Hi, has anyone tried performing classical laminate theory in reverse, i.e. getting lamina stiffness and strength values from experimental laminate data? I have been attempting to do so but I can’t seem to get my formulation to work correctly. I’m 99% sure it is correct because I can go from Q Matrix [FONT=Wingdings]—>[/FONT] A Matrix, but not the reverse calculation.
Surprisingly there doesn’t appear to be any commercial software that calculates this, and I have only found two academic papers which mention the reverse process. I’ve attached a PDF showing my workings as that will be a lot clearer than writing it out here.