Lower-Bound Analysis of Fiber-Reinforced Polymeric Laminated Cylindrical Shells
Author:
Affiliation:
1. Department of Civil, Environmental and Geomatic Engineering, University College London, London, England WC1E 6BT, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051691
Reference19 articles.
1. Toward a Probabilistic Preliminary Design Criterion for Buckling Critical Composite Shells
2. Stability of imperfect laminated cylinders - A comparison between theory and experiment
3. Experimental Buckling of Thin Composite Cylinders in Compression
4. SeideP.WeingartenV. I.PetersonJ. P. “Buckling of Thin-Walled Circular Cylinders, NASA Space Vehicle Design Criteria,” NASA SP-8007, 1965.
5. Future directions and challenges in shell stability analysis
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