -- SPRING. -// 2 -- RBF. +// 1 -- SPRING. +// 2 -- RBF. // stationalGridFile: Original grid file. // visualFileName : The visualization file path of deform grid. // nDeformStep : The max deform step. -// flapAngle : The max flap angle. +// flapAngle : The max flap angle. // rotatePostionZ : Rotate postion. // rotatePostionY : Rotate postion. // gridSlice : If dump slice grid. @@ -153,10 +168,10 @@ int sliceAxis = 1; double slicePosition = 13; // ----------------- RBF Parameters ------------------------------------- -// numberOfReferenceCP : Number of reference Control Points. -// influencePara : The RBF influence radius parameter. +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. int numberOfReferenceCP = 40; -double influencePara = 25.0; +double influencePara = 25.0; // ----------------- Periodic Parameters -------------------------------- // Notice: Rotational periodicity only support rotation along the X axis! @@ -168,9 +183,8 @@ double influencePara = 25.0; which only support one direction. // rotationAngle: The relative angle between two periodic face. which is recorded in degrees. - int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; +double translationLength[] = [0.0, 0.0, 0.0]; double rotationAngle = 0.0; ######################################################################### @@ -181,27 +195,29 @@ 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. // 1 -- Yes. // blockIndexOfMark: the block index of mark, only for structured grid partition. -// cellIndexOfMark: the cell 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]; +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; +// parallelStrategy: +// 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). +// 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"; @@ -219,11 +235,10 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts"; // 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; +double parmetisBalance = 1.05; // numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. // 1 -- single level. @@ -235,29 +250,35 @@ 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. +// 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; +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; int intervalStepSample = 1000; -int intervalStepForce = 100; -int intervalStepRes = 10; -int ifLowSpeedPrecon = 0; +int intervalStepForce = 100; +int intervalStepRes = 10; // compressible: // 0 -- incompressible flow. // 1 -- compressible flow. (default) int compressible = 1; +// 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) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 1; + //----------------------------------------------------------------------- # CFD Control Parameter # //----------------------------------------------------------------------- @@ -268,32 +289,36 @@ int compressible = 1; // 0 -- the nondimensional conditions. // 1 -- the flight conditions. // 2 -- the experiment conditions. -// 3 -- the subsonic boundary conditions. +// 3 -- the subsonic boundary conditions. (Useless!) // 4 -- the condition that the velocity, temperature and density are given. // 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 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. +// 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 = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. // forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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. -// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol. +// 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; +int flowInitMethod = 0; int inflowParaType = 0; double refReNumber = 6.5e6; @@ -307,33 +332,32 @@ double freestream_vibration_temperature = 300.00; //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; - -//The velocity, temperature and density are fixed. +// The velocity, temperature and density are fixed. //int inflowParaType = 4; //double refDimensionalVelocity = 1000.0; -//double refDimensionalDensity = 1.0e3; +//double refDimensionalDensity = 1.0e3; -//The velocity, temperature and pressure are fixed. +// The velocity, temperature and pressure are fixed. //int inflowParaType = 5; //double refDimensionalVelocity = 1000.0; //double refDimensionalPressure = 1.0e5; -//The MachNumber, temperature and pressure are fixed. +// The MachNumber, temperature and pressure are fixed. //int inflowParaType = 6; -//double refDimensionalTemperature = 293; +//double refDimensionalTemperature = 293.0; //double refDimensionalPressure = 8886.06; +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; + 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. @@ -342,35 +366,41 @@ 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. +double knudsenLength = 1.0; // unit of meter. double refMolecularWeight = 28.9644; // unit of g/mol. //----------------------------------------------------------------------- # Spatial Discretisation # //----------------------------------------------------------------------- -#******************************************************************* -# Struct Solver * -#******************************************************************* +#************************************************************************ +# 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". +// -- "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. +// -- "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"; -string str_limiter_name = "vanalbada"; +int isWennScheme = 0; +string str_limiter_name = "vanalbada"; -#******************************************************************* -# UnStruct Solver or Common * -#******************************************************************* +#************************************************************************ +# UnStruct Solver or Common * +#************************************************************************ // viscousType: Viscous model. -// 0 -- Euler. -// 1 -- Lamilar. -// 2 -- Algebraic. -// 3 -- 1eq turbulent. -// 4 -- 2eq turbulent. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. // viscousName: Laminar or tubulent model. // -- "0eq-bl". // -- "1eq-sa". @@ -389,16 +419,16 @@ string str_limiter_name = "vanalbada"; // 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". +// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // uns_limiter_name: Limiter of Unstruct grid. -// -- "barth", "vencat", "vanleer", "minmod". -// -- "vanalbada", "smooth", "nnd", "lpz", "1st". +// -- "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". // gradientName: Gradient reconstruction method. -// -- "default", "ggcell", "ggnode", "lsq". +// -- "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. @@ -421,17 +451,18 @@ 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; +//int viscousType = 0; //string viscousName = "Euler"; -//int viscousType = 1; +//int viscousType = 1; //string viscousName = "laminar"; -int viscousType = 3; +int viscousType = 3; string viscousName = "1eq-sa"; -//int viscousType = 4; +//int viscousType = 4; //string viscousName = "2eq-kw-menter-sst"; int DESType = 0; @@ -441,7 +472,7 @@ string uns_limiter_name = "vencat"; string uns_vis_name = "test"; string gradientName = "ggnode"; -int ivencat = 7; +int ivencat = 7; double venkatCoeff = 5.0; int reconmeth = 1; int limitVariables = 0; @@ -451,9 +482,11 @@ double skewnessAngle = 60.0; int roeEntropyFixMethod = 3; double roeEntropyScale = 1.0; -//----------------------------------------------------------------------- -# Temporal Discretisation # -//----------------------------------------------------------------------- +double AusmpwPlusLimiter = 1.0; + +#************************************************************************ +# Temporal Discretisation * +#************************************************************************ // iunsteady: Steady or unsteady. // 0 -- steady. // 1 -- unsteay. @@ -466,80 +499,101 @@ 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 = - ^2 - 1 --tau = +// 0 -- tau = - ^2 +// 1 -- tau = // 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. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 4 -- LU-SGS. +// 5 -- Block LU-SGS. +// 6 -- Jacobian iteration. +// 7 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. // 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. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. // 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. +// 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. -// 0 -- no ALE method. -// 1 -- ALE method for non-moving grids. -// 2 -- ALE method for moving grids. -// 3 -- ALE method for deforming grids. +// 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. +// 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; +int iunsteady = 0; double physicalTimeStep = 0.01; +double physicalTimeStepDimensional = -0.001; int ifStartFromSteadyResults = 0; int ifStaticsFlowField = 0; int ifStaticsReynoldsStress = 0; int startStatisticStep = 800000; double statisticalTimePeriod = -1.0; int statisticMethod = 0; -int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2; +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 tscheme = 4; int iSimplifyViscousTerm = 1; int ifLocalTimeStep = 0; -double CFLStart = 0.01; -double CFLEnd = 10.0; -int CFLVaryStep = 500; +int isUseLocalCFL = 0; +int isUsePreTwall = 0; +double CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; +double pMaxForCFL = 0.2; +double pMinForCFL = 0.1; +double deltaMaxForCFL = 0.2; +double magnifyFactorForCFL = 1.1; +double reduceFactorForCFL = 0.5; -double ktmax = 1.0e10; +double ktmax = 1.0e10; -int swapDq = 1; +int swapDq = 1; int nLUSGSSweeps = 1; double LUSGSTolerance = 0.01; -int order = 2; +int order = 2; double visl_min = 0.01; double turbCFLScale = 1.0; -double csrv = 2.0; +double csrv = 1.0; double timemax = 1.0e10; double dtsave = -1.0; int maxale = 10; @@ -548,17 +602,16 @@ 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; //int RKStage = 4; //double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; - -//----------------------------------------------------------------------- -# File In or Out # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. @@ -575,32 +628,48 @@ double lamda[] = 0.5, 1.0; // 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. +// 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. +// 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 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"; +string transitionResFile = "results/transitionRes.dat"; string aircoeffile = "results/aircoef.dat"; string restartNSFile = "results/flow.dat"; string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; string visualfile = "results/tecflow.plt"; string wall_aircoefile = "results/wall_aircoef.dat"; string samplefile = "results/sample.dat"; -int nDumpSurfaceInfo = 0; -string wall_varfile = ""; +string protectionFile0 = "results/flow0.dat"; +string protectionFile1 = "results/flow1.dat"; +string wall_heatfluxfile = "results/wall_heatflux.dat"; -string jetDefineFile = "bin/jet.hypara"; +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; + +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; string sixDofFileName = "results/sixDofInfo.dat"; string derivativeFileName = "results/identify.dat"; @@ -611,7 +680,8 @@ int plotFieldType = 0; // visualfileType: The file type of visualfile. // 0 -- Tecplot binary. // 1 -- Tecplot ASCII. - +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. int visualfileType = 1; // samplefileMode: The dump mode of sample file. @@ -648,22 +718,22 @@ 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). -// -- specific heat ratio(gama, 56) +// -- 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), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. //-----------the optional parameters list for the wall boundary condition---------------- // nVisualWallVariables: The number of visual variables on wall. // visualWallVariables : dumped variable types, listed as following: -// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4), -// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8), -// -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) - +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- 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), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). int nVisualVariables = 8; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; @@ -691,16 +761,18 @@ 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), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). // 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. +// 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; +int dataMonitorType = 0; string probesDefineFile = "bin/probes_XYZ.dat"; //int dataMonitorType = 1; @@ -713,24 +785,26 @@ string probesDefineFile = "bin/probes_XYZ.dat"; int searchCellsMethod = 0; -int nProbeVariables = 6; -int probeVariables[] = [0, 1, 2, 3, 4, 5]; -int probeVariablesInterpolationMethod = 0; -//----------------------------------------------------------------------- -# Turbulence Parameter # -//----------------------------------------------------------------------- +int nProbeVariables = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +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. - +// 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; 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; @@ -741,25 +815,25 @@ double freeDecayXLocation = 0.0; int compressibleCorrection = 0; int transitionMaFix = 1; -# maximum eddy viscosity (myt/my) max. +// maximum eddy viscosity (myt/my) max. double eddyViscosityLimit = 1.0e10; int monitor_vistmax = 0; -//----------------------------------------------------------------------- -# LES Parameter # -//----------------------------------------------------------------------- +#************************************************************************ +# LES Parameter * +#************************************************************************ // iLES: Create LESSolver or not. -// == 1 - Create LESSolver; -// != 1 - 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. +// = 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. +// = 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. @@ -767,23 +841,22 @@ int monitor_vistmax = 0; // = "dsmCom"; // = "wale"; // = "sigma". -// 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. +// 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. +// = 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. +// 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; @@ -799,18 +872,16 @@ double testFilterScale = 2.0; int averageWidth = 1; int monitorNegativeConstant = 0; -//----------------------------------------------------------------------- -# Other Parameters for Hypersonic Non-equilibrium Gas # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. @@ -821,35 +892,33 @@ int monitorNegativeConstant = 0; // 2 -- Argon. // 3 -- Nitrogen. // nEnergyRecycle: The type of EnergyModel Recycle. -// 0 -- not used . +// 0 -- not used. // 1 -- used. // nDensityModify: The type of densitymodify. - // 0 -- not used. // 1 -- used. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. -// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. // 0 -- perfect gas. // 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. -// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. -// the value equals to or is greater than 1, and 3 is for default value. -// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. -// the value equals to or is greater than 1, and 3 is for default value. -// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. -// the value equals to or is greater than 1, and 3 is for default value. -// nSlipBCModel : The computational model of slip boundary conditions. - -// 0 -- no slip. -// 1 -- the conventional Maxwell slip conditions. -// 2 -- the Gokcen slip conditions. -// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. -// 4 -- the Kogan simplified slip conditions. -// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. -// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). -// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. -// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). // nchemsrc: // 0 -- the source terms are not computed. // 1 -- the source terms are computed. @@ -860,99 +929,175 @@ int monitorNegativeConstant = 0; // 1 -- One-temperature model. // 2 -- Two-temperature model. // 3 -- Three-temperature model. -// nTEnergyModel: the method to computing temperature energy model. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. +// 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: -// 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. -// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. -// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. -// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. -// 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. +// 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. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// 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]. // velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. -// 1.0 -- proposed by Maxwell. -// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. -// 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]. -// 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 -// nDebug: cout the Wrong place and abort -// 0 -- not used. -// 1 -- used. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// 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. // nSpeciesLimit: limitter of gas species -// 0 -- not used. -// 1 -- used. -// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction -// 0 -- method 0. -// 1 -- method 1. -// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid -// 0 -- not used. -// 1 -- used. -// nChemcalSourceModified: Modified on ChemcalSource -// 0 -- not used. -// 1 -- used. +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// 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 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. // nAblation: -// 0 -- The wall ablation is not computed. -// 1 -- The wall ablation is computed. +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. // isInjection: -// 0 -- The injection velocity of ablation wall is not computed. -// 1 -- The injection velocity of ablation wall is computed. +// 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. +// 0 -- stands for selecting the Blotter curve fits mode. +// 1 -- stands for Sutherland relation. // 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. -// "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. -// For self-definition model, the gasfile is used to indicate the file path of the new gas model. +// "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. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "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. +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. int dg_high_order = 0; int iapplication = 0; -int iCodeBranch = 0; -int nm = 5; +int isAdaptiveSolver = 0; +int nm = 5; int nEquilibriumGas = 0; -int nPCWCycleStep = 3; -int nRETCycleStep = 3; -int nSLIPCycleStep= 3; +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; -double prt = 0.90; -double sc_l = 0.5; -double sc_t = 0.5; +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 nGasModel = 0; +int nchem = 0; +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 +1105,11 @@ 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; @@ -968,25 +1118,50 @@ double sigmaTemperature = 1.0; double sigmaMassFraction = 1.0; double velocitySlipCorrectConstant = 1.0; -double chemicalRelaxCorf = 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 iniSpeedMode = 0; -int nAblation = 0; -int isInjection = 0; -int nViscosityModel = 0; -int nMarsModel = 0; -string gasfile = "DK5"; -//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +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 nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; + +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; string speciesName = "O, O2, NO, N, N2"; string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; @@ -1000,16 +1175,16 @@ 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"; -//string gasfile = "Combustion-12"; +//string gasfile = "Combustion-12"; //string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; //string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; //string gasfile = "Gas-Mixture"; -//string speciesName ="SpeciesA, SpeciesB"; +//string speciesName = "SpeciesA, SpeciesB"; //string initMassFraction = "1.0, 0.0"; int nSutherland = 0; double gamaSpeciesA = 1.4; @@ -1017,8 +1192,21 @@ double gamaSpeciesB = 1.3; double molecularWeightSpeciesA = 29.0; double molecularWeightSpeciesB = 30.0; -int nChemicalFlowStep = 0; -int ifStartFromPerfectGasResults = 0; +//string gasfile = "Gas-Mixture"; +//string speciesName = "O2, N2"; +//string initMassFraction = "1.0, 0.0"; + +int nFraction = 0; +int nContinueModel = 0; +int nChemicalFlowStep = 0; +int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; ######################################################################### // Multi-Grid parameters. @@ -1039,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0; // 1 -- zero order. // 2 -- first-order. (default) // mgCorrectionLimit: Multi-grid correction limit. - int nMGLevel = 1; int MGCoarsestIteration = 1; int MGPreIteration = 1; @@ -1061,20 +1248,20 @@ 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"; +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 # -######################################################################### +#************************************************************************ +# High Order Struct Solver * +#************************************************************************ // isFVMOrFDM: -// 0 -- NSSolverStruct using Finite Volume Method. -// 1 -- NSSolverStruct using Finite Differ Method. +// 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) @@ -1116,64 +1303,93 @@ int allReduceStep = 1; // codeOfOversetGrid: Overlapping(overset) grid or not. // 0 -- NON-overlapping grid. // 1 -- Overlapping grid. -// oversetInterpolationMethod: the method of overset interpolation while field simulation +// oversetInterpolationMethod: the method of overset interpolation while field simulation. // 0 -- set the acceptor cell value by donor cell value. // 1 -- set the acceptor cell value by distance weight of donor cell value. - -int codeOfOversetGrid = 0; -int oversetInterpolationMethod = 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/iblank.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; +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; // ----------------- ALE configuration ------------------------------ -int codeOfAleModel = 1; +int codeOfAleModel = 0; int aleStartStrategy = -1; -int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd; -int strategyForGCLSource = 0; //0-present; 1-Ahn; +double referenceLength = 1.0; +double referenceVelocity = 1.0; +double referenceDensity = 1.0; -//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton +int strategyForFaceNormalVelocity = 0; // 0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd. +int strategyForGCLSource = 0; // 0-present; 1-Ahn. + +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. int methodForKineticEquation = 0; double relaxParameterOfKinetic = 1.0; -######################################################################### -# motive information # -######################################################################### +#************************************************************************ +# motive information * +#************************************************************************ int numberOfMovingBodies = 1; ############################## body0 ############################## -//mass of parts -double mass_0 = 1.0; -//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz -double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; -//initial six DOF position information of parts. xc yc zc -double massCenter_0[] = 0.0 , 0.0, 0.0; -//initial six DOF position information of parts. angleX angleY angleZ -double attitudeAngle_0[] = 0.0 , 0.0, 0.0; -//initial six DOF move information of parts. vc vy vz -double massCenterVelocity_0[] = 0.0, 0.0, 0.0; -//initial six DOF move information of parts. omigX omigY omigZ -double angularVelocity_0[] = 0.0, 0.0, 0.0; -//the object that the parts belong to. -int fartherIndex_0 = -1; -//the assembly position of the parts. xc yc zc angleX angleY angleZ -double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0; -//the move pattern of the parts. +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. // -1 given motion partten. // 0 still. // 1 six DOF motion. @@ -1184,37 +1400,68 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 // 14 forced pitch motion. // 15 forced yaw motion. // 16 forced roll motion. -int RBDMethod_0 = 0; -double amplitude_0 = 0.0; -double reduceFrequency_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 ; -//additional moment of Force (system axis) mX mY mZ -double addedMoment_0[] = 0.0 ,0.0 ,0.0 ; -//the deformation method of the parts. -int morphing_0 = 0; - -// post indentify -int integralOrder = 4; +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"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; +// post indentify. +int integralOrder = 4; // ---------------- ATP read -------------------------------------------- -//@int inflowParaType = 0; +//@int inflowParaType = 0; //@double refReNumber = 6.5e6; //@double refDimensionalTemperature = 288.15; //@double freestream_vibration_temperature = 300.00; -//@double refDimensionalPressure = 0; -//@double height = 0; -//@int nsubsonicInlet = 0; -//@int nsubsonicOutlet = 0; -//@string inLetFileName = "./bin/subsonicInlet.hypara"; -//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; //@double refDimensionalVelocity = 0; //@double refDimensionalDensity = 0; - -######################################################################### -# Old Parameter # -######################################################################### +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ int isPlotVolumeField = 0; +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; + +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; + +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ +int isSolveEnergyEquation = 0; +int isSolveTurbEquation = 0; +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/grid_para.hypara b/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/grid_para.hypara index d81e67a..d7a5b01 100644 --- a/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/grid_para.hypara +++ b/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/grid_para.hypara @@ -2,29 +2,41 @@ # 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. +// 0 -- Unstructured grid. +// 1 -- Structured grid. +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. // from_gtype: Type of grid data type in grid conversion process. -// -1 -- MULTI_TYPE. -// 1 -- PHengLEI, *.fts. -// 2 -- CGNS, *.cgns. -// 3 -- Plot3D type of structured grid, *.dat/*.grd. -// 4 -- Fieldview type of unstructured grid, *.dat/*.inp. -// 5 -- Fluent, *.cas/*.msh. -// 6 -- Ustar, mgrid.in. -// 7 -- Hybrid, include both of unstructured and structured grid, *.fts. -// 8 -- GMSH, *.msh. -int gridtype = 1; -int axisup = 1; -int from_gtype = 3; +// -1 -- MULTI_TYPE +// 1 -- HyperFLOW( PHengLEI ), *.fts. +// 2 -- CGNS, *.cgns. +// 3 -- Plot3D type of structured grid, *.dat/*.grd. +// 4 -- Fieldview type of unstructured grid, *.dat/*.inp. +// 5 -- Fluent, *.cas/*.msh. +// 6 -- Ustar, mgrid.in. +// 7 -- Hybrid, include both of unstructured and structured grid, *.fts. +// 8 -- GMSH, *.msh. +int gridtype = 1; +int nAxisRotateTimes = 1; +int axisRotateOrder[] = [1]; +double axisRotateAngles[] = [90.0]; +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/updatedgrid.grd"; -string out_gfile = "./grid/updatedgrid.fts"; +int numberOfGridFile = 4; +string from_gfile = "./grid/wing.cgns"; +string from_gfile1 = "./grid/missile1.cgns"; +string from_gfile2 = "./grid/missile2.cgns"; +string from_gfile3 = "./grid/missile3.cgns"; + + + + diff --git a/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/key.hypara b/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/key.hypara index 7b8a76d..7ffb08a 100644 --- a/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/key.hypara +++ b/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/key.hypara @@ -18,34 +18,36 @@ string defaultParaFile = "./bin/cfd_para.hypara"; int ndim = 3; int nparafile = 1; -int nsimutask = 0; +//int nsimutask = 0; //string parafilename = "./bin/cfd_para_subsonic.hypara"; -string parafilename = "./bin/cfd_para_transonic.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"; +//string parafilename1 = "./bin/overset_config.hypara"; +//string parafilename2 = "./bin/kinetic_para.hypara"; -//int nsimutask = 1; -//string parafilename = "./bin/grid_para.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 = 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"; //int nsimutask = 14; //string parafilename = "./bin/integrative_solver.hypara"; -//int nsimutask = 22; -//string parafilename = "./bin/grid_para.hypara"; - //int nsimutask = 99; //string parafilename = "./bin/post_processing.hypara"; diff --git a/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/overset.txt b/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/overset.txt deleted file mode 100644 index 863e15c..0000000 --- a/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/overset.txt +++ /dev/null @@ -1,17 +0,0 @@ -int taskSelector = 1; - -int codeOfLargeScale = 0; -int numberOfMultigrid = 1; -int numberOfProcessors = 8; - -string originalGridFile = "./grid/duodan.grd"; -string originalBoundaryFile = "./grid/duodan.inp"; - -int numberOfGridGroups = 4; -int zoneSpan[numberOfGridGroups] = 34,34,34,32; - -int solidBcSize = 4; -int solidColorList[solidBcSize] = 2,11,12,13; - -int outerBcSize = 1; -int outerColorList[outerBcSize] = 8; diff --git a/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/overset_config.hypara b/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/overset_config.hypara new file mode 100644 index 0000000..9b23a21 --- /dev/null +++ b/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/overset_config.hypara @@ -0,0 +1,36 @@ +// ----------------- overlap configuration ------------------------------ +// numberOfGridGroups: The number of grid groups. +// codeOfOversetGrid: Overlapping(overset) grid or not. +// 0 -- NON-overlapping grid. +// 1 -- Overlapping grid. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in + the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid +// 0 -- no. +// 1 -- yes. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. + +int numberOfGridGroups = 4; +string gridfile = "./grid/wing__8.fts"; +string gridfile1 = "./grid/missile1__8.fts"; +string gridfile2 = "./grid/missile2__8.fts"; +string gridfile3 = "./grid/missile3__8.fts"; +int codeOfOversetGrid = 1; +int symetryOrNot = 0; +double walldistMainZone = 1.0; +double toleranceForOversetSearch = 1.0e-5; +double toleranceForOversetBox = 1.0e-5; + +int twoOrderInterpolationOrNot = 0; +int keyEnlargeOfActiveNodes = 0; +int oversetInterpolationMethod = 1; +int outTecplotOverset = 1; +int outPutOversetVisualization = 0; diff --git a/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/partition.hypara b/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/partition.hypara new file mode 100644 index 0000000..57686d3 --- /dev/null +++ b/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/partition.hypara @@ -0,0 +1,30 @@ +// 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 numberOfGridFile = 4; +int pgridtype = 1; +int pgridtype1 = 1; +int pgridtype2 = 1; +int pgridtype3 = 1; +int maxproc = 8; +int maxproc1 = 8; +int maxproc2 = 8; +int maxproc3 = 8; + +string original_grid_file = "./grid/wing.fts"; +string original_grid_file1 = "./grid/missile1.fts"; +string original_grid_file2 = "./grid/missile2.fts"; +string original_grid_file3 = "./grid/missile3.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/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/三维多弹结构重叠网格算例说明文档.pdf b/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/三维多弹结构重叠网格算例说明文档.pdf deleted file mode 100644 index 7f43491..0000000 Binary files a/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/三维多弹结构重叠网格算例说明文档.pdf and /dev/null differ diff --git a/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/结构三维多弹网格重叠装配_算例说明文档.pdf b/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/结构三维多弹网格重叠装配_算例说明文档.pdf new file mode 100644 index 0000000..a03c668 Binary files /dev/null and b/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/结构三维多弹网格重叠装配_算例说明文档.pdf differ diff --git a/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/补充说明.txt b/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/补充说明.txt deleted file mode 100644 index 24b3bee..0000000 --- a/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/补充说明.txt +++ /dev/null @@ -1,2 +0,0 @@ -针对本算例，风雷代码cmake构建的时候需要勾选USE_OVERSET选项！！！ -该算例当前只支持2171版本 \ No newline at end of file diff --git a/F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU/bin/cfd_para.hypara b/F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU/bin/cfd_para.hypara index c344658..f903a5a 100644 --- a/F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU/bin/cfd_para.hypara +++ b/F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU/bin/cfd_para.hypara @@ -8,23 +8,24 @@ // Platform for Hybrid Engineering Simulation of Flows + // China Aerodynamics Research and Development Center + // (C) Copyright, Since 2010 + +// PHengLEI 2212 + //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ########################################################################### # 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. -// 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. +// 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. +// 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. @@ -46,19 +47,24 @@ 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. -int axisup = 1; +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; // 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; +int omitRepeatInterface = 1; //----------------------------------------------------------------------- # Grid data type # @@ -87,10 +93,9 @@ 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. int numberOfGridFile = 1; -string from_gfile = "./grid/rae2822_hybrid2d.cas"; -string from_gfile1= ""; - -string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; // ----------------- some advanced choices ------------------------------ // iunsteady: The Grid is for unsteady simulation or not. @@ -103,9 +108,9 @@ 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"; +// 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; @@ -119,31 +124,31 @@ string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp"; // 0 -- Not. (default) // 1 -- Yes. // geometryUnit: Geometry unit. -// 1 -- meter. -// 2 -- millimeter. -// 3 -- inch. +// 1 -- meter. +// 2 -- millimeter. +// 3 -- inch. // exclusiveCase: Parallel projection exclusive case. -// 0 -- NON case. -// 1 -- JSM-C2-NPOFF case. -// 2 -- CHNT. +// 0 -- NON case. +// 1 -- JSM-C2-NPOFF case. +// 2 -- CHNT. // projectOrgPoint: If the original wall points need to be projected or not. -int anisoRefine = 0; -int geometryUnit = 1; -int isProject = 0; -int readDist = 0; -int isDeform = 0; +int anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; int exclusiveCase = 0; int projectOrgPoint = 0; string geometryFileName = "./grid/jsm.igs"; // ----------------- Grid Deform Parameters ----------------------------- // deformationMethod: Grid Deform. -// 1 -- SPRING. -// 2 -- RBF. +// 1 -- SPRING. +// 2 -- RBF. // stationalGridFile: Original grid file. // visualFileName : The visualization file path of deform grid. // nDeformStep : The max deform step. -// flapAngle : The max flap angle. +// flapAngle : The max flap angle. // rotatePostionZ : Rotate postion. // rotatePostionY : Rotate postion. // gridSlice : If dump slice grid. @@ -163,10 +168,10 @@ int sliceAxis = 1; double slicePosition = 13; // ----------------- RBF Parameters ------------------------------------- -// numberOfReferenceCP : Number of reference Control Points. -// influencePara : The RBF influence radius parameter. +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. int numberOfReferenceCP = 40; -double influencePara = 25.0; +double influencePara = 25.0; // ----------------- Periodic Parameters -------------------------------- // Notice: Rotational periodicity only support rotation along the X axis! @@ -178,9 +183,8 @@ double influencePara = 25.0; which only support one direction. // rotationAngle: The relative angle between two periodic face. which is recorded in degrees. - int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; +double translationLength[] = [0.0, 0.0, 0.0]; double rotationAngle = 0.0; ######################################################################### @@ -192,7 +196,6 @@ double rotationAngle = 0.0; // 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; @@ -201,20 +204,20 @@ int numberOfMultifile = 1; // 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. +// cellIndexOfMark : the cell index of mark, only for structured grid partition. int traceMark = 0; int blockIndexOfMark = 0; -int cellIndexOfMark[] = [185,30,1]; +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; +// parallelStrategy: +// 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). +// 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"; @@ -232,11 +235,10 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts"; // 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; +double parmetisBalance = 1.05; // numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. // 1 -- single level. @@ -248,29 +250,35 @@ 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. +// 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; +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; int intervalStepSample = 1000; -int intervalStepForce = 100; -int intervalStepRes = 10; -int ifLowSpeedPrecon = 0; +int intervalStepForce = 100; +int intervalStepRes = 10; // compressible: // 0 -- incompressible flow. // 1 -- compressible flow. (default) int compressible = 1; +// 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) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 1; + //----------------------------------------------------------------------- # CFD Control Parameter # //----------------------------------------------------------------------- @@ -281,33 +289,36 @@ int compressible = 1; // 0 -- the nondimensional conditions. // 1 -- the flight conditions. // 2 -- the experiment conditions. -// 3 -- the subsonic boundary conditions. +// 3 -- the subsonic boundary conditions. (Useless!) // 4 -- the condition that the velocity, temperature and density are given. // 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 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. +// 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 = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. // forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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. -// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol. +// 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; +int directionMethod = 0; double refMachNumber = 0.73; double attackd = 2.79; double angleSlide = 0.00; +int flowInitMethod = 0; int inflowParaType = 0; double refReNumber = 6.5e6; @@ -321,29 +332,27 @@ double freestream_vibration_temperature = 300.00; //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; - -//The velocity, temperature and density are fixed. +// The velocity, temperature and density are fixed. //int inflowParaType = 4; //double refDimensionalVelocity = 1000.0; -//double refDimensionalDensity = 1.0e3; +//double refDimensionalDensity = 1.0e3; -//The velocity, temperature and pressure are fixed. +// The velocity, temperature and pressure are fixed. //int inflowParaType = 5; //double refDimensionalVelocity = 1000.0; //double refDimensionalPressure = 1.0e5; -//The MachNumber, temperature and pressure are fixed. +// The MachNumber, temperature and pressure are fixed. //int inflowParaType = 6; -//double refDimensionalTemperature = 293; +//double refDimensionalTemperature = 293.0; //double refDimensionalPressure = 8886.06; +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; + double wallTemperature = -1.0; double radiationCoef = 0.8; @@ -357,41 +366,41 @@ 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. +double knudsenLength = 1.0; // unit of meter. double refMolecularWeight = 28.9644; // unit of g/mol. //----------------------------------------------------------------------- # Spatial Discretisation # //----------------------------------------------------------------------- -#******************************************************************* -# Struct Solver * -#******************************************************************* +#************************************************************************ +# 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". +// -- "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. +// 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" - +// -- "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"; +string str_limiter_name = "vanalbada"; -#******************************************************************* -# UnStruct Solver or Common * -#******************************************************************* +#************************************************************************ +# UnStruct Solver or Common * +#************************************************************************ // viscousType: Viscous model. -// 0 -- Euler. -// 1 -- Lamilar. -// 2 -- Algebraic. -// 3 -- 1eq turbulent. -// 4 -- 2eq turbulent. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. // viscousName: Laminar or tubulent model. // -- "0eq-bl". // -- "1eq-sa". @@ -410,16 +419,16 @@ string str_limiter_name = "vanalbada"; // 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". +// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // uns_limiter_name: Limiter of Unstruct grid. -// -- "barth", "vencat", "vanleer", "minmod". -// -- "vanalbada", "smooth", "nnd", "lpz", "1st". +// -- "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". // gradientName: Gradient reconstruction method. -// -- "default", "ggcell", "ggnode", "lsq". +// -- "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. @@ -442,18 +451,18 @@ 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 +// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0. -//int viscousType = 0; +//int viscousType = 0; //string viscousName = "Euler"; -//int viscousType = 1; +//int viscousType = 1; //string viscousName = "laminar"; -int viscousType = 3; +int viscousType = 3; string viscousName = "1eq-sa"; -//int viscousType = 4; +//int viscousType = 4; //string viscousName = "2eq-kw-menter-sst"; int DESType = 0; @@ -463,7 +472,7 @@ string uns_limiter_name = "vencat"; string uns_vis_name = "test"; string gradientName = "ggnode"; -int ivencat = 7; +int ivencat = 7; double venkatCoeff = 5.0; int reconmeth = 1; int limitVariables = 0; @@ -475,9 +484,9 @@ double roeEntropyScale = 1.0; double AusmpwPlusLimiter = 1.0; -//----------------------------------------------------------------------- -# Temporal Discretisation # -//----------------------------------------------------------------------- +#************************************************************************ +# Temporal Discretisation * +#************************************************************************ // iunsteady: Steady or unsteady. // 0 -- steady. // 1 -- unsteay. @@ -490,51 +499,57 @@ double AusmpwPlusLimiter = 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 = - ^2 -// 1 -- tau = +// 0 -- tau = - ^2 +// 1 -- tau = // 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 -- Line LU-SGS. -// 8 -- Matrix LU-SGS. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 4 -- LU-SGS. +// 5 -- Block LU-SGS. +// 6 -- Jacobian iteration. +// 7 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. // 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. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. // 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. +// 0 --Local. +// 1 --Global. // isUseLocalCFL: use variable number of CFL or not. -// 0 -- global unified CFL number. -// 1 -- local CFL number. +// 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. -// 0 -- no ALE method. -// 1 -- ALE method for non-moving grids. -// 2 -- ALE method for moving grids. -// 3 -- ALE method for deforming grids. +// 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. +// 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; +int iunsteady = 0; double physicalTimeStep = 0.01; double physicalTimeStepDimensional = -0.001; int ifStartFromSteadyResults = 0; @@ -543,39 +558,42 @@ int ifStaticsReynoldsStress = 0; int startStatisticStep = 800000; double statisticalTimePeriod = -1.0; int statisticMethod = 0; -int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2; +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 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 CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; double pMaxForCFL = 0.2; double pMinForCFL = 0.1; double deltaMaxForCFL = 0.2; double magnifyFactorForCFL = 1.1; double reduceFactorForCFL = 0.5; -double ktmax = 1.0e10; +double ktmax = 1.0e10; -int swapDq = 1; +int swapDq = 1; int nLUSGSSweeps = 1; double LUSGSTolerance = 0.01; -int order = 2; +int order = 2; double visl_min = 0.01; double turbCFLScale = 1.0; -double csrv = 2.0; +double csrv = 1.0; double timemax = 1.0e10; double dtsave = -1.0; int maxale = 10; @@ -591,10 +609,9 @@ double lamda[] = [0.5, 1.0]; //int RKStage = 4; //double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; - -//----------------------------------------------------------------------- -# File In or Out # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. @@ -611,20 +628,18 @@ double lamda[] = [0.5, 1.0]; // 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. +// 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. // 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= ""; +// 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; @@ -632,10 +647,12 @@ int cellMethodOrNodeMethod = 0; string resSaveFile = "results/res.dat"; string turbresfile = "results/turbres.dat"; +string transitionResFile = "results/transitionRes.dat"; string aircoeffile = "results/aircoef.dat"; string restartNSFile = "results/flow.dat"; string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; string visualfile = "results/tecflow.plt"; string wall_aircoefile = "results/wall_aircoef.dat"; @@ -645,10 +662,14 @@ string protectionFile0 = "results/flow0.dat"; string protectionFile1 = "results/flow1.dat"; string wall_heatfluxfile = "results/wall_heatflux.dat"; -int nDumpSurfaceInfo = 0; -string wall_varfile = ""; +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; -string jetDefineFile = "bin/jet.hypara"; +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; string sixDofFileName = "results/sixDofInfo.dat"; string derivativeFileName = "results/identify.dat"; @@ -659,7 +680,8 @@ int plotFieldType = 0; // visualfileType: The file type of visualfile. // 0 -- Tecplot binary. // 1 -- Tecplot ASCII. - +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. int visualfileType = 1; // samplefileMode: The dump mode of sample file. @@ -697,21 +719,21 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), 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) +// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. //-----------the optional parameters list for the wall boundary condition---------------- // nVisualWallVariables: The number of visual variables on wall. // visualWallVariables : dumped variable types, listed as following: -// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4), -// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8), -// -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), -Grid Reynolds number on wall(Re_w, 23) +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- 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), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). int nVisualVariables = 8; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; @@ -739,16 +761,18 @@ 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), mach(6). +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). // 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. +// 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; +int dataMonitorType = 0; string probesDefineFile = "bin/probes_XYZ.dat"; //int dataMonitorType = 1; @@ -761,28 +785,26 @@ string probesDefineFile = "bin/probes_XYZ.dat"; int searchCellsMethod = 0; -int nProbeVariables = 7; -int probeVariables[] = [0, 1, 2, 3, 4, 5, 6]; -int probeVariablesInterpolationMethod = 0; -//----------------------------------------------------------------------- -# Turbulence Parameter # -//----------------------------------------------------------------------- +int nProbeVariables = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +int probeVariablesInterpolationMethod = 0; + +#************************************************************************ +# Turbulence Parameter * +#************************************************************************ // turbInterval: Iteration number of turbulence. // kindOfTurbSource: Kinds of turbulent source. // 0 -- Original. // mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0. -// transitionType: transition model type +// 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 - - +// 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; 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; @@ -790,29 +812,28 @@ int transitionType = 0; double turbIntensity = -1.0; int freeturbIntensitySRModify = 0; double freeDecayXLocation = 0.0; -int compressibleCorrection = 0; -int prandtlNumberCorrection = 0; +int compressibleCorrection = 0; int transitionMaFix = 1; -# maximum eddy viscosity (myt/my) max. +// maximum eddy viscosity (myt/my) max. double eddyViscosityLimit = 1.0e10; int monitor_vistmax = 0; -//----------------------------------------------------------------------- -# LES Parameter # -//----------------------------------------------------------------------- +#************************************************************************ +# LES Parameter * +#************************************************************************ // iLES: Create LESSolver or not. -// = 1 - Create LESSolver; -// != 1 - 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. +// = 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. +// = 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. @@ -820,23 +841,22 @@ int monitor_vistmax = 0; // = "dsmCom"; // = "wale"; // = "sigma". -// 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. +// 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. +// = 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. +// 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; @@ -852,19 +872,16 @@ double testFilterScale = 2.0; int averageWidth = 1; int monitorNegativeConstant = 0; -//----------------------------------------------------------------------- -# Other Parameters for Hypersonic Non-equilibrium Gas # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. -// 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. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. @@ -875,7 +892,7 @@ int monitorNegativeConstant = 0; // 2 -- Argon. // 3 -- Nitrogen. // nEnergyRecycle: The type of EnergyModel Recycle. -// 0 -- not used . +// 0 -- not used. // 1 -- used. // nDensityModify: The type of densitymodify. // 0 -- not used. @@ -883,26 +900,25 @@ int monitorNegativeConstant = 0; // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. -// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. // 0 -- perfect gas. // 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. -// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. -// the value equals to or is greater than 1, and 3 is for default value. -// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. -// the value equals to or is greater than 1, and 3 is for default value. -// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. -// the value equals to or is greater than 1, and 3 is for default value. -// nSlipBCModel : The computational model of slip boundary conditions. - -// 0 -- no slip. -// 1 -- the conventional Maxwell slip conditions. -// 2 -- the Gokcen slip conditions. -// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. -// 4 -- the Kogan simplified slip conditions. -// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. -// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). -// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. -// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). // nchemsrc: // 0 -- the source terms are not computed. // 1 -- the source terms are computed. @@ -913,148 +929,151 @@ int monitorNegativeConstant = 0; // 1 -- One-temperature model. // 2 -- Two-temperature model. // 3 -- Three-temperature model. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. // 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. +// 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 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: -// 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. -// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. -// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. -// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. -// 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. +// 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. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// 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]. // velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. -// 1.0 -- proposed by Maxwell. -// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. -// 1.146 -- proposed for an additional "fictitious" velocity slip. - -// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. -// 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. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// 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. // nSpeciesLimit: limitter of gas species -// 0 -- not used. -// 1 -- used. -// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction -// 0 -- method 0. -// 1 -- method 1. -// 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) - +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// 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 +// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs. +// 0 -- not used. +// 1 -- used. +// nDiagonalModified: Modified on Diagonal. +// 0 -- not used. +// 1 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. // nAblation: -// 0 -- The wall ablation is not computed. -// 1 -- The wall ablation is computed. +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. // isInjection: -// 0 -- The injection velocity of ablation wall is not computed. -// 1 -- The injection velocity of ablation wall is computed. +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. // nViscosityModel: -// 0 -- Blottner fitting method(N89). -// 1 -- Gupta fitting method(N90). +// 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. +// 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. +// 0 -- stands for selecting the Blotter curve fits mode. +// 1 -- stands for Sutherland relation. // 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. -// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. -// "Gas-Mixture" -- indicates the process of mixing gas without reacting. -// for struct solver mixing two speciesSpeciesA, SpeciesB. -// for unstruct solver mixing multi-speciesO2 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. +// "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. