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高焓空气等离子体放电若干关键问题研究 学位论文
博士论文,北京: 中国科学院大学, 2022
Authors:  韩宁
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高焓空气等离子体  感应耦合等离子体发生器  稳定放电  稀薄流场密度估算  石墨保型烧蚀  
水基与煤油基纳米流体导热及对流传热特性研究 学位论文
博士论文,北京: 中国科学院大学, 2021
Authors:  范文慧
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纳米流体  航空煤油  导热性能  对流传热性能  努塞尔数  
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
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High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Main performance analysis of kitchen waste gasification in a small-power horizontal plasma jet reactor 期刊论文
JOURNAL OF THE ENERGY INSTITUTE, 2020, 卷号: 93, 期号: 1, 页码: 367-376
Authors:  Li HX(李慧鑫);  Li T(李腾);  Wei XL(魏小林)
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Gasification  Plasma torch  Kitchen waste  Syngas  Graphitization  
Influence of Chemical Mechanisms on Supersonic Combustion Characteristics Fueled by Kerosene 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio, July 9-11, 2018
Authors:  Yao W(姚卫);  Wu K(吴坤);  Lee YC(李亚超);  Fan XJ(范学军)
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Combined tunable diode laser absorption spectroscopy and monochromatic radiation thermometry in ammonium dinitramide-based thruster 期刊论文
OPTICAL ENGINEERING, 2018, 卷号: 57, 期号: 2, 页码: 26106
Authors:  Zeng H(曾徽);  Ou DB;  Chen LZ;  Li F(李飞);  Yu XL(余西龙)
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Tunable Diode Laser Absorption Spectroscopy  Monochromatic Radiation Thermometry  Ammonium Dinitramide-based Thruster  
Molecular tagging velocimetry of NH fluorescence in a high-enthalpy rarefied gas flow 期刊论文
APPLIED PHYSICS B-LASERS AND OPTICS, 2017, 卷号: 123, 期号: 4
Authors:  Zhang SH(张少华);  Yu XL(余西龙);  Yan H;  Huang HJ(黄河激);  Liu HL(刘宏立);  Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.;  Yu, XL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
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Molecular Tagging Velocimetry  Nh Fluorescence  High-enthalpy  Rarefied Gas  
A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Fan XJ(范学军);  Fan, Xuejun(xfan@imech.ac.cn)
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Adiabatic Flame Temperature  Aerodynamics  Boundary Layer Flow  Boundary Layers  Chemical Analysis  Combustion  Computational Chemistry  Directed Graphs  Flow Separation  Mach Number  Principal Component Analysis  Regression Analysis  Sensitivity Analysis  Spacecraft  Supersonic Aerodynamics  Supersonic Aircraft  Transients  
Development of zone flamelet model for scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Yao W(姚卫);  Fan XJ(范学军)
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Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft  
Producing ultra-high-speed nitrogen jets by arc heating in a low-pressure chamber 期刊论文
Theoretical and Applied Mechanics Letters, 2016, 卷号: 6, 期号: 1, 页码: 60-63
Authors:  Pan WX(潘文霞);  Meng X(孟显);  Huang HJ(黄河激);  Wu CK(吴承康)
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Low-power Nitrogen Arc-heater  Lateral Bypass-exhausting  Very High Flow Speed  Nozzle Structure  Chamber Pressure