Optimum design of laminated fibre compos
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L. A. Schmit Jr.; B. Farshi
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Article
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1977
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John Wiley and Sons
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English
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## Abstract A method is presented for the minimum weight optimum design of laminated fibre composite plates, subject to multiple inplane loading conditions, which includes stiffness, strength and elastic stability constraints. The buckling analysis is based on an equivalent orthotropic plate approa