Approximate Solution and Optimum Design of Compression-Loaded, Postbuckled Laminated Composite Plates.-Reference-Cited by-同舟云学术

Approximate Solution and Optimum Design of Compression-Loaded, Postbuckled Laminated Composite Plates.

Published:2005-04 Issue:4 Volume:43 Page:906-914
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Diaconu Cezar G.¹,Weaver Paul M.¹

Affiliation:

1. University of Bristol, Bristol, England BS8 1TR, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.10827

Reference16 articles.

1. The buckling and post-buckling behaviour of composite plates under biaxial loading

2. Postbuckling of orthotropic composite plates loaded in compression

3. Importance of anisotropy on buckling of compression-loaded symmetriccomposite plates

4. 4Chia, C. Y., Nonlinear Analysis of Plates, McGraw-Hill, New York, 1980, pp.303-308.

5. 5Zhang, Y. "Buckling and Postbuckling Behaviour of Generally Layered Composite Panels," Ph.D. Dissertation,Dept. of Aeronautics, Imperial College, London,Oct. 1982.

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