[Question] Script to output airfoil/wing shapes

[r-ashwin]

(new user here and apologies if this has been raised/addressed before).

I want to perturb the Hicks and Henne bump function design variables and write out the airfoil shape, without running the primal or adjoint solvers. So I want to implement Y = f(X) where X is the vector of Hicks and Henne bump function weights and Y is a vector of the actual y coordinate of the airfoil at each x corresponding to an element of X.

Is there a script that already exists to this effect? If so can you share that with me? If not do you have suggestions as to how to implement this? Thank you!

[pcarruscag]

Run SU2_DEF