Reply To: Fluent adjoint solver; constant camber line constraint

[Aras karimi]

The goal is to optimize the shape of the wing, which ultimately leads to increased lift or reduced drag. The final optimized wing has improved increased lift and reduced drag, but the wing sections have gonacon airfoils and are different from the original wing geometry airfoils.

My goal is for the optimized wing to have the same airfoils as the original wing at different cross sections.