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Optimization of symmetric laminates for maximum buckling load including the effects of bending-twisting coupling

dc.contributor.authorWalker, Marken_US
dc.contributor.authorAdali, Sarpen_US
dc.contributor.authorVerijenko, Viktor E.en_US
dc.date.accessioned2011-08-01T07:45:53Z
dc.date.available2011-08-01T07:45:53Z
dc.date.issued1996
dc.descriptionOriginally published in: in Computers & Structures Vol. 58, No. 2, 1996.en_US
dc.description.abstractFinite element solutions are presented for the optimal design of symmetrically laminated rectangular plates subjected to a combination of simply supported, clamped and free boundary conditions. The design objective is the maximization of the biaxial buckling load by determining the fibre orientations optimally, with the effects of bending-twisting coupling taken into account. The finite element method coupled with an optimization routine is employed in analysing and optimizing the laminated plate designs. The effects of boundary conditions, the number of layers and bending-twisting coupling on the optimal ply angles and the buckling load are numerically studied.en_US
dc.format.extentpp. 313-319 (7 p,)en_US
dc.identifier.doi10.1016/0045-7949(95)00138-7
dc.identifier.urihttp://hdl.handle.net/10321/644
dc.language.isoenen_US
dc.publisherElsevieren_US
dc.publisher.urihttp://dx.doi.org/10.1016/0045-7949(95)00138-7en_US
dc.rightsThe electronic version of the article published in Computers & Structures 1996, 58(2): 313-319 © 1996 copyright Elsevier. Computers & Structures available online at: http://www.sciencedirect.com/science/article/pii/0045794995001387en_US
dc.titleOptimization of symmetric laminates for maximum buckling load including the effects of bending-twisting couplingen_US
dc.typeArticleen_US

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