Automated optimum design of shells of revolution with application to ring-stiffened cylindrical shells with wavy walls
Author:
Affiliation:
1. Lockheed Martin Advanced Technology Center, Palo Alto, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-1663
Reference82 articles.
1. Sensitivity of buckling loads of anisotropic shells of revolution to geometric imperfections and design changes
2. GENOPT—a program that writes user-friendly optimization code
3. Evaluation of various analytical models for buckling and vibration of stiffened shells.
Cited by 5 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
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