updating DV definition numbers to be consistent with new definition

Author: jayantmukho

Inviscid_2D_Unconstrained_NACA0012/inv_NACA0012_basic.cfg

@@ -306,12 +306,17 @@ WRT_CON_FREQ_DUALTIME= 10
 WRT_HALO= NO
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
+%
 % Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY,
+%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
 %    FORCE_X, FORCE_Y, FORCE_Z,
 %    MOMENT_X, MOMENT_Y, MOMENT_Z,
 %    THRUST, TORQUE, FIGURE_OF_MERIT,
 %    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
+%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
+%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
+%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
+%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
 %
 % Available geometrical based objective functions or constraint functions
 %    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
@@ -320,18 +325,27 @@ WRT_HALO= NO
 %    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
 %
 % Available design variables
-%    HICKS_HENNE 	(  1, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    SPHERICAL		(  3, Scale | Mark. List | ControlPoint_Index, Theta_Disp, R_Disp )
-%    NACA_4DIGITS	(  4, Scale | Mark. List |  1st digit, 2nd digit, 3rd and 4th digit )
-%    DISPLACEMENT	(  5, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION		(  6, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_CONTROL_POINT	(  7, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_TWIST 	(  9, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_ROTATION 	( 10, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_CAMBER 	( 11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_THICKNESS 	( 12, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_VOLUME 	( 13, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FOURIER 		( 14, Scale | Mark. List | Lower(0)/Upper(1) side, index, cos(0)/sin(1) )
+% 2D Design variables
+%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
+%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
+%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
+%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
+%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
+%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
+%
+% 3D Design variables
+%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
+%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
+%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
+%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
+%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
+%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
+%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
+%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
+%
+% Global design variables
+%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
+%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
 %
 % Optimization objective function with scaling factor, separated by semicolons.
 % To include quadratic penalty function: use OPT_CONSTRAINT option syntax within the OPT_OBJECTIVE list.
@@ -364,4 +378,4 @@ OPT_BOUND_UPPER= 0.1
 OPT_BOUND_LOWER= -0.1
 %
 % Optimization design variables, separated by semicolons
-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 )
+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

@@ -346,15 +346,17 @@ DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
+%
 % Available flow based objective functions or constraint functions
-%    DRAG, LIFT, SIDEFORCE, EFFICIENCY,
+%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
 %    FORCE_X, FORCE_Y, FORCE_Z,
 %    MOMENT_X, MOMENT_Y, MOMENT_Z,
 %    THRUST, TORQUE, FIGURE_OF_MERIT,
-%    EQUIVALENT_AREA, NEARFIELD_PRESSURE, 
+%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
 %    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
 %    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
-%    FREE_SURFACE, SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
+%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
+%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
 %
 % Available geometrical based objective functions or constraint functions
 %    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
@@ -363,21 +365,27 @@ DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
 %    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
 %
 % Available design variables
-%    HICKS_HENNE 	(  1, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%    SPHERICAL		(  3, Scale | Mark. List | ControlPoint_Index, Theta_Disp, R_Disp )
-%    NACA_4DIGITS	(  4, Scale | Mark. List | 1st digit, 2nd digit, 3rd and 4th digit )
-%    DISPLACEMENT	(  5, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%    ROTATION		(  6, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%    FFD_CONTROL_POINT	(  7, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%    FFD_TWIST 	(  9, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_ROTATION 	( 10, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%    FFD_CAMBER 	( 11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FFD_THICKNESS 	( 12, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%    FOURIER 		( 14, Scale | Mark. List | Lower(0)/Upper(1) side, index, cos(0)/sin(1) )
-%    FFD_CONTROL_POINT_2D (  15, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
-%    FFD_CAMBER_2D 	( 16, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_THICKNESS_2D 	( 17, Scale | Mark. List | FFD_BoxTag, i_Ind )
-%    FFD_CONTROL_SURFACE 	( 18, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
+% 2D Design variables
+%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
+%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
+%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
+%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
+%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
+%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
+%
+% 3D Design variables
+%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
+%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
+%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
+%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
+%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
+%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
+%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
+%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
+%
+% Global design variables
+%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
+%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
 %
 % Optimization objective function with scaling factor, separated by semicolons.
 % To include quadratic penalty function: use OPT_CONSTRAINT option syntax within the OPT_OBJECTIVE list.
@@ -404,5 +412,5 @@ OPT_BOUND_UPPER= 0.1
 OPT_BOUND_LOWER= -0.1
 %
 % Optimization design variables, separated by semicolons
-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)
+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)
 

Multi_Objective_Shape_Design/inv_wedge_ROE_multiobj_combo.cfg

@@ -392,5 +392,5 @@ OPT_BOUND_LOWER= -1E10
 %    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
 %    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
 %
-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 | 30, 0.05 ); ( 30, 1.0 | AIRFOIL | 30, 0.10 ); ( 30, 1.0 | AIRFOIL | 30, 0.15 ); ( 30, 1.0 | AIRFOIL | 30, 0.20 ); ( 30, 1.0 | AIRFOIL | 30, 0.25 ); ( 30, 1.0 | AIRFOIL | 30, 0.30 ); ( 30, 1.0 | AIRFOIL | 30, 0.35 ); ( 30, 1.0 | AIRFOIL | 30, 0.40 ); ( 30, 1.0 | AIRFOIL | 30, 0.45 ); ( 30, 1.0 | AIRFOIL | 30, 0.50 ); ( 30, 1.0 | AIRFOIL | 30, 0.55 ); ( 30, 1.0 | AIRFOIL | 30, 0.60 ); ( 30, 1.0 | AIRFOIL | 30, 0.65 ); ( 30, 1.0 | AIRFOIL | 30, 0.70 ); ( 30, 1.0 | AIRFOIL | 30, 0.75 ); ( 30, 1.0 | AIRFOIL | 30, 0.80 ); ( 30, 1.0 | AIRFOIL | 30, 0.85 ); ( 30, 1.0 | AIRFOIL | 30, 0.90 ); ( 30, 1.0 | AIRFOIL | 30, 0.95 )
+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 )
 

