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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:297/55  |  提交时间:2018/12/12 斜爆轰波 两步反应 波面不稳定性 |
| 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 作者: 罗大双; 王晶; 张旭辉; 鲁晓兵 浏览  |  Adobe PDF(719Kb)  |  收藏  |  浏览/下载:416/114  |  提交时间:2018/12/12 细颗粒运移 颗粒级配 渗流压差 出砂 |
| 深海水合物智能开采 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: 鲁晓兵; 张旭辉; 李鹏; 鲁力; 王淑云 浏览  |  Adobe PDF(472Kb)  |  收藏  |  浏览/下载:197/63  |  提交时间:2018/12/12 水合物 智能开采 传热 地层稳定 |
| 评价现场混装炸药爆热稳定性的实验研究 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: 李世海; 乔继延; 冯春; 郭汝坤 浏览  |  Adobe PDF(885Kb)  |  收藏  |  浏览/下载:190/56  |  提交时间:2018/12/12 现场混装炸药 爆热 气泡脉动周期 PVDF膜片 |
| 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:180/49  |  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:280/113  |  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) Adobe PDF(1173Kb)  |  收藏  |  浏览/下载:442/217  |  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:313/100  |  提交时间:2018/01/16 Combustors Cracks Diesel Engines Efficiency Ethylene Fighter Aircraft Fuels High Speed Cameras Ignition Kerosene Luminance Spacecraft Stabilization |