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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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余西龙 [6]
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Indexed By:SCI
Source Publication:AEROSPACE SCIENCE AND TECHNOLOGY
Community:高温气体动力学国家重点实验室
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Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 97, 页码: 8
Authors:
Wang ZZ(王泽众)
;
Lin X(林鑫)
;
Li F(李飞)
;
Yu XL(余西龙)
Adobe PDF(1961Kb)
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Submit date:2020/05/18
Hybrid rocket engine
Paraffin-based fuel
Acrylonitrile-butadiene-styrene
Regression rate
Combustion efficiency
Effect of the fuel-air flow velocity on heat release rate of swirling non-premixed methane flames
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 95, 页码: UNSP 105465
Authors:
Wang KL(王宽亮)
;
Li F(李飞)
;
Zou PF(邹鹏飞)
;
Lin X(林鑫)
;
Mao RH(毛荣海)
;
Yu XL(余西龙)
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Adobe PDF(2678Kb)
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View/Download:283/62
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Submit date:2020/03/21
Swirl flame
Heat release
Chemiluminescence
3D-CTC
Effect of the fuel-air flow velocity on heat release rate of swirling non-premixed methane flames
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 95, 页码: UNSP 105465
Authors:
Wang KL(王宽亮)
;
Li F(李飞)
;
Zou PF(邹鹏飞)
;
Lin X(林鑫)
;
Mao RH(毛荣海)
;
Yu XL(余西龙)
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  |  
Adobe PDF(2678Kb)
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Submit date:2020/03/21
Swirl flame
Heat release
Chemiluminescence
3D-CTC
Tunable diode laser absorption spectroscopy measurements of high-pressure ammonium dinitramide combustion
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 45, 页码: 140-149
Authors:
Yao, Zhaopu
;
Zhang, Wei
;
Wang, Meng
;
Chen, Jun
;
Shen, Yan
;
Wei, Yanming
;
Yu XL(余西龙)
;
Li F(李飞)
;
Ceng H(曾徽)
;
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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Submit date:2015/10/21
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
Authors:
Wang ZP(王知溥)
;
Li F(李飞)
;
Gu HS
;
Yu XL(余西龙)
;
Zhang XY(张新宇)
;
Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2015/06/12
Scramjet
Dual-mode Combustor
Divergent Angle
Cavity Location
Combustion Efficiency
Tdlas
Plasma-assisted ignition for a kerosene fueled scramjet at Mach 1.8
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 卷号: 28, 期号: 1, 页码: 72-78
Authors:
Li F(李飞)
;
Yu XL(余西龙)
;
Tong YG(仝颖刚)
;
Shen Y(沈岩)
;
Chen J(陈健)
;
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:1345/429
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Submit date:2013/07/30
Scramjet
Kerosene Fuel
Plasma Torch
Ignition