File size: 3,306 Bytes
a6eea8c | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 | % ------------- 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) |