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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：258/84  |  Submit date：2021/10/29
Parameters for evaluating the efficiency of inlet compression 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56
Authors:  Chen KT(陈科挺);  Yue LJ(岳连捷);  Zhang XY(张新宇)
Adobe PDF(511Kb)  |  Favorite  |  View/Download：224/49  |  Submit date：2022/01/12
Airbreathing engine  Compression efficiency  Compression quality  Inlet  Self-consistency  
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
Authors:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Ma SH(马生虎);  Zhang QF(张启帆);  Zhang, Peng;  Zhang XY(张新宇)
Adobe PDF(3937Kb)  |  Favorite  |  View/Download：208/52  |  Submit date：2021/03/30
Adverse pressure gradient  Back pressure  Hysteresis effects  Non-uniform flow  Shock train  
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
Authors:  Yang L;  Yue LJ(岳连捷);  Zhang QF(张启帆);  Zhang XY(张新宇)
Adobe PDF(5176Kb)  |  Favorite  |  View/Download：278/113  |  Submit date：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
Authors:  Zhang X(张旭);  Yue LJ(岳连捷);  Huang TL(黄庭隆);  Zhang QF(张启帆);  Zhang XY(张新宇)
View  |  Adobe PDF(3862Kb)  |  Favorite  |  View/Download：351/124  |  Submit date：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
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：264/79  |  Submit date：2019/04/11
supersonic combustion  one-dimensional modelling  heat release  CH* chemiluminescence  
Experimental study of flame characteristics of ethylene and its mixture with methane and hydrogen in supersonic combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 86, 页码: 775-781
Authors:  Zhong FQ(仲峰泉);  Cheng LW(程柳维);  Gu HB(顾洪斌);  Zhang XY(张新宇)
Adobe PDF(2032Kb)  |  Favorite  |  View/Download：309/93  |  Submit date：2019/05/29
Supersonic combustor  Hydrocarbon  Mixture fuel  Flame structure  Ignition  
Numerical Study of Impingement Cooling of Aviation Kerosene at Supercritical Conditions 期刊论文
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2018, 卷号: 140, 期号: 11, 页码: Ar-112201
Authors:  Xing YF(邢云绯);  Zhong FQ(仲峰泉);  Zhang XY(张新宇)
View  |  Adobe PDF(2044Kb)  |  Favorite  |  View/Download：330/135  |  Submit date：2018/12/12
impingement cooling  supercritical condition  heat transfer  kerosene  
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：282/116  |  Submit date：2018/07/17
Detached Eddy Simulation  Reduced Kinetic Mechanism  Supersonic Combustion  Hydrogen  Hydrocarbon  
Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions 期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
Authors:  Tian L;  Chen LH(陈立红);  Chen Q(陈强);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Chen, LH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1162Kb)  |  Favorite  |  View/Download：344/88  |  Submit date：2016/09/14
Dual-mode Scramjet  Engine Performance  Thrust  Optimization  Heat Release Distribution  Simulated Annealing Algorithm