Minimum Mass Sizing of a Large Low-Aspect Ratio Airframe for Flutter-Free Performance
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.57380
Reference12 articles.
Cited by 8 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. Aeroelastic Design by Combining Conventional Practice with Bi-Level Integrated System Synthesis (BLISS);10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference;2004-08-30
2. Ein Abriß der Aeroelastizität;Computerdynamik der Tragwerke;1997
3. Trusses and Frames;Optimal Structural Design under Stability Constraints;1988
4. EISI-EAL: A general engineering analysis and design language;Finite Elements in Analysis and Design;1986-04
5. A multiloop robust controller design study using singular value gradients;Journal of Guidance, Control, and Dynamics;1985-07
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