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The effect of aspect ratio on the elastoplastic response of stiffened plates loaded in uniaxial edge compression

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dc.contributor.author Toulios, M en
dc.contributor.author Caridis, PA en
dc.date.accessioned 2014-03-01T01:18:25Z
dc.date.available 2014-03-01T01:18:25Z
dc.date.issued 2002 en
dc.identifier.issn 0045-7949 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/14988
dc.subject Buckling en
dc.subject Dynamic relaxation en
dc.subject Residual Stresses en
dc.subject Stiffened plates en
dc.subject Ultimate strength en
dc.subject.classification Computer Science, Interdisciplinary Applications en
dc.subject.classification Engineering, Civil en
dc.subject.other Algorithms en
dc.subject.other Aspect ratio en
dc.subject.other Buckling en
dc.subject.other Compressibility of solids en
dc.subject.other Elastoplasticity en
dc.subject.other Finite element method en
dc.subject.other Residual stresses en
dc.subject.other Uniaxial edge compression en
dc.subject.other Plates (structural components) en
dc.title The effect of aspect ratio on the elastoplastic response of stiffened plates loaded in uniaxial edge compression en
heal.type journalArticle en
heal.identifier.primary 10.1016/S0045-7949(02)00080-9 en
heal.identifier.secondary http://dx.doi.org/10.1016/S0045-7949(02)00080-9 en
heal.language English en
heal.publicationDate 2002 en
heal.abstract A numerical study of the effect of aspect ratio on the buckling and collapse behaviour of flatbar-stiffened plates in compression is described. The plate equations are expressed in finite difference form and the solution is obtained using a dynamic relaxation algorithm. Initial imperfections and residual stresses are also introduced in the study. It was found that, for aspect ratios between 2 and 3.5, buckling occurs in the elastic regime, with the panels exhibiting significant post-buckling strength prior to collapse. For aspect ratios between I and 2 buckling occurs as the plastic zone increases, followed by rapid unloading as the panel collapses suddenly. The ultimate strength of the panel reduces with increasing aspect ratio, remaining practically constant at higher aspect ratios. The latter is attributed to the initial single half-wave distortion profile that prohibits the formation of the preferred buckling mode. (C) 2002 Elsevier Science Ltd. All rights reserved. en
heal.publisher PERGAMON-ELSEVIER SCIENCE LTD en
heal.journalName Computers and Structures en
dc.identifier.doi 10.1016/S0045-7949(02)00080-9 en
dc.identifier.isi ISI:000177620700009 en
dc.identifier.volume 80 en
dc.identifier.issue 14-15 en
dc.identifier.spage 1317 en
dc.identifier.epage 1328 en


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