updating tutorial for new fixed cl mode

Author: jayantmukho

Turbulent_2D_Constrained_RAE2822/turb_SA_RAE2822.cfg

@@ -53,8 +53,8 @@ TARGET_CL= 0.724
 % Estimation of dCL/dAlpha (0.2 per degree by default)
 DCL_DALPHA= 0.2
 %
-% Number of times the AoA is updated in a fix CL problem (5 by default)
-UPDATE_ALPHA= 5
+% Maximum number of iterations between AoA updates
+UPDATE_AOA_ITER_LIMIT= 100
 %
 % Number of iterations to evaluate dCL/dAlpha at the end of the simulation
 ITER_DCL_DALPHA= 500
@@ -100,6 +100,7 @@ CFL_NUMBER= 10.0
 %
 % Number of total iterations
 EXT_ITER= 5000
+ITER = 5000
 %
 % Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
 %                                             MOMENT_Y, MOMENT_Z, EFFICIENCY)
@@ -230,10 +231,10 @@ GEO_MODE= FUNCTION
 CONV_CRITERIA= RESIDUAL
 %
 % Residual reduction (order of magnitude with respect to the initial value)
-RESIDUAL_REDUCTION= 9
+RESIDUAL_REDUCTION= 8
 %
 % Min value of the residual (log10 of the residual)
-RESIDUAL_MINVAL= -12
+RESIDUAL_MINVAL= -10
 %
 % Start convergence criteria at iteration number
 STARTCONV_ITER= 10
@@ -367,17 +368,29 @@ OPT_BOUND_UPPER= 1E10
 % Lower bound for each design variable (bound in the python optimizer)
 OPT_BOUND_LOWER= -1E10
 
-% List of design variables (Design variables are separated by semicolons)
-%  - 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 )
-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 )
+% List of available design variables (Design variables are separated by semicolons)
+%
+% 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, 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 )
 

_tutorials/design_features/Turbulent_2D_Constrained_RAE2822.md

@@ -73,8 +73,8 @@ TARGET_CL= 0.724
 % Estimation of dCL/dAlpha (0.2 per degree by default)
 DCL_DALPHA= 0.2
 %
-% Number of times the AoA is updated in a fix CL problem (5 by default)
-UPDATE_ALPHA= 5
+% Maximum number of iterations between AoA updates
+UPDATE_AOA_ITER_LIMIT= 100
 %
 % Number of iterations to evaluate dCL/dAlpha at the end of the simulation
 ITER_DCL_DALPHA= 500