forked from PHengLEI/PHengLEI-TestCases
V2171 A12
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@ -27,9 +27,6 @@
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// 0 -- Not.
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// 1 -- Yes.
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// iadapt: Adaptation number for unstructure grid.
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// iovrlap: Overlapping(overset) grid or not.
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// 0 -- NON-overlapping grid.
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// 1 -- Overlapping grid.
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// SymmetryFaceVector: The vector of symmetry face.
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// 0 -- X axis.
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// 1 -- Y axis.
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@ -38,7 +35,6 @@ int gridtype = 0;
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int gridobj = 1;
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int multiblock = 0;
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int iadapt = 0;
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int iovrlap = 0;
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int SymmetryFaceVector = 1;
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// axisup: Type of Cartisien coordinates system, used in grid conversion.
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@ -83,6 +79,7 @@ string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
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// iunsteady: The Grid is for unsteady simulation or not.
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int iunsteady = 0;
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int iale = 0;
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int codeOfAleModel = 0;
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// fileformat: Ustar Grid file format.
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// 0 -- BINARY.
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@ -165,6 +162,11 @@ int traceMark = 0;
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int blockIndexOfMark = 0;
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int cellIndexOfMark[] = [185,30,1];
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// parallel Strategy:
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//! -# 0 : each zone is assigned to the one that defined in grid partition procedure.
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//! -# 1 : random assigned for each zone or by some else ways.
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int parallelStrategy = 1;
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//-----------------------------------------------------------------------
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# File path #
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//-----------------------------------------------------------------------
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@ -283,6 +285,7 @@ double wallTemperature = -1.0;
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double radiationCoef = 0.8;
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double gridScaleFactor = 1.0;
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int numberOfAerodynamicForceComponents = 1;
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double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
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double forceRefenenceLength = 1.0; // unit of meter.
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double forceRefenenceArea = 1.0; // unit of meter^2.
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@ -435,7 +438,7 @@ double roeEntropyScale = 1.0;
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// 1 --Global.
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// visl_min: Minimum value of laminar viscosity coefficient.
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// turbCFLScale: Turbulence model cfl number factor.
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// iale: Arbitrary Lagrangian-Eulerian method.
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// codeOfAleModel: Arbitrary Lagrangian-Eulerian method.
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// 0 -- no ALE method.
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// 1 -- ALE method for non-moving grids.
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// 2 -- ALE method for moving grids.
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@ -452,7 +455,9 @@ double physicalTimeStep = 0.01;
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int ifStartFromSteadyResults = 0;
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int ifStaticsFlowField = 0;
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int startStatisticStep = 800000;
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int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
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int methodOfDualTime = 3;
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int min_sub_iter = 50;
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int max_sub_iter = 50;
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double tol_sub_iter = 0.01;
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@ -474,11 +479,11 @@ int order = 2;
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double visl_min = 0.01;
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double turbCFLScale = 1.0;
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double csrv = 2.0;
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double timemax = 1.0e10;
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double dtsave = -1.0;
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int iale = 0;
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int ialetype = 2;
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int codeOfAleModel = 0;
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int aleStartStrategy = -1;
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int maxale = 10;
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double dtau = 0.001;
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@ -502,7 +507,7 @@ double lamda[] = 0.5, 1.0;
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// IMPORTANT WARNING: The file index should be ignored,
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// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
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// please use 'rae2822_hybrid2d__4.fts' here!
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// isPlotVolumeField: If dump out the field results to visulization.
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// plotFieldType: If dump out the field results to visulization.
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// walldistMethod: The method to compute wall distance.
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// 0 -- accurate but not fast enough.
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// 1 -- fast but not accurate enough.
