Structural optimization of axially compressed cylinders, consideringring-stringer eccentricity effects.
Author:
Affiliation:
1. Lockheed Missiles and Space Company, Palo Alto, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.28637
Reference13 articles.
1. Stability of stiffened cylinders.
Cited by 20 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Analysis and Limit State Design of Stiffened Plates and Shells: A World View;Applied Mechanics Reviews;2009-02-13
2. A Contribution to the stability of stiffened plates under uniform compression;Computers & Structures;1998-03
3. Optimization Of Stiffened Cylindrical Shells Subjected To Destabilizing Loads;Structural Optimization: Status And Promise;1993-01-01
4. Shells;Optimal Structural Design under Stability Constraints;1988
5. Panda—Interactive program for minimum weight design of stiffened cylindrical panels and shells;Computers & Structures;1983-01
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