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| 高马赫数超燃冲压发动机技术研究进展 期刊论文 力学学报, 2022, 卷号: 54, 期号: 02, 页码: 263-288 Authors: 岳连捷; 张旭; 张启帆; 陈科挺; 李进平; 陈昊; 姚卫; 仲峰泉; 李飞; 王春; 陈宏 Adobe PDF(2622Kb)  |  Favorite  |  View/Download:578/110  |  Submit date:2022/03/16 高马赫数 超燃冲压发动机 热化学非平衡 超声速燃烧 低雷诺数流动 激波风洞 飞行试验 |
| Numerical investigation on the performance of bluff body augmented micro cavity-combustor 期刊论文 INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 7, 页码: 4932-4945 Authors: Zhang Z; Wu K(吴坤); Yuen R; Yao W(姚卫); Wang J Adobe PDF(3438Kb)  |  Favorite  |  View/Download:333/113  |  Submit date:2020/04/07 Micro combustor Cavity Bluff body Combustion efficiency Local Damkohler number |
| 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:346/102  |  Submit date:2019/04/11 |
| 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:385/117  |  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) View  |  Adobe PDF(807Kb)  |  Favorite  |  View/Download:368/118  |  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) View  |  Adobe PDF(805Kb)  |  Favorite  |  View/Download:420/157  |  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) View  |  Adobe PDF(1377Kb)  |  Favorite  |  View/Download:305/118  |  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:448/115  |  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:281/98  |  Submit date:2018/01/16 Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |
| 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:510/104  |  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 |