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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 [5]
林鑫 [5]
王泽众 [5]
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Indexed By:EI
Creator:余西龙
First author
Funding Organization:National Natural Science Foundation of China
Document Type:期刊论文
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Effect of characteristic structure of nested composite hybrid rocket fuel grain on combustion properties
期刊论文
ACTA ASTRONAUTICA, 2024, 卷号: 218, 页码: 269-281
Authors:
Wang RY(王若岩)
;
Lin X(林鑫)
;
Wang ZZ(王泽众)
;
Wu K(吴坤)
;
Pan JJ(潘俊杰)
;
Zhang ZL(张泽林)
;
Luo JX(罗家枭)
;
Li F(李飞)
;
Yu XL(余西龙)
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View/Download:15/0
  |  
Submit date:2024/05/21
Hybrid rocket
Composite fuel grain
Characteristic structure
Radiation image
Combustion properties
Superior Al90Mg10-Based Composite Fuel Grain for a Hybrid Rocket Engine
期刊论文
JOURNAL OF SPACECRAFT AND ROCKETS, 2024, 页码: 9
Authors:
Wang ZZ(王泽众)
;
Lin X(林鑫)
;
Pan JJ(潘俊杰)
;
Luo JX(罗家枭)
;
Wang RY(王若岩)
;
Zhang ZL(张泽林)
;
Yu XL(余西龙)
Favorite
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View/Download:12/0
  |  
Submit date:2024/05/21
Combustion Efficiency
Emission Spectroscopy
Hybrid Rocket Engines
Paraffin Based Fuels
Regression rate
Aluminium Alloys
3D Printing
Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy
期刊论文
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 110-120
Authors:
Wang ZZ(王泽众)
;
Lin X(林鑫)
;
Li F(李飞)
;
Peng JL(彭锦龙)
;
Liu, Yan
;
Zhang ZL(张泽林)
;
Fang SH(方思晗)
;
Yu XL(余西龙)
Adobe PDF(6496Kb)
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View/Download:315/59
  |  
Submit date:2021/11/01
Hybrid rocket engine
Fuel mass flow rate
Tunable diode laser absorption spectroscopy
Temperature
Partial pressure
Characterizing combustion of a hybrid rocket using laser absorption spectroscopy
期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2021, 卷号: 127, 页码: 9
Authors:
Fang SH(方思晗)
;
Wang ZZ(王泽众)
;
Lin X(林鑫)
;
Li F(李飞)
;
Li RJ(李仁杰)
;
Li, Jing
;
Zhang, Zhedian
;
Liu, Yan
;
Yu XL(余西龙)
Adobe PDF(4367Kb)
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View/Download:547/67
  |  
Submit date:2021/08/03
Tunable diode laser absorption spectroscopy
Hybrid rocket motor
Temperature
Partial pressure
Combustion efficiency
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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View/Download:285/108
  |  
Submit date:2020/05/18
Hybrid rocket engine
Paraffin-based fuel
Acrylonitrile-butadiene-styrene
Regression rate
Combustion efficiency