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| 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:476/230  |  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:446/114  |  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:280/97  |  Submit date:2018/01/16 Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |
| 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:285/96  |  Submit date:2018/01/16 Spacecraft |
| 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:346/75  |  Submit date:2018/01/16 Boundary Layer Flow Boundary Layers Spacecraft Wind Tunnels |
| 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) View  |  Adobe PDF(1377Kb)  |  Favorite  |  View/Download:509/104  |  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) View  |  Adobe PDF(832Kb)  |  Favorite  |  View/Download:307/93  |  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 |
| Preliminary Study of Aerodynamic Performance for Waverider-based Hypersonic Vehicles with Dorsal Mounted Engines 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 Authors: Xiao Y(肖尧); Cui K(崔凯); Li GL(李广利); Xu YZ(徐应洲) View  |  Adobe PDF(639Kb)  |  Favorite  |  View/Download:298/96  |  Submit date:2018/01/16 Aerodynamics Air Engines Aspect Ratio Computational Fluid Dynamics Drag Engines Hypersonic Aerodynamics Lift Lift Drag Ratio Propulsion Spacecraft Vehicles |
| Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock Tunnel 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 Authors: Wang Q(汪球); Li JW; Lu P; Li JP(李进平); Zhao W(赵伟); Jiang ZL(姜宗林) View  |  Adobe PDF(679Kb)  |  Favorite  |  View/Download:411/77  |  Submit date:2018/01/16 Calibration Detonation Heat Transfer Nozzles Spacecraft Supersonic Aerodynamics Thermodynamics Uncertainty Analysis |
| 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 View  |  Adobe PDF(468Kb)  |  Favorite  |  View/Download:316/85  |  Submit date:2018/01/16 Detonation Gas Dynamics Hypersonic Flow Shock Tubes Supersonic Aerodynamics |