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| Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14 Authors: Yao W(姚卫); Liu H(刘杭); Yue LJ(岳连捷); Xiao YB(肖雅彬) Adobe PDF(2954Kb)  |  Favorite  |  View/Download:290/67  |  Submit date:2021/11/15 Hypersonic combustion Hydrogen Improved Delayed Detached Eddy Simulation (IDDES) Dynamic zone flamelet model Scramjet |
| Large eddy simulation of rest hypersonic combustor based on dynamic zone flamelet model 会议论文 AIAA Propulsion and Energy 2020 Forum, 24 August 2020 through 28 August 2020 Authors: Yao W(姚卫); Chen L(陈留) Adobe PDF(2272Kb)  |  Favorite  |  View/Download:283/150  |  Submit date:2021/06/11 |
| Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms 期刊论文 ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1155-1177 Authors: Yao W(姚卫) View  |  Adobe PDF(9586Kb)  |  Favorite  |  View/Download:660/296  |  Submit date:2019/12/17 Kerosene Supersonic combustion Large eddy simulation Skeletal mechanism Scramjet |
| Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor 期刊论文 JOURNAL OF AEROSPACE ENGINEERING, 2019, 卷号: 32, 期号: 5, 页码: 11 Authors: Cheng D(程迪); Wang J(王晶); Lu Y(陆阳); Li L(李龙); Yao W(姚卫); Fan XJ(范学军) View  |  Adobe PDF(2651Kb)  |  Favorite  |  View/Download:419/137  |  Submit date:2019/09/09 Heat flux measurement Kerosene Supersonic combustion Scramjet Heat flux sensor |
| 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) View  |  Adobe PDF(1783Kb)  |  Favorite  |  View/Download:412/125  |  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:360/114  |  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:412/154  |  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:294/115  |  Submit date:2020/08/26 Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems |
| A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 Authors: Yao W(姚卫); Yuan YM(袁越明); Li XP(李晓鹏); Wang J(王晶); Fan XJ(范学军); Fan, Xuejun(xfan@imech.ac.cn) Adobe PDF(1173Kb)  |  Favorite  |  View/Download:469/227  |  Submit date:2018/01/16 Adiabatic Flame Temperature Aerodynamics Boundary Layer Flow Boundary Layers Chemical Analysis Combustion Computational Chemistry Directed Graphs Flow Separation Mach Number Principal Component Analysis Regression Analysis Sensitivity Analysis Spacecraft Supersonic Aerodynamics Supersonic Aircraft Transients |
| 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: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 |