diff --git a/ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para.hypara b/A09_ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para.hypara similarity index 91% rename from ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para.hypara rename to A09_ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para.hypara index f52cf86..df090b7 100644 --- a/ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para.hypara +++ b/A09_ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para.hypara @@ -26,15 +26,7 @@ // multiblock: Multi-block grid or not, only for structured grid conversion. // 0 -- Not. // 1 -- Yes. -// grid_database_index: Case of typical case, only for gridobj=0. -// 1 -- Laminar flat plate of subsonic flow. -// 2 -- Laminar flat plate of supersonic flow. -// 3 -- Turbulent flat plate of subsonic flow. -// 4 -- Turbulent flat plate of supersonic flow. // iadapt: Adaptation number for unstructure grid. -// iovrlap: Overlapping(overset) grid or not. -// 0 -- NON-overlapping grid. -// 1 -- Overlapping grid. // SymmetryFaceVector: The vector of symmetry face. // 0 -- X axis. // 1 -- Y axis. @@ -42,9 +34,7 @@ int gridtype = 0; int gridobj = 1; int multiblock = 0; -int grid_database_index = 3; int iadapt = 0; -int iovrlap = 0; int SymmetryFaceVector = 1; // axisup: Type of Cartisien coordinates system, used in grid conversion. @@ -89,22 +79,18 @@ string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; // iunsteady: The Grid is for unsteady simulation or not. int iunsteady = 0; int iale = 0; +int codeOfAleModel = 0; // fileformat: Ustar Grid file format. // 0 -- BINARY. // 1 -- ASCII. int fileformat = 0; -// .skl meaning skeleton. -string original_grid_info_file = "./grid/FLUENT_test.skl"; - // Parameters for hybrid solver. // mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type. // mixgrid_str: path of structure grid file for hybrid solver, *.fts type. -// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver. string mixgrid_uns = "./grid/rae2822_uns2d_4.fts"; string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts"; -string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp"; // Some parameters for structured overlapping grid. int codeOfDigHoles = 1; @@ -176,6 +162,11 @@ int traceMark = 0; int blockIndexOfMark = 0; int cellIndexOfMark[] = [185,30,1]; +// parallel Strategy: +//! -# 0 : each zone is assigned to the one that defined in grid partition procedure. +//! -# 1 : random assigned for each zone or by some else ways. +int parallelStrategy = 1; + //----------------------------------------------------------------------- # File path # //----------------------------------------------------------------------- @@ -253,12 +244,6 @@ int compressible = 1; // refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition. // height: Fly height, unit of km. // wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition. -// dump_Q: Dump out thermal flux Q of solid wall. -// 0 -- no dump out. -// 1 -- dump out wall Q only. -// 2 -- dump out wall Q & the typical position Q of ball. -// 3 -- dump out wall Q & the typical position Q of cone. -// 4 -- dump out wall Q & the typical position Q of double sphere. // gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like: // 1 dm = 0.1 m. // 1 cm = 0.01 m. @@ -296,11 +281,11 @@ double freestream_vibration_temperature = 10000.00; //double refDimensionalPressure = 1.01313E05; double wallTemperature = -1.0; -int dump_Q = 0; double radiationCoef = 0.8; double gridScaleFactor = 1.0; +int numberOfAerodynamicForceComponents = 1; double forceRefenenceLengthSpanWise = 1.0; // unit of meter. double forceRefenenceLength = 1.0; // unit of meter. double forceRefenenceArea = 1.0; // unit of meter^2. @@ -410,7 +395,6 @@ double venkatCoeff = 5.0; int reconmeth = 1; int limitVariables = 0; int limitVector = 0; -double limit_angle = 0; double skewnessAngle = 60.0; int roeEntropyFixMethod = 3; @@ -454,7 +438,7 @@ double roeEntropyScale = 1.0; // 1 --Global. // visl_min: Minimum value of laminar viscosity coefficient. // turbCFLScale: Turbulence model cfl number factor. -// iale: Arbitrary Lagrangian-Eulerian method. +// codeOfAleModel: Arbitrary Lagrangian-Eulerian method. // 0 -- no ALE method. // 1 -- ALE method for non-moving