Author:
Miao Heyang,Wang Zhongwei,Niu Yaobin
Funder
National Natural Science Foundation of China
Subject
Industrial and Manufacturing Engineering,Energy Engineering and Power Technology
Reference44 articles.
1. Review on active thermal protection and its heat transfer for airbreathing hypersonic vehicles;Zhu;Chin. J. Aeronaut.,2018
2. Survey on the mode transition technique in com-bined cycle propulsion systems;Huang;Aerosp. Sci. Technol.,2014
3. Nicolas Gascoin, Philippe Gillard, Emmanuel Dufour, Youssoufi Toure, Validation of transient cooling modeling for hypersonic application, J. Thermophys. Heat Transf. 21(1) (2007) 86–94.
4. M.H. Naraghi, S. Dunn, D. Coats, Dual regenerative cooling circuits for liquid rocket engines, in: Proceedings of 42nd AIAA/ASME/SAE/ ASEE Joint Propulsion Conference and Exhibit, California, USA, 9–12 July 2006.
5. S.J. Scotti, C.J. Martin, S.H. Lucas, Active cooling design for scramjet engines using optimization methods. Technical report No. NASA 100581, March, 1998.
Cited by
33 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