Please use this identifier to cite or link to this item:
http://dspace.bits-pilani.ac.in:8080/jspui/handle/123456789/14705
Title: | Buckling of Laminated Composite Plate with Imperfections Subjected to In-Plane Pulse Loads |
Authors: | Kumar, Rajesh Patel, Shuvendu Narayan |
Keywords: | Civil Engineering CNT fiber-reinforced laminated composite (CNTFRLC) plate |
Issue Date: | Jun-2021 |
Publisher: | Springer |
Abstract: | In 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. |
URI: | https://link.springer.com/chapter/10.1007/978-981-16-1688-4_12 http://dspace.bits-pilani.ac.in:8080/jspui/xmlui/handle/123456789/14705 |
Appears in Collections: | Department of Civil Engineering |
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.