Buckling Behavior of Composite Laminated Stiffened Panels Under Combined Shear-Axial Compression
Author:
Affiliation:
1. Technion—Israel Institute of Technology, 32000 Haifa, Israel
2. Politecnico di Milano, 20156 Milano, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.27635
Reference15 articles.
1. Postbuckling behavior of composite-stiffened-curved panels loaded in compression
2. Postbuckling behavior of selected curved stiffened graphite-epoxy panels loaded in axial compression
3. Buckling Experiments: Experimental Methods in Buckling of Thin-Walled Structures
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