Design buckling curves for clamped orthotropic laminated plates

Tsouvalis, NG; Papazoglou, VJ

dc.contributor.author	Tsouvalis, NG	en
dc.contributor.author	Papazoglou, VJ	en
dc.date.accessioned	2014-03-01T01:20:07Z
dc.date.available	2014-03-01T01:20:07Z
dc.date.issued	2004	en
dc.identifier.issn	0963-6935	en
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/15844
dc.relation.uri	http://www.scopus.com/inward/record.url?eid=2-s2.0-15544368768&partnerID=40&md5=d4293168993e565be8118258acd40e74	en
dc.subject.classification	Materials Science, Composites	en
dc.subject.other	Algebra	en
dc.subject.other	Aspect ratio	en
dc.subject.other	Bending (deformation)	en
dc.subject.other	Boundary conditions	en
dc.subject.other	Buckling	en
dc.subject.other	Compaction	en
dc.subject.other	Laminates	en
dc.subject.other	Linear equations	en
dc.subject.other	Matrix algebra	en
dc.subject.other	Structural design	en
dc.subject.other	Buckling load	en
dc.subject.other	Clamped rectangular orthotropic plates	en
dc.subject.other	Classical lamination theory (CLT)	en
dc.subject.other	Rayleigh-Ritz method	en
dc.subject.other	Plates (structural components)	en
dc.title	Design buckling curves for clamped orthotropic laminated plates	en
heal.type	journalArticle	en
heal.language	English	en
heal.publicationDate	2004	en
heal.abstract	Non-dimensional design buckling curves for clamped rectangular orthotropic plates are presented in this study. These curves provide the critical buckling load of thin, symmetric, cross-ply laminated plates as a function of the laminate's rigidities and aspect ratio for the following seven configurations of the applied in-plane loads: uniform uniaxial compression, triangular uniaxial compression, uniaxial in-plane bending, pure shear, uniform uniaxial compression combined with shear, triangular uniaxial compression combined with shear, and uniaxial in-plane bending combined with shear. Approximate mathematical formulae are also provided. The Classical Lamination Theory, in conjunction with the Rayleigh-Ritz method, has been used for the determination of the critical buckling load. The validity of the study is confirmed by comparing its results with other both theoretical and numerical ones.	en
heal.publisher	ADCOTEC LTD	en
heal.journalName	Advanced Composites Letters	en
dc.identifier.isi	ISI:000228302800002	en
dc.identifier.volume	13	en
dc.identifier.issue	5	en
dc.identifier.spage	227	en
dc.identifier.epage	235	en