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| A one-dimensional transient calculation method for flow instability of supercritical hydrocarbon in cooling channels 会议论文
AIAA Propulsion and Energy Forum, VIRTUAL EVENT, 2021年8月9-11日
Authors: Jin YC(靳一超) ; Wu K(吴坤); Lu Y(陆阳); Fan XJ(范学军)
 Adobe PDF(1121Kb) |  Favorite | View/Download：185/50 | Submit date：2022/07/04 |
| Influences of Domain Symmetry on Supersonic Combustion Modeling 期刊论文
JOURNAL OF PROPULSION AND POWER, 2019, 卷号: 35, 期号: 2, 页码: 451-465
Authors: Yao W(姚卫); Wu K(吴坤); Fan XJ(范学军)
 Adobe PDF(862Kb) | Favorite | View/Download：350/104 | Submit date：2019/04/11 |
| 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)
Adobe PDF(1120Kb) | Favorite | View/Download：516/111 | Submit date：2018/12/26 |
| Low-Dissipative Hybrid Compressible Solver Designed for Large-Eddy Simulation of Supersonic Turbulent Flows 期刊论文
AIAA JOURNAL, 2018, 卷号: 56, 期号: 8, 页码: 3086-3096
Authors: Lee YC(李亚超); Yao W(姚卫); Fan XJ(范学军)
Adobe PDF(1783Kb) | Favorite | View/Download：426/128 | Submit date：2018/10/19 |
| Modeling Analysis of an Actively Cooled Scramjet Combustor Under Different Kerosene/Air Ratios 期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 4, 页码: 975-991
Authors: Yao W(姚卫); Lu Y(陆阳); Wu K(吴坤); Wang J(王晶); Fan XJ(范学军)
Adobe PDF(2427Kb) | Favorite | View/Download：389/119 | Submit date：2018/10/19 |
| Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 3, 页码: 772-786
Authors: Yao W(姚卫); Yuan YM(袁越明); Li XP(李晓鹏); Wang J(王晶); Wu K(吴坤); Fan XJ(范学军)
Adobe PDF(807Kb) | Favorite | View/Download：372/120 | Submit date：2018/07/17 |
| Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
Authors: Yao W(姚卫); Yuan YM(袁越明); Li XP(李晓鹏); Wang J(王晶); Wu K(吴坤); Fan XJ(范学军)
Adobe PDF(805Kb) | Favorite | View/Download：423/159 | Submit date：2018/06/06 |
| 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)
Adobe PDF(1377Kb) | Favorite | View/Download：308/120 | 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)
Adobe PDF(1358Kb) | Favorite | View/Download：451/116 | 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)
Adobe PDF(623Kb) | Favorite | View/Download：290/102 | Submit date：2018/01/16
Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |
