PNS computations for spinning shell at moderate angles of attack andfor long L/D finned projectiles
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/10.2514/6.1985-273
Reference47 articles.
1. Computational parametric study of the Magnus effect on boattailed shell at supersonic speeds
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3. rated Turbulent Flows," AIAA Paper No. 78-257,
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2. Navier-Stokes computations of finned kinetic energy projectile base flow;20th Atmospheric Flight Mechanics Conference;1995-08-07
3. Simple turbulence models for supersonic flows - Bodies at incidence and compression corners;AIAA Journal;1991-11
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