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Adapted tutorial cases
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26 files changed

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-132
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26 files changed

+192
-132
lines changed

‎Inc_Inviscid_Hydrofoil/inv_naca0012.cfg‎

Lines changed: 8 additions & 5 deletions
Original file line numberDiff line numberDiff line change
@@ -99,7 +99,7 @@ CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
9999
RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
100100
%
101101
% Number of total iterations
102-
EXT_ITER= 9999
102+
ITER= 9999
103103

104104
% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
105105
%
@@ -188,7 +188,7 @@ MESH_FILENAME= mesh_NACA0012_5deg_6814.su2
188188
MESH_FORMAT= SU2
189189
%
190190
% Restart flow input file
191-
SOLUTION_FLOW_FILENAME= solution_flow.dat
191+
SOLUTION_FILENAME= solution_flow.dat
192192
%
193193
% Output file format (PARAVIEW, TECPLOT)
194194
OUTPUT_FORMAT= PARAVIEW
@@ -197,16 +197,19 @@ OUTPUT_FORMAT= PARAVIEW
197197
CONV_FILENAME= history
198198
%
199199
% Output file restart flow
200-
RESTART_FLOW_FILENAME= restart_flow.dat
200+
RESTART_FILENAME= restart_flow.dat
201201
%
202202
% Output file flow (w/o extension) variables
203-
VOLUME_FLOW_FILENAME= flow
203+
VOLUME_FILENAME= flow
204204
%
205205
% Output file surface flow coefficient (w/o extension)
206-
SURFACE_FLOW_FILENAME= surface_flow
206+
SURFACE_FILENAME= surface_flow
207207
%
208208
% Writing solution file frequency
209209
WRT_SOL_FREQ= 50
210210
%
211211
% Writing convergence history frequency
212212
WRT_CON_FREQ= 1
213+
%
214+
% Screen output
215+
SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_VELOCITY-X, LIFT, DRAG)

‎Inc_Laminar_Cavity/lam_buoyancy_cavity.cfg‎

Lines changed: 8 additions & 6 deletions
Original file line numberDiff line numberDiff line change
@@ -138,7 +138,7 @@ MAX_DELTA_TIME= 1E6
138138
RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
139139
%
140140
% Number of total iterations
141-
EXT_ITER= 99999
141+
ITER= 99999
142142

143143
% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
144144
%
@@ -234,7 +234,7 @@ MESH_FORMAT= SU2
234234
MESH_OUT_FILENAME= mesh_out.su2
235235
%
236236
% Restart flow input file
237-
SOLUTION_FLOW_FILENAME= solution_flow.dat
237+
SOLUTION_FILENAME= solution_flow.dat
238238
%
239239
% Restart adjoint input file
240240
SOLUTION_ADJ_FILENAME= solution_adj.dat
@@ -246,13 +246,13 @@ OUTPUT_FORMAT= PARAVIEW
246246
CONV_FILENAME= history
247247
%
248248
% Output file restart flow
249-
RESTART_FLOW_FILENAME= restart_flow.dat
249+
RESTART_FILENAME= restart_flow.dat
250250
%
251251
% Output file restart adjoint
252252
RESTART_ADJ_FILENAME= restart_adj.dat
253253
%
254254
% Output file flow (w/o extension) variables
255-
VOLUME_FLOW_FILENAME= flow
255+
VOLUME_FILENAME= flow
256256
%
257257
% Output file adjoint (w/o extension) variables
258258
VOLUME_ADJ_FILENAME= adjoint
@@ -261,7 +261,7 @@ VOLUME_ADJ_FILENAME= adjoint
261261
GRAD_OBJFUNC_FILENAME= of_grad.dat
262262
%
263263
% Output file surface flow coefficient (w/o extension)
264-
SURFACE_FLOW_FILENAME= surface_flow
264+
SURFACE_FILENAME= surface_flow
265265
%
266266
% Output file surface adjoint coefficient (w/o extension)
267267
SURFACE_ADJ_FILENAME= surface_adjoint
@@ -271,7 +271,9 @@ WRT_SOL_FREQ= 100
271271
%
272272
% Writing convergence history frequency
273273
WRT_CON_FREQ= 1
274-
274+
%
275+
% Screen output
276+
SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_VELOCITY-X, LIFT, DRAG)
275277
% ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
276278
%
277279
% Extract a slice using GEO_BOUNDS (works with 2D cartesian grids only)

