CFD Prediction of M910 Projectile Aerodynamics: Unsteady Wake Effect on Magnus Moment
Author:
Affiliation:
1. U.S. Army Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-6580
Reference35 articles.
1. 4Graham, M. J., Weinacht, P., Brandeis, J., and Angelini, R. "A Numerical Investigation of Supersonic Jet Interaction for Finned Bodies,"U.S. Army ResearchLaboratory,ARL-TR-2312,AberdeenProving Ground, MD,Dec. 2000.
2. Aerodynamic Analysis of a Spinning Missile with Dithering Canards
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