Author:
Dong Wenjie,Wang Jianhua,Chen Siyuan,Ai Bangcheng,Luo Xiaoguang
Funder
Natural Science Foundation of China
China Academy of Aerospace Aerodynamics
Subject
Industrial and Manufacturing Engineering,Energy Engineering and Power Technology
Reference31 articles.
1. D. Greuel, A. Herbertz, O.J. Haidn, et al., Transpiration cooling applied to C/C liners of cryogenic liquid rocket engines, in: 40th Joint Propulsion Conference, AIAA Reston, VA, 2004.
2. Transpiration cooling effects on nozzle heat transfer and performance;Keener;J. Spacecr. Rockets,1995
3. W. Liu, Q. Chen, B. Wu, Transpiration cooling of rocket thrust chamber with liquid oxygen, AIAA Aerospace Sciences Meeting and Exhibit, 1998.
4. M. Thames, D. Landrum, J. Hendricks, Thermal/fluid study of perforated plates for transpiration cooled rocket chambers, in: AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 1998.
5. K. Fröhlke, O.J. Haidn, E. Serbest, New experimental results on transpiration cooling for hydrogen/oxygen rocket combustion chambers, in: 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cleveland, OH, 1998.
Cited by
38 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