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "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. +// 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. +// 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 - +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. int dg_high_order = 0; int iapplication = 0; int isAdaptiveSolver = 0; -int nm = 5; +int nm = 5; int nEquilibriumGas = 0; -int nPCWCycleStep = 3; -int nRETCycleStep = 3; -int nSLIPCycleStep= 3; +int nPCWCycleStep = 3; +int nRETCycleStep = 3; +int nSLIPCycleStep = 3; int nIterFirstStep = 1000; int nIterSecondStep= 2000; int nIterThirdStep = 2000; @@ -1065,17 +1084,17 @@ double secondStepError = 0.001; double thirdStepError = 0.001; double predictCFLError = 0.1; -double refGama = 1.4; -double prl = 0.72; -double prt = 0.90; -double sc_l = 0.5; -double sc_t = 0.5; +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 nGasModel = 0; +int nchem = 0; +int nchemsrc = 1; +int nchemrad = 1; +int ntmodel = 1; int nIdealState = 0; int nEnergyRecycle = 1; @@ -1099,12 +1118,12 @@ double sigmaTemperature = 1.0; double sigmaMassFraction = 1.0; double velocitySlipCorrectConstant = 1.0; -double chemicalRelaxCorf = 1.0; +double chemicalRelaxCorf = 1.0; double chemicalSpectrumRadiusCoef = 1.0; double viscousSpectrumRadiusCoef = 1.5; double inviscidSpectrumRadiusCoef = 1.5; -double spectrumRadiusCoef = 0.5; -double staticPressureRelaxCorf = 0.2; +double spectrumRadiusCoef = 0.5; +double staticPressureRelaxCorf = 0.2; double maxViscous = 10000.0; double trTemperatureMin = 10.0; @@ -1114,31 +1133,35 @@ double densityMin = 1.0e-8; double densityMinFactor = 0.1; double tAdjustmentFactor = 10.0; double iniSpeedCoef = 1.0; +int iniSpeedMode = 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 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 nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; -int nProtectData = 0; -int useHyflowSetting = 0; -int nAblation = 0; -int isInjection = 0; -int nViscosityModel = 0; -int nMarsModel = 0; -string gasfile = "DK5"; -//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; string speciesName = "O, O2, NO, N, N2"; string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; @@ -1152,16 +1175,16 @@ 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 = "Pa"; +//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"; -//string gasfile = "Combustion-12"; +//string gasfile = "Combustion-12"; //string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; //string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; //string gasfile = "Gas-Mixture"; -//string speciesName ="SpeciesA, SpeciesB"; +//string speciesName = "SpeciesA, SpeciesB"; //string initMassFraction = "1.0, 0.0"; int nSutherland = 0; double gamaSpeciesA = 1.4; @@ -1173,9 +1196,17 @@ double molecularWeightSpeciesB = 30.0; //string speciesName = "O2, N2"; //string initMassFraction = "1.0, 0.0"; +int nFraction = 0; int nContinueModel = 0; int nChemicalFlowStep = 0; int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; ######################################################################### // Multi-Grid parameters. @@ -1196,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0; // 1 -- zero order. // 2 -- first-order. (default) // mgCorrectionLimit: Multi-grid correction limit. - int nMGLevel = 1; int MGCoarsestIteration = 1; int MGPreIteration = 1; @@ -1218,20 +1248,20 @@ 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"; +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 # -######################################################################### +#************************************************************************ +# High Order Struct Solver * +#************************************************************************ // isFVMOrFDM: -// 0 -- NSSolverStruct using Finite Volume Method. -// 1 -- NSSolverStruct using Finite Differ Method. +// 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) @@ -1273,30 +1303,48 @@ int allReduceStep = 1; // codeOfOversetGrid: Overlapping(overset) grid or not. // 0 -- NON-overlapping grid. // 1 -- Overlapping grid. -// oversetInterpolationMethod: the method of overset interpolation while field simulation +// oversetInterpolationMethod: the method of overset interpolation while field simulation. // 0 -- set the acceptor cell value by donor cell value. // 1 -- set the acceptor cell value by distance weight of donor cell value. - -int codeOfOversetGrid = 0; -int oversetInterpolationMethod = 0; -int readOversetFileOrNot = 0; -int symetryOrNot = 0; -int readInAuxiliaryInnerGrid = 0; -int readInAuxiliaryOuterGrid = 0; -int readInSklFileOrNot = 0; -string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; -string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; -string auxiliaryInnerGrid2 = ""; -string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; - -int numberOfMovingBodies = 2; +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; // ----------------- ALE configuration ------------------------------ int codeOfAleModel = 0; @@ -1306,36 +1354,42 @@ 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; +int strategyForFaceNormalVelocity = 0; // 0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd. +int strategyForGCLSource = 0; // 0-present; 1-Ahn. -//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. int methodForKineticEquation = 0; double relaxParameterOfKinetic = 1.0; -######################################################################### -# motive information # -######################################################################### +#************************************************************************ +# motive information * +#************************************************************************ int numberOfMovingBodies = 1; ############################## body0 ############################## -//mass of parts -double mass_0 = 1.0; -//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz -double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; -//initial six DOF position information of parts. xc yc zc -double massCenter_0[] = 0.0 , 0.0, 0.0; -//initial six DOF position information of parts. angleX angleY angleZ -double attitudeAngle_0[] = 0.0 , 0.0, 0.0; -//initial six DOF move information of parts. vc vy vz -double massCenterVelocity_0[] = 0.0, 0.0, 0.0; -//initial six DOF move information of parts. omigX omigY omigZ -double angularVelocity_0[] = 0.0, 0.0, 0.0; -//the object that the parts belong to. -int fartherIndex_0 = -1; -//the assembly position of the parts. xc yc zc angleX angleY angleZ -double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0; -//the move pattern of the parts. +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. // -1 given motion partten. // 0 still. // 1 six DOF motion. @@ -1346,51 +1400,68 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 // 14 forced pitch motion. // 15 forced yaw motion. // 16 forced roll motion. -int RBDMethod_0 = 0; -double amplitude_0 = 0.0; -double reduceFrequency_0 = 0.0; -//direction of rotation +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 ; -//additional moment of Force (system axis) mX mY mZ -double addedMoment_0[] = 0.0 ,0.0 ,0.0 ; -//the deformation method of the parts. -int morphing_0 = 0; - -// post indentify -int integralOrder = 4; +int direction_0 = -1; +double rotateFrequency_0 = 0.0; +//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; +// post indentify. +int integralOrder = 4; // ---------------- ATP read -------------------------------------------- -//@int inflowParaType = 0; +//@int inflowParaType = 0; //@double refReNumber = 6.5e6; //@double refDimensionalTemperature = 288.15; //@double freestream_vibration_temperature = 300.00; -//@double refDimensionalPressure = 0; -//@double height = 0; -//@int nsubsonicInlet = 0; -//@int nsubsonicOutlet = 0; -//@string inLetFileName = "./bin/subsonicInlet.hypara"; -//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; //@double refDimensionalVelocity = 0; //@double refDimensionalDensity = 0; - -######################################################################### -# Old Parameter # -######################################################################### +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ int isPlotVolumeField = 0; +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; -######################################################################### -# Incompressible Parameter # -######################################################################### +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ int isSolveEnergyEquation = 0; int isSolveTurbEquation = 0; -int isSolveSpeciesEquation = 0; - +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU/bin/grid_para.hypara b/F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU/bin/grid_para.hypara index 06c2e39..bdab584 100644 --- a/F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU/bin/grid_para.hypara +++ b/F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU/bin/grid_para.hypara @@ -4,9 +4,12 @@ // 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. +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. // from_gtype: Type of grid data type in grid conversion process. // -1 -- MULTI_TYPE. // 1 -- PHengLEI, *.fts. @@ -18,7 +21,9 @@ // 7 -- Hybrid, include both of unstructured and structured grid, *.fts. // 8 -- GMSH, *.msh. int gridtype = 0; -int axisup = 1; +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; int from_gtype = 2; ######################################################################### diff --git a/F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU/bin/overset_config.hypara b/F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU/bin/overset_config.hypara index a46e672..e986101 100644 --- a/F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU/bin/overset_config.hypara +++ b/F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU/bin/overset_config.hypara @@ -28,7 +28,8 @@ string gridfile2 = "./grid/lowerwing__4.fts"; int codeOfOversetGrid = 1; int readOversetFileOrNot = 0; int symetryOrNot = 0; -int readInAuxiliaryInnerGrid = 1; +int readInAuxiliaryInnerGrid = 1; +double gridScaleFactor = 0.001; string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; string oversetGridFileName = "./grid/overlap.ovs"; diff --git a/F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU/二维双NACA0012翼型非结构重叠网格装配说明文档.pdf b/F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU/二维双NACA0012翼型非结构重叠网格装配说明文档.pdf index b704a14..b37b07a 100644 Binary files a/F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU/二维双NACA0012翼型非结构重叠网格装配说明文档.pdf and b/F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU/二维双NACA0012翼型非结构重叠网格装配说明文档.pdf differ diff --git a/F04_TwoD_Dual0012_OversetGrid_InvisCal_Unstruct_4CPU/bin/cfd_para.hypara b/F04_TwoD_Dual0012_OversetGrid_InvisCal_Unstruct_4CPU/bin/cfd_para.hypara index c344658..f903a5a 100644 --- a/F04_TwoD_Dual0012_OversetGrid_InvisCal_Unstruct_4CPU/bin/cfd_para.hypara +++ b/F04_TwoD_Dual0012_OversetGrid_InvisCal_Unstruct_4CPU/bin/cfd_para.hypara @@ -8,23 +8,24 @@ // Platform for Hybrid Engineering Simulation of Flows + // China Aerodynamics Research and Development Center + // (C) Copyright, Since 2010 + +// PHengLEI 2212 + //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ########################################################################### # 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. -// 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. +// 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. +// 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. @@ -46,19 +47,24 @@ 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. -int axisup = 1; +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; // 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; +int omitRepeatInterface = 1; //----------------------------------------------------------------------- # Grid data type # @@ -87,10 +93,9 @@ 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. int numberOfGridFile = 1; -string from_gfile = "./grid/rae2822_hybrid2d.cas"; -string from_gfile1= ""; - -string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; // ----------------- some advanced choices ------------------------------ // iunsteady: The Grid is for unsteady simulation or not. @@ -103,9 +108,9 @@ 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"; +// 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; @@ -119,31 +124,31 @@ string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp"; // 0 -- Not. (default) // 1 -- Yes. // geometryUnit: Geometry unit. -// 1 -- meter. -// 2 -- millimeter. -// 3 -- inch. +// 1 -- meter. +// 2 -- millimeter. +// 3 -- inch. // exclusiveCase: Parallel projection exclusive case. -// 0 -- NON case. -// 1 -- JSM-C2-NPOFF case. -// 2 -- CHNT. +// 0 -- NON case. +// 1 -- JSM-C2-NPOFF case. +// 2 -- CHNT. // projectOrgPoint: If the original wall points need to be projected or not. -int anisoRefine = 0; -int geometryUnit = 1; -int isProject = 0; -int readDist = 0; -int isDeform = 0; +int anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; int exclusiveCase = 0; int projectOrgPoint = 0; string geometryFileName = "./grid/jsm.igs"; // ----------------- Grid Deform Parameters ----------------------------- // deformationMethod: Grid Deform. -// 1 -- SPRING. -// 2 -- RBF. +// 1 -- SPRING. +// 2 -- RBF. // stationalGridFile: Original grid file. // visualFileName : The visualization file path of deform grid. // nDeformStep : The max deform step. -// flapAngle : The max flap angle. +// flapAngle : The max flap angle. // rotatePostionZ : Rotate postion. // rotatePostionY : Rotate postion. // gridSlice : If dump slice grid. @@ -163,10 +168,10 @@ int sliceAxis = 1; double slicePosition = 13; // ----------------- RBF Parameters ------------------------------------- -// numberOfReferenceCP : Number of reference Control Points. -// influencePara : The RBF influence radius parameter. +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. int numberOfReferenceCP = 40; -double influencePara = 25.0; +double influencePara = 25.0; // ----------------- Periodic Parameters -------------------------------- // Notice: Rotational periodicity only support rotation along the X axis! @@ -178,9 +183,8 @@ double influencePara = 25.0; which only support one direction. // rotationAngle: The relative angle between two periodic face. which is recorded in degrees. - int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; +double translationLength[] = [0.0, 0.0, 0.0]; double rotationAngle = 0.0; ######################################################################### @@ -192,7 +196,6 @@ double rotationAngle = 0.0; // 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; @@ -201,20 +204,20 @@ int numberOfMultifile = 1; // 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. +// cellIndexOfMark : the cell index of mark, only for structured grid partition. int traceMark = 0; int blockIndexOfMark = 0; -int cellIndexOfMark[] = [185,30,1]; +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; +// parallelStrategy: +// 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). +// 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"; @@ -232,11 +235,10 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts"; // 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; +double parmetisBalance = 1.05; // numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. // 1 -- single level. @@ -248,29 +250,35 @@ 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. +// 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; +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; int intervalStepSample = 1000; -int intervalStepForce = 100; -int intervalStepRes = 10; -int ifLowSpeedPrecon = 0; +int intervalStepForce = 100; +int intervalStepRes = 10; // compressible: // 0 -- incompressible flow. // 1 -- compressible flow. (default) int compressible = 1; +// 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) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 1; + //----------------------------------------------------------------------- # CFD Control Parameter # //----------------------------------------------------------------------- @@ -281,33 +289,36 @@ int compressible = 1; // 0 -- the nondimensional conditions. // 1 -- the flight conditions. // 2 -- the experiment conditions. -// 3 -- the subsonic boundary conditions. +// 3 -- the subsonic boundary conditions. (Useless!) // 4 -- the condition that the velocity, temperature and density are given. // 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 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. +// 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 = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. // forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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. -// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol. +// 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; +int directionMethod = 0; double refMachNumber = 0.73; double attackd = 2.79; double angleSlide = 0.00; +int flowInitMethod = 0; int inflowParaType = 0; double refReNumber = 6.5e6; @@ -321,29 +332,27 @@ double freestream_vibration_temperature = 300.00; //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; - -//The velocity, temperature and density are fixed. +// The velocity, temperature and density are fixed. //int inflowParaType = 4; //double refDimensionalVelocity = 1000.0; -//double refDimensionalDensity = 1.0e3; +//double refDimensionalDensity = 1.0e3; -//The velocity, temperature and pressure are fixed. +// The velocity, temperature and pressure are fixed. //int inflowParaType = 5; //double refDimensionalVelocity = 1000.0; //double refDimensionalPressure = 1.0e5; -//The MachNumber, temperature and pressure are fixed. +// The MachNumber, temperature and pressure are fixed. //int inflowParaType = 6; -//double refDimensionalTemperature = 293; +//double refDimensionalTemperature = 293.0; //double refDimensionalPressure = 8886.06; +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; + double wallTemperature = -1.0; double radiationCoef = 0.8; @@ -357,41 +366,41 @@ 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. +double knudsenLength = 1.0; // unit of meter. double refMolecularWeight = 28.9644; // unit of g/mol. //----------------------------------------------------------------------- # Spatial Discretisation # //----------------------------------------------------------------------- -#******************************************************************* -# Struct Solver * -#******************************************************************* +#************************************************************************ +# 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". +// -- "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. +// 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" - +// -- "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"; +string str_limiter_name = "vanalbada"; -#******************************************************************* -# UnStruct Solver or Common * -#******************************************************************* +#************************************************************************ +# UnStruct Solver or Common * +#************************************************************************ // viscousType: Viscous model. -// 0 -- Euler. -// 1 -- Lamilar. -// 2 -- Algebraic. -// 3 -- 1eq turbulent. -// 4 -- 2eq turbulent. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. // viscousName: Laminar or tubulent model. // -- "0eq-bl". // -- "1eq-sa". @@ -410,16 +419,16 @@ string str_limiter_name = "vanalbada"; // 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". +// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // uns_limiter_name: Limiter of Unstruct grid. -// -- "barth", "vencat", "vanleer", "minmod". -// -- "vanalbada", "smooth", "nnd", "lpz", "1st". +// -- "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". // gradientName: Gradient reconstruction method. -// -- "default", "ggcell", "ggnode", "lsq". +// -- "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. @@ -442,18 +451,18 @@ 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 +// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0. -//int viscousType = 0; +//int viscousType = 0; //string viscousName = "Euler"; -//int viscousType = 1; +//int viscousType = 1; //string viscousName = "laminar"; -int viscousType = 3; +int viscousType = 3; string viscousName = "1eq-sa"; -//int viscousType = 4; +//int viscousType = 4; //string viscousName = "2eq-kw-menter-sst"; int DESType = 0; @@ -463,7 +472,7 @@ string uns_limiter_name = "vencat"; string uns_vis_name = "test"; string gradientName = "ggnode"; -int ivencat = 7; +int ivencat = 7; double venkatCoeff = 5.0; int reconmeth = 1; int limitVariables = 0; @@ -475,9 +484,9 @@ double roeEntropyScale = 1.0; double AusmpwPlusLimiter = 1.0; -//----------------------------------------------------------------------- -# Temporal Discretisation # -//----------------------------------------------------------------------- +#************************************************************************ +# Temporal Discretisation * +#************************************************************************ // iunsteady: Steady or unsteady. // 0 -- steady. // 1 -- unsteay. @@ -490,51 +499,57 @@ double AusmpwPlusLimiter = 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 = - ^2 -// 1 -- tau = +// 0 -- tau = - ^2 +// 1 -- tau = // 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 -- Line LU-SGS. -// 8 -- Matrix LU-SGS. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 4 -- LU-SGS. +// 5 -- Block LU-SGS. +// 6 -- Jacobian iteration. +// 7 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. // 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. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. // 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. +// 0 --Local. +// 1 --Global. // isUseLocalCFL: use variable number of CFL or not. -// 0 -- global unified CFL number. -// 1 -- local CFL number. +// 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. -// 0 -- no ALE method. -// 1 -- ALE method for non-moving grids. -// 2 -- ALE method for moving grids. -// 3 -- ALE method for deforming grids. +// 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. +// 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; +int iunsteady = 0; double physicalTimeStep = 0.01; double physicalTimeStepDimensional = -0.001; int ifStartFromSteadyResults = 0; @@ -543,39 +558,42 @@ int ifStaticsReynoldsStress = 0; int startStatisticStep = 800000; double statisticalTimePeriod = -1.0; int statisticMethod = 0; -int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2; +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 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 CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; double pMaxForCFL = 0.2; double pMinForCFL = 0.1; double deltaMaxForCFL = 0.2; double magnifyFactorForCFL = 1.1; double reduceFactorForCFL = 0.5; -double ktmax = 1.0e10; +double ktmax = 1.0e10; -int swapDq = 1; +int swapDq = 1; int nLUSGSSweeps = 1; double LUSGSTolerance = 0.01; -int order = 2; +int order = 2; double visl_min = 0.01; double turbCFLScale = 1.0; -double csrv = 2.0; +double csrv = 1.0; double timemax = 1.0e10; double dtsave = -1.0; int maxale = 10; @@ -591,10 +609,9 @@ double lamda[] = [0.5, 1.0]; //int RKStage = 4; //double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; - -//----------------------------------------------------------------------- -# File In or Out # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. @@ -611,20 +628,18 @@ double lamda[] = [0.5, 1.0]; // 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. +// 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. // 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= ""; +// 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; @@ -632,10 +647,12 @@ int cellMethodOrNodeMethod = 0; string resSaveFile = "results/res.dat"; string turbresfile = "results/turbres.dat"; +string transitionResFile = "results/transitionRes.dat"; string aircoeffile = "results/aircoef.dat"; string restartNSFile = "results/flow.dat"; string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; string visualfile = "results/tecflow.plt"; string wall_aircoefile = "results/wall_aircoef.dat"; @@ -645,10 +662,14 @@ string protectionFile0 = "results/flow0.dat"; string protectionFile1 = "results/flow1.dat"; string wall_heatfluxfile = "results/wall_heatflux.dat"; -int nDumpSurfaceInfo = 0; -string wall_varfile = ""; +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; -string jetDefineFile = "bin/jet.hypara"; +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; string sixDofFileName = "results/sixDofInfo.dat"; string derivativeFileName = "results/identify.dat"; @@ -659,7 +680,8 @@ int plotFieldType = 0; // visualfileType: The file type of visualfile. // 0 -- Tecplot binary. // 1 -- Tecplot ASCII. - +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. int visualfileType = 1; // samplefileMode: The dump mode of sample file. @@ -697,21 +719,21 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), 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) +// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. //-----------the optional parameters list for the wall boundary condition---------------- // nVisualWallVariables: The number of visual variables on wall. // visualWallVariables : dumped variable types, listed as following: -// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4), -// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8), -// -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), -Grid Reynolds number on wall(Re_w, 23) +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- 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), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). int nVisualVariables = 8; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; @@ -739,16 +761,18 @@ 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), mach(6). +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). // 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. +// 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; +int dataMonitorType = 0; string probesDefineFile = "bin/probes_XYZ.dat"; //int dataMonitorType = 1; @@ -761,28 +785,26 @@ string probesDefineFile = "bin/probes_XYZ.dat"; int searchCellsMethod = 0; -int nProbeVariables = 7; -int probeVariables[] = [0, 1, 2, 3, 4, 5, 6]; -int probeVariablesInterpolationMethod = 0; -//----------------------------------------------------------------------- -# Turbulence Parameter # -//----------------------------------------------------------------------- +int nProbeVariables = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +int probeVariablesInterpolationMethod = 0; + +#************************************************************************ +# Turbulence Parameter * +#************************************************************************ // turbInterval: Iteration number of turbulence. // kindOfTurbSource: Kinds of turbulent source. // 0 -- Original. // mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0. -// transitionType: transition model type +// 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 - - +// 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; 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; @@ -790,29 +812,28 @@ int transitionType = 0; double turbIntensity = -1.0; int freeturbIntensitySRModify = 0; double freeDecayXLocation = 0.0; -int compressibleCorrection = 0; -int prandtlNumberCorrection = 0; +int compressibleCorrection = 0; int transitionMaFix = 1; -# maximum eddy viscosity (myt/my) max. +// maximum eddy viscosity (myt/my) max. double eddyViscosityLimit = 1.0e10; int monitor_vistmax = 0; -//----------------------------------------------------------------------- -# LES Parameter # -//----------------------------------------------------------------------- +#************************************************************************ +# LES Parameter * +#************************************************************************ // iLES: Create LESSolver or not. -// = 1 - Create LESSolver; -// != 1 - 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. +// = 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. +// = 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. @@ -820,23 +841,22 @@ int monitor_vistmax = 0; // = "dsmCom"; // = "wale"; // = "sigma". -// 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. +// 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. +// = 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. +// 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; @@ -852,19 +872,16 @@ double testFilterScale = 2.0; int averageWidth = 1; int monitorNegativeConstant = 0; -//----------------------------------------------------------------------- -# Other Parameters for Hypersonic Non-equilibrium Gas # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. -// 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. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. @@ -875,7 +892,7 @@ int monitorNegativeConstant = 0; // 2 -- Argon. // 3 -- Nitrogen. // nEnergyRecycle: The type of EnergyModel Recycle. -// 0 -- not used . +// 0 -- not used. // 1 -- used. // nDensityModify: The type of densitymodify. // 0 -- not used. @@ -883,26 +900,25 @@ int monitorNegativeConstant = 0; // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. -// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. // 0 -- perfect gas. // 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. -// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. -// the value equals to or is greater than 1, and 3 is for default value. -// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. -// the value equals to or is greater than 1, and 3 is for default value. -// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. -// the value equals to or is greater than 1, and 3 is for default value. -// nSlipBCModel : The computational model of slip boundary conditions. - -// 0 -- no slip. -// 1 -- the conventional Maxwell slip conditions. -// 2 -- the Gokcen slip conditions. -// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. -// 4 -- the Kogan simplified slip conditions. -// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. -// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). -// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. -// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). // nchemsrc: // 0 -- the source terms are not computed. // 1 -- the source terms are computed. @@ -913,148 +929,151 @@ int monitorNegativeConstant = 0; // 1 -- One-temperature model. // 2 -- Two-temperature model. // 3 -- Three-temperature model. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. // 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. +// 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 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: -// 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. -// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. -// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. -// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. -// 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. +// 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. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// 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]. // velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. -// 1.0 -- proposed by Maxwell. -// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. -// 1.146 -- proposed for an additional "fictitious" velocity slip. - -// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. -// 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. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// 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. // nSpeciesLimit: limitter of gas species -// 0 -- not used. -// 1 -- used. -// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction -// 0 -- method 0. -// 1 -- method 1. -// 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) - +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// 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 +// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs. +// 0 -- not used. +// 1 -- used. +// nDiagonalModified: Modified on Diagonal. +// 0 -- not used. +// 1 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. // nAblation: -// 0 -- The wall ablation is not computed. -// 1 -- The wall ablation is computed. +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. // isInjection: -// 0 -- The injection velocity of ablation wall is not computed. -// 1 -- The injection velocity of ablation wall is computed. +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. // nViscosityModel: -// 0 -- Blottner fitting method(N89). -// 1 -- Gupta fitting method(N90). +// 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. +// 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. +// 0 -- stands for selecting the Blotter curve fits mode. +// 1 -- stands for Sutherland relation. // 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. -// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. -// "Gas-Mixture" -- indicates the process of mixing gas without reacting. -// for struct solver mixing two speciesSpeciesA, SpeciesB. -// for unstruct solver mixing multi-speciesO2 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. +// "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. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "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. +// 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. +// 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 - +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. int dg_high_order = 0; int iapplication = 0; int isAdaptiveSolver = 0; -int nm = 5; +int nm = 5; int nEquilibriumGas = 0; -int nPCWCycleStep = 3; -int nRETCycleStep = 3; -int nSLIPCycleStep= 3; +int nPCWCycleStep = 3; +int nRETCycleStep = 3; +int nSLIPCycleStep = 3; int nIterFirstStep = 1000; int nIterSecondStep= 2000; int nIterThirdStep = 2000; @@ -1065,17 +1084,17 @@ double secondStepError = 0.001; double thirdStepError = 0.001; double predictCFLError = 0.1; -double refGama = 1.4; -double prl = 0.72; -double prt = 0.90; -double sc_l = 0.5; -double sc_t = 0.5; +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 nGasModel = 0; +int nchem = 0; +int nchemsrc = 1; +int nchemrad = 1; +int ntmodel = 1; int nIdealState = 0; int nEnergyRecycle = 1; @@ -1099,12 +1118,12 @@ double sigmaTemperature = 1.0; double sigmaMassFraction = 1.0; double velocitySlipCorrectConstant = 1.0; -double chemicalRelaxCorf = 1.0; +double chemicalRelaxCorf = 1.0; double chemicalSpectrumRadiusCoef = 1.0; double viscousSpectrumRadiusCoef = 1.5; double inviscidSpectrumRadiusCoef = 1.5; -double spectrumRadiusCoef = 0.5; -double staticPressureRelaxCorf = 0.2; +double spectrumRadiusCoef = 0.5; +double staticPressureRelaxCorf = 0.2; double maxViscous = 10000.0; double trTemperatureMin = 10.0; @@ -1114,31 +1133,35 @@ double densityMin = 1.0e-8; double densityMinFactor = 0.1; double tAdjustmentFactor = 10.0; double iniSpeedCoef = 1.0; +int iniSpeedMode = 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 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 nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; -int nProtectData = 0; -int useHyflowSetting = 0; -int nAblation = 0; -int isInjection = 0; -int nViscosityModel = 0; -int nMarsModel = 0; -string gasfile = "DK5"; -//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; string speciesName = "O, O2, NO, N, N2"; string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; @@ -1152,16 +1175,16 @@ 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 = "Pa"; +//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"; -//string gasfile = "Combustion-12"; +//string gasfile = "Combustion-12"; //string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; //string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; //string gasfile = "Gas-Mixture"; -//string speciesName ="SpeciesA, SpeciesB"; +//string speciesName = "SpeciesA, SpeciesB"; //string initMassFraction = "1.0, 0.0"; int nSutherland = 0; double gamaSpeciesA = 1.4; @@ -1173,9 +1196,17 @@ double molecularWeightSpeciesB = 30.0; //string speciesName = "O2, N2"; //string initMassFraction = "1.0, 0.0"; +int nFraction = 0; int nContinueModel = 0; int nChemicalFlowStep = 0; int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; ######################################################################### // Multi-Grid parameters. @@ -1196,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0; // 1 -- zero order. // 2 -- first-order. (default) // mgCorrectionLimit: Multi-grid correction limit. - int nMGLevel = 1; int MGCoarsestIteration = 1; int MGPreIteration = 1; @@ -1218,20 +1248,20 @@ 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"; +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 # -######################################################################### +#************************************************************************ +# High Order Struct Solver * +#************************************************************************ // isFVMOrFDM: -// 0 -- NSSolverStruct using Finite Volume Method. -// 1 -- NSSolverStruct using Finite Differ Method. +// 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) @@ -1273,30 +1303,48 @@ int allReduceStep = 1; // codeOfOversetGrid: Overlapping(overset) grid or not. // 0 -- NON-overlapping grid. // 1 -- Overlapping grid. -// oversetInterpolationMethod: the method of overset interpolation while field simulation +// oversetInterpolationMethod: the method of overset interpolation while field simulation. // 0 -- set the acceptor cell value by donor cell value. // 1 -- set the acceptor cell value by distance weight of donor cell value. - -int codeOfOversetGrid = 0; -int oversetInterpolationMethod = 0; -int readOversetFileOrNot = 0; -int symetryOrNot = 0; -int readInAuxiliaryInnerGrid = 0; -int readInAuxiliaryOuterGrid = 0; -int readInSklFileOrNot = 0; -string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; -string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; -string auxiliaryInnerGrid2 = ""; -string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; - -int numberOfMovingBodies = 2; +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; // ----------------- ALE configuration ------------------------------ int codeOfAleModel = 0; @@ -1306,36 +1354,42 @@ 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; +int strategyForFaceNormalVelocity = 0; // 0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd. +int strategyForGCLSource = 0; // 0-present; 1-Ahn. -//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. int methodForKineticEquation = 0; double relaxParameterOfKinetic = 1.0; -######################################################################### -# motive information # -######################################################################### +#************************************************************************ +# motive information * +#************************************************************************ int numberOfMovingBodies = 1; ############################## body0 ############################## -//mass of parts -double mass_0 = 1.0; -//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz -double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; -//initial six DOF position information of parts. xc yc zc -double massCenter_0[] = 0.0 , 0.0, 0.0; -//initial six DOF position information of parts. angleX angleY angleZ -double attitudeAngle_0[] = 0.0 , 0.0, 0.0; -//initial six DOF move information of parts. vc vy vz -double massCenterVelocity_0[] = 0.0, 0.0, 0.0; -//initial six DOF move information of parts. omigX omigY omigZ -double angularVelocity_0[] = 0.0, 0.0, 0.0; -//the object that the parts belong to. -int fartherIndex_0 = -1; -//the assembly position of the parts. xc yc zc angleX angleY angleZ -double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0; -//the move pattern of the parts. +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. // -1 given motion partten. // 0 still. // 1 six DOF motion. @@ -1346,51 +1400,68 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 // 14 forced pitch motion. // 15 forced yaw motion. // 16 forced roll motion. -int RBDMethod_0 = 0; -double amplitude_0 = 0.0; -double reduceFrequency_0 = 0.0; -//direction of rotation +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 ; -//additional moment of Force (system axis) mX mY mZ -double addedMoment_0[] = 0.0 ,0.0 ,0.0 ; -//the deformation method of the parts. -int morphing_0 = 0; - -// post indentify -int integralOrder = 4; +int direction_0 = -1; +double rotateFrequency_0 = 0.0; +//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; +// post indentify. +int integralOrder = 4; // ---------------- ATP read -------------------------------------------- -//@int inflowParaType = 0; +//@int inflowParaType = 0; //@double refReNumber = 6.5e6; //@double refDimensionalTemperature = 288.15; //@double freestream_vibration_temperature = 300.00; -//@double refDimensionalPressure = 0; -//@double height = 0; -//@int nsubsonicInlet = 0; -//@int nsubsonicOutlet = 0; -//@string inLetFileName = "./bin/subsonicInlet.hypara"; -//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; //@double refDimensionalVelocity = 0; //@double refDimensionalDensity = 0; - -######################################################################### -# Old Parameter # -######################################################################### +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ int isPlotVolumeField = 0; +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; -######################################################################### -# Incompressible Parameter # -######################################################################### +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ int isSolveEnergyEquation = 0; int isSolveTurbEquation = 0; -int isSolveSpeciesEquation = 0; - +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/F04_TwoD_Dual0012_OversetGrid_InvisCal_Unstruct_4CPU/bin/grid_para.hypara b/F04_TwoD_Dual0012_OversetGrid_InvisCal_Unstruct_4CPU/bin/grid_para.hypara index f414e19..034abce 100644 --- a/F04_TwoD_Dual0012_OversetGrid_InvisCal_Unstruct_4CPU/bin/grid_para.hypara +++ b/F04_TwoD_Dual0012_OversetGrid_InvisCal_Unstruct_4CPU/bin/grid_para.hypara @@ -4,9 +4,12 @@ // 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. +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. // from_gtype: Type of grid data type in grid conversion process. // -1 -- MULTI_TYPE. // 1 -- PHengLEI, *.fts. @@ -18,7 +21,9 @@ // 7 -- Hybrid, include both of unstructured and structured grid, *.fts. // 8 -- GMSH, *.msh. int gridtype = 0; -int axisup = 1; +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; int from_gtype = 2; ######################################################################### diff --git a/F04_TwoD_Dual0012_OversetGrid_InvisCal_Unstruct_4CPU/二维双NACA0012翼型非结构重叠网格计算算例说明文档.pdf b/F04_TwoD_Dual0012_OversetGrid_InvisCal_Unstruct_4CPU/二维双NACA0012翼型非结构重叠网格计算算例说明文档.pdf index 3f4a8d6..afb7d69 100644 Binary files a/F04_TwoD_Dual0012_OversetGrid_InvisCal_Unstruct_4CPU/二维双NACA0012翼型非结构重叠网格计算算例说明文档.pdf and b/F04_TwoD_Dual0012_OversetGrid_InvisCal_Unstruct_4CPU/二维双NACA0012翼型非结构重叠网格计算算例说明文档.pdf differ diff --git a/F05_ThreeD_AEDC_OversetConfig_Unstruct_8CPU/bin/grid_para.hypara b/F05_ThreeD_AEDC_OversetConfig_Unstruct_8CPU/bin/grid_para.hypara index 2019ffc..2847188 100644 --- a/F05_ThreeD_AEDC_OversetConfig_Unstruct_8CPU/bin/grid_para.hypara +++ b/F05_ThreeD_AEDC_OversetConfig_Unstruct_8CPU/bin/grid_para.hypara @@ -4,9 +4,12 @@ // 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. +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. // from_gtype: Type of grid data type in grid conversion process. // -1 -- MULTI_TYPE. // 1 -- PHengLEI, *.fts. @@ -18,7 +21,9 @@ // 7 -- Hybrid, include both of unstructured and structured grid, *.fts. // 8 -- GMSH, *.msh. int gridtype = 0; -int axisup = 2; +int nAxisRotateTimes = 1; +int axisRotateOrder[] = [1]; +double axisRotateAngles[] = [90.0]; int from_gtype = 2; ######################################################################### diff --git a/F05_ThreeD_AEDC_OversetConfig_Unstruct_8CPU/bin/overset_config.hypara b/F05_ThreeD_AEDC_OversetConfig_Unstruct_8CPU/bin/overset_config.hypara index 0308b7e..8e46233 100644 --- a/F05_ThreeD_AEDC_OversetConfig_Unstruct_8CPU/bin/overset_config.hypara +++ b/F05_ThreeD_AEDC_OversetConfig_Unstruct_8CPU/bin/overset_config.hypara @@ -24,8 +24,8 @@ string gridfile1 = "./grid/Missile__8.fts"; int codeOfOversetGrid = 1; int symetryOrNot = 1; int readInAuxiliaryInnerGrid = 1; -string auxiliaryInnerGrid0 = ". -string auxiliaryInnerGrid1 = ". +string auxiliaryInnerGrid0 = "./grid/WingIn.fts"; +string auxiliaryInnerGrid1 = "./grid/MissileIn.fts"; int twoOrderInterpolationOrNot = 1; int keyEnlargeOfActiveNodes = 3; diff --git a/F05_ThreeD_AEDC_OversetConfig_Unstruct_8CPU/非结构三维AEDC吊舱分离_重叠装配算例说明文档.pdf b/F05_ThreeD_AEDC_OversetConfig_Unstruct_8CPU/非结构三维AEDC吊舱分离_重叠装配算例说明文档.pdf index 91f3279..8fc58ba 100644 Binary files a/F05_ThreeD_AEDC_OversetConfig_Unstruct_8CPU/非结构三维AEDC吊舱分离_重叠装配算例说明文档.pdf and b/F05_ThreeD_AEDC_OversetConfig_Unstruct_8CPU/非结构三维AEDC吊舱分离_重叠装配算例说明文档.pdf differ diff --git a/F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU/bin/cfd_para.hypara b/F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU/bin/cfd_para.hypara index c344658..f903a5a 100644 --- a/F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU/bin/cfd_para.hypara +++ b/F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU/bin/cfd_para.hypara @@ -8,23 +8,24 @@ // Platform for Hybrid Engineering Simulation of Flows + // China Aerodynamics Research and Development Center + // (C) Copyright, Since 2010 + +// PHengLEI 2212 + //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ########################################################################### # 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. -// 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. +// 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. +// 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. @@ -46,19 +47,24 @@ 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. -int axisup = 1; +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; // 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; +int omitRepeatInterface = 1; //----------------------------------------------------------------------- # Grid data type # @@ -87,10 +93,9 @@ 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. int numberOfGridFile = 1; -string from_gfile = "./grid/rae2822_hybrid2d.cas"; -string from_gfile1= ""; - -string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; // ----------------- some advanced choices ------------------------------ // iunsteady: The Grid is for unsteady simulation or not. @@ -103,9 +108,9 @@ 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"; +// 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; @@ -119,31 +124,31 @@ string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp"; // 0 -- Not. (default) // 1 -- Yes. // geometryUnit: Geometry unit. -// 1 -- meter. -// 2 -- millimeter. -// 3 -- inch. +// 1 -- meter. +// 2 -- millimeter. +// 3 -- inch. // exclusiveCase: Parallel projection exclusive case. -// 0 -- NON case. -// 1 -- JSM-C2-NPOFF case. -// 2 -- CHNT. +// 0 -- NON case. +// 1 -- JSM-C2-NPOFF case. +// 2 -- CHNT. // projectOrgPoint: If the original wall points need to be projected or not. -int anisoRefine = 0; -int geometryUnit = 1; -int isProject = 0; -int readDist = 0; -int isDeform = 0; +int anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; int exclusiveCase = 0; int projectOrgPoint = 0; string geometryFileName = "./grid/jsm.igs"; // ----------------- Grid Deform Parameters ----------------------------- // deformationMethod: Grid Deform. -// 1 -- SPRING. -// 2 -- RBF. +// 1 -- SPRING. +// 2 -- RBF. // stationalGridFile: Original grid file. // visualFileName : The visualization file path of deform grid. // nDeformStep : The max deform step. -// flapAngle : The max flap angle. +// flapAngle : The max flap angle. // rotatePostionZ : Rotate postion. // rotatePostionY : Rotate postion. // gridSlice : If dump slice grid. @@ -163,10 +168,10 @@ int sliceAxis = 1; double slicePosition = 13; // ----------------- RBF Parameters ------------------------------------- -// numberOfReferenceCP : Number of reference Control Points. -// influencePara : The RBF influence radius parameter. +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. int numberOfReferenceCP = 40; -double influencePara = 25.0; +double influencePara = 25.0; // ----------------- Periodic Parameters -------------------------------- // Notice: Rotational periodicity only support rotation along the X axis! @@ -178,9 +183,8 @@ double influencePara = 25.0; which only support one direction. // rotationAngle: The relative angle between two periodic face. which is recorded in degrees. - int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; +double translationLength[] = [0.0, 0.0, 0.0]; double rotationAngle = 0.0; ######################################################################### @@ -192,7 +196,6 @@ double rotationAngle = 0.0; // 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; @@ -201,20 +204,20 @@ int numberOfMultifile = 1; // 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. +// cellIndexOfMark : the cell index of mark, only for structured grid partition. int traceMark = 0; int blockIndexOfMark = 0; -int cellIndexOfMark[] = [185,30,1]; +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; +// parallelStrategy: +// 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). +// 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"; @@ -232,11 +235,10 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts"; // 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; +double parmetisBalance = 1.05; // numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. // 1 -- single level. @@ -248,29 +250,35 @@ 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. +// 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; +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; int intervalStepSample = 1000; -int intervalStepForce = 100; -int intervalStepRes = 10; -int ifLowSpeedPrecon = 0; +int intervalStepForce = 100; +int intervalStepRes = 10; // compressible: // 0 -- incompressible flow. // 1 -- compressible flow. (default) int compressible = 1; +// 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) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 1; + //----------------------------------------------------------------------- # CFD Control Parameter # //----------------------------------------------------------------------- @@ -281,33 +289,36 @@ int compressible = 1; // 0 -- the nondimensional conditions. // 1 -- the flight conditions. // 2 -- the experiment conditions. -// 3 -- the subsonic boundary conditions. +// 3 -- the subsonic boundary conditions. (Useless!) // 4 -- the condition that the velocity, temperature and density are given. // 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 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. +// 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 = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. // forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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. -// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol. +// 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; +int directionMethod = 0; double refMachNumber = 0.73; double attackd = 2.79; double angleSlide = 0.00; +int flowInitMethod = 0; int inflowParaType = 0; double refReNumber = 6.5e6; @@ -321,29 +332,27 @@ double freestream_vibration_temperature = 300.00; //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; - -//The velocity, temperature and density are fixed. +// The velocity, temperature and density are fixed. //int inflowParaType = 4; //double refDimensionalVelocity = 1000.0; -//double refDimensionalDensity = 1.0e3; +//double refDimensionalDensity = 1.0e3; -//The velocity, temperature and pressure are fixed. +// The velocity, temperature and pressure are fixed. //int inflowParaType = 5; //double refDimensionalVelocity = 1000.0; //double refDimensionalPressure = 1.0e5; -//The MachNumber, temperature and pressure are fixed. +// The MachNumber, temperature and pressure are fixed. //int inflowParaType = 6; -//double refDimensionalTemperature = 293; +//double refDimensionalTemperature = 293.0; //double refDimensionalPressure = 8886.06; +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; + double wallTemperature = -1.0; double radiationCoef = 0.8; @@ -357,41 +366,41 @@ 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. +double knudsenLength = 1.0; // unit of meter. double refMolecularWeight = 28.9644; // unit of g/mol. //----------------------------------------------------------------------- # Spatial Discretisation # //----------------------------------------------------------------------- -#******************************************************************* -# Struct Solver * -#******************************************************************* +#************************************************************************ +# 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". +// -- "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. +// 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" - +// -- "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"; +string str_limiter_name = "vanalbada"; -#******************************************************************* -# UnStruct Solver or Common * -#******************************************************************* +#************************************************************************ +# UnStruct Solver or Common * +#************************************************************************ // viscousType: Viscous model. -// 0 -- Euler. -// 1 -- Lamilar. -// 2 -- Algebraic. -// 3 -- 1eq turbulent. -// 4 -- 2eq turbulent. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. // viscousName: Laminar or tubulent model. // -- "0eq-bl". // -- "1eq-sa". @@ -410,16 +419,16 @@ string str_limiter_name = "vanalbada"; // 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". +// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // uns_limiter_name: Limiter of Unstruct grid. -// -- "barth", "vencat", "vanleer", "minmod". -// -- "vanalbada", "smooth", "nnd", "lpz", "1st". +// -- "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". // gradientName: Gradient reconstruction method. -// -- "default", "ggcell", "ggnode", "lsq". +// -- "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. @@ -442,18 +451,18 @@ 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 +// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0. -//int viscousType = 0; +//int viscousType = 0; //string viscousName = "Euler"; -//int viscousType = 1; +//int viscousType = 1; //string viscousName = "laminar"; -int viscousType = 3; +int viscousType = 3; string viscousName = "1eq-sa"; -//int viscousType = 4; +//int viscousType = 4; //string viscousName = "2eq-kw-menter-sst"; int DESType = 0; @@ -463,7 +472,7 @@ string uns_limiter_name = "vencat"; string uns_vis_name = "test"; string gradientName = "ggnode"; -int ivencat = 7; +int ivencat = 7; double venkatCoeff = 5.0; int reconmeth = 1; int limitVariables = 0; @@ -475,9 +484,9 @@ double roeEntropyScale = 1.0; double AusmpwPlusLimiter = 1.0; -//----------------------------------------------------------------------- -# Temporal Discretisation # -//----------------------------------------------------------------------- +#************************************************************************ +# Temporal Discretisation * +#************************************************************************ // iunsteady: Steady or unsteady. // 0 -- steady. // 1 -- unsteay. @@ -490,51 +499,57 @@ double AusmpwPlusLimiter = 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 = - ^2 -// 1 -- tau = +// 0 -- tau = - ^2 +// 1 -- tau = // 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 -- Line LU-SGS. -// 8 -- Matrix LU-SGS. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 4 -- LU-SGS. +// 5 -- Block LU-SGS. +// 6 -- Jacobian iteration. +// 7 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. // 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. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. // 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. +// 0 --Local. +// 1 --Global. // isUseLocalCFL: use variable number of CFL or not. -// 0 -- global unified CFL number. -// 1 -- local CFL number. +// 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. -// 0 -- no ALE method. -// 1 -- ALE method for non-moving grids. -// 2 -- ALE method for moving grids. -// 3 -- ALE method for deforming grids. +// 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. +// 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; +int iunsteady = 0; double physicalTimeStep = 0.01; double physicalTimeStepDimensional = -0.001; int ifStartFromSteadyResults = 0; @@ -543,39 +558,42 @@ int ifStaticsReynoldsStress = 0; int startStatisticStep = 800000; double statisticalTimePeriod = -1.0; int statisticMethod = 0; -int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2; +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 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 CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; double pMaxForCFL = 0.2; double pMinForCFL = 0.1; double deltaMaxForCFL = 0.2; double magnifyFactorForCFL = 1.1; double reduceFactorForCFL = 0.5; -double ktmax = 1.0e10; +double ktmax = 1.0e10; -int swapDq = 1; +int swapDq = 1; int nLUSGSSweeps = 1; double LUSGSTolerance = 0.01; -int order = 2; +int order = 2; double visl_min = 0.01; double turbCFLScale = 1.0; -double csrv = 2.0; +double csrv = 1.0; double timemax = 1.0e10; double dtsave = -1.0; int maxale = 10; @@ -591,10 +609,9 @@ double lamda[] = [0.5, 1.0]; //int RKStage = 4; //double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; - -//----------------------------------------------------------------------- -# File In or Out # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. @@ -611,20 +628,18 @@ double lamda[] = [0.5, 1.0]; // 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. +// 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. // 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= ""; +// 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; @@ -632,10 +647,12 @@ int cellMethodOrNodeMethod = 0; string resSaveFile = "results/res.dat"; string turbresfile = "results/turbres.dat"; +string transitionResFile = "results/transitionRes.dat"; string aircoeffile = "results/aircoef.dat"; string restartNSFile = "results/flow.dat"; string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; string visualfile = "results/tecflow.plt"; string wall_aircoefile = "results/wall_aircoef.dat"; @@ -645,10 +662,14 @@ string protectionFile0 = "results/flow0.dat"; string protectionFile1 = "results/flow1.dat"; string wall_heatfluxfile = "results/wall_heatflux.dat"; -int nDumpSurfaceInfo = 0; -string wall_varfile = ""; +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; -string jetDefineFile = "bin/jet.hypara"; +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; string sixDofFileName = "results/sixDofInfo.dat"; string derivativeFileName = "results/identify.dat"; @@ -659,7 +680,8 @@ int plotFieldType = 0; // visualfileType: The file type of visualfile. // 0 -- Tecplot binary. // 1 -- Tecplot ASCII. - +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. int visualfileType = 1; // samplefileMode: The dump mode of sample file. @@ -697,21 +719,21 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), 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) +// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. //-----------the optional parameters list for the wall boundary condition---------------- // nVisualWallVariables: The number of visual variables on wall. // visualWallVariables : dumped variable types, listed as following: -// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4), -// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8), -// -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), -Grid Reynolds number on wall(Re_w, 23) +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- 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), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). int nVisualVariables = 8; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; @@ -739,16 +761,18 @@ 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), mach(6). +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). // 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. +// 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; +int dataMonitorType = 0; string probesDefineFile = "bin/probes_XYZ.dat"; //int dataMonitorType = 1; @@ -761,28 +785,26 @@ string probesDefineFile = "bin/probes_XYZ.dat"; int searchCellsMethod = 0; -int nProbeVariables = 7; -int probeVariables[] = [0, 1, 2, 3, 4, 5, 6]; -int probeVariablesInterpolationMethod = 0; -//----------------------------------------------------------------------- -# Turbulence Parameter # -//----------------------------------------------------------------------- +int nProbeVariables = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +int probeVariablesInterpolationMethod = 0; + +#************************************************************************ +# Turbulence Parameter * +#************************************************************************ // turbInterval: Iteration number of turbulence. // kindOfTurbSource: Kinds of turbulent source. // 0 -- Original. // mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0. -// transitionType: transition model type +// 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 - - +// 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; 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; @@ -790,29 +812,28 @@ int transitionType = 0; double turbIntensity = -1.0; int freeturbIntensitySRModify = 0; double freeDecayXLocation = 0.0; -int compressibleCorrection = 0; -int prandtlNumberCorrection = 0; +int compressibleCorrection = 0; int transitionMaFix = 1; -# maximum eddy viscosity (myt/my) max. +// maximum eddy viscosity (myt/my) max. double eddyViscosityLimit = 1.0e10; int monitor_vistmax = 0; -//----------------------------------------------------------------------- -# LES Parameter # -//----------------------------------------------------------------------- +#************************************************************************ +# LES Parameter * +#************************************************************************ // iLES: Create LESSolver or not. -// = 1 - Create LESSolver; -// != 1 - 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. +// = 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. +// = 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. @@ -820,23 +841,22 @@ int monitor_vistmax = 0; // = "dsmCom"; // = "wale"; // = "sigma". -// 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. +// 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. +// = 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. +// 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; @@ -852,19 +872,16 @@ double testFilterScale = 2.0; int averageWidth = 1; int monitorNegativeConstant = 0; -//----------------------------------------------------------------------- -# Other Parameters for Hypersonic Non-equilibrium Gas # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. -// 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. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. @@ -875,7 +892,7 @@ int monitorNegativeConstant = 0; // 2 -- Argon. // 3 -- Nitrogen. // nEnergyRecycle: The type of EnergyModel Recycle. -// 0 -- not used . +// 0 -- not used. // 1 -- used. // nDensityModify: The type of densitymodify. // 0 -- not used. @@ -883,26 +900,25 @@ int monitorNegativeConstant = 0; // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. -// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. // 0 -- perfect gas. // 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. -// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. -// the value equals to or is greater than 1, and 3 is for default value. -// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. -// the value equals to or is greater than 1, and 3 is for default value. -// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. -// the value equals to or is greater than 1, and 3 is for default value. -// nSlipBCModel : The computational model of slip boundary conditions. - -// 0 -- no slip. -// 1 -- the conventional Maxwell slip conditions. -// 2 -- the Gokcen slip conditions. -// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. -// 4 -- the Kogan simplified slip conditions. -// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. -// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). -// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. -// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). // nchemsrc: // 0 -- the source terms are not computed. // 1 -- the source terms are computed. @@ -913,148 +929,151 @@ int monitorNegativeConstant = 0; // 1 -- One-temperature model. // 2 -- Two-temperature model. // 3 -- Three-temperature model. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. // 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. +// 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 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: -// 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. -// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. -// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. -// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. -// 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. +// 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. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// 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]. // velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. -// 1.0 -- proposed by Maxwell. -// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. -// 1.146 -- proposed for an additional "fictitious" velocity slip. - -// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. -// 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. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// 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. // nSpeciesLimit: limitter of gas species -// 0 -- not used. -// 1 -- used. -// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction -// 0 -- method 0. -// 1 -- method 1. -// 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) - +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// 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 +// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs. +// 0 -- not used. +// 1 -- used. +// nDiagonalModified: Modified on Diagonal. +// 0 -- not used. +// 1 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. // nAblation: -// 0 -- The wall ablation is not computed. -// 1 -- The wall ablation is computed. +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. // isInjection: -// 0 -- The injection velocity of ablation wall is not computed. -// 1 -- The injection velocity of ablation wall is computed. +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. // nViscosityModel: -// 0 -- Blottner fitting method(N89). -// 1 -- Gupta fitting method(N90). +// 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. +// 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. +// 0 -- stands for selecting the Blotter curve fits mode. +// 1 -- stands for Sutherland relation. // 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. -// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. -// "Gas-Mixture" -- indicates the process of mixing gas without reacting. -// for struct solver mixing two speciesSpeciesA, SpeciesB. -// for unstruct solver mixing multi-speciesO2 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. +// "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. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "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. +// 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. +// 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 - +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. int dg_high_order = 0; int iapplication = 0; int isAdaptiveSolver = 0; -int nm = 5; +int nm = 5; int nEquilibriumGas = 0; -int nPCWCycleStep = 3; -int nRETCycleStep = 3; -int nSLIPCycleStep= 3; +int nPCWCycleStep = 3; +int nRETCycleStep = 3; +int nSLIPCycleStep = 3; int nIterFirstStep = 1000; int nIterSecondStep= 2000; int nIterThirdStep = 2000; @@ -1065,17 +1084,17 @@ double secondStepError = 0.001; double thirdStepError = 0.001; double predictCFLError = 0.1; -double refGama = 1.4; -double prl = 0.72; -double prt = 0.90; -double sc_l = 0.5; -double sc_t = 0.5; +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 nGasModel = 0; +int nchem = 0; +int nchemsrc = 1; +int nchemrad = 1; +int ntmodel = 1; int nIdealState = 0; int nEnergyRecycle = 1; @@ -1099,12 +1118,12 @@ double sigmaTemperature = 1.0; double sigmaMassFraction = 1.0; double velocitySlipCorrectConstant = 1.0; -double chemicalRelaxCorf = 1.0; +double chemicalRelaxCorf = 1.0; double chemicalSpectrumRadiusCoef = 1.0; double viscousSpectrumRadiusCoef = 1.5; double inviscidSpectrumRadiusCoef = 1.5; -double spectrumRadiusCoef = 0.5; -double staticPressureRelaxCorf = 0.2; +double spectrumRadiusCoef = 0.5; +double staticPressureRelaxCorf = 0.2; double maxViscous = 10000.0; double trTemperatureMin = 10.0; @@ -1114,31 +1133,35 @@ double densityMin = 1.0e-8; double densityMinFactor = 0.1; double tAdjustmentFactor = 10.0; double iniSpeedCoef = 1.0; +int iniSpeedMode = 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 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 nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; -int nProtectData = 0; -int useHyflowSetting = 0; -int nAblation = 0; -int isInjection = 0; -int nViscosityModel = 0; -int nMarsModel = 0; -string gasfile = "DK5"; -//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; string speciesName = "O, O2, NO, N, N2"; string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; @@ -1152,16 +1175,16 @@ 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 = "Pa"; +//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"; -//string gasfile = "Combustion-12"; +//string gasfile = "Combustion-12"; //string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; //string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; //string gasfile = "Gas-Mixture"; -//string speciesName ="SpeciesA, SpeciesB"; +//string speciesName = "SpeciesA, SpeciesB"; //string initMassFraction = "1.0, 0.0"; int nSutherland = 0; double gamaSpeciesA = 1.4; @@ -1173,9 +1196,17 @@ double molecularWeightSpeciesB = 30.0; //string speciesName = "O2, N2"; //string initMassFraction = "1.0, 0.0"; +int nFraction = 0; int nContinueModel = 0; int nChemicalFlowStep = 0; int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; ######################################################################### // Multi-Grid parameters. @@ -1196,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0; // 1 -- zero order. // 2 -- first-order. (default) // mgCorrectionLimit: Multi-grid correction limit. - int nMGLevel = 1; int MGCoarsestIteration = 1; int MGPreIteration = 1; @@ -1218,20 +1248,20 @@ 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"; +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 # -######################################################################### +#************************************************************************ +# High Order Struct Solver * +#************************************************************************ // isFVMOrFDM: -// 0 -- NSSolverStruct using Finite Volume Method. -// 1 -- NSSolverStruct using Finite Differ Method. +// 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) @@ -1273,30 +1303,48 @@ int allReduceStep = 1; // codeOfOversetGrid: Overlapping(overset) grid or not. // 0 -- NON-overlapping grid. // 1 -- Overlapping grid. -// oversetInterpolationMethod: the method of overset interpolation while field simulation +// oversetInterpolationMethod: the method of overset interpolation while field simulation. // 0 -- set the acceptor cell value by donor cell value. // 1 -- set the acceptor cell value by distance weight of donor cell value. - -int codeOfOversetGrid = 0; -int oversetInterpolationMethod = 0; -int readOversetFileOrNot = 0; -int symetryOrNot = 0; -int readInAuxiliaryInnerGrid = 0; -int readInAuxiliaryOuterGrid = 0; -int readInSklFileOrNot = 0; -string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; -string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; -string auxiliaryInnerGrid2 = ""; -string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; - -int numberOfMovingBodies = 2; +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; // ----------------- ALE configuration ------------------------------ int codeOfAleModel = 0; @@ -1306,36 +1354,42 @@ 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; +int strategyForFaceNormalVelocity = 0; // 0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd. +int strategyForGCLSource = 0; // 0-present; 1-Ahn. -//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. int methodForKineticEquation = 0; double relaxParameterOfKinetic = 1.0; -######################################################################### -# motive information # -######################################################################### +#************************************************************************ +# motive information * +#************************************************************************ int numberOfMovingBodies = 1; ############################## body0 ############################## -//mass of parts -double mass_0 = 1.0; -//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz -double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; -//initial six DOF position information of parts. xc yc zc -double massCenter_0[] = 0.0 , 0.0, 0.0; -//initial six DOF position information of parts. angleX angleY angleZ -double attitudeAngle_0[] = 0.0 , 0.0, 0.0; -//initial six DOF move information of parts. vc vy vz -double massCenterVelocity_0[] = 0.0, 0.0, 0.0; -//initial six DOF move information of parts. omigX omigY omigZ -double angularVelocity_0[] = 0.0, 0.0, 0.0; -//the object that the parts belong to. -int fartherIndex_0 = -1; -//the assembly position of the parts. xc yc zc angleX angleY angleZ -double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0; -//the move pattern of the parts. +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. // -1 given motion partten. // 0 still. // 1 six DOF motion. @@ -1346,51 +1400,68 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 // 14 forced pitch motion. // 15 forced yaw motion. // 16 forced roll motion. -int RBDMethod_0 = 0; -double amplitude_0 = 0.0; -double reduceFrequency_0 = 0.0; -//direction of rotation +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 ; -//additional moment of Force (system axis) mX mY mZ -double addedMoment_0[] = 0.0 ,0.0 ,0.0 ; -//the deformation method of the parts. -int morphing_0 = 0; - -// post indentify -int integralOrder = 4; +int direction_0 = -1; +double rotateFrequency_0 = 0.0; +//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; +// post indentify. +int integralOrder = 4; // ---------------- ATP read -------------------------------------------- -//@int inflowParaType = 0; +//@int inflowParaType = 0; //@double refReNumber = 6.5e6; //@double refDimensionalTemperature = 288.15; //@double freestream_vibration_temperature = 300.00; -//@double refDimensionalPressure = 0; -//@double height = 0; -//@int nsubsonicInlet = 0; -//@int nsubsonicOutlet = 0; -//@string inLetFileName = "./bin/subsonicInlet.hypara"; -//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; //@double refDimensionalVelocity = 0; //@double refDimensionalDensity = 0; - -######################################################################### -# Old Parameter # -######################################################################### +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ int isPlotVolumeField = 0; +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; -######################################################################### -# Incompressible Parameter # -######################################################################### +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ int isSolveEnergyEquation = 0; int isSolveTurbEquation = 0; -int isSolveSpeciesEquation = 0; - +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU/bin/cfd_para_transonic_unsteady.hypara b/F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU/bin/cfd_para_transonic_unsteady.hypara index b254bd5..cbc441e 100644 --- a/F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU/bin/cfd_para_transonic_unsteady.hypara +++ b/F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU/bin/cfd_para_transonic_unsteady.hypara @@ -179,7 +179,6 @@ int flowInitStep = 0; // isPlotVolumeField: If dump out the whole field results to tecplot or not, 0 / 1. int plotFieldType = 1; -int visualfileType = 0; // ----------------- Advanced Parameters, DO NOT care it ---------------- // nVisualVariables: Number of variables want to be dumped for tecplot visualization. diff --git a/F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU/bin/grid_para.hypara b/F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU/bin/grid_para.hypara index 2019ffc..2847188 100644 --- a/F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU/bin/grid_para.hypara +++ b/F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU/bin/grid_para.hypara @@ -4,9 +4,12 @@ // 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. +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. // from_gtype: Type of grid data type in grid conversion process. // -1 -- MULTI_TYPE. // 1 -- PHengLEI, *.fts. @@ -18,7 +21,9 @@ // 7 -- Hybrid, include both of unstructured and structured grid, *.fts. // 8 -- GMSH, *.msh. int gridtype = 0; -int axisup = 2; +int nAxisRotateTimes = 1; +int axisRotateOrder[] = [1]; +double axisRotateAngles[] = [90.0]; int from_gtype = 2; ######################################################################### diff --git a/F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU/非结构三维AEDC吊舱分离非定常计算_算例说明文档.pdf b/F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU/非结构三维AEDC吊舱分离非定常计算_算例说明文档.pdf index 243826b..b0882a6 100644 Binary files a/F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU/非结构三维AEDC吊舱分离非定常计算_算例说明文档.pdf and b/F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU/非结构三维AEDC吊舱分离非定常计算_算例说明文档.pdf differ diff --git a/F07-TwoD_NACA0012_PitchingMovement_SA_Struct_4CPU/bin/grid_para.hypara b/F07-TwoD_NACA0012_PitchingMovement_SA_Struct_4CPU/bin/grid_para.hypara index 92d8a64..5c5fff0 100644 --- a/F07-TwoD_NACA0012_PitchingMovement_SA_Struct_4CPU/bin/grid_para.hypara +++ b/F07-TwoD_NACA0012_PitchingMovement_SA_Struct_4CPU/bin/grid_para.hypara @@ -4,9 +4,12 @@ // 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. +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. // from_gtype: Type of grid data type in grid conversion process. // -1 -- MULTI_TYPE // 1 -- HyperFLOW( PHengLEI ), *.fts. @@ -18,7 +21,9 @@ // 7 -- Hybrid, include both of unstructured and structured grid, *.fts. // 8 -- GMSH, *.msh. int gridtype = 1; -int axisup = 1; +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; int from_gtype = 2; ######################################################################### diff --git a/F07-TwoD_NACA0012_PitchingMovement_SA_Struct_4CPU/二维结构NACA0012翼型俯仰振荡_算例说明文档.pdf b/F07-TwoD_NACA0012_PitchingMovement_SA_Struct_4CPU/二维结构NACA0012翼型俯仰振荡_算例说明文档.pdf index 7776710..490d6ee 100644 Binary files a/F07-TwoD_NACA0012_PitchingMovement_SA_Struct_4CPU/二维结构NACA0012翼型俯仰振荡_算例说明文档.pdf and b/F07-TwoD_NACA0012_PitchingMovement_SA_Struct_4CPU/二维结构NACA0012翼型俯仰振荡_算例说明文档.pdf differ diff --git a/F08-ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU/bin/boundary_condition.hypara b/F08-ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU/bin/boundary_condition.hypara deleted file mode 100644 index df701ef..0000000 --- a/F08-ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU/bin/boundary_condition.hypara +++ /dev/null @@ -1,69 +0,0 @@ -# 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 = 6; -string bcName = "BCWall"; -{ - string bodyName = "body"; - int bcType = 2; -} -string bcName = "BCFarfield"; -{ - int bcType = 4; -} -string bcName = "BCInflow"; -{ - int bcType = 5; -} -string bcName = "BCOutflow"; -{ - int bcType = 6; -} -string bcName = "BCDegenerateLine"; -{ - int bcType = 71; -} -string bcName = "BCDegenerateLine"; -{ - int bcType = 73; -} - -# 'bcType' is defined as following: -# 99: PERIODIC -# -2: WAKE -# -1: INTERFACE -# 0 : NO_BOUNDARY_CONDITION -# 1 : EXTRAPOLATION -# 2 : SOLID_SURFACE -# 3 : SYMMETRY -# 4 : FARFIELD -# 5 : INFLOW -# 6 : OUTFLOW -# 52: PRESSURE_INLET -# 62: PRESSURE_OUTLET -# 61: OUTFLOW_CONFINED -# 7 : POLE diff --git a/F08-ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU/bin/cfd_para.hypara b/F08-ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU/bin/cfd_para.hypara index c344658..f903a5a 100644 --- a/F08-ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU/bin/cfd_para.hypara +++ b/F08-ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU/bin/cfd_para.hypara @@ -8,23 +8,24 @@ // Platform for Hybrid Engineering Simulation of Flows + // China Aerodynamics Research and Development Center + // (C) Copyright, Since 2010 + +// PHengLEI 2212 + //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ########################################################################### # 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. -// 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. +// 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. +// 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. @@ -46,19 +47,24 @@ 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. -int axisup = 1; +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; // 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; +int omitRepeatInterface = 1; //----------------------------------------------------------------------- # Grid data type # @@ -87,10 +93,9 @@ 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. int numberOfGridFile = 1; -string from_gfile = "./grid/rae2822_hybrid2d.cas"; -string from_gfile1= ""; - -string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; // ----------------- some advanced choices ------------------------------ // iunsteady: The Grid is for unsteady simulation or not. @@ -103,9 +108,9 @@ 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"; +// 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; @@ -119,31 +124,31 @@ string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp"; // 0 -- Not. (default) // 1 -- Yes. // geometryUnit: Geometry unit. -// 1 -- meter. -// 2 -- millimeter. -// 3 -- inch. +// 1 -- meter. +// 2 -- millimeter. +// 3 -- inch. // exclusiveCase: Parallel projection exclusive case. -// 0 -- NON case. -// 1 -- JSM-C2-NPOFF case. -// 2 -- CHNT. +// 0 -- NON case. +// 1 -- JSM-C2-NPOFF case. +// 2 -- CHNT. // projectOrgPoint: If the original wall points need to be projected or not. -int anisoRefine = 0; -int geometryUnit = 1; -int isProject = 0; -int readDist = 0; -int isDeform = 0; +int anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; int exclusiveCase = 0; int projectOrgPoint = 0; string geometryFileName = "./grid/jsm.igs"; // ----------------- Grid Deform Parameters ----------------------------- // deformationMethod: Grid Deform. -// 1 -- SPRING. -// 2 -- RBF. +// 1 -- SPRING. +// 2 -- RBF. // stationalGridFile: Original grid file. // visualFileName : The visualization file path of deform grid. // nDeformStep : The max deform step. -// flapAngle : The max flap angle. +// flapAngle : The max flap angle. // rotatePostionZ : Rotate postion. // rotatePostionY : Rotate postion. // gridSlice : If dump slice grid. @@ -163,10 +168,10 @@ int sliceAxis = 1; double slicePosition = 13; // ----------------- RBF Parameters ------------------------------------- -// numberOfReferenceCP : Number of reference Control Points. -// influencePara : The RBF influence radius parameter. +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. int numberOfReferenceCP = 40; -double influencePara = 25.0; +double influencePara = 25.0; // ----------------- Periodic Parameters -------------------------------- // Notice: Rotational periodicity only support rotation along the X axis! @@ -178,9 +183,8 @@ double influencePara = 25.0; which only support one direction. // rotationAngle: The relative angle between two periodic face. which is recorded in degrees. - int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; +double translationLength[] = [0.0, 0.0, 0.0]; double rotationAngle = 0.0; ######################################################################### @@ -192,7 +196,6 @@ double rotationAngle = 0.0; // 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; @@ -201,20 +204,20 @@ int numberOfMultifile = 1; // 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. +// cellIndexOfMark : the cell index of mark, only for structured grid partition. int traceMark = 0; int blockIndexOfMark = 0; -int cellIndexOfMark[] = [185,30,1]; +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; +// parallelStrategy: +// 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). +// 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"; @@ -232,11 +235,10 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts"; // 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; +double parmetisBalance = 1.05; // numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. // 1 -- single level. @@ -248,29 +250,35 @@ 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. +// 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; +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; int intervalStepSample = 1000; -int intervalStepForce = 100; -int intervalStepRes = 10; -int ifLowSpeedPrecon = 0; +int intervalStepForce = 100; +int intervalStepRes = 10; // compressible: // 0 -- incompressible flow. // 1 -- compressible flow. (default) int compressible = 1; +// 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) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 1; + //----------------------------------------------------------------------- # CFD Control Parameter # //----------------------------------------------------------------------- @@ -281,33 +289,36 @@ int compressible = 1; // 0 -- the nondimensional conditions. // 1 -- the flight conditions. // 2 -- the experiment conditions. -// 3 -- the subsonic boundary conditions. +// 3 -- the subsonic boundary conditions. (Useless!) // 4 -- the condition that the velocity, temperature and density are given. // 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 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. +// 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 = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. // forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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. -// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol. +// 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; +int directionMethod = 0; double refMachNumber = 0.73; double attackd = 2.79; double angleSlide = 0.00; +int flowInitMethod = 0; int inflowParaType = 0; double refReNumber = 6.5e6; @@ -321,29 +332,27 @@ double freestream_vibration_temperature = 300.00; //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; - -//The velocity, temperature and density are fixed. +// The velocity, temperature and density are fixed. //int inflowParaType = 4; //double refDimensionalVelocity = 1000.0; -//double refDimensionalDensity = 1.0e3; +//double refDimensionalDensity = 1.0e3; -//The velocity, temperature and pressure are fixed. +// The velocity, temperature and pressure are fixed. //int inflowParaType = 5; //double refDimensionalVelocity = 1000.0; //double refDimensionalPressure = 1.0e5; -//The MachNumber, temperature and pressure are fixed. +// The MachNumber, temperature and pressure are fixed. //int inflowParaType = 6; -//double refDimensionalTemperature = 293; +//double refDimensionalTemperature = 293.0; //double refDimensionalPressure = 8886.06; +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; + double wallTemperature = -1.0; double radiationCoef = 0.8; @@ -357,41 +366,41 @@ 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. +double knudsenLength = 1.0; // unit of meter. double refMolecularWeight = 28.9644; // unit of g/mol. //----------------------------------------------------------------------- # Spatial Discretisation # //----------------------------------------------------------------------- -#******************************************************************* -# Struct Solver * -#******************************************************************* +#************************************************************************ +# 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". +// -- "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. +// 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" - +// -- "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"; +string str_limiter_name = "vanalbada"; -#******************************************************************* -# UnStruct Solver or Common * -#******************************************************************* +#************************************************************************ +# UnStruct Solver or Common * +#************************************************************************ // viscousType: Viscous model. -// 0 -- Euler. -// 1 -- Lamilar. -// 2 -- Algebraic. -// 3 -- 1eq turbulent. -// 4 -- 2eq turbulent. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. // viscousName: Laminar or tubulent model. // -- "0eq-bl". // -- "1eq-sa". @@ -410,16 +419,16 @@ string str_limiter_name = "vanalbada"; // 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". +// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // uns_limiter_name: Limiter of Unstruct grid. -// -- "barth", "vencat", "vanleer", "minmod". -// -- "vanalbada", "smooth", "nnd", "lpz", "1st". +// -- "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". // gradientName: Gradient reconstruction method. -// -- "default", "ggcell", "ggnode", "lsq". +// -- "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. @@ -442,18 +451,18 @@ 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 +// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0. -//int viscousType = 0; +//int viscousType = 0; //string viscousName = "Euler"; -//int viscousType = 1; +//int viscousType = 1; //string viscousName = "laminar"; -int viscousType = 3; +int viscousType = 3; string viscousName = "1eq-sa"; -//int viscousType = 4; +//int viscousType = 4; //string viscousName = "2eq-kw-menter-sst"; int DESType = 0; @@ -463,7 +472,7 @@ string uns_limiter_name = "vencat"; string uns_vis_name = "test"; string gradientName = "ggnode"; -int ivencat = 7; +int ivencat = 7; double venkatCoeff = 5.0; int reconmeth = 1; int limitVariables = 0; @@ -475,9 +484,9 @@ double roeEntropyScale = 1.0; double AusmpwPlusLimiter = 1.0; -//----------------------------------------------------------------------- -# Temporal Discretisation # -//----------------------------------------------------------------------- +#************************************************************************ +# Temporal Discretisation * +#************************************************************************ // iunsteady: Steady or unsteady. // 0 -- steady. // 1 -- unsteay. @@ -490,51 +499,57 @@ double AusmpwPlusLimiter = 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 = - ^2 -// 1 -- tau = +// 0 -- tau = - ^2 +// 1 -- tau = // 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 -- Line LU-SGS. -// 8 -- Matrix LU-SGS. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 4 -- LU-SGS. +// 5 -- Block LU-SGS. +// 6 -- Jacobian iteration. +// 7 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. // 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. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. // 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. +// 0 --Local. +// 1 --Global. // isUseLocalCFL: use variable number of CFL or not. -// 0 -- global unified CFL number. -// 1 -- local CFL number. +// 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. -// 0 -- no ALE method. -// 1 -- ALE method for non-moving grids. -// 2 -- ALE method for moving grids. -// 3 -- ALE method for deforming grids. +// 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. +// 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; +int iunsteady = 0; double physicalTimeStep = 0.01; double physicalTimeStepDimensional = -0.001; int ifStartFromSteadyResults = 0; @@ -543,39 +558,42 @@ int ifStaticsReynoldsStress = 0; int startStatisticStep = 800000; double statisticalTimePeriod = -1.0; int statisticMethod = 0; -int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2; +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 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 CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; double pMaxForCFL = 0.2; double pMinForCFL = 0.1; double deltaMaxForCFL = 0.2; double magnifyFactorForCFL = 1.1; double reduceFactorForCFL = 0.5; -double ktmax = 1.0e10; +double ktmax = 1.0e10; -int swapDq = 1; +int swapDq = 1; int nLUSGSSweeps = 1; double LUSGSTolerance = 0.01; -int order = 2; +int order = 2; double visl_min = 0.01; double turbCFLScale = 1.0; -double csrv = 2.0; +double csrv = 1.0; double timemax = 1.0e10; double dtsave = -1.0; int maxale = 10; @@ -591,10 +609,9 @@ double lamda[] = [0.5, 1.0]; //int RKStage = 4; //double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; - -//----------------------------------------------------------------------- -# File In or Out # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. @@ -611,20 +628,18 @@ double lamda[] = [0.5, 1.0]; // 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. +// 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. // 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= ""; +// 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; @@ -632,10 +647,12 @@ int cellMethodOrNodeMethod = 0; string resSaveFile = "results/res.dat"; string turbresfile = "results/turbres.dat"; +string transitionResFile = "results/transitionRes.dat"; string aircoeffile = "results/aircoef.dat"; string restartNSFile = "results/flow.dat"; string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; string visualfile = "results/tecflow.plt"; string wall_aircoefile = "results/wall_aircoef.dat"; @@ -645,10 +662,14 @@ string protectionFile0 = "results/flow0.dat"; string protectionFile1 = "results/flow1.dat"; string wall_heatfluxfile = "results/wall_heatflux.dat"; -int nDumpSurfaceInfo = 0; -string wall_varfile = ""; +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; -string jetDefineFile = "bin/jet.hypara"; +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; string sixDofFileName = "results/sixDofInfo.dat"; string derivativeFileName = "results/identify.dat"; @@ -659,7 +680,8 @@ int plotFieldType = 0; // visualfileType: The file type of visualfile. // 0 -- Tecplot binary. // 1 -- Tecplot ASCII. - +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. int visualfileType = 1; // samplefileMode: The dump mode of sample file. @@ -697,21 +719,21 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), 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) +// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. //-----------the optional parameters list for the wall boundary condition---------------- // nVisualWallVariables: The number of visual variables on wall. // visualWallVariables : dumped variable types, listed as following: -// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4), -// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8), -// -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), -Grid Reynolds number on wall(Re_w, 23) +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- 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), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). int nVisualVariables = 8; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; @@ -739,16 +761,18 @@ 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), mach(6). +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). // 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. +// 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; +int dataMonitorType = 0; string probesDefineFile = "bin/probes_XYZ.dat"; //int dataMonitorType = 1; @@ -761,28 +785,26 @@ string probesDefineFile = "bin/probes_XYZ.dat"; int searchCellsMethod = 0; -int nProbeVariables = 7; -int probeVariables[] = [0, 1, 2, 3, 4, 5, 6]; -int probeVariablesInterpolationMethod = 0; -//----------------------------------------------------------------------- -# Turbulence Parameter # -//----------------------------------------------------------------------- +int nProbeVariables = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +int probeVariablesInterpolationMethod = 0; + +#************************************************************************ +# Turbulence Parameter * +#************************************************************************ // turbInterval: Iteration number of turbulence. // kindOfTurbSource: Kinds of turbulent source. // 0 -- Original. // mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0. -// transitionType: transition model type +// 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 - - +// 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; 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; @@ -790,29 +812,28 @@ int transitionType = 0; double turbIntensity = -1.0; int freeturbIntensitySRModify = 0; double freeDecayXLocation = 0.0; -int compressibleCorrection = 0; -int prandtlNumberCorrection = 0; +int compressibleCorrection = 0; int transitionMaFix = 1; -# maximum eddy viscosity (myt/my) max. +// maximum eddy viscosity (myt/my) max. double eddyViscosityLimit = 1.0e10; int monitor_vistmax = 0; -//----------------------------------------------------------------------- -# LES Parameter # -//----------------------------------------------------------------------- +#************************************************************************ +# LES Parameter * +#************************************************************************ // iLES: Create LESSolver or not. -// = 1 - Create LESSolver; -// != 1 - 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. +// = 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. +// = 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. @@ -820,23 +841,22 @@ int monitor_vistmax = 0; // = "dsmCom"; // = "wale"; // = "sigma". -// 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. +// 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. +// = 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. +// 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; @@ -852,19 +872,16 @@ double testFilterScale = 2.0; int averageWidth = 1; int monitorNegativeConstant = 0; -//----------------------------------------------------------------------- -# Other Parameters for Hypersonic Non-equilibrium Gas # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. -// 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. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. @@ -875,7 +892,7 @@ int monitorNegativeConstant = 0; // 2 -- Argon. // 3 -- Nitrogen. // nEnergyRecycle: The type of EnergyModel Recycle. -// 0 -- not used . +// 0 -- not used. // 1 -- used. // nDensityModify: The type of densitymodify. // 0 -- not used. @@ -883,26 +900,25 @@ int monitorNegativeConstant = 0; // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. -// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. // 0 -- perfect gas. // 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. -// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. -// the value equals to or is greater than 1, and 3 is for default value. -// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. -// the value equals to or is greater than 1, and 3 is for default value. -// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. -// the value equals to or is greater than 1, and 3 is for default value. -// nSlipBCModel : The computational model of slip boundary conditions. - -// 0 -- no slip. -// 1 -- the conventional Maxwell slip conditions. -// 2 -- the Gokcen slip conditions. -// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. -// 4 -- the Kogan simplified slip conditions. -// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. -// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). -// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. -// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). // nchemsrc: // 0 -- the source terms are not computed. // 1 -- the source terms are computed. @@ -913,148 +929,151 @@ int monitorNegativeConstant = 0; // 1 -- One-temperature model. // 2 -- Two-temperature model. // 3 -- Three-temperature model. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. // 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. +// 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 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: -// 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. -// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. -// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. -// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. -// 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. +// 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. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// 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]. // velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. -// 1.0 -- proposed by Maxwell. -// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. -// 1.146 -- proposed for an additional "fictitious" velocity slip. - -// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. -// 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. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// 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. // nSpeciesLimit: limitter of gas species -// 0 -- not used. -// 1 -- used. -// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction -// 0 -- method 0. -// 1 -- method 1. -// 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) - +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// 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 +// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs. +// 0 -- not used. +// 1 -- used. +// nDiagonalModified: Modified on Diagonal. +// 0 -- not used. +// 1 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. // nAblation: -// 0 -- The wall ablation is not computed. -// 1 -- The wall ablation is computed. +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. // isInjection: -// 0 -- The injection velocity of ablation wall is not computed. -// 1 -- The injection velocity of ablation wall is computed. +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. // nViscosityModel: -// 0 -- Blottner fitting method(N89). -// 1 -- Gupta fitting method(N90). +// 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. +// 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. +// 0 -- stands for selecting the Blotter curve fits mode. +// 1 -- stands for Sutherland relation. // 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. -// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. -// "Gas-Mixture" -- indicates the process of mixing gas without reacting. -// for struct solver mixing two speciesSpeciesA, SpeciesB. -// for unstruct solver mixing multi-speciesO2 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. +// "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. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "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. +// 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. +// 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 - +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. int dg_high_order = 0; int iapplication = 0; int isAdaptiveSolver = 0; -int nm = 5; +int nm = 5; int nEquilibriumGas = 0; -int nPCWCycleStep = 3; -int nRETCycleStep = 3; -int nSLIPCycleStep= 3; +int nPCWCycleStep = 3; +int nRETCycleStep = 3; +int nSLIPCycleStep = 3; int nIterFirstStep = 1000; int nIterSecondStep= 2000; int nIterThirdStep = 2000; @@ -1065,17 +1084,17 @@ double secondStepError = 0.001; double thirdStepError = 0.001; double predictCFLError = 0.1; -double refGama = 1.4; -double prl = 0.72; -double prt = 0.90; -double sc_l = 0.5; -double sc_t = 0.5; +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 nGasModel = 0; +int nchem = 0; +int nchemsrc = 1; +int nchemrad = 1; +int ntmodel = 1; int nIdealState = 0; int nEnergyRecycle = 1; @@ -1099,12 +1118,12 @@ double sigmaTemperature = 1.0; double sigmaMassFraction = 1.0; double velocitySlipCorrectConstant = 1.0; -double chemicalRelaxCorf = 1.0; +double chemicalRelaxCorf = 1.0; double chemicalSpectrumRadiusCoef = 1.0; double viscousSpectrumRadiusCoef = 1.5; double inviscidSpectrumRadiusCoef = 1.5; -double spectrumRadiusCoef = 0.5; -double staticPressureRelaxCorf = 0.2; +double spectrumRadiusCoef = 0.5; +double staticPressureRelaxCorf = 0.2; double maxViscous = 10000.0; double trTemperatureMin = 10.0; @@ -1114,31 +1133,35 @@ double densityMin = 1.0e-8; double densityMinFactor = 0.1; double tAdjustmentFactor = 10.0; double iniSpeedCoef = 1.0; +int iniSpeedMode = 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 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 nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; -int nProtectData = 0; -int useHyflowSetting = 0; -int nAblation = 0; -int isInjection = 0; -int nViscosityModel = 0; -int nMarsModel = 0; -string gasfile = "DK5"; -//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; string speciesName = "O, O2, NO, N, N2"; string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; @@ -1152,16 +1175,16 @@ 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 = "Pa"; +//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"; -//string gasfile = "Combustion-12"; +//string gasfile = "Combustion-12"; //string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; //string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; //string gasfile = "Gas-Mixture"; -//string speciesName ="SpeciesA, SpeciesB"; +//string speciesName = "SpeciesA, SpeciesB"; //string initMassFraction = "1.0, 0.0"; int nSutherland = 0; double gamaSpeciesA = 1.4; @@ -1173,9 +1196,17 @@ double molecularWeightSpeciesB = 30.0; //string speciesName = "O2, N2"; //string initMassFraction = "1.0, 0.0"; +int nFraction = 0; int nContinueModel = 0; int nChemicalFlowStep = 0; int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; ######################################################################### // Multi-Grid parameters. @@ -1196,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0; // 1 -- zero order. // 2 -- first-order. (default) // mgCorrectionLimit: Multi-grid correction limit. - int nMGLevel = 1; int MGCoarsestIteration = 1; int MGPreIteration = 1; @@ -1218,20 +1248,20 @@ 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"; +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 # -######################################################################### +#************************************************************************ +# High Order Struct Solver * +#************************************************************************ // isFVMOrFDM: -// 0 -- NSSolverStruct using Finite Volume Method. -// 1 -- NSSolverStruct using Finite Differ Method. +// 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) @@ -1273,30 +1303,48 @@ int allReduceStep = 1; // codeOfOversetGrid: Overlapping(overset) grid or not. // 0 -- NON-overlapping grid. // 1 -- Overlapping grid. -// oversetInterpolationMethod: the method of overset interpolation while field simulation +// oversetInterpolationMethod: the method of overset interpolation while field simulation. // 0 -- set the acceptor cell value by donor cell value. // 1 -- set the acceptor cell value by distance weight of donor cell value. - -int codeOfOversetGrid = 0; -int oversetInterpolationMethod = 0; -int readOversetFileOrNot = 0; -int symetryOrNot = 0; -int readInAuxiliaryInnerGrid = 0; -int readInAuxiliaryOuterGrid = 0; -int readInSklFileOrNot = 0; -string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; -string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; -string auxiliaryInnerGrid2 = ""; -string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; - -int numberOfMovingBodies = 2; +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; // ----------------- ALE configuration ------------------------------ int codeOfAleModel = 0; @@ -1306,36 +1354,42 @@ 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; +int strategyForFaceNormalVelocity = 0; // 0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd. +int strategyForGCLSource = 0; // 0-present; 1-Ahn. -//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. int methodForKineticEquation = 0; double relaxParameterOfKinetic = 1.0; -######################################################################### -# motive information # -######################################################################### +#************************************************************************ +# motive information * +#************************************************************************ int numberOfMovingBodies = 1; ############################## body0 ############################## -//mass of parts -double mass_0 = 1.0; -//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz -double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; -//initial six DOF position information of parts. xc yc zc -double massCenter_0[] = 0.0 , 0.0, 0.0; -//initial six DOF position information of parts. angleX angleY angleZ -double attitudeAngle_0[] = 0.0 , 0.0, 0.0; -//initial six DOF move information of parts. vc vy vz -double massCenterVelocity_0[] = 0.0, 0.0, 0.0; -//initial six DOF move information of parts. omigX omigY omigZ -double angularVelocity_0[] = 0.0, 0.0, 0.0; -//the object that the parts belong to. -int fartherIndex_0 = -1; -//the assembly position of the parts. xc yc zc angleX angleY angleZ -double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0; -//the move pattern of the parts. +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. // -1 given motion partten. // 0 still. // 1 six DOF motion. @@ -1346,51 +1400,68 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 // 14 forced pitch motion. // 15 forced yaw motion. // 16 forced roll motion. -int RBDMethod_0 = 0; -double amplitude_0 = 0.0; -double reduceFrequency_0 = 0.0; -//direction of rotation +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 ; -//additional moment of Force (system axis) mX mY mZ -double addedMoment_0[] = 0.0 ,0.0 ,0.0 ; -//the deformation method of the parts. -int morphing_0 = 0; - -// post indentify -int integralOrder = 4; +int direction_0 = -1; +double rotateFrequency_0 = 0.0; +//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; +// post indentify. +int integralOrder = 4; // ---------------- ATP read -------------------------------------------- -//@int inflowParaType = 0; +//@int inflowParaType = 0; //@double refReNumber = 6.5e6; //@double refDimensionalTemperature = 288.15; //@double freestream_vibration_temperature = 300.00; -//@double refDimensionalPressure = 0; -//@double height = 0; -//@int nsubsonicInlet = 0; -//@int nsubsonicOutlet = 0; -//@string inLetFileName = "./bin/subsonicInlet.hypara"; -//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; //@double refDimensionalVelocity = 0; //@double refDimensionalDensity = 0; - -######################################################################### -# Old Parameter # -######################################################################### +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ int isPlotVolumeField = 0; +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; -######################################################################### -# Incompressible Parameter # -######################################################################### +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ int isSolveEnergyEquation = 0; int isSolveTurbEquation = 0; -int isSolveSpeciesEquation = 0; - +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/F08-ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU/bin/grid_para.hypara b/F08-ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU/bin/grid_para.hypara index 45b5f8b..2676cea 100644 --- a/F08-ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU/bin/grid_para.hypara +++ b/F08-ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU/bin/grid_para.hypara @@ -4,9 +4,12 @@ // 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. +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. // from_gtype: Type of grid data type in grid conversion process. // -1 -- MULTI_TYPE // 1 -- HyperFLOW( PHengLEI ), *.fts. @@ -18,7 +21,9 @@ // 7 -- Hybrid, include both of unstructured and structured grid, *.fts. // 8 -- GMSH, *.msh. int gridtype = 1; -int axisup = 1; +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; int from_gtype = 2; ######################################################################### diff --git a/F08-ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU/三维结构Finner弹体俯仰振荡_算例说明文档.pdf b/F08-ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU/三维结构Finner弹体俯仰振荡_算例说明文档.pdf index 1510f86..4039e47 100644 Binary files a/F08-ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU/三维结构Finner弹体俯仰振荡_算例说明文档.pdf and b/F08-ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU/三维结构Finner弹体俯仰振荡_算例说明文档.pdf differ diff --git a/F09-ThreeD_Brid_GridDeformationSPRING_Unstruct_1CPU/bin/cfd_para.hypara b/F09-ThreeD_Brid_GridDeformationSPRING_Unstruct_1CPU/bin/cfd_para.hypara index c344658..f903a5a 100644 --- a/F09-ThreeD_Brid_GridDeformationSPRING_Unstruct_1CPU/bin/cfd_para.hypara +++ b/F09-ThreeD_Brid_GridDeformationSPRING_Unstruct_1CPU/bin/cfd_para.hypara @@ -8,23 +8,24 @@ // Platform for Hybrid Engineering Simulation of Flows + // China Aerodynamics Research and Development Center + // (C) Copyright, Since 2010 + +// PHengLEI 2212 + //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ########################################################################### # 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. -// 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. +// 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. +// 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. @@ -46,19 +47,24 @@ 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. -int axisup = 1; +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; // 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; +int omitRepeatInterface = 1; //----------------------------------------------------------------------- # Grid data type # @@ -87,10 +93,9 @@ 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. int numberOfGridFile = 1; -string from_gfile = "./grid/rae2822_hybrid2d.cas"; -string from_gfile1= ""; - -string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; // ----------------- some advanced choices ------------------------------ // iunsteady: The Grid is for unsteady simulation or not. @@ -103,9 +108,9 @@ 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"; +// 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; @@ -119,31 +124,31 @@ string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp"; // 0 -- Not. (default) // 1 -- Yes. // geometryUnit: Geometry unit. -// 1 -- meter. -// 2 -- millimeter. -// 3 -- inch. +// 1 -- meter. +// 2 -- millimeter. +// 3 -- inch. // exclusiveCase: Parallel projection exclusive case. -// 0 -- NON case. -// 1 -- JSM-C2-NPOFF case. -// 2 -- CHNT. +// 0 -- NON case. +// 1 -- JSM-C2-NPOFF case. +// 2 -- CHNT. // projectOrgPoint: If the original wall points need to be projected or not. -int anisoRefine = 0; -int geometryUnit = 1; -int isProject = 0; -int readDist = 0; -int isDeform = 0; +int anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; int exclusiveCase = 0; int projectOrgPoint = 0; string geometryFileName = "./grid/jsm.igs"; // ----------------- Grid Deform Parameters ----------------------------- // deformationMethod: Grid Deform. -// 1 -- SPRING. -// 2 -- RBF. +// 1 -- SPRING. +// 2 -- RBF. // stationalGridFile: Original grid file. // visualFileName : The visualization file path of deform grid. // nDeformStep : The max deform step. -// flapAngle : The max flap angle. +// flapAngle : The max flap angle. // rotatePostionZ : Rotate postion. // rotatePostionY : Rotate postion. // gridSlice : If dump slice grid. @@ -163,10 +168,10 @@ int sliceAxis = 1; double slicePosition = 13; // ----------------- RBF Parameters ------------------------------------- -// numberOfReferenceCP : Number of reference Control Points. -// influencePara : The RBF influence radius parameter. +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. int numberOfReferenceCP = 40; -double influencePara = 25.0; +double influencePara = 25.0; // ----------------- Periodic Parameters -------------------------------- // Notice: Rotational periodicity only support rotation along the X axis! @@ -178,9 +183,8 @@ double influencePara = 25.0; which only support one direction. // rotationAngle: The relative angle between two periodic face. which is recorded in degrees. - int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; +double translationLength[] = [0.0, 0.0, 0.0]; double rotationAngle = 0.0; ######################################################################### @@ -192,7 +196,6 @@ double rotationAngle = 0.0; // 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; @@ -201,20 +204,20 @@ int numberOfMultifile = 1; // 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. +// cellIndexOfMark : the cell index of mark, only for structured grid partition. int traceMark = 0; int blockIndexOfMark = 0; -int cellIndexOfMark[] = [185,30,1]; +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; +// parallelStrategy: +// 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). +// 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"; @@ -232,11 +235,10 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts"; // 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; +double parmetisBalance = 1.05; // numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. // 1 -- single level. @@ -248,29 +250,35 @@ 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. +// 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; +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; int intervalStepSample = 1000; -int intervalStepForce = 100; -int intervalStepRes = 10; -int ifLowSpeedPrecon = 0; +int intervalStepForce = 100; +int intervalStepRes = 10; // compressible: // 0 -- incompressible flow. // 1 -- compressible flow. (default) int compressible = 1; +// 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) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 1; + //----------------------------------------------------------------------- # CFD Control Parameter # //----------------------------------------------------------------------- @@ -281,33 +289,36 @@ int compressible = 1; // 0 -- the nondimensional conditions. // 1 -- the flight conditions. // 2 -- the experiment conditions. -// 3 -- the subsonic boundary conditions. +// 3 -- the subsonic boundary conditions. (Useless!) // 4 -- the condition that the velocity, temperature and density are given. // 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 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. +// 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 = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. // forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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. -// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol. +// 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; +int directionMethod = 0; double refMachNumber = 0.73; double attackd = 2.79; double angleSlide = 0.00; +int flowInitMethod = 0; int inflowParaType = 0; double refReNumber = 6.5e6; @@ -321,29 +332,27 @@ double freestream_vibration_temperature = 300.00; //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; - -//The velocity, temperature and density are fixed. +// The velocity, temperature and density are fixed. //int inflowParaType = 4; //double refDimensionalVelocity = 1000.0; -//double refDimensionalDensity = 1.0e3; +//double refDimensionalDensity = 1.0e3; -//The velocity, temperature and pressure are fixed. +// The velocity, temperature and pressure are fixed. //int inflowParaType = 5; //double refDimensionalVelocity = 1000.0; //double refDimensionalPressure = 1.0e5; -//The MachNumber, temperature and pressure are fixed. +// The MachNumber, temperature and pressure are fixed. //int inflowParaType = 6; -//double refDimensionalTemperature = 293; +//double refDimensionalTemperature = 293.0; //double refDimensionalPressure = 8886.06; +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; + double wallTemperature = -1.0; double radiationCoef = 0.8; @@ -357,41 +366,41 @@ 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. +double knudsenLength = 1.0; // unit of meter. double refMolecularWeight = 28.9644; // unit of g/mol. //----------------------------------------------------------------------- # Spatial Discretisation # //----------------------------------------------------------------------- -#******************************************************************* -# Struct Solver * -#******************************************************************* +#************************************************************************ +# 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". +// -- "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. +// 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" - +// -- "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"; +string str_limiter_name = "vanalbada"; -#******************************************************************* -# UnStruct Solver or Common * -#******************************************************************* +#************************************************************************ +# UnStruct Solver or Common * +#************************************************************************ // viscousType: Viscous model. -// 0 -- Euler. -// 1 -- Lamilar. -// 2 -- Algebraic. -// 3 -- 1eq turbulent. -// 4 -- 2eq turbulent. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. // viscousName: Laminar or tubulent model. // -- "0eq-bl". // -- "1eq-sa". @@ -410,16 +419,16 @@ string str_limiter_name = "vanalbada"; // 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". +// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // uns_limiter_name: Limiter of Unstruct grid. -// -- "barth", "vencat", "vanleer", "minmod". -// -- "vanalbada", "smooth", "nnd", "lpz", "1st". +// -- "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". // gradientName: Gradient reconstruction method. -// -- "default", "ggcell", "ggnode", "lsq". +// -- "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. @@ -442,18 +451,18 @@ 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 +// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0. -//int viscousType = 0; +//int viscousType = 0; //string viscousName = "Euler"; -//int viscousType = 1; +//int viscousType = 1; //string viscousName = "laminar"; -int viscousType = 3; +int viscousType = 3; string viscousName = "1eq-sa"; -//int viscousType = 4; +//int viscousType = 4; //string viscousName = "2eq-kw-menter-sst"; int DESType = 0; @@ -463,7 +472,7 @@ string uns_limiter_name = "vencat"; string uns_vis_name = "test"; string gradientName = "ggnode"; -int ivencat = 7; +int ivencat = 7; double venkatCoeff = 5.0; int reconmeth = 1; int limitVariables = 0; @@ -475,9 +484,9 @@ double roeEntropyScale = 1.0; double AusmpwPlusLimiter = 1.0; -//----------------------------------------------------------------------- -# Temporal Discretisation # -//----------------------------------------------------------------------- +#************************************************************************ +# Temporal Discretisation * +#************************************************************************ // iunsteady: Steady or unsteady. // 0 -- steady. // 1 -- unsteay. @@ -490,51 +499,57 @@ double AusmpwPlusLimiter = 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 = - ^2 -// 1 -- tau = +// 0 -- tau = - ^2 +// 1 -- tau = // 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 -- Line LU-SGS. -// 8 -- Matrix LU-SGS. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 4 -- LU-SGS. +// 5 -- Block LU-SGS. +// 6 -- Jacobian iteration. +// 7 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. // 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. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. // 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. +// 0 --Local. +// 1 --Global. // isUseLocalCFL: use variable number of CFL or not. -// 0 -- global unified CFL number. -// 1 -- local CFL number. +// 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. -// 0 -- no ALE method. -// 1 -- ALE method for non-moving grids. -// 2 -- ALE method for moving grids. -// 3 -- ALE method for deforming grids. +// 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. +// 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; +int iunsteady = 0; double physicalTimeStep = 0.01; double physicalTimeStepDimensional = -0.001; int ifStartFromSteadyResults = 0; @@ -543,39 +558,42 @@ int ifStaticsReynoldsStress = 0; int startStatisticStep = 800000; double statisticalTimePeriod = -1.0; int statisticMethod = 0; -int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2; +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 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 CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; double pMaxForCFL = 0.2; double pMinForCFL = 0.1; double deltaMaxForCFL = 0.2; double magnifyFactorForCFL = 1.1; double reduceFactorForCFL = 0.5; -double ktmax = 1.0e10; +double ktmax = 1.0e10; -int swapDq = 1; +int swapDq = 1; int nLUSGSSweeps = 1; double LUSGSTolerance = 0.01; -int order = 2; +int order = 2; double visl_min = 0.01; double turbCFLScale = 1.0; -double csrv = 2.0; +double csrv = 1.0; double timemax = 1.0e10; double dtsave = -1.0; int maxale = 10; @@ -591,10 +609,9 @@ double lamda[] = [0.5, 1.0]; //int RKStage = 4; //double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; - -//----------------------------------------------------------------------- -# File In or Out # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. @@ -611,20 +628,18 @@ double lamda[] = [0.5, 1.0]; // 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. +// 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. // 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= ""; +// 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; @@ -632,10 +647,12 @@ int cellMethodOrNodeMethod = 0; string resSaveFile = "results/res.dat"; string turbresfile = "results/turbres.dat"; +string transitionResFile = "results/transitionRes.dat"; string aircoeffile = "results/aircoef.dat"; string restartNSFile = "results/flow.dat"; string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; string visualfile = "results/tecflow.plt"; string wall_aircoefile = "results/wall_aircoef.dat"; @@ -645,10 +662,14 @@ string protectionFile0 = "results/flow0.dat"; string protectionFile1 = "results/flow1.dat"; string wall_heatfluxfile = "results/wall_heatflux.dat"; -int nDumpSurfaceInfo = 0; -string wall_varfile = ""; +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; -string jetDefineFile = "bin/jet.hypara"; +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; string sixDofFileName = "results/sixDofInfo.dat"; string derivativeFileName = "results/identify.dat"; @@ -659,7 +680,8 @@ int plotFieldType = 0; // visualfileType: The file type of visualfile. // 0 -- Tecplot binary. // 1 -- Tecplot ASCII. - +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. int visualfileType = 1; // samplefileMode: The dump mode of sample file. @@ -697,21 +719,21 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), 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) +// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. //-----------the optional parameters list for the wall boundary condition---------------- // nVisualWallVariables: The number of visual variables on wall. // visualWallVariables : dumped variable types, listed as following: -// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4), -// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8), -// -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), -Grid Reynolds number on wall(Re_w, 23) +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- 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), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). int nVisualVariables = 8; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; @@ -739,16 +761,18 @@ 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), mach(6). +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). // 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. +// 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; +int dataMonitorType = 0; string probesDefineFile = "bin/probes_XYZ.dat"; //int dataMonitorType = 1; @@ -761,28 +785,26 @@ string probesDefineFile = "bin/probes_XYZ.dat"; int searchCellsMethod = 0; -int nProbeVariables = 7; -int probeVariables[] = [0, 1, 2, 3, 4, 5, 6]; -int probeVariablesInterpolationMethod = 0; -//----------------------------------------------------------------------- -# Turbulence Parameter # -//----------------------------------------------------------------------- +int nProbeVariables = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +int probeVariablesInterpolationMethod = 0; + +#************************************************************************ +# Turbulence Parameter * +#************************************************************************ // turbInterval: Iteration number of turbulence. // kindOfTurbSource: Kinds of turbulent source. // 0 -- Original. // mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0. -// transitionType: transition model type +// 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 - - +// 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; 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; @@ -790,29 +812,28 @@ int transitionType = 0; double turbIntensity = -1.0; int freeturbIntensitySRModify = 0; double freeDecayXLocation = 0.0; -int compressibleCorrection = 0; -int prandtlNumberCorrection = 0; +int compressibleCorrection = 0; int transitionMaFix = 1; -# maximum eddy viscosity (myt/my) max. +// maximum eddy viscosity (myt/my) max. double eddyViscosityLimit = 1.0e10; int monitor_vistmax = 0; -//----------------------------------------------------------------------- -# LES Parameter # -//----------------------------------------------------------------------- +#************************************************************************ +# LES Parameter * +#************************************************************************ // iLES: Create LESSolver or not. -// = 1 - Create LESSolver; -// != 1 - 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. +// = 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. +// = 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. @@ -820,23 +841,22 @@ int monitor_vistmax = 0; // = "dsmCom"; // = "wale"; // = "sigma". -// 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. +// 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. +// = 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. +// 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; @@ -852,19 +872,16 @@ double testFilterScale = 2.0; int averageWidth = 1; int monitorNegativeConstant = 0; -//----------------------------------------------------------------------- -# Other Parameters for Hypersonic Non-equilibrium Gas # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. -// 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. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. @@ -875,7 +892,7 @@ int monitorNegativeConstant = 0; // 2 -- Argon. // 3 -- Nitrogen. // nEnergyRecycle: The type of EnergyModel Recycle. -// 0 -- not used . +// 0 -- not used. // 1 -- used. // nDensityModify: The type of densitymodify. // 0 -- not used. @@ -883,26 +900,25 @@ int monitorNegativeConstant = 0; // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. -// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. // 0 -- perfect gas. // 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. -// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. -// the value equals to or is greater than 1, and 3 is for default value. -// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. -// the value equals to or is greater than 1, and 3 is for default value. -// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. -// the value equals to or is greater than 1, and 3 is for default value. -// nSlipBCModel : The computational model of slip boundary conditions. - -// 0 -- no slip. -// 1 -- the conventional Maxwell slip conditions. -// 2 -- the Gokcen slip conditions. -// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. -// 4 -- the Kogan simplified slip conditions. -// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. -// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). -// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. -// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). // nchemsrc: // 0 -- the source terms are not computed. // 1 -- the source terms are computed. @@ -913,148 +929,151 @@ int monitorNegativeConstant = 0; // 1 -- One-temperature model. // 2 -- Two-temperature model. // 3 -- Three-temperature model. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. // 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. +// 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 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: -// 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. -// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. -// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. -// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. -// 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. +// 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. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// 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]. // velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. -// 1.0 -- proposed by Maxwell. -// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. -// 1.146 -- proposed for an additional "fictitious" velocity slip. - -// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. -// 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. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// 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. // nSpeciesLimit: limitter of gas species -// 0 -- not used. -// 1 -- used. -// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction -// 0 -- method 0. -// 1 -- method 1. -// 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) - +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// 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 +// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs. +// 0 -- not used. +// 1 -- used. +// nDiagonalModified: Modified on Diagonal. +// 0 -- not used. +// 1 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. // nAblation: -// 0 -- The wall ablation is not computed. -// 1 -- The wall ablation is computed. +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. // isInjection: -// 0 -- The injection velocity of ablation wall is not computed. -// 1 -- The injection velocity of ablation wall is computed. +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. // nViscosityModel: -// 0 -- Blottner fitting method(N89). -// 1 -- Gupta fitting method(N90). +// 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. +// 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. +// 0 -- stands for selecting the Blotter curve fits mode. +// 1 -- stands for Sutherland relation. // 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. -// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. -// "Gas-Mixture" -- indicates the process of mixing gas without reacting. -// for struct solver mixing two speciesSpeciesA, SpeciesB. -// for unstruct solver mixing multi-speciesO2 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. +// "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. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "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. +// 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. +// 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 - +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. int dg_high_order = 0; int iapplication = 0; int isAdaptiveSolver = 0; -int nm = 5; +int nm = 5; int nEquilibriumGas = 0; -int nPCWCycleStep = 3; -int nRETCycleStep = 3; -int nSLIPCycleStep= 3; +int nPCWCycleStep = 3; +int nRETCycleStep = 3; +int nSLIPCycleStep = 3; int nIterFirstStep = 1000; int nIterSecondStep= 2000; int nIterThirdStep = 2000; @@ -1065,17 +1084,17 @@ double secondStepError = 0.001; double thirdStepError = 0.001; double predictCFLError = 0.1; -double refGama = 1.4; -double prl = 0.72; -double prt = 0.90; -double sc_l = 0.5; -double sc_t = 0.5; +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 nGasModel = 0; +int nchem = 0; +int nchemsrc = 1; +int nchemrad = 1; +int ntmodel = 1; int nIdealState = 0; int nEnergyRecycle = 1; @@ -1099,12 +1118,12 @@ double sigmaTemperature = 1.0; double sigmaMassFraction = 1.0; double velocitySlipCorrectConstant = 1.0; -double chemicalRelaxCorf = 1.0; +double chemicalRelaxCorf = 1.0; double chemicalSpectrumRadiusCoef = 1.0; double viscousSpectrumRadiusCoef = 1.5; double inviscidSpectrumRadiusCoef = 1.5; -double spectrumRadiusCoef = 0.5; -double staticPressureRelaxCorf = 0.2; +double spectrumRadiusCoef = 0.5; +double staticPressureRelaxCorf = 0.2; double maxViscous = 10000.0; double trTemperatureMin = 10.0; @@ -1114,31 +1133,35 @@ double densityMin = 1.0e-8; double densityMinFactor = 0.1; double tAdjustmentFactor = 10.0; double iniSpeedCoef = 1.0; +int iniSpeedMode = 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 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 nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; -int nProtectData = 0; -int useHyflowSetting = 0; -int nAblation = 0; -int isInjection = 0; -int nViscosityModel = 0; -int nMarsModel = 0; -string gasfile = "DK5"; -//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; string speciesName = "O, O2, NO, N, N2"; string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; @@ -1152,16 +1175,16 @@ 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 = "Pa"; +//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"; -//string gasfile = "Combustion-12"; +//string gasfile = "Combustion-12"; //string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; //string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; //string gasfile = "Gas-Mixture"; -//string speciesName ="SpeciesA, SpeciesB"; +//string speciesName = "SpeciesA, SpeciesB"; //string initMassFraction = "1.0, 0.0"; int nSutherland = 0; double gamaSpeciesA = 1.4; @@ -1173,9 +1196,17 @@ double molecularWeightSpeciesB = 30.0; //string speciesName = "O2, N2"; //string initMassFraction = "1.0, 0.0"; +int nFraction = 0; int nContinueModel = 0; int nChemicalFlowStep = 0; int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; ######################################################################### // Multi-Grid parameters. @@ -1196,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0; // 1 -- zero order. // 2 -- first-order. (default) // mgCorrectionLimit: Multi-grid correction limit. - int nMGLevel = 1; int MGCoarsestIteration = 1; int MGPreIteration = 1; @@ -1218,20 +1248,20 @@ 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"; +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 # -######################################################################### +#************************************************************************ +# High Order Struct Solver * +#************************************************************************ // isFVMOrFDM: -// 0 -- NSSolverStruct using Finite Volume Method. -// 1 -- NSSolverStruct using Finite Differ Method. +// 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) @@ -1273,30 +1303,48 @@ int allReduceStep = 1; // codeOfOversetGrid: Overlapping(overset) grid or not. // 0 -- NON-overlapping grid. // 1 -- Overlapping grid. -// oversetInterpolationMethod: the method of overset interpolation while field simulation +// oversetInterpolationMethod: the method of overset interpolation while field simulation. // 0 -- set the acceptor cell value by donor cell value. // 1 -- set the acceptor cell value by distance weight of donor cell value. - -int codeOfOversetGrid = 0; -int oversetInterpolationMethod = 0; -int readOversetFileOrNot = 0; -int symetryOrNot = 0; -int readInAuxiliaryInnerGrid = 0; -int readInAuxiliaryOuterGrid = 0; -int readInSklFileOrNot = 0; -string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; -string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; -string auxiliaryInnerGrid2 = ""; -string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; - -int numberOfMovingBodies = 2; +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; // ----------------- ALE configuration ------------------------------ int codeOfAleModel = 0; @@ -1306,36 +1354,42 @@ 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; +int strategyForFaceNormalVelocity = 0; // 0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd. +int strategyForGCLSource = 0; // 0-present; 1-Ahn. -//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. int methodForKineticEquation = 0; double relaxParameterOfKinetic = 1.0; -######################################################################### -# motive information # -######################################################################### +#************************************************************************ +# motive information * +#************************************************************************ int numberOfMovingBodies = 1; ############################## body0 ############################## -//mass of parts -double mass_0 = 1.0; -//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz -double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; -//initial six DOF position information of parts. xc yc zc -double massCenter_0[] = 0.0 , 0.0, 0.0; -//initial six DOF position information of parts. angleX angleY angleZ -double attitudeAngle_0[] = 0.0 , 0.0, 0.0; -//initial six DOF move information of parts. vc vy vz -double massCenterVelocity_0[] = 0.0, 0.0, 0.0; -//initial six DOF move information of parts. omigX omigY omigZ -double angularVelocity_0[] = 0.0, 0.0, 0.0; -//the object that the parts belong to. -int fartherIndex_0 = -1; -//the assembly position of the parts. xc yc zc angleX angleY angleZ -double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0; -//the move pattern of the parts. +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. // -1 given motion partten. // 0 still. // 1 six DOF motion. @@ -1346,51 +1400,68 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 // 14 forced pitch motion. // 15 forced yaw motion. // 16 forced roll motion. -int RBDMethod_0 = 0; -double amplitude_0 = 0.0; -double reduceFrequency_0 = 0.0; -//direction of rotation +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 ; -//additional moment of Force (system axis) mX mY mZ -double addedMoment_0[] = 0.0 ,0.0 ,0.0 ; -//the deformation method of the parts. -int morphing_0 = 0; - -// post indentify -int integralOrder = 4; +int direction_0 = -1; +double rotateFrequency_0 = 0.0; +//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; +// post indentify. +int integralOrder = 4; // ---------------- ATP read -------------------------------------------- -//@int inflowParaType = 0; +//@int inflowParaType = 0; //@double refReNumber = 6.5e6; //@double refDimensionalTemperature = 288.15; //@double freestream_vibration_temperature = 300.00; -//@double refDimensionalPressure = 0; -//@double height = 0; -//@int nsubsonicInlet = 0; -//@int nsubsonicOutlet = 0; -//@string inLetFileName = "./bin/subsonicInlet.hypara"; -//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; //@double refDimensionalVelocity = 0; //@double refDimensionalDensity = 0; - -######################################################################### -# Old Parameter # -######################################################################### +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ int isPlotVolumeField = 0; +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; -######################################################################### -# Incompressible Parameter # -######################################################################### +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ int isSolveEnergyEquation = 0; int isSolveTurbEquation = 0; -int isSolveSpeciesEquation = 0; - +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/F09-ThreeD_Brid_GridDeformationSPRING_Unstruct_1CPU/bin/grid_para.hypara b/F09-ThreeD_Brid_GridDeformationSPRING_Unstruct_1CPU/bin/grid_para.hypara index efcaa55..3899a80 100644 --- a/F09-ThreeD_Brid_GridDeformationSPRING_Unstruct_1CPU/bin/grid_para.hypara +++ b/F09-ThreeD_Brid_GridDeformationSPRING_Unstruct_1CPU/bin/grid_para.hypara @@ -4,9 +4,12 @@ // 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. +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. // from_gtype: Type of grid data type in grid conversion process. // -1 -- MULTI_TYPE. // 1 -- PHengLEI, *.fts. @@ -18,7 +21,9 @@ // 7 -- Hybrid, include both of unstructured and structured grid, *.fts. // 8 -- GMSH, *.msh. int gridtype = 0; -int axisup = 1; +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; int from_gtype = 2; ######################################################################### diff --git a/F09-ThreeD_Brid_GridDeformationSPRING_Unstruct_1CPU/三维非结构扑翼动网格_算例说明文档 - SPRING.pdf b/F09-ThreeD_Brid_GridDeformationSPRING_Unstruct_1CPU/三维非结构扑翼动网格_算例说明文档 - SPRING.pdf index 9c731ca..f9603df 100644 Binary files a/F09-ThreeD_Brid_GridDeformationSPRING_Unstruct_1CPU/三维非结构扑翼动网格_算例说明文档 - SPRING.pdf and b/F09-ThreeD_Brid_GridDeformationSPRING_Unstruct_1CPU/三维非结构扑翼动网格_算例说明文档 - SPRING.pdf differ diff --git a/F10-ThreeD_Brid_GridDeformationRBF_Unstruct_1CPU/bin/cfd_para.hypara b/F10-ThreeD_Brid_GridDeformationRBF_Unstruct_1CPU/bin/cfd_para.hypara index c344658..f903a5a 100644 --- a/F10-ThreeD_Brid_GridDeformationRBF_Unstruct_1CPU/bin/cfd_para.hypara +++ b/F10-ThreeD_Brid_GridDeformationRBF_Unstruct_1CPU/bin/cfd_para.hypara @@ -8,23 +8,24 @@ // Platform for Hybrid Engineering Simulation of Flows + // China Aerodynamics Research and Development Center + // (C) Copyright, Since 2010 + +// PHengLEI 2212 + //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ########################################################################### # 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. -// 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. +// 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. +// 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. @@ -46,19 +47,24 @@ 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. -int axisup = 1; +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; // 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; +int omitRepeatInterface = 1; //----------------------------------------------------------------------- # Grid data type # @@ -87,10 +93,9 @@ 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. int numberOfGridFile = 1; -string from_gfile = "./grid/rae2822_hybrid2d.cas"; -string from_gfile1= ""; - -string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; // ----------------- some advanced choices ------------------------------ // iunsteady: The Grid is for unsteady simulation or not. @@ -103,9 +108,9 @@ 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"; +// 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; @@ -119,31 +124,31 @@ string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp"; // 0 -- Not. (default) // 1 -- Yes. // geometryUnit: Geometry unit. -// 1 -- meter. -// 2 -- millimeter. -// 3 -- inch. +// 1 -- meter. +// 2 -- millimeter. +// 3 -- inch. // exclusiveCase: Parallel projection exclusive case. -// 0 -- NON case. -// 1 -- JSM-C2-NPOFF case. -// 2 -- CHNT. +// 0 -- NON case. +// 1 -- JSM-C2-NPOFF case. +// 2 -- CHNT. // projectOrgPoint: If the original wall points need to be projected or not. -int anisoRefine = 0; -int geometryUnit = 1; -int isProject = 0; -int readDist = 0; -int isDeform = 0; +int anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; int exclusiveCase = 0; int projectOrgPoint = 0; string geometryFileName = "./grid/jsm.igs"; // ----------------- Grid Deform Parameters ----------------------------- // deformationMethod: Grid Deform. -// 1 -- SPRING. -// 2 -- RBF. +// 1 -- SPRING. +// 2 -- RBF. // stationalGridFile: Original grid file. // visualFileName : The visualization file path of deform grid. // nDeformStep : The max deform step. -// flapAngle : The max flap angle. +// flapAngle : The max flap angle. // rotatePostionZ : Rotate postion. // rotatePostionY : Rotate postion. // gridSlice : If dump slice grid. @@ -163,10 +168,10 @@ int sliceAxis = 1; double slicePosition = 13; // ----------------- RBF Parameters ------------------------------------- -// numberOfReferenceCP : Number of reference Control Points. -// influencePara : The RBF influence radius parameter. +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. int numberOfReferenceCP = 40; -double influencePara = 25.0; +double influencePara = 25.0; // ----------------- Periodic Parameters -------------------------------- // Notice: Rotational periodicity only support rotation along the X axis! @@ -178,9 +183,8 @@ double influencePara = 25.0; which only support one direction. // rotationAngle: The relative angle between two periodic face. which is recorded in degrees. - int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; +double translationLength[] = [0.0, 0.0, 0.0]; double rotationAngle = 0.0; ######################################################################### @@ -192,7 +196,6 @@ double rotationAngle = 0.0; // 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; @@ -201,20 +204,20 @@ int numberOfMultifile = 1; // 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. +// cellIndexOfMark : the cell index of mark, only for structured grid partition. int traceMark = 0; int blockIndexOfMark = 0; -int cellIndexOfMark[] = [185,30,1]; +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; +// parallelStrategy: +// 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). +// 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"; @@ -232,11 +235,10 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts"; // 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; +double parmetisBalance = 1.05; // numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. // 1 -- single level. @@ -248,29 +250,35 @@ 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. +// 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; +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; int intervalStepSample = 1000; -int intervalStepForce = 100; -int intervalStepRes = 10; -int ifLowSpeedPrecon = 0; +int intervalStepForce = 100; +int intervalStepRes = 10; // compressible: // 0 -- incompressible flow. // 1 -- compressible flow. (default) int compressible = 1; +// 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) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 1; + //----------------------------------------------------------------------- # CFD Control Parameter # //----------------------------------------------------------------------- @@ -281,33 +289,36 @@ int compressible = 1; // 0 -- the nondimensional conditions. // 1 -- the flight conditions. // 2 -- the experiment conditions. -// 3 -- the subsonic boundary conditions. +// 3 -- the subsonic boundary conditions. (Useless!) // 4 -- the condition that the velocity, temperature and density are given. // 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 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. +// 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 = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. // forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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. -// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol. +// 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; +int directionMethod = 0; double refMachNumber = 0.73; double attackd = 2.79; double angleSlide = 0.00; +int flowInitMethod = 0; int inflowParaType = 0; double refReNumber = 6.5e6; @@ -321,29 +332,27 @@ double freestream_vibration_temperature = 300.00; //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; - -//The velocity, temperature and density are fixed. +// The velocity, temperature and density are fixed. //int inflowParaType = 4; //double refDimensionalVelocity = 1000.0; -//double refDimensionalDensity = 1.0e3; +//double refDimensionalDensity = 1.0e3; -//The velocity, temperature and pressure are fixed. +// The velocity, temperature and pressure are fixed. //int inflowParaType = 5; //double refDimensionalVelocity = 1000.0; //double refDimensionalPressure = 1.0e5; -//The MachNumber, temperature and pressure are fixed. +// The MachNumber, temperature and pressure are fixed. //int inflowParaType = 6; -//double refDimensionalTemperature = 293; +//double refDimensionalTemperature = 293.0; //double refDimensionalPressure = 8886.06; +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; + double wallTemperature = -1.0; double radiationCoef = 0.8; @@ -357,41 +366,41 @@ 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. +double knudsenLength = 1.0; // unit of meter. double refMolecularWeight = 28.9644; // unit of g/mol. //----------------------------------------------------------------------- # Spatial Discretisation # //----------------------------------------------------------------------- -#******************************************************************* -# Struct Solver * -#******************************************************************* +#************************************************************************ +# 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". +// -- "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. +// 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" - +// -- "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"; +string str_limiter_name = "vanalbada"; -#******************************************************************* -# UnStruct Solver or Common * -#******************************************************************* +#************************************************************************ +# UnStruct Solver or Common * +#************************************************************************ // viscousType: Viscous model. -// 0 -- Euler. -// 1 -- Lamilar. -// 2 -- Algebraic. -// 3 -- 1eq turbulent. -// 4 -- 2eq turbulent. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. // viscousName: Laminar or tubulent model. // -- "0eq-bl". // -- "1eq-sa". @@ -410,16 +419,16 @@ string str_limiter_name = "vanalbada"; // 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". +// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // uns_limiter_name: Limiter of Unstruct grid. -// -- "barth", "vencat", "vanleer", "minmod". -// -- "vanalbada", "smooth", "nnd", "lpz", "1st". +// -- "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". // gradientName: Gradient reconstruction method. -// -- "default", "ggcell", "ggnode", "lsq". +// -- "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. @@ -442,18 +451,18 @@ 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 +// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0. -//int viscousType = 0; +//int viscousType = 0; //string viscousName = "Euler"; -//int viscousType = 1; +//int viscousType = 1; //string viscousName = "laminar"; -int viscousType = 3; +int viscousType = 3; string viscousName = "1eq-sa"; -//int viscousType = 4; +//int viscousType = 4; //string viscousName = "2eq-kw-menter-sst"; int DESType = 0; @@ -463,7 +472,7 @@ string uns_limiter_name = "vencat"; string uns_vis_name = "test"; string gradientName = "ggnode"; -int ivencat = 7; +int ivencat = 7; double venkatCoeff = 5.0; int reconmeth = 1; int limitVariables = 0; @@ -475,9 +484,9 @@ double roeEntropyScale = 1.0; double AusmpwPlusLimiter = 1.0; -//----------------------------------------------------------------------- -# Temporal Discretisation # -//----------------------------------------------------------------------- +#************************************************************************ +# Temporal Discretisation * +#************************************************************************ // iunsteady: Steady or unsteady. // 0 -- steady. // 1 -- unsteay. @@ -490,51 +499,57 @@ double AusmpwPlusLimiter = 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 = - ^2 -// 1 -- tau = +// 0 -- tau = - ^2 +// 1 -- tau = // 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 -- Line LU-SGS. -// 8 -- Matrix LU-SGS. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 4 -- LU-SGS. +// 5 -- Block LU-SGS. +// 6 -- Jacobian iteration. +// 7 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. // 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. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. // 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. +// 0 --Local. +// 1 --Global. // isUseLocalCFL: use variable number of CFL or not. -// 0 -- global unified CFL number. -// 1 -- local CFL number. +// 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. -// 0 -- no ALE method. -// 1 -- ALE method for non-moving grids. -// 2 -- ALE method for moving grids. -// 3 -- ALE method for deforming grids. +// 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. +// 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; +int iunsteady = 0; double physicalTimeStep = 0.01; double physicalTimeStepDimensional = -0.001; int ifStartFromSteadyResults = 0; @@ -543,39 +558,42 @@ int ifStaticsReynoldsStress = 0; int startStatisticStep = 800000; double statisticalTimePeriod = -1.0; int statisticMethod = 0; -int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2; +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 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 CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; double pMaxForCFL = 0.2; double pMinForCFL = 0.1; double deltaMaxForCFL = 0.2; double magnifyFactorForCFL = 1.1; double reduceFactorForCFL = 0.5; -double ktmax = 1.0e10; +double ktmax = 1.0e10; -int swapDq = 1; +int swapDq = 1; int nLUSGSSweeps = 1; double LUSGSTolerance = 0.01; -int order = 2; +int order = 2; double visl_min = 0.01; double turbCFLScale = 1.0; -double csrv = 2.0; +double csrv = 1.0; double timemax = 1.0e10; double dtsave = -1.0; int maxale = 10; @@ -591,10 +609,9 @@ double lamda[] = [0.5, 1.0]; //int RKStage = 4; //double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; - -//----------------------------------------------------------------------- -# File In or Out # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. @@ -611,20 +628,18 @@ double lamda[] = [0.5, 1.0]; // 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. +// 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. // 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= ""; +// 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; @@ -632,10 +647,12 @@ int cellMethodOrNodeMethod = 0; string resSaveFile = "results/res.dat"; string turbresfile = "results/turbres.dat"; +string transitionResFile = "results/transitionRes.dat"; string aircoeffile = "results/aircoef.dat"; string restartNSFile = "results/flow.dat"; string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; string visualfile = "results/tecflow.plt"; string wall_aircoefile = "results/wall_aircoef.dat"; @@ -645,10 +662,14 @@ string protectionFile0 = "results/flow0.dat"; string protectionFile1 = "results/flow1.dat"; string wall_heatfluxfile = "results/wall_heatflux.dat"; -int nDumpSurfaceInfo = 0; -string wall_varfile = ""; +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; -string jetDefineFile = "bin/jet.hypara"; +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; string sixDofFileName = "results/sixDofInfo.dat"; string derivativeFileName = "results/identify.dat"; @@ -659,7 +680,8 @@ int plotFieldType = 0; // visualfileType: The file type of visualfile. // 0 -- Tecplot binary. // 1 -- Tecplot ASCII. - +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. int visualfileType = 1; // samplefileMode: The dump mode of sample file. @@ -697,21 +719,21 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), 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) +// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. //-----------the optional parameters list for the wall boundary condition---------------- // nVisualWallVariables: The number of visual variables on wall. // visualWallVariables : dumped variable types, listed as following: -// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4), -// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8), -// -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), -Grid Reynolds number on wall(Re_w, 23) +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- 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), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). int nVisualVariables = 8; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; @@ -739,16 +761,18 @@ 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), mach(6). +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). // 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. +// 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; +int dataMonitorType = 0; string probesDefineFile = "bin/probes_XYZ.dat"; //int dataMonitorType = 1; @@ -761,28 +785,26 @@ string probesDefineFile = "bin/probes_XYZ.dat"; int searchCellsMethod = 0; -int nProbeVariables = 7; -int probeVariables[] = [0, 1, 2, 3, 4, 5, 6]; -int probeVariablesInterpolationMethod = 0; -//----------------------------------------------------------------------- -# Turbulence Parameter # -//----------------------------------------------------------------------- +int nProbeVariables = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +int probeVariablesInterpolationMethod = 0; + +#************************************************************************ +# Turbulence Parameter * +#************************************************************************ // turbInterval: Iteration number of turbulence. // kindOfTurbSource: Kinds of turbulent source. // 0 -- Original. // mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0. -// transitionType: transition model type +// 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 - - +// 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; 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; @@ -790,29 +812,28 @@ int transitionType = 0; double turbIntensity = -1.0; int freeturbIntensitySRModify = 0; double freeDecayXLocation = 0.0; -int compressibleCorrection = 0; -int prandtlNumberCorrection = 0; +int compressibleCorrection = 0; int transitionMaFix = 1; -# maximum eddy viscosity (myt/my) max. +// maximum eddy viscosity (myt/my) max. double eddyViscosityLimit = 1.0e10; int monitor_vistmax = 0; -//----------------------------------------------------------------------- -# LES Parameter # -//----------------------------------------------------------------------- +#************************************************************************ +# LES Parameter * +#************************************************************************ // iLES: Create LESSolver or not. -// = 1 - Create LESSolver; -// != 1 - 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. +// = 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. +// = 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. @@ -820,23 +841,22 @@ int monitor_vistmax = 0; // = "dsmCom"; // = "wale"; // = "sigma". -// 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. +// 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. +// = 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. +// 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; @@ -852,19 +872,16 @@ double testFilterScale = 2.0; int averageWidth = 1; int monitorNegativeConstant = 0; -//----------------------------------------------------------------------- -# Other Parameters for Hypersonic Non-equilibrium Gas # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. -// 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. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. @@ -875,7 +892,7 @@ int monitorNegativeConstant = 0; // 2 -- Argon. // 3 -- Nitrogen. // nEnergyRecycle: The type of EnergyModel Recycle. -// 0 -- not used . +// 0 -- not used. // 1 -- used. // nDensityModify: The type of densitymodify. // 0 -- not used. @@ -883,26 +900,25 @@ int monitorNegativeConstant = 0; // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. -// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. // 0 -- perfect gas. // 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. -// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. -// the value equals to or is greater than 1, and 3 is for default value. -// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. -// the value equals to or is greater than 1, and 3 is for default value. -// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. -// the value equals to or is greater than 1, and 3 is for default value. -// nSlipBCModel : The computational model of slip boundary conditions. - -// 0 -- no slip. -// 1 -- the conventional Maxwell slip conditions. -// 2 -- the Gokcen slip conditions. -// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. -// 4 -- the Kogan simplified slip conditions. -// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. -// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). -// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. -// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). // nchemsrc: // 0 -- the source terms are not computed. // 1 -- the source terms are computed. @@ -913,148 +929,151 @@ int monitorNegativeConstant = 0; // 1 -- One-temperature model. // 2 -- Two-temperature model. // 3 -- Three-temperature model. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. // 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. +// 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 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: -// 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. -// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. -// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. -// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. -// 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. +// 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. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// 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]. // velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. -// 1.0 -- proposed by Maxwell. -// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. -// 1.146 -- proposed for an additional "fictitious" velocity slip. - -// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. -// 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. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// 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. // nSpeciesLimit: limitter of gas species -// 0 -- not used. -// 1 -- used. -// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction -// 0 -- method 0. -// 1 -- method 1. -// 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) - +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// 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 +// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs. +// 0 -- not used. +// 1 -- used. +// nDiagonalModified: Modified on Diagonal. +// 0 -- not used. +// 1 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. // nAblation: -// 0 -- The wall ablation is not computed. -// 1 -- The wall ablation is computed. +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. // isInjection: -// 0 -- The injection velocity of ablation wall is not computed. -// 1 -- The injection velocity of ablation wall is computed. +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. // nViscosityModel: -// 0 -- Blottner fitting method(N89). -// 1 -- Gupta fitting method(N90). +// 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. +// 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. +// 0 -- stands for selecting the Blotter curve fits mode. +// 1 -- stands for Sutherland relation. // 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. -// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. -// "Gas-Mixture" -- indicates the process of mixing gas without reacting. -// for struct solver mixing two speciesSpeciesA, SpeciesB. -// for unstruct solver mixing multi-speciesO2 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. +// "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. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "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. +// 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. +// 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 - +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. int dg_high_order = 0; int iapplication = 0; int isAdaptiveSolver = 0; -int nm = 5; +int nm = 5; int nEquilibriumGas = 0; -int nPCWCycleStep = 3; -int nRETCycleStep = 3; -int nSLIPCycleStep= 3; +int nPCWCycleStep = 3; +int nRETCycleStep = 3; +int nSLIPCycleStep = 3; int nIterFirstStep = 1000; int nIterSecondStep= 2000; int nIterThirdStep = 2000; @@ -1065,17 +1084,17 @@ double secondStepError = 0.001; double thirdStepError = 0.001; double predictCFLError = 0.1; -double refGama = 1.4; -double prl = 0.72; -double prt = 0.90; -double sc_l = 0.5; -double sc_t = 0.5; +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 nGasModel = 0; +int nchem = 0; +int nchemsrc = 1; +int nchemrad = 1; +int ntmodel = 1; int nIdealState = 0; int nEnergyRecycle = 1; @@ -1099,12 +1118,12 @@ double sigmaTemperature = 1.0; double sigmaMassFraction = 1.0; double velocitySlipCorrectConstant = 1.0; -double chemicalRelaxCorf = 1.0; +double chemicalRelaxCorf = 1.0; double chemicalSpectrumRadiusCoef = 1.0; double viscousSpectrumRadiusCoef = 1.5; double inviscidSpectrumRadiusCoef = 1.5; -double spectrumRadiusCoef = 0.5; -double staticPressureRelaxCorf = 0.2; +double spectrumRadiusCoef = 0.5; +double staticPressureRelaxCorf = 0.2; double maxViscous = 10000.0; double trTemperatureMin = 10.0; @@ -1114,31 +1133,35 @@ double densityMin = 1.0e-8; double densityMinFactor = 0.1; double tAdjustmentFactor = 10.0; double iniSpeedCoef = 1.0; +int iniSpeedMode = 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 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 nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; -int nProtectData = 0; -int useHyflowSetting = 0; -int nAblation = 0; -int isInjection = 0; -int nViscosityModel = 0; -int nMarsModel = 0; -string gasfile = "DK5"; -//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; string speciesName = "O, O2, NO, N, N2"; string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; @@ -1152,16 +1175,16 @@ 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 = "Pa"; +//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"; -//string gasfile = "Combustion-12"; +//string gasfile = "Combustion-12"; //string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; //string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; //string gasfile = "Gas-Mixture"; -//string speciesName ="SpeciesA, SpeciesB"; +//string speciesName = "SpeciesA, SpeciesB"; //string initMassFraction = "1.0, 0.0"; int nSutherland = 0; double gamaSpeciesA = 1.4; @@ -1173,9 +1196,17 @@ double molecularWeightSpeciesB = 30.0; //string speciesName = "O2, N2"; //string initMassFraction = "1.0, 0.0"; +int nFraction = 0; int nContinueModel = 0; int nChemicalFlowStep = 0; int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; ######################################################################### // Multi-Grid parameters. @@ -1196,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0; // 1 -- zero order. // 2 -- first-order. (default) // mgCorrectionLimit: Multi-grid correction limit. - int nMGLevel = 1; int MGCoarsestIteration = 1; int MGPreIteration = 1; @@ -1218,20 +1248,20 @@ 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"; +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 # -######################################################################### +#************************************************************************ +# High Order Struct Solver * +#************************************************************************ // isFVMOrFDM: -// 0 -- NSSolverStruct using Finite Volume Method. -// 1 -- NSSolverStruct using Finite Differ Method. +// 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) @@ -1273,30 +1303,48 @@ int allReduceStep = 1; // codeOfOversetGrid: Overlapping(overset) grid or not. // 0 -- NON-overlapping grid. // 1 -- Overlapping grid. -// oversetInterpolationMethod: the method of overset interpolation while field simulation +// oversetInterpolationMethod: the method of overset interpolation while field simulation. // 0 -- set the acceptor cell value by donor cell value. // 1 -- set the acceptor cell value by distance weight of donor cell value. - -int codeOfOversetGrid = 0; -int oversetInterpolationMethod = 0; -int readOversetFileOrNot = 0; -int symetryOrNot = 0; -int readInAuxiliaryInnerGrid = 0; -int readInAuxiliaryOuterGrid = 0; -int readInSklFileOrNot = 0; -string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; -string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; -string auxiliaryInnerGrid2 = ""; -string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; - -int numberOfMovingBodies = 2; +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; // ----------------- ALE configuration ------------------------------ int codeOfAleModel = 0; @@ -1306,36 +1354,42 @@ 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; +int strategyForFaceNormalVelocity = 0; // 0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd. +int strategyForGCLSource = 0; // 0-present; 1-Ahn. -//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. int methodForKineticEquation = 0; double relaxParameterOfKinetic = 1.0; -######################################################################### -# motive information # -######################################################################### +#************************************************************************ +# motive information * +#************************************************************************ int numberOfMovingBodies = 1; ############################## body0 ############################## -//mass of parts -double mass_0 = 1.0; -//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz -double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; -//initial six DOF position information of parts. xc yc zc -double massCenter_0[] = 0.0 , 0.0, 0.0; -//initial six DOF position information of parts. angleX angleY angleZ -double attitudeAngle_0[] = 0.0 , 0.0, 0.0; -//initial six DOF move information of parts. vc vy vz -double massCenterVelocity_0[] = 0.0, 0.0, 0.0; -//initial six DOF move information of parts. omigX omigY omigZ -double angularVelocity_0[] = 0.0, 0.0, 0.0; -//the object that the parts belong to. -int fartherIndex_0 = -1; -//the assembly position of the parts. xc yc zc angleX angleY angleZ -double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0; -//the move pattern of the parts. +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. // -1 given motion partten. // 0 still. // 1 six DOF motion. @@ -1346,51 +1400,68 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 // 14 forced pitch motion. // 15 forced yaw motion. // 16 forced roll motion. -int RBDMethod_0 = 0; -double amplitude_0 = 0.0; -double reduceFrequency_0 = 0.0; -//direction of rotation +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 ; -//additional moment of Force (system axis) mX mY mZ -double addedMoment_0[] = 0.0 ,0.0 ,0.0 ; -//the deformation method of the parts. -int morphing_0 = 0; - -// post indentify -int integralOrder = 4; +int direction_0 = -1; +double rotateFrequency_0 = 0.0; +//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; +// post indentify. +int integralOrder = 4; // ---------------- ATP read -------------------------------------------- -//@int inflowParaType = 0; +//@int inflowParaType = 0; //@double refReNumber = 6.5e6; //@double refDimensionalTemperature = 288.15; //@double freestream_vibration_temperature = 300.00; -//@double refDimensionalPressure = 0; -//@double height = 0; -//@int nsubsonicInlet = 0; -//@int nsubsonicOutlet = 0; -//@string inLetFileName = "./bin/subsonicInlet.hypara"; -//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; //@double refDimensionalVelocity = 0; //@double refDimensionalDensity = 0; - -######################################################################### -# Old Parameter # -######################################################################### +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ int isPlotVolumeField = 0; +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; -######################################################################### -# Incompressible Parameter # -######################################################################### +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ int isSolveEnergyEquation = 0; int isSolveTurbEquation = 0; -int isSolveSpeciesEquation = 0; - +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/F10-ThreeD_Brid_GridDeformationRBF_Unstruct_1CPU/bin/grid_para.hypara b/F10-ThreeD_Brid_GridDeformationRBF_Unstruct_1CPU/bin/grid_para.hypara index efcaa55..3899a80 100644 --- a/F10-ThreeD_Brid_GridDeformationRBF_Unstruct_1CPU/bin/grid_para.hypara +++ b/F10-ThreeD_Brid_GridDeformationRBF_Unstruct_1CPU/bin/grid_para.hypara @@ -4,9 +4,12 @@ // 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. +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. // from_gtype: Type of grid data type in grid conversion process. // -1 -- MULTI_TYPE. // 1 -- PHengLEI, *.fts. @@ -18,7 +21,9 @@ // 7 -- Hybrid, include both of unstructured and structured grid, *.fts. // 8 -- GMSH, *.msh. int gridtype = 0; -int axisup = 1; +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; int from_gtype = 2; ######################################################################### diff --git a/F10-ThreeD_Brid_GridDeformationRBF_Unstruct_1CPU/三维非结构扑翼动网格RBF_算例说明文档 - RBF.pdf b/F10-ThreeD_Brid_GridDeformationRBF_Unstruct_1CPU/三维非结构扑翼动网格RBF_算例说明文档 - RBF.pdf index 54f2f53..f1e0446 100644 Binary files a/F10-ThreeD_Brid_GridDeformationRBF_Unstruct_1CPU/三维非结构扑翼动网格RBF_算例说明文档 - RBF.pdf and b/F10-ThreeD_Brid_GridDeformationRBF_Unstruct_1CPU/三维非结构扑翼动网格RBF_算例说明文档 - RBF.pdf differ diff --git a/F11_ThreeD_M6_GridParallelRefine_Unstruct_4CPU/bin/cfd_para.hypara b/F11_ThreeD_M6_GridParallelRefine_Unstruct_4CPU/bin/cfd_para.hypara index c344658..f903a5a 100644 --- a/F11_ThreeD_M6_GridParallelRefine_Unstruct_4CPU/bin/cfd_para.hypara +++ b/F11_ThreeD_M6_GridParallelRefine_Unstruct_4CPU/bin/cfd_para.hypara @@ -8,23 +8,24 @@ // Platform for Hybrid Engineering Simulation of Flows + // China Aerodynamics Research and Development Center + // (C) Copyright, Since 2010 + +// PHengLEI 2212 + //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ########################################################################### # 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. -// 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. +// 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. +// 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. @@ -46,19 +47,24 @@ 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. -int axisup = 1; +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; // 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; +int omitRepeatInterface = 1; //----------------------------------------------------------------------- # Grid data type # @@ -87,10 +93,9 @@ 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. int numberOfGridFile = 1; -string from_gfile = "./grid/rae2822_hybrid2d.cas"; -string from_gfile1= ""; - -string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; // ----------------- some advanced choices ------------------------------ // iunsteady: The Grid is for unsteady simulation or not. @@ -103,9 +108,9 @@ 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"; +// 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; @@ -119,31 +124,31 @@ string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp"; // 0 -- Not. (default) // 1 -- Yes. // geometryUnit: Geometry unit. -// 1 -- meter. -// 2 -- millimeter. -// 3 -- inch. +// 1 -- meter. +// 2 -- millimeter. +// 3 -- inch. // exclusiveCase: Parallel projection exclusive case. -// 0 -- NON case. -// 1 -- JSM-C2-NPOFF case. -// 2 -- CHNT. +// 0 -- NON case. +// 1 -- JSM-C2-NPOFF case. +// 2 -- CHNT. // projectOrgPoint: If the original wall points need to be projected or not. -int anisoRefine = 0; -int geometryUnit = 1; -int isProject = 0; -int readDist = 0; -int isDeform = 0; +int anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; int exclusiveCase = 0; int projectOrgPoint = 0; string geometryFileName = "./grid/jsm.igs"; // ----------------- Grid Deform Parameters ----------------------------- // deformationMethod: Grid Deform. -// 1 -- SPRING. -// 2 -- RBF. +// 1 -- SPRING. +// 2 -- RBF. // stationalGridFile: Original grid file. // visualFileName : The visualization file path of deform grid. // nDeformStep : The max deform step. -// flapAngle : The max flap angle. +// flapAngle : The max flap angle. // rotatePostionZ : Rotate postion. // rotatePostionY : Rotate postion. // gridSlice : If dump slice grid. @@ -163,10 +168,10 @@ int sliceAxis = 1; double slicePosition = 13; // ----------------- RBF Parameters ------------------------------------- -// numberOfReferenceCP : Number of reference Control Points. -// influencePara : The RBF influence radius parameter. +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. int numberOfReferenceCP = 40; -double influencePara = 25.0; +double influencePara = 25.0; // ----------------- Periodic Parameters -------------------------------- // Notice: Rotational periodicity only support rotation along the X axis! @@ -178,9 +183,8 @@ double influencePara = 25.0; which only support one direction. // rotationAngle: The relative angle between two periodic face. which is recorded in degrees. - int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; +double translationLength[] = [0.0, 0.0, 0.0]; double rotationAngle = 0.0; ######################################################################### @@ -192,7 +196,6 @@ double rotationAngle = 0.0; // 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; @@ -201,20 +204,20 @@ int numberOfMultifile = 1; // 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. +// cellIndexOfMark : the cell index of mark, only for structured grid partition. int traceMark = 0; int blockIndexOfMark = 0; -int cellIndexOfMark[] = [185,30,1]; +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; +// parallelStrategy: +// 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). +// 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"; @@ -232,11 +235,10 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts"; // 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; +double parmetisBalance = 1.05; // numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. // 1 -- single level. @@ -248,29 +250,35 @@ 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. +// 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; +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; int intervalStepSample = 1000; -int intervalStepForce = 100; -int intervalStepRes = 10; -int ifLowSpeedPrecon = 0; +int intervalStepForce = 100; +int intervalStepRes = 10; // compressible: // 0 -- incompressible flow. // 1 -- compressible flow. (default) int compressible = 1; +// 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) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 1; + //----------------------------------------------------------------------- # CFD Control Parameter # //----------------------------------------------------------------------- @@ -281,33 +289,36 @@ int compressible = 1; // 0 -- the nondimensional conditions. // 1 -- the flight conditions. // 2 -- the experiment conditions. -// 3 -- the subsonic boundary conditions. +// 3 -- the subsonic boundary conditions. (Useless!) // 4 -- the condition that the velocity, temperature and density are given. // 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 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. +// 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 = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. // forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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. -// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol. +// 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; +int directionMethod = 0; double refMachNumber = 0.73; double attackd = 2.79; double angleSlide = 0.00; +int flowInitMethod = 0; int inflowParaType = 0; double refReNumber = 6.5e6; @@ -321,29 +332,27 @@ double freestream_vibration_temperature = 300.00; //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; - -//The velocity, temperature and density are fixed. +// The velocity, temperature and density are fixed. //int inflowParaType = 4; //double refDimensionalVelocity = 1000.0; -//double refDimensionalDensity = 1.0e3; +//double refDimensionalDensity = 1.0e3; -//The velocity, temperature and pressure are fixed. +// The velocity, temperature and pressure are fixed. //int inflowParaType = 5; //double refDimensionalVelocity = 1000.0; //double refDimensionalPressure = 1.0e5; -//The MachNumber, temperature and pressure are fixed. +// The MachNumber, temperature and pressure are fixed. //int inflowParaType = 6; -//double refDimensionalTemperature = 293; +//double refDimensionalTemperature = 293.0; //double refDimensionalPressure = 8886.06; +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; + double wallTemperature = -1.0; double radiationCoef = 0.8; @@ -357,41 +366,41 @@ 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. +double knudsenLength = 1.0; // unit of meter. double refMolecularWeight = 28.9644; // unit of g/mol. //----------------------------------------------------------------------- # Spatial Discretisation # //----------------------------------------------------------------------- -#******************************************************************* -# Struct Solver * -#******************************************************************* +#************************************************************************ +# 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". +// -- "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. +// 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" - +// -- "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"; +string str_limiter_name = "vanalbada"; -#******************************************************************* -# UnStruct Solver or Common * -#******************************************************************* +#************************************************************************ +# UnStruct Solver or Common * +#************************************************************************ // viscousType: Viscous model. -// 0 -- Euler. -// 1 -- Lamilar. -// 2 -- Algebraic. -// 3 -- 1eq turbulent. -// 4 -- 2eq turbulent. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. // viscousName: Laminar or tubulent model. // -- "0eq-bl". // -- "1eq-sa". @@ -410,16 +419,16 @@ string str_limiter_name = "vanalbada"; // 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". +// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // uns_limiter_name: Limiter of Unstruct grid. -// -- "barth", "vencat", "vanleer", "minmod". -// -- "vanalbada", "smooth", "nnd", "lpz", "1st". +// -- "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". // gradientName: Gradient reconstruction method. -// -- "default", "ggcell", "ggnode", "lsq". +// -- "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. @@ -442,18 +451,18 @@ 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 +// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0. -//int viscousType = 0; +//int viscousType = 0; //string viscousName = "Euler"; -//int viscousType = 1; +//int viscousType = 1; //string viscousName = "laminar"; -int viscousType = 3; +int viscousType = 3; string viscousName = "1eq-sa"; -//int viscousType = 4; +//int viscousType = 4; //string viscousName = "2eq-kw-menter-sst"; int DESType = 0; @@ -463,7 +472,7 @@ string uns_limiter_name = "vencat"; string uns_vis_name = "test"; string gradientName = "ggnode"; -int ivencat = 7; +int ivencat = 7; double venkatCoeff = 5.0; int reconmeth = 1; int limitVariables = 0; @@ -475,9 +484,9 @@ double roeEntropyScale = 1.0; double AusmpwPlusLimiter = 1.0; -//----------------------------------------------------------------------- -# Temporal Discretisation # -//----------------------------------------------------------------------- +#************************************************************************ +# Temporal Discretisation * +#************************************************************************ // iunsteady: Steady or unsteady. // 0 -- steady. // 1 -- unsteay. @@ -490,51 +499,57 @@ double AusmpwPlusLimiter = 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 = - ^2 -// 1 -- tau = +// 0 -- tau = - ^2 +// 1 -- tau = // 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 -- Line LU-SGS. -// 8 -- Matrix LU-SGS. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 4 -- LU-SGS. +// 5 -- Block LU-SGS. +// 6 -- Jacobian iteration. +// 7 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. // 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. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. // 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. +// 0 --Local. +// 1 --Global. // isUseLocalCFL: use variable number of CFL or not. -// 0 -- global unified CFL number. -// 1 -- local CFL number. +// 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. -// 0 -- no ALE method. -// 1 -- ALE method for non-moving grids. -// 2 -- ALE method for moving grids. -// 3 -- ALE method for deforming grids. +// 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. +// 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; +int iunsteady = 0; double physicalTimeStep = 0.01; double physicalTimeStepDimensional = -0.001; int ifStartFromSteadyResults = 0; @@ -543,39 +558,42 @@ int ifStaticsReynoldsStress = 0; int startStatisticStep = 800000; double statisticalTimePeriod = -1.0; int statisticMethod = 0; -int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2; +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 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 CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; double pMaxForCFL = 0.2; double pMinForCFL = 0.1; double deltaMaxForCFL = 0.2; double magnifyFactorForCFL = 1.1; double reduceFactorForCFL = 0.5; -double ktmax = 1.0e10; +double ktmax = 1.0e10; -int swapDq = 1; +int swapDq = 1; int nLUSGSSweeps = 1; double LUSGSTolerance = 0.01; -int order = 2; +int order = 2; double visl_min = 0.01; double turbCFLScale = 1.0; -double csrv = 2.0; +double csrv = 1.0; double timemax = 1.0e10; double dtsave = -1.0; int maxale = 10; @@ -591,10 +609,9 @@ double lamda[] = [0.5, 1.0]; //int RKStage = 4; //double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; - -//----------------------------------------------------------------------- -# File In or Out # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. @@ -611,20 +628,18 @@ double lamda[] = [0.5, 1.0]; // 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. +// 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. // 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= ""; +// 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; @@ -632,10 +647,12 @@ int cellMethodOrNodeMethod = 0; string resSaveFile = "results/res.dat"; string turbresfile = "results/turbres.dat"; +string transitionResFile = "results/transitionRes.dat"; string aircoeffile = "results/aircoef.dat"; string restartNSFile = "results/flow.dat"; string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; string visualfile = "results/tecflow.plt"; string wall_aircoefile = "results/wall_aircoef.dat"; @@ -645,10 +662,14 @@ string protectionFile0 = "results/flow0.dat"; string protectionFile1 = "results/flow1.dat"; string wall_heatfluxfile = "results/wall_heatflux.dat"; -int nDumpSurfaceInfo = 0; -string wall_varfile = ""; +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; -string jetDefineFile = "bin/jet.hypara"; +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; string sixDofFileName = "results/sixDofInfo.dat"; string derivativeFileName = "results/identify.dat"; @@ -659,7 +680,8 @@ int plotFieldType = 0; // visualfileType: The file type of visualfile. // 0 -- Tecplot binary. // 1 -- Tecplot ASCII. - +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. int visualfileType = 1; // samplefileMode: The dump mode of sample file. @@ -697,21 +719,21 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), 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) +// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. //-----------the optional parameters list for the wall boundary condition---------------- // nVisualWallVariables: The number of visual variables on wall. // visualWallVariables : dumped variable types, listed as following: -// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4), -// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8), -// -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), -Grid Reynolds number on wall(Re_w, 23) +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- 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), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). int nVisualVariables = 8; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; @@ -739,16 +761,18 @@ 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), mach(6). +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). // 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. +// 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; +int dataMonitorType = 0; string probesDefineFile = "bin/probes_XYZ.dat"; //int dataMonitorType = 1; @@ -761,28 +785,26 @@ string probesDefineFile = "bin/probes_XYZ.dat"; int searchCellsMethod = 0; -int nProbeVariables = 7; -int probeVariables[] = [0, 1, 2, 3, 4, 5, 6]; -int probeVariablesInterpolationMethod = 0; -//----------------------------------------------------------------------- -# Turbulence Parameter # -//----------------------------------------------------------------------- +int nProbeVariables = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +int probeVariablesInterpolationMethod = 0; + +#************************************************************************ +# Turbulence Parameter * +#************************************************************************ // turbInterval: Iteration number of turbulence. // kindOfTurbSource: Kinds of turbulent source. // 0 -- Original. // mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0. -// transitionType: transition model type +// 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 - - +// 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; 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; @@ -790,29 +812,28 @@ int transitionType = 0; double turbIntensity = -1.0; int freeturbIntensitySRModify = 0; double freeDecayXLocation = 0.0; -int compressibleCorrection = 0; -int prandtlNumberCorrection = 0; +int compressibleCorrection = 0; int transitionMaFix = 1; -# maximum eddy viscosity (myt/my) max. +// maximum eddy viscosity (myt/my) max. double eddyViscosityLimit = 1.0e10; int monitor_vistmax = 0; -//----------------------------------------------------------------------- -# LES Parameter # -//----------------------------------------------------------------------- +#************************************************************************ +# LES Parameter * +#************************************************************************ // iLES: Create LESSolver or not. -// = 1 - Create LESSolver; -// != 1 - 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. +// = 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. +// = 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. @@ -820,23 +841,22 @@ int monitor_vistmax = 0; // = "dsmCom"; // = "wale"; // = "sigma". -// 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. +// 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. +// = 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. +// 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; @@ -852,19 +872,16 @@ double testFilterScale = 2.0; int averageWidth = 1; int monitorNegativeConstant = 0; -//----------------------------------------------------------------------- -# Other Parameters for Hypersonic Non-equilibrium Gas # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. -// 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. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. @@ -875,7 +892,7 @@ int monitorNegativeConstant = 0; // 2 -- Argon. // 3 -- Nitrogen. // nEnergyRecycle: The type of EnergyModel Recycle. -// 0 -- not used . +// 0 -- not used. // 1 -- used. // nDensityModify: The type of densitymodify. // 0 -- not used. @@ -883,26 +900,25 @@ int monitorNegativeConstant = 0; // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. -// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. // 0 -- perfect gas. // 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. -// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. -// the value equals to or is greater than 1, and 3 is for default value. -// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. -// the value equals to or is greater than 1, and 3 is for default value. -// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. -// the value equals to or is greater than 1, and 3 is for default value. -// nSlipBCModel : The computational model of slip boundary conditions. - -// 0 -- no slip. -// 1 -- the conventional Maxwell slip conditions. -// 2 -- the Gokcen slip conditions. -// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. -// 4 -- the Kogan simplified slip conditions. -// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. -// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). -// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. -// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). // nchemsrc: // 0 -- the source terms are not computed. // 1 -- the source terms are computed. @@ -913,148 +929,151 @@ int monitorNegativeConstant = 0; // 1 -- One-temperature model. // 2 -- Two-temperature model. // 3 -- Three-temperature model. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. // 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. +// 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 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: -// 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. -// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. -// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. -// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. -// 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. +// 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. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// 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]. // velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. -// 1.0 -- proposed by Maxwell. -// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. -// 1.146 -- proposed for an additional "fictitious" velocity slip. - -// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. -// 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. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// 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. // nSpeciesLimit: limitter of gas species -// 0 -- not used. -// 1 -- used. -// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction -// 0 -- method 0. -// 1 -- method 1. -// 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) - +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// 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 +// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs. +// 0 -- not used. +// 1 -- used. +// nDiagonalModified: Modified on Diagonal. +// 0 -- not used. +// 1 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. // nAblation: -// 0 -- The wall ablation is not computed. -// 1 -- The wall ablation is computed. +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. // isInjection: -// 0 -- The injection velocity of ablation wall is not computed. -// 1 -- The injection velocity of ablation wall is computed. +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. // nViscosityModel: -// 0 -- Blottner fitting method(N89). -// 1 -- Gupta fitting method(N90). +// 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. +// 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. +// 0 -- stands for selecting the Blotter curve fits mode. +// 1 -- stands for Sutherland relation. // 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. -// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. -// "Gas-Mixture" -- indicates the process of mixing gas without reacting. -// for struct solver mixing two speciesSpeciesA, SpeciesB. -// for unstruct solver mixing multi-speciesO2 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. +// "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. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "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. +// 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. +// 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 - +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. int dg_high_order = 0; int iapplication = 0; int isAdaptiveSolver = 0; -int nm = 5; +int nm = 5; int nEquilibriumGas = 0; -int nPCWCycleStep = 3; -int nRETCycleStep = 3; -int nSLIPCycleStep= 3; +int nPCWCycleStep = 3; +int nRETCycleStep = 3; +int nSLIPCycleStep = 3; int nIterFirstStep = 1000; int nIterSecondStep= 2000; int nIterThirdStep = 2000; @@ -1065,17 +1084,17 @@ double secondStepError = 0.001; double thirdStepError = 0.001; double predictCFLError = 0.1; -double refGama = 1.4; -double prl = 0.72; -double prt = 0.90; -double sc_l = 0.5; -double sc_t = 0.5; +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 nGasModel = 0; +int nchem = 0; +int nchemsrc = 1; +int nchemrad = 1; +int ntmodel = 1; int nIdealState = 0; int nEnergyRecycle = 1; @@ -1099,12 +1118,12 @@ double sigmaTemperature = 1.0; double sigmaMassFraction = 1.0; double velocitySlipCorrectConstant = 1.0; -double chemicalRelaxCorf = 1.0; +double chemicalRelaxCorf = 1.0; double chemicalSpectrumRadiusCoef = 1.0; double viscousSpectrumRadiusCoef = 1.5; double inviscidSpectrumRadiusCoef = 1.5; -double spectrumRadiusCoef = 0.5; -double staticPressureRelaxCorf = 0.2; +double spectrumRadiusCoef = 0.5; +double staticPressureRelaxCorf = 0.2; double maxViscous = 10000.0; double trTemperatureMin = 10.0; @@ -1114,31 +1133,35 @@ double densityMin = 1.0e-8; double densityMinFactor = 0.1; double tAdjustmentFactor = 10.0; double iniSpeedCoef = 1.0; +int iniSpeedMode = 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 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 nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; -int nProtectData = 0; -int useHyflowSetting = 0; -int nAblation = 0; -int isInjection = 0; -int nViscosityModel = 0; -int nMarsModel = 0; -string gasfile = "DK5"; -//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; string speciesName = "O, O2, NO, N, N2"; string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; @@ -1152,16 +1175,16 @@ 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 = "Pa"; +//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"; -//string gasfile = "Combustion-12"; +//string gasfile = "Combustion-12"; //string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; //string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; //string gasfile = "Gas-Mixture"; -//string speciesName ="SpeciesA, SpeciesB"; +//string speciesName = "SpeciesA, SpeciesB"; //string initMassFraction = "1.0, 0.0"; int nSutherland = 0; double gamaSpeciesA = 1.4; @@ -1173,9 +1196,17 @@ double molecularWeightSpeciesB = 30.0; //string speciesName = "O2, N2"; //string initMassFraction = "1.0, 0.0"; +int nFraction = 0; int nContinueModel = 0; int nChemicalFlowStep = 0; int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; ######################################################################### // Multi-Grid parameters. @@ -1196,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0; // 1 -- zero order. // 2 -- first-order. (default) // mgCorrectionLimit: Multi-grid correction limit. - int nMGLevel = 1; int MGCoarsestIteration = 1; int MGPreIteration = 1; @@ -1218,20 +1248,20 @@ 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"; +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 # -######################################################################### +#************************************************************************ +# High Order Struct Solver * +#************************************************************************ // isFVMOrFDM: -// 0 -- NSSolverStruct using Finite Volume Method. -// 1 -- NSSolverStruct using Finite Differ Method. +// 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) @@ -1273,30 +1303,48 @@ int allReduceStep = 1; // codeOfOversetGrid: Overlapping(overset) grid or not. // 0 -- NON-overlapping grid. // 1 -- Overlapping grid. -// oversetInterpolationMethod: the method of overset interpolation while field simulation +// oversetInterpolationMethod: the method of overset interpolation while field simulation. // 0 -- set the acceptor cell value by donor cell value. // 1 -- set the acceptor cell value by distance weight of donor cell value. - -int codeOfOversetGrid = 0; -int oversetInterpolationMethod = 0; -int readOversetFileOrNot = 0; -int symetryOrNot = 0; -int readInAuxiliaryInnerGrid = 0; -int readInAuxiliaryOuterGrid = 0; -int readInSklFileOrNot = 0; -string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; -string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; -string auxiliaryInnerGrid2 = ""; -string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; - -int numberOfMovingBodies = 2; +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; // ----------------- ALE configuration ------------------------------ int codeOfAleModel = 0; @@ -1306,36 +1354,42 @@ 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; +int strategyForFaceNormalVelocity = 0; // 0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd. +int strategyForGCLSource = 0; // 0-present; 1-Ahn. -//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. int methodForKineticEquation = 0; double relaxParameterOfKinetic = 1.0; -######################################################################### -# motive information # -######################################################################### +#************************************************************************ +# motive information * +#************************************************************************ int numberOfMovingBodies = 1; ############################## body0 ############################## -//mass of parts -double mass_0 = 1.0; -//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz -double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; -//initial six DOF position information of parts. xc yc zc -double massCenter_0[] = 0.0 , 0.0, 0.0; -//initial six DOF position information of parts. angleX angleY angleZ -double attitudeAngle_0[] = 0.0 , 0.0, 0.0; -//initial six DOF move information of parts. vc vy vz -double massCenterVelocity_0[] = 0.0, 0.0, 0.0; -//initial six DOF move information of parts. omigX omigY omigZ -double angularVelocity_0[] = 0.0, 0.0, 0.0; -//the object that the parts belong to. -int fartherIndex_0 = -1; -//the assembly position of the parts. xc yc zc angleX angleY angleZ -double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0; -//the move pattern of the parts. +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. // -1 given motion partten. // 0 still. // 1 six DOF motion. @@ -1346,51 +1400,68 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 // 14 forced pitch motion. // 15 forced yaw motion. // 16 forced roll motion. -int RBDMethod_0 = 0; -double amplitude_0 = 0.0; -double reduceFrequency_0 = 0.0; -//direction of rotation +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 ; -//additional moment of Force (system axis) mX mY mZ -double addedMoment_0[] = 0.0 ,0.0 ,0.0 ; -//the deformation method of the parts. -int morphing_0 = 0; - -// post indentify -int integralOrder = 4; +int direction_0 = -1; +double rotateFrequency_0 = 0.0; +//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; +// post indentify. +int integralOrder = 4; // ---------------- ATP read -------------------------------------------- -//@int inflowParaType = 0; +//@int inflowParaType = 0; //@double refReNumber = 6.5e6; //@double refDimensionalTemperature = 288.15; //@double freestream_vibration_temperature = 300.00; -//@double refDimensionalPressure = 0; -//@double height = 0; -//@int nsubsonicInlet = 0; -//@int nsubsonicOutlet = 0; -//@string inLetFileName = "./bin/subsonicInlet.hypara"; -//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; //@double refDimensionalVelocity = 0; //@double refDimensionalDensity = 0; - -######################################################################### -# Old Parameter # -######################################################################### +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ int isPlotVolumeField = 0; +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; -######################################################################### -# Incompressible Parameter # -######################################################################### +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ int isSolveEnergyEquation = 0; int isSolveTurbEquation = 0; -int isSolveSpeciesEquation = 0; - +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/F11_ThreeD_M6_GridParallelRefine_Unstruct_4CPU/bin/grid_para.hypara b/F11_ThreeD_M6_GridParallelRefine_Unstruct_4CPU/bin/grid_para.hypara index 9f33df2..68e7bf8 100644 --- a/F11_ThreeD_M6_GridParallelRefine_Unstruct_4CPU/bin/grid_para.hypara +++ b/F11_ThreeD_M6_GridParallelRefine_Unstruct_4CPU/bin/grid_para.hypara @@ -4,9 +4,12 @@ // 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. +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. // from_gtype: Type of grid data type in grid conversion process. // -1 -- MULTI_TYPE. // 1 -- PHengLEI, *.fts. @@ -19,7 +22,9 @@ // 8 -- GMSH, *.msh. // 9 -- Gridgen type of structured grid, *.dat/*.grd. int gridtype = 0; -int axisup = 1; +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; int from_gtype = 2; ######################################################################### diff --git a/F11_ThreeD_M6_GridParallelRefine_Unstruct_4CPU/非结构三维M6机翼并行加密_算例说明文档.pdf b/F11_ThreeD_M6_GridParallelRefine_Unstruct_4CPU/非结构三维M6机翼并行加密_算例说明文档.pdf index 249bdd1..7798dbe 100644 Binary files a/F11_ThreeD_M6_GridParallelRefine_Unstruct_4CPU/非结构三维M6机翼并行加密_算例说明文档.pdf and b/F11_ThreeD_M6_GridParallelRefine_Unstruct_4CPU/非结构三维M6机翼并行加密_算例说明文档.pdf differ diff --git a/G01_TwoD_Cylinder_Laminar_OneTemperMode_FCW_Struct/bin/cfd_para.hypara b/G01_TwoD_Cylinder_Laminar_OneTemperMode_FCW_Struct/bin/cfd_para.hypara index f52cf86..f903a5a 100644 --- a/G01_TwoD_Cylinder_Laminar_OneTemperMode_FCW_Struct/bin/cfd_para.hypara +++ b/G01_TwoD_Cylinder_Laminar_OneTemperMode_FCW_Struct/bin/cfd_para.hypara @@ -8,54 +8,63 @@ // Platform for Hybrid Engineering Simulation of Flows + // China Aerodynamics Research and Development Center + // (C) Copyright, Since 2010 + +// PHengLEI 2212 + //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ########################################################################### # 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. +// 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. +// 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. -// grid_database_index: Case of typical case, only for gridobj=0. -// 1 -- Laminar flat plate of subsonic flow. -// 2 -- Laminar flat plate of supersonic flow. -// 3 -- Turbulent flat plate of subsonic flow. -// 4 -- Turbulent flat plate of supersonic flow. // iadapt: Adaptation number for unstructure grid. -// iovrlap: Overlapping(overset) grid or not. -// 0 -- NON-overlapping grid. -// 1 -- Overlapping grid. // SymmetryFaceVector: The vector of symmetry face. // 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 grid_database_index = 3; int iadapt = 0; -int iovrlap = 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. -int axisup = 1; +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; // 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; +int omitRepeatInterface = 1; //----------------------------------------------------------------------- # Grid data type # @@ -70,6 +79,7 @@ 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. @@ -82,29 +92,25 @@ 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/rae2822_hybrid2d.cas"; -string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; +int numberOfGridFile = 1; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +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; // fileformat: Ustar Grid file format. // 0 -- BINARY. // 1 -- ASCII. int fileformat = 0; -// .skl meaning skeleton. -string original_grid_info_file = "./grid/FLUENT_test.skl"; - // 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. -// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver. -string mixgrid_uns = "./grid/rae2822_uns2d_4.fts"; -string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts"; -string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp"; +// 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; @@ -113,38 +119,59 @@ 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"; +// ----------------- Grid Refine Parameters ----------------------------- +// anisoRefine: If refine grid by anisoRefine type. +// 0 -- Not. (default) +// 1 -- Yes. +// 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 anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; +int exclusiveCase = 0; +int projectOrgPoint = 0; 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. +// ----------------- Grid Deform Parameters ----------------------------- +// deformationMethod: Grid Deform. +// 1 -- SPRING. +// 2 -- RBF. +// stationalGridFile: Original grid file. +// visualFileName : The visualization file path of deform grid. +// nDeformStep : The max deform step. +// flapAngle : The max flap angle. +// rotatePostionZ : Rotate postion. +// rotatePostionY : Rotate postion. +// gridSlice : If dump slice grid. +// sliceAxis : Grid slice axis. +// slicePosition : Grid slice position. +int nDeformStep = 40; +double flapAngle = 10.0; +double rotatePostionZ = 4.00003; +double rotatePostionY = 3.05; + +int deformationMethod = 2; +string stationalGridFile = "./grid/Segment2Brid.fts"; +string visualFileName = "./results/deformedGrid.dat" + +int gridSlice = 1; +int sliceAxis = 1; +double slicePosition = 13; // ----------------- RBF Parameters ------------------------------------- -// 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; +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. +int numberOfReferenceCP = 40; +double influencePara = 25.0; // ----------------- Periodic Parameters -------------------------------- // Notice: Rotational periodicity only support rotation along the X axis! @@ -152,8 +179,12 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of // 0 -- without Periodic Boundary. // 1 -- Translational periodicity. // 2 -- Rotational periodicity. +// translationLength[]: The relative distance between two periodic face + which only support one direction. +// rotationAngle: The relative angle between two periodic face. + which is recorded in degrees. int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; +double translationLength[] = [0.0, 0.0, 0.0]; double rotationAngle = 0.0; ######################################################################### @@ -164,22 +195,29 @@ 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. // 1 -- Yes. // blockIndexOfMark: the block index of mark, only for structured grid partition. -// cellIndexOfMark: the cell 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]; +int cellIndexOfMark[] = [185, 30, 1]; + +// parallelStrategy: +// 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). +// 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"; @@ -189,7 +227,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts"; // 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. +// parallelPartitionMethod: 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. @@ -197,11 +235,10 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts"; // 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; +double parmetisBalance = 1.05; // numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. // 1 -- single level. @@ -213,29 +250,35 @@ 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. +// 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; +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; int intervalStepSample = 1000; -int intervalStepForce = 100; -int intervalStepRes = 10; -int ifLowSpeedPrecon = 0; +int intervalStepForce = 100; +int intervalStepRes = 10; // compressible: // 0 -- incompressible flow. // 1 -- compressible flow. (default) int compressible = 1; +// 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) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 1; + //----------------------------------------------------------------------- # CFD Control Parameter # //----------------------------------------------------------------------- @@ -246,39 +289,41 @@ int compressible = 1; // 0 -- the nondimensional conditions. // 1 -- the flight conditions. // 2 -- the experiment conditions. -// 3 -- the subsonic boundary conditions. +// 3 -- the subsonic boundary conditions. (Useless!) +// 4 -- the condition that the velocity, temperature and density are given. +// 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 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. -// dump_Q: Dump out thermal flux Q of solid wall. -// 0 -- no dump out. -// 1 -- dump out wall Q only. -// 2 -- dump out wall Q & the typical position Q of ball. -// 3 -- dump out wall Q & the typical position Q of cone. -// 4 -- dump out wall Q & the typical position Q of double sphere. -// 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. +// 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 = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. +// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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. - +// 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; +int flowInitMethod = 0; int inflowParaType = 0; double refReNumber = 6.5e6; double refDimensionalTemperature = 288.15; -double freestream_vibration_temperature = 10000.00; +double freestream_vibration_temperature = 300.00; //int inflowParaType = 1; //double height = 0.001; @@ -287,54 +332,75 @@ double freestream_vibration_temperature = 10000.00; //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; +// 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 = 1000.0; +//double refDimensionalPressure = 1.0e5; + +// The MachNumber, temperature and pressure are fixed. +//int inflowParaType = 6; +//double refDimensionalTemperature = 293.0; +//double refDimensionalPressure = 8886.06; + +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; double wallTemperature = -1.0; -int dump_Q = 0; double radiationCoef = 0.8; double gridScaleFactor = 1.0; +double gridTranslationVector[] = [0.0, 0.0, 0.0]; -double forceRefenenceLengthSpanWise = 1.0; // unit of meter. -double forceRefenenceLength = 1.0; // unit of meter. -double forceRefenenceArea = 1.0; // unit of meter^2. +int numberOfAerodynamicForceComponents = 1; +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. +double knudsenLength = 1.0; // unit of meter. +double refMolecularWeight = 28.9644; // unit of g/mol. //----------------------------------------------------------------------- # Spatial Discretisation # //----------------------------------------------------------------------- -#******************************************************************* -# Struct Solver * -#******************************************************************* +#************************************************************************ +# 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". +// -- "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. +// -- "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"; -string str_limiter_name = "vanalbada"; +int isWennScheme = 0; +string str_limiter_name = "vanalbada"; -#******************************************************************* -# UnStruct Solver or Common * -#******************************************************************* +#************************************************************************ +# UnStruct Solver or Common * +#************************************************************************ // viscousType: Viscous model. -// 0 -- Euler. -// 1 -- Lamilar. -// 2 -- Algebraic. -// 3 -- 1eq turbulent. -// 4 -- 2eq turbulent. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. // viscousName: Laminar or tubulent model. // -- "0eq-bl". // -- "1eq-sa". @@ -353,16 +419,16 @@ string str_limiter_name = "vanalbada"; // 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". +// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", +// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // uns_limiter_name: Limiter of Unstruct grid. -// -- "barth", "vencat", "vanleer", "minmod". -// -- "vanalbada", "smooth", "nnd", "lpz", "1st". +// -- "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". +// gradientName: 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. @@ -385,17 +451,18 @@ 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; +//int viscousType = 0; //string viscousName = "Euler"; -//int viscousType = 1; +//int viscousType = 1; //string viscousName = "laminar"; -int viscousType = 3; +int viscousType = 3; string viscousName = "1eq-sa"; -//int viscousType = 4; +//int viscousType = 4; //string viscousName = "2eq-kw-menter-sst"; int DESType = 0; @@ -405,124 +472,153 @@ string uns_limiter_name = "vencat"; string uns_vis_name = "test"; string gradientName = "ggnode"; -int ivencat = 7; +int ivencat = 7; double venkatCoeff = 5.0; int reconmeth = 1; int limitVariables = 0; int limitVector = 0; -double limit_angle = 0; double skewnessAngle = 60.0; int roeEntropyFixMethod = 3; double roeEntropyScale = 1.0; -//----------------------------------------------------------------------- -# Temporal Discretisation # -//----------------------------------------------------------------------- +double AusmpwPlusLimiter = 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. +// ifStaticsFlowField: Statistical variables for unsteady simulation. +// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation. // startStatisticStep: Outer step when start statistics. // when the value is larger than "maxSimuStep", it is useless. +// 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 = - ^2 +// 1 -- tau = // 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. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 4 -- LU-SGS. +// 5 -- Block LU-SGS. +// 6 -- Jacobian iteration. +// 7 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. // 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. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. // 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. +// 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. -// iale: 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. +// 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. +// 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; +int iunsteady = 0; double physicalTimeStep = 0.01; +double physicalTimeStepDimensional = -0.001; int ifStartFromSteadyResults = 0; int ifStaticsFlowField = 0; +int ifStaticsReynoldsStress = 0; int startStatisticStep = 800000; +double statisticalTimePeriod = -1.0; +int statisticMethod = 0; +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 tscheme = 4; int iSimplifyViscousTerm = 1; int ifLocalTimeStep = 0; -double CFLStart = 0.01; -double CFLEnd = 10.0; -int CFLVaryStep = 500; +int isUseLocalCFL = 0; +int isUsePreTwall = 0; +double CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; +double pMaxForCFL = 0.2; +double pMinForCFL = 0.1; +double deltaMaxForCFL = 0.2; +double magnifyFactorForCFL = 1.1; +double reduceFactorForCFL = 0.5; -double ktmax = 1.0e10; +double ktmax = 1.0e10; -int swapDq = 1; +int swapDq = 1; int nLUSGSSweeps = 1; double LUSGSTolerance = 0.01; -int order = 2; +int order = 2; double visl_min = 0.01; double turbCFLScale = 1.0; - +double csrv = 1.0; double timemax = 1.0e10; double dtsave = -1.0; -int iale = 0; -int ialetype = 2; int maxale = 10; double dtau = 0.001; -double dtau_max = 1E-01; 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; //int RKStage = 4; //double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; - -//----------------------------------------------------------------------- -# File In or Out # -//----------------------------------------------------------------------- +#************************************************************************ +# 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! -// isPlotVolumeField: If dump out the field results to visulization. +// 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. @@ -532,47 +628,67 @@ double lamda[] = 0.5, 1.0; // 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. +// 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. +// 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 numberOfGridGroups = 1; -string gridfile = "./grid/rae2822_hybrid2d__4.fts"; - +int nIsComputeWallDist = 0; int walldistMethod = 1; +int cellMethodOrNodeMethod = 0; string resSaveFile = "results/res.dat"; string turbresfile = "results/turbres.dat"; +string transitionResFile = "results/transitionRes.dat"; string aircoeffile = "results/aircoef.dat"; string restartNSFile = "results/flow.dat"; string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; string visualfile = "results/tecflow.plt"; -string Qwall_file = "results/Qwall.dat"; string wall_aircoefile = "results/wall_aircoef.dat"; -string probesflowfile = "results/sample.dat"; -string surfacefile = ""; +string samplefile = "results/sample.dat"; -int nDumpSurfaceInfo = 0; +string protectionFile0 = "results/flow0.dat"; +string protectionFile1 = "results/flow1.dat"; +string wall_heatfluxfile = "results/wall_heatflux.dat"; + +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; + +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; string wall_varfile = ""; -string componentDefineFile = "bin/component.hypara"; -string jetDefineFile = "bin/jet.hypara"; +string sixDofFileName = "results/sixDofInfo.dat"; +string derivativeFileName = "results/identify.dat"; +string hysteresisFileName = "results/force_beta.plt"; -string componentforcefile = "results/component_aircoef.dat"; - -string overset_gridfile = "iblank.ovs"; - -int isPlotVolumeField = 0; +int plotFieldType = 0; // visualfileType: The file type of visualfile. // 0 -- Tecplot binary. // 1 -- Tecplot ASCII. - +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. int visualfileType = 1; +// samplefileMode: The dump mode of sample file. +// 0 -- dump out every probe/line/surface data for all step intervals. +// 1 -- dump out all probe/line/surface data for every step intervals. +int samplefileMode = 0; + // visualSlice: The slice of tecflow. // 0 -- Do not save slice data. // 1 -- comput and save it to sliceFile. @@ -586,11 +702,13 @@ int visualSlice = 0; int sliceAxis = 1; double slicePostion = -0.5; string sliceFile = "results/Slice.plt"; +int dumpWallFaceCenter = 0; // min-max box of the visual block. double lowerPlotFieldBox[] = [0.0 0.0 0.0]; double upperPlotFieldBox[] = [1.0 1.0 1.0]; +//-----------the optional parameters list for the flow field output---------------- // 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), @@ -600,128 +718,207 @@ 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). +// -- 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), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. +//-----------the optional parameters list for the wall boundary condition---------------- +// nVisualWallVariables: The number of visual variables on wall. +// visualWallVariables : dumped variable types, listed as following: +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- 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), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). int nVisualVariables = 8; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; +int nVisualWallVariables = 9; +int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; + // dumpStandardModel: Dump many standard model data. // 1 -- Turbulent flat plate. int dumpStandardModel = 0; -// ifSetProbesToMonitor: Set probes location to Monitor. -// 0 -- Do not monitor. -// 1 -- To monitor and save data to files. -// probesDefineFile: probes location information file. +// 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). +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). // Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!! // probeVariables order must from small to big. -int ifSetProbesToMonitor = 0; -string probesDefineFile = "bin/probes_location.hypara"; -int nProbeVariables = 6; -int probeVariables[] = [0, 1, 2, 3, 4, 5]; -//----------------------------------------------------------------------- -# Turbulence Parameter # -//----------------------------------------------------------------------- +// 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 = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +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. - +// 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 turb_vis_kind = 2; +int turbOrderStruct = 2; int kindOfTurbSource = 0; int mod_turb_res = 0; -double turb_relax = 1.0; -double turb_min_coef = 1.0e-1; double freeStreamViscosity = 1.0e-3; -double muoo = 1.0e-1; -double kwoo = 1.0; +double muoo = 3.0; +double kwoo = 5.0; +int transitionType = 0; +double turbIntensity = -1.0; +int freeturbIntensitySRModify = 0; +double freeDecayXLocation = 0.0; +int compressibleCorrection = 0; +int transitionMaFix = 1; -# maximum eddy viscosity (myt/my) max. +// maximum eddy viscosity (myt/my) max. double eddyViscosityLimit = 1.0e10; -double sdilim = 1.0e20; -double coef_kvist = 1.0; int monitor_vistmax = 0; -//----------------------------------------------------------------------- -# LES Parameter # -//----------------------------------------------------------------------- +#************************************************************************ +# LES Parameter * +#************************************************************************ // iLES: Create LESSolver or not. -// >= 1 - Create LESSolver; -// < 1 - 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. +// = 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. +// = 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. +// = "dsmCom"; +// = "wale"; +// = "sigma". +// 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. +// = 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. +// 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 smagConstant = 0.1; double isotropicConstant = 0.0; double waleConstant = 0.6; +double sigmaConstant = 1.35; 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 # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic 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. +// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas. +// Otherwise, the pure gas with one component is used for perfect gas. // 0 -- Earth gas. // 1 -- Mars gas. +// 2 -- Argon. +// 3 -- Nitrogen. +// nEnergyRecycle: The type of EnergyModel Recycle. +// 0 -- not used. +// 1 -- used. +// nDensityModify: The type of densitymodify. +// 0 -- not used. +// 1 -- used. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. +// 0 -- perfect gas. +// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). // nchemsrc: // 0 -- the source terms are not computed. // 1 -- the source terms are computed. @@ -732,59 +929,284 @@ int monitorNegativeConstant = 0; // 1 -- One-temperature model. // 2 -- Two-temperature model. // 3 -- Three-temperature model. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. +// 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 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: -// 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. +// 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. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// 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]. +// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// 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. +// nSpeciesLimit: limitter of gas species +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// 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 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. +// nAblation: +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. +// isInjection: +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. +// nViscosityModel: +// 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. // 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. +// "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. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "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. +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. int dg_high_order = 0; int iapplication = 0; -int iCodeBranch = 0; -int nm = 5; +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; -// MHD -double bxoo = 0.0; -double byoo = 0.0; -double bzoo = 0.0; +double refGama = 1.4; +double prl = 0.72; +double prt = 0.90; +double sc_l = 0.5; +double sc_t = 0.5; -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 nGasModel = 0; -int nchem = 0; -int nchemsrc = 1; -int nchemrad = 1; -int ntmodel = 1; -int nChemicalFlowStep = 0; +int nIdealState = 0; +int nEnergyRecycle = 1; +int nSlipBCModel = 0; +int nDensityModify = 1; +int nTEnergyModel = 0; +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; -string gasfile = "DK5"; -//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +double sigmaVelocity = 1.0; +double sigmaTemperature = 1.0; +double sigmaMassFraction = 1.0; +double velocitySlipCorrectConstant = 1.0; + +double chemicalRelaxCorf = 1.0; +double chemicalSpectrumRadiusCoef = 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; +double maxTemperature = 50000.0; +double densityMin = 1.0e-8; +double densityMinFactor = 0.1; +double tAdjustmentFactor = 10.0; +double iniSpeedCoef = 1.0; +int iniSpeedMode = 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 nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; + +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; //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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 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; +//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"; + +//string gasfile = "Combustion-12"; +//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; +//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; + +//string gasfile = "Gas-Mixture"; +//string speciesName = "SpeciesA, SpeciesB"; +//string initMassFraction = "1.0, 0.0"; +int nSutherland = 0; +double gamaSpeciesA = 1.4; +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 nFraction = 0; +int nContinueModel = 0; +int nChemicalFlowStep = 0; +int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; ######################################################################### // Multi-Grid parameters. @@ -805,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0; // 1 -- zero order. // 2 -- first-order. (default) // mgCorrectionLimit: Multi-grid correction limit. - int nMGLevel = 1; int MGCoarsestIteration = 1; int MGPreIteration = 1; @@ -827,20 +1248,20 @@ 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"; +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. +#************************************************************************ +# High Order Struct Solver * +#************************************************************************ +// isFVMOrFDM: +// 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) @@ -853,7 +1274,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp"; // -- "roe", "steger". // structhighordergradient: // -- "conservation", "chain_rule". -int ifvfd = 0; +int isFVMOrFDM = 0; string str_highorder_solver = "WCNS"; int SolverStructOrder = 0; double str_highorder_interpolation_epsilon = 1.0e-6; @@ -878,13 +1299,169 @@ 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. +// oversetInterpolationMethod: the method of overset interpolation while field simulation. +// 0 -- set the acceptor cell value by donor cell value. +// 1 -- set the acceptor cell value by distance weight of donor cell value. +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; + +// ----------------- ALE configuration ------------------------------ +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. + +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. +int methodForKineticEquation = 0; +double relaxParameterOfKinetic = 1.0; + +#************************************************************************ +# motive information * +#************************************************************************ +int numberOfMovingBodies = 1; + +############################## body0 ############################## +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. +// -1 given motion partten. +// 0 still. +// 1 six DOF motion. +// 2 three DOF motion. +// 11 X-axis forced motion. +// 12 Y-axis forced motion. +// 13 Z-axis forced motion. +// 14 forced pitch motion. +// 15 forced yaw motion. +// 16 forced roll motion. +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"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; + +// post indentify. +int integralOrder = 4; + // ---------------- 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"; +//@int inflowParaType = 0; +//@double refReNumber = 6.5e6; +//@double refDimensionalTemperature = 288.15; +//@double freestream_vibration_temperature = 300.00; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalVelocity = 0; +//@double refDimensionalDensity = 0; +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ +int isPlotVolumeField = 0; + +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; + +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; + +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ +int isSolveEnergyEquation = 0; +int isSolveTurbEquation = 0; +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/G01_TwoD_Cylinder_Laminar_OneTemperMode_FCW_Struct/bin/grid_para.hypara b/G01_TwoD_Cylinder_Laminar_OneTemperMode_FCW_Struct/bin/grid_para.hypara index 9852ca0..c02b51d 100644 --- a/G01_TwoD_Cylinder_Laminar_OneTemperMode_FCW_Struct/bin/grid_para.hypara +++ b/G01_TwoD_Cylinder_Laminar_OneTemperMode_FCW_Struct/bin/grid_para.hypara @@ -4,9 +4,12 @@ // 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. +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. // from_gtype: Type of grid data type in grid conversion process. // -1 -- MULTI_TYPE. // 1 -- PHengLEI, *.fts. @@ -18,7 +21,9 @@ // 7 -- Hybrid, include both of unstructured and structured grid, *.fts. // 8 -- GMSH, *.msh. int gridtype = 1; -int axisup = 1; +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; int from_gtype = 3; ######################################################################### diff --git a/G02_ThreeD_Electre_Laminar_OneTemperMode_NCW_Struct/bin/cfd_para.hypara b/G02_ThreeD_Electre_Laminar_OneTemperMode_NCW_Struct/bin/cfd_para.hypara index f52cf86..f903a5a 100644 --- a/G02_ThreeD_Electre_Laminar_OneTemperMode_NCW_Struct/bin/cfd_para.hypara +++ b/G02_ThreeD_Electre_Laminar_OneTemperMode_NCW_Struct/bin/cfd_para.hypara @@ -8,54 +8,63 @@ // Platform for Hybrid Engineering Simulation of Flows + // China Aerodynamics Research and Development Center + // (C) Copyright, Since 2010 + +// PHengLEI 2212 + //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ########################################################################### # 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. +// 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. +// 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. -// grid_database_index: Case of typical case, only for gridobj=0. -// 1 -- Laminar flat plate of subsonic flow. -// 2 -- Laminar flat plate of supersonic flow. -// 3 -- Turbulent flat plate of subsonic flow. -// 4 -- Turbulent flat plate of supersonic flow. // iadapt: Adaptation number for unstructure grid. -// iovrlap: Overlapping(overset) grid or not. -// 0 -- NON-overlapping grid. -// 1 -- Overlapping grid. // SymmetryFaceVector: The vector of symmetry face. // 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 grid_database_index = 3; int iadapt = 0; -int iovrlap = 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. -int axisup = 1; +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; // 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; +int omitRepeatInterface = 1; //----------------------------------------------------------------------- # Grid data type # @@ -70,6 +79,7 @@ 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. @@ -82,29 +92,25 @@ 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/rae2822_hybrid2d.cas"; -string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; +int numberOfGridFile = 1; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +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; // fileformat: Ustar Grid file format. // 0 -- BINARY. // 1 -- ASCII. int fileformat = 0; -// .skl meaning skeleton. -string original_grid_info_file = "./grid/FLUENT_test.skl"; - // 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. -// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver. -string mixgrid_uns = "./grid/rae2822_uns2d_4.fts"; -string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts"; -string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp"; +// 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; @@ -113,38 +119,59 @@ 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"; +// ----------------- Grid Refine Parameters ----------------------------- +// anisoRefine: If refine grid by anisoRefine type. +// 0 -- Not. (default) +// 1 -- Yes. +// 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 anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; +int exclusiveCase = 0; +int projectOrgPoint = 0; 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. +// ----------------- Grid Deform Parameters ----------------------------- +// deformationMethod: Grid Deform. +// 1 -- SPRING. +// 2 -- RBF. +// stationalGridFile: Original grid file. +// visualFileName : The visualization file path of deform grid. +// nDeformStep : The max deform step. +// flapAngle : The max flap angle. +// rotatePostionZ : Rotate postion. +// rotatePostionY : Rotate postion. +// gridSlice : If dump slice grid. +// sliceAxis : Grid slice axis. +// slicePosition : Grid slice position. +int nDeformStep = 40; +double flapAngle = 10.0; +double rotatePostionZ = 4.00003; +double rotatePostionY = 3.05; + +int deformationMethod = 2; +string stationalGridFile = "./grid/Segment2Brid.fts"; +string visualFileName = "./results/deformedGrid.dat" + +int gridSlice = 1; +int sliceAxis = 1; +double slicePosition = 13; // ----------------- RBF Parameters ------------------------------------- -// 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; +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. +int numberOfReferenceCP = 40; +double influencePara = 25.0; // ----------------- Periodic Parameters -------------------------------- // Notice: Rotational periodicity only support rotation along the X axis! @@ -152,8 +179,12 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of // 0 -- without Periodic Boundary. // 1 -- Translational periodicity. // 2 -- Rotational periodicity. +// translationLength[]: The relative distance between two periodic face + which only support one direction. +// rotationAngle: The relative angle between two periodic face. + which is recorded in degrees. int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; +double translationLength[] = [0.0, 0.0, 0.0]; double rotationAngle = 0.0; ######################################################################### @@ -164,22 +195,29 @@ 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. // 1 -- Yes. // blockIndexOfMark: the block index of mark, only for structured grid partition. -// cellIndexOfMark: the cell 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]; +int cellIndexOfMark[] = [185, 30, 1]; + +// parallelStrategy: +// 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). +// 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"; @@ -189,7 +227,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts"; // 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. +// parallelPartitionMethod: 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. @@ -197,11 +235,10 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts"; // 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; +double parmetisBalance = 1.05; // numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. // 1 -- single level. @@ -213,29 +250,35 @@ 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. +// 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; +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; int intervalStepSample = 1000; -int intervalStepForce = 100; -int intervalStepRes = 10; -int ifLowSpeedPrecon = 0; +int intervalStepForce = 100; +int intervalStepRes = 10; // compressible: // 0 -- incompressible flow. // 1 -- compressible flow. (default) int compressible = 1; +// 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) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 1; + //----------------------------------------------------------------------- # CFD Control Parameter # //----------------------------------------------------------------------- @@ -246,39 +289,41 @@ int compressible = 1; // 0 -- the nondimensional conditions. // 1 -- the flight conditions. // 2 -- the experiment conditions. -// 3 -- the subsonic boundary conditions. +// 3 -- the subsonic boundary conditions. (Useless!) +// 4 -- the condition that the velocity, temperature and density are given. +// 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 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. -// dump_Q: Dump out thermal flux Q of solid wall. -// 0 -- no dump out. -// 1 -- dump out wall Q only. -// 2 -- dump out wall Q & the typical position Q of ball. -// 3 -- dump out wall Q & the typical position Q of cone. -// 4 -- dump out wall Q & the typical position Q of double sphere. -// 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. +// 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 = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. +// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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. - +// 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; +int flowInitMethod = 0; int inflowParaType = 0; double refReNumber = 6.5e6; double refDimensionalTemperature = 288.15; -double freestream_vibration_temperature = 10000.00; +double freestream_vibration_temperature = 300.00; //int inflowParaType = 1; //double height = 0.001; @@ -287,54 +332,75 @@ double freestream_vibration_temperature = 10000.00; //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; +// 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 = 1000.0; +//double refDimensionalPressure = 1.0e5; + +// The MachNumber, temperature and pressure are fixed. +//int inflowParaType = 6; +//double refDimensionalTemperature = 293.0; +//double refDimensionalPressure = 8886.06; + +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; double wallTemperature = -1.0; -int dump_Q = 0; double radiationCoef = 0.8; double gridScaleFactor = 1.0; +double gridTranslationVector[] = [0.0, 0.0, 0.0]; -double forceRefenenceLengthSpanWise = 1.0; // unit of meter. -double forceRefenenceLength = 1.0; // unit of meter. -double forceRefenenceArea = 1.0; // unit of meter^2. +int numberOfAerodynamicForceComponents = 1; +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. +double knudsenLength = 1.0; // unit of meter. +double refMolecularWeight = 28.9644; // unit of g/mol. //----------------------------------------------------------------------- # Spatial Discretisation # //----------------------------------------------------------------------- -#******************************************************************* -# Struct Solver * -#******************************************************************* +#************************************************************************ +# 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". +// -- "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. +// -- "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"; -string str_limiter_name = "vanalbada"; +int isWennScheme = 0; +string str_limiter_name = "vanalbada"; -#******************************************************************* -# UnStruct Solver or Common * -#******************************************************************* +#************************************************************************ +# UnStruct Solver or Common * +#************************************************************************ // viscousType: Viscous model. -// 0 -- Euler. -// 1 -- Lamilar. -// 2 -- Algebraic. -// 3 -- 1eq turbulent. -// 4 -- 2eq turbulent. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. // viscousName: Laminar or tubulent model. // -- "0eq-bl". // -- "1eq-sa". @@ -353,16 +419,16 @@ string str_limiter_name = "vanalbada"; // 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". +// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", +// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // uns_limiter_name: Limiter of Unstruct grid. -// -- "barth", "vencat", "vanleer", "minmod". -// -- "vanalbada", "smooth", "nnd", "lpz", "1st". +// -- "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". +// gradientName: 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. @@ -385,17 +451,18 @@ 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; +//int viscousType = 0; //string viscousName = "Euler"; -//int viscousType = 1; +//int viscousType = 1; //string viscousName = "laminar"; -int viscousType = 3; +int viscousType = 3; string viscousName = "1eq-sa"; -//int viscousType = 4; +//int viscousType = 4; //string viscousName = "2eq-kw-menter-sst"; int DESType = 0; @@ -405,124 +472,153 @@ string uns_limiter_name = "vencat"; string uns_vis_name = "test"; string gradientName = "ggnode"; -int ivencat = 7; +int ivencat = 7; double venkatCoeff = 5.0; int reconmeth = 1; int limitVariables = 0; int limitVector = 0; -double limit_angle = 0; double skewnessAngle = 60.0; int roeEntropyFixMethod = 3; double roeEntropyScale = 1.0; -//----------------------------------------------------------------------- -# Temporal Discretisation # -//----------------------------------------------------------------------- +double AusmpwPlusLimiter = 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. +// ifStaticsFlowField: Statistical variables for unsteady simulation. +// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation. // startStatisticStep: Outer step when start statistics. // when the value is larger than "maxSimuStep", it is useless. +// 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 = - ^2 +// 1 -- tau = // 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. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 4 -- LU-SGS. +// 5 -- Block LU-SGS. +// 6 -- Jacobian iteration. +// 7 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. // 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. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. // 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. +// 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. -// iale: 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. +// 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. +// 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; +int iunsteady = 0; double physicalTimeStep = 0.01; +double physicalTimeStepDimensional = -0.001; int ifStartFromSteadyResults = 0; int ifStaticsFlowField = 0; +int ifStaticsReynoldsStress = 0; int startStatisticStep = 800000; +double statisticalTimePeriod = -1.0; +int statisticMethod = 0; +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 tscheme = 4; int iSimplifyViscousTerm = 1; int ifLocalTimeStep = 0; -double CFLStart = 0.01; -double CFLEnd = 10.0; -int CFLVaryStep = 500; +int isUseLocalCFL = 0; +int isUsePreTwall = 0; +double CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; +double pMaxForCFL = 0.2; +double pMinForCFL = 0.1; +double deltaMaxForCFL = 0.2; +double magnifyFactorForCFL = 1.1; +double reduceFactorForCFL = 0.5; -double ktmax = 1.0e10; +double ktmax = 1.0e10; -int swapDq = 1; +int swapDq = 1; int nLUSGSSweeps = 1; double LUSGSTolerance = 0.01; -int order = 2; +int order = 2; double visl_min = 0.01; double turbCFLScale = 1.0; - +double csrv = 1.0; double timemax = 1.0e10; double dtsave = -1.0; -int iale = 0; -int ialetype = 2; int maxale = 10; double dtau = 0.001; -double dtau_max = 1E-01; 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; //int RKStage = 4; //double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; - -//----------------------------------------------------------------------- -# File In or Out # -//----------------------------------------------------------------------- +#************************************************************************ +# 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! -// isPlotVolumeField: If dump out the field results to visulization. +// 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. @@ -532,47 +628,67 @@ double lamda[] = 0.5, 1.0; // 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. +// 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. +// 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 numberOfGridGroups = 1; -string gridfile = "./grid/rae2822_hybrid2d__4.fts"; - +int nIsComputeWallDist = 0; int walldistMethod = 1; +int cellMethodOrNodeMethod = 0; string resSaveFile = "results/res.dat"; string turbresfile = "results/turbres.dat"; +string transitionResFile = "results/transitionRes.dat"; string aircoeffile = "results/aircoef.dat"; string restartNSFile = "results/flow.dat"; string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; string visualfile = "results/tecflow.plt"; -string Qwall_file = "results/Qwall.dat"; string wall_aircoefile = "results/wall_aircoef.dat"; -string probesflowfile = "results/sample.dat"; -string surfacefile = ""; +string samplefile = "results/sample.dat"; -int nDumpSurfaceInfo = 0; +string protectionFile0 = "results/flow0.dat"; +string protectionFile1 = "results/flow1.dat"; +string wall_heatfluxfile = "results/wall_heatflux.dat"; + +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; + +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; string wall_varfile = ""; -string componentDefineFile = "bin/component.hypara"; -string jetDefineFile = "bin/jet.hypara"; +string sixDofFileName = "results/sixDofInfo.dat"; +string derivativeFileName = "results/identify.dat"; +string hysteresisFileName = "results/force_beta.plt"; -string componentforcefile = "results/component_aircoef.dat"; - -string overset_gridfile = "iblank.ovs"; - -int isPlotVolumeField = 0; +int plotFieldType = 0; // visualfileType: The file type of visualfile. // 0 -- Tecplot binary. // 1 -- Tecplot ASCII. - +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. int visualfileType = 1; +// samplefileMode: The dump mode of sample file. +// 0 -- dump out every probe/line/surface data for all step intervals. +// 1 -- dump out all probe/line/surface data for every step intervals. +int samplefileMode = 0; + // visualSlice: The slice of tecflow. // 0 -- Do not save slice data. // 1 -- comput and save it to sliceFile. @@ -586,11 +702,13 @@ int visualSlice = 0; int sliceAxis = 1; double slicePostion = -0.5; string sliceFile = "results/Slice.plt"; +int dumpWallFaceCenter = 0; // min-max box of the visual block. double lowerPlotFieldBox[] = [0.0 0.0 0.0]; double upperPlotFieldBox[] = [1.0 1.0 1.0]; +//-----------the optional parameters list for the flow field output---------------- // 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), @@ -600,128 +718,207 @@ 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). +// -- 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), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. +//-----------the optional parameters list for the wall boundary condition---------------- +// nVisualWallVariables: The number of visual variables on wall. +// visualWallVariables : dumped variable types, listed as following: +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- 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), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). int nVisualVariables = 8; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; +int nVisualWallVariables = 9; +int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; + // dumpStandardModel: Dump many standard model data. // 1 -- Turbulent flat plate. int dumpStandardModel = 0; -// ifSetProbesToMonitor: Set probes location to Monitor. -// 0 -- Do not monitor. -// 1 -- To monitor and save data to files. -// probesDefineFile: probes location information file. +// 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). +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). // Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!! // probeVariables order must from small to big. -int ifSetProbesToMonitor = 0; -string probesDefineFile = "bin/probes_location.hypara"; -int nProbeVariables = 6; -int probeVariables[] = [0, 1, 2, 3, 4, 5]; -//----------------------------------------------------------------------- -# Turbulence Parameter # -//----------------------------------------------------------------------- +// 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 = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +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. - +// 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 turb_vis_kind = 2; +int turbOrderStruct = 2; int kindOfTurbSource = 0; int mod_turb_res = 0; -double turb_relax = 1.0; -double turb_min_coef = 1.0e-1; double freeStreamViscosity = 1.0e-3; -double muoo = 1.0e-1; -double kwoo = 1.0; +double muoo = 3.0; +double kwoo = 5.0; +int transitionType = 0; +double turbIntensity = -1.0; +int freeturbIntensitySRModify = 0; +double freeDecayXLocation = 0.0; +int compressibleCorrection = 0; +int transitionMaFix = 1; -# maximum eddy viscosity (myt/my) max. +// maximum eddy viscosity (myt/my) max. double eddyViscosityLimit = 1.0e10; -double sdilim = 1.0e20; -double coef_kvist = 1.0; int monitor_vistmax = 0; -//----------------------------------------------------------------------- -# LES Parameter # -//----------------------------------------------------------------------- +#************************************************************************ +# LES Parameter * +#************************************************************************ // iLES: Create LESSolver or not. -// >= 1 - Create LESSolver; -// < 1 - 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. +// = 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. +// = 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. +// = "dsmCom"; +// = "wale"; +// = "sigma". +// 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. +// = 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. +// 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 smagConstant = 0.1; double isotropicConstant = 0.0; double waleConstant = 0.6; +double sigmaConstant = 1.35; 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 # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic 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. +// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas. +// Otherwise, the pure gas with one component is used for perfect gas. // 0 -- Earth gas. // 1 -- Mars gas. +// 2 -- Argon. +// 3 -- Nitrogen. +// nEnergyRecycle: The type of EnergyModel Recycle. +// 0 -- not used. +// 1 -- used. +// nDensityModify: The type of densitymodify. +// 0 -- not used. +// 1 -- used. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. +// 0 -- perfect gas. +// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). // nchemsrc: // 0 -- the source terms are not computed. // 1 -- the source terms are computed. @@ -732,59 +929,284 @@ int monitorNegativeConstant = 0; // 1 -- One-temperature model. // 2 -- Two-temperature model. // 3 -- Three-temperature model. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. +// 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 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: -// 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. +// 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. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// 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]. +// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// 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. +// nSpeciesLimit: limitter of gas species +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// 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 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. +// nAblation: +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. +// isInjection: +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. +// nViscosityModel: +// 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. // 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. +// "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. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "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. +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. int dg_high_order = 0; int iapplication = 0; -int iCodeBranch = 0; -int nm = 5; +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; -// MHD -double bxoo = 0.0; -double byoo = 0.0; -double bzoo = 0.0; +double refGama = 1.4; +double prl = 0.72; +double prt = 0.90; +double sc_l = 0.5; +double sc_t = 0.5; -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 nGasModel = 0; -int nchem = 0; -int nchemsrc = 1; -int nchemrad = 1; -int ntmodel = 1; -int nChemicalFlowStep = 0; +int nIdealState = 0; +int nEnergyRecycle = 1; +int nSlipBCModel = 0; +int nDensityModify = 1; +int nTEnergyModel = 0; +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; -string gasfile = "DK5"; -//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +double sigmaVelocity = 1.0; +double sigmaTemperature = 1.0; +double sigmaMassFraction = 1.0; +double velocitySlipCorrectConstant = 1.0; + +double chemicalRelaxCorf = 1.0; +double chemicalSpectrumRadiusCoef = 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; +double maxTemperature = 50000.0; +double densityMin = 1.0e-8; +double densityMinFactor = 0.1; +double tAdjustmentFactor = 10.0; +double iniSpeedCoef = 1.0; +int iniSpeedMode = 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 nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; + +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; //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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 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; +//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"; + +//string gasfile = "Combustion-12"; +//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; +//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; + +//string gasfile = "Gas-Mixture"; +//string speciesName = "SpeciesA, SpeciesB"; +//string initMassFraction = "1.0, 0.0"; +int nSutherland = 0; +double gamaSpeciesA = 1.4; +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 nFraction = 0; +int nContinueModel = 0; +int nChemicalFlowStep = 0; +int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; ######################################################################### // Multi-Grid parameters. @@ -805,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0; // 1 -- zero order. // 2 -- first-order. (default) // mgCorrectionLimit: Multi-grid correction limit. - int nMGLevel = 1; int MGCoarsestIteration = 1; int MGPreIteration = 1; @@ -827,20 +1248,20 @@ 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"; +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. +#************************************************************************ +# High Order Struct Solver * +#************************************************************************ +// isFVMOrFDM: +// 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) @@ -853,7 +1274,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp"; // -- "roe", "steger". // structhighordergradient: // -- "conservation", "chain_rule". -int ifvfd = 0; +int isFVMOrFDM = 0; string str_highorder_solver = "WCNS"; int SolverStructOrder = 0; double str_highorder_interpolation_epsilon = 1.0e-6; @@ -878,13 +1299,169 @@ 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. +// oversetInterpolationMethod: the method of overset interpolation while field simulation. +// 0 -- set the acceptor cell value by donor cell value. +// 1 -- set the acceptor cell value by distance weight of donor cell value. +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; + +// ----------------- ALE configuration ------------------------------ +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. + +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. +int methodForKineticEquation = 0; +double relaxParameterOfKinetic = 1.0; + +#************************************************************************ +# motive information * +#************************************************************************ +int numberOfMovingBodies = 1; + +############################## body0 ############################## +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. +// -1 given motion partten. +// 0 still. +// 1 six DOF motion. +// 2 three DOF motion. +// 11 X-axis forced motion. +// 12 Y-axis forced motion. +// 13 Z-axis forced motion. +// 14 forced pitch motion. +// 15 forced yaw motion. +// 16 forced roll motion. +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"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; + +// post indentify. +int integralOrder = 4; + // ---------------- 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"; +//@int inflowParaType = 0; +//@double refReNumber = 6.5e6; +//@double refDimensionalTemperature = 288.15; +//@double freestream_vibration_temperature = 300.00; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalVelocity = 0; +//@double refDimensionalDensity = 0; +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ +int isPlotVolumeField = 0; + +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; + +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; + +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ +int isSolveEnergyEquation = 0; +int isSolveTurbEquation = 0; +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/G02_ThreeD_Electre_Laminar_OneTemperMode_NCW_Struct/bin/grid_para.hypara b/G02_ThreeD_Electre_Laminar_OneTemperMode_NCW_Struct/bin/grid_para.hypara index ebb256e..eb53699 100644 --- a/G02_ThreeD_Electre_Laminar_OneTemperMode_NCW_Struct/bin/grid_para.hypara +++ b/G02_ThreeD_Electre_Laminar_OneTemperMode_NCW_Struct/bin/grid_para.hypara @@ -4,9 +4,12 @@ // 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. +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. // from_gtype: Type of grid data type in grid conversion process. // -1 -- MULTI_TYPE. // 1 -- PHengLEI, *.fts. @@ -18,7 +21,9 @@ // 7 -- Hybrid, include both of unstructured and structured grid, *.fts. // 8 -- GMSH, *.msh. int gridtype = 1; -int axisup = 1; +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; int from_gtype = 3; ######################################################################### diff --git a/G05_TwoD_Cylinder_N2-O2_Premixing-Unstruct_1CPU/bin/cfd_para.hypara b/G05_TwoD_Cylinder_N2-O2_Premixing-Unstruct_1CPU/bin/cfd_para.hypara index c344658..f903a5a 100644 --- a/G05_TwoD_Cylinder_N2-O2_Premixing-Unstruct_1CPU/bin/cfd_para.hypara +++ b/G05_TwoD_Cylinder_N2-O2_Premixing-Unstruct_1CPU/bin/cfd_para.hypara @@ -8,23 +8,24 @@ // Platform for Hybrid Engineering Simulation of Flows + // China Aerodynamics Research and Development Center + // (C) Copyright, Since 2010 + +// PHengLEI 2212 + //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ########################################################################### # 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. -// 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. +// 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. +// 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. @@ -46,19 +47,24 @@ 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. -int axisup = 1; +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; // 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; +int omitRepeatInterface = 1; //----------------------------------------------------------------------- # Grid data type # @@ -87,10 +93,9 @@ 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. int numberOfGridFile = 1; -string from_gfile = "./grid/rae2822_hybrid2d.cas"; -string from_gfile1= ""; - -string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; // ----------------- some advanced choices ------------------------------ // iunsteady: The Grid is for unsteady simulation or not. @@ -103,9 +108,9 @@ 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"; +// 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; @@ -119,31 +124,31 @@ string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp"; // 0 -- Not. (default) // 1 -- Yes. // geometryUnit: Geometry unit. -// 1 -- meter. -// 2 -- millimeter. -// 3 -- inch. +// 1 -- meter. +// 2 -- millimeter. +// 3 -- inch. // exclusiveCase: Parallel projection exclusive case. -// 0 -- NON case. -// 1 -- JSM-C2-NPOFF case. -// 2 -- CHNT. +// 0 -- NON case. +// 1 -- JSM-C2-NPOFF case. +// 2 -- CHNT. // projectOrgPoint: If the original wall points need to be projected or not. -int anisoRefine = 0; -int geometryUnit = 1; -int isProject = 0; -int readDist = 0; -int isDeform = 0; +int anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; int exclusiveCase = 0; int projectOrgPoint = 0; string geometryFileName = "./grid/jsm.igs"; // ----------------- Grid Deform Parameters ----------------------------- // deformationMethod: Grid Deform. -// 1 -- SPRING. -// 2 -- RBF. +// 1 -- SPRING. +// 2 -- RBF. // stationalGridFile: Original grid file. // visualFileName : The visualization file path of deform grid. // nDeformStep : The max deform step. -// flapAngle : The max flap angle. +// flapAngle : The max flap angle. // rotatePostionZ : Rotate postion. // rotatePostionY : Rotate postion. // gridSlice : If dump slice grid. @@ -163,10 +168,10 @@ int sliceAxis = 1; double slicePosition = 13; // ----------------- RBF Parameters ------------------------------------- -// numberOfReferenceCP : Number of reference Control Points. -// influencePara : The RBF influence radius parameter. +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. int numberOfReferenceCP = 40; -double influencePara = 25.0; +double influencePara = 25.0; // ----------------- Periodic Parameters -------------------------------- // Notice: Rotational periodicity only support rotation along the X axis! @@ -178,9 +183,8 @@ double influencePara = 25.0; which only support one direction. // rotationAngle: The relative angle between two periodic face. which is recorded in degrees. - int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; +double translationLength[] = [0.0, 0.0, 0.0]; double rotationAngle = 0.0; ######################################################################### @@ -192,7 +196,6 @@ double rotationAngle = 0.0; // 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; @@ -201,20 +204,20 @@ int numberOfMultifile = 1; // 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. +// cellIndexOfMark : the cell index of mark, only for structured grid partition. int traceMark = 0; int blockIndexOfMark = 0; -int cellIndexOfMark[] = [185,30,1]; +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; +// parallelStrategy: +// 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). +// 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"; @@ -232,11 +235,10 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts"; // 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; +double parmetisBalance = 1.05; // numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. // 1 -- single level. @@ -248,29 +250,35 @@ 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. +// 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; +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; int intervalStepSample = 1000; -int intervalStepForce = 100; -int intervalStepRes = 10; -int ifLowSpeedPrecon = 0; +int intervalStepForce = 100; +int intervalStepRes = 10; // compressible: // 0 -- incompressible flow. // 1 -- compressible flow. (default) int compressible = 1; +// 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) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 1; + //----------------------------------------------------------------------- # CFD Control Parameter # //----------------------------------------------------------------------- @@ -281,33 +289,36 @@ int compressible = 1; // 0 -- the nondimensional conditions. // 1 -- the flight conditions. // 2 -- the experiment conditions. -// 3 -- the subsonic boundary conditions. +// 3 -- the subsonic boundary conditions. (Useless!) // 4 -- the condition that the velocity, temperature and density are given. // 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 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. +// 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 = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. // forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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. -// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol. +// 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; +int directionMethod = 0; double refMachNumber = 0.73; double attackd = 2.79; double angleSlide = 0.00; +int flowInitMethod = 0; int inflowParaType = 0; double refReNumber = 6.5e6; @@ -321,29 +332,27 @@ double freestream_vibration_temperature = 300.00; //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; - -//The velocity, temperature and density are fixed. +// The velocity, temperature and density are fixed. //int inflowParaType = 4; //double refDimensionalVelocity = 1000.0; -//double refDimensionalDensity = 1.0e3; +//double refDimensionalDensity = 1.0e3; -//The velocity, temperature and pressure are fixed. +// The velocity, temperature and pressure are fixed. //int inflowParaType = 5; //double refDimensionalVelocity = 1000.0; //double refDimensionalPressure = 1.0e5; -//The MachNumber, temperature and pressure are fixed. +// The MachNumber, temperature and pressure are fixed. //int inflowParaType = 6; -//double refDimensionalTemperature = 293; +//double refDimensionalTemperature = 293.0; //double refDimensionalPressure = 8886.06; +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; + double wallTemperature = -1.0; double radiationCoef = 0.8; @@ -357,41 +366,41 @@ 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. +double knudsenLength = 1.0; // unit of meter. double refMolecularWeight = 28.9644; // unit of g/mol. //----------------------------------------------------------------------- # Spatial Discretisation # //----------------------------------------------------------------------- -#******************************************************************* -# Struct Solver * -#******************************************************************* +#************************************************************************ +# 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". +// -- "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. +// 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" - +// -- "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"; +string str_limiter_name = "vanalbada"; -#******************************************************************* -# UnStruct Solver or Common * -#******************************************************************* +#************************************************************************ +# UnStruct Solver or Common * +#************************************************************************ // viscousType: Viscous model. -// 0 -- Euler. -// 1 -- Lamilar. -// 2 -- Algebraic. -// 3 -- 1eq turbulent. -// 4 -- 2eq turbulent. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. // viscousName: Laminar or tubulent model. // -- "0eq-bl". // -- "1eq-sa". @@ -410,16 +419,16 @@ string str_limiter_name = "vanalbada"; // 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". +// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // uns_limiter_name: Limiter of Unstruct grid. -// -- "barth", "vencat", "vanleer", "minmod". -// -- "vanalbada", "smooth", "nnd", "lpz", "1st". +// -- "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". // gradientName: Gradient reconstruction method. -// -- "default", "ggcell", "ggnode", "lsq". +// -- "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. @@ -442,18 +451,18 @@ 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 +// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0. -//int viscousType = 0; +//int viscousType = 0; //string viscousName = "Euler"; -//int viscousType = 1; +//int viscousType = 1; //string viscousName = "laminar"; -int viscousType = 3; +int viscousType = 3; string viscousName = "1eq-sa"; -//int viscousType = 4; +//int viscousType = 4; //string viscousName = "2eq-kw-menter-sst"; int DESType = 0; @@ -463,7 +472,7 @@ string uns_limiter_name = "vencat"; string uns_vis_name = "test"; string gradientName = "ggnode"; -int ivencat = 7; +int ivencat = 7; double venkatCoeff = 5.0; int reconmeth = 1; int limitVariables = 0; @@ -475,9 +484,9 @@ double roeEntropyScale = 1.0; double AusmpwPlusLimiter = 1.0; -//----------------------------------------------------------------------- -# Temporal Discretisation # -//----------------------------------------------------------------------- +#************************************************************************ +# Temporal Discretisation * +#************************************************************************ // iunsteady: Steady or unsteady. // 0 -- steady. // 1 -- unsteay. @@ -490,51 +499,57 @@ double AusmpwPlusLimiter = 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 = - ^2 -// 1 -- tau = +// 0 -- tau = - ^2 +// 1 -- tau = // 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 -- Line LU-SGS. -// 8 -- Matrix LU-SGS. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 4 -- LU-SGS. +// 5 -- Block LU-SGS. +// 6 -- Jacobian iteration. +// 7 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. // 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. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. // 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. +// 0 --Local. +// 1 --Global. // isUseLocalCFL: use variable number of CFL or not. -// 0 -- global unified CFL number. -// 1 -- local CFL number. +// 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. -// 0 -- no ALE method. -// 1 -- ALE method for non-moving grids. -// 2 -- ALE method for moving grids. -// 3 -- ALE method for deforming grids. +// 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. +// 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; +int iunsteady = 0; double physicalTimeStep = 0.01; double physicalTimeStepDimensional = -0.001; int ifStartFromSteadyResults = 0; @@ -543,39 +558,42 @@ int ifStaticsReynoldsStress = 0; int startStatisticStep = 800000; double statisticalTimePeriod = -1.0; int statisticMethod = 0; -int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2; +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 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 CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; double pMaxForCFL = 0.2; double pMinForCFL = 0.1; double deltaMaxForCFL = 0.2; double magnifyFactorForCFL = 1.1; double reduceFactorForCFL = 0.5; -double ktmax = 1.0e10; +double ktmax = 1.0e10; -int swapDq = 1; +int swapDq = 1; int nLUSGSSweeps = 1; double LUSGSTolerance = 0.01; -int order = 2; +int order = 2; double visl_min = 0.01; double turbCFLScale = 1.0; -double csrv = 2.0; +double csrv = 1.0; double timemax = 1.0e10; double dtsave = -1.0; int maxale = 10; @@ -591,10 +609,9 @@ double lamda[] = [0.5, 1.0]; //int RKStage = 4; //double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; - -//----------------------------------------------------------------------- -# File In or Out # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. @@ -611,20 +628,18 @@ double lamda[] = [0.5, 1.0]; // 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. +// 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. // 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= ""; +// 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; @@ -632,10 +647,12 @@ int cellMethodOrNodeMethod = 0; string resSaveFile = "results/res.dat"; string turbresfile = "results/turbres.dat"; +string transitionResFile = "results/transitionRes.dat"; string aircoeffile = "results/aircoef.dat"; string restartNSFile = "results/flow.dat"; string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; string visualfile = "results/tecflow.plt"; string wall_aircoefile = "results/wall_aircoef.dat"; @@ -645,10 +662,14 @@ string protectionFile0 = "results/flow0.dat"; string protectionFile1 = "results/flow1.dat"; string wall_heatfluxfile = "results/wall_heatflux.dat"; -int nDumpSurfaceInfo = 0; -string wall_varfile = ""; +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; -string jetDefineFile = "bin/jet.hypara"; +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; string sixDofFileName = "results/sixDofInfo.dat"; string derivativeFileName = "results/identify.dat"; @@ -659,7 +680,8 @@ int plotFieldType = 0; // visualfileType: The file type of visualfile. // 0 -- Tecplot binary. // 1 -- Tecplot ASCII. - +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. int visualfileType = 1; // samplefileMode: The dump mode of sample file. @@ -697,21 +719,21 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), 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) +// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. //-----------the optional parameters list for the wall boundary condition---------------- // nVisualWallVariables: The number of visual variables on wall. // visualWallVariables : dumped variable types, listed as following: -// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4), -// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8), -// -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), -Grid Reynolds number on wall(Re_w, 23) +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- 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), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). int nVisualVariables = 8; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; @@ -739,16 +761,18 @@ 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), mach(6). +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). // 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. +// 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; +int dataMonitorType = 0; string probesDefineFile = "bin/probes_XYZ.dat"; //int dataMonitorType = 1; @@ -761,28 +785,26 @@ string probesDefineFile = "bin/probes_XYZ.dat"; int searchCellsMethod = 0; -int nProbeVariables = 7; -int probeVariables[] = [0, 1, 2, 3, 4, 5, 6]; -int probeVariablesInterpolationMethod = 0; -//----------------------------------------------------------------------- -# Turbulence Parameter # -//----------------------------------------------------------------------- +int nProbeVariables = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +int probeVariablesInterpolationMethod = 0; + +#************************************************************************ +# Turbulence Parameter * +#************************************************************************ // turbInterval: Iteration number of turbulence. // kindOfTurbSource: Kinds of turbulent source. // 0 -- Original. // mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0. -// transitionType: transition model type +// 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 - - +// 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; 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; @@ -790,29 +812,28 @@ int transitionType = 0; double turbIntensity = -1.0; int freeturbIntensitySRModify = 0; double freeDecayXLocation = 0.0; -int compressibleCorrection = 0; -int prandtlNumberCorrection = 0; +int compressibleCorrection = 0; int transitionMaFix = 1; -# maximum eddy viscosity (myt/my) max. +// maximum eddy viscosity (myt/my) max. double eddyViscosityLimit = 1.0e10; int monitor_vistmax = 0; -//----------------------------------------------------------------------- -# LES Parameter # -//----------------------------------------------------------------------- +#************************************************************************ +# LES Parameter * +#************************************************************************ // iLES: Create LESSolver or not. -// = 1 - Create LESSolver; -// != 1 - 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. +// = 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. +// = 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. @@ -820,23 +841,22 @@ int monitor_vistmax = 0; // = "dsmCom"; // = "wale"; // = "sigma". -// 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. +// 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. +// = 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. +// 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; @@ -852,19 +872,16 @@ double testFilterScale = 2.0; int averageWidth = 1; int monitorNegativeConstant = 0; -//----------------------------------------------------------------------- -# Other Parameters for Hypersonic Non-equilibrium Gas # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. -// 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. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. @@ -875,7 +892,7 @@ int monitorNegativeConstant = 0; // 2 -- Argon. // 3 -- Nitrogen. // nEnergyRecycle: The type of EnergyModel Recycle. -// 0 -- not used . +// 0 -- not used. // 1 -- used. // nDensityModify: The type of densitymodify. // 0 -- not used. @@ -883,26 +900,25 @@ int monitorNegativeConstant = 0; // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. -// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. // 0 -- perfect gas. // 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. -// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. -// the value equals to or is greater than 1, and 3 is for default value. -// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. -// the value equals to or is greater than 1, and 3 is for default value. -// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. -// the value equals to or is greater than 1, and 3 is for default value. -// nSlipBCModel : The computational model of slip boundary conditions. - -// 0 -- no slip. -// 1 -- the conventional Maxwell slip conditions. -// 2 -- the Gokcen slip conditions. -// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. -// 4 -- the Kogan simplified slip conditions. -// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. -// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). -// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. -// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). // nchemsrc: // 0 -- the source terms are not computed. // 1 -- the source terms are computed. @@ -913,148 +929,151 @@ int monitorNegativeConstant = 0; // 1 -- One-temperature model. // 2 -- Two-temperature model. // 3 -- Three-temperature model. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. // 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. +// 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 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: -// 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. -// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. -// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. -// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. -// 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. +// 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. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// 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]. // velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. -// 1.0 -- proposed by Maxwell. -// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. -// 1.146 -- proposed for an additional "fictitious" velocity slip. - -// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. -// 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. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// 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. // nSpeciesLimit: limitter of gas species -// 0 -- not used. -// 1 -- used. -// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction -// 0 -- method 0. -// 1 -- method 1. -// 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) - +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// 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 +// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs. +// 0 -- not used. +// 1 -- used. +// nDiagonalModified: Modified on Diagonal. +// 0 -- not used. +// 1 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. // nAblation: -// 0 -- The wall ablation is not computed. -// 1 -- The wall ablation is computed. +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. // isInjection: -// 0 -- The injection velocity of ablation wall is not computed. -// 1 -- The injection velocity of ablation wall is computed. +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. // nViscosityModel: -// 0 -- Blottner fitting method(N89). -// 1 -- Gupta fitting method(N90). +// 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. +// 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. +// 0 -- stands for selecting the Blotter curve fits mode. +// 1 -- stands for Sutherland relation. // 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. -// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. -// "Gas-Mixture" -- indicates the process of mixing gas without reacting. -// for struct solver mixing two speciesSpeciesA, SpeciesB. -// for unstruct solver mixing multi-speciesO2 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. +// "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. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "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. +// 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. +// 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 - +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. int dg_high_order = 0; int iapplication = 0; int isAdaptiveSolver = 0; -int nm = 5; +int nm = 5; int nEquilibriumGas = 0; -int nPCWCycleStep = 3; -int nRETCycleStep = 3; -int nSLIPCycleStep= 3; +int nPCWCycleStep = 3; +int nRETCycleStep = 3; +int nSLIPCycleStep = 3; int nIterFirstStep = 1000; int nIterSecondStep= 2000; int nIterThirdStep = 2000; @@ -1065,17 +1084,17 @@ double secondStepError = 0.001; double thirdStepError = 0.001; double predictCFLError = 0.1; -double refGama = 1.4; -double prl = 0.72; -double prt = 0.90; -double sc_l = 0.5; -double sc_t = 0.5; +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 nGasModel = 0; +int nchem = 0; +int nchemsrc = 1; +int nchemrad = 1; +int ntmodel = 1; int nIdealState = 0; int nEnergyRecycle = 1; @@ -1099,12 +1118,12 @@ double sigmaTemperature = 1.0; double sigmaMassFraction = 1.0; double velocitySlipCorrectConstant = 1.0; -double chemicalRelaxCorf = 1.0; +double chemicalRelaxCorf = 1.0; double chemicalSpectrumRadiusCoef = 1.0; double viscousSpectrumRadiusCoef = 1.5; double inviscidSpectrumRadiusCoef = 1.5; -double spectrumRadiusCoef = 0.5; -double staticPressureRelaxCorf = 0.2; +double spectrumRadiusCoef = 0.5; +double staticPressureRelaxCorf = 0.2; double maxViscous = 10000.0; double trTemperatureMin = 10.0; @@ -1114,31 +1133,35 @@ double densityMin = 1.0e-8; double densityMinFactor = 0.1; double tAdjustmentFactor = 10.0; double iniSpeedCoef = 1.0; +int iniSpeedMode = 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 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 nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; -int nProtectData = 0; -int useHyflowSetting = 0; -int nAblation = 0; -int isInjection = 0; -int nViscosityModel = 0; -int nMarsModel = 0; -string gasfile = "DK5"; -//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; string speciesName = "O, O2, NO, N, N2"; string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; @@ -1152,16 +1175,16 @@ 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 = "Pa"; +//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"; -//string gasfile = "Combustion-12"; +//string gasfile = "Combustion-12"; //string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; //string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; //string gasfile = "Gas-Mixture"; -//string speciesName ="SpeciesA, SpeciesB"; +//string speciesName = "SpeciesA, SpeciesB"; //string initMassFraction = "1.0, 0.0"; int nSutherland = 0; double gamaSpeciesA = 1.4; @@ -1173,9 +1196,17 @@ double molecularWeightSpeciesB = 30.0; //string speciesName = "O2, N2"; //string initMassFraction = "1.0, 0.0"; +int nFraction = 0; int nContinueModel = 0; int nChemicalFlowStep = 0; int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; ######################################################################### // Multi-Grid parameters. @@ -1196,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0; // 1 -- zero order. // 2 -- first-order. (default) // mgCorrectionLimit: Multi-grid correction limit. - int nMGLevel = 1; int MGCoarsestIteration = 1; int MGPreIteration = 1; @@ -1218,20 +1248,20 @@ 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"; +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 # -######################################################################### +#************************************************************************ +# High Order Struct Solver * +#************************************************************************ // isFVMOrFDM: -// 0 -- NSSolverStruct using Finite Volume Method. -// 1 -- NSSolverStruct using Finite Differ Method. +// 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) @@ -1273,30 +1303,48 @@ int allReduceStep = 1; // codeOfOversetGrid: Overlapping(overset) grid or not. // 0 -- NON-overlapping grid. // 1 -- Overlapping grid. -// oversetInterpolationMethod: the method of overset interpolation while field simulation +// oversetInterpolationMethod: the method of overset interpolation while field simulation. // 0 -- set the acceptor cell value by donor cell value. // 1 -- set the acceptor cell value by distance weight of donor cell value. - -int codeOfOversetGrid = 0; -int oversetInterpolationMethod = 0; -int readOversetFileOrNot = 0; -int symetryOrNot = 0; -int readInAuxiliaryInnerGrid = 0; -int readInAuxiliaryOuterGrid = 0; -int readInSklFileOrNot = 0; -string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; -string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; -string auxiliaryInnerGrid2 = ""; -string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; - -int numberOfMovingBodies = 2; +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; // ----------------- ALE configuration ------------------------------ int codeOfAleModel = 0; @@ -1306,36 +1354,42 @@ 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; +int strategyForFaceNormalVelocity = 0; // 0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd. +int strategyForGCLSource = 0; // 0-present; 1-Ahn. -//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. int methodForKineticEquation = 0; double relaxParameterOfKinetic = 1.0; -######################################################################### -# motive information # -######################################################################### +#************************************************************************ +# motive information * +#************************************************************************ int numberOfMovingBodies = 1; ############################## body0 ############################## -//mass of parts -double mass_0 = 1.0; -//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz -double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; -//initial six DOF position information of parts. xc yc zc -double massCenter_0[] = 0.0 , 0.0, 0.0; -//initial six DOF position information of parts. angleX angleY angleZ -double attitudeAngle_0[] = 0.0 , 0.0, 0.0; -//initial six DOF move information of parts. vc vy vz -double massCenterVelocity_0[] = 0.0, 0.0, 0.0; -//initial six DOF move information of parts. omigX omigY omigZ -double angularVelocity_0[] = 0.0, 0.0, 0.0; -//the object that the parts belong to. -int fartherIndex_0 = -1; -//the assembly position of the parts. xc yc zc angleX angleY angleZ -double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0; -//the move pattern of the parts. +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. // -1 given motion partten. // 0 still. // 1 six DOF motion. @@ -1346,51 +1400,68 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 // 14 forced pitch motion. // 15 forced yaw motion. // 16 forced roll motion. -int RBDMethod_0 = 0; -double amplitude_0 = 0.0; -double reduceFrequency_0 = 0.0; -//direction of rotation +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 ; -//additional moment of Force (system axis) mX mY mZ -double addedMoment_0[] = 0.0 ,0.0 ,0.0 ; -//the deformation method of the parts. -int morphing_0 = 0; - -// post indentify -int integralOrder = 4; +int direction_0 = -1; +double rotateFrequency_0 = 0.0; +//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; +// post indentify. +int integralOrder = 4; // ---------------- ATP read -------------------------------------------- -//@int inflowParaType = 0; +//@int inflowParaType = 0; //@double refReNumber = 6.5e6; //@double refDimensionalTemperature = 288.15; //@double freestream_vibration_temperature = 300.00; -//@double refDimensionalPressure = 0; -//@double height = 0; -//@int nsubsonicInlet = 0; -//@int nsubsonicOutlet = 0; -//@string inLetFileName = "./bin/subsonicInlet.hypara"; -//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; //@double refDimensionalVelocity = 0; //@double refDimensionalDensity = 0; - -######################################################################### -# Old Parameter # -######################################################################### +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ int isPlotVolumeField = 0; +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; -######################################################################### -# Incompressible Parameter # -######################################################################### +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ int isSolveEnergyEquation = 0; int isSolveTurbEquation = 0; -int isSolveSpeciesEquation = 0; - +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/G05_TwoD_Cylinder_N2-O2_Premixing-Unstruct_1CPU/bin/grid_para.hypara b/G05_TwoD_Cylinder_N2-O2_Premixing-Unstruct_1CPU/bin/grid_para.hypara index caa5018..ded8b44 100644 --- a/G05_TwoD_Cylinder_N2-O2_Premixing-Unstruct_1CPU/bin/grid_para.hypara +++ b/G05_TwoD_Cylinder_N2-O2_Premixing-Unstruct_1CPU/bin/grid_para.hypara @@ -4,9 +4,12 @@ // 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. +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. // from_gtype: Type of grid data type in grid conversion process. // -1 -- MULTI_TYPE. // 1 -- PHengLEI, *.fts. @@ -18,7 +21,9 @@ // 7 -- Hybrid, include both of unstructured and structured grid, *.fts. // 8 -- GMSH, *.msh. int gridtype = 0; -int axisup = 1; +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; int from_gtype = 2; ######################################################################### # File path # diff --git a/G05_TwoD_Cylinder_N2-O2_Premixing-Unstruct_1CPU/二维非结构圆柱高超声速两气体组分预混算例说明文档.pdf b/G05_TwoD_Cylinder_N2-O2_Premixing-Unstruct_1CPU/二维非结构圆柱高超声速两气体组分预混算例说明文档.pdf index 7137ba0..59a6a4c 100644 Binary files a/G05_TwoD_Cylinder_N2-O2_Premixing-Unstruct_1CPU/二维非结构圆柱高超声速两气体组分预混算例说明文档.pdf and b/G05_TwoD_Cylinder_N2-O2_Premixing-Unstruct_1CPU/二维非结构圆柱高超声速两气体组分预混算例说明文档.pdf differ diff --git a/G06_ThreeD_Sphere_N2-O2_Premixing-Unstruct_1CPU/bin/cfd_para.hypara b/G06_ThreeD_Sphere_N2-O2_Premixing-Unstruct_1CPU/bin/cfd_para.hypara index c344658..f903a5a 100644 --- a/G06_ThreeD_Sphere_N2-O2_Premixing-Unstruct_1CPU/bin/cfd_para.hypara +++ b/G06_ThreeD_Sphere_N2-O2_Premixing-Unstruct_1CPU/bin/cfd_para.hypara @@ -8,23 +8,24 @@ // Platform for Hybrid Engineering Simulation of Flows + // China Aerodynamics Research and Development Center + // (C) Copyright, Since 2010 + +// PHengLEI 2212 + //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ########################################################################### # 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. -// 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. +// 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. +// 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. @@ -46,19 +47,24 @@ 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. -int axisup = 1; +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; // 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; +int omitRepeatInterface = 1; //----------------------------------------------------------------------- # Grid data type # @@ -87,10 +93,9 @@ 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. int numberOfGridFile = 1; -string from_gfile = "./grid/rae2822_hybrid2d.cas"; -string from_gfile1= ""; - -string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; // ----------------- some advanced choices ------------------------------ // iunsteady: The Grid is for unsteady simulation or not. @@ -103,9 +108,9 @@ 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"; +// 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; @@ -119,31 +124,31 @@ string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp"; // 0 -- Not. (default) // 1 -- Yes. // geometryUnit: Geometry unit. -// 1 -- meter. -// 2 -- millimeter. -// 3 -- inch. +// 1 -- meter. +// 2 -- millimeter. +// 3 -- inch. // exclusiveCase: Parallel projection exclusive case. -// 0 -- NON case. -// 1 -- JSM-C2-NPOFF case. -// 2 -- CHNT. +// 0 -- NON case. +// 1 -- JSM-C2-NPOFF case. +// 2 -- CHNT. // projectOrgPoint: If the original wall points need to be projected or not. -int anisoRefine = 0; -int geometryUnit = 1; -int isProject = 0; -int readDist = 0; -int isDeform = 0; +int anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; int exclusiveCase = 0; int projectOrgPoint = 0; string geometryFileName = "./grid/jsm.igs"; // ----------------- Grid Deform Parameters ----------------------------- // deformationMethod: Grid Deform. -// 1 -- SPRING. -// 2 -- RBF. +// 1 -- SPRING. +// 2 -- RBF. // stationalGridFile: Original grid file. // visualFileName : The visualization file path of deform grid. // nDeformStep : The max deform step. -// flapAngle : The max flap angle. +// flapAngle : The max flap angle. // rotatePostionZ : Rotate postion. // rotatePostionY : Rotate postion. // gridSlice : If dump slice grid. @@ -163,10 +168,10 @@ int sliceAxis = 1; double slicePosition = 13; // ----------------- RBF Parameters ------------------------------------- -// numberOfReferenceCP : Number of reference Control Points. -// influencePara : The RBF influence radius parameter. +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. int numberOfReferenceCP = 40; -double influencePara = 25.0; +double influencePara = 25.0; // ----------------- Periodic Parameters -------------------------------- // Notice: Rotational periodicity only support rotation along the X axis! @@ -178,9 +183,8 @@ double influencePara = 25.0; which only support one direction. // rotationAngle: The relative angle between two periodic face. which is recorded in degrees. - int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; +double translationLength[] = [0.0, 0.0, 0.0]; double rotationAngle = 0.0; ######################################################################### @@ -192,7 +196,6 @@ double rotationAngle = 0.0; // 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; @@ -201,20 +204,20 @@ int numberOfMultifile = 1; // 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. +// cellIndexOfMark : the cell index of mark, only for structured grid partition. int traceMark = 0; int blockIndexOfMark = 0; -int cellIndexOfMark[] = [185,30,1]; +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; +// parallelStrategy: +// 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). +// 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"; @@ -232,11 +235,10 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts"; // 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; +double parmetisBalance = 1.05; // numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. // 1 -- single level. @@ -248,29 +250,35 @@ 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. +// 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; +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; int intervalStepSample = 1000; -int intervalStepForce = 100; -int intervalStepRes = 10; -int ifLowSpeedPrecon = 0; +int intervalStepForce = 100; +int intervalStepRes = 10; // compressible: // 0 -- incompressible flow. // 1 -- compressible flow. (default) int compressible = 1; +// 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) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 1; + //----------------------------------------------------------------------- # CFD Control Parameter # //----------------------------------------------------------------------- @@ -281,33 +289,36 @@ int compressible = 1; // 0 -- the nondimensional conditions. // 1 -- the flight conditions. // 2 -- the experiment conditions. -// 3 -- the subsonic boundary conditions. +// 3 -- the subsonic boundary conditions. (Useless!) // 4 -- the condition that the velocity, temperature and density are given. // 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 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. +// 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 = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. // forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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. -// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol. +// 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; +int directionMethod = 0; double refMachNumber = 0.73; double attackd = 2.79; double angleSlide = 0.00; +int flowInitMethod = 0; int inflowParaType = 0; double refReNumber = 6.5e6; @@ -321,29 +332,27 @@ double freestream_vibration_temperature = 300.00; //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; - -//The velocity, temperature and density are fixed. +// The velocity, temperature and density are fixed. //int inflowParaType = 4; //double refDimensionalVelocity = 1000.0; -//double refDimensionalDensity = 1.0e3; +//double refDimensionalDensity = 1.0e3; -//The velocity, temperature and pressure are fixed. +// The velocity, temperature and pressure are fixed. //int inflowParaType = 5; //double refDimensionalVelocity = 1000.0; //double refDimensionalPressure = 1.0e5; -//The MachNumber, temperature and pressure are fixed. +// The MachNumber, temperature and pressure are fixed. //int inflowParaType = 6; -//double refDimensionalTemperature = 293; +//double refDimensionalTemperature = 293.0; //double refDimensionalPressure = 8886.06; +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; + double wallTemperature = -1.0; double radiationCoef = 0.8; @@ -357,41 +366,41 @@ 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. +double knudsenLength = 1.0; // unit of meter. double refMolecularWeight = 28.9644; // unit of g/mol. //----------------------------------------------------------------------- # Spatial Discretisation # //----------------------------------------------------------------------- -#******************************************************************* -# Struct Solver * -#******************************************************************* +#************************************************************************ +# 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". +// -- "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. +// 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" - +// -- "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"; +string str_limiter_name = "vanalbada"; -#******************************************************************* -# UnStruct Solver or Common * -#******************************************************************* +#************************************************************************ +# UnStruct Solver or Common * +#************************************************************************ // viscousType: Viscous model. -// 0 -- Euler. -// 1 -- Lamilar. -// 2 -- Algebraic. -// 3 -- 1eq turbulent. -// 4 -- 2eq turbulent. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. // viscousName: Laminar or tubulent model. // -- "0eq-bl". // -- "1eq-sa". @@ -410,16 +419,16 @@ string str_limiter_name = "vanalbada"; // 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". +// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // uns_limiter_name: Limiter of Unstruct grid. -// -- "barth", "vencat", "vanleer", "minmod". -// -- "vanalbada", "smooth", "nnd", "lpz", "1st". +// -- "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". // gradientName: Gradient reconstruction method. -// -- "default", "ggcell", "ggnode", "lsq". +// -- "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. @@ -442,18 +451,18 @@ 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 +// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0. -//int viscousType = 0; +//int viscousType = 0; //string viscousName = "Euler"; -//int viscousType = 1; +//int viscousType = 1; //string viscousName = "laminar"; -int viscousType = 3; +int viscousType = 3; string viscousName = "1eq-sa"; -//int viscousType = 4; +//int viscousType = 4; //string viscousName = "2eq-kw-menter-sst"; int DESType = 0; @@ -463,7 +472,7 @@ string uns_limiter_name = "vencat"; string uns_vis_name = "test"; string gradientName = "ggnode"; -int ivencat = 7; +int ivencat = 7; double venkatCoeff = 5.0; int reconmeth = 1; int limitVariables = 0; @@ -475,9 +484,9 @@ double roeEntropyScale = 1.0; double AusmpwPlusLimiter = 1.0; -//----------------------------------------------------------------------- -# Temporal Discretisation # -//----------------------------------------------------------------------- +#************************************************************************ +# Temporal Discretisation * +#************************************************************************ // iunsteady: Steady or unsteady. // 0 -- steady. // 1 -- unsteay. @@ -490,51 +499,57 @@ double AusmpwPlusLimiter = 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 = - ^2 -// 1 -- tau = +// 0 -- tau = - ^2 +// 1 -- tau = // 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 -- Line LU-SGS. -// 8 -- Matrix LU-SGS. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 4 -- LU-SGS. +// 5 -- Block LU-SGS. +// 6 -- Jacobian iteration. +// 7 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. // 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. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. // 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. +// 0 --Local. +// 1 --Global. // isUseLocalCFL: use variable number of CFL or not. -// 0 -- global unified CFL number. -// 1 -- local CFL number. +// 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. -// 0 -- no ALE method. -// 1 -- ALE method for non-moving grids. -// 2 -- ALE method for moving grids. -// 3 -- ALE method for deforming grids. +// 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. +// 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; +int iunsteady = 0; double physicalTimeStep = 0.01; double physicalTimeStepDimensional = -0.001; int ifStartFromSteadyResults = 0; @@ -543,39 +558,42 @@ int ifStaticsReynoldsStress = 0; int startStatisticStep = 800000; double statisticalTimePeriod = -1.0; int statisticMethod = 0; -int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2; +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 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 CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; double pMaxForCFL = 0.2; double pMinForCFL = 0.1; double deltaMaxForCFL = 0.2; double magnifyFactorForCFL = 1.1; double reduceFactorForCFL = 0.5; -double ktmax = 1.0e10; +double ktmax = 1.0e10; -int swapDq = 1; +int swapDq = 1; int nLUSGSSweeps = 1; double LUSGSTolerance = 0.01; -int order = 2; +int order = 2; double visl_min = 0.01; double turbCFLScale = 1.0; -double csrv = 2.0; +double csrv = 1.0; double timemax = 1.0e10; double dtsave = -1.0; int maxale = 10; @@ -591,10 +609,9 @@ double lamda[] = [0.5, 1.0]; //int RKStage = 4; //double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; - -//----------------------------------------------------------------------- -# File In or Out # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. @@ -611,20 +628,18 @@ double lamda[] = [0.5, 1.0]; // 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. +// 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. // 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= ""; +// 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; @@ -632,10 +647,12 @@ int cellMethodOrNodeMethod = 0; string resSaveFile = "results/res.dat"; string turbresfile = "results/turbres.dat"; +string transitionResFile = "results/transitionRes.dat"; string aircoeffile = "results/aircoef.dat"; string restartNSFile = "results/flow.dat"; string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; string visualfile = "results/tecflow.plt"; string wall_aircoefile = "results/wall_aircoef.dat"; @@ -645,10 +662,14 @@ string protectionFile0 = "results/flow0.dat"; string protectionFile1 = "results/flow1.dat"; string wall_heatfluxfile = "results/wall_heatflux.dat"; -int nDumpSurfaceInfo = 0; -string wall_varfile = ""; +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; -string jetDefineFile = "bin/jet.hypara"; +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; string sixDofFileName = "results/sixDofInfo.dat"; string derivativeFileName = "results/identify.dat"; @@ -659,7 +680,8 @@ int plotFieldType = 0; // visualfileType: The file type of visualfile. // 0 -- Tecplot binary. // 1 -- Tecplot ASCII. - +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. int visualfileType = 1; // samplefileMode: The dump mode of sample file. @@ -697,21 +719,21 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), 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) +// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. //-----------the optional parameters list for the wall boundary condition---------------- // nVisualWallVariables: The number of visual variables on wall. // visualWallVariables : dumped variable types, listed as following: -// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4), -// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8), -// -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), -Grid Reynolds number on wall(Re_w, 23) +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- 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), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). int nVisualVariables = 8; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; @@ -739,16 +761,18 @@ 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), mach(6). +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). // 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. +// 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; +int dataMonitorType = 0; string probesDefineFile = "bin/probes_XYZ.dat"; //int dataMonitorType = 1; @@ -761,28 +785,26 @@ string probesDefineFile = "bin/probes_XYZ.dat"; int searchCellsMethod = 0; -int nProbeVariables = 7; -int probeVariables[] = [0, 1, 2, 3, 4, 5, 6]; -int probeVariablesInterpolationMethod = 0; -//----------------------------------------------------------------------- -# Turbulence Parameter # -//----------------------------------------------------------------------- +int nProbeVariables = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +int probeVariablesInterpolationMethod = 0; + +#************************************************************************ +# Turbulence Parameter * +#************************************************************************ // turbInterval: Iteration number of turbulence. // kindOfTurbSource: Kinds of turbulent source. // 0 -- Original. // mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0. -// transitionType: transition model type +// 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 - - +// 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; 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; @@ -790,29 +812,28 @@ int transitionType = 0; double turbIntensity = -1.0; int freeturbIntensitySRModify = 0; double freeDecayXLocation = 0.0; -int compressibleCorrection = 0; -int prandtlNumberCorrection = 0; +int compressibleCorrection = 0; int transitionMaFix = 1; -# maximum eddy viscosity (myt/my) max. +// maximum eddy viscosity (myt/my) max. double eddyViscosityLimit = 1.0e10; int monitor_vistmax = 0; -//----------------------------------------------------------------------- -# LES Parameter # -//----------------------------------------------------------------------- +#************************************************************************ +# LES Parameter * +#************************************************************************ // iLES: Create LESSolver or not. -// = 1 - Create LESSolver; -// != 1 - 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. +// = 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. +// = 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. @@ -820,23 +841,22 @@ int monitor_vistmax = 0; // = "dsmCom"; // = "wale"; // = "sigma". -// 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. +// 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. +// = 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. +// 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; @@ -852,19 +872,16 @@ double testFilterScale = 2.0; int averageWidth = 1; int monitorNegativeConstant = 0; -//----------------------------------------------------------------------- -# Other Parameters for Hypersonic Non-equilibrium Gas # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. -// 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. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. @@ -875,7 +892,7 @@ int monitorNegativeConstant = 0; // 2 -- Argon. // 3 -- Nitrogen. // nEnergyRecycle: The type of EnergyModel Recycle. -// 0 -- not used . +// 0 -- not used. // 1 -- used. // nDensityModify: The type of densitymodify. // 0 -- not used. @@ -883,26 +900,25 @@ int monitorNegativeConstant = 0; // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. -// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. // 0 -- perfect gas. // 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. -// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. -// the value equals to or is greater than 1, and 3 is for default value. -// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. -// the value equals to or is greater than 1, and 3 is for default value. -// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. -// the value equals to or is greater than 1, and 3 is for default value. -// nSlipBCModel : The computational model of slip boundary conditions. - -// 0 -- no slip. -// 1 -- the conventional Maxwell slip conditions. -// 2 -- the Gokcen slip conditions. -// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. -// 4 -- the Kogan simplified slip conditions. -// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. -// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). -// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. -// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). // nchemsrc: // 0 -- the source terms are not computed. // 1 -- the source terms are computed. @@ -913,148 +929,151 @@ int monitorNegativeConstant = 0; // 1 -- One-temperature model. // 2 -- Two-temperature model. // 3 -- Three-temperature model. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. // 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. +// 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 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: -// 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. -// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. -// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. -// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. -// 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. +// 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. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// 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]. // velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. -// 1.0 -- proposed by Maxwell. -// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. -// 1.146 -- proposed for an additional "fictitious" velocity slip. - -// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. -// 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. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// 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. // nSpeciesLimit: limitter of gas species -// 0 -- not used. -// 1 -- used. -// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction -// 0 -- method 0. -// 1 -- method 1. -// 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) - +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// 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 +// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs. +// 0 -- not used. +// 1 -- used. +// nDiagonalModified: Modified on Diagonal. +// 0 -- not used. +// 1 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. // nAblation: -// 0 -- The wall ablation is not computed. -// 1 -- The wall ablation is computed. +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. // isInjection: -// 0 -- The injection velocity of ablation wall is not computed. -// 1 -- The injection velocity of ablation wall is computed. +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. // nViscosityModel: -// 0 -- Blottner fitting method(N89). -// 1 -- Gupta fitting method(N90). +// 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. +// 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. +// 0 -- stands for selecting the Blotter curve fits mode. +// 1 -- stands for Sutherland relation. // 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. -// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. -// "Gas-Mixture" -- indicates the process of mixing gas without reacting. -// for struct solver mixing two speciesSpeciesA, SpeciesB. -// for unstruct solver mixing multi-speciesO2 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. +// "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. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "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. +// 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. +// 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 - +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. int dg_high_order = 0; int iapplication = 0; int isAdaptiveSolver = 0; -int nm = 5; +int nm = 5; int nEquilibriumGas = 0; -int nPCWCycleStep = 3; -int nRETCycleStep = 3; -int nSLIPCycleStep= 3; +int nPCWCycleStep = 3; +int nRETCycleStep = 3; +int nSLIPCycleStep = 3; int nIterFirstStep = 1000; int nIterSecondStep= 2000; int nIterThirdStep = 2000; @@ -1065,17 +1084,17 @@ double secondStepError = 0.001; double thirdStepError = 0.001; double predictCFLError = 0.1; -double refGama = 1.4; -double prl = 0.72; -double prt = 0.90; -double sc_l = 0.5; -double sc_t = 0.5; +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 nGasModel = 0; +int nchem = 0; +int nchemsrc = 1; +int nchemrad = 1; +int ntmodel = 1; int nIdealState = 0; int nEnergyRecycle = 1; @@ -1099,12 +1118,12 @@ double sigmaTemperature = 1.0; double sigmaMassFraction = 1.0; double velocitySlipCorrectConstant = 1.0; -double chemicalRelaxCorf = 1.0; +double chemicalRelaxCorf = 1.0; double chemicalSpectrumRadiusCoef = 1.0; double viscousSpectrumRadiusCoef = 1.5; double inviscidSpectrumRadiusCoef = 1.5; -double spectrumRadiusCoef = 0.5; -double staticPressureRelaxCorf = 0.2; +double spectrumRadiusCoef = 0.5; +double staticPressureRelaxCorf = 0.2; double maxViscous = 10000.0; double trTemperatureMin = 10.0; @@ -1114,31 +1133,35 @@ double densityMin = 1.0e-8; double densityMinFactor = 0.1; double tAdjustmentFactor = 10.0; double iniSpeedCoef = 1.0; +int iniSpeedMode = 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 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 nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; -int nProtectData = 0; -int useHyflowSetting = 0; -int nAblation = 0; -int isInjection = 0; -int nViscosityModel = 0; -int nMarsModel = 0; -string gasfile = "DK5"; -//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; string speciesName = "O, O2, NO, N, N2"; string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; @@ -1152,16 +1175,16 @@ 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 = "Pa"; +//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"; -//string gasfile = "Combustion-12"; +//string gasfile = "Combustion-12"; //string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; //string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; //string gasfile = "Gas-Mixture"; -//string speciesName ="SpeciesA, SpeciesB"; +//string speciesName = "SpeciesA, SpeciesB"; //string initMassFraction = "1.0, 0.0"; int nSutherland = 0; double gamaSpeciesA = 1.4; @@ -1173,9 +1196,17 @@ double molecularWeightSpeciesB = 30.0; //string speciesName = "O2, N2"; //string initMassFraction = "1.0, 0.0"; +int nFraction = 0; int nContinueModel = 0; int nChemicalFlowStep = 0; int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; ######################################################################### // Multi-Grid parameters. @@ -1196,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0; // 1 -- zero order. // 2 -- first-order. (default) // mgCorrectionLimit: Multi-grid correction limit. - int nMGLevel = 1; int MGCoarsestIteration = 1; int MGPreIteration = 1; @@ -1218,20 +1248,20 @@ 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"; +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 # -######################################################################### +#************************************************************************ +# High Order Struct Solver * +#************************************************************************ // isFVMOrFDM: -// 0 -- NSSolverStruct using Finite Volume Method. -// 1 -- NSSolverStruct using Finite Differ Method. +// 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) @@ -1273,30 +1303,48 @@ int allReduceStep = 1; // codeOfOversetGrid: Overlapping(overset) grid or not. // 0 -- NON-overlapping grid. // 1 -- Overlapping grid. -// oversetInterpolationMethod: the method of overset interpolation while field simulation +// oversetInterpolationMethod: the method of overset interpolation while field simulation. // 0 -- set the acceptor cell value by donor cell value. // 1 -- set the acceptor cell value by distance weight of donor cell value. - -int codeOfOversetGrid = 0; -int oversetInterpolationMethod = 0; -int readOversetFileOrNot = 0; -int symetryOrNot = 0; -int readInAuxiliaryInnerGrid = 0; -int readInAuxiliaryOuterGrid = 0; -int readInSklFileOrNot = 0; -string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; -string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; -string auxiliaryInnerGrid2 = ""; -string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; - -int numberOfMovingBodies = 2; +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; // ----------------- ALE configuration ------------------------------ int codeOfAleModel = 0; @@ -1306,36 +1354,42 @@ 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; +int strategyForFaceNormalVelocity = 0; // 0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd. +int strategyForGCLSource = 0; // 0-present; 1-Ahn. -//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. int methodForKineticEquation = 0; double relaxParameterOfKinetic = 1.0; -######################################################################### -# motive information # -######################################################################### +#************************************************************************ +# motive information * +#************************************************************************ int numberOfMovingBodies = 1; ############################## body0 ############################## -//mass of parts -double mass_0 = 1.0; -//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz -double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; -//initial six DOF position information of parts. xc yc zc -double massCenter_0[] = 0.0 , 0.0, 0.0; -//initial six DOF position information of parts. angleX angleY angleZ -double attitudeAngle_0[] = 0.0 , 0.0, 0.0; -//initial six DOF move information of parts. vc vy vz -double massCenterVelocity_0[] = 0.0, 0.0, 0.0; -//initial six DOF move information of parts. omigX omigY omigZ -double angularVelocity_0[] = 0.0, 0.0, 0.0; -//the object that the parts belong to. -int fartherIndex_0 = -1; -//the assembly position of the parts. xc yc zc angleX angleY angleZ -double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0; -//the move pattern of the parts. +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. // -1 given motion partten. // 0 still. // 1 six DOF motion. @@ -1346,51 +1400,68 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 // 14 forced pitch motion. // 15 forced yaw motion. // 16 forced roll motion. -int RBDMethod_0 = 0; -double amplitude_0 = 0.0; -double reduceFrequency_0 = 0.0; -//direction of rotation +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 ; -//additional moment of Force (system axis) mX mY mZ -double addedMoment_0[] = 0.0 ,0.0 ,0.0 ; -//the deformation method of the parts. -int morphing_0 = 0; - -// post indentify -int integralOrder = 4; +int direction_0 = -1; +double rotateFrequency_0 = 0.0; +//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; +// post indentify. +int integralOrder = 4; // ---------------- ATP read -------------------------------------------- -//@int inflowParaType = 0; +//@int inflowParaType = 0; //@double refReNumber = 6.5e6; //@double refDimensionalTemperature = 288.15; //@double freestream_vibration_temperature = 300.00; -//@double refDimensionalPressure = 0; -//@double height = 0; -//@int nsubsonicInlet = 0; -//@int nsubsonicOutlet = 0; -//@string inLetFileName = "./bin/subsonicInlet.hypara"; -//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; //@double refDimensionalVelocity = 0; //@double refDimensionalDensity = 0; - -######################################################################### -# Old Parameter # -######################################################################### +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ int isPlotVolumeField = 0; +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; -######################################################################### -# Incompressible Parameter # -######################################################################### +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ int isSolveEnergyEquation = 0; int isSolveTurbEquation = 0; -int isSolveSpeciesEquation = 0; - +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/G06_ThreeD_Sphere_N2-O2_Premixing-Unstruct_1CPU/bin/grid_para.hypara b/G06_ThreeD_Sphere_N2-O2_Premixing-Unstruct_1CPU/bin/grid_para.hypara index 4bdba51..e70cb41 100644 --- a/G06_ThreeD_Sphere_N2-O2_Premixing-Unstruct_1CPU/bin/grid_para.hypara +++ b/G06_ThreeD_Sphere_N2-O2_Premixing-Unstruct_1CPU/bin/grid_para.hypara @@ -4,9 +4,12 @@ // 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. +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. // from_gtype: Type of grid data type in grid conversion process. // -1 -- MULTI_TYPE. // 1 -- PHengLEI, *.fts. @@ -18,7 +21,9 @@ // 7 -- Hybrid, include both of unstructured and structured grid, *.fts. // 8 -- GMSH, *.msh. int gridtype = 0; -int axisup = 1; +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; int from_gtype = 2; ######################################################################### # File path # diff --git a/G06_ThreeD_Sphere_N2-O2_Premixing-Unstruct_1CPU/三维非结构球头高超声速两气体组分预混算例说明文档.pdf b/G06_ThreeD_Sphere_N2-O2_Premixing-Unstruct_1CPU/三维非结构球头高超声速两气体组分预混算例说明文档.pdf index 90fae97..9391637 100644 Binary files a/G06_ThreeD_Sphere_N2-O2_Premixing-Unstruct_1CPU/三维非结构球头高超声速两气体组分预混算例说明文档.pdf and b/G06_ThreeD_Sphere_N2-O2_Premixing-Unstruct_1CPU/三维非结构球头高超声速两气体组分预混算例说明文档.pdf differ diff --git a/G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/bin/boundary_condition_reference.hypara b/G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/bin/boundary_condition_ref.hypara similarity index 100% rename from G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/bin/boundary_condition_reference.hypara rename to G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/bin/boundary_condition_ref.hypara diff --git a/G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/bin/cfd_para.hypara b/G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/bin/cfd_para.hypara index c344658..f903a5a 100644 --- a/G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/bin/cfd_para.hypara +++ b/G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/bin/cfd_para.hypara @@ -8,23 +8,24 @@ // Platform for Hybrid Engineering Simulation of Flows + // China Aerodynamics Research and Development Center + // (C) Copyright, Since 2010 + +// PHengLEI 2212 + //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ########################################################################### # 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. -// 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. +// 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. +// 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. @@ -46,19 +47,24 @@ 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. -int axisup = 1; +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; // 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; +int omitRepeatInterface = 1; //----------------------------------------------------------------------- # Grid data type # @@ -87,10 +93,9 @@ 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. int numberOfGridFile = 1; -string from_gfile = "./grid/rae2822_hybrid2d.cas"; -string from_gfile1= ""; - -string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; // ----------------- some advanced choices ------------------------------ // iunsteady: The Grid is for unsteady simulation or not. @@ -103,9 +108,9 @@ 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"; +// 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; @@ -119,31 +124,31 @@ string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp"; // 0 -- Not. (default) // 1 -- Yes. // geometryUnit: Geometry unit. -// 1 -- meter. -// 2 -- millimeter. -// 3 -- inch. +// 1 -- meter. +// 2 -- millimeter. +// 3 -- inch. // exclusiveCase: Parallel projection exclusive case. -// 0 -- NON case. -// 1 -- JSM-C2-NPOFF case. -// 2 -- CHNT. +// 0 -- NON case. +// 1 -- JSM-C2-NPOFF case. +// 2 -- CHNT. // projectOrgPoint: If the original wall points need to be projected or not. -int anisoRefine = 0; -int geometryUnit = 1; -int isProject = 0; -int readDist = 0; -int isDeform = 0; +int anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; int exclusiveCase = 0; int projectOrgPoint = 0; string geometryFileName = "./grid/jsm.igs"; // ----------------- Grid Deform Parameters ----------------------------- // deformationMethod: Grid Deform. -// 1 -- SPRING. -// 2 -- RBF. +// 1 -- SPRING. +// 2 -- RBF. // stationalGridFile: Original grid file. // visualFileName : The visualization file path of deform grid. // nDeformStep : The max deform step. -// flapAngle : The max flap angle. +// flapAngle : The max flap angle. // rotatePostionZ : Rotate postion. // rotatePostionY : Rotate postion. // gridSlice : If dump slice grid. @@ -163,10 +168,10 @@ int sliceAxis = 1; double slicePosition = 13; // ----------------- RBF Parameters ------------------------------------- -// numberOfReferenceCP : Number of reference Control Points. -// influencePara : The RBF influence radius parameter. +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. int numberOfReferenceCP = 40; -double influencePara = 25.0; +double influencePara = 25.0; // ----------------- Periodic Parameters -------------------------------- // Notice: Rotational periodicity only support rotation along the X axis! @@ -178,9 +183,8 @@ double influencePara = 25.0; which only support one direction. // rotationAngle: The relative angle between two periodic face. which is recorded in degrees. - int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; +double translationLength[] = [0.0, 0.0, 0.0]; double rotationAngle = 0.0; ######################################################################### @@ -192,7 +196,6 @@ double rotationAngle = 0.0; // 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; @@ -201,20 +204,20 @@ int numberOfMultifile = 1; // 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. +// cellIndexOfMark : the cell index of mark, only for structured grid partition. int traceMark = 0; int blockIndexOfMark = 0; -int cellIndexOfMark[] = [185,30,1]; +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; +// parallelStrategy: +// 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). +// 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"; @@ -232,11 +235,10 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts"; // 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; +double parmetisBalance = 1.05; // numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. // 1 -- single level. @@ -248,29 +250,35 @@ 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. +// 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; +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; int intervalStepSample = 1000; -int intervalStepForce = 100; -int intervalStepRes = 10; -int ifLowSpeedPrecon = 0; +int intervalStepForce = 100; +int intervalStepRes = 10; // compressible: // 0 -- incompressible flow. // 1 -- compressible flow. (default) int compressible = 1; +// 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) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 1; + //----------------------------------------------------------------------- # CFD Control Parameter # //----------------------------------------------------------------------- @@ -281,33 +289,36 @@ int compressible = 1; // 0 -- the nondimensional conditions. // 1 -- the flight conditions. // 2 -- the experiment conditions. -// 3 -- the subsonic boundary conditions. +// 3 -- the subsonic boundary conditions. (Useless!) // 4 -- the condition that the velocity, temperature and density are given. // 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // 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. +// 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 = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. // forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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. -// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol. +// 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; +int directionMethod = 0; double refMachNumber = 0.73; double attackd = 2.79; double angleSlide = 0.00; +int flowInitMethod = 0; int inflowParaType = 0; double refReNumber = 6.5e6; @@ -321,29 +332,27 @@ double freestream_vibration_temperature = 300.00; //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; - -//The velocity, temperature and density are fixed. +// The velocity, temperature and density are fixed. //int inflowParaType = 4; //double refDimensionalVelocity = 1000.0; -//double refDimensionalDensity = 1.0e3; +//double refDimensionalDensity = 1.0e3; -//The velocity, temperature and pressure are fixed. +// The velocity, temperature and pressure are fixed. //int inflowParaType = 5; //double refDimensionalVelocity = 1000.0; //double refDimensionalPressure = 1.0e5; -//The MachNumber, temperature and pressure are fixed. +// The MachNumber, temperature and pressure are fixed. //int inflowParaType = 6; -//double refDimensionalTemperature = 293; +//double refDimensionalTemperature = 293.0; //double refDimensionalPressure = 8886.06; +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; + double wallTemperature = -1.0; double radiationCoef = 0.8; @@ -357,41 +366,41 @@ 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. +double knudsenLength = 1.0; // unit of meter. double refMolecularWeight = 28.9644; // unit of g/mol. //----------------------------------------------------------------------- # Spatial Discretisation # //----------------------------------------------------------------------- -#******************************************************************* -# Struct Solver * -#******************************************************************* +#************************************************************************ +# 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". +// -- "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. +// 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" - +// -- "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"; +string str_limiter_name = "vanalbada"; -#******************************************************************* -# UnStruct Solver or Common * -#******************************************************************* +#************************************************************************ +# UnStruct Solver or Common * +#************************************************************************ // viscousType: Viscous model. -// 0 -- Euler. -// 1 -- Lamilar. -// 2 -- Algebraic. -// 3 -- 1eq turbulent. -// 4 -- 2eq turbulent. