Evaluation of various analytical models for buckling and vibration of stiffened shells.
Author:
Affiliation:
1. Lockheed Palo Alto Research Laboratory, Palo Alto, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference29 articles.
1. Effect of Eccentricity of Stiffeners on the General Instability of Stiffened Cylindrical Shells under Hydrostatic Pressure
2. Design criteria for axially loaded cylindrical shells
3. Analysis of ring-stiffened shells of revolution under combined thermal and mechanical loading
4. Timoshenko, S., Theory of Elastic Stability, McGraw-Hill, New York, 1936, Chap. 8, pp.325-350.
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