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| 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:439/112  |  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 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:332/112  |  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:340/74  |  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:501/101  |  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:298/89  |  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 |
| Multispecies Absorption Measurement in an Ammonium Dinitramide based Thruster 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 Authors: Zeng W(曾徽); Lin X(林鑫); Zhen RP; Chen LZ; Li F(李飞); Yu XL(余西龙); Li, Fei(lifei@imech.ac.cn) View  |  Adobe PDF(897Kb)  |  Favorite  |  View/Download:478/102  |  Submit date:2018/01/16 Combustion Gas Absorption Infrared Devices Monopropellants Optical Parametric Oscillators Spacecraft |
| 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:403/98  |  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 |
| 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:289/91  |  Submit date:2018/01/16 Aerodynamics Air Engines Aspect Ratio Computational Fluid Dynamics Drag Engines Hypersonic Aerodynamics Lift Lift Drag Ratio Propulsion Spacecraft Vehicles |
| Study on Compression Surface Deformation of Waveriders 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 Authors: Xu YZ(徐应洲); Cui K(崔凯); Li GL(李广利); Xiao Y(肖尧) View  |  Adobe PDF(461Kb)  |  Favorite  |  View/Download:329/89  |  Submit date:2018/01/16 Aerodynamic Configurations Aerodynamics Computational Fluid Dynamics Deformation Evolutionary Algorithms Fluid Dynamics Hypersonic Aerodynamics Optimization Spacecraft |