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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 ... [4]
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张新宇 [4]
李智 [4]
李飞 [4]
陈立红 [4]
顾洪斌 [4]
余西龙 [3]
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2011 [4]
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力学学报 [1]
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Indexed By:EI
Creator:lizhi分李智
Creator:张新宇
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超燃燃烧室气流参数诊断
期刊论文
力学学报, 2011, 卷号: 43, 期号: 6, 页码: 1061-1067
Authors:
李飞
;
余西龙
;
顾洪斌
;
李智
;
陈立红
;
张新宇
Adobe PDF(765Kb)
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View/Download:1912/206
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Submit date:2012/04/01
可调谐二极管吸收光谱技术
温度分布
速度分布
超声速燃烧
燃烧效率
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:1218/259
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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)
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Adobe PDF(420Kb)
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View/Download:626/212
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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)
View
  |  
Adobe PDF(242Kb)
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View/Download:585/224
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Submit date:2014/02/24