Buckling of laminated columns containing delaminations

Nagesh Babu, G. L. ; Krishna Murty, A. V. (1989) Buckling of laminated columns containing delaminations Journal of the Aeronautical Society of India, 41 (2). pp. 183-190. ISSN 0001-9267

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Abstract

Compressive load carrying capability of delaminated columns depends upon the buckling and growth charactenstics of the sublaminate. For purposes of analysis, the delaminated column is divided into four regions. Linear beam-column theory is employed in three regions and large deformation terms are retained in the fourth region to consider the post buckled state of sublaminate. Strain energy release rate criteria is employed to obtain the growth characteristics of the delamination. Compressive load carrying behaviour of the delaminated columns fixed at either end containing a through delamination has been studied. A simple continuum procedure is used in the first instance to bring out the phenomenon. The finite element scheme is used, later to confirm the results. In general the compressive load carrying capability reduces with the increase in the size of the delamination. Buckling load of the completely slit configuration of the columr represents the highest load it can carry when the delamination is larger than a certain critical size.

Item Type:Article
Source:Copyright of this article belongs to Aeronautical Society of India.
ID Code:93886
Deposited On:29 Jun 2012 11:17
Last Modified:29 Jun 2012 11:17

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