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Experimental study on shock wave control in high-enthalpy hypersonic flow by using SparkJet actuator 期刊论文
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 416-425
Authors:  Xie, Wei;  Luo, Zhenbing;  Zhou, Yan;  Gao, Tianxiang;  Wu, Yun;  Wang Q(汪球)
Adobe PDF(8485Kb)  |  Favorite  |  View/Download：132/68  |  Submit date：2022/10/25
SparkJet  High-enthalpy hypersonic flow  Shock control  Shock-on-shock interaction  Air supply  
Advances in plasma-assisted ignition and combustion for combustors of aerospace engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
Authors:  Li, Mengzhe;  Wang, Zhikai;  Xu, Rongguang;  Zhang, Xiaoliang;  Chen, Zhitong;  Wang Q(汪球)
Adobe PDF(8841Kb)  |  Favorite  |  View/Download：283/109  |  Submit date：2021/11/01
Non-equilibrium plasma  Plasma-assisted ignition  Plasma-assisted combustion  Aerospace engine  Combustor  Extreme condition  
Effects of Cowl-Induced Expansion on the Wave Complex Induced by Oblique Detonation Wave Reflection 期刊论文
PROCESSES, 2021, 卷号: 9, 期号: 7, 页码: 10
Authors:  Wang, Aifeng;  Shang JH(尚佳豪);  Wang Q(汪球);  Wang KL(王宽亮)
Adobe PDF(3951Kb)  |  Favorite  |  View/Download：212/37  |  Submit date：2021/08/16
oblique detonation  asymmetric  nozzle  reflection