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Noise reduction for temperature-sensitive paint measurement contaminated by strong background radiation in a high enthalpy hypersonic tunnel 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 7
作者:  Peng, Di;  Liu, Xu;  Jiao, Lingrui;  Li, Ziyan;  Wen, Xin;  Yuan CK(苑朝凯);  Han GL(韩桂来);  Liu YF(刘云峰);  Liu, Yingzheng;  Jiang ZL(姜宗林)
Adobe PDF(3477Kb)  |  收藏  |  浏览/下载:250/48  |  提交时间:2021/03/30
Temperature-sensitive paint  Time-resolved measurement  Hypersonic flow  Background radiation  
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:324/169  |  提交时间:2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8
作者:  Luo K(罗凯);  Wang Q(汪球);  Li JW(栗继伟);  Li JP(李进平);  Zhao W(赵伟)
Adobe PDF(2023Kb)  |  收藏  |  浏览/下载:312/100  |  提交时间:2020/11/30
Quasi-one-dimensional  Detonation  Shock tunnel  Shock speed  
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:253/79  |  提交时间:2020/08/26
Shock tunnel  Detonation driver  Diaphragm  Dual ignition  High-enthalpy flow  
Influence of test model material on the accuracy of transient heat transfer measurements in impulse facilities 期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2019, 卷号: 104, 页码: 59-66
作者:  Wang Q(汪球);  Olivier H;  Einhoff J;  Li JP(李进平);  Zhao W(赵伟)
浏览  |  Adobe PDF(1085Kb)  |  收藏  |  浏览/下载:417/100  |  提交时间:2019/05/29
Heat transfer measurement  Lateral heat conduction  Shock tunnel  Thermocouple  Hypersonic  
Comparative Heat Flux Measurement of a Sharp Cone Between Three Hypersonic Test Facilities at LHD 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Wang Q(汪球);  Lu P(卢盼);  Li JW(栗继伟);  Wu S(吴松);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
Adobe PDF(299Kb)  |  收藏  |  浏览/下载:84/33  |  提交时间:2023/03/17
Aerodynamic Force Measurement in a Large-Scale Shock Tunnel 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(556Kb)  |  收藏  |  浏览/下载:162/42  |  提交时间:2020/01/06
Aerodynamic Testing at Duplicating Hypersonic Flight Conditions with Hyper-Dragon 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Jiang ZL(姜宗林);  Yu HR(俞鸿儒)
浏览  |  Adobe PDF(523Kb)  |  收藏  |  浏览/下载:477/55  |  提交时间:2020/01/06
Aerodynamic Force Measurement Techniques in JF12 Shock Tunnel 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Liu YF(刘云峰);  Wang YP(汪运鹏);  Yuan CK(苑朝凯);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(532Kb)  |  收藏  |  浏览/下载:188/67  |  提交时间:2020/01/06
Numerical investigation of the axial impulse load during the startup in the shock tunnel 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 332-342
作者:  Meng BQ(孟宝清);  Han GL(韩桂来);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(1937Kb)  |  收藏  |  浏览/下载:262/86  |  提交时间:2018/10/30
Hypersonic  Shock tunnel  Start-up process  Impulse force  Vibration