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Experimental study on the full cycle evolution of high-intensity atmospheric dc arc discharge from breakdown to extinguishment 期刊论文
PHYSICAL REVIEW E, 2024, 卷号: 109, 期号: 2, 页码: 11
作者:  Hu YH(胡亚豪);  Sun, SuRong;  Meng X(孟显);  Huang HJ(黄河激);  Wang, Hai Xing
收藏  |  浏览/下载：8/0  |  提交时间：2024/04/15
Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition 期刊论文
AIP ADVANCES, 2021, 卷号: 11, 期号: 12, 页码: 17
作者:  Zhang WS(张文硕);  Zhang, Zijian;  Jiang ZL(姜宗林);  Han X(韩信);  Liu, Yunfeng;  Wang, Chun
Adobe PDF(15045Kb)  |  收藏  |  浏览/下载：237/22  |  提交时间：2022/01/24
Near-field relaxation subsequent to the onset of oblique detonations with a two-step kinetic model 期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 9, 页码: 11
作者:  Teng, Honghui;  Ng, Hoi Dick;  Yang PF(杨鹏飞);  Wang, Kuanliang
Adobe PDF(5463Kb)  |  收藏  |  浏览/下载：149/29  |  提交时间：2022/01/13
Characterizing combustion of a hybrid rocket using laser absorption spectroscopy 期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2021, 卷号: 127, 页码: 9
作者:  Fang SH(方思晗);  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Li RJ(李仁杰);  Li, Jing;  Zhang, Zhedian;  Liu, Yan;  Yu XL(余西龙)
Adobe PDF(4367Kb)  |  收藏  |  浏览/下载：515/62  |  提交时间：2021/08/03
Tunable diode laser absorption spectroscopy  Hybrid rocket motor  Temperature  Partial pressure  Combustion efficiency  
Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
作者:  Zhou GX(周功喜);  Zhang X(张旭);  Li JP(李进平);  Zhang XY(张晓源);  Zhang SZ(张仕忠);  Lin X(林鑫);  Li F(李飞);  Chen H(陈宏);  Yue LJ(岳连捷);  Yu XL(余西龙)
Adobe PDF(4108Kb)  |  收藏  |  浏览/下载：329/47  |  提交时间：2021/09/07
High mach number scramjet  Circular cross-section  TDLAS  Multi-view simultaneous imaging  POD  
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  
Formation of stabilized oblique detonation waves in a combustor 期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
作者:  Zhang ZJ(张子健);  Wen, Chihyung;  Zhang WS(张文硕);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
Adobe PDF(3599Kb)  |  收藏  |  浏览/下载：327/89  |  提交时间：2021/03/03
Oblique detonation wave  Combustor  Oblique detonation engine  Normal detonation wave  Boundary layer separation  
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  
Impulse force-measurement system 期刊论文
SHOCK WAVES, 2020, 页码: 11
作者:  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(1551Kb)  |  收藏  |  浏览/下载：238/67  |  提交时间：2020/11/30
Shock tunnel  High enthalpy  Aerodynamic force measurement  Strain gauge balance