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Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration 期刊论文
Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: UNSP 105316
作者:  Meng Y(孟宇);  Gu HB(顾洪斌);  Zhuang JH(庄金衡);  Sun WM(孙文明);  Gao ZB(高占彪);  Lian H(连欢);  Yue LJ(岳连捷);  Chang XY(张新宇)
浏览  |  Adobe PDF(3099Kb)  |  收藏  |  浏览/下载：361/94  |  提交时间：2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration  
Numerical study of a fully confined supersonic slot impinging jet from bleed system 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22
作者:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Chang XY(张新宇)
浏览  |  Adobe PDF(3918Kb)  |  收藏  |  浏览/下载：521/165  |  提交时间：2019/09/09
Fully confined supersonic jet  Inclined impingement  Heat transfer  Boundary layer bleed  Numerical simulation  
Comment on "Mechanics of Combustion Mode Transition in a Direct-Connect Ramjet-Scramjet Experiment" 期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 2, 页码: 550-551
作者:  Chen KT(陈科挺);  Yue LJ(岳连捷);  Chang XY(张新宇)
浏览  |  Adobe PDF(148Kb)  |  收藏  |  浏览/下载：246/81  |  提交时间：2018/10/30
Experimental study of combustion oscillations in a dual-mode scramjet 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, 2015
作者:  Tian XD;  Chen LH(陈立红);  Gu HB(顾洪斌);  Liu C;  Cheng LW;  Chang XY(张新宇);  Chen, Lihong (lhchen@imech.ac.cn)
浏览  |  Adobe PDF(824Kb)  |  收藏  |  浏览/下载：226/64  |  提交时间：2017/09/04
A compact sensor based on near infrared absorption spectroscopy for flow diagnostics in a low density hydrogen and oxygen combustion driven shock tube 期刊论文
Lasers in Engineering, 2012, 卷号: 23, 期号: 1-2, 页码: 1-17
作者:  Yu XL(余西龙);  Li F(李飞);  Chen LH(陈立红);  Chang XY(张新宇)
Adobe PDF(1693Kb)  |  收藏  |  浏览/下载：790/211  |  提交时间：2012/12/04
Tunable Diode-laser  Water-vapor  Scramjet Combustor  Temperature  Gases  H2o  Co  Oh  Tunable Diode Laser Absorption Spectroscopy (Tdlas)  Combustion  Rapid Time-division-multiplexing (Tdm)  Temperature  Water Vapour Concentration  Low Density Shock Tube  
Numerical study of ignition and combustion of partially cracked kerosene in a mach 2.5 supersonic model combustor 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
作者:  Zhong FQ(仲峰泉);  Chen LH(陈立红);  Chang XY(张新宇);  Zhong FQ(仲峰泉)
Adobe PDF(6469Kb)  |  收藏  |  浏览/下载：425/98  |  提交时间：2014/02/24
Design of Base Flow for Streamline-Traced Hypersonic Inlet 会议论文
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, International Space Planes and Hypersonic Systems and Technologies Conferences, Bremen, Germany, 19 October 2009 - 22 October 2009
作者:  Yue LJ(岳连捷);  Xiao YB;  Chen LH(陈立红);  Chang XY(张新宇)
浏览  |  Adobe PDF(472Kb)  |  收藏  |  浏览/下载：205/81  |  提交时间：2017/06/01
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
作者:  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)
浏览  |  Adobe PDF(167Kb)  |  收藏  |  浏览/下载：173/59  |  提交时间：2017/07/14
Concentration Profiles  Engine Design  Fuel Injectors  Fuel-air Mixing  Gas Sampling  Ramp Injector  Scramjet Combustors  Scramjet Test  Supersonic Combustors  
Flow-field of the excited jet and mixing in the supersonic flow 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
作者:  Gu SL(顾声龙);  Chen LH(陈立红);  Gu HB(顾洪斌);  Li F(李飞);  Wei Z(卫喆);  Chang XY(张新宇);  Gu, S. (gushenglong@imech.ac.cn)
浏览  |  Adobe PDF(261Kb)  |  收藏  |  浏览/下载：221/71  |  提交时间：2017/07/14
Different Frequency  Gas Sampling  Hartmann  Jet Devices  Large-scale Structure  Planar Laser  Shear Layer  Total-pressure Loss  
Investigation on a truncated streamline-traced hypersonic Busemann inlet 会议论文
15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, OH, United states, April 28, 2008 - May 1, 2008
作者:  Xiao YB(肖雅彬);  Yue LJ(岳连捷);  Gong P;  Chang XY(张新宇)
浏览  |  Adobe PDF(3472Kb)  |  收藏  |  浏览/下载：205/82  |  提交时间：2017/06/01
Boundary Layer Corrections  Busemann Inlet  Core Flow  Correction Method  Design Points  Finite Differential Methods  Internal Contraction Ratio  Internal Flows  Mass Flow