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Buckling Studies on Laminated Composite Skew Plates

by C.V. Srinivasa, Y.J. Suresh, W.P. Prema Kumar
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International Journal of Computer Applications
Foundation of Computer Science (FCS), NY, USA
Volume 37 - Number 1
Year of Publication: 2012
Authors: C.V. Srinivasa, Y.J. Suresh, W.P. Prema Kumar
10.5120/4575-6612

C.V. Srinivasa, Y.J. Suresh, W.P. Prema Kumar . Buckling Studies on Laminated Composite Skew Plates. International Journal of Computer Applications. 37, 1 ( January 2012), 35-47. DOI=10.5120/4575-6612

@article{ 10.5120/4575-6612,
author = { C.V. Srinivasa, Y.J. Suresh, W.P. Prema Kumar },
title = { Buckling Studies on Laminated Composite Skew Plates },
journal = { International Journal of Computer Applications },
issue_date = { January 2012 },
volume = { 37 },
number = { 1 },
month = { January },
year = { 2012 },
issn = { 0975-8887 },
pages = { 35-47 },
numpages = {9},
url = { https://ijcaonline.org/archives/volume37/number1/4575-6612/ },
doi = { 10.5120/4575-6612 },
publisher = {Foundation of Computer Science (FCS), NY, USA},
address = {New York, USA}
}
%0 Journal Article
%1 2024-02-06T20:23:12.848070+05:30
%A C.V. Srinivasa
%A Y.J. Suresh
%A W.P. Prema Kumar
%T Buckling Studies on Laminated Composite Skew Plates
%J International Journal of Computer Applications
%@ 0975-8887
%V 37
%N 1
%P 35-47
%D 2012
%I Foundation of Computer Science (FCS), NY, USA
Abstract

This paper presents buckling studies made on skew plates using finite element. The effects of the skew angle, aspect ratio, length-to-thickness-ratio, fibre orientation angle, and numbers of layers in the laminate and laminate sequence on the critical buckling load factor (Kcr) of antisymmetric composite laminates have also been presented. The critical buckling load factor (Kcr) is found to increase with the skew angle. When the number of layers in the laminate is large, the variation of critical buckling load factor (Kcr) with the number of layers is not appreciable.

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Index Terms

Computer Science
Information Sciences

Keywords

Skew Plates Antisymmetric Laminates Buckling Finite Element

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