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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
Authors:  Yue LJ(岳连捷);  Xiao YB;  Chen LH(陈立红);  Chang XY(张新宇)
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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)
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Kerosene Fuel  Mass Flow Rate  Scramjet Engine  
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)
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Combustor Geometries  Flame Stabilization  Mixing Enhancement  Scramjets  
Analyses of supersonic combustion by gas sampling 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:  Chen LH(陈立红);  Lin R;  Gu HB(顾洪斌);  Chang XY(张新宇)
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Combustion Efficiency  Gas Sampling  Probe Sampling  Scramjet  
Fuel Injection and Flame Stabilization in a Liquid-Kerosene-Fueled Supersonic Combustor 期刊论文
Journal of Propulsion and Power, 2003, 卷号: 19, 期号: 5, 页码: 885-893
Authors:  Yu G(俞刚);  Li JG(李建国);  Zhang XY(张新宇);  Chen LH(陈立红);  Sung CJ;  Yu, G (reprint author), Chinese Acad Sci, Inst Mech, 15 Zhongguancun Rd, Beijing 100080, Peoples R China.
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Experimental Investigation on Flameholding Mechanism and Combustion Performance in Hydrogen-Fueled Supersonic Combustors 期刊论文
Combustion Science and Technology, 2002, 卷号: 174, 期号: 3, 页码: 1-27
Authors:  Yu G(俞刚);  Li JG(李建国);  Zhang XY(张新宇);  Chen LH(陈立红);  Han B;  Sung CJ;  Sung, CJ (reprint author), Case Western Reserve Univ, Dept Mech & Aerosp Engn, Cleveland, OH 44106 USA.
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Investigation of kerosene combustion characteristics with pilot hydrogen in model supersonic combustors 期刊论文
Journal of Propulsion and Power, 2001, 卷号: 17, 期号: 6, 页码: 1263-1272
Authors:  Yu G(俞刚);  Li JG(李建国);  Zhang XY(张新宇);  Chen LH(陈立红);  Song CJ;  Yu, G (reprint author), Chinese Acad Sci, Inst Mech, 15 Zhongguancun Rd,Haidian Dist, Beijing 100080, Peoples R China.
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Development of the facility for model scramjet testing 会议论文
10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001, Kyoto, Japan, April 24, 2001 - April 27, 2001
Authors:  Chang XY(张新宇);  Chen LH(陈立红);  Yu G(俞刚);  Qian DX(钱大兴)
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Chinese Academy Of Sciences  Enthalpy Flow  Hypersonic Propulsion Test Facility  Performance Tests  Scramjet Testing  Supersonic Combustion  Total Pressure  Total Temperatures