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Consider a unidirectional Kevlar/Epoxy lamina. The stiffness in the fiber direction must be at least 70 GPa, and the stiffnes

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The mentioned equations are not given the question, hence the problem is completely solved.

Ef = 12uapa V = 0.35 Em-3,5 GPA Vm = 0.33 E = TOGPA E = 10opa By rule of mixtures: E, = Ef uft Emvm. ve volume Vm= 1- Vf frac

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