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@ -536,11 +541,12 @@ string probesflowfile = "results/sample.dat";
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int nDumpSurfaceInfo = 0;
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string wall_varfile = "";
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string jetDefineFile = "bin/jet.hypara";
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string jetDefineFile = "bin/jet.hypara";
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string overset_gridfile = "iblank.ovs";
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string overset_gridfile = "results/iblank.ovs";
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string sixDofFileName = "results/sixDofInfo.dat";
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int isPlotVolumeField = 0;
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int plotFieldType = 0;
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// visualfileType: The file type of visualfile.
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// 0 -- Tecplot binary.
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@ -575,7 +581,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
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// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
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// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
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// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
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// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44).
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// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), iblank(81).
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// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
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// Variables order must from small to big.
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int nVisualVariables = 8;
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@ -585,19 +591,48 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
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// 1 -- Turbulent flat plate.
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int dumpStandardModel = 0;
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// ifSetProbesToMonitor: Set probes location to Monitor.
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// 0 -- Do not monitor.
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// 1 -- To monitor and save data to files.
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// probesDefineFile: probes location information file.
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// ifSetDataMonitor: Whether to set the data monitor.
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// 0 -- No.
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// 1 -- Yes.
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// dataMonitorType: The type of data Monitor.
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// 0 -- Probes data monitor.
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// 1 -- Lines data monitor.
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// 2 -- Surfaces data monitor.
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// probesDefineFile: Probes location information file.
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// nLines: The number of lines need to be monitored.
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// linesDefineFile: Lines location information file.
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// nSurfaces: The number of surfaces need to be monitored.
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// surfacesDefineFile: Surfaces location information file.
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// searchCellsMethod: method to search the cell of each probe.
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// 0 -- Nearest cell to the probe.
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// 1 -- Real cell where the probe is located.
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// nProbeVariables: Number of variables want to be dumped for probes monitered.
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// probeVariables : Variable types dumped, listed as following:
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// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
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// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
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// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
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// probeVariables order must from small to big.
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int ifSetProbesToMonitor = 0;
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string probesDefineFile = "bin/probes_location.hypara";
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// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables.
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// 0 -- Take the value of probe's cell as probe real value.
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// 1 -- Interpolation from probe's and neighbouring cell to probe.
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// 2 -- Interpolation from probe's cell nodes to probe.
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int ifSetDataMonitor = 0;
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int dataMonitorType = 0;
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string probesDefineFile = "bin/probes_XYZ.dat";
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//int dataMonitorType = 1;
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//int nLines = 1;
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//string linesDefineFile = "bin/lines_XYZ.dat";
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//int dataMonitorType = 2;
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//int nSurfaces = 4;
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//string surfacesDefineFile = "bin/surfaces_XYZ.dat";
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int searchCellsMethod = 0;
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int nProbeVariables = 6;
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int probeVariables[] = [0, 1, 2, 3, 4, 5];
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int probeVariablesInterpolationMethod = 0;
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//-----------------------------------------------------------------------
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# Turbulence Parameter #
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//-----------------------------------------------------------------------
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@ -613,8 +648,10 @@ int kindOfTurbSource = 0;
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int mod_turb_res = 0;
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double turb_relax = 1.0;
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double freeStreamViscosity = 1.0e-3;
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double muoo = 1.0e-1;
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double kwoo = 1.0;
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double muoo = 3.0;
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double kwoo = 5.0;
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int transitionType = 0;
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double turbIntensity = -1.0;
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# maximum eddy viscosity (myt/my) max.
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double eddyViscosityLimit = 1.0e10;
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@ -844,6 +881,30 @@ double MUSCLCoefXk = -1;
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double MUSCLCoefXb = 1.0;
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int allReduceStep = 1;
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// ----------------- overlap configuration ------------------------------
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// codeOfOversetGrid: Overlapping(overset) grid or not.
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// 0 -- NON-overlapping grid.
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// 1 -- Overlapping grid.
