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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 ... [2]
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卫喆 [2]
张新宇 [2]
李飞 [2]
陈立红 [2]
顾声龙 [2]
顾洪斌 [2]
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2009 [2]
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16th AIAA/... [2]
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Creator:卫喆
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Creator:陈立红
Creator:顾洪斌
Date Issued:2009
Language:英语
Author:李飞
Author:卫喆
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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)
View
  |  
Adobe PDF(261Kb)
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View/Download:257/82
  |  
Submit date:2017/07/14
Different Frequency
Gas Sampling
Hartmann
Jet Devices
Large-scale Structure
Planar Laser
Shear Layer
Total-pressure Loss