grids. // 2 -- ALE method for moving grids. @@ -471,7 +455,9 @@ double physicalTimeStep = 0.01; int ifStartFromSteadyResults = 0; int ifStaticsFlowField = 0; int startStatisticStep = 800000; +int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2; +int methodOfDualTime = 3; int min_sub_iter = 50; int max_sub_iter = 50; double tol_sub_iter = 0.01; @@ -493,14 +479,13 @@ int order = 2; double visl_min = 0.01; double turbCFLScale = 1.0; - +double csrv = 2.0; double timemax = 1.0e10; double dtsave = -1.0; -int iale = 0; -int ialetype = 2; +int codeOfAleModel = 0; +int aleStartStrategy = -1; int maxale = 10; double dtau = 0.001; -double dtau_max = 1E-01; int wallFunctionType = 0; @@ -522,7 +507,7 @@ double lamda[] = 0.5, 1.0; // IMPORTANT WARNING: The file index should be ignored, // e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts, // please use 'rae2822_hybrid2d__4.fts' here! -// isPlotVolumeField: If dump out the field results to visulization. +// plotFieldType: If dump out the field results to visulization. // walldistMethod: The method to compute wall distance. // 0 -- accurate but not fast enough. // 1 -- fast but not accurate enough. @@ -550,22 +535,18 @@ string restartNSFile = "results/flow.dat"; string turbfile = "results/turb.dat"; string visualfile = "results/tecflow.plt"; -string Qwall_file = "results/Qwall.dat"; string wall_aircoefile = "results/wall_aircoef.dat"; string probesflowfile = "results/sample.dat"; -string surfacefile = ""; -int nDumpSurfaceInfo = 0; +int nDumpSurfaceInfo = 0; string wall_varfile = ""; -string componentDefineFile = "bin/component.hypara"; -string jetDefineFile = "bin/jet.hypara"; +string jetDefineFile = "bin/jet.hypara"; -string componentforcefile = "results/component_aircoef.dat"; +string overset_gridfile = "results/iblank.ovs"; +string sixDofFileName = "results/sixDofInfo.dat"; -string overset_gridfile = "iblank.ovs"; - -int isPlotVolumeField = 0; +int plotFieldType = 0; // visualfileType: The file type of visualfile. // 0 -- Tecplot binary. @@ -600,7 +581,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), // -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), -// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44). +// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), iblank(81). // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. int nVisualVariables = 8; @@ -610,19 +591,48 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; // 1 -- Turbulent flat plate. int dumpStandardModel = 0; -// ifSetProbesToMonitor: Set probes location to Monitor. -// 0 -- Do not monitor. -// 1 -- To monitor and save data to files. -// probesDefineFile: probes location information file. +// ifSetDataMonitor: Whether to set the data monitor. +// 0 -- No. +// 1 -- Yes. +// dataMonitorType: The type of data Monitor. +// 0 -- Probes data monitor. +// 1 -- Lines data monitor. +// 2 -- Surfaces data monitor. +// probesDefineFile: Probes location information file. +// nLines: The number of lines need to be monitored. +// linesDefineFile: Lines location information file. +// nSurfaces: The number of surfaces need to be monitored. +// surfacesDefineFile: Surfaces location information file. +// searchCellsMethod: method to search the cell of each probe. +// 0 -- Nearest cell to the probe. +// 1 -- Real cell where the probe is located. // nProbeVariables: Number of variables want to be dumped for probes monitered. // probeVariables : Variable types dumped, listed as following: -// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5). +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5). // Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!! // probeVariables order must from small to big. -int ifSetProbesToMonitor = 0; -string probesDefineFile = "bin/probes_location.hypara"; +// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables. +// 0 -- Take the value of probe's cell as probe real value. +// 1 -- Interpolation from probe's and neighbouring cell to probe. +// 2 -- Interpolation from probe's cell nodes to probe. +int ifSetDataMonitor = 0; + +int dataMonitorType = 0; +string probesDefineFile = "bin/probes_XYZ.dat"; + +//int dataMonitorType = 1; +//int nLines = 1; +//string linesDefineFile = "bin/lines_XYZ.dat"; + +//int