Author:
Yi Jiang,Yanli Ma,Weichen Wang,Liwu Shao
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.
Cited by
16 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献