Effects of supersonic nozzle guide vanes on the performance and flow structures of a rotating detonation combustor

被引：0
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作者：
Shen, Dawen [1 ]
Cheng, Miao [1 ]
Wu, Kevin [1 ]
Sheng, Zhaohua [1 ]
Wang, Jianping [1 ]
机构：
[1] Center for Combustion and Propulsion, CAPT & SKLTCS, Department of Mechanics and Engineering Sciences, College of Engineering, Peking University, Beijing,100871, China
来源：
Acta Astronautica | 2022年 / 193卷
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页码：90 / 99
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