diff --git a/A14_TwoD_Plate_TotalPressTempBC_SA_Struct_4CPU/bin/boundary_condition _ref.hypara b/A14_TwoD_Plate_TotalPressTempBC_SA_Struct_4CPU/bin/boundary_condition_ref.hypara similarity index 100% rename from A14_TwoD_Plate_TotalPressTempBC_SA_Struct_4CPU/bin/boundary_condition _ref.hypara rename to A14_TwoD_Plate_TotalPressTempBC_SA_Struct_4CPU/bin/boundary_condition_ref.hypara diff --git a/B18-ThreeD_CRM-HL_Level-B_SA_Unstruct_1024CPU/bin/cfd_para_subsonic.hypara b/B18-ThreeD_CRM-HL_Level-B_SA_Unstruct_1024CPU/bin/cfd_para_subsonic.hypara index c7f0211..8a47f58 100644 --- a/B18-ThreeD_CRM-HL_Level-B_SA_Unstruct_1024CPU/bin/cfd_para_subsonic.hypara +++ b/B18-ThreeD_CRM-HL_Level-B_SA_Unstruct_1024CPU/bin/cfd_para_subsonic.hypara @@ -162,7 +162,7 @@ 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/CRM-HL_40-37__Level-B__1024.fts"; +string gridfile = "./grid/CRM-HL_40-37_Nominal_Unstr_LevelB_Q1__1024.fts"; int plotFieldType = 0; // ----------------- Advanced Parameters, DO NOT care it ---------------- diff --git a/H01_TwoD_BackStep_KE_QUICK_4CPU/grid/网格地址.txt b/B18-ThreeD_CRM-HL_Level-B_SA_Unstruct_1024CPU/grid/网格地址.txt similarity index 100% rename from H01_TwoD_BackStep_KE_QUICK_4CPU/grid/网格地址.txt rename to B18-ThreeD_CRM-HL_Level-B_SA_Unstruct_1024CPU/grid/网格地址.txt diff --git a/E01_ThreeD_Cylinder_LES_Re3900_Struct_120CPU/bin/cfd_para.hypara b/E01_ThreeD_Cylinder_LES_Re3900_Struct_120CPU/bin/cfd_para.hypara index c344658..f903a5a 100644 --- a/E01_ThreeD_Cylinder_LES_Re3900_Struct_120CPU/bin/cfd_para.hypara +++ b/E01_ThreeD_Cylinder_LES_Re3900_Struct_120CPU/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/F05_ThreeD_AEDC_OversetConfig_Unstruct_8CPU/bin/cfd_para.hypara b/F05_ThreeD_AEDC_OversetConfig_Unstruct_8CPU/bin/cfd_para.hypara index c344658..f903a5a 100644 --- a/F05_ThreeD_AEDC_OversetConfig_Unstruct_8CPU/bin/cfd_para.hypara +++ b/F05_ThreeD_AEDC_OversetConfig_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/F07-TwoD_NACA0012_PitchingMovement_SA_Struct_4CPU/bin/cfd_para.hypara b/F07-TwoD_NACA0012_PitchingMovement_SA_Struct_4CPU/bin/cfd_para.hypara index c344658..f903a5a 100644 --- a/F07-TwoD_NACA0012_PitchingMovement_SA_Struct_4CPU/bin/cfd_para.hypara +++ b/F07-TwoD_NACA0012_PitchingMovement_SA_Struct_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/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 1f706fe..e23deef 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 @@ -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/H01_TwoD_BackStep_KE_QUICK_4CPU/bin/boundary_condition_ref.hypara b/H01_TwoD_BackStep_KE_UPWIND_4CPU/bin/boundary_condition_ref.hypara similarity index 100% rename from H01_TwoD_BackStep_KE_QUICK_4CPU/bin/boundary_condition_ref.hypara rename to H01_TwoD_BackStep_KE_UPWIND_4CPU/bin/boundary_condition_ref.hypara diff --git a/H01_TwoD_BackStep_KE_QUICK_4CPU/bin/cfd_para.hypara b/H01_TwoD_BackStep_KE_UPWIND_4CPU/bin/cfd_para.hypara similarity index 100% rename from H01_TwoD_BackStep_KE_QUICK_4CPU/bin/cfd_para.hypara