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Composite Structures
Volume 51, Issue 4, April 2001, Pages 439-449
 
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doi:10.1016/S0263-8223(00)00159-8    How to Cite or Link Using DOI (Opens New Window)
Copyright © 2001 Elsevier Science Ltd. All rights reserved.

Application of DQM as an effective simulation tool for buckling response of delaminated composite plates

Farid TaheriCorresponding Author Contact Information, E-mail The Corresponding Author, a and Shapour Moradib

a Department of Civil Engineering, Dalhousie University, P.O. Box 1000, Halifax, NS, Canada B3J 2X4 b Department of Mechanical Engineering, Shaheed Chamran University, Ahwaz, Iran

Available online 9 February 2001.

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Abstract

The application of differential quadrature method (DQM), as an effective and robust numerical method, for the analysis of buckling of delaminated composite plates is introduced. The analysis investigated the response of laminated composite plates hosting a circular or an elliptical delamination. The delaminations were assumed to be fairly thinner than the plate hosting them, and thus, they could be treated as plates with clamped edges. Several case studies were used to verify the integrity of DQM in predicting the buckling strain of the plates. The investigation included the examination of several parameters influencing the buckling strength. The results obtained from DQM were compared with those obtained by the Rayleigh–Ritz and finite element solutions of other workers.

Article Outline

1. Introduction
2. Differential quadrature method
3. Formulation
4. Loading and boundary conditions
5. DQM considerations
6. Case studies
7. Conclusions
Acknowledgements
References










Composite Structures
Volume 51, Issue 4, April 2001, Pages 439-449
 
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