My geometry is a three-dimensional wing that is not straight in the span direction and has an angular amplitude. How do I define a line as a Chord line of the wing?
Also, which of the following design conditions should I use to apply this constraint?
There is one more design condition, and that is that the Camber line of the wing must remain constant. How do I apply this?
The subject of applying the design condition in the adjoint solver has taken me a lot of time and I have spent several months on it. It is hoped that together we can solve this problem and continue to help other researchers a lot.
If necessary, I will place the shape of the wing from the leading edge.
Regards.
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