Engineering & Analysis Methods > Panel Buckling

curved panel buckling


I am using Hypersizer V 8.0.58 for stiffened composite panel. For failure mode AID 011 what are the required inputs on all forms? I get N/A for Limit MS and it is not obvious to me why. I get an ultimate MS value. I don't want failure at limit load. Is it because I am using composites that I need to use ultimate check even for limit loads? Yes, I have compression.



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