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| 有限雷诺数下颗粒靠近壁面运动的受力和力矩模型 会议论文 中国力学大会-2017暨庆祝中国力学学会成立60周年大会(B), 中国北京, 2017-08-13 作者: 周志登; 晋国栋 浏览  |  Adobe PDF(816Kb)  |  收藏  |  浏览/下载:390/95  |  提交时间:2018/12/12 受力和力矩模型 有限颗粒雷诺数 靠近壁面 格子Boltzmann方法 亚格子尺度模型 |
| 液态CO_2多致裂管爆破同步性及爆破效果优化试验研究 会议论文 中国力学大会-2017暨庆祝中国力学学会成立60周年大会(C), 中国北京, 2017-08-13 作者: 范永波; 李世海; 乔继延; 段文杰 浏览  |  Adobe PDF(790Kb)  |  收藏  |  浏览/下载:165/59  |  提交时间:2018/12/12 爆破管 液态CO2 同步性 试验研究 |
| 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:283/113  |  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) Adobe PDF(1173Kb)  |  收藏  |  浏览/下载:451/222  |  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 |
| 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 作者: Lee YC; Yao W(姚卫); Fan XJ(范学军); Yao, Wei(weiyao@imech.ac.cn) Adobe PDF(1358Kb)  |  收藏  |  浏览/下载:428/108  |  提交时间: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 作者: Yao W(姚卫); Fan XJ(范学军) 浏览  |  Adobe PDF(623Kb)  |  收藏  |  浏览/下载:266/92  |  提交时间: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 作者: Wu K(吴坤); Zhang P(张鹏); Yao W(姚卫); Fan XJ(范学军); Zhang, Peng(pengzhang.zhang@polyu.edu.hk) 浏览  |  Adobe PDF(1249Kb)  |  收藏  |  浏览/下载:304/90  |  提交时间:2018/01/16 Combustion Diesel Engines Hydrogen Large Eddy Simulation Spacecraft Stabilization Supersonic Aircraft Temperature Measurement Wall Flow |
| Full Scale Detached Eddy Simulation of Transverse Hydrogen Jet in Supersonic Combustion 会议论文 53rd AIAA/SAE/ASEE Joint Propulsion Conference , Atlanta, GA., 10-12 July 2017 作者: Fan E; Wu K(吴坤); Lee YC; Yao W(姚卫); Fan XJ(范学军) 浏览  |  Adobe PDF(2297Kb)  |  收藏  |  浏览/下载:260/112  |  提交时间:2018/01/16 |
| 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:487/95  |  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 |
| Development of zone flamelet modelfor scramjet combustor modeling 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: Yao W(姚卫); Fan XJ(范学军) 浏览  |  Adobe PDF(832Kb)  |  收藏  |  浏览/下载:280/83  |  提交时间:2018/11/08 Combustion Cost benefit analysis Costs Mixtures Ramjet engines Supersonic aircraft Computational costs Equivalence ratios Local flow conditions Scramjet combustors Statistics approaches Supersonic combustion Supersonic combustors Turbulent combustion |