dataMonitorType = 2; +//int nSurfaces = 4; +//string surfacesDefineFile = "bin/surfaces_XYZ.dat"; + +int searchCellsMethod = 0; + int nProbeVariables = 6; int probeVariables[] = [0, 1, 2, 3, 4, 5]; +int probeVariablesInterpolationMethod = 0; //----------------------------------------------------------------------- # Turbulence Parameter # //----------------------------------------------------------------------- @@ -634,19 +644,17 @@ int probeVariables[] = [0, 1, 2, 3, 4, 5]; // mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0. int turbInterval = 1; -int turb_vis_kind = 2; int kindOfTurbSource = 0; int mod_turb_res = 0; double turb_relax = 1.0; -double turb_min_coef = 1.0e-1; double freeStreamViscosity = 1.0e-3; -double muoo = 1.0e-1; -double kwoo = 1.0; +double muoo = 3.0; +double kwoo = 5.0; +int transitionType = 0; +double turbIntensity = -1.0; # maximum eddy viscosity (myt/my) max. double eddyViscosityLimit = 1.0e10; -double sdilim = 1.0e20; -double coef_kvist = 1.0; int monitor_vistmax = 0; //----------------------------------------------------------------------- @@ -748,14 +756,9 @@ int monitorNegativeConstant = 0; int dg_high_order = 0; int iapplication = 0; -int iCodeBranch = 0; +int iCodeBranch = 0; int nm = 5; -// MHD -double bxoo = 0.0; -double byoo = 0.0; -double bzoo = 0.0; - double refGama = 1.4; double prl = 0.72; double prt = 0.90; @@ -878,6 +881,30 @@ double MUSCLCoefXk = -1; double MUSCLCoefXb = 1.0; int allReduceStep = 1; +// ----------------- overlap configuration ------------------------------ +// codeOfOversetGrid: Overlapping(overset) grid or not. +// 0 -- NON-overlapping grid. +// 1 -- Overlapping grid. +int codeOfOversetGrid = 0; +int codeOfOversetSlipGrid = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 1; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/overlap.ovs"; +double walldistMainZone = 1.0 +double toleranceForOversetSearch = 1.0e-3; +double toleranceForOversetBox = 1.0e-3; +int twoOrderInterpolationOrNot = 0; +int keyEnlargeOfActiveNodes = 0; +int outTecplotOverset = 0; + +int numberOfMovingBodies = 2; + // ---------------- ATP read -------------------------------------------- //@int inflowParaType = 0; //@double refReNumber = 2.329418E08; @@ -888,3 +915,9 @@ int allReduceStep = 1; //@int nsubsonicOutlet = 0; //@string inLetFileName = "./bin/subsonicInlet.hypara"; //@string outLetFileName = "./bin/subsonicOutlet.hypara"; + +######################################################################### +# Old Parameter # +######################################################################### +int isPlotVolumeField = 0; + diff --git a/ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para_transonic.hypara b/A09_ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para_transonic.hypara similarity index 96% rename from ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para_transonic.hypara rename to A09_ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para_transonic.hypara index e282f23..a56ed7e 100644 --- a/ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para_transonic.hypara +++ b/A09_ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para_transonic.hypara @@ -81,16 +81,16 @@ double TorqueRefZ = 0.0; // unit of meter. // 3 -- IDDES. //int viscousType = 0; -//string viscousName = "Euler"; +//string viscousName = "Euler"; //int viscousType = 1; -//string viscousName = "laminar"; +//string viscousName = "laminar"; //int viscousType = 3; -//string viscousName = "1eq-sa"; +//string viscousName = "1eq-sa"; int viscousType = 4; -string viscousName = "2eq-kw-menter-sst"; +string viscousName = "2eq-kw-menter-sst"; int DESType = 0; @@ -139,7 +139,7 @@ double venkatCoeff = 5.0; // CFLEnd: The CFL number, [0.1, 100]. // The bigger the value, the convergence faster but lower robustness. // nLUSGSSweeps: Number of Sub-iteration of LU-SGS. -// 0 -- is recommended for structured solver. +// 1 -- is recommended for structured solver. // 1-3 -- is recommended for unstructured solver. int iunsteady = 0; @@ -169,10 +169,10 @@ int flowInitStep = 100; // IMPORTANT WARNING: The file index should be ignored, // e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts, // Please use 'rae2822_hybrid2d__4.fts' here! -// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0 / 1. +// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1. string gridfile = "./grid/m6_str__4.fts"; -int isPlotVolumeField = 0; +int plotFieldType = 0; // ----------------- Advanced Parameters, DO NOT care it ---------------- // nVisualVariables: Number of variables want to be dumped for tecplot visualization. @@ -181,7 +181,7 @@ int isPlotVolumeField = 0; // -- viscosityLaminar(7), viscosityTurbulent(8), // -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12), // -- strain_rate(13), Q_criteria(14), Cp(15), timeStep(16), volume(17), -// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21). +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), iblank(81). // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. diff --git a/ThreeD_M6_SST_Struct_MG2_4CPU/bin/grid_para.hypara b/A09_ThreeD_M6_SST_Struct_MG2_4CPU/bin/grid_para.hypara similarity index 57% rename from ThreeD_M6_SST_Struct_MG2_4CPU/bin/grid_para.hypara rename to A09_ThreeD_M6_SST_Struct_MG2_4CPU/bin/grid_para.hypara index ec67950..2e232da 100644 --- a/ThreeD_M6_SST_Struct_MG2_4CPU/bin/grid_para.hypara +++ b/A09_ThreeD_M6_SST_Struct_MG2_4CPU/bin/grid_para.hypara @@ -2,24 +2,24 @@ # Grid data type # ######################################################################### // gridtype: Grid type for generation, conversion, reconstruction, merging. -// 0 -- Unstructured grid. -// 1 -- Structured grid. -// axisup: Type of Cartisien coordinates system, used in grid conversion. -// 1 -- Y upward. (default) -// 2 -- Z upward. +// 0 -- Unstructured grid. +// 1 -- Structured grid. +// axisup: Type of Cartisien coordinates system, used in grid conversion. +// 1 -- Y upward. (default) +// 2 -- Z upward. // from_gtype: Type of grid data type in grid conversion process. // -1 -- MULTI_TYPE. // 1 -- PHengLEI, *.fts. -// 2 -- CGNS, *.cgns. -// 3 -- Plot3D type of structured grid, *.dat/*.grd. -// 4 -- Fieldview type of unstructured grid, *.dat/*.inp. -// 5 -- Fluent, *.cas/*.msh. -// 6 -- Ustar, mgrid.in. -// 7 -- Hybrid, include both of unstructured and structured grid, *.fts. -// 8 -- GMSH, *.msh. -int gridtype = 1; -int axisup = 2; -int from_gtype = 2; +// 2 -- CGNS, *.cgns. +// 3 -- Plot3D type of structured grid, *.dat/*.grd. +// 4 -- Fieldview type of unstructured grid, *.dat/*.inp. +// 5 -- Fluent, *.cas/*.msh. +// 6 -- Ustar, mgrid.in. +// 7 -- Hybrid, include both of unstructured and structured grid, *.fts. +// 8 -- GMSH, *.msh. +int gridtype = 1; +int axisup = 2; +int from_gtype = 2; ######################################################################### # File path # diff --git a/A09_ThreeD_M6_SST_Struct_MG2_4CPU/bin/key.hypara b/A09_ThreeD_M6_SST_Struct_MG2_4CPU/bin/key.hypara new file mode 100644 index 0000000..2332f09 --- /dev/null +++ b/A09_ThreeD_M6_SST_Struct_MG2_4CPU/bin/key.hypara @@ -0,0 +1,53 @@ +string title = "PHengLEI Main Parameter Control File"; + +// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE. +string defaultParaFile = "./bin/cfd_para.hypara"; + +// ndim: Dimensional of the grid, 2 or 3. +// nparafile: the number of parameter files. +// nsimutask: simulation task type. +// 0 -- CFD Solver of NS or Turbulation. +// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc. +// Grid conversion: from other format to PHengLEI format (.fts). +// Grid reconstruction: such as grid adaptation. +// Grid merging: merge two blocks into one block. +// Grid repairing: repair the original grid in order to remove the negative volume cells. +// 2 -- Wall distance computation for turb-solver. +// 3 -- Grid partition. +// 4 -- Knowledge repository / examples of PHengLEI-API. +int ndim = 3; +int nparafile = 1; + +int nsimutask = 0; +//string parafilename = "./bin/cfd_para_subsonic.hypara"; +string parafilename = "./bin/cfd_para_transonic.hypara"; +//string parafilename = "./bin/cfd_para_supersonic.hypara"; +//string parafilename = "./bin/cfd_para_hypersonic.hypara"; +//string parafilename = "./bin/incompressible.hypara"; + +//int nsimutask = 1; +//string parafilename = "./bin/grid_para.hypara"; + +//int nsimutask = 2; +//string parafilename = "./bin/cfd_para.hypara"; + +//int nsimutask = 3; +//string parafilename = "./bin/partition.hypara"; + +//int nsimutask = 4; +//string parafilename = "./bin/repository.hypara"; + +//int nsimutask = 5; +//string parafilename = "./bin/overset_grid_view.hypara"; + +//int nsimutask = 14; +//string parafilename = "./bin/integrative_solver.hypara"; + +//int nsimutask = 99; +//string parafilename = "./bin/post_processing.hypara"; + +// ---------------- Advanced Parameters, DO NOT care it ---------------- +int numberOfGridProcessor = 0; +// ATP read +//@string parafilename1 = "" +//@string parafilename2 = ""; diff --git a/ThreeD_M6_SST_Struct_MG2_4CPU/bin/partition.hypara b/A09_ThreeD_M6_SST_Struct_MG2_4CPU/bin/partition.hypara similarity index 66% rename from ThreeD_M6_SST_Struct_MG2_4CPU/bin/partition.hypara rename to A09_ThreeD_M6_SST_Struct_MG2_4CPU/bin/partition.hypara index 75cd057..49d50d7 100644 --- a/ThreeD_M6_SST_Struct_MG2_4CPU/bin/partition.hypara +++ b/A09_ThreeD_M6_SST_Struct_MG2_4CPU/bin/partition.hypara @@ -3,19 +3,19 @@ // 1 -- struct grid. // maxproc: The number of partition zones that want to be divided into, // which is equal to the number of CPU processors you want. -// Usually, 50~100 thousands structured cells per CPU-Core is suggested. -// 30~70 thousands unstructured cells per CPU-Core is suggested. +// Usually, 50~100 thousands structured cells per CPU-Core is suggested. +// 30~70 thousands unstructured cells per CPU-Core is suggested. // original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts). // partition_grid_file: Target partition grid file(PHengLEI type, *.fts). -int pgridtype = 1; -int maxproc = 4; +int pgridtype = 1; +int maxproc = 4; -string original_grid_file = "./grid/m6_str.fts"; -string partition_grid_file = "./grid/m6_str__4.fts"; +string original_grid_file = "./grid/m6_str.fts"; +string partition_grid_file = "./grid/m6_str__4.fts"; // numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. // 1 -- single level. // 2 -- 2 level. // N -- N level,..., et al. -int numberOfMultigrid = 2; \ No newline at end of file +int numberOfMultigrid = 2; diff --git a/ThreeD_M6_SST_Struct_MG2_4CPU/grid/m6_str.cgns b/A09_ThreeD_M6_SST_Struct_MG2_4CPU/grid/m6_str.cgns similarity index 100% rename from ThreeD_M6_SST_Struct_MG2_4CPU/grid/m6_str.cgns rename to A09_ThreeD_M6_SST_Struct_MG2_4CPU/grid/m6_str.cgns diff --git a/ThreeD_M6_SST_Struct_MG2_4CPU/bin/key.hypara b/ThreeD_M6_SST_Struct_MG2_4CPU/bin/key.hypara deleted file mode 100644 index c977a1e..0000000 --- a/ThreeD_M6_SST_Struct_MG2_4CPU/bin/key.hypara +++ /dev/null @@ -1,45 +0,0 @@ -string title = "PHengLEI Main Parameter Control File"; - -// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE. -string defaultParaFile = "./bin/cfd_para.hypara"; - -// ndim: Dimensional of the grid, 2 or 3. -// nparafile: the number of parameter files. -// nsimutask: simulation task type. -// 0 -- CFD Solver of NS or Turbulation. -// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc. -// Grid conversion: from other format to PHengLEI format (.fts). -// Grid reconstruction: such as grid adaptation. -// Grid merging: merge two blocks into one block. -// Grid repairing: repair the original grid in order to remove the negative volume cells. -// 2 -- Wall distance computation for turb-solver. -// 3 -- Grid partition. -// 4 -- Knowledge repository / examples of PHengLEI-API. -int ndim = 3; -int nparafile = 1; - -int nsimutask = 0; -string parafilename = "./bin/cfd_para_transonic.hypara"; -//string parafilename = "./bin/cfd_para_transonic.hypara"; -//string parafilename = "./bin/cfd_para_supersonic.hypara"; -//string parafilename = "./bin/cfd_para_hypersonic.hypara"; -//string parafilename = "./bin/incompressible.hypara"; -//int nsimutask = 1; -//string parafilename = "./bin/grid_para.hypara"; -//int nsimutask = 2; -//string parafilename = "./bin/cfd_para.hypara"; -//int nsimutask = 3; -//string parafilename = "./bin/partition.hypara"; -//int nsimutask = 4; -//string parafilename = "./bin/repository.hypara"; -//int nsimutask = 5; -//string parafilename = "./bin/overset_grid_view.hypara"; -//int nsimutask = 99; -//string parafilename = "./bin/post_processing.hypara"; - -// ---------------- Advanced Parameters, DO NOT care it ---------------- -int iovrlap = 0; -int numberOfGridProcessor = 0; -// ATP read -//@string parafilename1 = "" -//@string parafilename2 = "";