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int codeOfOversetGrid = 0;
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int codeOfOversetSlipGrid = 0;
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int readOversetFileOrNot = 0;
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int symetryOrNot = 0;
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int readInAuxiliaryInnerGrid = 1;
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int readInAuxiliaryOuterGrid = 0;
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int readInSklFileOrNot = 0;
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string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
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string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
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string auxiliaryInnerGrid2 = "";
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string oversetGridFileName = "./grid/overlap.ovs";
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double walldistMainZone = 1.0
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double toleranceForOversetSearch = 1.0e-3;
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double toleranceForOversetBox = 1.0e-3;
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int twoOrderInterpolationOrNot = 0;
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int keyEnlargeOfActiveNodes = 0;
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int outTecplotOverset = 0;
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int numberOfMovingBodies = 2;
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// ---------------- ATP read --------------------------------------------
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//@int inflowParaType = 0;
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//@double refReNumber = 2.329418E08;
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@ -854,3 +915,9 @@ int allReduceStep = 1;
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//@int nsubsonicOutlet = 0;
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//@string inLetFileName = "./bin/subsonicInlet.hypara";
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//@string outLetFileName = "./bin/subsonicOutlet.hypara";
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#########################################################################
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# Old Parameter #
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#########################################################################
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int isPlotVolumeField = 0;
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@ -62,7 +62,7 @@ double freestream_vibration_temperature = 10000.0;
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double gridScaleFactor = 0.01;
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double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
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double forceRefenenceLength = 1.0; // unit of meter.
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double forceRefenenceLength = 1.0; // unit of meter.
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double forceRefenenceArea = 1.0; // unit of meter^2.
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double TorqueRefX = 0.0; // unit of meter.
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double TorqueRefY = 0.0; // unit of meter.
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@ -158,10 +158,10 @@ double ktmax = 1.0e10;
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// IMPORTANT WARNING: The file index should be ignored,
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// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
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// Please use 'rae2822_hybrid2d__4.fts' here!
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// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0 / 1.
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// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
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string gridfile = "./grid/DoubleEllipse__4.fts";
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int isPlotVolumeField = 0;
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int plotFieldType = 0;
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// ----------------- Advanced Parameters, DO NOT care it ----------------
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// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
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@ -47,7 +47,6 @@ string parafilename = "./bin/cfd_para_hypersonic.hypara";
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//string parafilename = "./bin/post_processing.hypara";
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// ---------------- Advanced Parameters, DO NOT care it ----------------
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int iovrlap = 0;
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int numberOfGridProcessor = 0;
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// ATP read
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//@string parafilename1 = ""
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@ -1,48 +0,0 @@
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# nBoundaryConditons : number of global boundary conditions.
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# bcName : Boundary Condition Name.
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# bcType(in PHengLEI): Boundary Condition Type.
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# Account of how to set boundaryconditon.
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# string bcName = "Farfield";
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# {
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# int bcType = 4;
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# int inflowParaType = 1;
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# double attackd = 0;
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# double refReNumber = 6.5e6;
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# double refMachNumber = 3.5;
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# double angleSlide = 0;
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# }
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int nBoundaryConditons = 4;
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string bcName = "SOLID_SURFACE";
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{
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int bcType = 2;
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}
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string bcName = "SYMMETRY";
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{
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int bcType = 3;
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}
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string bcName = "INFLOW";
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{
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int bcType = 5;
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}
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string bcName = "OUTFLOW";
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{
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int bcType = 6;
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}
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# 'bcType' is defined as following:
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# 99: PERIODIC
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# -2: WAKE
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# -1: INTERFACE
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# 0 : NO_BOUNDARY_CONDITION
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# 1 : EXTRAPOLATION
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# 2 : SOLID_SURFACE
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# 3 : SYMMETRY
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# 4 : FARFIELD
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# 5 : INFLOW
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# 6 : OUTFLOW
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# 52: PRESSURE_INLET
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# 62: PRESSURE_OUTLET
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# 61: OUTFLOW_CONFINED
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# 7 : POLE
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