Solve the following problem:
Compute the laminate moduli (Ex, Ey, Gxy, and νxy) and the laminate bending moduli (Ex, Ey, Gxy, and νbxy) for the laminate in Problem 1.
Problem 1: Consider a [0/90]S laminate made out of Kevlar 49-epoxy (see Table), each lamina 1.0 mm thick. Compute the stresses in material coordinates when Nx = 1 N/m.