rename to H01_TwoD_BackStep_KE_UPWIND_4CPU/bin/cfd_para.hypara diff --git a/H01_TwoD_BackStep_KE_QUICK_4CPU/bin/cfd_para_incompressible.hypara b/H01_TwoD_BackStep_KE_UPWIND_4CPU/bin/cfd_para_incompressible.hypara similarity index 100% rename from H01_TwoD_BackStep_KE_QUICK_4CPU/bin/cfd_para_incompressible.hypara rename to H01_TwoD_BackStep_KE_UPWIND_4CPU/bin/cfd_para_incompressible.hypara diff --git a/H01_TwoD_BackStep_KE_QUICK_4CPU/bin/grid_para.hypara b/H01_TwoD_BackStep_KE_UPWIND_4CPU/bin/grid_para.hypara similarity index 100% rename from H01_TwoD_BackStep_KE_QUICK_4CPU/bin/grid_para.hypara rename to H01_TwoD_BackStep_KE_UPWIND_4CPU/bin/grid_para.hypara diff --git a/H01_TwoD_BackStep_KE_QUICK_4CPU/bin/key.hypara b/H01_TwoD_BackStep_KE_UPWIND_4CPU/bin/key.hypara similarity index 100% rename from H01_TwoD_BackStep_KE_QUICK_4CPU/bin/key.hypara rename to H01_TwoD_BackStep_KE_UPWIND_4CPU/bin/key.hypara diff --git a/H01_TwoD_BackStep_KE_QUICK_4CPU/bin/partition.hypara b/H01_TwoD_BackStep_KE_UPWIND_4CPU/bin/partition.hypara similarity index 100% rename from H01_TwoD_BackStep_KE_QUICK_4CPU/bin/partition.hypara rename to H01_TwoD_BackStep_KE_UPWIND_4CPU/bin/partition.hypara diff --git a/H02_TwoD_Cavitity_Re100_SUDS_4CPU/grid/网格地址.txt b/H01_TwoD_BackStep_KE_UPWIND_4CPU/grid/网格地址.txt similarity index 100% rename from H02_TwoD_Cavitity_Re100_SUDS_4CPU/grid/网格地址.txt rename to H01_TwoD_BackStep_KE_UPWIND_4CPU/grid/网格地址.txt diff --git a/H02_TwoD_Cavitity_Re100_SUDS_4CPU/bin/boundary_condition_ref.hypara b/H02_TwoD_Cavitity_Re100_UPWIND_4CPU/bin/boundary_condition_ref.hypara similarity index 100% rename from H02_TwoD_Cavitity_Re100_SUDS_4CPU/bin/boundary_condition_ref.hypara rename to H02_TwoD_Cavitity_Re100_UPWIND_4CPU/bin/boundary_condition_ref.hypara diff --git a/H02_TwoD_Cavitity_Re100_SUDS_4CPU/bin/cfd_para.hypara b/H02_TwoD_Cavitity_Re100_UPWIND_4CPU/bin/cfd_para.hypara similarity index 100% rename from H02_TwoD_Cavitity_Re100_SUDS_4CPU/bin/cfd_para.hypara rename to H02_TwoD_Cavitity_Re100_UPWIND_4CPU/bin/cfd_para.hypara diff --git a/H02_TwoD_Cavitity_Re100_SUDS_4CPU/bin/cfd_para_incompressible.hypara b/H02_TwoD_Cavitity_Re100_UPWIND_4CPU/bin/cfd_para_incompressible.hypara similarity index 100% rename from H02_TwoD_Cavitity_Re100_SUDS_4CPU/bin/cfd_para_incompressible.hypara rename to H02_TwoD_Cavitity_Re100_UPWIND_4CPU/bin/cfd_para_incompressible.hypara diff --git a/H02_TwoD_Cavitity_Re100_SUDS_4CPU/bin/grid_para.hypara b/H02_TwoD_Cavitity_Re100_UPWIND_4CPU/bin/grid_para.hypara similarity index 100% rename from H02_TwoD_Cavitity_Re100_SUDS_4CPU/bin/grid_para.hypara rename to H02_TwoD_Cavitity_Re100_UPWIND_4CPU/bin/grid_para.hypara diff --git a/H02_TwoD_Cavitity_Re100_SUDS_4CPU/bin/key.hypara b/H02_TwoD_Cavitity_Re100_UPWIND_4CPU/bin/key.hypara similarity index 100% rename from H02_TwoD_Cavitity_Re100_SUDS_4CPU/bin/key.hypara rename to H02_TwoD_Cavitity_Re100_UPWIND_4CPU/bin/key.hypara diff --git a/H02_TwoD_Cavitity_Re100_SUDS_4CPU/bin/partition.hypara