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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：437/111  |  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  
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：319/94  |  Submit date：2018/01/16
Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow  
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：499/99  |  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  
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)
View  |  Adobe PDF(1066Kb)  |  Favorite  |  View/Download：428/92  |  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