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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：251/27  |  提交时间：2022/01/24
Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy 期刊论文
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 110-120
作者:  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Peng JL(彭锦龙);  Liu, Yan;  Zhang ZL(张泽林);  Fang SH(方思晗);  Yu XL(余西龙)
Adobe PDF(6496Kb)  |  收藏  |  浏览/下载：294/54  |  提交时间：2021/11/01
Hybrid rocket engine  Fuel mass flow rate  Tunable diode laser absorption spectroscopy  Temperature  Partial pressure  
Magnetic and Pressure Effects on E-H Mode Transition Power and Electron Energy Distribution in Helical Antenna-Coupled RF Plasma 期刊论文
IEEE TRANSACTIONS ON PLASMA SCIENCE, 2021, 卷号: 49, 期号: 9, 页码: 2806-2816
作者:  Wang CS(王传胜);  Liu, Xuhui;  Geng, Jinyue;  Li F(李飞);  Lin X(林鑫);  Yu XL(余西龙)
Adobe PDF(3369Kb)  |  收藏  |  浏览/下载：234/58  |  提交时间：2021/11/01
E-H mode transition  electron energy distribution function (EEDF)  helical antenna  magnetic  
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：525/64  |  提交时间：2021/08/03
Tunable diode laser absorption spectroscopy  Hybrid rocket motor  Temperature  Partial pressure  Combustion efficiency  
Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
作者:  Jiang ZL(姜宗林);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Wang C(王春);  Luo ZT(罗长童)
Adobe PDF(1806Kb)  |  收藏  |  浏览/下载：284/57  |  提交时间：2021/05/17
Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test  
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：209/43  |  提交时间：2021/04/07
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：262/52  |  提交时间：2021/03/30
Temperature-sensitive paint  Time-resolved measurement  Hypersonic flow  Background radiation  
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：341/90  |  提交时间：2021/03/03
Oblique detonation wave  Combustor  Oblique detonation engine  Normal detonation wave  Boundary layer separation