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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
作者:  Tong XT(仝晓通);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang XY(张新宇)
Adobe PDF(8067Kb)  |  收藏  |  浏览/下载：376/61  |  提交时间：2021/03/03
Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow  
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
作者:  Zhong FQ(仲峰泉);  Cheng LW(程柳维);  Gu HB(顾洪斌);  Zhang XY(张新宇)
Adobe PDF(2032Kb)  |  收藏  |  浏览/下载：294/85  |  提交时间：2019/05/29
Supersonic combustor  Hydrocarbon  Mixture fuel  Flame structure  Ignition  
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：263/109  |  提交时间：2018/07/17
Detached Eddy Simulation  Reduced Kinetic Mechanism  Supersonic Combustion  Hydrogen  Hydrocarbon  
Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80
作者:  Yue LJ(岳连捷);  Jia YN(贾轶南);  Xu X;  Zhang XY(张新宇);  Zhang P(张鹏)
浏览  |  Adobe PDF(2110Kb)  |  收藏  |  浏览/下载：367/135  |  提交时间：2018/10/30
Inlet restart  Cowl shock  Shock wave boundary layer interactions  
RP-3 型航空煤油荧光光谱研究 会议论文
LHD2013夏季学术研讨会, 河北平山, 2013
作者:  张少华;  余西龙;  张新宇
Adobe PDF(543Kb)  |  收藏  |  浏览/下载：1029/401  |  提交时间：2014/01/23
煤油  激光诱导荧光（lif）  光谱  猝灭  
Effects of entry conditions on cracked kerosene-fueled supersonic combustor performance 期刊论文
Combustion Science and Technology, 2007, 卷号: 179, 期号: 10, 页码: 2199-2217
作者:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Sung CJ;  Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
Adobe PDF(1524Kb)  |  收藏  |  浏览/下载：845/231  |  提交时间：2009/08/03
Entry Conditions  Kerosene  Supersonic Combustion  Thermal Cracking  Model Combustor  Propulsion  Injection  
An Experimental Study of Kerosene Combustion in a Supersonic Model Combustor Using Effervescent Atomization 期刊论文
Proceedings of the Combustion Institute, 2005
作者:  Yu G(俞刚);  Li JG(李建国);  Zhao JR(赵建荣);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Sung CJ;  Yu, G (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
Adobe PDF(1268Kb)  |  收藏  |  浏览/下载：936/286  |  提交时间：2007/06/15
An Experimental Study of Kerosene Combustion in a Supersonic Model Combustor Using Effervescent Atomization 会议论文
30th International Symposium on Combustion, JUL 25-30, 2004 Univ Illinois Chicago, Chicago, IL
作者:  Yu G(俞刚);  Li JG(李建国);  Zhao JR(赵建荣);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Song ZR(宋知人)
Adobe PDF(1268Kb)  |  收藏  |  浏览/下载：783/234  |  提交时间：2007/12/18