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| A low-dissipation solver based on OpenFOAM designed for large eddy simulation in compressible flows 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 Authors: Lee YC(李亚超); Yao W(姚卫); Fan XJ(范学军) View  |  Adobe PDF(1377Kb)  |  Favorite  |  View/Download:296/116  |  Submit date:2020/08/26 Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems |
| 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:470/228  |  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 |
| A low-dissipation scheme based on OpenFoam designed for large eddy simulation in compressible flow 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 Authors: Lee YC; Yao W(姚卫); Fan XJ(范学军); Yao, Wei(weiyao@imech.ac.cn) View  |  Adobe PDF(1358Kb)  |  Favorite  |  View/Download:440/112  |  Submit date:2018/01/16 Computational Fluid Dynamics Computer Software Digital Storage Kinetic Energy Kinetics Open Source Software Open Systems Runge Kutta Methods Shock Tubes Shock Waves Spacecraft Turbulence Two Phase Flow |
| 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) View  |  Adobe PDF(623Kb)  |  Favorite  |  View/Download:273/94  |  Submit date:2018/01/16 Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |
| 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 Authors: 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) View  |  Adobe PDF(517Kb)  |  Favorite  |  View/Download:333/109  |  Submit date: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 Authors: Wu K(吴坤); Zhang P(张鹏); Yao W(姚卫); Fan XJ(范学军); Zhang, Peng(pengzhang.zhang@polyu.edu.hk) View  |  Adobe PDF(1249Kb)  |  Favorite  |  View/Download:323/96  |  Submit date: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 Authors: 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) View  |  Adobe PDF(704Kb)  |  Favorite  |  View/Download:276/93  |  Submit date: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 Authors: Fan C(樊川); Wang J(王晶); Fan XJ(范学军) View  |  Adobe PDF(735Kb)  |  Favorite  |  View/Download:334/112  |  Submit date:2018/01/16 Combustion Combustors Coolants Kerosene Spacecraft Supersonic Aerodynamics |
| The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 Authors: Jia YN(贾轶南); Yue LJ(岳连捷); Zhang XY(张新宇); Jia, Yinan(yuelj@imech.ac.cn) View  |  Adobe PDF(566Kb)  |  Favorite  |  View/Download:341/74  |  Submit date:2018/01/16 Boundary Layer Flow Boundary Layers Spacecraft Wind Tunnels |
| Numerical study of oblique detonation initiations with chain-branching kinetics 会议论文 AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting, Grapevine, Texas, 9-13 January 2017 Authors: Teng HH(滕宏辉); Yang PF(杨鹏飞); Jiang ZL(姜宗林) View  |  Adobe PDF(464Kb)  |  Favorite  |  View/Download:291/116  |  Submit date:2018/01/16 |