Control of aeroelastic divergence
Author:
Affiliation:
1. Grumman Aerospace Corporation, Bethpage, New York
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.48204
Reference15 articles.
1. 3Sevart, F. "Development of Active Flutter-Suppression Wind-Tunnel Testing Technology," AFFDL-TR-74-126,1975.
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4. Integrated aerodynamic-structural-control wing design;4th Symposium on Multidisciplinary Analysis and Optimization;1992-08-17
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