Failure results of composite materials modeled by Shell163 in Explicit Dynamic (classic-APDL)
I'm doing low-velocity impact on composite using explicit dynamic by APDL. To model my composite I used Shell163 and RMODIF command to lay-up it.
I want to get the failure results like Tsai-wu but I can't. May I ask you to guide me in applying the material model that can be able to see the failure modes?
Note: I tried FC commands but those ones seem to not working on Explicit Dynamic.