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Assessment of thermochemical models on nonequilibrium flowfield and radiation in shock-heated nitrogen 期刊论文
COMPUTERS & FLUIDS, 2025, 卷号: 289, 页码: 17./通讯作者：Hong, Qizhen, Sun, Quanhua
Authors:  Zhang YZ(张宇哲);  Hong QZ(洪启臻);  Wang XY(王小永);  Yang, Chao;  Sun QH(孙泉华)
Favorite  |  View/Download：217/0  |  Submit date：2025/02/24
High enthalpy flow  Thermochemical nonequilibrium model  Vibration-dissociation coupling  Nonequilibrium radiative metric  
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
Favorite  |  View/Download：118/0  |  Submit date：2024/06/11
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)
Adobe PDF(2554Kb)  |  Favorite  |  View/Download：251/60  |  Submit date：2022/06/10
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)
Adobe PDF(8485Kb)  |  Favorite  |  View/Download：218/96  |  Submit date：2022/10/25
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：457/236  |  Submit date：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
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./通讯作者：Li, Jiwei
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：334/97  |  Submit date：2020/08/26
Shock tunnel  Detonation driver  Diaphragm  Dual ignition  High-enthalpy flow  
Development of the detonation-driven expansion tube for orbital speed experiments 期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 4, 页码: 695-700
Authors:  Jiang ZL(姜宗林);  Wu B(吴波);  Gao YL;  Zhao W(赵伟);  Hu ZM(胡宗民);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(532Kb)  |  Favorite  |  View/Download：768/204  |  Submit date：2015/04/28
Detonation Driver  Shock-expansion Tube  High-enthalpy Flow  Test Flow