b/H02_TwoD_Cavitity_Re100_UPWIND_4CPU/bin/partition.hypara similarity index 100% rename from H02_TwoD_Cavitity_Re100_SUDS_4CPU/bin/partition.hypara rename to H02_TwoD_Cavitity_Re100_UPWIND_4CPU/bin/partition.hypara diff --git a/H03_TwoD_GasLeakage_Steady_QUICK_4CPU/grid/网格地址.txt b/H02_TwoD_Cavitity_Re100_UPWIND_4CPU/grid/网格地址.txt similarity index 100% rename from H03_TwoD_GasLeakage_Steady_QUICK_4CPU/grid/网格地址.txt rename to H02_TwoD_Cavitity_Re100_UPWIND_4CPU/grid/网格地址.txt diff --git a/H03_TwoD_GasLeakage_Steady_QUICK_4CPU/bin/boundary_condition_ref.hypara b/H03_TwoD_GasLeakage_Steady_UPWIND_4CPU/bin/boundary_condition_ref.hypara similarity index 100% rename from H03_TwoD_GasLeakage_Steady_QUICK_4CPU/bin/boundary_condition_ref.hypara rename to H03_TwoD_GasLeakage_Steady_UPWIND_4CPU/bin/boundary_condition_ref.hypara diff --git a/H03_TwoD_GasLeakage_Steady_QUICK_4CPU/bin/cfd_para.hypara b/H03_TwoD_GasLeakage_Steady_UPWIND_4CPU/bin/cfd_para.hypara similarity index 100% rename from H03_TwoD_GasLeakage_Steady_QUICK_4CPU/bin/cfd_para.hypara rename to H03_TwoD_GasLeakage_Steady_UPWIND_4CPU/bin/cfd_para.hypara diff --git a/H03_TwoD_GasLeakage_Steady_QUICK_4CPU/bin/cfd_para_incompressible.hypara b/H03_TwoD_GasLeakage_Steady_UPWIND_4CPU/bin/cfd_para_incompressible.hypara similarity index 100% rename from H03_TwoD_GasLeakage_Steady_QUICK_4CPU/bin/cfd_para_incompressible.hypara rename to H03_TwoD_GasLeakage_Steady_UPWIND_4CPU/bin/cfd_para_incompressible.hypara diff --git a/H03_TwoD_GasLeakage_Steady_QUICK_4CPU/bin/grid_para.hypara b/H03_TwoD_GasLeakage_Steady_UPWIND_4CPU/bin/grid_para.hypara similarity index 100% rename from H03_TwoD_GasLeakage_Steady_QUICK_4CPU/bin/grid_para.hypara rename to H03_TwoD_GasLeakage_Steady_UPWIND_4CPU/bin/grid_para.hypara diff --git a/H03_TwoD_GasLeakage_Steady_QUICK_4CPU/bin/key.hypara b/H03_TwoD_GasLeakage_Steady_UPWIND_4CPU/bin/key.hypara similarity index 100% rename from H03_TwoD_GasLeakage_Steady_QUICK_4CPU/bin/key.hypara rename to H03_TwoD_GasLeakage_Steady_UPWIND_4CPU/bin/key.hypara diff --git a/H03_TwoD_GasLeakage_Steady_QUICK_4CPU/bin/partition.hypara b/H03_TwoD_GasLeakage_Steady_UPWIND_4CPU/bin/partition.hypara similarity index 100% rename from H03_TwoD_GasLeakage_Steady_QUICK_4CPU/bin/partition.hypara rename to H03_TwoD_GasLeakage_Steady_UPWIND_4CPU/bin/partition.hypara diff --git a/H04_TwoD_NACA0012_PISO_SA_4CPU/grid/网格地址.txt b/H03_TwoD_GasLeakage_Steady_UPWIND_4CPU/grid/网格地址.txt similarity index 100% rename from H04_TwoD_NACA0012_PISO_SA_4CPU/grid/网格地址.txt rename to H03_TwoD_GasLeakage_Steady_UPWIND_4CPU/grid/网格地址.txt diff --git a/H04_TwoD_NACA0012_PISO_SA_4CPU/bin/boundary_condition_ref.hypara b/H04_TwoD_NACA0012_UPWIND_SA_4CPU/bin/boundary_condition_ref.hypara similarity index 100% rename from H04_TwoD_NACA0012_PISO_SA_4CPU/bin/boundary_condition_ref.hypara rename to H04_TwoD_NACA0012_UPWIND_SA_4CPU/bin/boundary_condition_ref.hypara diff --git a/H04_TwoD_NACA0012_PISO_SA_4CPU/bin/cfd_para.hypara b/H04_TwoD_NACA0012_UPWIND_SA_4CPU/bin/cfd_para.hypara similarity