Use of Material Tailoring to Improve Buckling Capacity of Elliptical Composite Cylinders
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
2. AREVA NP Inc., Lynchburg, Virginia 24501
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.32495
Reference24 articles.
1. Mechanics of Cylindrical Shells With Non-Circular Cross-Section: A Survey
2. Buckling analysis of laminated cylindrical shells with arbitrary noncircular cross section
3. Buckling and Initial Post-Buckling Behavior of Laminated Oval Cylindrical Shells Under Axial Compression
4. Buckling and vibration of cross-ply laminated non-circular cylindrical shells
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