Postbuckling behavior of selected curved stiffened graphite-epoxy panels loaded in axial compression
- 1 March 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 26 (3) , 344-352
- https://doi.org/10.2514/3.9895
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
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- Postbuckling and failure characteristics of selected flat rectangular graphite-epoxy plates loaded in compressionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- General Panel Sizing Computer Code and Its Application to Composite Structural PanelsAIAA Journal, 1979
- Buckling and post-buckling of orthotropic laminated platesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
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- Buckling and postbuckling behavior of composite cylindrical shells under axial compressionAIAA Journal, 1970