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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
作者:  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2554Kb)  |  收藏  |  浏览/下载：140/27  |  提交时间：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
作者:  Xie, Wei;  Luo, Zhenbing;  Zhou, Yan;  Gao, Tianxiang;  Wu, Yun;  Wang Q(汪球)
Adobe PDF(8485Kb)  |  收藏  |  浏览/下载：115/57  |  提交时间：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
作者:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  收藏  |  浏览/下载：320/168  |  提交时间：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
作者:  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)  |  收藏  |  浏览/下载：251/78  |  提交时间：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
作者:  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.
浏览  |  Adobe PDF(532Kb)  |  收藏  |  浏览/下载：627/151  |  提交时间：2015/04/28
Detonation Driver  Shock-expansion Tube  High-enthalpy Flow  Test Flow