| % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------% |
| % |
| SOLVER= RANS |
| KIND_TURB_MODEL= SA |
| SA_OPTIONS= ROTATION |
| RESTART_SOL= NO |
|
|
| % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------% |
| % |
| MACH_NUMBER= 0.3 |
| AOA= 15.0 |
| FREESTREAM_TEMPERATURE= 285.0 |
| REYNOLDS_NUMBER= 8.04E7 |
| REYNOLDS_LENGTH= 16 |
|
|
| % ---------------------- REFERENCE VALUE DEFINITION ---------------------------% |
| % |
| REF_ORIGIN_MOMENT_X = 36.38 |
| REF_ORIGIN_MOMENT_Y = 0.00 |
| REF_ORIGIN_MOMENT_Z = 0.00 |
| REF_LENGTH= 16 |
| REF_AREA= 468.1112730923969 |
|
|
| % --------------------FLUID MODEL----------------------------------------------% |
| % |
| FLUID_MODEL= STANDARD_AIR |
| GAMMA_VALUE= 1.4 |
| GAS_CONSTANT= 287.058 |
|
|
| % -----------------------VISCOSITY MODEL--------------------------------------% |
| % |
| VISCOSITY_MODEL= SUTHERLAND |
| MU_CONSTANT=1.716e-05 |
|
|
| % --------------------------THERMAL MODEL-------------------------------------% |
| % |
| CONDUCTIVITY_MODEL= CONSTANT_PRANDTL |
| PRANDTL_LAM= 0.72 |
| PRANDTL_TURB= 0.90 |
|
|
| % -------------------- BOUNDARY CONDITION DEFINITION --------------------------% |
| % |
| MARKER_HEATFLUX= ( wall, 0.0 ) |
| %MARKER_EULER= ( wall ) |
| MARKER_FAR= ( farfield ) |
| MARKER_PLOTTING= ( wall ) |
| MARKER_MONITORING= ( wall ) |
| FREESTREAM_TURBULENCEINTENSITY= 0.03 |
|
|
| % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------% |
| % |
| NUM_METHOD_GRAD= GREEN_GAUSS |
| CFL_NUMBER= 10.0 |
| CFL_ADAPT= YES |
| CFL_ADAPT_PARAM= ( 0.2, 1.5, 0.00001, 2000 ) |
| ITER= 29999 |
| LINEAR_SOLVER= FGMRES |
| LINEAR_SOLVER_ERROR= 1E-7 |
| LINEAR_SOLVER_ITER= 50 |
| LINEAR_SOLVER_PREC= ILU |
|
|
| % -------------------------- MULTIGRID PARAMETERS -----------------------------% |
| % |
| MGLEVEL= 0 |
| MGCYCLE= W_CYCLE |
| MG_PRE_SMOOTH= ( 1, 2, 3, 3 ) |
| MG_POST_SMOOTH= ( 0, 0, 0, 0 ) |
| MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 ) |
| MG_DAMP_RESTRICTION= 0.95 |
| MG_DAMP_PROLONGATION= 0.95 |
|
|
| % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------% |
| % |
| CONV_NUM_METHOD_FLOW= JST |
| MUSCL_FLOW= NO |
| SLOPE_LIMITER_FLOW= VENKATAKRISHNAN |
| VENKAT_LIMITER_COEFF= 0.08 |
| JST_SENSOR_COEFF= ( 0.5, 0.02 ) |
| TIME_DISCRE_FLOW= EULER_IMPLICIT |
|
|
| % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------% |
| % |
| CONV_NUM_METHOD_TURB= SCALAR_UPWIND |
| MUSCL_TURB= NO |
| SLOPE_LIMITER_TURB= VENKATAKRISHNAN |
| TIME_DISCRE_TURB= EULER_IMPLICIT |
|
|
| % --------------------------- CONVERGENCE PARAMETERS --------------------------% |
| % |
| CONV_RESIDUAL_MINVAL= -6 |
| CONV_STARTITER= 800 |
| CONV_FIELD= DRAG |
| CONV_CAUCHY_ELEMS= 100 |
| CONV_CAUCHY_EPS= 1E-5 |
|
|
| % ------------------------- INPUT/OUTPUT INFORMATION --------------------------% |
| % |
| MESH_FILENAME= 192401-8QF.su2 |
| MESH_FORMAT= SU2 |
| MESH_OUT_FILENAME= mesh_out.su2 |
| SOLUTION_FILENAME= solution_flow.dat |
| TABULAR_FORMAT= CSV |
| CONV_FILENAME= history |
| RESTART_FILENAME= restart_flow.dat |
| VOLUME_FILENAME= flow |
| SURFACE_FILENAME= surface_flow |
| OUTPUT_WRT_FREQ= 200 |
| WRT_FORCES_BREAKDOWN= YES |
| BREAKDOWN_FILENAME= forces_breakdown.dat |
| SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG, CFL_NUMBER, LINSOL, CAUCHY) |
| HISTORY_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG, CFL_NUMBER, LINSOL, CAUCHY) |
| % Change to Tecplot if needed |
| VOLUME_OUTPUT= (COORDINATES, SOLUTION, PRIMITIVE, DISSIPATION, MESH_QUALITY) |
| OUTPUT_FILES= (RESTART, PARAVIEW, SURFACE_PARAVIEW, SURFACE_PARAVIEW_ASCII) |
|
|
