Local buckling and crippling of thin-walled composite structures under axial compression
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, GA
2. McDonnell Douglas Aircraft Co., St. Louis, MO; Georgia Institute of Technology, Atlanta, GA
3. Sikorsky Aircraft, Stratford, CT
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1985-672
Reference15 articles.
1. Becker, H., Handbook of Structural Stabilitv. Part I1 -Buckling of Composite Elements, NACA TN 3782,1957.
2. Gerard G., Handbook of Structural Stability, Part IV - Failure of Plates and Composite Elements, NACA TN 3784,1957.
3. Crippling/column buckling analysis and test of graphite/epoxy-stiffened panels
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1. Experimental and analytical investigations on short GFRP composite compression members;Composites Part B: Engineering;2000-10
2. Postbuckling and Crippling of I-Section Composite Stiffeners;Journal of Aerospace Engineering;1995-01
3. Local crippling of thin-walled graphite-epoxy stiffeners;AIAA Journal;1991-11
4. Recent advances in analysis of laminated beams and plates. Part I - Sheareffects and buckling.;AIAA Journal;1989-07
5. Observations on compressive local buckling, postbuckling and crippling of graphite/epoxy airframe structure;27th Structures, Structural Dynamics and Materials Conference;1986-05-19
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