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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
Authors: 周志登; 晋国栋
 View |  Adobe PDF(816Kb) |  Favorite | View/Download：420/101 | Submit date：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 |
| 多孔介质中渗流致细颗粒运移实验探讨 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（A）, 中国北京, 2017-08-13
Authors: 罗大双; 王晶; 张旭辉; 鲁晓兵
View | Adobe PDF(719Kb) | Favorite | View/Download：461/135 | Submit date：2018/12/12
细颗粒运移 颗粒级配 渗流压差 出砂 |
| 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：318/122 | Submit date：2020/08/26
Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems |
| 金属材料双晶体薄板界面能密度的尺寸效应 会议论文
北京力学会第二十三届学术年会, 中国北京, 2017-01-14
Authors: 王帅; 陈少华
View | Adobe PDF(2620Kb) | Favorite | View/Download：157/43 | Submit date：2018/12/12
金属材料 双晶体薄板界面 界面能密度 尺寸效应 |
| 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)
View | Adobe PDF(1173Kb) | Favorite | View/Download：487/235 | 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)
View | Adobe PDF(1358Kb) | Favorite | View/Download：462/118 | 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：304/108 | Submit date：2018/01/16
Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |
| Downstream pressure variation induced hysteresis in the scramjet isolator 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors: Huang TL(黄庭隆); Yue LJ(岳连捷); Ma SH; Jia YN(贾轶南); Zhang XY(张新宇); Yue, Lianjie(yuelj@imech.ac.cn)
View | Adobe PDF(704Kb) | Favorite | View/Download：294/100 | Submit date：2018/01/16
Spacecraft |
| Force Test in a Large-Scale Shock Tunnel 会议论文
55th AIAA Aerospace Sciences Meeting , Grapevine, Texas, 9-13 January 2017
Authors: Wang YP(汪运鹏); Liu YF(刘云峰); Luo ZT(罗长童); Jiang ZL(姜宗林)
View | Adobe PDF(6096Kb) | Favorite | View/Download：349/100 | Submit date：2018/01/16 |
| Resonance-coupling effect on broad band gap formation and sound absorption in locally resonant Sonic metamaterials with Woodpile structure 会议论文
24th International Congress on Sound and Vibration, ICSV 2017, London, United kingdom, July 23, 2017 - July 27, 2017
Authors: Wang YR(王育人); Jiang H(姜恒); Chen M(陈猛); Guo, Yanhong
View | Adobe PDF(477Kb) | Favorite | View/Download：374/123 | Submit date：2017/12/18 |
