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Gaseous Detonation Physics and Its Universal Framework Theory 专著
Beijing:Springer Nature, 2022
作者:  Jiang ZL(姜宗林);  Teng, Honghui
Adobe PDF(13641Kb)  |  收藏  |  浏览/下载：104/2  |  提交时间：2023/03/23
Design of a milli-newton force balance for hypersonic rarefied wind tunnel 期刊论文
MEASUREMENT, 2021, 卷号: 185, 页码: 7
作者:  Wu CW(吴臣武);  Liu C(刘聪);  Hu DL(胡灯亮);  Liu HL(刘宏立);  Huang HJ(黄河激)
Adobe PDF(4178Kb)  |  收藏  |  浏览/下载：283/67  |  提交时间：2021/11/15
Strain  Balance  Milli-newton  Design  Calibration  
Advances in plasma-assisted ignition and combustion for combustors of aerospace engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
作者:  Li, Mengzhe;  Wang, Zhikai;  Xu, Rongguang;  Zhang, Xiaoliang;  Chen, Zhitong;  Wang Q(汪球)
Adobe PDF(8841Kb)  |  收藏  |  浏览/下载：268/107  |  提交时间：2021/11/01
Non-equilibrium plasma  Plasma-assisted ignition  Plasma-assisted combustion  Aerospace engine  Combustor  Extreme condition  
Quantitative measurement of the mixture ratio for ADN-based liquid propellants using laser-induced breakdown spectroscopy 期刊论文
JOURNAL OF ANALYTICAL ATOMIC SPECTROMETRY, 2021, 页码: 11
作者:  Wang FY(王方仪);  Zhang SH(张少华);  Yu XL(余西龙);  Lin X(林鑫);  Li, Jing;  Liu, Yan
Adobe PDF(1277Kb)  |  收藏  |  浏览/下载：296/43  |  提交时间：2021/09/08
Instability mechanism and discharge regime diagnosis of microthrusters based on plasma properties 期刊论文
APPLIED OPTICS, 2021, 卷号: 60, 期号: 4, 页码: 1021-1030
作者:  Wang FY(王方仪);  Zhang SH(张少华);  Liu, Yan;  Yu XL(余西龙)
Adobe PDF(9020Kb)  |  收藏  |  浏览/下载：203/42  |  提交时间：2021/04/07
Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 12
作者:  Yuan CK(苑朝凯);  Jiang ZL(姜宗林)
Adobe PDF(3790Kb)  |  收藏  |  浏览/下载：380/57  |  提交时间：2021/03/03
Hypersonics  Shock tunnels  Flow characteristics  
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：321/168  |  提交时间：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Effects of inflow Mach number on oblique detonation initiation with a two-step induction-reaction kinetic model 期刊论文
COMBUSTION AND FLAME, 2018, 卷号: 193, 页码: 246-256
作者:  Yang PF;  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Ng HD
浏览  |  Adobe PDF(2840Kb)  |  收藏  |  浏览/下载：761/121  |  提交时间：2018/10/30
Oblique detonation  Induction-reaction kinetics  Initiation length  Initiation structure  
AERODYNAMIC DRAG MEASUREMENT IN A HIGH-ENTHALPY SHOCK TUNNEL 会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
作者:  Wang YP(汪运鹏);  Jiang ZL(姜宗林);  Teng HH(滕宏辉)
浏览  |  Adobe PDF(4139Kb)  |  收藏  |  浏览/下载：269/57  |  提交时间：2019/04/19
Numerical investigation of the effects of shock tube geometry on the propagation of an ideal blast wave profile 期刊论文
SHOCK WAVES, 2017, 卷号: 27, 期号: 5, 页码: 771-779
作者:  Li, X. D.;  Hu ZM(胡宗民);  Jiang ZL(姜宗林);  Hu, ZM (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Hu, ZM (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
浏览  |  Adobe PDF(2166Kb)  |  收藏  |  浏览/下载：425/107  |  提交时间：2017/11/16
Blast Wave Profile  Biological Shock Tube  Blast Overpressure  Geometrical Configuration