[D]. (25 2. Find the ply-by-ply failure loads for a [05/905]s glass fiber/epoxy laminate. O Properties...

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[D]. (25 2. Find the ply-by-ply failure loads for a [05/905]s glass fiber/epoxy laminate. O Properties of unidirectional lamina are below: E = 45, E = 8.0, G = 4.0 (GPa), D = 0.26, T-ult C-ult ult T = 12 (35 point) =1045, -610, 35, 135, 75 (MPa) T-ul o 2 = The thickness of each ply is 0.15 mm. 2 = The only applied load is a tensile normal load in the 0-fiber direction. Maximum stress failure theory is employed, and using full discounted stiffness. methods for damaged plies. [D]. (25 2. Find the ply-by-ply failure loads for a [05/905]s glass fiber/epoxy laminate. O Properties of unidirectional lamina are below: E = 45, E = 8.0, G = 4.0 (GPa), D = 0.26, T-ult C-ult ult T = 12 (35 point) =1045, -610, 35, 135, 75 (MPa) T-ul o 2 = The thickness of each ply is 0.15 mm. 2 = The only applied load is a tensile normal load in the 0-fiber direction. Maximum stress failure theory is employed, and using full discounted stiffness. methods for damaged plies.