Buckling of Composite Plates with a Reinforced Circular Cutout Subjected to Uniform and Non-Uniform Compression-Reference-Cited by-同舟云学术

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Buckling of Composite Plates with a Reinforced Circular Cutout Subjected to Uniform and Non-Uniform Compression

Published:2004-04-19 Issue: Volume: Page:
ISSN:
Container-title:45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference
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Author:

Oterkus Erkan,Barut Atila,Madenci Erdogan

Publisher

American Institute of Aeronautics and Astronautics

Reference16 articles.

1. 2Owen, V., and Klang, F. "Shear Buckling of Specially Orthotropic Plates with Centrally Located Cutouts," NASA Conference Publication 3087, Part 2, pp.695-706,1990.

2. Shear and compression buckling analysis for anisotropic panels with elliptical cutouts

3. Buckling and postbuckling of composite panels with cutouts subjected to combined loads

4. Vibration, buckling and parametric instability behaviour of plates with centrally located cutouts subjected to in-plane edge loading (Tension or compression)

5. Optimal design of symmetric laminates with cut-outs for maximum buckling load

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