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| On the application of dynamic zone flamelet model to large eddy simulation of supersonic hydrogen flame 期刊论文 INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 41, 页码: 21940-21955 作者: Yao W(姚卫) Adobe PDF(3791Kb)  |  收藏  |  浏览/下载:262/132  |  提交时间:2020/09/27 Dynamic zone flamelet model Supersonic hydrogen jet Large eddy simulation Supersonic combustion Turbulent combustion model |
| 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 作者: Yao W(姚卫); Chen L(陈留) Adobe PDF(2272Kb)  |  收藏  |  浏览/下载:264/145  |  提交时间:2021/06/11 |
| 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 作者: 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) 浏览  |  Adobe PDF(2651Kb)  |  收藏  |  浏览/下载:405/132  |  提交时间:2019/09/09 Heat flux measurement Kerosene Supersonic combustion Scramjet Heat flux sensor |
| 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 作者: Yao W(姚卫); Wu K(吴坤); Fan XJ(范学军) Adobe PDF(862Kb)  |  收藏  |  浏览/下载:322/97  |  提交时间:2019/04/11 |
| Application of dynamic zone flamelet model to a GH2/GO2 rocket combustor 会议论文 AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019 作者: Yao W(姚卫); Li B(李波) Adobe PDF(1665Kb)  |  收藏  |  浏览/下载:143/43  |  提交时间:2020/11/20 Dynamic zone flamelet model GH2/GO2 Large Eddy Simulation (LES) Rocket combustor Turbulence-chemistry interaction |
| 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 作者: Yao W(姚卫); Lu Y(陆阳); Wu K(吴坤); Wang J(王晶); Fan XJ(范学军) 浏览  |  Adobe PDF(2427Kb)  |  收藏  |  浏览/下载:357/108  |  提交时间:2018/10/19 |
| 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 作者: Lee YC(李亚超); Yao W(姚卫); Fan XJ(范学军) 浏览  |  Adobe PDF(1377Kb)  |  收藏  |  浏览/下载:280/113  |  提交时间: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 作者: 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) 浏览  |  Adobe PDF(1173Kb)  |  收藏  |  浏览/下载:442/217  |  提交时间: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 |
| 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 作者: Yao W(姚卫); Fan XJ(范学军) 浏览  |  Adobe PDF(623Kb)  |  收藏  |  浏览/下载:263/90  |  提交时间: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 作者: Lee YC; Yao W(姚卫); Fan XJ(范学军) 浏览  |  Adobe PDF(1377Kb)  |  收藏  |  浏览/下载:483/93  |  提交时间: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 |