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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：377/61  |  提交时间：2021/03/03
Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow  
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：368/135  |  提交时间：2018/10/30
Inlet restart  Cowl shock  Shock wave boundary layer interactions  
The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Jia YN(贾轶南);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Jia, Yinan(yuelj@imech.ac.cn)
浏览  |  Adobe PDF(566Kb)  |  收藏  |  浏览/下载：327/71  |  提交时间：2018/01/16
Boundary Layer Flow  Boundary Layers  Spacecraft  Wind Tunnels  
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
作者:  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.
浏览  |  Adobe PDF(860Kb)  |  收藏  |  浏览/下载：441/189  |  提交时间：2015/04/28
Hypersonic Scramjet Test Tunnel  Nozzle  Aerodynamic Heating  Convective Heat Transfer  
Numerical Study of Turbulent Flow and Convective Heat Transfer Characteristics in Helical Rectangular Ducts 期刊论文
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2014, 卷号: 136, 期号: 12, 页码: 121701
作者:  Xing YF(邢云绯);  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(1918Kb)  |  收藏  |  浏览/下载：326/74  |  提交时间：2015/01/04
Helical Rectangular Duct  Heat Transfer  Turbulent Flow  Curvature  Torsion  
The vitiation effects of water vapor and carbon dioxide on the autoignition characteristics of kerosene 期刊论文
Acta Mechanica Sinica, 2014, 卷号: 30, 期号: 4, 页码: 485-494
作者:  Liang JH(梁金虎);  Wang S(王苏);  Zhang ST(张胜涛);  Yue LJ(岳连捷);  Fan BC(范秉诚);  Zhang XY(张新宇);  Cui JP(崔季平);  Wang S(王苏)
浏览  |  Adobe PDF(1351Kb)  |  收藏  |  浏览/下载：885/215  |  提交时间：2014/08/14
Ignition Delay  Vitiation Effect  Kerosene  Water  Carbon Dioxide  Shock Tube  
Simultaneous measurements of multiple flow parameters for scramjet characterization using tunable diode-laser sensors 期刊论文
Applied Optics, 2011, 卷号: 50, 期号: 36, 页码: 6697-6707
作者:  Li F(李飞);  Yu XL(余西龙);  Gu HB(顾洪斌);  Li Z(李智);  Zhao Y;  Ma L;  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
Adobe PDF(1090Kb)  |  收藏  |  浏览/下载：1197/257  |  提交时间：2012/04/01
Absorption-spectroscopy  Water-vapor  Temperature Distributions  Gas Temperature  Combustion  Cavity  Operation  Engines  Model  
Experimental investigation on the cavity-based scramjet model 期刊论文
CHINESE SCIENCE BULLETIN, 2009, 卷号: 54, 期号: 16, 页码: 2794-2799
作者:  Gu HB(顾洪斌);  Chen LH(陈立红);  Zhang XY(张新宇);  Gu HB(顾洪斌)
浏览  |  Adobe PDF(627Kb)  |  收藏  |  浏览/下载：1163/317  |  提交时间：2009/09/28
Scramjet  Combustor  Cavity  Performance  
Research on three-dimensional scramjet inlet 会议论文
14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006, Beijing, China, 20-23 April 2006
作者:  Yue LJ(岳连捷);  Xiao YB(肖雅彬);  Chen LH(陈立红);  Xiang AY(向安宇);  Zhang XY(张新宇)
浏览  |  Adobe PDF(1265Kb)  |  收藏  |  浏览/下载：240/72  |  提交时间：2015/09/21