index 100% rename from H04_TwoD_NACA0012_PISO_SA_4CPU/bin/cfd_para.hypara rename to H04_TwoD_NACA0012_UPWIND_SA_4CPU/bin/cfd_para.hypara diff --git a/H04_TwoD_NACA0012_PISO_SA_4CPU/bin/cfd_para_incompressible.hypara b/H04_TwoD_NACA0012_UPWIND_SA_4CPU/bin/cfd_para_incompressible.hypara similarity index 100% rename from H04_TwoD_NACA0012_PISO_SA_4CPU/bin/cfd_para_incompressible.hypara rename to H04_TwoD_NACA0012_UPWIND_SA_4CPU/bin/cfd_para_incompressible.hypara diff --git a/H04_TwoD_NACA0012_PISO_SA_4CPU/bin/grid_para.hypara b/H04_TwoD_NACA0012_UPWIND_SA_4CPU/bin/grid_para.hypara similarity index 100% rename from H04_TwoD_NACA0012_PISO_SA_4CPU/bin/grid_para.hypara rename to H04_TwoD_NACA0012_UPWIND_SA_4CPU/bin/grid_para.hypara diff --git a/H04_TwoD_NACA0012_PISO_SA_4CPU/bin/key.hypara b/H04_TwoD_NACA0012_UPWIND_SA_4CPU/bin/key.hypara similarity index 100% rename from H04_TwoD_NACA0012_PISO_SA_4CPU/bin/key.hypara rename to H04_TwoD_NACA0012_UPWIND_SA_4CPU/bin/key.hypara diff --git a/H04_TwoD_NACA0012_PISO_SA_4CPU/bin/partition.hypara b/H04_TwoD_NACA0012_UPWIND_SA_4CPU/bin/partition.hypara similarity index 100% rename from H04_TwoD_NACA0012_PISO_SA_4CPU/bin/partition.hypara rename to H04_TwoD_NACA0012_UPWIND_SA_4CPU/bin/partition.hypara diff --git a/H07_TwoD_Plate_Turb_QUICK_4CPU/grid/网格地址.txt b/H04_TwoD_NACA0012_UPWIND_SA_4CPU/grid/网格地址.txt similarity index 100% rename from H07_TwoD_Plate_Turb_QUICK_4CPU/grid/网格地址.txt rename to H04_TwoD_NACA0012_UPWIND_SA_4CPU/grid/网格地址.txt diff --git a/H07_TwoD_Plate_Turb_QUICK_4CPU/bin/boundary_condition_ref.hypara b/H07_TwoD_Plate_Turb_UPWIND_4CPU/bin/boundary_condition_ref.hypara similarity index 100% rename from H07_TwoD_Plate_Turb_QUICK_4CPU/bin/boundary_condition_ref.hypara rename to H07_TwoD_Plate_Turb_UPWIND_4CPU/bin/boundary_condition_ref.hypara diff --git a/H07_TwoD_Plate_Turb_QUICK_4CPU/bin/cfd_para.hypara b/H07_TwoD_Plate_Turb_UPWIND_4CPU/bin/cfd_para.hypara similarity index 100% rename from H07_TwoD_Plate_Turb_QUICK_4CPU/bin/cfd_para.hypara rename to H07_TwoD_Plate_Turb_UPWIND_4CPU/bin/cfd_para.hypara diff --git a/H07_TwoD_Plate_Turb_QUICK_4CPU/bin/cfd_para_incompressible.hypara b/H07_TwoD_Plate_Turb_UPWIND_4CPU/bin/cfd_para_incompressible.hypara similarity index 100% rename from H07_TwoD_Plate_Turb_QUICK_4CPU/bin/cfd_para_incompressible.hypara rename to H07_TwoD_Plate_Turb_UPWIND_4CPU/bin/cfd_para_incompressible.hypara diff --git a/H07_TwoD_Plate_Turb_QUICK_4CPU/bin/grid_para.hypara b/H07_TwoD_Plate_Turb_UPWIND_4CPU/bin/grid_para.hypara similarity index 100% rename from H07_TwoD_Plate_Turb_QUICK_4CPU/bin/grid_para.hypara rename to H07_TwoD_Plate_Turb_UPWIND_4CPU/bin/grid_para.hypara diff --git a/H07_TwoD_Plate_Turb_QUICK_4CPU/bin/key.hypara b/H07_TwoD_Plate_Turb_UPWIND_4CPU/bin/key.hypara similarity index 100% rename from H07_TwoD_Plate_Turb_QUICK_4CPU/bin/key.hypara rename to H07_TwoD_Plate_Turb_UPWIND_4CPU/bin/key.hypara diff --git a/H07_TwoD_Plate_Turb_QUICK_4CPU/bin/partition.hypara b/H07_TwoD_Plate_Turb_UPWIND_4CPU/bin/partition.hypara