Problem 2: Determine the load N, that can be supported by the laminate shown prior to...

 

Transcribed Image Text:

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 × 10º psi 1.29 × 10º 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 E₁ = E₂ G12 = = Figure 1: Nx 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 × 10º psi 1.29 × 10º 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 E₁ = E₂ G12 = = Figure 1: Nx

Answer rating: 100% (QA)

Given The laminate is made of AC2501 900 E 199x106 psi F2 129x106 psi G 102 X 106 psi X10017X106f 2 ... View the full answer