Postbuckling fatigue behavior of graphite-epoxy stiffeners
Author:
Affiliation:
1. General Dynamics Corp., Convair Div., San Diego, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1982-779
Reference4 articles.
1. Stability of graphite/epoxy structures with arbitrary symmetrical laminates
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Postbuckling and Crippling of I-Section Composite Stiffeners;Journal of Aerospace Engineering;1995-01
2. Scale Effects in Buckling, Postbuckling, and Crippling of Graphite-Epoxy 2-section Stiffeners;AIAA Journal;1992-11
3. Local crippling of thin-walled graphite-epoxy stiffeners;AIAA Journal;1991-11
4. Buckling and Postbuckling of Thin-Walled Composite Stiffeners;International Journal of Space Structures;1991-06
5. Recent advances in analysis of laminated beams and plates. Part I - Sheareffects and buckling.;AIAA Journal;1989-07
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