Hi TG_eng,
I've look into the subject a bit more. You are right, I need to apply a global ply to each one of the layup in order to postprocess with global plies. It works now.
Thank you,
Hi,
I've started using 3D laminate elements in Femap in order to model a thick carbon beam with important transverse shear load.
I am having trouble post processing stresses in the laminate.
My stacking is the following :
And for the post processing, ply numbers in the stacking and ply...