WING FLUTTER BOUNDARY PREDICTION USING UNSTEADY EULER AERODYNAMIC METHOD
Author:
Affiliation:
1. NASA LANGLEY RESEARCH CENTER, HAMPTON, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-1422
Reference27 articles.
1. namics and Aeroelasticity,Paper No. 1,October 1991.
2. ler Equations,"AIAA Paper No. 88-2281,April 1988.
3. vol. 28, pp. 778-788, November 1991.
4. No. 90-0435, January 1990.
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