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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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陈立红 [10]
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Creator:陈立红
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Language:英语
Document Type:会议论文
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Experimental study of combustion oscillations in a dual-mode scramjet
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, 2015
Authors:
Tian XD
;
Chen LH(陈立红)
;
Gu HB(顾洪斌)
;
Liu C
;
Cheng LW
;
Chang XY(张新宇)
;
Chen, Lihong (lhchen@imech.ac.cn)
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Submit date:2017/09/04
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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Adobe PDF(759Kb)
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Submit date:2014/03/11
Combustion Mode
Scramjet
Artificial Neural Network
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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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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Adobe PDF(261Kb)
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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 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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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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Submit date:2017/06/01
Combustor Geometries
Flame Stabilization
Mixing Enhancement
Scramjets
Analyses of supersonic combustion by gas sampling
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:
Chen LH(陈立红)
;
Lin R
;
Gu HB(顾洪斌)
;
Chang XY(张新宇)
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View/Download:215/87
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Submit date:2017/06/01
Combustion Efficiency
Gas Sampling
Probe Sampling
Scramjet
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