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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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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  
Research on three-dimensional scramjet inlet 会议论文
14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006, Beijing, China, 20-23 April 2006
Authors:  Yue LJ(岳连捷);  Xiao YB(肖雅彬);  Chen LH(陈立红);  Xiang AY(向安宇);  Zhang XY(张新宇)
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Research on three-dimensional scramiet inlet 会议论文
14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference, Canberra, Australia, November 6, 2006 - November 9, 2006
Authors:  Yue LJ(岳连捷);  Chen LH(陈立红);  Xiao YB;  Gong P;  Chang XY(张新宇)
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Capture Ratio  Mass Flow  Surface Oil Dot Visualization  Three-dimensional Scramjet Inlet  
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  
Experimental Studies on Model Scramjet in a Mach 6 High Enthalpy Free-Jet Wind Tunnel 会议论文
The 24th International Symposium on Shock Waves, Beijing, 2004-07-11
Authors:  Zhang XY(张新宇);  Chen LH(陈立红);  Gu HB(顾洪斌);  Yu G(俞刚);  Zhang XY(张新宇)
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Gas Sampling/Analysis of the High Enthalpy Supersonic Flow 会议论文
24th International Symposium on Shock Waves, JUL 11-16, 2004 Beijing, PEOPLES R CHINA
Authors:  Chen LH(陈立红);  Zheng BK(郑必可);  张新宇(Zhang XY)
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Three-dimensional sidewall-compression scramjet inlet CFD simulation and experimental comparison 会议论文
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2003, Huntsville, AL, United states, July 20, 2003 - July 23, 2003
Authors:  Chen F;  Chen LH(陈立红);  Chang XY(张新宇)
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Compressible Navier-stokes  Computational Studies  Experimental Comparison  Experimental Investigations  Flow Charac-teristics  Hypersonic Propulsion Test Facility  Performance Parameters  Scramjet Inlets