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| 波流-桩体-海床动力耦合作用及其对单桩水平承载特性的影响 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: 漆文刚; 胡存; 高福平 浏览  |  Adobe PDF(917Kb)  |  收藏  |  浏览/下载:268/73  |  提交时间:2018/12/12 刚性单桩 多物理场 承载力 循环载荷 |
| 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:227/59  |  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 |
| 非线性水弹性波与超大型海洋浮式结构物 会议论文 第十届全国流体力学青年研讨会, 中国陕西西安, 2017-05-12 作者: 王展 浏览  |  Adobe PDF(753Kb)  |  收藏  |  浏览/下载:196/51  |  提交时间:2018/12/12 水弹性力学 挠曲重力波 超大型浮式结构物 内波 流固耦合 |
| 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:320/123  |  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:490/236  |  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:465/119  |  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:307/109  |  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:345/106  |  提交时间: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 作者: Wang YP(汪运鹏); Liu YF(刘云峰); Luo ZT(罗长童); Jiang ZL(姜宗林) 浏览  |  Adobe PDF(6096Kb)  |  收藏  |  浏览/下载:351/101  |  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) 浏览  |  Adobe PDF(566Kb)  |  收藏  |  浏览/下载:360/80  |  提交时间:2018/01/16 Boundary Layer Flow Boundary Layers Spacecraft Wind Tunnels |