Cyclic Buckling Tests Under Combined Loading on Predamaged Composite Stiffened Boxes
Author:
Affiliation:
1. 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.J050999
Reference16 articles.
1. COCOMAT—improved material exploitation of composite airframe structures by accurate simulation of postbuckling and collapse
2. CFRP fuselage structures - postbuckling permitted
3. Postbuckling behavior of selected curved stiffened graphite-epoxy panels loaded in axial compression
4. Buckling and postbuckling investigations of imperfect curved stringer-stiffened composite shells. Part B: Computational investigations
5. Buckling Behavior of Composite Laminated Stiffened Panels Under Combined Shear-Axial Compression
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