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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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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
Authors:  Xiao YB(肖雅彬);  Yue LJ(岳连捷);  Gong P;  Chang XY(张新宇)
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Boundary Layer Corrections  Busemann Inlet  Core Flow  Correction Method  Design Points  Finite Differential Methods  Internal Contraction Ratio  Internal Flows  Mass Flow  
A tunable diode-laser absorption spectroscopy (TDLAS) thermometry for combustion diagnostics 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
Authors:  Yu XL(余西龙);  Li F(李飞);  Chen LH(陈立红);  Chang XY(张新宇)
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Absorption Lines  Combustion Diagnostics  Direct Absorption  Fiber-coupled  Flat Flame Burner  High Sensitivity  Near Infrared  Non-intrusive  Premixed  Scan Rates  Thermocouple Measurements  Tunable Diode Laser Absorption Spectroscopy  Tunable Diode Lasers  Water Vapor Concentration  Water-vapor Absorption  
Effects of entry conditions on cracked kerosene-fueled supersonic combustor performance 期刊论文
Combustion Science and Technology, 2007, 卷号: 179, 期号: 10, 页码: 2199-2217
Authors:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Sung CJ;  Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
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Entry Conditions  Kerosene  Supersonic Combustion  Thermal Cracking  Model Combustor  Propulsion  Injection  
Investigation of Vaporized Kerosene Injection and Combustion in a Supersonic Model Combustor 期刊论文
Journal of Propulsion and Power, 2006
Authors:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Zhang XY(张新宇);  Sung CJ;  Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, 15 Zhongguancun Rd, Beijing 100080, Peoples R China.
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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  
An Experimental Study of Kerosene Combustion in a Supersonic Model Combustor Using Effervescent Atomization 期刊论文
Proceedings of the Combustion Institute, 2005
Authors:  Yu G(俞刚);  Li JG(李建国);  Zhao JR(赵建荣);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Sung CJ;  Yu, G (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
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Direct initiation of detonation with ignition tube 会议论文
24th International Symposium on Shock Waves, JUL 11-16, 2004 Beijing, PEOPLES R CHINA, Beijing, PEOPLES R CHINA, JUL 11-16, 2004
Authors:  Chen H(陈宏);  Zhang XY(张新宇);  Yu HR(俞鸿儒);  Chen H(陈宏)
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An Experimental Study of Kerosene Combustion in a Supersonic Model Combustor Using Effervescent Atomization 会议论文
30th International Symposium on Combustion, JUL 25-30, 2004 Univ Illinois Chicago, Chicago, IL
Authors:  Yu G(俞刚);  Li JG(李建国);  Zhao JR(赵建荣);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Song ZR(宋知人)
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