Consider a [0/45/-45]S laminate, subject to a load Nx = Ny = 1000 N/mm. Compute the [A], and [D] matrices (neglect shear deformations) for the intact laminate. Each lamina is 2.5 mm thick. Do not adjust for in-situ strength. The material properties are:
E1 = 204.6 GPa
E2 = 20.46 GPa
G12 = 6.89 MPa
v12 = 0.3
F1t = 826.8 MPa
F1c = 482.3 MPa
F2t = F2c = 68.9 MPa
F6 = 241.15 MPa