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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?
The text was updated successfully, but these errors were encountered:
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?
The text was updated successfully, but these errors were encountered: