Roll motion of a wraparound fin configuration at subsonic and transonic Mach numbers
Author:
Affiliation:
1. Agency of Defense Development, Republic of Korea
2. Air Force Armament Laboratory, Eglin Air Force Base, Florida
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.20100
Reference6 articles.
1. FREE FLIGHT MOTION OF SYMMETRIC MISSILES
2. Subsonic Free-Flight Data for a Complex Asymmetric Missile
3. 5Sabot, S.M., Chapman, G.T., and Winchenbach, G.L. "Comparison of Various Drag Coefficient Expansions Using Polynomials and Splines," AIAA Paper 84-2113, Aug. 1984.
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2. Nonlinear Yaw-Pitch-Roll Coupling of Unguided Missiles with Wraparound Fins;Journal of Spacecraft and Rockets;2000-11
3. Non-linear flight dynamics of unguided missiles with wrap-around fins;23rd Atmospheric Flight Mechanics Conference;1998-08-10
4. Magnus Effects on Stability of Wraparound-Finned Missiles;Journal of Spacecraft and Rockets;1998-07
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