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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
Authors:  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)
View  |  Adobe PDF(824Kb)  |  Favorite  |  View/Download：253/74  |  Submit date：2017/09/04
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：1212/258  |  Submit date：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
Authors:  Gu HB(顾洪斌);  Chen LH(陈立红);  Zhang XY(张新宇);  Gu HB(顾洪斌)
View  |  Adobe PDF(627Kb)  |  Favorite  |  View/Download：1181/326  |  Submit date：2009/09/28
Scramjet  Combustor  Cavity  Performance  
Experimental investigation of cavity-based scramjet model 会议论文
14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference, Canberra, Australia, November 6, 2006 - November 9, 2006
Authors:  Gu HB(顾洪斌);  Chen LH(陈立红);  张新宇(Chang XY)
View  |  Adobe PDF(162Kb)  |  Favorite  |  View/Download：180/78  |  Submit date：2017/06/01
Kerosene Fuel  Mass Flow Rate  Scramjet Engine  
扫描式总压耙在高超声速推进风洞流场测量中的应用 期刊论文
实验流体力学, 2005, 卷号: 19, 期号: 2, 页码: 71-73,83
Authors:  常远;  顾洪斌;  陈立红;  张新宇
Adobe PDF(256Kb)  |  Favorite  |  View/Download：550/160  |  Submit date：2010/05/03
扫描式总压耙  超声速喷管流场  总压分布  马赫数分布  
Thrust and drag of a scramjet model with different combustor geometries 会议论文
13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference, Capua, Italy, May 16, 2005 - May 20, 2005
Authors:  Chang XY(张新宇);  Gu HB(顾洪斌);  Chen LH(陈立红)
View  |  Adobe PDF(139Kb)  |  Favorite  |  View/Download：193/78  |  Submit date：2017/06/01
Combustor Geometries  Flame Stabilization  Mixing Enhancement  Scramjets  
扩压段对高超声速推进风洞起动的影响 期刊论文
推进技术, 2004, 卷号: 25, 期号: 5, 页码: 430-434
Authors:  陈立红;  张新宇;  顾洪斌
Adobe PDF(347Kb)  |  Favorite  |  View/Download：675/232  |  Submit date：2007/06/15
超音速冲压喷气发动机  超高速风洞  超声速扩压段  模型