Hello! I have a model of a (solar) panel deployment with torsion spring and contact element on my hinges. I included a sandwich panel (CFRP faceskins + AL honeycomb) as a flexible body to obtain stresses. The faceskins have a certain layup and the whole panel is defined through a PCOMP elements(in Nastran) faceskin - honeycomb - faceskin.
I have succesfully ran the simulation and obtained Von Misses stresses around the bolt holes (defined with compliant fixed constraints and stifnesses).
The question is - can I obtain the stresses on individual layers? Just the core or an i-th layer of the faceskin.
Thank you very much!