Combined Compression-Torsion Buckling Tests of Laminated Composite Cylindrical Shells
Author:
Affiliation:
1. General Dynamics Corporation, Fort Worth, Tex.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.59889
Reference8 articles.
1. Elastic Torsional Buckling of Thin-Walled Composite Cylinders
2. Wu, C., Buckling of Anisotropic Circular Cylindrical Shells, Ph.D dissertation,Case-Western Reserve University, Cleveland, Ohio, June 1971.
3. On experimental technique for interaction curves of buckling of shells
4. Compression Buckling Tests of Laminated Graphite-Epoxy Curved Panels
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