Numerical simulation on impingement cooling characteristics of pulsed detonation tube

被引:0
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作者
Wang, Xing-Tao [1 ]
Zhang, Jing-Zhou [1 ]
Tan, Xiao-Ming [1 ]
机构
[1] College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
来源
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2011年 / 26卷 / 11期
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页码:2515 / 2521
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