Numerical Study on Aerodynamic Performance of Turbine for Rotating Detonation Combustor

被引：0
|
作者：
Meng, Bo-Wei [1 ]
Yang, Bo [2 ]
Zhang, Cui-Zhen [3 ]
Wang, Feng-Ming [3 ]
Ma, Hu [1 ]
Xia, Zhen-Juan [1 ]
Zhou, Chang-Sheng [1 ]
机构：
[1] School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing,210094, China
[2] Xi’an Aerospace Power Research Institute, Xi’an,710100, China
[3] China Aero Engine Research Institute, Beijing,101399, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2023年 / 44卷 / 09期
关键词：
D O I：
10.13675/j.cnki.tjjs.2208076
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