Unsteady flow separation on slender bodies at high angles of attack
Author:
Affiliation:
1. Lockheed Missiles and Space Co., Inc., Sunnyvale, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1990-2835
Reference27 articles.
1. J. Aircraft, Vol. 17, Aug. 1980, pp. 561-566.
2. Academy, Colorado Springs, August 1983, pp.
3. 1-9.
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Closed-Loop Missile Yaw Control via Manipulation of Forebody Flow Asymmetrics;Journal of Spacecraft and Rockets;2004-05
2. Rotating nose tip effects on slender body aerodynamics at high angles of attack;Journal of Spacecraft and Rockets;1995-11
3. An investigation of high angle of attack aerodynamics on a finned and finless body with a fineness ratio of 20.0;32nd Aerospace Sciences Meeting and Exhibit;1994-01-10
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