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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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微重力重点实验室 [1]
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Indexed By:EI
Date Issued:2009
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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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View/Download:207/61
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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
Influence of Rayleigh-Taylor Instability on Liquid Propellant Reorientation in a Low-Gravity Environment
期刊论文
Chinese Physics Letters, 2009, 卷号: 26, 期号: 11, 页码: 114701
Authors:
Li ZG(李章国)
;
Liu QS(刘秋生)
;
Liu R(刘荣)
;
Hu W
;
Deng XY
;
Li ZG
Adobe PDF(753Kb)
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View/Download:766/179
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Submit date:2009/08/03
Direct Numerical-simulation
Surface
Volume
Effects of anode temperature on working characteristics and performance of a low power arcjet thruster
期刊论文
Chinese Physics Letters, 2009, 卷号: 26, 期号: 12, 页码: 125201
Authors:
Pan WX(潘文霞)
;
Li T(李腾)
;
Wu CK(吴承康)
Adobe PDF(444Kb)
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Submit date:2009/12/22