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余西龙 [3]
李飞 [2]
林鑫 [2]
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Funding Organization:National Natural Science Foundation of China
Funding Project:National Natural Science Foundation of China[11872368]
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Instability mechanism and discharge regime diagnosis of microthrusters based on plasma properties
期刊论文
APPLIED OPTICS, 2021, 卷号: 60, 期号: 4, 页码: 1021-1030
Authors:
Wang FY(王方仪)
;
Zhang SH(张少华)
;
Liu, Yan
;
Yu XL(余西龙)
Adobe PDF(9020Kb)
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View/Download:225/47
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Submit date:2021/04/07
Improving the Combustion Performance of a Hybrid Rocket Engine using a Novel Fuel Grain with a Nested Helical Structure
期刊论文
JOVE-JOURNAL OF VISUALIZED EXPERIMENTS, 2021, 期号: 167, 页码: 17
Authors:
Wang ZZ(王泽众)
;
Lin X(林鑫)
;
Li F(李飞)
;
Zhang ZL(张泽林)
;
Yu XL(余西龙)
Adobe PDF(1456Kb)
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Submit date:2021/06/15
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:291/110
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Submit date:2020/05/18
Hybrid rocket engine
Paraffin-based fuel
Acrylonitrile-butadiene-styrene
Regression rate
Combustion efficiency