Hi guys

I'm designing a wing for one of my courses in uni and I need some specific info.

How would the loads acting on an airplane wing change during a sandstorm? How would the lift and drag coefficients change? How would the mass of the wing change? Is there anything else I need to know about in terms of wing structural design?

If you don't know, then could you point me in the right direction?

I'm sorry if this is not the right place to post this, I'm new here.

I'm designing a wing for one of my courses in uni and I need some specific info.

How would the loads acting on an airplane wing change during a sandstorm? How would the lift and drag coefficients change? How would the mass of the wing change? Is there anything else I need to know about in terms of wing structural design?

If you don't know, then could you point me in the right direction?

I'm sorry if this is not the right place to post this, I'm new here.

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