Navier-Stokes computations of projectile base flow with and without mass injection
Author:
Affiliation:
1. U.S. Army Ballistic Research Laboratory, Aberdeen Proving Ground, Maryland
2. Stanford University, Palo Alto, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9091
Reference21 articles.
1. Cylindrical and boat-tailed afterbodies in transonic flow with gas ejection
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