Hello All,
Does anyone know how to get laminate failure criteria output from NASTRAN for post processing in FEMAP ? I'm trying to get Hoffman's Theory failure criteria to display - I believe it's output vector 6060 but I must be missing something.
Thank you in advance for your help,
Carl
Solved! Go to Solution.
Solved by Andrew.Sartorelli. Go to Solution.
Hi @carl,
The result vector 6060 is the shell composite maximum stability failure index. If you are looking for the shell composite ply failure index, that is 6099. Here is a complete list of the result vectors available for shell composite elements.
I hope this helps.
Best Regards,
Andrew
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