Design curves for specially orthotropic laminated plates under combined in-plane loading

Papazoglou, VJ; Tsouvalis, NG

dc.contributor.author	Papazoglou, VJ	en
dc.contributor.author	Tsouvalis, NG	en
dc.date.accessioned	2014-03-01T01:40:47Z
dc.date.available	2014-03-01T01:40:47Z
dc.date.issued	1991	en
dc.identifier.issn	00811661	en
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/23239
dc.relation.uri	http://www.scopus.com/inward/record.url?eid=2-s2.0-0026364388&partnerID=40&md5=407d5ed70b32722f4f93f2dd29342638	en
dc.subject.other	Buckling	en
dc.subject.other	Design	en
dc.subject.other	Laminates	en
dc.subject.other	Subroutines	en
dc.subject.other	Classical lamination theory	en
dc.subject.other	Combined in plane loading	en
dc.subject.other	Design curves	en
dc.subject.other	Specially orthotropic laminated plates	en
dc.subject.other	Plates (structural components)	en
dc.title	Design curves for specially orthotropic laminated plates under combined in-plane loading	en
heal.type	journalArticle	en
heal.publicationDate	1991	en
heal.abstract	Non-dimensional design buckling curves are presented for simply supported, rectangular, symmetric specially orthotropic laminated plates under various loading conditions, including linearly varying in-plane biaxial loads, combined with shear. The theoretical modeling, based on the use of Classical Lamination Theory in conjunction with the Rayleigh-Ritz method, is also presented. The numerical implementation of the method is described in detail, including the presentation of some computer subroutines. Finally, analysis and design examples are given for several loading cases.	en
heal.journalName	Transactions - Society of Naval Architects and Marine Engineers	en
dc.identifier.volume	99	en
dc.identifier.spage	377	en
dc.identifier.epage	403	en