Buckling of Laminated Conical Shells Given the Variations of the Stiffness Coefficients
Author:
Affiliation:
1. Delft University of Technology, 2629 HS Delft, The Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.2765
Reference21 articles.
1. Laminated conical shells - Considerations for the variations of the stiffness coefficients
2. Stability of laminated composite circular conical shells under external pressure
3. Simple solutions for buckling of laminated conical shells
4. Buckling analysis of laminated composite conical shells
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