Effect of Cutouts or Low-Speed Impact Damage on the Postbuckling Behavior of Composite Plates Loaded in Shear
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1990-966
Reference17 articles.
1. Effect of Impact Damage and Holes on the Compressive Strength of a Graphite/Epoxy Laminate
2. Postbuckling and failure characteristics of selected flat rectangular graphite-epoxy plates loaded in compression
3. Postbuckling behavior of selected flat stiffened graphite-epoxy panels loaded in compression
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1. Cutout reinforcements for shear loaded laminate and sandwich composite panels;International Journal of Mechanics and Materials in Design;2007-12-11
2. Stress concentration and buckling behaviour of shear loaded composite panels with reinforced cutouts;Composite Structures;2007-09
3. Prediction of progressive failure in multidirectional composite laminated panels;International Journal of Solids and Structures;2007-05
4. Maximization of buckling load of laminated composite plates with central circular holes using MFD method;Structural and Multidisciplinary Optimization;2007-04-05
5. Intralaminar and interlaminar progressive failure analyses of composite panels with circular cutouts;Composite Structures;2004-04
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