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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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力学所知识产出(1... [10]
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陈立红 [10]
张新宇 [9]
岳连捷 [3]
顾洪斌 [3]
Xiao YB [2]
余西龙 [2]
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Creator:chenlihong分陈立红
Document Type:会议论文
Community:力学所知识产出(1956-2008)
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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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Adobe PDF(472Kb)
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View/Download:239/96
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Submit date:2017/06/01
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)
View
  |  
Adobe PDF(265Kb)
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View/Download:394/114
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Submit date:2017/06/01
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
Adobe PDF(1154Kb)
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Submit date:2014/02/14
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
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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  |  
Adobe PDF(1265Kb)
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  |  
Submit date:2015/09/21
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)
View
  |  
Adobe PDF(1267Kb)
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Submit date:2017/06/01
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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  |  
Adobe PDF(162Kb)
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View/Download:188/81
  |  
Submit date: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
Authors:
Chang XY(张新宇)
;
Gu HB(顾洪斌)
;
Chen LH(陈立红)
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  |  
Adobe PDF(139Kb)
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View/Download:200/82
  |  
Submit date:2017/06/01
Combustor Geometries
Flame Stabilization
Mixing Enhancement
Scramjets
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)
Adobe PDF(853Kb)
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Submit date:2007/12/18
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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  |  
Adobe PDF(4312Kb)
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View/Download:173/70
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Submit date:2017/06/01
Compressible Navier-stokes
Computational Studies
Experimental Comparison
Experimental Investigations
Flow Charac-teristics
Hypersonic Propulsion Test Facility
Performance Parameters
Scramjet Inlets
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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Adobe PDF(872Kb)
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Submit date:2017/06/01
Chinese Academy Of Sciences
Enthalpy Flow
Hypersonic Propulsion Test Facility
Performance Tests
Scramjet Testing
Supersonic Combustion
Total Pressure
Total Temperatures