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High-Pressure Capturing Wing Configurations 期刊论文
AIAA JOURNAL, 2017, 卷号: 55, 期号: 6, 页码: 1909-1919
作者:  Cui K(崔凯);  Li GL;  Xiao Y(肖尧);  Xu YZ;  Cui,K(reprint author), Chinese Acad Sci, Inst Mech
浏览  |  Adobe PDF(671Kb)  |  收藏  |  浏览/下载：617/171  |  提交时间：2017/07/24
Theories and technologies for duplicating hypersonic flight conditions for ground testing 期刊论文
NATIONAL SCIENCE REVIEW, 2017, 卷号: 4, 期号: 3, 页码: 290-U461
作者:  Jiang ZL(姜宗林);  Yu HR(俞鸿儒);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing, Peoples R China.;  Jiang, ZL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing, Peoples R China.
浏览  |  Adobe PDF(1315Kb)  |  收藏  |  浏览/下载：336/128  |  提交时间：2017/11/29
Numerical investigation of characteristic frequency excited highly underexpanded jets 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 63, 页码: 304-316
作者:  Li XP;  Fan E;  Yao W(姚卫);  Fan XJ(范学军);  Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Fan, XJ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
浏览  |  Adobe PDF(3588Kb)  |  收藏  |  浏览/下载：441/141  |  提交时间：2017/07/24
Fuel Jets  Underexpanded Jets  Jet Mixing Control  Excited Jets  Large Eddy Simulation  
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
作者:  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)
浏览  |  Adobe PDF(1173Kb)  |  收藏  |  浏览/下载：440/216  |  提交时间：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  
Experimental Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic Crossflow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Cheng LW(程柳维);  Zhong FQ(仲峰泉);  Wang ZP(王知溥);  Gu HB(顾洪斌);  Ma SG(马素刚);  Zhang XY(张新宇)
浏览  |  Adobe PDF(517Kb)  |  收藏  |  浏览/下载：310/100  |  提交时间：2018/01/16
Combustors  Cracks  Diesel Engines  Efficiency  Ethylene  Fighter Aircraft  Fuels  High Speed Cameras  Ignition  Kerosene  Luminance  Spacecraft  Stabilization  
LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军);  Zhang, Peng(pengzhang.zhang@polyu.edu.hk)
浏览  |  Adobe PDF(1249Kb)  |  收藏  |  浏览/下载：300/89  |  提交时间：2018/01/16
Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow  
Downstream pressure variation induced hysteresis in the scramjet isolator 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Ma SH;  Jia YN(贾轶南);  Zhang XY(张新宇);  Yue, Lianjie(yuelj@imech.ac.cn)
浏览  |  Adobe PDF(704Kb)  |  收藏  |  浏览/下载：259/90  |  提交时间：2018/01/16
Spacecraft  
Experimental Studies of Film Cooling in Supersonic Combustors 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Fan C(樊川);  Wang J(王晶);  Fan XJ(范学军)
浏览  |  Adobe PDF(735Kb)  |  收藏  |  浏览/下载：308/101  |  提交时间：2018/01/16
Combustion  Combustors  Coolants  Kerosene  Spacecraft  Supersonic Aerodynamics  
A low-dissipation solver based on openFOAM designed for large eddy simulation in compressible flow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
作者:  Lee YC;  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(1377Kb)  |  收藏  |  浏览/下载：480/91  |  提交时间：2018/11/08
Computational Fluid Dynamics  Digital Storage  Kinetic Energy  Kinetics  Open Source Software  Open Systems  Ramjet Engines  Runge Kutta Methods  Shock Tubes  Turbulence  Two Phase Flow  Bench  Mark Problems  Central  Upwind Scheme  Computational Fluid Dynamics Software  Skew  Symmetric Forms  Temporal Discretization  Turbulence Structures  Unstructured Meshes  Wall Bounded Turbulence  
Development of zone flamelet modelfor scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
作者:  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(832Kb)  |  收藏  |  浏览/下载：274/81  |  提交时间：2018/11/08
Combustion  Cost benefit analysis  Costs  Mixtures  Ramjet engines  Supersonic aircraft  Computational costs  Equivalence ratios  Local flow conditions  Scramjet combustors  Statistics approaches  Supersonic combustion  Supersonic combustors  Turbulent combustion