Technique for the prediction of airfoil flutter characteristics in separated flow
Author:
Affiliation:
1. National Central University, Chong-Li, Taiwan
2. NASA Lewis Research Center, Cleveland, Ohio
3. Georgia Institute of Technology, Atlanta, Georgia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45740
Reference22 articles.
1. 4Ballhaus, W. F. and Goorjian, P.M. "Computation of Unsteady Transonic Flow by the Indicial Method,'ML4y4 Journal, Vol.16, Feb. 1978, pp.117-126.
2. Flutter analysis of a NACA 64A006 airfoil in small disturbance transonic flow
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