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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(19... [1]
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张新宇 [9]
陈立红 [9]
顾洪斌 [9]
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Creator:陈立红
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Creator:顾洪斌
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Study on Judgment Method of Combustion Mode on Dual-mode Scramjet
会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
Authors:
Chen Q(陈强)
;
Chen LH(陈立红)
;
Gu HB(顾洪斌)
;
Zhang XY(张新宇)
;
Wang P
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Submit date:2014/03/11
Combustion Mode
Scramjet
Artificial Neural Network
Study on Judgment Method of Combustion Mode on Dual-mode Scramjet
期刊论文
Procedia Engineering, 2013, 卷号: 67, 页码: 147-154
Authors:
Chen Q(陈强)
;
Chen LH(陈立红)
;
Gu HB(顾洪斌)
;
Zhang XY(张新宇)
;
Wang P
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  |  
Adobe PDF(771Kb)
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View/Download:243/102
  |  
Submit date:2015/09/24
Scramjet
Artificial Neural Network
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
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View/Download:1207/258
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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)
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Adobe PDF(420Kb)
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View/Download:610/205
  |  
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)
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Adobe PDF(242Kb)
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View/Download:563/213
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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)
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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)
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View/Download:238/76
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Submit date:2017/07/14
Different Frequency
Gas Sampling
Hartmann
Jet Devices
Large-scale Structure
Planar Laser
Shear Layer
Total-pressure Loss
Experimental investigation on the cavity-based scramjet model
期刊论文
CHINESE SCIENCE BULLETIN, 2009, 卷号: 54, 期号: 16, 页码: 2794-2799
Authors:
Gu HB(顾洪斌)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Gu HB(顾洪斌)
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Adobe PDF(627Kb)
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View/Download:1177/324
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Submit date:2009/09/28
Scramjet
Combustor
Cavity
Performance
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