‎Inc_Laminar_Flat_Plate/lam_flatplate.cfg‎

Lines changed: 8 additions & 5 deletions
Original file line numberDiff line numberDiff line change
@@ -145,7 +145,7 @@ CFL_ADAPT= NO
145145
CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
146146
%
147147
% Number of total iterations
148-
EXT_ITER= 99999
148+
ITER= 99999
149149

150150
% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
151151
%
@@ -246,7 +246,7 @@ MESH_FORMAT= SU2
246246
MESH_OUT_FILENAME= mesh_out.su2
247247
%
248248
% Restart flow input file
249-
SOLUTION_FLOW_FILENAME= solution_flow.dat
249+
SOLUTION_FILENAME= solution_flow.dat
250250
%
251251
% Restart adjoint input file
252252
SOLUTION_ADJ_FILENAME= solution_adj.dat
@@ -258,13 +258,13 @@ OUTPUT_FORMAT= PARAVIEW
258258
CONV_FILENAME= history
259259
%
260260
% Output file restart flow
261-
RESTART_FLOW_FILENAME= restart_flow.dat
261+
RESTART_FILENAME= restart_flow.dat
262262
%
263263
% Output file restart adjoint
264264
RESTART_ADJ_FILENAME= restart_adj.dat
265265
%
266266
% Output file flow (w/o extension) variables
267-
VOLUME_FLOW_FILENAME= flow
267+
VOLUME_FILENAME= flow
268268
%
269269
% Output file adjoint (w/o extension) variables
270270
VOLUME_ADJ_FILENAME= adjoint
@@ -273,7 +273,7 @@ VOLUME_ADJ_FILENAME= adjoint
273273
GRAD_OBJFUNC_FILENAME= of_grad.dat
274274
%
275275
% Output file surface flow coefficient (w/o extension)
276-
SURFACE_FLOW_FILENAME= surface_flow
276+
SURFACE_FILENAME= surface_flow
277277
%
278278
% Output file surface adjoint coefficient (w/o extension)
279279
SURFACE_ADJ_FILENAME= surface_adjoint
@@ -283,6 +283,9 @@ WRT_SOL_FREQ= 250
283283
%
284284
% Writing convergence history frequency
285285
WRT_CON_FREQ= 1
286+
%
287+
% Screen output
288+
SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_VELOCITY-X, LIFT, DRAG)
286289
287290
% ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
288291
%

‎Inc_Laminar_Step/lam_backwardstep.cfg‎

Lines changed: 8 additions & 5 deletions
Original file line numberDiff line numberDiff line change
@@ -119,7 +119,7 @@ MAX_DELTA_TIME= 1E30
119119
RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
120120
%
121121
% Number of total iterations
122-
EXT_ITER= 99999
122+
ITER= 99999
123123

124124
% ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
125125
%
@@ -231,7 +231,7 @@ MESH_FORMAT= SU2
231231
MESH_OUT_FILENAME= mesh_out.su2
232232
%
233233
% Restart flow input file
234-
SOLUTION_FLOW_FILENAME= solution_flow.dat
234+
SOLUTION_FILENAME= solution_flow.dat
235235
%
236236
% Restart adjoint input file
237237
SOLUTION_ADJ_FILENAME= solution_adj.dat
@@ -243,13 +243,13 @@ OUTPUT_FORMAT= PARAVIEW
243243
CONV_FILENAME= history
244244
%
245245
% Output file restart flow
246-
RESTART_FLOW_FILENAME= restart_flow.dat
246+
RESTART_FILENAME= restart_flow.dat
247247
%
248248
% Output file restart adjoint
249249
RESTART_ADJ_FILENAME= restart_adj.dat
250250
%
251251
% Output file flow (w/o extension) variables
252-
VOLUME_FLOW_FILENAME= flow
252+
VOLUME_FILENAME= flow
253253
%
254254
% Output file adjoint (w/o extension) variables
255255
VOLUME_ADJ_FILENAME= adjoint
@@ -258,7 +258,7 @@ VOLUME_ADJ_FILENAME= adjoint
258258
GRAD_OBJFUNC_FILENAME= of_grad.dat
259259
%
260260
% Output file surface flow coefficient (w/o extension)
261-
SURFACE_FLOW_FILENAME= surface_flow
261+
SURFACE_FILENAME= surface_flow
262262
%
263263
% Output file surface adjoint coefficient (w/o extension)
264264
SURFACE_ADJ_FILENAME= surface_adjoint
@@ -268,6 +268,9 @@ WRT_SOL_FREQ= 250
268268
%
269269
% Writing convergence history frequency
270270
WRT_CON_FREQ= 1
271+
%
272+
% Screen output
273+
SCREEN_OUTPUT=(INNER_ITER, RMS_PRESSURE, RMS_VELOCITY-X, LIFT, DRAG)
271274

