Spinning Tail Aerodynamics of a Low Cost Precision Guided Missile
Author:
Affiliation:
1. U.S. Army Aviation and Missile Command
2. University of Alabama in Huntsville
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-3935
Reference19 articles.
1. HYDRA 70 MK66 Aerodynamics and Roll Analysis
2. 2Dahlke, C. W., Deep, R. A., and Oskay, V. "Techniques for Roll Tailoring for Missiles with Wrap-Around Fins," AIAA Paper 83-0463, January1983.
3. Subsonic and transonic aerodynamics of a wraparound fin configuration
4. 4Abate, G. L., and Winchenbach, "Aerodynamics of Missiles with Slotted Fin Configurations," AIAApaper 91-0676,January1991.
5. 5Tilmann, C. P., Huffman, R. E. Jr., Buter, T. A., and Bowersox, R. D. W. "Characterization of the Flow Structure in the Vicinity of a Wrap-Around Fin at Supersonic Speeds," AIAA Paper 96-0190, January1996.
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