similarity index 100% rename from H07_TwoD_Plate_Turb_QUICK_4CPU/bin/partition.hypara rename to H07_TwoD_Plate_Turb_UPWIND_4CPU/bin/partition.hypara diff --git a/H08_TwoD_Species_Turb_QUICK_4CPU/grid/网格地址.txt b/H07_TwoD_Plate_Turb_UPWIND_4CPU/grid/网格地址.txt similarity index 100% rename from H08_TwoD_Species_Turb_QUICK_4CPU/grid/网格地址.txt rename to H07_TwoD_Plate_Turb_UPWIND_4CPU/grid/网格地址.txt diff --git a/H08_TwoD_Species_Turb_QUICK_4CPU/bin/boundary_condition_ref.hypara b/H08_TwoD_Species_Turb_UPWIND_4CPU/bin/boundary_condition_ref.hypara similarity index 100% rename from H08_TwoD_Species_Turb_QUICK_4CPU/bin/boundary_condition_ref.hypara rename to H08_TwoD_Species_Turb_UPWIND_4CPU/bin/boundary_condition_ref.hypara diff --git a/H08_TwoD_Species_Turb_QUICK_4CPU/bin/cfd_para.hypara b/H08_TwoD_Species_Turb_UPWIND_4CPU/bin/cfd_para.hypara similarity index 100% rename from H08_TwoD_Species_Turb_QUICK_4CPU/bin/cfd_para.hypara rename to H08_TwoD_Species_Turb_UPWIND_4CPU/bin/cfd_para.hypara diff --git a/H08_TwoD_Species_Turb_QUICK_4CPU/bin/cfd_para_incompressible.hypara b/H08_TwoD_Species_Turb_UPWIND_4CPU/bin/cfd_para_incompressible.hypara similarity index 100% rename from H08_TwoD_Species_Turb_QUICK_4CPU/bin/cfd_para_incompressible.hypara rename to H08_TwoD_Species_Turb_UPWIND_4CPU/bin/cfd_para_incompressible.hypara diff --git a/H08_TwoD_Species_Turb_QUICK_4CPU/bin/grid_para.hypara b/H08_TwoD_Species_Turb_UPWIND_4CPU/bin/grid_para.hypara similarity index 100% rename from H08_TwoD_Species_Turb_QUICK_4CPU/bin/grid_para.hypara rename to H08_TwoD_Species_Turb_UPWIND_4CPU/bin/grid_para.hypara diff --git a/H08_TwoD_Species_Turb_QUICK_4CPU/bin/key.hypara b/H08_TwoD_Species_Turb_UPWIND_4CPU/bin/key.hypara similarity index 100% rename from H08_TwoD_Species_Turb_QUICK_4CPU/bin/key.hypara rename to H08_TwoD_Species_Turb_UPWIND_4CPU/bin/key.hypara diff --git a/H08_TwoD_Species_Turb_QUICK_4CPU/bin/partition.hypara b/H08_TwoD_Species_Turb_UPWIND_4CPU/bin/partition.hypara similarity index 100% rename from H08_TwoD_Species_Turb_QUICK_4CPU/bin/partition.hypara rename to H08_TwoD_Species_Turb_UPWIND_4CPU/bin/partition.hypara diff --git a/H09_ThreeD_Car_Turb_QUICK_4CPU/grid/网格地址.txt b/H08_TwoD_Species_Turb_UPWIND_4CPU/grid/网格地址.txt similarity index 100% rename from H09_ThreeD_Car_Turb_QUICK_4CPU/grid/网格地址.txt rename to H08_TwoD_Species_Turb_UPWIND_4CPU/grid/网格地址.txt diff --git a/H09_ThreeD_Car_Turb_QUICK_4CPU/bin/boundary_condition_ref.hypara b/H09_ThreeD_Car_Turb_UPWIND_4CPU/bin/boundary_condition_ref.hypara similarity index 100% rename from H09_ThreeD_Car_Turb_QUICK_4CPU/bin/boundary_condition_ref.hypara rename to H09_ThreeD_Car_Turb_UPWIND_4CPU/bin/boundary_condition_ref.hypara diff --git a/H09_ThreeD_Car_Turb_QUICK_4CPU/bin/cfd_para.hypara b/H09_ThreeD_Car_Turb_UPWIND_4CPU/bin/cfd_para.hypara similarity index 100% rename from H09_ThreeD_Car_Turb_QUICK_4CPU/bin/cfd_para.hypara rename to H09_ThreeD_Car_Turb_UPWIND_4CPU/bin/cfd_para.hypara diff --git