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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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Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
Authors:
Yao W(姚卫)
;
Yuan YM(袁越明)
;
Li XP(李晓鹏)
;
Wang J(王晶)
;
Wu K(吴坤)
;
Fan XJ(范学军)
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Adobe PDF(805Kb)
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Submit date:2018/06/06
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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Submit date:2018/01/16
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
不同喷压比下欠膨胀射流对特征频率激励的响应
会议论文
第九届全国流体力学学术会议, 中国江苏南京, 2016-10-20
Authors:
李晓鹏
;
姚卫
;
范学军
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Adobe PDF(122Kb)
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Submit date:2017/09/27
欠膨胀射流
喷压比
特征频率激励
大涡模拟
流动响应
The effects of air vitiation on the supersonic turbulent channel flow using direct numerical simulation
会议论文
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016, Salt Lake City, UT, United states, July 25, 2016 - July 27, 2016
Authors:
Chen XP
;
Li XP(李晓鹏)
;
Dou HS
Adobe PDF(1216Kb)
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Submit date:2017/05/05
Mass Fraction
Mean Velocities
Nondimensional
Reynolds Analogy
Static Temperature
Statistical Characteristics
Temperature Correlation
Turbulent Channel Flows
Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Yao W(姚卫)
;
Wang J(王晶)
;
Lu Y(陆阳)
;
Li XP(李晓鹏)
;
Fan XJ(范学军)
Adobe PDF(1195Kb)
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Submit date:2016/07/01
Adiabatic Flame Temperature
Combustion
Directed Graphs
Flow Separation
Heat Flux
Kerosene
Large Eddy Simulation
Musculoskeletal System
Real Time Systems
Sensitivity Analysis
Spacecraft
Transients
A comparative study of highly underexpanded nitrogen and hydrogenjets using large eddy simulation
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Li XP(李晓鹏)
;
Wu K(吴坤)
;
Yao W(姚卫)
;
Fan XJ(范学军)
Adobe PDF(728Kb)
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Submit date:2017/05/05
Comparative Studies
Flow Charac
Teristics
High Order Harmonics
High Resolution
Instability Modes
Near
Field Structure
Shock Structure
Under
Expanded Jets
Three-dimensional numerical study of the acoustic properities of a highly underexpanded jet
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Wu K(吴坤)
;
Li XP(李晓鹏)
;
Yao W(姚卫)
;
Fan XJ(范学军)
Adobe PDF(590Kb)
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Submit date:2017/05/05
Frequency Spectrum Analysis
High Temporal Resolution
Instantaneous Flow
Noise Generation Mechanisms
Theoretical Modeling
Three
Dimensional Numerical Studies
Transport Mechanism
Under
Expanded Jets
基于大庆RP-3航空煤油的轴对称截面燃烧室DES模拟
会议论文
第八届全国高超声速科技学术会议, 中国黑龙江哈尔滨, 2015-12-28
Authors:
姚卫
;
李晓鹏
;
吴坤
;
范学军
Adobe PDF(653Kb)
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View/Download:327/87
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Submit date:2016/08/16
Des
Rp-3
超声速燃烧
流场结构
航空煤油
点火过程
湍流模型
自由基浓度
热释放速率
预测分析
欠膨胀声速氮气射流大涡模拟研究
会议论文
第八届全国流体力学学术会议, 中国甘肃兰州, 2014-09-18
Authors:
李晓鹏
;
姚卫
;
范学军
Adobe PDF(127Kb)
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Submit date:2015/07/01
欠膨胀声速射流
蘑菇型涡结构
射流穿透深度
射流最大宽度
失稳机理
Characteristic scales in supersonic combustion
会议论文
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, San Jose, CA, United states, JUL 14-17, 2013
Authors:
Li XP(李晓鹏)
;
Fan XJ(范学军)
;
Li XP(李晓鹏)
Adobe PDF(669Kb)
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Submit date:2014/02/24