272275
% ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
273276
%

‎Inc_Turbulent_Flat_Plate/turb_flatplate.cfg‎

Lines changed: 8 additions & 5 deletions
Original file line numberDiff line numberDiff line change
@@ -113,7 +113,7 @@ CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
113113
RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
114114
%
115115
% Number of total iterations
116-
EXT_ITER= 99999
116+
ITER= 99999
117117

118118
% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
119119
%
@@ -237,7 +237,7 @@ MESH_FORMAT= SU2
237237
MESH_OUT_FILENAME= mesh_out.su2
238238
%
239239
% Restart flow input file
240-
SOLUTION_FLOW_FILENAME= solution_flow.dat
240+
SOLUTION_FILENAME= solution_flow.dat
241241
%
242242
% Restart adjoint input file
243243
SOLUTION_ADJ_FILENAME= solution_adj.dat
@@ -249,13 +249,13 @@ OUTPUT_FORMAT= PARAVIEW
249249
CONV_FILENAME= history
250250
%
251251
% Output file restart flow
252-
RESTART_FLOW_FILENAME= restart_flow.dat
252+
RESTART_FILENAME= restart_flow.dat
253253
%
254254
% Output file restart adjoint
255255
RESTART_ADJ_FILENAME= restart_adj.dat
256256
%
257257
% Output file flow (w/o extension) variables
258-
VOLUME_FLOW_FILENAME= flow
258+
VOLUME_FILENAME= flow
259259
%
260260
% Output file adjoint (w/o extension) variables
261261
VOLUME_ADJ_FILENAME= adjoint
@@ -264,7 +264,7 @@ VOLUME_ADJ_FILENAME= adjoint
264264
GRAD_OBJFUNC_FILENAME= of_grad.dat
265265
%
266266
% Output file surface flow coefficient (w/o extension)
267-
SURFACE_FLOW_FILENAME= surface_flow
267+
SURFACE_FILENAME= surface_flow
268268
%
269269
% Output file surface adjoint coefficient (w/o extension)
270270
SURFACE_ADJ_FILENAME= surface_adjoint
@@ -274,6 +274,9 @@ WRT_SOL_FREQ= 250
274274
%
275275
% Writing convergence history frequency
276276
WRT_CON_FREQ= 1
277+
%
278+
% Screen output
279+
SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_NU_TILDE, LIFT, DRAG)
277280

278281
% ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
279282
%

‎Inc_Turbulent_NACA0012/turb_naca0012.cfg‎

Lines changed: 9 additions & 5 deletions
Original file line numberDiff line numberDiff line change
@@ -113,7 +113,7 @@ MAX_DELTA_TIME= 1E6
113113
RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
114114
%
115115
% Number of total iterations
116-
EXT_ITER= 99999
116+
ITER= 99999
117117

