Hi,
greetings.
I'm doing aeroelastic optimization of composite structure using thickness of each lamina as design variable.
I have done optimization using aluminium and it worked, then I changed the material into composite by change the PSHELL properties into PCOMP and MAT1 into MAT8.
I can't...
Hi,
I want to do optimization using Nastran SOL 200, some design variable are more important than the other although it affect not so much, can i determine which variable i want to optimize first? how?
thank you.