A、B系列编号后均改为下划线

B22_ThreeD_Rotor67_SngleZone_RotatingFrame_6CPU/bin/cfd_para_subsonic.hypara

@@ -159,7 +159,7 @@ int nLUSGSSweeps = 1;
 //                     Please use 'rae2822_hybrid2d__4.fts' here!
 // plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
 
-string gridfile = "./grid/R67.fts";
+string gridfile = "./grid/R67__6.fts";
 int plotFieldType = 1;
 
 // ----------------- Advanced Parameters, DO NOT care it ----------------

F04_TwoD_Dual0012_OversetGrid_InvisCal_Unstruct_4CPU/bin/cfd_para_transonic.hypara

@@ -184,8 +184,8 @@ int plotFieldType = 1;
 // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
 // Variables order must from small to big.
 
-int nVisualVariables = 8;
-int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
+int nVisualVariables = 9;
+int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15, 81];
 
 // limitVariables: Limit model (It is useful only if limitVector is 0).
 //                 0 -- limit only for pressure and denstiny, then get the min value.

F06_ThreeD_AEDC_Separation_OversetGrid_Unsteady_InvisCal_Unstruct_8CPU/bin/kinetic_para.hypara

@@ -50,7 +50,10 @@ int  RBDMethod_1              = 1;
 double gravity_1 = 9.8;
 
 // dimensional physical time for additional force(s).
-double addedForceTime_1[] = 0.054;
+double addedForceTime_1[] = 0.0;
+
+// dimensional massCenterPosition for additional force(s).
+double addedForcePosition_1[] = 0.0, -0.9947, 0.0;
 
 // additional force(inertia system) fX fY fZ.  
 double addedForce_1[] = 0.0, -53342.42, 0.0;

F08-ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU/bin/cfd_para_supersonic.hypara

@@ -7,12 +7,12 @@
 // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
 // intervalStepRes: The step intervals for residual 'res.dat' saved.
 
-int maxSimuStep       = 2000;
+int maxSimuStep       = 1000;
 
-int intervalStepFlow  = 50;
-int intervalStepPlot  = 50;
-int intervalStepForce = 1;
-int intervalStepRes   = 1;
+int intervalStepFlow  = 100;
+int intervalStepPlot  = 100;
+int intervalStepForce = 50;
+int intervalStepRes   = 10;
 
 #########################################################################
 #                       Inflow Parameter                                #
@@ -149,7 +149,7 @@ double venkatCoeff      = 0.5;
 //         The bigger the value, the convergence faster but lower robustness.
 // ktmax: The lower the value, the more robustness, 1.0e5 - 1.0e10.
 
-int    iunsteady        = 1;
+int    iunsteady        = 0;
 double physicalTimeStep = 0.05;
 int    min_sub_iter     = 15;
 int    max_sub_iter     = 31;
@@ -158,9 +158,9 @@ int    aleStartStrategy = 1;
 int    ifStartFromSteadyResults = 1;
 
 int    ifLocalTimeStep  = 0;
-double CFLStart         = 0.1;
-double CFLEnd           = 20.0;
-int    CFLVaryStep      = 10;
+double CFLStart         = 0.01;
+double CFLEnd           = 10.0;
+int    CFLVaryStep      = 50;
 
 #########################################################################
 #                       File In or Out                                  #

F08-ThreeD_Finner_Laminar_Ma2d5_Struct_16CPU/bin/cfd_para_supersonic_unsteady.hypara

