Hello, I'm a newbie here, please help me to solve for the bending moment of my design airplane. I want to know if my wing spar is strong enough to support the weight of my design which is 490 lb. I want also to know if what is the breaking point of the wing spar. Please see the attached picture.(adsbygoogle = window.adsbygoogle || []).push({});

Thank you...

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# Aerospace How to solve for bending moment?

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