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余西龙 [6]
李飞 [6]
林鑫 [6]
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Funding Project:National Natural Science Foundation of China[11802315]
Document Type:期刊论文
Community:高温气体动力学国家重点实验室
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Error Analysis of Integrated Absorbance for TDLAS in a Nonuniform Flow Field
期刊论文
APPLIED SCIENCES-BASEL, 2021, 卷号: 11, 期号: 22, 页码: 15
Authors:
Li RJ(李仁杰)
;
Li F(李飞)
;
Lin X(林鑫)
;
Yu XL(余西龙)
Adobe PDF(7410Kb)
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View/Download:274/48
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Submit date:2022/01/13
TDLAS
integrated absorbance
error analysis
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
Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
Authors:
Zhou GX(周功喜)
;
Zhang X(张旭)
;
Li JP(李进平)
;
Zhang XY(张晓源)
;
Zhang SZ(张仕忠)
;
Lin X(林鑫)
;
Li F(李飞)
;
Chen H(陈宏)
;
Yue LJ(岳连捷)
;
Yu XL(余西龙)
Adobe PDF(4108Kb)
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Submit date:2021/09/07
High mach number scramjet
Circular cross-section
TDLAS
Multi-view simultaneous imaging
POD
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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Submit date:2020/05/18
Hybrid rocket engine
Paraffin-based fuel
Acrylonitrile-butadiene-styrene
Regression rate
Combustion efficiency