Hopf-Bifurcation Analysis of Airfoil Flutter at Transonic Speeds
Author:
Affiliation:
1. U.S. Air Force Institute of Technology, Wright-Patterson Air Force Base, Ohio 45433-7542
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2447
Reference15 articles.
1. Computational methods for unsteady transonic flows
2. Current status of computational methods for transonic unsteady aerodynamics and aeroelastic applications
3. Technique for the prediction of airfoil flutter characteristics in separated flow
4. Nonlinear aspects of the transonic aeroelastic stability problem
5. Bifurcation analysis of aircraft pitching motions about large mean angles of attack
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