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| 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：164/59 | 提交时间：2018/12/12
爆破管 液态CO2 同步性 试验研究 |
| 帽型粘接结构的动态力学行为研究 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（A）, 中国北京, 2017-08-13
作者: 廖丽涓; 杨喆; 魏延鹏; 吴先前; 郭雅悰; 黄晨光; 殷秋运; 孟昶宇
浏览 | Adobe PDF(1405Kb) | 收藏 | 浏览/下载：196/52 | 提交时间：2018/12/12
动态响应 帽型粘接结构 混合破坏 率相关 内聚力模型 |
| 椭圆声学超材料模型构建与带隙分析 会议论文
第十六届船舶水下噪声学术讨论会, 中国贵州贵阳, 2017-08-01
作者: 徐文帅; 蒙丹; 陈猛; 姜恒; 王育人; 刘宇; 刘瑞霞
浏览 | Adobe PDF(1574Kb) | 收藏 | 浏览/下载：207/32 | 提交时间：2018/12/12
声学超材料 椭圆散射体 振动模态 能带结构 |
| 新型压电导电材料阻尼特性研究 会议论文
第十六届船舶水下噪声学术讨论会, 中国贵州贵阳, 2017-08-01
作者: 刘宇; 韩金花; 陈猛; 姜恒; 王育人; 徐文帅; 刘瑞霞
浏览 | Adobe PDF(1578Kb) | 收藏 | 浏览/下载：267/93 | 提交时间：2018/12/12
压电导电材料 导电相 阻尼特性 |
| 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：279/113 | 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：441/217 | 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 |
| 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)
浏览 | Adobe PDF(1358Kb) | 收藏 | 浏览/下载：424/107 | 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：263/90 | 提交时间：2018/01/16
Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |
| Experimental Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic Crossflow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者: Cheng LW(程柳维); Zhong FQ(仲峰泉); Wang ZP(王知溥); Gu HB(顾洪斌); Ma SG(马素刚); Zhang XY(张新宇)
浏览 | Adobe PDF(517Kb) | 收藏 | 浏览/下载：311/100 | 提交时间：2018/01/16
Combustors Cracks Diesel Engines Efficiency Ethylene Fighter Aircraft Fuels High Speed Cameras Ignition Kerosene Luminance Spacecraft Stabilization |
| 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：300/89 | 提交时间：2018/01/16
Combustion Diesel Engines Hydrogen Large Eddy Simulation Spacecraft Stabilization Supersonic Aircraft Temperature Measurement Wall Flow |
