Hi,
I’ve been trying to work out a means of calculating the required thickness for a composite plate (approx. 50% Fibre Volume Fraction) for a specified load L. My difficulty here is that under the plate are stiffener beams (also composite), in reality these beams are what take the applied load - the “plate” is simply spanning over them. What criteria should I use when deciding what thickness to make my top plate? It must be of sufficient strength to avoid puncture, and I would assume that its stiffness must match that of the beams beneath it?