@@ -0,0 +1,206 @@
+#########################################################################
+#                     General Control Parameter                         #
+#########################################################################
+// 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.
+// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
+// intervalStepRes: The step intervals for residual 'res.dat' saved.
+
+int maxSimuStep       = 2000;
+
+int intervalStepFlow  = 50;
+int intervalStepPlot  = 50;
+int intervalStepForce = 1;
+int intervalStepRes   = 1;
+
+#########################################################################
+#                       Inflow Parameter                                #
+#########################################################################
+// refMachNumber: Mach number.
+// attackd: Angle of attack.
+// angleSlide: Angle of sideslip.
+// 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.
+// inflowParaType: The type of inflow parameters.
+//                 0 -- the nondimensional conditions.
+//                 1 -- the flight conditions.
+//                 2 -- the experiment conditions.
+//                 3 -- the subsonic boundary conditions.
+// 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.
+// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
+// height: Fly height, unit of km.
+// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
+//                    1 dm = 0.1  m.
+//                    1 cm = 0.01 m.
+//                    1 mm = 0.001m.
+//                    1 inch             = 0.0254m.
+//                    1 foot = 12 inches = 0.3048m.
+//                    1 yard = 3  feet   = 0.9144m.
+// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
+// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
+
+double refMachNumber = 2.50;
+double attackd       = 0.0;
+double angleSlide    = 0.0;
+
+double wallTemperature = -1.0;
+int    dump_Q = 0;
+
+int inflowParaType = 0;
+double refReNumber = 4.8e6;
+double refDimensionalTemperature = 51.0;
+
+//int inflowParaType = 1;
+//double height = 0.001;
+
+//int inflowParaType = 2;
+//double refDimensionalTemperature = 6051.024;    // The total temper ature, T*(1+(refGama-1)*M*M/2).
+//double refDimensionalPressure = 4.299696E09;    // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
+
+double gridScaleFactor = 1.0;
+
+double forceReferenceLengthSpanWise = 1.0;    // unit of meter.
+double forceReferenceLength         = 1.0;            // unit of meter.
+double forceReferenceArea           = 0.7854;              // unit of meter^2.
+double TorqueRefX = 5.0;                      // unit of meter. 
+double TorqueRefY = 0.0;                      // unit of meter.
+double TorqueRefZ = 0.0;                      // unit of meter.
+
+#########################################################################
+#                       Physical models                                 #
+#########################################################################
+// viscousType : Viscous model.
+//           0 -- Euler.
+//           1 -- Lamilar.
+//           3 -- 1eq turbulent.
+//           4 -- 2eq turbulent.
+// viscousName: Laminar or tubulent model.
+//              -- "1eq-sa", when viscousType = 3.
+//              -- "2eq-kw-menter-sst", when viscousType = 4.
+// DESType: Type of DES.
+//          0 -- RANS.(default)
+//          1 -- DES.
+//          2 -- DDES.
+//          3 -- IDDES.
+
+//int    viscousType    = 0;
+//string viscousName = "Euler";
+
+int    viscousType    = 1;
+string viscousName = "laminar";
+
+//int    viscousType    = 3;
+//string viscousName = "1eq-sa";
+
+//int    viscousType    = 4;
+//string viscousName = "2eq-kw-menter-sst";
+
+int DESType = 0;
+
+int roeEntropyFixMethod = 2;
+double roeEntropyScale  = 1.0;
+#########################################################################
+#                       Spatial Discretisation                          #
+#########################################################################
+#*******************************************************************
+#                       Struct Solver                              *
+#*******************************************************************
+// inviscidSchemeName: Spatial discretisation scheme of struct grid.
+//                     Using this when solve structered grid or hybrid.
+//                     -- "vanleer", "steger", "ausmpw".
+// str_limiter_name: Limiter of struct grid.
+//                   -- "minmod", "3rd_minmod_smooth".
+
+string inviscidSchemeName   = "steger";
+string str_limiter_name     = "minvan";
+
+#*******************************************************************
+#                       UnStruct Solver                            *
+#*******************************************************************
+// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
+//                  Using this when solve Unstructered grid or hybrid.
+//                  -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
+//                  -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
+// uns_limiter_name: Limiter of Unstruct grid.
+//                   -- "vencat", "barth".
+//                   -- "1st", meaning accuracy of first-order.
+//                   --  "nolim", no limiter.
+// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'.
+//              The smaller the value, the more robust it is.
+
+string uns_scheme_name  = "vanleer";
+string uns_limiter_name = "vencat";
+double venkatCoeff      = 0.5;
+
+#########################################################################
+#                       Temporal Discretisation                         #
+#########################################################################
+// iunsteady: Steady or unsteady.
+//            0 -- steady.
+//            1 -- unsteay.
+// CFLEnd: The CFL number, [0.1, 100].
+//         The bigger the value, the convergence faster but lower robustness.
+// ktmax: The lower the value, the more robustness, 1.0e5 - 1.0e10.
+
+int    iunsteady        = 1;
+double physicalTimeStep = 0.05;
+int    min_sub_iter     = 15;
+int    max_sub_iter     = 31;
+double tol_sub_iter     = 0.0001;
+int    aleStartStrategy = 1;
+int    ifStartFromSteadyResults = 1;
+
+int    ifLocalTimeStep  = 0;
+double CFLStart         = 0.1;
+double CFLEnd           = 20.0;
+int    CFLVaryStep      = 10;
+
+#########################################################################
+#                       File In or Out                                  #
+#########################################################################
+// gridfile: The partitioned Grid file path, using relative path,
+//           which is relative to the working directory.
+// IMPORTANT WARNING: The file index should be ignored,
+//                     e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
+//                     Please use 'rae2822_hybrid2d__4.fts' here!
+// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
+
+string gridfile = "./grid/finner__16.fts";
+int plotFieldType  = 1;
+int visualfileType = 1;
+int walldistMethod = 3;
+
+// ----------------- Advanced Parameters, DO NOT care it ----------------
+// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
+// visualVariables:  Variable types dumped, listed as following:
+//                   -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
+//                   -- viscosityLaminar(7), viscosityTurbulent(8),
+//                   -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12),
+//                   -- strain_rate(13), Q_criteria(14), Cp(15), timeStep(16), volume(17),
+//                   -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21).
+// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
+// Variables order must from small to big.
+
+int nVisualVariables = 8;
+int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
+
+// limitVariables: Limit model (It is useful only if limitVector is 0).
+//                 0 -- limit only for pressure and denstiny, then get the min value.
+//                 1 -- limit for every variables, then get the min value.
+// limitVector:
+//              0 -- Each variable use the same limiter coefficient.
+//              1 -- Each variable use the respective limiter coefficients.
+// reconmeth:
+//            0 -- When reconstruct face value, Q+, Q- use respective limiter coefficients.
+//            1 -- Q+, Q- use the min limiter coefficients of left and right cell.
+
+int reconmeth = 0;
+int limitVariables = 0;
+int limitVector = 0;