Hi,
Nice work. I cannot find a way to affect the wing geometry in the same way I would define an airfoil geometry (or cl,cd coefficients). To my understanding, the present implementation has a pre-defined orientation for the panels? Or am I missing something?
Hi,
Nice work. I cannot find a way to affect the wing geometry in the same way I would define an airfoil geometry (or cl,cd coefficients). To my understanding, the present implementation has a pre-defined orientation for the panels? Or am I missing something?