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Experimental study on shock interaction control of double wedge in high-enthalpy hypersonic flow subject to plasma synthetic jet 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2024, 卷号: 37, 期号: 4, 页码: 151-165
Authors:  Xie, Xuzhen;  Liu, Qiang;  Zhou, Yan;  Luo, Zhenbing;  Xie,Wei;  Bai, Guanghui;  Luo K(罗凯);  Wang Q(汪球);  Wu, Jianjun
Favorite  |  View/Download：10/0  |  Submit date：2024/06/11
Hypersonic flow  High-enthalpy flow  Plasma synthetic jet  Shock wave  Flow control  
Investigation of dual ignition for a detonation-driven shock tunnel in forward driving mode 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 5, 页码: 1468-1475
Authors:  Wang Q(汪球);  Luo K(罗凯);  Li JW(栗继伟);  Li JP(李进平);  Zhao W(赵伟)
Adobe PDF(2057Kb)  |  Favorite  |  View/Download：276/85  |  Submit date：2020/08/26
Shock tunnel  Detonation driver  Diaphragm  Dual ignition  High-enthalpy flow  
高焓流动中电子密度的静电探针测试技术研究 期刊论文
中国科学. 技术科学, 2016, 卷号: 46, 期号: 5, 页码: 500-508
Authors:  汪球;  黄建栋;  聂春生;  赵伟;  余西龙
View  |  Adobe PDF(643Kb)  |  Favorite  |  View/Download：438/112  |  Submit date：2016/12/16
High Enthalpy  Shock Tunnel  Electron Denstiy  Electrostatci Probe  
高超声速电离绕流中电子密度的静电探针测量方法研究 期刊论文
实验流体力学, 2013, 卷号: 27, 期号: 6, 页码: 64-69+85
Authors:  汪球;  赵伟;  余西龙;  姜宗林
Adobe PDF(487Kb)  |  Favorite  |  View/Download：912/237  |  Submit date：2014/01/24
静电探针  电子密度  高超声速  高焓激波风洞  Electrostatic Probe  Electron Density  Hypersonic  High Enthalpy Shock Tunnel