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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  
TDLAS测量甲烷/空气预混平面火焰温度和H_20浓度 会议论文
第一届高超声速科技学术会议, 中国云南丽江, 2008-12-28
Authors:  余西龙;  李飞;  陈立红;  张新宇
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可调谐二极管吸收光谱技术(Tdlas)  温度测量  浓度测量  预混平面火焰  Hitran00  
超声速燃烧室凹腔火焰稳定器的数值模拟 期刊论文
推进技术, 2007, 卷号: 28, 期号: 2, 页码: 135-140
Authors:  陈方;  陈立红;  张新宇
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超音速燃烧  凹体  燃烧性能  氢  数值仿真  
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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直联式超燃实验台超声速燃气取样分析 期刊论文
实验流体力学, 2006, 卷号: 20, 期号: 1, 页码: 67-71,79
Authors:  林然;  陈立红;  张新宇
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气体取样  探针  超燃冲压发动机  燃烧效率  色谱  
壁面凹腔强化H2超声速燃烧的数值模拟 期刊论文
推进技术, 2006, 期号: 6, 页码: 563-567
Authors:  陈方;  陈立红;  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