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| 1 | +%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% |
| 2 | +% % |
| 3 | +% SU2 configuration file % |
| 4 | +% Case description: 2D cylinder array with CHT couplings % |
| 5 | +% Author: O. Burghardt, T. Economon % |
| 6 | +% Institution: Chair for Scientific Computing, TU Kaiserslautern % |
| 7 | +% Date: August 8, 2019 % |
| 8 | +% File Version 6.0.1 "Falcon" % |
| 9 | +% % |
| 10 | +%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% |
| 11 | + |
| 12 | +% |
| 13 | +% Physical governing equations (EULER, NAVIER_STOKES, |
| 14 | +% WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY, |
| 15 | +% POISSON_EQUATION) |
| 16 | +SOLVER= MULTIPHYSICS |
| 17 | +% |
| 18 | +% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT) |
| 19 | +MATH_PROBLEM= DIRECT |
| 20 | +% |
| 21 | +% |
| 22 | +CONFIG_LIST = (flow_cylinder.cfg, solid_cylinder1.cfg, solid_cylinder2.cfg, solid_cylinder3.cfg) |
| 23 | +% |
| 24 | +% |
| 25 | +MARKER_ZONE_INTERFACE= (cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3) |
| 26 | +% |
| 27 | +% |
| 28 | +MARKER_CHT_INTERFACE= (cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3) |
| 29 | +% |
| 30 | +% |
| 31 | +TIME_DOMAIN = YES |
| 32 | +% |
| 33 | +% |
| 34 | +TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER |
| 35 | +% |
| 36 | +% |
| 37 | +TIME_STEP= 0.05 |
| 38 | +% |
| 39 | +% |
| 40 | +MAX_TIME= 100.0 |
| 41 | +% |
| 42 | +% |
| 43 | +TIME_ITER= 2000 |
| 44 | +% |
| 45 | +% Number of total iterations |
| 46 | +OUTER_ITER = 100 |
| 47 | +% |
| 48 | +% Courant-Friedrichs-Lewy condition of the finest grid |
| 49 | +CFL_NUMBER= 100.0 |
| 50 | +% |
| 51 | +% Mesh input file |
| 52 | +MESH_FILENAME= mesh_cht_3cyl.su2 |
| 53 | +% |
| 54 | +% Mesh input file format (SU2, CGNS, NETCDF_ASCII) |
| 55 | +MESH_FORMAT= SU2 |
| 56 | +% |
| 57 | +% |
| 58 | +HISTORY_OUTPUT= (ITER, BGS_RES[0], BGS_RES[1], BGS_RES[2], BGS_RES[3], HEAT[0], AERO_COEFF[0]) |
| 59 | +% |
| 60 | +% |
| 61 | +OUTPUT_FILES=(RESTART, PARAVIEW_MULTIBLOCK) |
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