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Please use this identifier to cite or link to this item: http://dspace.bits-pilani.ac.in:8080/jspui/handle/123456789/14705
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dc.contributor.authorKumar, Rajesh-
dc.contributor.authorPatel, Shuvendu Narayan-
dc.date.accessioned2024-04-27T06:42:15Z-
dc.date.available2024-04-27T06:42:15Z-
dc.date.issued2021-06-
dc.identifier.urihttps://link.springer.com/chapter/10.1007/978-981-16-1688-4_12-
dc.identifier.urihttp://dspace.bits-pilani.ac.in:8080/jspui/xmlui/handle/123456789/14705-
dc.description.abstractIn this article, the stability of a laminated composite plate when subjected to in-plane compressive pulse load is investigated in the finite element method framework. Convergence and validation studies are carried out using the current mathematical formulation and compared with the results from the existing literatures. The effects of loading duration, imperfection and ply orientation on the dynamic buckling behavior of the plate with irregular imperfection are studied in detail and the results are reported. It is observed that the plate having irregular imperfection of the order of 20% of the plate thickness has a lower non-linear dynamic buckling load than the plate with 15% irregular imperfection.en_US
dc.language.isoenen_US
dc.publisherSpringeren_US
dc.subjectCivil Engineeringen_US
dc.subjectCNT fiber-reinforced laminated composite (CNTFRLC) plateen_US
dc.titleBuckling of Laminated Composite Plate with Imperfections Subjected to In-Plane Pulse Loadsen_US
dc.typeBook chapteren_US
Appears in Collections:Department of Civil Engineering

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