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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./通讯作者:Zhou, Yan, Luo, Zhenbing
Authors:  Xie, Xuzhen;  Liu, Qiang;  Zhou, Yan;  Luo, Zhenbing;  Xie,Wei;  Bai, Guanghui;  Luo K(罗凯);  Wang Q(汪球);  Wu, Jianjun
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Hypersonic flow  High-enthalpy flow  Plasma synthetic jet  Shock wave  Flow control  
Theories and methods for designing hypersonic high-enthalpy flow nozzles 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 1, 页码: 318-339./通讯作者:Wang, Yunpeng
Authors:  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
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Boundary layer correction  High-enthalpy flow  Hypersonic wind tunnel  Nozzle design  Real-gas effects  
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./通讯作者:Luo, ZB, Zhou, Y (corresponding author), Natl Univ Def Technol, Changsha 410073, Peoples R China.
Authors:  Xie, Wei;  Luo, Zhenbing;  Zhou, Yan;  Gao, Tianxiang;  Wu, Yun;  Wang Q(汪球)
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SparkJet  High-enthalpy hypersonic flow  Shock control  Shock-on-shock interaction  Air supply  
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038./通讯作者:HU, Zongmin
Authors:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  Favorite  |  View/Download:403/187  |  Submit date:2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique