I have a model of a shell plate with several layers of composite materials, designed using CQUAD elements. As part of the static analysis of the model, Nastran provides me with the stress and strain in the middle plane of each layer. Is it possible to obtain the stress and strain in the top and bottom planes of each layer by modifying the .bdf file? I do not wish to use Patran for post-processing.

More Mohammed Abir Mahdi's questions See All
Similar questions and discussions