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Laminate Failure Criteria

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carl
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Laminate Failure Criteria

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

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Andrew.Sartorelli
in reply to: carl

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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Andrew Sartorelli - Autodesk GmbH

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