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Numerical study of a fully confined supersonic slot impinging jet from bleed system 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22
Authors:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Chang XY(张新宇)
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Fully confined supersonic jet  Inclined impingement  Heat transfer  Boundary layer bleed  Numerical simulation  
External-Compression Supersonic Inlet Free from Violent Buzz 期刊论文
AIAA JOURNAL, 2019, 卷号: 57, 期号: 6, 页码: 2513-2523
Authors:  Chen H;  Tan H;  Liu YZ;  Zhang QF(张启帆)
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真实气体效应对Ma10级进气道流动的影响 期刊论文
推进技术, 2019, 卷号: 40, 期号: 05, 页码: 1042-1050
Authors:  张启帆;  岳连捷;  贾轶楠;  张新宇;  李欣;  高雄
View  |  Adobe PDF(1675Kb)  |  Favorite  |  View/Download:15/1  |  Submit date:2019/09/12
真实气体效应  高马赫数进气道  化学非平衡气体模型  热完全气体模型  前缘钝化  再起动性能  
Full-scale Improved Delayed Detached Eddy Simulation of Transverse Hydrogen Jet in Supersonic Combustion 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018
Authors:  Fan E;  Wu K(吴坤);  Lee YC(李亚超);  Yao W(姚卫);  Fan XJ(范学军)
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高超声速进气道再起动特性影响规律研究 学位论文
博士论文,北京: 中国科学院大学, 2018
Authors:  贾轶楠
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高超声速进气道、再起动、激波-边界层相互作用  
Effect of peak perforation on flow past a conic cylinder at Re=100: drag lift and Strouhal number 期刊论文
CHINA OCEAN ENGINEERING, 2017, 卷号: 31, 期号: 3, 页码: 330-340
Authors:  Lin LM(林黎明);  Zhong XF(钟兴福);  Wu YX(吴应湘)
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Vortex-induced Vibration  Perforation  Conic Disturbance  Drag  Lift  Strouhal Number  
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)
View  |  Adobe PDF(1173Kb)  |  Favorite  |  View/Download:139/45  |  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  
Full Scale Detached Eddy Simulation of Transverse Hydrogen Jet in Supersonic Combustion 会议论文
53rd AIAA/SAE/ASEE Joint Propulsion Conference , Atlanta, GA., 10-12 July 2017
Authors:  Fan E;  Wu K(吴坤);  Lee YC;  Yao W(姚卫);  Fan XJ(范学军)
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Role of wall temperature on shock train in a rectangular isolator 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:  Lu HB;  Wang D;  Chen X;  Yue LJ(岳连捷);  Ji, Feng (yuelj@imech.ac.cn)
View  |  Adobe PDF(560Kb)  |  Favorite  |  View/Download:100/37  |  Submit date:2017/05/05
Aero  Heating  Dual Mechanisms  On Flow  Shock Train  Specific Heat Ratio  Total Pressure  Total Temperatures  Wall Temperatures  
壁温对激波-湍流边界层干扰的影响规律研究 学位论文
硕士论文,北京: 中国科学院大学, 2016
Authors:  朱兴坤
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