|
| 1 | +%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% |
| 2 | +% % |
| 3 | +% SU2 configuration file % |
| 4 | +% Case description: 2D 5x5 Square Test Case representing a thermal bath % |
| 5 | +% with thermal nonequilibrium and finite-rate chemistry % |
| 6 | +% % |
| 7 | +% This is only serves as a validation case. % |
| 8 | +% % |
| 9 | +% % |
| 10 | +% Author: W. Maier % |
| 11 | +% File Version 7.3.0 "Blackbird" % |
| 12 | +% % |
| 13 | +%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% |
| 14 | + |
| 15 | +% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------% |
| 16 | +% |
| 17 | +% Physical governing equations (EULER, NAVIER_STOKES, |
| 18 | +% WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY, |
| 19 | +% POISSON_EQUATION) |
| 20 | +SOLVER= NEMO_EULER |
| 21 | +GAS_MODEL= AIR-7 |
| 22 | +GAS_COMPOSITION=(0.0, 0.767, 0.233, 0.0, 0.0, 0.0, 0.0) |
| 23 | +MATH_PROBLEM= DIRECT |
| 24 | +READ_BINARY_RESTART= NO |
| 25 | + |
| 26 | +TIME_MARCHING=TIME_STEPPING |
| 27 | +TIME_DOMAIN= YES |
| 28 | +TIME_STEP= 0.000000001 % 1.e-09 |
| 29 | +MAX_TIME= 0.001 |
| 30 | + |
| 31 | +% ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE_STREAM DEFINITION ----------% |
| 32 | +% |
| 33 | +MACH_NUMBER= 0.0 |
| 34 | +AOA = 0.0 |
| 35 | +FREESTREAM_PRESSURE = 101325.0 |
| 36 | +FREESTREAM_TEMPERATURE = 30000 |
| 37 | +FREESTREAM_TEMPERATURE_VE= 1000 |
| 38 | + |
| 39 | +% ---- NONEQUILIBRIUM GAS, IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------% |
| 40 | +FLUID_MODEL= SU2_NONEQ |
| 41 | + |
| 42 | +% -------------------- BOUNDARY CONDITION DEFINITION --------------------------% |
| 43 | +% |
| 44 | +MARKER_SYM= (left,bottom,top,right ) |
| 45 | + |
| 46 | +% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------% |
| 47 | +% |
| 48 | +NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES |
| 49 | +CFL_NUMBER= 1.0 |
| 50 | +TIME_ITER= 11 |
| 51 | + |
| 52 | +% ------------------------ LINEAR SOLVER DEFINITION ---------------------------% |
| 53 | +% |
| 54 | +LINEAR_SOLVER= FGMRES |
| 55 | +LINEAR_SOLVER_PREC= ILU |
| 56 | +LINEAR_SOLVER_ERROR= 1E-10 |
| 57 | +LINEAR_SOLVER_ITER= 10 |
| 58 | + |
| 59 | +% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------% |
| 60 | +% |
| 61 | +CONV_NUM_METHOD_FLOW= AUSM |
| 62 | +MUSCL_FLOW= NO |
| 63 | +SLOPE_LIMITER_FLOW= VENKATAKRISHNAN |
| 64 | +TIME_DISCRE_FLOW= EULER_EXPLICIT |
| 65 | + |
| 66 | +% --------------------------- CONVERGENCE PARAMETERS --------------------------% |
| 67 | +% |
| 68 | +CONV_RESIDUAL_MINVAL= -50 |
| 69 | +CONV_STARTITER= 10 |
| 70 | +CONV_CAUCHY_ELEMS= 100 |
| 71 | +CONV_CAUCHY_EPS= 1E-6 |
| 72 | +OBJECTIVE_FUNCTION= DRAG |
| 73 | + |
| 74 | +% ------------------------- INPUT/OUTPUT INFORMATION --------------------------% |
| 75 | +% |
| 76 | +MESH_FILENAME= 5x5Mesh.su2 |
| 77 | +MESH_FORMAT= SU2 |
| 78 | +MESH_OUT_FILENAME= mesh_out.su2 |
| 79 | +SOLUTION_FILENAME= restart_flow.dat |
| 80 | +SOLUTION_ADJ_FILENAME= solution_adj.dat |
| 81 | +TABULAR_FORMAT= TECPLOT |
| 82 | +OUTPUT_FILES= (RESTART_ASCII) |
| 83 | +CONV_FILENAME= history |
| 84 | +RESTART_FILENAME= restart_flow.dat |
| 85 | +RESTART_ADJ_FILENAME= restart_adj.dat |
| 86 | +VOLUME_FILENAME= test_flow |
| 87 | +VOLUME_ADJ_FILENAME= adjoint |
| 88 | +GRAD_OBJFUNC_FILENAME= of_grad.dat |
| 89 | +SURFACE_FILENAME= surface_flow |
| 90 | +SURFACE_ADJ_FILENAME= surface_adjoint |
| 91 | +SCREEN_WRT_FREQ_INNER= 10 |
| 92 | +OUTPUT_WRT_FREQ= 10 |
0 commit comments