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

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

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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