a/H09_ThreeD_Car_Turb_QUICK_4CPU/bin/cfd_para_incompressible.hypara b/H09_ThreeD_Car_Turb_UPWIND_4CPU/bin/cfd_para_incompressible.hypara similarity index 100% rename from H09_ThreeD_Car_Turb_QUICK_4CPU/bin/cfd_para_incompressible.hypara rename to H09_ThreeD_Car_Turb_UPWIND_4CPU/bin/cfd_para_incompressible.hypara diff --git a/H09_ThreeD_Car_Turb_QUICK_4CPU/bin/grid_para.hypara b/H09_ThreeD_Car_Turb_UPWIND_4CPU/bin/grid_para.hypara similarity index 100% rename from H09_ThreeD_Car_Turb_QUICK_4CPU/bin/grid_para.hypara rename to H09_ThreeD_Car_Turb_UPWIND_4CPU/bin/grid_para.hypara diff --git a/H09_ThreeD_Car_Turb_QUICK_4CPU/bin/key.hypara b/H09_ThreeD_Car_Turb_UPWIND_4CPU/bin/key.hypara similarity index 100% rename from H09_ThreeD_Car_Turb_QUICK_4CPU/bin/key.hypara rename to H09_ThreeD_Car_Turb_UPWIND_4CPU/bin/key.hypara diff --git a/H09_ThreeD_Car_Turb_QUICK_4CPU/bin/partition.hypara b/H09_ThreeD_Car_Turb_UPWIND_4CPU/bin/partition.hypara similarity index 100% rename from H09_ThreeD_Car_Turb_QUICK_4CPU/bin/partition.hypara rename to H09_ThreeD_Car_Turb_UPWIND_4CPU/bin/partition.hypara diff --git a/H11_ThreeD_GasLeakage_Unsteady_SUDS_4CPU/grid/网格地址.txt b/H09_ThreeD_Car_Turb_UPWIND_4CPU/grid/网格地址.txt similarity index 100% rename from H11_ThreeD_GasLeakage_Unsteady_SUDS_4CPU/grid/网格地址.txt rename to H09_ThreeD_Car_Turb_UPWIND_4CPU/grid/网格地址.txt diff --git a/H11_ThreeD_GasLeakage_Unsteady_SUDS_4CPU/bin/boundary_condition_ref.hypara b/H11_ThreeD_GasLeakage_Unsteady_UPWIND_4CPU/bin/boundary_condition_ref.hypara similarity index 100% rename from H11_ThreeD_GasLeakage_Unsteady_SUDS_4CPU/bin/boundary_condition_ref.hypara rename to H11_ThreeD_GasLeakage_Unsteady_UPWIND_4CPU/bin/boundary_condition_ref.hypara diff --git a/H11_ThreeD_GasLeakage_Unsteady_SUDS_4CPU/bin/cfd_para.hypara b/H11_ThreeD_GasLeakage_Unsteady_UPWIND_4CPU/bin/cfd_para.hypara similarity index 100% rename from H11_ThreeD_GasLeakage_Unsteady_SUDS_4CPU/bin/cfd_para.hypara rename to H11_ThreeD_GasLeakage_Unsteady_UPWIND_4CPU/bin/cfd_para.hypara diff --git a/H11_ThreeD_GasLeakage_Unsteady_SUDS_4CPU/bin/cfd_para_incompressible.hypara b/H11_ThreeD_GasLeakage_Unsteady_UPWIND_4CPU/bin/cfd_para_incompressible.hypara similarity index 100% rename from H11_ThreeD_GasLeakage_Unsteady_SUDS_4CPU/bin/cfd_para_incompressible.hypara rename to H11_ThreeD_GasLeakage_Unsteady_UPWIND_4CPU/bin/cfd_para_incompressible.hypara diff --git a/H11_ThreeD_GasLeakage_Unsteady_SUDS_4CPU/bin/grid_para.hypara b/H11_ThreeD_GasLeakage_Unsteady_UPWIND_4CPU/bin/grid_para.hypara similarity index 100% rename from H11_ThreeD_GasLeakage_Unsteady_SUDS_4CPU/bin/grid_para.hypara rename to H11_ThreeD_GasLeakage_Unsteady_UPWIND_4CPU/bin/grid_para.hypara diff --git a/H11_ThreeD_GasLeakage_Unsteady_SUDS_4CPU/bin/key.hypara b/H11_ThreeD_GasLeakage_Unsteady_UPWIND_4CPU/bin/key.hypara similarity index 100% rename from H11_ThreeD_GasLeakage_Unsteady_SUDS_4CPU/bin/key.hypara rename to H11_ThreeD_GasLeakage_Unsteady_UPWIND_4CPU/bin/key.hypara diff --git a/H11_ThreeD_GasLeakage_Unsteady_SUDS_4CPU/bin/partition.hypara