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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)
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Study on Judgment Method of Combustion Mode on Dual-mode Scramjet 会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
Authors:  Chen Q(陈强);  Chen LH(陈立红);  Gu HB(顾洪斌);  Zhang XY(张新宇);  Wang P
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Combustion Mode  Scramjet  Artificial Neural Network  
Study on Judgment Method of Combustion Mode on Dual-mode Scramjet 期刊论文
Procedia Engineering, 2013, 卷号: 67, 页码: 147-154
Authors:  Chen Q(陈强);  Chen LH(陈立红);  Gu HB(顾洪斌);  Zhang XY(张新宇);  Wang P
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Scramjet  Artificial Neural Network  
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
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Absorption-spectroscopy  Water-vapor  Temperature Distributions  Gas Temperature  Combustion  Cavity  Operation  Engines  Model  
Characteristics of supersonic combustion with Hartmann-Sprenger tube aided fuel injection 会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, United states, APR 11-14, 2011
Authors:  Gu HB(顾洪斌);  Li Z(李智);  Li F(李飞);  Chen LH(陈立红);  Gu SL(顾声龙);  Zhang XY(张新宇);  Gu HB(顾洪斌)
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小支板增强超声速混合的实验研究 会议论文
第三届高超声速科技学术会议, 江苏·无锡
Authors:  李智;  陈立红;  顾洪斌;  李飞;  张新宇
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H-S管激励射流超声速燃烧实验研究 会议论文
第三届高超声速科技学术会议, 江苏·无锡, 2010-10-26
Authors:  顾洪斌;  顾声龙;  李智;  李飞;  陈立红;  张新宇
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激励射流在超声速流场中的混合特性研究 期刊论文
力学学报, 2010, 卷号: 42, 期号: 5, 页码: 957-961
Authors:  顾声龙;  陈立红;  顾洪斌;  李飞;  卫喆;  张新宇
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激励射流  超声速混合  穿透深度  大尺度结构  
激励射流在超声速流场中的混合的特性研究 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:  顾声龙;  陈立红;  顾洪斌;  李飞;  卫喆;  张新宇
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激励射流  超声速混合  穿透深度  大尺度结构  
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)
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Concentration Profiles  Engine Design  Fuel Injectors  Fuel-air Mixing  Gas Sampling  Ramp Injector  Scramjet Combustors  Scramjet Test  Supersonic Combustors