Effects of afterburning on a solid divert control system. II
Author:
Affiliation:
1. U.S. Army, Aviation and Missile Command, Redstone Arsenal, AL
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-3620
Reference12 articles.
1. Gordonand McBride,"Computer Programfor Calculation of Complex Chemical Equilibrium Compositions, Rocket Performance, Incident and Reflected Shocks, and Chapman-Jouguet Detonations,"NASA SP-273,March 1976.
2. Upwind unstructured scheme for three-dimensional combusting flows
3. Unstructured grid Navier-Stokes solver for turbulent reacting flows with dynamic domains
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1. Jet interaction effects on a missile with aerodynamic control surfaces;37th Aerospace Sciences Meeting and Exhibit;1999-01-11
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