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jayantmukhojayantmukho
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Merge pull request #16 from su2code/enhancement_fixed_cl
Changing tutorial for fixed CL mode and updating DV definition values
2 parents 54fed59 + 0b617df commit 69d284d

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‎Inviscid_2D_Unconstrained_NACA0012/inv_NACA0012_basic.cfg‎

Lines changed: 28 additions & 14 deletions
Original file line numberDiff line numberDiff line change
@@ -301,12 +301,17 @@ WRT_HALO= NO
301301
SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
302302

303303
% --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
304+
%
304305
% Available flow based objective functions or constraint functions
305-
% DRAG, LIFT, SIDEFORCE, EFFICIENCY,
306+
% DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET,
306307
% FORCE_X, FORCE_Y, FORCE_Z,
307308
% MOMENT_X, MOMENT_Y, MOMENT_Z,
308309
% THRUST, TORQUE, FIGURE_OF_MERIT,
309310
% EQUIVALENT_AREA, NEARFIELD_PRESSURE,
311+
% TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
312+
% INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
313+
% SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
314+
% SURFACE_STATIC_PRESSURE, SURFACE_MACH
310315
%
311316
% Available geometrical based objective functions or constraint functions
312317
% AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
@@ -315,18 +320,27 @@ SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
315320
% STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
316321
%
317322
% Available design variables
318-
% HICKS_HENNE ( 1, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
319-
% SPHERICAL ( 3, Scale | Mark. List | ControlPoint_Index, Theta_Disp, R_Disp )
320-
% NACA_4DIGITS ( 4, Scale | Mark. List | 1st digit, 2nd digit, 3rd and 4th digit )
321-
% DISPLACEMENT ( 5, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
322-
% ROTATION ( 6, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
323-
% FFD_CONTROL_POINT ( 7, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
324-
% FFD_TWIST ( 9, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
325-
% FFD_ROTATION ( 10, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
326-
% FFD_CAMBER ( 11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
327-
% FFD_THICKNESS ( 12, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
328-
% FFD_VOLUME ( 13, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
329-
% FOURIER ( 14, Scale | Mark. List | Lower(0)/Upper(1) side, index, cos(0)/sin(1) )
323+
% 2D Design variables
324+
% FFD_CONTROL_POINT_2D ( 19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
325+
% FFD_CAMBER_2D ( 20, Scale | Mark. List | FFD_BoxTag, i_Ind )
