Buckling and post-buckling of orthotropic laminated plates-Reference-Cited by-同舟云学术

Buckling and post-buckling of orthotropic laminated plates

Published:1975-05-27 Issue: Volume: Page:
ISSN:
Container-title:16th Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

HARRIS G.¹

Affiliation:

1. Royal Aircraft Establishment, Farnborough, Hants., England

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1975-813

Reference6 articles.

1. stability problems far orthotropic and iaotropic plates under biaxial and uniaxial direct stress. Aeronautical Cuarterly. Vo 1.4. 1952. pp.83-92. (2) Lekhnitskii,S.C. Anisotropicpbtes, trans

2. problems of orthotropic pla,'.xutical b t E r l y , VOl.8. 1957. pp. (4) Harris. G.Z. The buckling and poet-buckling

3. behaviour of composite plates under biaxial loading. InternationaZ Journal of Uechmrical Soimces, vo 1.17. narch 1915, pp.187-202. (5) Ashton,J.E.and Whitney, J.M.Theoly of

4. hrinated pkltes. Technomic. Stamford, 1970, Chapter 2.

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