Calculation of pitch damping coefficients for projectiles
Author:
Affiliation:
1. Cranfield College of Aeronautics, Bedford, United Kingdom
2. DRA, Sevenoaks, United Kingdom
3. Defence Research Establishment Valcartier, Quebec, Canada
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-405
Reference21 articles.
1. FREE FLIGHT MOTION OF SYMMETRIC MISSILES
2. Aerodynamics of bodies of revolution in coning motion.
3. Results from a new wind-tunnel apparatus for studying coning and spinning motions of bodies of revolution
4. Nonlinear Aerodynamics of Bodies in Coning Motion
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