b/H11_ThreeD_GasLeakage_Unsteady_UPWIND_4CPU/bin/partition.hypara similarity index 100% rename from H11_ThreeD_GasLeakage_Unsteady_SUDS_4CPU/bin/partition.hypara rename to H11_ThreeD_GasLeakage_Unsteady_UPWIND_4CPU/bin/partition.hypara diff --git a/H12_ThreeD_Species_Transient_QUICK_4CPU/grid/网格地址.txt b/H11_ThreeD_GasLeakage_Unsteady_UPWIND_4CPU/grid/网格地址.txt similarity index 100% rename from H12_ThreeD_Species_Transient_QUICK_4CPU/grid/网格地址.txt rename to H11_ThreeD_GasLeakage_Unsteady_UPWIND_4CPU/grid/网格地址.txt diff --git a/H12_ThreeD_Species_Transient_QUICK_4CPU/bin/boundary_condition_ref.hypara b/H12_ThreeD_Species_Transient_UPWIND_4CPU/bin/boundary_condition_ref.hypara similarity index 100% rename from H12_ThreeD_Species_Transient_QUICK_4CPU/bin/boundary_condition_ref.hypara rename to H12_ThreeD_Species_Transient_UPWIND_4CPU/bin/boundary_condition_ref.hypara diff --git a/H12_ThreeD_Species_Transient_QUICK_4CPU/bin/cfd_para.hypara b/H12_ThreeD_Species_Transient_UPWIND_4CPU/bin/cfd_para.hypara similarity index 100% rename from H12_ThreeD_Species_Transient_QUICK_4CPU/bin/cfd_para.hypara rename to H12_ThreeD_Species_Transient_UPWIND_4CPU/bin/cfd_para.hypara diff --git a/H12_ThreeD_Species_Transient_QUICK_4CPU/bin/cfd_para_incompressible.hypara b/H12_ThreeD_Species_Transient_UPWIND_4CPU/bin/cfd_para_incompressible.hypara similarity index 100% rename from H12_ThreeD_Species_Transient_QUICK_4CPU/bin/cfd_para_incompressible.hypara rename to H12_ThreeD_Species_Transient_UPWIND_4CPU/bin/cfd_para_incompressible.hypara diff --git a/H12_ThreeD_Species_Transient_QUICK_4CPU/bin/grid_para.hypara b/H12_ThreeD_Species_Transient_UPWIND_4CPU/bin/grid_para.hypara similarity index 100% rename from H12_ThreeD_Species_Transient_QUICK_4CPU/bin/grid_para.hypara rename to H12_ThreeD_Species_Transient_UPWIND_4CPU/bin/grid_para.hypara diff --git a/H12_ThreeD_Species_Transient_QUICK_4CPU/bin/key.hypara b/H12_ThreeD_Species_Transient_UPWIND_4CPU/bin/key.hypara similarity index 100% rename from H12_ThreeD_Species_Transient_QUICK_4CPU/bin/key.hypara rename to H12_ThreeD_Species_Transient_UPWIND_4CPU/bin/key.hypara diff --git a/H12_ThreeD_Species_Transient_QUICK_4CPU/bin/partition.hypara b/H12_ThreeD_Species_Transient_UPWIND_4CPU/bin/partition.hypara similarity index 100% rename from H12_ThreeD_Species_Transient_QUICK_4CPU/bin/partition.hypara rename to H12_ThreeD_Species_Transient_UPWIND_4CPU/bin/partition.hypara diff --git a/H12_ThreeD_Species_Transient_UPWIND_4CPU/grid/网格地址.txt b/H12_ThreeD_Species_Transient_UPWIND_4CPU/grid/网格地址.txt new file mode 100644 index 0000000..899f977 --- /dev/null +++ b/H12_ThreeD_Species_Transient_UPWIND_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/README.md b/README.md index 80bc9f6..4c62a89 100644 --- a/README.md +++ b/README.md @@ -49,6 +49,9 @@ A 结构 | 二维结构30p30n翼型低速绕流(熵修正) | A27_TwoD_30p30n_SA_Entropyfix6_Struct_4CPU | | 二维结构圆柱超声速绕流(熵修正) | A28_TwoD_Cylinder_Inv_Ma3d0_Entropyfix6_Struct_1CPU | | 二维结构Rae2822翼型跨声速绕流(熵修正) | A29_TwoD_Rae2822_SA_Entropyfix6_Struct_4CPU | +| 二维结构圆柱高超声速绕流(熵修正) | A30_TwoD_Cylinder_Inv_Ma10d0_Entropyfix6_Struct_1CPU | +| 三维结构CHNT跨声速流动(Matrix LUSGS) | A31_ThreeD_CHNT_SST_MatrixLUSGS_Struct_256CPU | +| 二维结构NACA0012翼型低速绕流（低速预处理） | A32_TwoD_NACA0012_Inv_Ma0d2_Precondition_Struct_1CPU | B 非结构 @@ -71,7 +74,10 @@ B 非结构 | 二维非结构NLR7301翼型低速绕流 | B15_TwoD_NLR7301_SA_Unstruct_4CPU | | 三维非结构空心圆柱裙 | B16_ThreeD_Hollow_Cylinder_Flare_Laminar_Unstruct_16CPU | | 二维非结构S-K低速平板转捩模拟 | B17_TwoD_Plate_S-KSR_SST_Unstruct_4CPU | -| 三维非结构CRM-HL高升力外形模拟 | B18-ThreeD_CRM-HL_Level-B_SA_Unstruct_1024CPU | +| 三维非结构CRM-HL高升力外形模拟 | B18_ThreeD_CRM-HL_Level-B_SA_Unstruct_1024CPU | +| 三维非结构TrapWing外形模拟 | B19_ThreeD_TrapWing_SA_AoA13_256CPU | +| 二维非结构NACA0012低速绕流（Gmresh） | B20_TwoD_NACA0012_SA_Gmresh_Unstruct_1CPU | +| 三维非结构球头高速绕流（Gmresh） | B21_ThreeD_Sphere_Laminar_Gmresh_Unstruct_1CPU | C 混合 @@ -104,7 +110,7 @@ F 重叠网格、动网格 | 中文 | 英文 | | :------------------------- | :--------------------------------- | -| 三维结构30p30n重叠网格装配 | F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU | +| 二维结构30p30n重叠网格装配 | F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU | | 三维结构多弹体重叠网格装配 | F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU | | 二维非结构双0012重叠网格装配 | F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU | | 二维非结构双0012重叠网格计算 | F04_TwoD_Dual0012_OversetGrid_InvisCal_Unstruct_4CPU | @@ -127,16 +133,25 @@ G 非平衡 | 二维非结构高速圆柱两气体组分预混 | G05_TwoD_Cylinder_N2-O2_Premixing-Unstruct_1CPU | | 三维非结构高速球头两气体组分预混 | G06_ThreeD_Sphere_N2-O2_Premixing-Unstruct_1CPU | | 二维非结构管道喷流两气体组分预混 | G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU | +| 二维储气罐泄漏非定常模拟 | G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU | H 不可压 -| 中文 | 英文 | -| :----------------------------------- | :-------------------------------------------------------- | -| 二维非结构不可压层流后台阶流动 | H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU | -| 二维非结构不可压层流方腔自然对流 | H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU | -| 二维非结构不可压层流方腔流动 | H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU | -| 三维非结构不可压圆管湍流压降模拟 | H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU | -| 三维非结构不可压AFF-1 半艇外流场模拟 | H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU | +| 中文 | 英文 | +| :---------------------------------- | :--------------------------------------- | +| 二维后台阶流动 | H01_TwoD_BackStep_KE_QUICK_4CPU | +| 二维方腔驱动流 | H02_TwoD_Cavitity_Re100_SUDS_4CPU | +| 二维两组分混合气体模拟 | H03_TwoD_GasLeakage_Steady_QUICK_4CPU | +| NACA0012翼型低速绕流PISO方法模拟 | H04_TwoD_NACA0012_PISO_SA_4CPU | +| NACA0012翼型高速流动SIMPLEC方法模拟 | H05_TwoD_NACA0012_SIMPLEC_4CPU | +| 二维自然对流模拟 | H06_TwoD_NaturalConvection_CDS_4CPU | +| 二维湍流平板模拟 | H07_TwoD_Plate_Turb_QUICK_4CPU | +| 二维湍流多组分混合气体模拟 | H08_TwoD_Species_Turb_QUICK_4CPU | +| 三维小车湍流模拟 | H09_ThreeD_Car_Turb_QUICK_4CPU | +| 三维CHNT模型层流模拟 | H10_ThreeD_Chnt_Lam_UPWIND_4CPU | +| 三维多组分泄漏非定常流动模拟 | H11_ThreeD_GasLeakage_Unsteady_SUDS_4CPU | +| 三维多组分扩散非定常流动模拟 | H12_ThreeD_Species_Transient_QUICK_4CPU | +| 三维半艇绕流模拟 | H13_ThreeD_SUBOFF_UPWIND_4CPU | X 用户分享算例