Experimental Study on Quasi-Limit-Cycle Wing Rock of a Chined Forebody Configuration at High Angle of Attack
Author:
Affiliation:
1. Beihang University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2309
Reference9 articles.
1. Wing/vortex interactions and wing rock
2. The unsteady aerodynamics of slender wings and aircraft undergoing large amplitude maneuvers
3. 3Erickson, G. E., and Brandon, J. M. "Low-Speed Experimental Study of the Vortex Flow Effects of a Fighter Forebody Having Unconventional Cross-Section," 12th Atmospheric Flight Mechanics Conference, AIAA, Snowmass, CO, 1985, pp.257, 290.
4. 4Erickson, G. E., and Brandon, J. M. "On the Nonlinear Aerodynamic and Stability Characteristics of a Generic Chine-Forebody Slender-Wing Fighter Configuration," 5th Applied Aerodynamics Conference, AIAA, Monterey, CA, 1987, pp.607, 641.
5. 5Ross, F. W., and Magness, C. L. "Yaw Effects on the High-Alpha Flow Field of a Chined Forebody," 32nd Aerospace Sciences Meeting and Exhibit, AIAA, Reno, NV, 1994.
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