Dear all,
I am trying to run a composite size optimization. I want to find the optimal thickness of each ply I have created in my laminate.
My model consists in shell elements. I only have created one laminate that have multiple plies.
I want to optimize each ply thickness. I tried with the 'ply thickness' and PTMIN and PTMAN but did not work (minimize mass subjected to displacement). No iterations are run and it just gives me the results of a normal FEM analysis. Any idea why? Or how should I do it?
Second question..I inserted the control card 'global output request' CSTRESS CSTRAIN CFAILURE. The first two work fine, but I can not see the results of Composite Failure after the FEM analysis. It just gives me all value of 1.
Any suggestion on how I can see the failure results of the composite?
Thank you very much!!!!