326+
% FFD_THICKNESS_2D ( 21, Scale | Mark. List | FFD_BoxTag, i_Ind )
327+
% FFD_TWIST_2D ( 22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
328+
% HICKS_HENNE ( 30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
329+
% ANGLE_OF_ATTACK ( 101, Scale | Mark. List | 1.0 )
330+
%
331+
% 3D Design variables
332+
% FFD_CONTROL_POINT ( 11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
333+
% FFD_NACELLE ( 12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
334+
% FFD_GULL ( 13, Scale | Mark. List | FFD_BoxTag, j_Ind )
335+
% FFD_CAMBER ( 14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
336+
% FFD_TWIST ( 15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
337+
% FFD_THICKNESS ( 16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
338+
% FFD_ROTATION ( 18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
339+
% FFD_ANGLE_OF_ATTACK ( 24, Scale | Mark. List | FFD_BoxTag, 1.0 )
340+
%
341+
% Global design variables
342+
% TRANSLATION ( 1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
343+
% ROTATION ( 2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
330344
%
331345
% Optimization objective function with scaling factor, separated by semicolons.
332346
% To include quadratic penalty function: use OPT_CONSTRAINT option syntax within the OPT_OBJECTIVE list.
@@ -359,4 +373,4 @@ OPT_BOUND_UPPER= 0.1
359373
OPT_BOUND_LOWER= -0.1
360374
%
361375
% Optimization design variables, separated by semicolons
362-
DEFINITION_DV= ( 1, 1.0 | airfoil | 0, 0.05 ); ( 1, 1.0 | airfoil | 0, 0.10 ); ( 1, 1.0 | airfoil | 0, 0.15 ); ( 1, 1.0 | airfoil | 0, 0.20 ); ( 1, 1.0 | airfoil | 0, 0.25 ); ( 1, 1.0 | airfoil | 0, 0.30 ); ( 1, 1.0 | airfoil | 0, 0.35 ); ( 1, 1.0 | airfoil | 0, 0.40 ); ( 1, 1.0 | airfoil | 0, 0.45 ); ( 1, 1.0 | airfoil | 0, 0.50 ); ( 1, 1.0 | airfoil | 0, 0.55 ); ( 1, 1.0 | airfoil | 0, 0.60 ); ( 1, 1.0 | airfoil | 0, 0.65 ); ( 1, 1.0 | airfoil | 0, 0.70 ); ( 1, 1.0 | airfoil | 0, 0.75 ); ( 1, 1.0 | airfoil | 0, 0.80 ); ( 1, 1.0 | airfoil | 0, 0.85 ); ( 1, 1.0 | airfoil | 0, 0.90 ); ( 1, 1.0 | airfoil | 0, 0.95 ); ( 1, 1.0 | airfoil | 1, 0.05 ); ( 1, 1.0 | airfoil | 1, 0.10 ); ( 1, 1.0 | airfoil | 1, 0.15 ); ( 1, 1.0 | airfoil | 1, 0.20 ); ( 1, 1.0 | airfoil | 1, 0.25 ); ( 1, 1.0 | airfoil | 1, 0.30 ); ( 1, 1.0 | airfoil | 1, 0.35 ); ( 1, 1.0 | airfoil | 1, 0.40 ); ( 1, 1.0 | airfoil | 1, 0.45 ); ( 1, 1.0 | airfoil | 1, 0.50 ); ( 1, 1.0 | airfoil | 1, 0.55 ); ( 1, 1.0 | airfoil | 1, 0.60 ); ( 1, 1.0 | airfoil | 1, 0.65 ); ( 1, 1.0 | airfoil | 1, 0.70 ); ( 1, 1.0 | airfoil | 1, 0.75 ); ( 1, 1.0 | airfoil | 1, 0.80 ); ( 1, 1.0 | airfoil | 1, 0.85 ); ( 1, 1.0 | airfoil | 1, 0.90 ); ( 1, 1.0 | airfoil | 1, 0.95 )
376+
DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )

‎Inviscid_3D_Constrained_ONERAM6/inv_ONERAM6_adv.cfg‎

Lines changed: 32 additions & 21 deletions
Large diffs are not rendered by default.

‎Multi_Objective_Shape_Design/inv_wedge_ROE_multiobj_combo.cfg‎

Lines changed: 27 additions & 19 deletions
Original file line numberDiff line numberDiff line change
@@ -346,15 +346,17 @@ DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
346346

347347
% --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
348348
%
349+
%
349350
% Available flow based objective functions or constraint functions
350-
% DRAG, LIFT, SIDEFORCE, EFFICIENCY,
351+
% DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET,
351352
% FORCE_X, FORCE_Y, FORCE_Z,
352353
% MOMENT_X, MOMENT_Y, MOMENT_Z,
353354
% THRUST, TORQUE, FIGURE_OF_MERIT,
354-
% EQUIVALENT_AREA, NEARFIELD_PRESSURE,
355+
% EQUIVALENT_AREA, NEARFIELD_PRESSURE,
355356
% TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
356357
% INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
357-
% FREE_SURFACE, SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
358+
% SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
359+
% SURFACE_STATIC_PRESSURE, SURFACE_MACH
358360
%
359361
% Available geometrical based objective functions or constraint functions
360362
% AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
@@ -363,21 +365,27 @@ DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
363365
% STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
364366
%
365367
% Available design variables
366-
% HICKS_HENNE ( 1, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
367-
% SPHERICAL ( 3, Scale | Mark. List | ControlPoint_Index, Theta_Disp, R_Disp )
368-
% NACA_4DIGITS ( 4, Scale | Mark. List | 1st digit, 2nd digit, 3rd and 4th digit )
369-
% DISPLACEMENT ( 5, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
370-
% ROTATION ( 6, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
371-
% FFD_CONTROL_POINT ( 7, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
372-
% FFD_TWIST ( 9, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
373-
% FFD_ROTATION ( 10, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
374-
% FFD_CAMBER ( 11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
375-
% FFD_THICKNESS ( 12, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
376-
% FOURIER ( 14, Scale | Mark. List | Lower(0)/Upper(1) side, index, cos(0)/sin(1) )
377-
% FFD_CONTROL_POINT_2D ( 15, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
378-
% FFD_CAMBER_2D ( 16, Scale | Mark. List | FFD_BoxTag, i_Ind )
379-
% FFD_THICKNESS_2D ( 17, Scale | Mark. List | FFD_BoxTag, i_Ind )
380-
% FFD_CONTROL_SURFACE ( 18, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
368+
% 2D Design variables
369+
% FFD_CONTROL_POINT_2D ( 19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
370+
% FFD_CAMBER_2D ( 20, Scale | Mark. List | FFD_BoxTag, i_Ind )
371+
% FFD_THICKNESS_2D ( 21, Scale | Mark. List | FFD_BoxTag, i_Ind )
372+
% FFD_TWIST_2D ( 22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
373+
% HICKS_HENNE ( 30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
374+
% ANGLE_OF_ATTACK ( 101, Scale | Mark. List | 1.0 )
375+
%
376+
% 3D Design variables
377+
% FFD_CONTROL_POINT ( 11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
378+
% FFD_NACELLE ( 12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
379+
% FFD_GULL ( 13, Scale | Mark. List | FFD_BoxTag, j_Ind )
380+
% FFD_CAMBER ( 14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
381+
% FFD_TWIST ( 15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
382+
% FFD_THICKNESS ( 16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
383+
% FFD_ROTATION ( 18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
384+
% FFD_ANGLE_OF_ATTACK ( 24, Scale | Mark. List | FFD_BoxTag, 1.0 )
385+
%
386+
% Global design variables
387+
% TRANSLATION ( 1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
388+
% ROTATION ( 2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
381389
%
382390
% Optimization objective function with scaling factor, separated by semicolons.
383391
% To include quadratic penalty function: use OPT_CONSTRAINT option syntax within the OPT_OBJECTIVE list.
@@ -404,5 +412,5 @@ OPT_BOUND_UPPER= 0.1
404412
OPT_BOUND_LOWER= -0.1
405413
%
406414
% Optimization design variables, separated by semicolons
407-
DEFINITION_DV= (15, 1.0| lower | MAIN_BOX, 3,0,0,1.0);(15, 1.0| lower | MAIN_BOX, 4,0,0,1.0);(15, 1.0| lower | MAIN_BOX, 5,0,0,1.0);(15, 1.0| lower | MAIN_BOX, 6,0,0,1.0)
415+
DEFINITION_DV= ( 19, 1.0| lower | MAIN_BOX, 3,0,0,1.0);( 19, 1.0| lower | MAIN_BOX, 4,0,0,1.0);( 19, 1.0| lower | MAIN_BOX, 5,0,0,1.0);( 19, 1.0| lower | MAIN_BOX, 6,0,0,1.0)
408416

‎Turbulent_2D_Constrained_RAE2822/turb_SA_RAE2822.cfg‎

Lines changed: 28 additions & 18 deletions
Original file line numberDiff line numberDiff line change
@@ -42,7 +42,7 @@ REYNOLDS_NUMBER= 6.5E6
4242
% Reynolds length (1 m by default)
4343
REYNOLDS_LENGTH= 1.0
4444

