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余西龙 [3]
方思晗 [3]
李飞 [3]
林鑫 [3]
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Indexed By:SCI
Funding Project:National Natural Science Foundation of China[11872368]
Funding Project:National Natural Science Foundation of China[11927803]
Funding Project:National Natural Science Foundation of China[12072355]
Author:余西龙
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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:117/17
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Submit date:2022/11/08
Hybrid rocket engine
Swirl injection
Novel composite fuel grain
Regression rate
Oxidizer-to-fuel ratio
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:349/70
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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:569/75
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Submit date:2021/08/03
Tunable diode laser absorption spectroscopy
Hybrid rocket motor
Temperature
Partial pressure
Combustion efficiency