Structural Theory for Laminated Anisotropic Elastic Shells

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dc.contributor.authorCharles W. Bert
dc.date.accessioned2016-01-14T19:52:42Z
dc.date.accessioned2016-03-30T15:32:58Z
dc.date.available2016-01-14T19:52:42Z
dc.date.available2016-03-30T15:32:58Z
dc.date.issued1967-10-01
dc.description.abstractA linear theory is formulated for analysis of small deflections of thin shells with arbitrary geometrical configuration and laminated of an arbitrary number of layers of different thicknesses, orientations, and anisotropic elastic coefficients. An accurate shell theory (Vlasov's) is used, and the composite-shell constitutive relation incorporates the anisotropic stretching-bending coupling effects considered by Stavsky. For shells of arbitrary geometry, it is found necessary to introduce a new parameter Fij ≡ ∫h z 3Qijdz in the con stitutive relation. This parameter is zero for homogeneous aniso tropic materials and for anisotropic materials laminated symmetri cally with respect to the middle surface. However, for a two-layer filament-wound shell, this parameter can increase the flexural rigidity by 3%, which is greater than a 2% effect considered in a previous layered-anisotropic cylindrical shell analysis.en_US
dc.description.peerreviewYesen_US
dc.description.peerreviewnoteshttps://us.sagepub.com/en-us/nam/manuscript-submission-guidelinesen_US
dc.identifier.citationBert, C. W. (1967). Structural Theory for Laminated Anisotropic Elastic Shells. Journal of Composite Materials, 1(4), 414-423. doi: 10.1177/002199836700100409en_US
dc.identifier.doi10.1177/002199836700100409en_US
dc.identifier.urihttp://hdl.handle.net/11244/24858
dc.language.isoen_USen_US
dc.publisherJournal of Composite Materials
dc.rights.requestablefalseen_US
dc.titleStructural Theory for Laminated Anisotropic Elastic Shellsen_US
dc.typeResearch Articleen_US

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