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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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State Key ... [5]
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张新宇 [5]
李飞 [5]
陈立红 [5]
顾洪斌 [5]
李智 [3]
顾声龙 [3]
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Indexed By:EI
Creator:李飞
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Creator:陈立红
Language:英语
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Simultaneous measurements of multiple flow parameters for scramjet characterization using tunable diode-laser sensors
期刊论文
Applied Optics, 2011, 卷号: 50, 期号: 36, 页码: 6697-6707
Authors:
Li F(李飞)
;
Yu XL(余西龙)
;
Gu HB(顾洪斌)
;
Li Z(李智)
;
Zhao Y
;
Ma L
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
Adobe PDF(1090Kb)
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View/Download:1211/258
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Submit date:2012/04/01
Absorption-spectroscopy
Water-vapor
Temperature Distributions
Gas Temperature
Combustion
Cavity
Operation
Engines
Model
Measurement of temperature, velocity and water vapor concentration in a scramjet combustor based on nearinfrared diode laser absorption
会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, United states, APR 11-14, 2011
Authors:
Li F(李飞)
;
Yu XL(余西龙)
;
Gu HB(顾洪斌)
;
Li Z(李智)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Li F(李飞)
Adobe PDF(420Kb)
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View/Download:615/207
  |  
Submit date:2014/02/24
Characteristics of supersonic combustion with Hartmann-Sprenger tube aided fuel injection
会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, United states, APR 11-14, 2011
Authors:
Gu HB(顾洪斌)
;
Li Z(李智)
;
Li F(李飞)
;
Chen LH(陈立红)
;
Gu SL(顾声龙)
;
Zhang XY(张新宇)
;
Gu HB(顾洪斌)
Adobe PDF(242Kb)
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View/Download:570/217
  |  
Submit date:2014/02/24
Performance of the fuel injector in supersonic combustor
会议论文
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, October 19, 2009 - October 22, 2009
Authors:
Wei Z(卫喆)
;
Chen LH(陈立红)
;
Gu HB(顾洪斌)
;
Li F(李飞)
;
Gu SL(顾声龙)
;
Chang XY(张新宇)
;
Wei, Z. (weizhejiji@yahoo.com.cn)
Adobe PDF(167Kb)
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View/Download:190/60
  |  
Submit date:2017/07/14
Concentration Profiles
Engine Design
Fuel Injectors
Fuel-air Mixing
Gas Sampling
Ramp Injector
Scramjet Combustors
Scramjet Test
Supersonic Combustors
Flow-field of the excited jet and mixing in the supersonic flow
会议论文
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, October 19, 2009 - October 22, 2009
Authors:
Gu SL(顾声龙)
;
Chen LH(陈立红)
;
Gu HB(顾洪斌)
;
Li F(李飞)
;
Wei Z(卫喆)
;
Chang XY(张新宇)
;
Gu, S. (gushenglong@imech.ac.cn)
Adobe PDF(261Kb)
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View/Download:245/79
  |  
Submit date:2017/07/14
Different Frequency
Gas Sampling
Hartmann
Jet Devices
Large-scale Structure
Planar Laser
Shear Layer
Total-pressure Loss