Please use this identifier to cite or link to this item: https://hdl.handle.net/10321/628
DC FieldValueLanguage
dc.contributor.authorWalker, Marken_US
dc.contributor.authorReiss, Talmonen_US
dc.contributor.authorAdali, Sarpen_US
dc.date.accessioned2011-07-12T13:50:36Z-
dc.date.available2011-07-12T13:50:36Z-
dc.date.issued1997-
dc.identifier.urihttp://hdl.handle.net/10321/628-
dc.descriptionOriginally published in: Composite Structures, Vol. 39, No. 3-4, 1997.en_US
dc.description.abstractThe minimum deflection and weight designs of laminated composite plates are given. The finite element method using Mindlin plate theory is used in conjunction with optimisation routines in order to obtain the optimal designs. Various boundary conditions are considered and results are given for varying aspect ratios and for different loading types. Comparative results are presented for minimum weight priority design as an alternative to minimum deflection/minimum weight priority design to investigate the effect of priority on the deflection and weight.en_US
dc.format.extentpp. 337-346 (10 p.)en_US
dc.language.isoenen_US
dc.publisherElsevieren_US
dc.rightsThe electronic version of the article published in Composite Structures 1997, 39(3-4): 337-346 © 1997 copyright Elsevier. Composite Structures available online at: http://www.sciencedirect.com/science/article/pii/S0263822397001098en_US
dc.titleOptimal design of symmetrically laminated plates for minimum deflection and weighten_US
dc.typeArticleen_US
dc.publisher.urihttp://dx.doi.org/10.1016/S0263-8223(97)00109-8en_US
dc.identifier.doi10.1016/S0263-8223(97)00109-8-
item.fulltextNo Fulltext-
item.openairecristypehttp://purl.org/coar/resource_type/c_18cf-
item.languageiso639-1en-
item.openairetypeArticle-
item.grantfulltextnone-
item.cerifentitytypePublications-
Appears in Collections:Research Publications (Engineering and Built Environment)
Show simple item record

Page view(s) 20

1,394
checked on Dec 22, 2024

Google ScholarTM

Check

Altmetric

Altmetric


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.