How to do ANSYS of [0, 90] symmetric laminated composite plate with hole under inplane loading?
If possible send ANSYS command file to do so.
How to do ANSYS of [0, 90] symmetric laminated composite plate with hole under inplane loading?
If possible send ANSYS command file to do so.
i don't know about ansys but
i don't know about ansys but abaqus has a such ability to analyze composite lyup with cohesive part and also damage initiation and propagation