hello, i am new to aerodynamics. I am interested on how to calculate the minimum number of inner structure of a wing must have to tolerate the maximum downforce (not deform).
Maybe my explanation not clear, here is my project:https://www.simscale.com/projects/bning12/inner_structure_stress_test_1/
my question is how to calculate the distance between the inner structure and how many i need to put it inside the foil.
Thank you very much.