Elastic Instability of a Cylindrical Shell Under Arbitrary Circumferential Variation of Axial Stress
Author:
Affiliation:
1. Bell Aerosystems Company,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.8776
Reference18 articles.
1. A Simple Method of Matric Structural Analysis
2. A Simple Method of Matric Structural Analysis: Part II-Effects of Taper and Consideration of Curvature
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