Merge branch 'master' of https://github.com/su2code/su2code.github.io

su2code · Feb 14, 2018 · 794d3e1 · 794d3e1
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diff --git a/Turbulent_2D_Constrained_RAE2822/images/CD_CL.png b/Turbulent_2D_Constrained_RAE2822/images/CD_CL.png
diff --git a/Turbulent_2D_Constrained_RAE2822/images/CM_THICK.png b/Turbulent_2D_Constrained_RAE2822/images/CM_THICK.png
diff --git a/Turbulent_2D_Constrained_RAE2822/images/Optimization.png b/Turbulent_2D_Constrained_RAE2822/images/Optimization.png
diff --git a/_tutorials/design_features/Turbulent_2D_Constrained_RAE2822.md b/_tutorials/design_features/Turbulent_2D_Constrained_RAE2822.md
@@ -173,12 +173,11 @@ where #cores is the number of cores. Depending of the installation, the keyword
 
 ### Results for the optimal shape design problem:
 
-![RAE 2822 Final Contour](../../Turbulent_2D_Constrained_RAE2822/images/rae2822_final_contour.png)
-Figure (4): Pressure contours around the final airfoil design. Note the nearly shock-free final design.
+![RAE 2822 Final Cp](../../Turbulent_2D_Constrained_RAE2822/images/Optimization.png)
+Figure (4): Cp distribution comparison for the initial and final airfoil designs.
 
-![RAE 2822 Final Cp](../../Turbulent_2D_Constrained_RAE2822/images/rae2822_final_cp.png)
-Figure (5): Cp distribution and profile shape comparison for the initial and final airfoil designs.
-
-![RAE 2822 Final History](../../Turbulent_2D_Constrained_RAE2822/images/rae2822_final_history.png)
-Figure (6): Function evaluation history during the optimization process.
+![RAE 2822 Final History Objective Function](../../Turbulent_2D_Constrained_RAE2822/images/CD_CL.png)
+Figure (5): Objective function evaluation history during the optimization process.
 
+![RAE 2822 Final History Constraints](../../Turbulent_2D_Constrained_RAE2822/images/CM_THICK.png)
+Figure (6): Constraints evaluation history during the optimization process.