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.
TIA, T
Topic: curved panel buckling (Read 57609 times)