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| Evaluation of the influence of radiation on a GH2/GO2 rocket combustor 会议论文 AIAA Propulsion & Energy Forum, VIRTUAL EVENT, 2020-08-17 Authors: Li B(李波); Yao W(姚卫); Fan XJ(范学军) Adobe PDF(1358Kb)  |  Favorite  |  View/Download:158/49  |  Submit date:2021/02/01 |
| Influence of compressibility effect on supersonic combustion modeling 会议论文 AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019 Authors: Chen L; Yao W(姚卫); Fan XJ(范学军) Adobe PDF(1280Kb)  |  Favorite  |  View/Download:177/73  |  Submit date:2020/11/20 |
| Prediction of kerosene properties at supercritical pressures by Artificial Neural Network 会议论文 2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018 Authors: Li B; Lee YC(李亚超); Yao W(姚卫); Lu Y(陆阳); Fan XJ(范学军) View  |  Adobe PDF(1813Kb)  |  Favorite  |  View/Download:323/85  |  Submit date:2018/12/26 |
| Full-scale Improved Delayed Detached Eddy Simulation of Transverse Hydrogen Jet in Supersonic Combustion 会议论文 2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018 Authors: Fan E; Wu K(吴坤); Lee YC(李亚超); Yao W(姚卫); Fan XJ(范学军) View  |  Adobe PDF(567Kb)  |  Favorite  |  View/Download:342/102  |  Submit date:2018/12/26 |
| Real-gas Effect Accounted for by the Principle of Extended Corresponding States in Modeling Supersonic Kerosene Jet 会议论文 2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018 Authors: Wang Y; Yao W(姚卫); Fan XJ(范学军) View  |  Adobe PDF(1120Kb)  |  Favorite  |  View/Download:504/109  |  Submit date:2018/12/26 |
| Prediction of kerosene properties at supercritical pressures by Artificial Neural Network 会议论文 2018 Joint Propulsion Conference, Cincinnati, Ohio., July 9-11, 2018 Authors: Li B(李波); Lee YC(李亚超); Yao W(姚卫); Fan XJ(范学军) View  |  Adobe PDF(1813Kb)  |  Favorite  |  View/Download:191/67  |  Submit date:2020/08/27 |
| 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) View  |  Adobe PDF(1377Kb)  |  Favorite  |  View/Download:291/114  |  Submit date:2020/08/26 Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems |
| 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:436/111  |  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 |
| 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) Adobe PDF(623Kb)  |  Favorite  |  View/Download:271/94  |  Submit date:2018/01/16 Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |
| 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:317/93  |  Submit date:2018/01/16 Combustion Diesel Engines Hydrogen Large Eddy Simulation Spacecraft Stabilization Supersonic Aircraft Temperature Measurement Wall Flow |