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| 灾变破坏的一种单参数前兆及其在破坏时间预测中的应用 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: 杨航; 郝圣旺 View  |  Adobe PDF(826Kb)  |  Favorite  |  View/Download:204/64  |  Submit date:2018/12/12 临界 前兆 破坏时间 预测 |
| 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 Authors: 范永波; 李世海; 乔继延; 段文杰 View  |  Adobe PDF(790Kb)  |  Favorite  |  View/Download:182/66  |  Submit date: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 Authors: Lee YC(李亚超); Yao W(姚卫); Fan XJ(范学军) View  |  Adobe PDF(1377Kb)  |  Favorite  |  View/Download:302/117  |  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) View  |  Adobe PDF(1173Kb)  |  Favorite  |  View/Download:475/230  |  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:446/114  |  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:280/97  |  Submit date: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 Authors: Wu K(吴坤); Zhang P(张鹏); Yao W(姚卫); Fan XJ(范学军); Zhang, Peng(pengzhang.zhang@polyu.edu.hk) View  |  Adobe PDF(1249Kb)  |  Favorite  |  View/Download:329/99  |  Submit date:2018/01/16 Combustion Diesel Engines Hydrogen Large Eddy Simulation Spacecraft Stabilization Supersonic Aircraft Temperature Measurement Wall Flow |
| 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:333/95  |  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:359/115  |  Submit date:2017/12/18 |
| 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 Authors: Lee YC; Yao W(姚卫); Fan XJ(范学军) View  |  Adobe PDF(1377Kb)  |  Favorite  |  View/Download:509/104  |  Submit date: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 |