@@ -30,84 +30,45 @@ REF_ORIGIN_MOMENT_Z = 0.00
3030REF_LENGTH = 1.0
3131REF_AREA = 1.0
3232
33- % ------------------------ SUPERSONIC SIMULATION ------------------------------%
34- %
35- EQUIV_AREA = YES
36- EA_INT_LIMIT = ( -100.0, 100.0, 2.0 )
37-
3833% ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
3934%
4035MARKER_EULER = ( airfoil )
41- MARKER_FAR = ( farfield )
42- MARKER_NEARFIELD = ( upper_nearfield, lower_nearfield )
36+ MARKER_FAR = ( farfield, upper_nearfield, lower_nearfield )
4337MARKER_PLOTTING = ( airfoil )
44- MARKER_MONITORING = ( airfoil, upper_nearfield )
38+ MARKER_MONITORING = ( airfoil )
4539
4640% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
4741%
4842NUM_METHOD_GRAD = GREEN_GAUSS
49- CFL_NUMBER = 25.0
50- CFL_ADAPT = NO
51- CFL_ADAPT_PARAM = ( 1.5, 0.5, 1.0, 100.0 )
52- RK_ALPHA_COEFF = ( 0.66667, 0.66667, 1.000000 )
53- EXT_ITER = 99999999
43+ CFL_NUMBER = 2.0
44+ CFL_ADAPT = YES
45+ CFL_ADAPT_PARAM = ( 0.5, 1.5, 1.0, 50.0 )
46+ ITER = 25
5447
5548% -------------------------- MULTIGRID PARAMETERS -----------------------------%
5649%
57- MGLEVEL = 3
58- MGCYCLE = V_CYCLE
59- MG_PRE_SMOOTH = ( 4, 4, 4, 4 )
60- MG_POST_SMOOTH = ( 4, 4, 4, 4 )
61- MG_CORRECTION_SMOOTH = ( 1, 1, 1, 1 )
62- MG_DAMP_RESTRICTION = 0.5
63- MG_DAMP_PROLONGATION = 0.5
50+ MGLEVEL = 0
6451
6552% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
6653%
67- CONV_NUM_METHOD_FLOW = JST
68- VENKAT_LIMITER_COEFF = 0.03
69- JST_SENSOR_COEFF = ( 0.5, 0.02 )
54+ CONV_NUM_METHOD_FLOW = ROE
55+ MUSCL_FLOW = YES
56+ SLOPE_LIMITER_FLOW = VENKATAKRISHNAN
57+ VENKAT_LIMITER_COEFF = 0.05
7058TIME_DISCRE_FLOW = EULER_IMPLICIT
7159
72- % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
73- %
74- OBJECTIVE_FUNCTION = EQUIVALENT_AREA
75- CONV_NUM_METHOD_ADJFLOW = JST
76- ADJ_SHARP_LIMITER_COEFF = 3.0
77- ADJ_JST_SENSOR_COEFF = ( 0.0, 0.02 )
78- CFL_REDUCTION_ADJFLOW = 0.8
79- TIME_DISCRE_ADJFLOW = EULER_IMPLICIT
80-
81- % ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
82- %
83- DV_KIND = PARABOLIC
84- DV_MARKER = ( airfoil )
85- DV_PARAM = ( 0.5, 5 )
86- DV_VALUE = 0.01
87- HOLD_GRID_FIXED = YES
88- HOLD_GRID_FIXED_COORD = ( -0.2, -0.4, 0.0, 2.2, 0.4, 0.0 )
89-
9060% --------------------------- CONVERGENCE PARAMETERS --------------------------%
9161%
9262CONV_RESIDUAL_MINVAL = -6
9363CONV_STARTITER = 10
94- CONV_CAUCHY_ELEMS = 100
95- CONV_CAUCHY_EPS = 1E-10
9664
9765% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
9866%
9967MESH_FILENAME = mesh_BIPARABOLIC_sup.su2
10068MESH_FORMAT = SU2
101- MESH_OUT_FILENAME = mesh_out
102- SOLUTION_FILENAME = solution_flow
103- SOLUTION_ADJ_FILENAME = solution_adj
10469TABULAR_FORMAT = CSV
10570CONV_FILENAME = history
10671RESTART_FILENAME = restart_flow
107- RESTART_ADJ_FILENAME = restart_adj
10872VOLUME_FILENAME = volume_flow
109- VOLUME_ADJ_FILENAME = volume_adjoint
110- GRAD_OBJFUNC_FILENAME = of_grad
11173SURFACE_FILENAME = surface_flow
112- SURFACE_ADJ_FILENAME = surface_adjoint
113- OUTPUT_WRT_FREQ = 100
74+ OUTPUT_WRT_FREQ = 500
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