Please use this identifier to cite or link to this item: https://hdl.handle.net/2440/46513
Citations
Scopus Web of Science® Altmetric
?
?
Full metadata record
DC FieldValueLanguage
dc.contributor.authorChakrabarti, A.-
dc.contributor.authorSheikh, A.-
dc.date.issued2006-
dc.identifier.citationOcean Engineering, 2006; 33(17-18):2287-2309-
dc.identifier.issn0029-8018-
dc.identifier.urihttp://hdl.handle.net/2440/46513-
dc.descriptionCopyright © 2006 Elsevier Ltd All rights reserved.-
dc.description.abstractThe dynamic instability of laminated sandwich plates subjected to in-plane partial edge loading is studied for the first time using an efficient finite element plate model. The plate model is based on a refined higher order shear deformation plate theory, where the transverse shear stresses are continuous at the layer interfaces with stress free conditions at plate top and bottom surfaces. Interestingly the plate model having all these refined features requires unknowns at the reference plane only. However, this theory requires C1 continuity of transverse displacement, which is difficult to satisfy arbitrarily in any existing finite element. To deal with this, a new triangular element developed by the authors is used in the present paper. © 2006 Elsevier Ltd. All rights reserved.-
dc.description.statementofresponsibilityAnupam Chakrabarti and Abdul Hamid Sheikh-
dc.description.urihttp://www.elsevier.com/wps/find/journaldescription.cws_home/320/description#description-
dc.language.isoen-
dc.publisherPergamon-Elsevier Science Ltd-
dc.source.urihttp://dx.doi.org/10.1016/j.oceaneng.2005.11.003-
dc.titleDynamic instability of laminated sandwich plates subjected to in-plane partial edge loading-
dc.typeJournal article-
dc.identifier.doi10.1016/j.oceaneng.2005.11.003-
pubs.publication-statusPublished-
dc.identifier.orcidSheikh, A. [0000-0002-2839-1707]-
Appears in Collections:Aurora harvest 6
Civil and Environmental Engineering publications

Files in This Item:
There are no files associated with this item.


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