Computational parametric study of the Magnus effect on boattailed shell at supersonic speeds
Author:
Affiliation:
1. U.S. Army, Ballistics Research Laboratories, Aberdeen Proving Ground, MD
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1981-1900
Reference9 articles.
1. Numerical Simulation of Steady Supersonic Viscous Flow
2. Numerical simulation of steady supersonic flow over an ogive-cylinder-boattail body
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