Turbulent_2D_Constrained_RAE2822/turb_SA_RAE2822.cfg

@@ -305,20 +305,45 @@ WRT_CON_FREQ= 1
 
 % --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
 %
-% List of design variables (Design variables are separated by semicolons)
-% From 1 to 99, Geometrycal design variables.
-%  - HICKS_HENNE ( 1, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
-%  - NACA_4DIGITS ( 4, Scale | Mark. List |  1st digit, 2nd digit, 3rd and 4th digit )
-%  - DISPLACEMENT ( 5, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
-%  - ROTATION ( 6, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
-%  - FFD_CONTROL_POINT ( 7, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
-%  - FFD_DIHEDRAL_ANGLE ( 8, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%  - FFD_TWIST_ANGLE ( 9, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%  - FFD_ROTATION ( 10, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
-%  - FFD_CAMBER ( 11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%  - FFD_THICKNESS ( 12, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-%  - FFD_VOLUME ( 13, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
-% From 100 to 199, Flow solver design variables.
-%  - MACH_NUMBER ( 101, Scale | Markers List )
-%  - AOA ( 102, Scale | Markers List )
-DEFINITION_DV= ( 1, 0.001 | airfoil | 0, 0.1 ); ( 1, 0.001 | airfoil | 0, 0.2 )
+%
+% Available flow based objective functions or constraint functions
+%    DRAG, LIFT, SIDEFORCE, EFFICIENCY, BUFFET, 
+%    FORCE_X, FORCE_Y, FORCE_Z,
+%    MOMENT_X, MOMENT_Y, MOMENT_Z,
+%    THRUST, TORQUE, FIGURE_OF_MERIT,
+%    EQUIVALENT_AREA, NEARFIELD_PRESSURE,
+%    TOTAL_HEATFLUX, MAXIMUM_HEATFLUX,
+%    INVERSE_DESIGN_PRESSURE, INVERSE_DESIGN_HEATFLUX,
+%    SURFACE_TOTAL_PRESSURE, SURFACE_MASSFLOW
+%    SURFACE_STATIC_PRESSURE, SURFACE_MACH
+%
+% Available geometrical based objective functions or constraint functions
+%    AIRFOIL_AREA, AIRFOIL_THICKNESS, AIRFOIL_CHORD, AIRFOIL_TOC, AIRFOIL_AOA,
+%    WING_VOLUME, WING_MIN_THICKNESS, WING_MAX_THICKNESS, WING_MAX_CHORD, WING_MIN_TOC, WING_MAX_TWIST, WING_MAX_CURVATURE, WING_MAX_DIHEDRAL
+%    STATION#_WIDTH, STATION#_AREA, STATION#_THICKNESS, STATION#_CHORD, STATION#_TOC,
+%    STATION#_TWIST (where # is the index of the station defined in GEO_LOCATION_STATIONS)
+%
+% Available design variables
+% 2D Design variables
+%    FFD_CONTROL_POINT_2D   (  19, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, x_Mov, y_Mov )
+%    FFD_CAMBER_2D          (  20, Scale | Mark. List | FFD_BoxTag, i_Ind )
+%    FFD_THICKNESS_2D       (  21, Scale | Mark. List | FFD_BoxTag, i_Ind )
+%    FFD_TWIST_2D           (  22, Scale | Mark. List | FFD_BoxTag, x_Orig, y_Orig )
+%    HICKS_HENNE            (  30, Scale | Mark. List | Lower(0)/Upper(1) side, x_Loc )
+%    ANGLE_OF_ATTACK        ( 101, Scale | Mark. List | 1.0 )
+%
+% 3D Design variables
+%    FFD_CONTROL_POINT      (  11, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind, k_Ind, x_Mov, y_Mov, z_Mov )
+%    FFD_NACELLE            (  12, Scale | Mark. List | FFD_BoxTag, rho_Ind, theta_Ind, phi_Ind, rho_Mov, phi_Mov )
+%    FFD_GULL               (  13, Scale | Mark. List | FFD_BoxTag, j_Ind )
+%    FFD_CAMBER             (  14, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
+%    FFD_TWIST              (  15, Scale | Mark. List | FFD_BoxTag, j_Ind, x_Orig, y_Orig, z_Orig, x_End, y_End, z_End )
+%    FFD_THICKNESS          (  16, Scale | Mark. List | FFD_BoxTag, i_Ind, j_Ind )
+%    FFD_ROTATION           (  18, Scale | Mark. List | FFD_BoxTag, x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
+%    FFD_ANGLE_OF_ATTACK    (  24, Scale | Mark. List | FFD_BoxTag, 1.0 )
+%
+% Global design variables
+%    TRANSLATION            (   1, Scale | Mark. List | x_Disp, y_Disp, z_Disp )
+%    ROTATION               (   2, Scale | Mark. List | x_Axis, y_Axis, z_Axis, x_Turn, y_Turn, z_Turn )
+%
+DEFINITION_DV= ( 30, 0.001 | airfoil | 0, 0.1 ); ( 30, 0.001 | airfoil | 0, 0.2 )