118118
% ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
119119
%
@@ -240,7 +240,7 @@ MESH_FORMAT= SU2
240240
MESH_OUT_FILENAME= mesh_out.su2
241241
%
242242
% Restart flow input file
243-
SOLUTION_FLOW_FILENAME= solution_flow.dat
243+
SOLUTION_FILENAME= solution_flow.dat
244244
%
245245
% Restart adjoint input file
246246
SOLUTION_ADJ_FILENAME= solution_adj.dat
@@ -252,13 +252,13 @@ OUTPUT_FORMAT= PARAVIEW
252252
CONV_FILENAME= history
253253
%
254254
% Output file restart flow
255-
RESTART_FLOW_FILENAME= restart_flow.dat
255+
RESTART_FILENAME= restart_flow.dat
256256
%
257257
% Output file restart adjoint
258258
RESTART_ADJ_FILENAME= restart_adj.dat
259259
%
260260
% Output file flow (w/o extension) variables
261-
VOLUME_FLOW_FILENAME= flow
261+
VOLUME_FILENAME= flow
262262
%
263263
% Output file adjoint (w/o extension) variables
264264
VOLUME_ADJ_FILENAME= adjoint
@@ -267,7 +267,7 @@ VOLUME_ADJ_FILENAME= adjoint
267267
GRAD_OBJFUNC_FILENAME= of_grad.dat
268268
%
269269
% Output file surface flow coefficient (w/o extension)
270-
SURFACE_FLOW_FILENAME= surface_flow
270+
SURFACE_FILENAME= surface_flow
271271
%
272272
% Output file surface adjoint coefficient (w/o extension)
273273
SURFACE_ADJ_FILENAME= surface_adjoint
@@ -277,3 +277,7 @@ WRT_SOL_FREQ= 250
277277
%
278278
% Writing convergence history frequency
279279
WRT_CON_FREQ= 1
280+
%
281+
% Screen output
282+
SCREEN_OUTPUT = (INNER_ITER, RMS_PRESSURE, RMS_NU_TILDE, LIFT, DRAG)
283+

‎Inviscid_2D_Unconstrained_NACA0012/inv_NACA0012_basic.cfg‎

Lines changed: 8 additions & 5 deletions
Original file line numberDiff line numberDiff line change
@@ -88,7 +88,7 @@ CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
8888
RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
8989
%
9090
% Number of total iterations
91-
EXT_ITER= 1000
91+
ITER= 1000
9292

9393
% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
9494
%
@@ -258,7 +258,7 @@ MESH_FORMAT= SU2
258258
MESH_OUT_FILENAME= mesh_out.su2
259259
%
260260
% Restart flow input file
261-
SOLUTION_FLOW_FILENAME= solution_flow.dat
261+
SOLUTION_FILENAME= solution_flow.dat
262262
%
263263
% Restart adjoint input file
264264
SOLUTION_ADJ_FILENAME= solution_adj.dat
@@ -270,13 +270,13 @@ OUTPUT_FORMAT= TECPLOT
270270
CONV_FILENAME= history
271271
%
272272
% Output file restart flow
273-
RESTART_FLOW_FILENAME= restart_flow.dat
273+
RESTART_FILENAME= restart_flow.dat
274274
%
275275
% Output file restart adjoint
276276
RESTART_ADJ_FILENAME= restart_adj.dat
277277
%
278278
% Output file flow (w/o extension) variables
279-
VOLUME_FLOW_FILENAME= flow
279+
VOLUME_FILENAME= flow
280280
%
281281
% Output file adjoint (w/o extension) variables
282282
VOLUME_ADJ_FILENAME= adjoint
@@ -285,7 +285,7 @@ VOLUME_ADJ_FILENAME= adjoint
285285
GRAD_OBJFUNC_FILENAME= of_grad.dat
286286
%
287287
% Output file surface flow coefficient (w/o extension)
288-
SURFACE_FLOW_FILENAME= surface_flow
288+
SURFACE_FILENAME= surface_flow
289289
%
290290
% Output file surface adjoint coefficient (w/o extension)
291291
SURFACE_ADJ_FILENAME= surface_adjoint
@@ -304,6 +304,9 @@ WRT_CON_FREQ_DUALTIME= 10
304304
%
305305
% Output rind layers in the solution files
306306
WRT_HALO= NO
307+
%
308+
% Screen output
309+
SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
307310

308311
% --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
309312
% Available flow based objective functions or constraint functions

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