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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
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：215/85  |  提交时间：2017/06/01
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
作者:  Gu HB(顾洪斌);  Chen LH(陈立红);  张新宇(Chang XY)
浏览  |  Adobe PDF(162Kb)  |  收藏  |  浏览/下载：166/72  |  提交时间：2017/06/01
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
作者:  Chang XY(张新宇);  Gu HB(顾洪斌);  Chen LH(陈立红)
浏览  |  Adobe PDF(139Kb)  |  收藏  |  浏览/下载：177/71  |  提交时间：2017/06/01
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
作者:  Chen LH(陈立红);  Lin R;  Gu HB(顾洪斌);  Chang XY(张新宇)
浏览  |  Adobe PDF(93Kb)  |  收藏  |  浏览/下载：207/85  |  提交时间：2017/06/01
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
作者:  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.
Adobe PDF(834Kb)  |  收藏  |  浏览/下载：1046/414  |  提交时间：2007/06/15
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
作者:  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.
Adobe PDF(423Kb)  |  收藏  |  浏览/下载：719/220  |  提交时间：2007/06/15
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
作者:  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.
Adobe PDF(482Kb)  |  收藏  |  浏览/下载：971/395  |  提交时间：2007/06/15
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
作者:  Chang XY(张新宇);  Chen LH(陈立红);  Yu G(俞刚);  Qian DX(钱大兴)
浏览  |  Adobe PDF(872Kb)  |  收藏  |  浏览/下载：221/82  |  提交时间：2017/06/01
Chinese Academy Of Sciences  Enthalpy Flow  Hypersonic Propulsion Test Facility  Performance Tests  Scramjet Testing  Supersonic Combustion  Total Pressure  Total Temperatures