puzha518
Aerospace
- Oct 11, 2012
- 5
I was not able to recover the composite ply stress or failure index when I was running a transient analysis with either SOL 109 or SOL 112. I tried to set NOCOMPS to be 0, 1 or -1. Just no ply stress (I can get element stresses and element forces though). Anybody has this type of experience or explaination? Thanks a lot.