Aerodynamic Control of a Small Projectile

Author:

Patel Mehul1,Sowle Zak1,Stucke Russ1,Ng Terry2

Affiliation:

1. Orbital Research Inc.

2. University of Toledo

Publisher

American Institute of Aeronautics and Astronautics

Reference16 articles.

1. Genesis simulation of a modified VISTA/F-16

2. 5Commerce Business Daily, Jan. 13, 2004, "Acquisition Strategy for FY04 Contract Award for the Following: IRCM Flare Family of M-206, MJU-7A/B and MJU-10B."

Cited by 5 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. Effect of Slender Body Geometry on Flow Control at High Alpha;28th AIAA Applied Aerodynamics Conference;2010-06-28

2. Forebody Geometry Effects on the Flow of a Blunt-Nose Projectile at High Alpha;Journal of Aircraft;2007-11

3. Coning Motion Control of a Blunt-Nose Projectile Using Small Deployable Strakes;25th AIAA Applied Aerodynamics Conference;2007-06-15

4. Yaw Control of a Blunt-Nose Projectile at High Angles of Attack Using Strakes;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08

5. Range and Endgame Performance Assessment of a Smart Projectile Using Hingeless Flight Control;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09

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