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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 ... [3]
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余西龙 [3]
张泽林 [3]
方思晗 [3]
李飞 [3]
林鑫 [3]
王泽众 [3]
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Creator:李飞
First author
Creator:王泽众
Language:英语
Author:余西龙
Community:高温气体动力学国家重点实验室
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Charactering Catalytic Ignition and Combustion for the Ninety Percent Hydrogen Peroxide/Paraffin Based Hybrid Rocket Engine
期刊论文
JOURNAL OF PROPULSION AND POWER, 2023
Authors:
Wang ZZ(王泽众)
;
Lin X(林鑫)
;
Wu K(吴坤)
;
Zhang ZL(张泽林)
;
Fang SH(方思晗)
;
Meng DD(孟东东)
;
Li F(李飞)
;
Yu XL(余西龙)
Adobe PDF(712Kb)
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View/Download:92/8
  |  
Submit date:2023/04/20
Hybrid Rocket Engines
Propellant
Thermocouples
Numerical Analysis
Catalysis
Absorption Spectroscopy
Combustion Products
decomposition efficiency
Paraffin Fuel
Ignition Systems
Effects of swirl injection on the combustion of a novel composite hybrid rocket fuel grain
期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 199, 页码: 174-182
Authors:
Zhang ZL(张泽林)
;
Lin X(林鑫)
;
Wang ZZ(王泽众)
;
Wu K(吴坤)
;
Luo JX(罗家枭)
;
Fang SH(方思晗)
;
Zhang CY(张春元)
;
Li F(李飞)
;
Yu XL(余西龙)
Adobe PDF(9227Kb)
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View/Download:110/14
  |  
Submit date:2022/11/08
Hybrid rocket engine
Swirl injection
Novel composite fuel grain
Regression rate
Oxidizer-to-fuel ratio
Temperature and H2O concentration measurements for a hybrid rocket motor plume using a single mid-infrared tunable diode laser
会议论文
2020 Applied Optics and Photonics China: Optical Sensing and Imaging Technology, AOPC 2020, Xiamen, PEOPLES R CHINA, 25 August 2020 through 27 August 2020
Authors:
Fang SH(方思晗)
;
Wang ZZ(王泽众)
;
Li RJ(李仁杰)
;
Zhang ZL(张泽林)
;
Lin X(林鑫)
;
Li F(李飞)
;
Yu XL(余西龙)
Adobe PDF(1569Kb)
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View/Download:230/68
  |  
Submit date:2021/06/11
concentration
hybrid rocket motor
nozzle exit
temperature
Tunable diode laser absorption spectroscopy (TDLAS)
water vapor