Problem 2: Determine the load N, that can be supported by the laminate shown prior to catastrophic failure (i.e. failure in all three laminae). The laminate is made of AS/3501 [902/0]s with individual lamina thickness of t = 0.005. The laminate was cured at a temperature of 370F and is tested at 70F. Use the Tsai-Hill theory and neglect hygral effects. Nx 19.9 10 psi 1.29 10 psi 1.03 10 psi 1/12 0.3 -0.17 x 10-6/F 01 CX2 = 15.57 x 10-6/F XT Xc = 210ksi YT = 7.5ksi Ye = 29.9ksi S = 13.5ksi E = E G12 = = Figure 1: Nx