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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：426/82  |  Submit date：2021/03/03
Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow  
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.
View  |  Adobe PDF(860Kb)  |  Favorite  |  View/Download：472/207  |  Submit date：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
Authors:  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.
View  |  Adobe PDF(1918Kb)  |  Favorite  |  View/Download：344/80  |  Submit date：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
Authors:  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)
View  |  Adobe PDF(1351Kb)  |  Favorite  |  View/Download：905/230  |  Submit date：2014/08/14
Ignition Delay  Vitiation Effect  Kerosene  Water  Carbon Dioxide  Shock Tube  
CO concentration and temperature measurements in a shock tube for Martian mixtures by coupling OES and TDLAS 期刊论文
APPLIED PHYSICS B-LASERS AND OPTICS, 2013, 卷号: 110, 期号: 3, 页码: 401-409
Authors:  Lin X(林鑫);  Yu XL(余西龙);  Li F(李飞);  Zhang SH(张少华);  Xin JG;  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(716Kb)  |  Favorite  |  View/Download：1093/340  |  Submit date：2013/04/16
Diode-laser Absorption  Nonequilibrium Radiation  Cn Radiation  Sensor  Entry  Flows  Wave  
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
Authors:  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)  |  Favorite  |  View/Download：1218/259  |  Submit date：2012/04/01
Absorption-spectroscopy  Water-vapor  Temperature Distributions  Gas Temperature  Combustion  Cavity  Operation  Engines  Model  
超声速燃烧中气动斜坡的研究 会议论文
第二届高超声速科技学术会议, 中国安徽黄山, 2009-11-02
Authors:  卫喆;  陈立红;  顾洪斌;  李飞;  顾声龙;  张新宇
Adobe PDF(569Kb)  |  Favorite  |  View/Download：605/161  |  Submit date：2010/11/25
超燃冲压发动机  气动斜坡  直连式实验台  散射  
Performance of the fuel injector in supersonic combustor 会议论文
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, October 19, 2009 - October 22, 2009
Authors:  Wei Z(卫喆);  Chen LH(陈立红);  Gu HB(顾洪斌);  Li F(李飞);  Gu SL(顾声龙);  Chang XY(张新宇);  Wei, Z. (weizhejiji@yahoo.com.cn)
View  |  Adobe PDF(167Kb)  |  Favorite  |  View/Download：203/61  |  Submit date：2017/07/14
Concentration Profiles  Engine Design  Fuel Injectors  Fuel-air Mixing  Gas Sampling  Ramp Injector  Scramjet Combustors  Scramjet Test  Supersonic Combustors  
超声速燃烧室凹腔火焰稳定器的数值模拟 期刊论文
推进技术, 2007, 卷号: 28, 期号: 2, 页码: 135-140
Authors:  陈方;  陈立红;  张新宇
Adobe PDF(815Kb)  |  Favorite  |  View/Download：491/139  |  Submit date：2010/05/03
超音速燃烧  凹体  燃烧性能  氢  数值仿真  
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
Authors:  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)  |  Favorite  |  View/Download：876/243  |  Submit date：2009/08/03
Entry Conditions  Kerosene  Supersonic Combustion  Thermal Cracking  Model Combustor  Propulsion  Injection