Engineering, 13.09.2019 23:10 preachersgirl5
Acarbon/epoxy (as/3501) unidirectional laminate with a fiber orientation q = 30° is exposed to the following stresses, sx = 40 ksi, sy = -20 ksi, txy = 20 ksi. determine the engineering strains in the fiber coordinate system. use the following typical properties for carbon/epoxy e1 = 18.4 msi, e2 = 1.6 msi, g12 = 0.95 msi, n12 = 0.28.
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Acarbon/epoxy (as/3501) unidirectional laminate with a fiber orientation q = 30° is exposed to the f...
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