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| 基于两步反应模型的斜爆轰波面不稳定性的数值研究 会议论文
中国航天第三专业信息网第三十八届技术交流会暨第二届空天动力联合会议, 中国辽宁大连, 2017-08-23
作者: 杨鹏飞; 滕宏辉 ; 姜宗林
 浏览 |  Adobe PDF(893Kb) |  收藏 | 浏览/下载：299/55 | 提交时间：2018/12/12
斜爆轰波 两步反应 波面不稳定性 |
| 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：388/95 | 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 |
| 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：281/113 | 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：448/221 | 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：426/108 | 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)
Adobe PDF(623Kb) | 收藏 | 浏览/下载：264/91 | 提交时间：2018/01/16
Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |
| Force Test in a Large-Scale Shock Tunnel 会议论文
55th AIAA Aerospace Sciences Meeting , Grapevine, Texas, 9-13 January 2017
作者: Wang YP(汪运鹏); Liu YF(刘云峰); Luo ZT(罗长童); Jiang ZL(姜宗林)
Adobe PDF(6096Kb) | 收藏 | 浏览/下载：310/90 | 提交时间：2018/01/16 |
| The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者: Jia YN(贾轶南); Yue LJ(岳连捷); Zhang XY(张新宇); Jia, Yinan(yuelj@imech.ac.cn)
Adobe PDF(566Kb) | 收藏 | 浏览/下载：331/73 | 提交时间：2018/01/16
Boundary Layer Flow Boundary Layers Spacecraft Wind Tunnels |
| 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)
Adobe PDF(2297Kb) | 收藏 | 浏览/下载：257/111 | 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)
Adobe PDF(1377Kb) | 收藏 | 浏览/下载：484/94 | 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 |