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. // viscousName: Laminar or tubulent model. // -- "0eq-bl". // -- "1eq-sa". @@ -410,16 +419,16 @@ string str_limiter_name = "vanalbada"; // 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". +// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // uns_limiter_name: Limiter of Unstruct grid. -// -- "barth", "vencat", "vanleer", "minmod". -// -- "vanalbada", "smooth", "nnd", "lpz", "1st". +// -- "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". // gradientName: Gradient reconstruction method. -// -- "default", "ggcell", "ggnode", "lsq". +// -- "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. @@ -442,18 +451,18 @@ 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 +// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0. -//int viscousType = 0; +//int viscousType = 0; //string viscousName = "Euler"; -//int viscousType = 1; +//int viscousType = 1; //string viscousName = "laminar"; -int viscousType = 3; +int viscousType = 3; string viscousName = "1eq-sa"; -//int viscousType = 4; +//int viscousType = 4; //string viscousName = "2eq-kw-menter-sst"; int DESType = 0; @@ -463,7 +472,7 @@ string uns_limiter_name = "vencat"; string uns_vis_name = "test"; string gradientName = "ggnode"; -int ivencat = 7; +int ivencat = 7; double venkatCoeff = 5.0; int reconmeth = 1; int limitVariables = 0; @@ -475,9 +484,9 @@ double roeEntropyScale = 1.0; double AusmpwPlusLimiter = 1.0; -//----------------------------------------------------------------------- -# Temporal Discretisation # -//----------------------------------------------------------------------- +#************************************************************************ +# Temporal Discretisation * +#************************************************************************ // iunsteady: Steady or unsteady. // 0 -- steady. // 1 -- unsteay. @@ -490,51 +499,57 @@ double AusmpwPlusLimiter = 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 = - ^2 -// 1 -- tau = +// 0 -- tau = - ^2 +// 1 -- tau = // 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 -- Line LU-SGS. -// 8 -- Matrix LU-SGS. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 4 -- LU-SGS. +// 5 -- Block LU-SGS. +// 6 -- Jacobian iteration. +// 7 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. // 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. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. // 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. +// 0 --Local. +// 1 --Global. // isUseLocalCFL: use variable number of CFL or not. -// 0 -- global unified CFL number. -// 1 -- local CFL number. +// 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. -// 0 -- no ALE method. -// 1 -- ALE method for non-moving grids. -// 2 -- ALE method for moving grids. -// 3 -- ALE method for deforming grids. +// 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. +// 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; +int iunsteady = 0; double physicalTimeStep = 0.01; double physicalTimeStepDimensional = -0.001; int ifStartFromSteadyResults = 0; @@ -543,39 +558,42 @@ int ifStaticsReynoldsStress = 0; int startStatisticStep = 800000; double statisticalTimePeriod = -1.0; int statisticMethod = 0; -int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2; +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 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 CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; double pMaxForCFL = 0.2; double pMinForCFL = 0.1; double deltaMaxForCFL = 0.2; double magnifyFactorForCFL = 1.1; double reduceFactorForCFL = 0.5; -double ktmax = 1.0e10; +double ktmax = 1.0e10; -int swapDq = 1; +int swapDq = 1; int nLUSGSSweeps = 1; double LUSGSTolerance = 0.01; -int order = 2; +int order = 2; double visl_min = 0.01; double turbCFLScale = 1.0; -double csrv = 2.0; +double csrv = 1.0; double timemax = 1.0e10; double dtsave = -1.0; int maxale = 10; @@ -591,10 +609,9 @@ double lamda[] = [0.5, 1.0]; //int RKStage = 4; //double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; - -//----------------------------------------------------------------------- -# File In or Out # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. @@ -611,20 +628,18 @@ double lamda[] = [0.5, 1.0]; // 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. +// 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. // 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= ""; +// 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; @@ -632,10 +647,12 @@ int cellMethodOrNodeMethod = 0; string resSaveFile = "results/res.dat"; string turbresfile = "results/turbres.dat"; +string transitionResFile = "results/transitionRes.dat"; string aircoeffile = "results/aircoef.dat"; string restartNSFile = "results/flow.dat"; string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; string visualfile = "results/tecflow.plt"; string wall_aircoefile = "results/wall_aircoef.dat"; @@ -645,10 +662,14 @@ string protectionFile0 = "results/flow0.dat"; string protectionFile1 = "results/flow1.dat"; string wall_heatfluxfile = "results/wall_heatflux.dat"; -int nDumpSurfaceInfo = 0; -string wall_varfile = ""; +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; -string jetDefineFile = "bin/jet.hypara"; +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; string sixDofFileName = "results/sixDofInfo.dat"; string derivativeFileName = "results/identify.dat"; @@ -659,7 +680,8 @@ int plotFieldType = 0; // visualfileType: The file type of visualfile. // 0 -- Tecplot binary. // 1 -- Tecplot ASCII. - +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. int visualfileType = 1; // samplefileMode: The dump mode of sample file. @@ -697,21 +719,21 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), 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) +// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. //-----------the optional parameters list for the wall boundary condition---------------- // nVisualWallVariables: The number of visual variables on wall. // visualWallVariables : dumped variable types, listed as following: -// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4), -// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8), -// -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), -Grid Reynolds number on wall(Re_w, 23) +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- 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), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). int nVisualVariables = 8; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; @@ -739,16 +761,18 @@ 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), mach(6). +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). // 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. +// 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; +int dataMonitorType = 0; string probesDefineFile = "bin/probes_XYZ.dat"; //int dataMonitorType = 1; @@ -761,28 +785,26 @@ string probesDefineFile = "bin/probes_XYZ.dat"; int searchCellsMethod = 0; -int nProbeVariables = 7; -int probeVariables[] = [0, 1, 2, 3, 4, 5, 6]; -int probeVariablesInterpolationMethod = 0; -//----------------------------------------------------------------------- -# Turbulence Parameter # -//----------------------------------------------------------------------- +int nProbeVariables = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +int probeVariablesInterpolationMethod = 0; + +#************************************************************************ +# Turbulence Parameter * +#************************************************************************ // turbInterval: Iteration number of turbulence. // kindOfTurbSource: Kinds of turbulent source. // 0 -- Original. // mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0. -// transitionType: transition model type +// 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 - - +// 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; 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; @@ -790,29 +812,28 @@ int transitionType = 0; double turbIntensity = -1.0; int freeturbIntensitySRModify = 0; double freeDecayXLocation = 0.0; -int compressibleCorrection = 0; -int prandtlNumberCorrection = 0; +int compressibleCorrection = 0; int transitionMaFix = 1; -# maximum eddy viscosity (myt/my) max. +// maximum eddy viscosity (myt/my) max. double eddyViscosityLimit = 1.0e10; int monitor_vistmax = 0; -//----------------------------------------------------------------------- -# LES Parameter # -//----------------------------------------------------------------------- +#************************************************************************ +# LES Parameter * +#************************************************************************ // iLES: Create LESSolver or not. -// = 1 - Create LESSolver; -// != 1 - 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. +// = 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. +// = 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. @@ -820,23 +841,22 @@ int monitor_vistmax = 0; // = "dsmCom"; // = "wale"; // = "sigma". -// 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. +// 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. +// = 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. +// 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; @@ -852,19 +872,16 @@ double testFilterScale = 2.0; int averageWidth = 1; int monitorNegativeConstant = 0; -//----------------------------------------------------------------------- -# Other Parameters for Hypersonic Non-equilibrium Gas # -//----------------------------------------------------------------------- +#************************************************************************ +# 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. -// 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. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. @@ -875,7 +892,7 @@ int monitorNegativeConstant = 0; // 2 -- Argon. // 3 -- Nitrogen. // nEnergyRecycle: The type of EnergyModel Recycle. -// 0 -- not used . +// 0 -- not used. // 1 -- used. // nDensityModify: The type of densitymodify. // 0 -- not used. @@ -883,26 +900,25 @@ int monitorNegativeConstant = 0; // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. -// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. // 0 -- perfect gas. // 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. -// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. -// the value equals to or is greater than 1, and 3 is for default value. -// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. -// the value equals to or is greater than 1, and 3 is for default value. -// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. -// the value equals to or is greater than 1, and 3 is for default value. -// nSlipBCModel : The computational model of slip boundary conditions. - -// 0 -- no slip. -// 1 -- the conventional Maxwell slip conditions. -// 2 -- the Gokcen slip conditions. -// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. -// 4 -- the Kogan simplified slip conditions. -// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. -// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). -// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. -// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). // nchemsrc: // 0 -- the source terms are not computed. // 1 -- the source terms are computed. @@ -913,148 +929,151 @@ int monitorNegativeConstant = 0; // 1 -- One-temperature model. // 2 -- Two-temperature model. // 3 -- Three-temperature model. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. // 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. +// 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 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: -// 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. -// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. -// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. -// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. -// 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. +// 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. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// 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]. // velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. -// 1.0 -- proposed by Maxwell. -// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. -// 1.146 -- proposed for an additional "fictitious" velocity slip. - -// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. -// 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. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// 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. // nSpeciesLimit: limitter of gas species -// 0 -- not used. -// 1 -- used. -// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction -// 0 -- method 0. -// 1 -- method 1. -// 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) - +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// 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 +// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs. +// 0 -- not used. +// 1 -- used. +// nDiagonalModified: Modified on Diagonal. +// 0 -- not used. +// 1 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. // nAblation: -// 0 -- The wall ablation is not computed. -// 1 -- The wall ablation is computed. +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. // isInjection: -// 0 -- The injection velocity of ablation wall is not computed. -// 1 -- The injection velocity of ablation wall is computed. +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. // nViscosityModel: -// 0 -- Blottner fitting method(N89). -// 1 -- Gupta fitting method(N90). +// 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. +// 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. +// 0 -- stands for selecting the Blotter curve fits mode. +// 1 -- stands for Sutherland relation. // 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. -// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. -// "Gas-Mixture" -- indicates the process of mixing gas without reacting. -// for struct solver mixing two speciesSpeciesA, SpeciesB. -// for unstruct solver mixing multi-speciesO2 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. +// "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. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "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. +// 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. +// 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 - +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. int dg_high_order = 0; int iapplication = 0; int isAdaptiveSolver = 0; -int nm = 5; +int nm = 5; int nEquilibriumGas = 0; -int nPCWCycleStep = 3; -int nRETCycleStep = 3; -int nSLIPCycleStep= 3; +int nPCWCycleStep = 3; +int nRETCycleStep = 3; +int nSLIPCycleStep = 3; int nIterFirstStep = 1000; int nIterSecondStep= 2000; int nIterThirdStep = 2000; @@ -1065,17 +1084,17 @@ double secondStepError = 0.001; double thirdStepError = 0.001; double predictCFLError = 0.1; -double refGama = 1.4; -double prl = 0.72; -double prt = 0.90; -double sc_l = 0.5; -double sc_t = 0.5; +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 nGasModel = 0; +int nchem = 0; +int nchemsrc = 1; +int nchemrad = 1; +int ntmodel = 1; int nIdealState = 0; int nEnergyRecycle = 1; @@ -1099,12 +1118,12 @@ double sigmaTemperature = 1.0; double sigmaMassFraction = 1.0; double velocitySlipCorrectConstant = 1.0; -double chemicalRelaxCorf = 1.0; +double chemicalRelaxCorf = 1.0; double chemicalSpectrumRadiusCoef = 1.0; double viscousSpectrumRadiusCoef = 1.5; double inviscidSpectrumRadiusCoef = 1.5; -double spectrumRadiusCoef = 0.5; -double staticPressureRelaxCorf = 0.2; +double spectrumRadiusCoef = 0.5; +double staticPressureRelaxCorf = 0.2; double maxViscous = 10000.0; double trTemperatureMin = 10.0; @@ -1114,31 +1133,35 @@ double densityMin = 1.0e-8; double densityMinFactor = 0.1; double tAdjustmentFactor = 10.0; double iniSpeedCoef = 1.0; +int iniSpeedMode = 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 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 nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; -int nProtectData = 0; -int useHyflowSetting = 0; -int nAblation = 0; -int isInjection = 0; -int nViscosityModel = 0; -int nMarsModel = 0; -string gasfile = "DK5"; -//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; string speciesName = "O, O2, NO, N, N2"; string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; @@ -1152,16 +1175,16 @@ 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 = "Pa"; +//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"; -//string gasfile = "Combustion-12"; +//string gasfile = "Combustion-12"; //string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; //string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; //string gasfile = "Gas-Mixture"; -//string speciesName ="SpeciesA, SpeciesB"; +//string speciesName = "SpeciesA, SpeciesB"; //string initMassFraction = "1.0, 0.0"; int nSutherland = 0; double gamaSpeciesA = 1.4; @@ -1173,9 +1196,17 @@ double molecularWeightSpeciesB = 30.0; //string speciesName = "O2, N2"; //string initMassFraction = "1.0, 0.0"; +int nFraction = 0; int nContinueModel = 0; int nChemicalFlowStep = 0; int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; ######################################################################### // Multi-Grid parameters. @@ -1196,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0; // 1 -- zero order. // 2 -- first-order. (default) // mgCorrectionLimit: Multi-grid correction limit. - int nMGLevel = 1; int MGCoarsestIteration = 1; int MGPreIteration = 1; @@ -1218,20 +1248,20 @@ 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"; +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 # -######################################################################### +#************************************************************************ +# High Order Struct Solver * +#************************************************************************ // isFVMOrFDM: -// 0 -- NSSolverStruct using Finite Volume Method. -// 1 -- NSSolverStruct using Finite Differ Method. +// 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) @@ -1273,30 +1303,48 @@ int allReduceStep = 1; // codeOfOversetGrid: Overlapping(overset) grid or not. // 0 -- NON-overlapping grid. // 1 -- Overlapping grid. -// oversetInterpolationMethod: the method of overset interpolation while field simulation +// oversetInterpolationMethod: the method of overset interpolation while field simulation. // 0 -- set the acceptor cell value by donor cell value. // 1 -- set the acceptor cell value by distance weight of donor cell value. - -int codeOfOversetGrid = 0; -int oversetInterpolationMethod = 0; -int readOversetFileOrNot = 0; -int symetryOrNot = 0; -int readInAuxiliaryInnerGrid = 0; -int readInAuxiliaryOuterGrid = 0; -int readInSklFileOrNot = 0; -string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; -string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; -string auxiliaryInnerGrid2 = ""; -string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; - -int numberOfMovingBodies = 2; +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; // ----------------- ALE configuration ------------------------------ int codeOfAleModel = 0; @@ -1306,36 +1354,42 @@ 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; +int strategyForFaceNormalVelocity = 0; // 0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd. +int strategyForGCLSource = 0; // 0-present; 1-Ahn. -//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. int methodForKineticEquation = 0; double relaxParameterOfKinetic = 1.0; -######################################################################### -# motive information # -######################################################################### +#************************************************************************ +# motive information * +#************************************************************************ int numberOfMovingBodies = 1; ############################## body0 ############################## -//mass of parts -double mass_0 = 1.0; -//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz -double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; -//initial six DOF position information of parts. xc yc zc -double massCenter_0[] = 0.0 , 0.0, 0.0; -//initial six DOF position information of parts. angleX angleY angleZ -double attitudeAngle_0[] = 0.0 , 0.0, 0.0; -//initial six DOF move information of parts. vc vy vz -double massCenterVelocity_0[] = 0.0, 0.0, 0.0; -//initial six DOF move information of parts. omigX omigY omigZ -double angularVelocity_0[] = 0.0, 0.0, 0.0; -//the object that the parts belong to. -int fartherIndex_0 = -1; -//the assembly position of the parts. xc yc zc angleX angleY angleZ -double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0; -//the move pattern of the parts. +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. // -1 given motion partten. // 0 still. // 1 six DOF motion. @@ -1346,51 +1400,68 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 // 14 forced pitch motion. // 15 forced yaw motion. // 16 forced roll motion. -int RBDMethod_0 = 0; -double amplitude_0 = 0.0; -double reduceFrequency_0 = 0.0; -//direction of rotation +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 ; -//additional moment of Force (system axis) mX mY mZ -double addedMoment_0[] = 0.0 ,0.0 ,0.0 ; -//the deformation method of the parts. -int morphing_0 = 0; - -// post indentify -int integralOrder = 4; +int direction_0 = -1; +double rotateFrequency_0 = 0.0; +//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; +// post indentify. +int integralOrder = 4; // ---------------- ATP read -------------------------------------------- -//@int inflowParaType = 0; +//@int inflowParaType = 0; //@double refReNumber = 6.5e6; //@double refDimensionalTemperature = 288.15; //@double freestream_vibration_temperature = 300.00; -//@double refDimensionalPressure = 0; -//@double height = 0; -//@int nsubsonicInlet = 0; -//@int nsubsonicOutlet = 0; -//@string inLetFileName = "./bin/subsonicInlet.hypara"; -//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; //@double refDimensionalVelocity = 0; //@double refDimensionalDensity = 0; - -######################################################################### -# Old Parameter # -######################################################################### +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ int isPlotVolumeField = 0; +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; -######################################################################### -# Incompressible Parameter # -######################################################################### +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ int isSolveEnergyEquation = 0; int isSolveTurbEquation = 0; -int isSolveSpeciesEquation = 0; - +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/bin/cfd_para_subsonic.hypara b/G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/bin/cfd_para_subsonic.hypara index b000b89..1f706fe 100644 --- a/G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/bin/cfd_para_subsonic.hypara +++ b/G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/bin/cfd_para_subsonic.hypara @@ -7,7 +7,7 @@ // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. // intervalStepRes: The step intervals for residual 'res.dat' saved. -int maxSimuStep = 30000; +int maxSimuStep = 10000; int intervalStepFlow = 1000; int intervalStepPlot = 1000; int intervalStepForce = 100; @@ -71,7 +71,7 @@ double freestream_vibration_temperature = 300.0; //The velocity, temperature and pressure are fixed. int inflowParaType = 5; -double refDimensionalVelocity = 9.2; +double refDimensionalVelocity = 340.5; double refDimensionalPressure = 101325.0; double gridScaleFactor = 0.001; @@ -146,7 +146,7 @@ string str_limiter_name = "minmod"; // 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_scheme_name = "roe"; string uns_limiter_name = "vencat"; double venkatCoeff = 0.5; @@ -163,7 +163,7 @@ double venkatCoeff = 0.5; // 1-3 -- is recommended for unstructured solver. int iunsteady = 0; -double CFLEnd = 50.0; +double CFLEnd = 10.0; int nLUSGSSweeps = 1; @@ -190,7 +190,7 @@ 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/multi-species.fts"; +string gridfile = "../grid/multi-species.fts"; int plotFieldType = 0; // ----------------- Advanced Parameters, DO NOT care it ---------------- diff --git a/G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/bin/grid_para.hypara b/G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/bin/grid_para.hypara index d2eb133..1835fd7 100644 --- a/G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/bin/grid_para.hypara +++ b/G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/bin/grid_para.hypara @@ -4,9 +4,12 @@ // 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. +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. // from_gtype: Type of grid data type in grid conversion process. // -1 -- MULTI_TYPE. // 1 -- PHengLEI, *.fts. @@ -18,7 +21,9 @@ // 7 -- Hybrid, include both of unstructured and structured grid, *.fts. // 8 -- GMSH, *.msh. int gridtype = 0; -int axisup = 1; +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; int from_gtype = 2; ######################################################################### diff --git a/G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/二维非结构管道喷流气体混合算例说明文档.pdf b/G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/二维非结构管道喷流气体混合算例说明文档.pdf index f84da93..e98ee26 100644 Binary files a/G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/二维非结构管道喷流气体混合算例说明文档.pdf and b/G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU/二维非结构管道喷流气体混合算例说明文档.pdf differ diff --git a/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/boundary_condition_ref.hypara b/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/boundary_condition_ref.hypara new file mode 100644 index 0000000..a7dbdaf --- /dev/null +++ b/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/boundary_condition_ref.hypara @@ -0,0 +1,35 @@ +int nBoundaryConditions = 4; +string bcName = "farinlet"; +{ + int bcType = 5; + int inflowParaType = 5; + double angleSlide = 0; + double attackd = 0; + int directionMethod = 0; + double initMassFraction[] = [1.0,0.0,0.0,0.0]; + double refDimensionalPressure = 101325; + double refDimensionalTemperature = 308.15; + double refDimensionalVelocity = 2; + string speciesName = "Air,CH4,H2S,CO2"; +} +string bcName = "outlet"; +{ + int bcType = 6; +} +string bcName = "wall"; +{ + int bcType = 2; + int dumpHingeMoment = 0; + int twall_control_select = 0; + double wallTemperature = -1.0; +} +string bcName = "ycinlet"; +{ + int bcType = 52; + int directionMethod = 1; + double direction_inlet[] = [0,1,0]; + double initMassFraction[] = [0.0,0.75,0.16,0.09]; + string speciesName = "Air,CH4,H2S,CO2"; + double totalPressure = 8.3e6; + double totalTemperature = 308.15; +} diff --git a/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/cfd_para.hypara b/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/cfd_para.hypara new file mode 100644 index 0000000..f903a5a --- /dev/null +++ b/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/cfd_para.hypara @@ -0,0 +1,1467 @@ +//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ +// 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 + +// PHengLEI 2212 + +//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ +########################################################################### +# 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. +// 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. +// iadapt: Adaptation number for unstructure grid. +// SymmetryFaceVector: The vector of symmetry face. +// 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; + +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; + +// 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; +int omitRepeatInterface = 1; + +//----------------------------------------------------------------------- +# 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. +// 9 -- Gridgen type of structured grid, *.dat/*.grd. +// 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. +int numberOfGridFile = 1; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +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; + +// 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"; + +// ----------------- Grid Refine Parameters ----------------------------- +// anisoRefine: If refine grid by anisoRefine type. +// 0 -- Not. (default) +// 1 -- Yes. +// 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 anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; +int exclusiveCase = 0; +int projectOrgPoint = 0; +string geometryFileName = "./grid/jsm.igs"; + +// ----------------- Grid Deform Parameters ----------------------------- +// deformationMethod: Grid Deform. +// 1 -- SPRING. +// 2 -- RBF. +// stationalGridFile: Original grid file. +// visualFileName : The visualization file path of deform grid. +// nDeformStep : The max deform step. +// flapAngle : The max flap angle. +// rotatePostionZ : Rotate postion. +// rotatePostionY : Rotate postion. +// gridSlice : If dump slice grid. +// sliceAxis : Grid slice axis. +// slicePosition : Grid slice position. +int nDeformStep = 40; +double flapAngle = 10.0; +double rotatePostionZ = 4.00003; +double rotatePostionY = 3.05; + +int deformationMethod = 2; +string stationalGridFile = "./grid/Segment2Brid.fts"; +string visualFileName = "./results/deformedGrid.dat" + +int gridSlice = 1; +int sliceAxis = 1; +double slicePosition = 13; + +// ----------------- RBF Parameters ------------------------------------- +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. +int numberOfReferenceCP = 40; +double influencePara = 25.0; + +// ----------------- 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. +// translationLength[]: The relative distance between two periodic face + which only support one direction. +// rotationAngle: The relative angle between two periodic face. + which is recorded in degrees. +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. +// 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. +// 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]; + +// parallelStrategy: +// 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. +// parallelPartitionMethod: 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. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; +int intervalStepSample = 1000; +int intervalStepForce = 100; +int intervalStepRes = 10; + +// compressible: +// 0 -- incompressible flow. +// 1 -- compressible flow. (default) +int compressible = 1; + +// 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) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 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. (Useless!) +// 4 -- the condition that the velocity, temperature and density are given. +// 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. +// 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 = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. +// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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. +// 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; +int flowInitMethod = 0; + +int inflowParaType = 0; +double refReNumber = 6.5e6; +double refDimensionalTemperature = 288.15; +double freestream_vibration_temperature = 300.00; + +//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)). + +// 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 = 1000.0; +//double refDimensionalPressure = 1.0e5; + +// The MachNumber, temperature and pressure are fixed. +//int inflowParaType = 6; +//double refDimensionalTemperature = 293.0; +//double refDimensionalPressure = 8886.06; + +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; + +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. +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. +double knudsenLength = 1.0; // unit of meter. +double refMolecularWeight = 28.9644; // unit of g/mol. + +//----------------------------------------------------------------------- +# 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", "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"; + +#************************************************************************ +# 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", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", +// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". +// 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". +// gradientName: 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. +// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0. + +//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; + +double AusmpwPlusLimiter = 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 unsteady simulation. +// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation. +// startStatisticStep: Outer step when start statistics. +// when the value is larger than "maxSimuStep", it is useless. +// 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 = - ^2 +// 1 -- tau = +// 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 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. +// 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. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. +// 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. +// 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. +// 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; +double physicalTimeStepDimensional = -0.001; +int ifStartFromSteadyResults = 0; +int ifStaticsFlowField = 0; +int ifStaticsReynoldsStress = 0; +int startStatisticStep = 800000; +double statisticalTimePeriod = -1.0; +int statisticMethod = 0; +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; +int isUseLocalCFL = 0; +int isUsePreTwall = 0; +double CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; +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; + +int nLUSGSSweeps = 1; +double LUSGSTolerance = 0.01; +int order = 2; + +double visl_min = 0.01; +double turbCFLScale = 1.0; +double csrv = 1.0; +double timemax = 1.0e10; +double dtsave = -1.0; +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. +// 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"; +string transitionResFile = "results/transitionRes.dat"; +string aircoeffile = "results/aircoef.dat"; + +string restartNSFile = "results/flow.dat"; +string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; + +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"; + +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; + +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; + +string sixDofFileName = "results/sixDofInfo.dat"; +string derivativeFileName = "results/identify.dat"; +string hysteresisFileName = "results/force_beta.plt"; + +int plotFieldType = 0; + +// visualfileType: The file type of visualfile. +// 0 -- Tecplot binary. +// 1 -- Tecplot ASCII. +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. +int visualfileType = 1; + +// samplefileMode: The dump mode of sample file. +// 0 -- dump out every probe/line/surface data for all step intervals. +// 1 -- dump out all probe/line/surface data for every step intervals. +int samplefileMode = 0; + +// 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"; +int dumpWallFaceCenter = 0; + +// min-max box of the visual block. +double lowerPlotFieldBox[] = [0.0 0.0 0.0]; +double upperPlotFieldBox[] = [1.0 1.0 1.0]; + +//-----------the optional parameters list for the flow field output---------------- +// 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), streamline_u(45), streamline_v(46), streamline_w(47), +// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). +// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! +// Variables order must from small to big. +//-----------the optional parameters list for the wall boundary condition---------------- +// nVisualWallVariables: The number of visual variables on wall. +// visualWallVariables : dumped variable types, listed as following: +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- 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), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). +int nVisualVariables = 8; +int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; + +int nVisualWallVariables = 9; +int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; + +// 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), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). +// 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 = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +int probeVariablesInterpolationMethod = 0; + +#************************************************************************ +# Turbulence Parameter * +#************************************************************************ +// turbInterval: Iteration number of turbulence. +// kindOfTurbSource: Kinds of turbulent source. +// 0 -- Original. +// 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; +int kindOfTurbSource = 0; +int mod_turb_res = 0; +double freeStreamViscosity = 1.0e-3; +double muoo = 3.0; +double kwoo = 5.0; +int transitionType = 0; +double turbIntensity = -1.0; +int freeturbIntensitySRModify = 0; +double freeDecayXLocation = 0.0; +int compressibleCorrection = 0; +int transitionMaFix = 1; + +// 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"; +// = "dsmCom"; +// = "wale"; +// = "sigma". +// 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 = 0.1; +double isotropicConstant = 0.0; +double waleConstant = 0.6; +double sigmaConstant = 1.35; +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. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic 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. less than and equal to 1 represents the mixture gas. +// Otherwise, the pure gas with one component is used for perfect gas. +// 0 -- Earth gas. +// 1 -- Mars gas. +// 2 -- Argon. +// 3 -- Nitrogen. +// nEnergyRecycle: The type of EnergyModel Recycle. +// 0 -- not used. +// 1 -- used. +// nDensityModify: The type of densitymodify. +// 0 -- not used. +// 1 -- used. +// nchem: +// 0 -- without chemical reaction flow. +// 1 -- the chemical reaction flow is considered. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. +// 0 -- perfect gas. +// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). +// 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. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. +// 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 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: +// 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. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// 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]. +// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// 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. +// nSpeciesLimit: limitter of gas species +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// 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 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. +// nAblation: +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. +// isInjection: +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. +// nViscosityModel: +// 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. +// 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. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "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. +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. +int dg_high_order = 0; +int iapplication = 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; +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 nIdealState = 0; +int nEnergyRecycle = 1; +int nSlipBCModel = 0; +int nDensityModify = 1; +int nTEnergyModel = 0; +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; +double sigmaVelocity = 1.0; +double sigmaTemperature = 1.0; +double sigmaMassFraction = 1.0; +double velocitySlipCorrectConstant = 1.0; + +double chemicalRelaxCorf = 1.0; +double chemicalSpectrumRadiusCoef = 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; +double maxTemperature = 50000.0; +double densityMin = 1.0e-8; +double densityMinFactor = 0.1; +double tAdjustmentFactor = 10.0; +double iniSpeedCoef = 1.0; +int iniSpeedMode = 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 nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; + +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +string speciesName = "O, O2, NO, N, N2"; +string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; + +//string speciesName = "O, O2, NO, N, NO+, N2, e-"; +//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 0.0"; + +//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-"; +//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 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"; + +//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"; + +//string gasfile = "Combustion-12"; +//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; +//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; + +//string gasfile = "Gas-Mixture"; +//string speciesName = "SpeciesA, SpeciesB"; +//string initMassFraction = "1.0, 0.0"; +int nSutherland = 0; +double gamaSpeciesA = 1.4; +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 nFraction = 0; +int nContinueModel = 0; +int nChemicalFlowStep = 0; +int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; + +######################################################################### +// 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 * +#************************************************************************ +// isFVMOrFDM: +// 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 isFVMOrFDM = 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. +// oversetInterpolationMethod: the method of overset interpolation while field simulation. +// 0 -- set the acceptor cell value by donor cell value. +// 1 -- set the acceptor cell value by distance weight of donor cell value. +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.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 outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; + +// ----------------- ALE configuration ------------------------------ +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. + +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. +int methodForKineticEquation = 0; +double relaxParameterOfKinetic = 1.0; + +#************************************************************************ +# motive information * +#************************************************************************ +int numberOfMovingBodies = 1; + +############################## body0 ############################## +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. +// -1 given motion partten. +// 0 still. +// 1 six DOF motion. +// 2 three DOF motion. +// 11 X-axis forced motion. +// 12 Y-axis forced motion. +// 13 Z-axis forced motion. +// 14 forced pitch motion. +// 15 forced yaw motion. +// 16 forced roll motion. +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"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; + +// post indentify. +int integralOrder = 4; + +// ---------------- ATP read -------------------------------------------- +//@int inflowParaType = 0; +//@double refReNumber = 6.5e6; +//@double refDimensionalTemperature = 288.15; +//@double freestream_vibration_temperature = 300.00; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalVelocity = 0; +//@double refDimensionalDensity = 0; +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ +int isPlotVolumeField = 0; + +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; + +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; + +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ +int isSolveEnergyEquation = 0; +int isSolveTurbEquation = 0; +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/cfd_para_transonic.hypara b/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/cfd_para_hypersonic.hypara similarity index 65% rename from F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/cfd_para_transonic.hypara rename to G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/cfd_para_hypersonic.hypara index b269ee0..7c12e7d 100644 --- a/F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU/bin/cfd_para_transonic.hypara +++ b/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/cfd_para_hypersonic.hypara @@ -7,11 +7,12 @@ // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. // intervalStepRes: The step intervals for residual 'res.dat' saved. -int maxSimuStep = 1; +int maxSimuStep = 5000; -int intervalStepFlow = 1; -int intervalStepPlot = 1; -int intervalStepForce = 1; +int intervalStepFlow = 100; +int intervalStepPlot = 10; +int intervalStepSample = 1; +int intervalStepForce = 100; int intervalStepRes = 1; ######################################################################### @@ -20,13 +21,17 @@ int intervalStepRes = 1; // 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: @@ -36,23 +41,21 @@ int intervalStepRes = 1; // 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. +// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit. // TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit. -double refMachNumber = 0.95; -double attackd = 2.79; +double refMachNumber = 0.20; +double attackd = 0.00; double angleSlide = 0.00; -int inflowParaType = 0; -double refReNumber = 6.5e6; -double refDimensionalTemperature = 288.15; +double wallTemperature = -1.0; +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 pressure are fixed. +int inflowParaType = 5; +double refDimensionalVelocity = 2.0; +double refDimensionalPressure = 101325; +double refDimensionalTemperature = 308.15; double gridScaleFactor = 1.0; @@ -62,11 +65,12 @@ 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. +double knudsenLength = 1.0; // unit of meter. ######################################################################### # Physical models # ######################################################################### -// viscousType : Viscous model. +// viscousType: Viscous model. // 0 -- Euler. // 1 -- Lamilar. // 3 -- 1eq turbulent. @@ -80,16 +84,16 @@ double TorqueRefZ = 0.0; // unit of meter. // 2 -- DDES. // 3 -- IDDES. -//int viscousType = 0; +//int viscousType = 0; //string viscousName = "Euler"; -//int viscousType = 1; -//string viscousName = "laminar"; +int viscousType = 1; +string viscousName = "laminar"; -int viscousType = 3; -string viscousName = "1eq-sa"; +//int viscousType = 3; +//string viscousName = "1eq-sa"; -//int viscousType = 4; +//int viscousType = 4; //string viscousName = "2eq-kw-menter-sst"; int DESType = 0; @@ -104,13 +108,12 @@ double roeEntropyScale = 1.0; #******************************************************************* // inviscidSchemeName: Spatial discretisation scheme of struct grid. // Using this when solve structered grid or hybrid. -// -- "roe", "vanleer", "ausm+up", "ausmpw". +// -- "vanleer", "steger", "ausmpw", "ausmpw+". // str_limiter_name: Limiter of struct grid. -// -- "3rdsmooth", "smooth". -// -- "nolim", no limiter. +// -- "minmod", "3rd_minmod_smooth", "vanalbada". -string inviscidSchemeName = "roe"; -string str_limiter_name = "smooth"; +string inviscidSchemeName = "steger"; +string str_limiter_name = "minmod"; #******************************************************************* # UnStruct Solver * @@ -126,9 +129,9 @@ string str_limiter_name = "smooth"; // 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; +string uns_scheme_name = "vanleer"; +string uns_limiter_name = "1st"; +double venkatCoeff = 0.5; ######################################################################### # Temporal Discretisation # @@ -138,28 +141,14 @@ double venkatCoeff = 5.0; // 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; +int iunsteady = 1; +double physicalTimeStep = 0.2; +int min_sub_iter = 50; +int max_sub_iter = 50; +double tol_sub_iter = 0.001; -double CFLEnd = 10.0; - -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; +double CFLEnd = 50.0; ######################################################################### # File In or Out # @@ -171,8 +160,8 @@ 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/updatedgrid.fts"; -int plotFieldType = 1; +string gridfile = "./grid/yanchongCase14__4.fts"; +int plotFieldType = 0; // ----------------- Advanced Parameters, DO NOT care it ---------------- // nVisualVariables: Number of variables want to be dumped for tecplot visualization. @@ -181,12 +170,30 @@ int plotFieldType = 1; // -- 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). +// -- 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). +// -- Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62) // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. -int nVisualVariables = 1; -int visualVariables[] = [81]; +int nVisualVariables = 13; +int visualVariables[] = [0,1,2,3,4,5,6,38,39,40,53,54,55]; + +int ifSetDataMonitor = 1; + +//-----------the optional parameters list for the wall boundary condition---------------- +// nVisualWallVariables: The number of visual variables on wall. +// visualWallVariables : dumped variable types, listed as following: +// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4), +// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8), +// -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), -Grid Reynolds number on wall(Re_w, 23) , -Knudsen number(Kn_wall, 24) + +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. @@ -201,3 +208,18 @@ int visualVariables[] = [81]; int reconmeth = 1; int limitVariables = 0; int limitVector = 0; + + +int nchem = 1; +int nchemsrc = 0; +int nchemrad = 0; +int ntmodel = 1; +int nIdealState = 1; + +string gasfile = "Gas-Mixture"; +string speciesName = "Air,CH4,H2S,CO2"; +string initMassFraction = "1.0,0.0,0.0,0.0"; +int nFraction = 1; +int nLeakageMonitor = 1; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; diff --git a/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/grid_para.hypara b/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/grid_para.hypara new file mode 100644 index 0000000..05ea4ff --- /dev/null +++ b/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/grid_para.hypara @@ -0,0 +1,36 @@ +######################################################################### +# Grid data type # +######################################################################### +// gridtype: Grid type for generation, conversion, reconstruction, merging. +// 0 -- Unstructured grid. +// 1 -- Structured grid. +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +// 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. +// 9 -- Gridgen type of structured grid, *.dat/*.grd. +int gridtype = 0; +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; +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/yanchongCase14.cas"; +string out_gfile = "./grid/yanchongCase14.fts"; diff --git a/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/key.hypara b/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/key.hypara new file mode 100644 index 0000000..1acf624 --- /dev/null +++ b/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/key.hypara @@ -0,0 +1,58 @@ +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 = 5; +//string parafilename = "./bin/overset_grid_view.hypara"; + +//int nsimutask = 13; +//string parafilename = "./bin/lbm_para.hypara"; + +//int nsimutask = 14; +//string parafilename = "./bin/integrative_solver.hypara"; + +//int nsimutask = 99; +//string parafilename = "./bin/post_processing.hypara"; + +// ---------------- Advanced Parameters, DO NOT care it ---------------- +int numberOfGridProcessor = 0; +// ATP read +//@string parafilename1 = "" +//@string parafilename2 = ""; diff --git a/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/partition.hypara b/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/partition.hypara new file mode 100644 index 0000000..85a3249 --- /dev/null +++ b/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/partition.hypara @@ -0,0 +1,24 @@ +// 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). +// numberOfMultifile: The number of partition grid files that want to be dumped out. + +int pgridtype = 0; +int maxproc = 4; + +string original_grid_file = "./grid/yanchongCase14.fts"; +string partition_grid_file = "./grid/yanchongCase14__4.fts"; + +int numberOfMultifile = 1; + +// 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/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/probes_XYZ.dat b/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/probes_XYZ.dat new file mode 100644 index 0000000..e713b1d --- /dev/null +++ b/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/bin/probes_XYZ.dat @@ -0,0 +1,5 @@ +4 +28.678 55.643 0 +80.785 116.821 0 +125.335 158.357 0 +162.272 308.038 0 diff --git a/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/grid/网格地址.txt b/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/grid/网格地址.txt new file mode 100644 index 0000000..899f977 --- /dev/null +++ b/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/grid/网格地址.txt @@ -0,0 +1,5 @@ +红山开源风雷算例库原始网格获取百度网盘链接： +链接：http://pan.baidu.com/s/1aZ9cdkp6CkT9il4fEpnTcA +提取码：w47m + +注：plot3D格式网格需同时下载.grd和.inp文件 \ No newline at end of file diff --git a/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/二维储罐泄露多组分气体非定常算例说明文档.pdf b/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/二维储罐泄露多组分气体非定常算例说明文档.pdf new file mode 100644 index 0000000..f46e804 Binary files /dev/null and b/G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU/二维储罐泄露多组分气体非定常算例说明文档.pdf differ