Abstract
Laminated composite plates are fabricated of laminae (also called layers or plies), where each lamina consists of high-strength fibres (e.g. glass, boron, graphite) embedded in a surrounding matrix material (e.g. epoxy resin). The present work is limited to laminae wherein the fibres are assumed to be all parallel and continuous (i.e. long fibres). Thus each layer may be treated in a macroscopic sense as being a homogeneous, orthotropic material, for which the deformation behaviour is linearly elastic.
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Leissa, A.W. (1995). Buckling and postbuckling theory for laminated composite plates. In: Turvey, G.J., Marshall, I.H. (eds) Buckling and Postbuckling of Composite Plates. Springer, Dordrecht. https://doi.org/10.1007/978-94-011-1228-4_1
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DOI: https://doi.org/10.1007/978-94-011-1228-4_1
Publisher Name: Springer, Dordrecht
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