Techniques for roll tailoring for missiles with wrap-around fins

Author:

DAHLKE C.1,DEEP R.1,OSKAY V.2

Affiliation:

1. U.S. Army, Missile Command, Redstone Arsenal, AL

2. U.S. Army, Ballistics Research Laboratories, Aberdeen Proving Ground, MD

Publisher

American Institute of Aeronautics and Astronautics

Reference4 articles.

1. Dahlke, C. Wayne, "The Aerodynamic Characteristics of Wrap-Around Fins at Mach Numbers of 0.3 to 3.0". US Amy Missile Command, Redstone Arsenal, At.# Report No. RD-77-4, 15 Oct 76.

2. '"2.75 Inch Rocket Mark 66 MOD 1, NASA-Ames Wind Tunnel Data Report", Indian Head Technical Report, IHTR-795, Dec 82.

Cited by 4 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. Induced Aerodynamics of Wrap-Around Fins Using an Empirical Technique;25th AIAA Applied Aerodynamics Conference;2007-06-15

2. Spinning Tail Aerodynamics of a Low Cost Precision Guided Missile;21st AIAA Applied Aerodynamics Conference;2003-06-21

3. Magnus Effects on Stability of Wraparound-Finned Missiles;Journal of Spacecraft and Rockets;1998-07

4. Wrap-around finned missiles - Neat but nasty;22nd Atmospheric Flight Mechanics Conference;1997-08-11

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