Selected(0)Clear
Items/Page: Sort: |
| 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)![](/image/person.jpg)
View  |   Adobe PDF(1377Kb)  |   Favorite  |  View/Download:315/121  |  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:485/234  |  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:457/116  |  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)![](/image/person.jpg)
Adobe PDF(623Kb)  |   Favorite  |  View/Download:299/105  |  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)![](/image/person.jpg)
Adobe PDF(517Kb)  |   Favorite  |  View/Download:350/114  |  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)
Adobe PDF(1249Kb)  |   Favorite  |  View/Download:341/105  |  Submit date:2018/01/16 Combustion Diesel Engines Hydrogen Large Eddy Simulation Spacecraft Stabilization Supersonic Aircraft Temperature Measurement Wall Flow |
| 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)![](/image/person.jpg)
Adobe PDF(2297Kb)  |   Favorite  |  View/Download:286/122  |  Submit date:2018/01/16 |
| 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 Authors: Lee YC; Yao W(姚卫) ; Fan XJ(范学军)![](/image/person.jpg)
Adobe PDF(1377Kb)  |   Favorite  |  View/Download:525/110  |  Submit date: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 Authors: Yao W(姚卫) ; Fan XJ(范学军)![](/image/person.jpg)
Adobe PDF(832Kb)  |   Favorite  |  View/Download:315/95  |  Submit date: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 |
| Performance of a detonation driven shock tunnel 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 Authors: Li JW ; Wang Q(汪球) ; Zhao W(赵伟) ; Lu P; Tan YX
Adobe PDF(468Kb)  |   Favorite  |  View/Download:320/86  |  Submit date:2018/01/16 Detonation Gas Dynamics Hypersonic Flow Shock Tubes Supersonic Aerodynamics |