Consider a quasi-isotropic laminate 090 plusmn 45s 8 mm


Consider a quasi-isotropic laminate [0/90/ ± 45]S, 8 mm thick, made of carbon-epoxy AS4-3501-6. Use the truncated-maximum-strain failure criterion without matrix cutoff. Estimate the strains-to-failure using the data equation (7.8). Explain the mode of failure under the following loading conditions:

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English: Consider a quasi-isotropic laminate 090 plusmn 45s 8 mm
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