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dc.contributor.authorCharles W. Bert
dc.contributor.authorMoinuddin Malik
dc.date.accessioned2016-01-14T19:53:18Z
dc.date.accessioned2016-03-30T15:32:49Z
dc.date.available2016-01-14T19:53:18Z
dc.date.available2016-03-30T15:32:49Z
dc.date.issued1999-09-01
dc.identifier.citationBert, C. W., & Malik, M. (1999). Buckling Analysis of Thick Laminated Plates: Higher-Order Theory with Rotatory Moments. Journal of Thermoplastic Composite Materials, 12(5), 336-350. doi: 10.1177/089270579901200501en_US
dc.identifier.urihttps://hdl.handle.net/11244/25174
dc.description.abstractThe higher-order shear deformable plate theory presented here concerns the buckling of laminated composite plates. The theory extends Reddy's higher-order theory (1984) to include the effect of rotatory moments sometimes called curvature terms. General equations of equilibrium in terms of stress resultants and boundary conditions are derived for plates laminated of orthotropic layers. Subsequently, the equations of equilibrium and boundary conditions are also obtained in terms of kinematic variables for the special case of symmetrically laminated crossply plates.en_US
dc.language.isoen_USen_US
dc.publisherJournal of Thermoplastic Composite Materials
dc.titleBuckling Analysis of Thick Laminated Plates: Higher-Order Theory with Rotatory Momentsen_US
dc.typeResearch Articleen_US
dc.description.peerreviewYesen_US
dc.description.peerreviewnoteshttps://us.sagepub.com/en-us/nam/manuscript-submission-guidelinesen_US
dc.identifier.doi10.1177/089270579901200501en_US
dc.rights.requestablefalseen_US


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