Inhibition Effect of Water Injection on Afterburning of Rocket Motor Exhaust Plume

Author:

Yi Jiang,Yanli Ma,Weichen Wang,Liwu Shao

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference25 articles.

1. Buckley F T, Myers R B. Studies of solid rocket exhaust afterburning with a finite difference equilibrium chemistry plume model. JANNAF 6th Plume Technology Meeting. 1971; 59-80.

2. Kennedy R E, Olmsted G S, Ryan R E, et al. Cooling apparatus for a missile launching system. U.S. Patent No.5847307, 1998.

3. Calhoon W H Jr. Evaluation of afterburning cessation mechanisms in fuel rich rocket exhaust plumes. ADA404895, 1998.

4. Pressure effects on the spectral behavior of the thermal field in non-reacting and low Damkohler reacting flows;Bounif;International Journal of Thermal Sciences,1999

5. Roblin A, Dubois I, Grisch F, et al. Comparison between computations and measurements of a H2/LOX rocket motor plume. AIAA-2002-3107, 2002.

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