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Numerical study on the shock/combustion interaction of oblique detonation waves 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13
作者:  Yang L;  Yue LJ(岳连捷);  Zhang QF(张启帆);  Zhang XY(张新宇)
Adobe PDF(5176Kb)  |  收藏  |  浏览/下载：254/103  |  提交时间：2020/11/30
Oblique detonation wave  Shock/combustion interaction  Shock polar analysis  High-resolution simulation  
Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10
作者:  Zhang X(张旭);  Yue LJ(岳连捷);  Huang TL(黄庭隆);  Zhang QF(张启帆);  Zhang XY(张新宇)
浏览  |  Adobe PDF(3862Kb)  |  收藏  |  浏览/下载：331/114  |  提交时间：2020/03/21
Hysteresis  Dual-mode scramjet  Supersonic combustion  Mode transition  Flame stabilization  Combustion oscillation  
CH* Luminance Distribution Application and a One-Dimensional Model of the Supersonic Combustor Heat Release Quantization 期刊论文
INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2019, 卷号: 36, 期号: 1, 页码: 45-50
作者:  Wang ZP(王知溥);  Gu HB(顾洪斌);  Cheng L W;  Zhong FQ(仲峰泉);  Zhang XY(张新宇)
浏览  |  Adobe PDF(2630Kb)  |  收藏  |  浏览/下载：251/76  |  提交时间：2019/04/11
supersonic combustion  one-dimensional modelling  heat release  CH* chemiluminescence  
Numerical study on supersonic combustion of hydrogen and its mixture with Ethylene and methane with strut injection 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2018, 卷号: 43, 期号: 15, 页码: 7591-7599
作者:  Ma SG(马素刚);  Zhong FQ(仲峰泉);  Zhang XY(张新宇)
浏览  |  Adobe PDF(2634Kb)  |  收藏  |  浏览/下载：265/111  |  提交时间：2018/07/17
Detached Eddy Simulation  Reduced Kinetic Mechanism  Supersonic Combustion  Hydrogen  Hydrocarbon  
Numerical Study of Unsteady Properties of Ethylene/Air Turbulent Jet Diffusion Flame with Detached Eddy Simulation 期刊论文
INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2016, 卷号: 33, 期号: 4, 页码: 407-411
作者:  Ma SG;  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(2908Kb)  |  收藏  |  浏览/下载：275/70  |  提交时间：2017/02/24
Combustion  Ignition  Hydrocarbon Fuel  Reduced Mechanism  Detached Eddy Simulation  
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
作者:  Wang ZP(王知溥);  Li F(李飞);  Gu HS;  Yu XL(余西龙);  Zhang XY(张新宇);  Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1112Kb)  |  收藏  |  浏览/下载：538/226  |  提交时间：2015/06/12
Scramjet  Dual-mode Combustor  Divergent Angle  Cavity Location  Combustion Efficiency  Tdlas  
Large eddy simulation of ignition and combustion of ethylene/air turbulent jet diffusion flame with reduced kinetic mechanism 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
作者:  Ma SG(马素刚);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Zhong, Fengquan (fzhong@imech.ac.cn)
浏览  |  Adobe PDF(496Kb)  |  收藏  |  浏览/下载：247/74  |  提交时间：2017/05/05
Combustion Pro  Cess  Directed Relation Graph  Dynamic Evolution  Fuel Injection Velocities  Kinetic Mechanism  Reduced Mechanisms  Temperature Profiles  Temporal And Spatial Evolutions  
Numerical simulation of ignition and combustion of ethylene in a supersonic model combustor with a reduced kinetic mechanism 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2013, 卷号: 185, 期号: 4, 页码: 548-563
作者:  Zhong FQ(仲峰泉);  Chen LH(陈立红);  Li F(李飞);  Zhang XY(张新宇);  Sung CJ;  Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(1454Kb)  |  收藏  |  浏览/下载：1414/482  |  提交时间：2013/05/03
Ethylene  Ignition  Numerical Simulation  Reduced Kinetic Mechanism  Supersonic Combustion  
Study on Judgment Method of Combustion Mode on Dual-mode Scramjet 会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
作者:  Chen Q(陈强);  Chen LH(陈立红);  Gu HB(顾洪斌);  Zhang XY(张新宇);  Wang P
浏览  |  Adobe PDF(759Kb)  |  收藏  |  浏览/下载：565/186  |  提交时间：2014/03/11
Combustion Mode  Scramjet  Artificial Neural Network  
A compact sensor based on near infrared absorption spectroscopy for flow diagnostics in a low density hydrogen and oxygen combustion driven shock tube 期刊论文
Lasers in Engineering, 2012, 卷号: 23, 期号: 1-2, 页码: 1-17
作者:  Yu XL(余西龙);  Li F(李飞);  Chen LH(陈立红);  Chang XY(张新宇)
Adobe PDF(1693Kb)  |  收藏  |  浏览/下载：790/211  |  提交时间：2012/12/04
Tunable Diode-laser  Water-vapor  Scramjet Combustor  Temperature  Gases  H2o  Co  Oh  Tunable Diode Laser Absorption Spectroscopy (Tdlas)  Combustion  Rapid Time-division-multiplexing (Tdm)  Temperature  Water Vapour Concentration  Low Density Shock Tube