Aerodynamic test and analysis of wrap around fins with base cavities
Author:
Affiliation:
1. USAF, Wright Lab., Eglin AFB, FL
2. Arrow Tech Associates, South Burlington, VT
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1994-51
Reference11 articles.
1. I. Washington. W.D. "Experimental Investigation of RollingMoment foraBody-Wing-Tail Missile Configuration with WrapAroundWings and Straight 'rails atSupersonicSpeeds,"AIAA Paper 83-2081, August 1983.
2. Winchenbach,G.L. Buff,R. S.,Whyte,R. H., Hathaway,W.H."Subsonic andTransonicAerodynamics of aWraparoundFin Configuration,"AIAA Paper85-0106,January 1985.
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1. Comparison of Flow field in the proximity of A Single Planar & Wrap-around Fin;International Journal of Aviation, Aeronautics, and Aerospace;2019
2. Rolling Moment Characteristic Analysis of Wrap-Around Fins;Journal of Applied Mechanics;2010-05-21
3. Roll-Rate Stability Limits of Unguided Rockets with Wraparound Fins;Journal of Spacecraft and Rockets;2006-07
4. Magnus Effects on Stability of Wraparound-Finned Missiles;Journal of Spacecraft and Rockets;1998-07
5. Wrap-around finned missiles - Neat but nasty;22nd Atmospheric Flight Mechanics Conference;1997-08-11
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