Computations of projectile Magnus effect at transonic velocities
Author:
Affiliation:
1. U.S. Army, Ballistics Research Laboratory, Aberdeen Proving Ground, MD
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1983-237
Reference20 articles.
1. Computations of Magnus effects for a yawed, spinning body of revolution
2. a. Supersonic Flow", AIAA Paper No. 80-1586-CP, August 11-13, 1980.
3. Navier-Stokes computations for conventional and hollow projectile shapes at transonic velocities
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