Elastic buckling of composite cylindrical shells under torsion.
Author:
Affiliation:
1. Nova Scotia Technical College, Nova Scotia, Canada
2. University of Wisconsin, Madison, Wis
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.29398
Reference23 articles.
1. On the Theory of Laminated Anisotropic Shells and Plates
2. Elastic Stability of Orthotropic Shells
3. Stability of Orthotropic Cylindrical Shells Under Combined Loading
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