Postbuckling behavior of selected flat stiffened graphite-epoxy panels loaded in compression
Authors:
- 1 August 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 23 (8) , 1236-1246
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
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- A PRELIMINARY DESIGN PROCEDURE FOR COMPOSITE PANELS WITH OPEN-SECTION STIFFENERS LOADED IN THE POST-BUCKLING RANGE1980
- Effect of Impact Damage and Holes on the Compressive Strength of a Graphite/Epoxy Laminate1979
- General Panel Sizing Computer Code and Its Application to Composite Structural PanelsAIAA Journal, 1979
- The buckling and post-buckling behaviour of composite plates under biaxial loadingInternational Journal of Mechanical Sciences, 1975
- Evaluation of various analytical models for buckling and vibration of stiffened shells.AIAA Journal, 1973
- The Large Deflection and Post-Buckling Behaviour of Some Laminated PlatesAeronautical Quarterly, 1973