45-
% -------------------------- CL & CM DRIVER DEFINITION ------------------------%
45+
% -------------------------- CL DRIVER DEFINITION -----------------------------%
4646
%
4747
% Activate fixed lift mode (specify a CL instead of AoA, NO/YES)
4848
FIXED_CL_MODE= YES
@@ -53,8 +53,8 @@ TARGET_CL= 0.724
5353
% Estimation of dCL/dAlpha (0.2 per degree by default)
5454
DCL_DALPHA= 0.2
5555
%
56-
% Number of times the AoA is updated in a fix CL problem (5 by default)
57-
UPDATE_ALPHA= 5
56+
% Maximum number of iterations between AoA updates
57+
UPDATE_AOA_ITER_LIMIT= 100
5858
%
5959
% Number of iterations to evaluate dCL/dAlpha at the end of the simulation
6060
ITER_DCL_DALPHA= 500
@@ -226,10 +226,8 @@ GEO_MODE= FUNCTION
226226
% --------------------------- CONVERGENCE PARAMETERS --------------------------%
227227
%
228228
% Convergence criteria (CAUCHY, RESIDUAL)
229-
%
230229
CONV_CRITERIA= RESIDUAL
231230
%
232-
%
233231
% Min value of the residual (log10 of the residual)
234232
CONV_RESIDUAL_MINVAL= -12
235233
%
@@ -364,17 +362,29 @@ OPT_BOUND_UPPER= 1E10
364362
% Lower bound for each design variable (bound in the python optimizer)
365363
OPT_BOUND_LOWER= -1E10
366364
367-
% List of design variables (Design variables are separated by semicolons)
368-
% - HICKS_HENNE ( 1, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
369-
% - NACA_4DIGITS ( 4, Scale | Mark. List | 1st digit, 2nd digit, 3rd and 4th digit )
370-
% - DISPLACEMENT ( 5, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
371-
% - ROTATION ( 6, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
372-
% - FFD_CONTROL_POINT ( 7, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
373-
% - FFD_DIHEDRAL_ANGLE ( 8, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
374-
% - FFD_TWIST_ANGLE ( 9, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
375-
% - FFD_ROTATION ( 10, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
376-
% - FFD_CAMBER ( 11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
377-
% - FFD_THICKNESS ( 12, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
378-
% - FFD_VOLUME ( 13, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
379-
DEFINITION_DV= ( 1, 1.0 | AIRFOIL | 0, 0.05 ); ( 1, 1.0 | AIRFOIL | 0, 0.10 ); ( 1, 1.0 | AIRFOIL | 0, 0.15 ); ( 1, 1.0 | AIRFOIL | 0, 0.20 ); ( 1, 1.0 | AIRFOIL | 0, 0.25 ); ( 1, 1.0 | AIRFOIL | 0, 0.30 ); ( 1, 1.0 | AIRFOIL | 0, 0.35 ); ( 1, 1.0 | AIRFOIL | 0, 0.40 ); ( 1, 1.0 | AIRFOIL | 0, 0.45 ); ( 1, 1.0 | AIRFOIL | 0, 0.50 ); ( 1, 1.0 | AIRFOIL | 0, 0.55 ); ( 1, 1.0 | AIRFOIL | 0, 0.60 ); ( 1, 1.0 | AIRFOIL | 0, 0.65 ); ( 1, 1.0 | AIRFOIL | 0, 0.70 ); ( 1, 1.0 | AIRFOIL | 0, 0.75 ); ( 1, 1.0 | AIRFOIL | 0, 0.80 ); ( 1, 1.0 | AIRFOIL | 0, 0.85 ); ( 1, 1.0 | AIRFOIL | 0, 0.90 ); ( 1, 1.0 | AIRFOIL | 0, 0.95 ); ( 1, 1.0 | AIRFOIL | 1, 0.05 ); ( 1, 1.0 | AIRFOIL | 1, 0.10 ); ( 1, 1.0 | AIRFOIL | 1, 0.15 ); ( 1, 1.0 | AIRFOIL | 1, 0.20 ); ( 1, 1.0 | AIRFOIL | 1, 0.25 ); ( 1, 1.0 | AIRFOIL | 1, 0.30 ); ( 1, 1.0 | AIRFOIL | 1, 0.35 ); ( 1, 1.0 | AIRFOIL | 1, 0.40 ); ( 1, 1.0 | AIRFOIL | 1, 0.45 ); ( 1, 1.0 | AIRFOIL | 1, 0.50 ); ( 1, 1.0 | AIRFOIL | 1, 0.55 ); ( 1, 1.0 | AIRFOIL | 1, 0.60 ); ( 1, 1.0 | AIRFOIL | 1, 0.65 ); ( 1, 1.0 | AIRFOIL | 1, 0.70 ); ( 1, 1.0 | AIRFOIL | 1, 0.75 ); ( 1, 1.0 | AIRFOIL | 1, 0.80 ); ( 1, 1.0 | AIRFOIL | 1, 0.85 ); ( 1, 1.0 | AIRFOIL | 1, 0.90 ); ( 1, 1.0 | AIRFOIL | 1, 0.95 )
365+
% List of available design variables (Design variables are separated by semicolons)
366+
%
367+
% 2D Design variables
368+
% FFD_CONTROL_POINT_2D ( 19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
369+
% FFD_CAMBER_2D ( 20, Scale | Mark. List | FFD_BoxTag, i_Ind )
370+
% FFD_THICKNESS_2D ( 21, Scale | Mark. List | FFD_BoxTag, i_Ind )
371+
% FFD_TWIST_2D ( 22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
372+
% HICKS_HENNE ( 30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
373+
% ANGLE_OF_ATTACK ( 101, Scale | Mark. List | 1.0 )
374+
%
375+
% 3D Design variables
376+
% FFD_CONTROL_POINT ( 11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
377+
% FFD_NACELLE ( 12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
378+
% FFD_GULL ( 13, Scale | Mark. List | FFD_BoxTag, j_Ind )
379+
% FFD_CAMBER ( 14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
380+
% FFD_TWIST ( 15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
381+
% FFD_THICKNESS ( 16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
382+
% FFD_ROTATION ( 18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
383+
% FFD_ANGLE_OF_ATTACK ( 24, Scale | Mark. List | FFD_BoxTag, 1.0 )
384+
%
385+
% Global design variables
386+
% TRANSLATION ( 1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
387+
% ROTATION ( 2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
388+
%
389+
DEFINITION_DV= ( 30, 1.0 | AIRFOIL | 0, 0.05 ); ( 30, 1.0 | AIRFOIL | 0, 0.10 ); ( 30, 1.0 | AIRFOIL | 0, 0.15 ); ( 30, 1.0 | AIRFOIL | 0, 0.20 ); ( 30, 1.0 | AIRFOIL | 0, 0.25 ); ( 30, 1.0 | AIRFOIL | 0, 0.30 ); ( 30, 1.0 | AIRFOIL | 0, 0.35 ); ( 30, 1.0 | AIRFOIL | 0, 0.40 ); ( 30, 1.0 | AIRFOIL | 0, 0.45 ); ( 30, 1.0 | AIRFOIL | 0, 0.50 ); ( 30, 1.0 | AIRFOIL | 0, 0.55 ); ( 30, 1.0 | AIRFOIL | 0, 0.60 ); ( 30, 1.0 | AIRFOIL | 0, 0.65 ); ( 30, 1.0 | AIRFOIL | 0, 0.70 ); ( 30, 1.0 | AIRFOIL | 0, 0.75 ); ( 30, 1.0 | AIRFOIL | 0, 0.80 ); ( 30, 1.0 | AIRFOIL | 0, 0.85 ); ( 30, 1.0 | AIRFOIL | 0, 0.90 ); ( 30, 1.0 | AIRFOIL | 0, 0.95 ); ( 30, 1.0 | AIRFOIL | 1, 0.05 ); ( 30, 1.0 | AIRFOIL | 1, 0.10 ); ( 30, 1.0 | AIRFOIL | 1, 0.15 ); ( 30, 1.0 | AIRFOIL | 1, 0.20 ); ( 30, 1.0 | AIRFOIL | 1, 0.25 ); ( 30, 1.0 | AIRFOIL | 1, 0.30 ); ( 30, 1.0 | AIRFOIL | 1, 0.35 ); ( 30, 1.0 | AIRFOIL | 1, 0.40 ); ( 30, 1.0 | AIRFOIL | 1, 0.45 ); ( 30, 1.0 | AIRFOIL | 1, 0.50 ); ( 30, 1.0 | AIRFOIL | 1, 0.55 ); ( 30, 1.0 | AIRFOIL | 1, 0.60 ); ( 30, 1.0 | AIRFOIL | 1, 0.65 ); ( 30, 1.0 | AIRFOIL | 1, 0.70 ); ( 30, 1.0 | AIRFOIL | 1, 0.75 ); ( 30, 1.0 | AIRFOIL | 1, 0.80 ); ( 30, 1.0 | AIRFOIL | 1, 0.85 ); ( 30, 1.0 | AIRFOIL | 1, 0.90 ); ( 30, 1.0 | AIRFOIL | 1, 0.95 )
380390

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