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Experimental Study of Kerosene Ignition and Flame Stabilization in a Supersonic Combustor 期刊论文
International Journal of Turbo & Jet-Engines, 2022, 卷号: 39, 期号: 3, 页码: 403-410
Authors:  Meng Y(孟宇);  Gu HB(顾洪斌);  Zhang XY(张新宇)
Adobe PDF(3187Kb)  |  Favorite  |  View/Download：294/90  |  Submit date：2021/10/29
Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
Authors:  Tong XT(仝晓通);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang XY(张新宇)
Adobe PDF(8067Kb)  |  Favorite  |  View/Download：423/80  |  Submit date：2021/03/03
Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow  
微波增强滑移电弧等离子体辅助超声速燃烧 期刊论文
航空学报, 2020, 卷号: 41, 期号: 2, 页码: 123345
Authors:  孟宇;  顾洪斌;  孙文明;  张新宇
Adobe PDF(945Kb)  |  Favorite  |  View/Download：251/36  |  Submit date：2019/12/16
超燃冲压发动机  超声速燃烧  等离子体助燃  滑移电弧  微波  
Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
Authors:  Fan WH(范文慧);  Zhong FQ(仲峰泉);  Ma SG(马素刚);  Zhang XY(张新宇)
Adobe PDF(4075Kb)  |  Favorite  |  View/Download：325/98  |  Submit date：2020/03/11
Wall heat flux  Numerical simulation  Ethylene  Supersonic combustor  
Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration 期刊论文
Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: UNSP 105316
Authors:  Meng Y(孟宇);  Gu HB(顾洪斌);  Zhuang JH(庄金衡);  Sun WM(孙文明);  Gao ZB(高占彪);  Lian H(连欢);  Yue LJ(岳连捷);  Chang XY(张新宇)
View  |  Adobe PDF(3099Kb)  |  Favorite  |  View/Download：378/100  |  Submit date：2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration  
Numerical study of a fully confined supersonic slot impinging jet from bleed system 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22
Authors:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Chang XY(张新宇)
View  |  Adobe PDF(3918Kb)  |  Favorite  |  View/Download：552/181  |  Submit date：2019/09/09
Fully confined supersonic jet  Inclined impingement  Heat transfer  Boundary layer bleed  Numerical simulation  
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
Authors:  Wang ZP(王知溥);  Gu HB(顾洪斌);  Cheng L W;  Zhong FQ(仲峰泉);  Zhang XY(张新宇)
View  |  Adobe PDF(2630Kb)  |  Favorite  |  View/Download：276/82  |  Submit date：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
Authors:  Ma SG(马素刚);  Zhong FQ(仲峰泉);  Zhang XY(张新宇)
View  |  Adobe PDF(2634Kb)  |  Favorite  |  View/Download：300/124  |  Submit date：2018/07/17
Detached Eddy Simulation  Reduced Kinetic Mechanism  Supersonic Combustion  Hydrogen  Hydrocarbon  
Downstream pressure variation induced hysteresis in the scramjet isolator 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Ma SH;  Jia YN(贾轶南);  Zhang XY(张新宇);  Yue, Lianjie(yuelj@imech.ac.cn)
Adobe PDF(704Kb)  |  Favorite  |  View/Download：289/99  |  Submit date：2018/01/16
Spacecraft  
Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel 期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 3, 页码: 470-475
Authors:  Xing YF(邢云绯);  Zhong FQ(仲峰泉);  Li DX(李东霞);  Zhang XY(张新宇);  Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(860Kb)  |  Favorite  |  View/Download：468/206  |  Submit date：2015/04/28
Hypersonic Scramjet Test Tunnel  Nozzle  Aerodynamic Heating  Convective Heat Transfer