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Optimum Design of Laminated Composite Plates Using Lamination Parameters

โœ Scribed by Miki, Mitsunori; Sugiyamat, Yoshihiko

Book ID
126286530
Publisher
American Institute of Aeronautics and Astronautics
Year
1993
Tongue
English
Weight
241 KB
Volume
31
Category
Article
ISSN
0001-1452

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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