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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:486/234  |  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)
View  |   Adobe PDF(623Kb)  |   Favorite  |  View/Download:302/106  |  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:293/100  |  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)![](/image/person.jpg)
View  |   Adobe PDF(735Kb)  |   Favorite  |  View/Download:352/120  |  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:353/78  |  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)![](/image/person.jpg)
View  |   Adobe PDF(1377Kb)  |   Favorite  |  View/Download:526/110  |  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)
View  |   Adobe PDF(832Kb)  |   Favorite  |  View/Download:320/97  |  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 |
| Normal acceleration reduce guidanceand control for sub-orbit vehicle re-entry 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 Authors: Li WH(李文皓) ; Xiao XX(肖歆昕) ; Zhang H(张珩) ; Xiao XX(肖歆昕)![](/image/person.jpg)
View  |   Adobe PDF(1066Kb)  |   Favorite  |  View/Download:446/97  |  Submit date:2018/01/16 Aerodynamics Air Navigation Angle Of Attack Control Surfaces Control Theory Degrees Of Freedom (Mechanics) Dynamic Models Flight Control Systems Flight Simulators Monte Carlo Methods Reentry Spacecraft Surface Reactions Uncertainty Analysis Vehicles |
| Effects of Shock Impingement on Aerothermal and Aerodynamic Performance for High-pressure Capturing Wings 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 Authors: Li GL(李广利) ; Cui K(崔凯) ; Xiao Y(肖尧) ; Xu YZ(徐应洲)
View  |   Adobe PDF(664Kb)  |   Favorite  |  View/Download:418/103  |  Submit date:2018/01/16 Aerodynamics Angle Of Attack Angle Of Attack Indicators Boundary Layers Drag Drag Coefficient High Pressure Effects Hypersonic Aerodynamics Hypersonic Flow Spacecraft |