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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：399/69  |  Submit date：2021/03/03
Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow  
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：277/113  |  Submit date：2020/11/30
Oblique detonation wave  Shock/combustion interaction  Shock polar analysis  High-resolution simulation  
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：308/93  |  Submit date：2019/05/29
Supersonic combustor  Hydrocarbon  Mixture fuel  Flame structure  Ignition  
Plasma-assisted ignition for a kerosene fueled scramjet at Mach 1.8 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 卷号: 28, 期号: 1, 页码: 72-78
Authors:  Li F(李飞);  Yu XL(余西龙);  Tong YG(仝颖刚);  Shen Y(沈岩);  Chen J(陈健);  Chen LH(陈立红);  Zhang XY(张新宇);  Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1235Kb)  |  Favorite  |  View/Download：1328/421  |  Submit date：2013/07/30
Scramjet  Kerosene Fuel  Plasma Torch  Ignition