V2171 A09

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    codeOfAleModel   = 0;
-int    ialetype = 2;
+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;
 string wall_varfile       = "";
 
-string componentDefineFile = "bin/component.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 plotFieldType = 0;
-
-int    isPlotVolumeField  = 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.
+// ifSetDataMonitor: Whether to set the data monitor.
-//              0 -- Do not monitor.
+//                   0 -- No.
-//              1 -- To monitor and save data to files.
+//                   1 -- Yes.
-// probesDefineFile: probes location information file.
+// dataMonitorType: The type of data Monitor.
+//                  0 -- Probes data monitor.
+//                  1 -- Lines data monitor.
+//                  2 -- Surfaces data monitor.
+// probesDefineFile: Probes location information file.
+// nLines: The number of lines need to be monitored.
+// linesDefineFile: Lines location information file.
+// nSurfaces: The number of surfaces need to be monitored.
+// surfacesDefineFile: Surfaces location information file.
+// searchCellsMethod: method to search the cell of each probe.
+//                    0 -- Nearest cell to the probe.
+//                    1 -- Real cell where the probe is located.
 // nProbeVariables: Number of variables want to be dumped for probes monitered.
 // probeVariables : Variable types dumped, listed as following:
 //                  -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
 // Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
 // probeVariables order must from small to big.
-int    ifSetProbesToMonitor  = 0;
+// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables.
-string probesDefineFile      = "bin/probes_location.hypara";
+//                 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 muoo          = 3.0;
-double kwoo          = 1.0;
+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;
 
 //-----------------------------------------------------------------------
@@ -751,11 +759,6 @@ int iapplication  = 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;
+

A09_ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para_transonic.hypara

@@ -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.
 

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 = "";

ThreeD_M6_SST_Struct_MG2_4CPU/bin/key.hypara

@@ -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 = "";