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Article: Stability and failure of symmetrically laminated plates

TitleStability and failure of symmetrically laminated plates
Authors
KeywordsFailure
Flat panels
Laminated composites
Postbuckling
Stability
Issue Date1996
PublisherTechno-Press. The Journal's web site is located at http://technopress.kaist.ac.kr/?journal=sem&subpage=5
Citation
Structural Engineering And Mechanics, 1996, v. 4 n. 5, p. 485-496 How to Cite?
AbstractThis paper describes a numerical and experimental study on the stability and failure behaviour of rectangular symmetric laminated composite plates. The plates are simply supported along the unloaded edges and clamped along the loaded ends, and they are subjected to uniaxial in-plane compression. The finite element method was employed for the theoretical study. The study examines the effect of the plate's stacking sequence and aspect ratio on the stability and failure response of rectangular symmetric laminated carbon fibre reinforced plastics composite plates. The study also includes the effect of the unloaded edge support conditions on the postbuckling response and failure of the plates. Extensive experimental investigation were also carried out to supplement the finite element study. A comprehensive comparison between theory and experimental data are presented and discussed in this contribution.
Persistent Identifierhttp://hdl.handle.net/10722/75759
ISSN
2015 Impact Factor: 1.021
2015 SCImago Journal Rankings: 0.450
References

 

DC FieldValueLanguage
dc.contributor.authorChai, GBen_HK
dc.contributor.authorHoon, KHen_HK
dc.contributor.authorChin, SSen_HK
dc.contributor.authorSoh, AKen_HK
dc.date.accessioned2010-09-06T07:14:17Z-
dc.date.available2010-09-06T07:14:17Z-
dc.date.issued1996en_HK
dc.identifier.citationStructural Engineering And Mechanics, 1996, v. 4 n. 5, p. 485-496en_HK
dc.identifier.issn1225-4568en_HK
dc.identifier.urihttp://hdl.handle.net/10722/75759-
dc.description.abstractThis paper describes a numerical and experimental study on the stability and failure behaviour of rectangular symmetric laminated composite plates. The plates are simply supported along the unloaded edges and clamped along the loaded ends, and they are subjected to uniaxial in-plane compression. The finite element method was employed for the theoretical study. The study examines the effect of the plate's stacking sequence and aspect ratio on the stability and failure response of rectangular symmetric laminated carbon fibre reinforced plastics composite plates. The study also includes the effect of the unloaded edge support conditions on the postbuckling response and failure of the plates. Extensive experimental investigation were also carried out to supplement the finite element study. A comprehensive comparison between theory and experimental data are presented and discussed in this contribution.en_HK
dc.languageengen_HK
dc.publisherTechno-Press. The Journal's web site is located at http://technopress.kaist.ac.kr/?journal=sem&subpage=5en_HK
dc.relation.ispartofStructural Engineering and Mechanicsen_HK
dc.subjectFailureen_HK
dc.subjectFlat panelsen_HK
dc.subjectLaminated compositesen_HK
dc.subjectPostbucklingen_HK
dc.subjectStabilityen_HK
dc.titleStability and failure of symmetrically laminated platesen_HK
dc.typeArticleen_HK
dc.identifier.emailSoh, AK:aksoh@hkucc.hku.hken_HK
dc.identifier.authoritySoh, AK=rp00170en_HK
dc.description.naturelink_to_subscribed_fulltext-
dc.identifier.scopuseid_2-s2.0-0030245824en_HK
dc.identifier.hkuros23546en_HK
dc.relation.referenceshttp://www.scopus.com/mlt/select.url?eid=2-s2.0-0030245824&selection=ref&src=s&origin=recordpageen_HK
dc.identifier.volume4en_HK
dc.identifier.issue5en_HK
dc.identifier.spage485en_HK
dc.identifier.epage496en_HK
dc.publisher.placeKorea, Republic ofen_HK
dc.identifier.scopusauthoridChai, GB=6602160796en_HK
dc.identifier.scopusauthoridHoon, KH=12544836300en_HK
dc.identifier.scopusauthoridChin, SS=7202600495en_HK
dc.identifier.scopusauthoridSoh, AK=7006795203en_HK

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