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A numerical method for the solid mechanics with Euler variables 会议论文
International Conference on Physics Research and Application 2021 (CPRA 2021), Wuhan, China, 10-11 July 2021
作者:  Liu,Junchen;  Li SH(李世海);  Wang,Ling;  Feng C(冯春);  Qian,Feng;  Wang,Junfu;  Zhu XG(朱心广)
Adobe PDF(640Kb)  |  收藏  |  浏览/下载：194/41  |  提交时间：2021/08/30
Large eddy simulation of rest hypersonic combustor based on dynamic zone flamelet model 会议论文
AIAA Propulsion and Energy 2020 Forum, 24 August 2020 through 28 August 2020
作者:  Yao W(姚卫);  Chen L(陈留)
Adobe PDF(2272Kb)  |  收藏  |  浏览/下载：260/144  |  提交时间：2021/06/11
Numerical prediction of cooling performance sensitivity of 1st stage nozzle guide vane under aerothermal conditions 会议论文
ASME 2019 Gas Turbine India Conference, GTINDIA 2019, Chennai, Tamil Nadu, India, December 5, 2019 - December 6, 2019
作者:  Prapamonthon P;  Yin B(银波);  Yang GW(杨国伟);  Zhang MH(张莫晗)
Adobe PDF(2782Kb)  |  收藏  |  浏览/下载：160/61  |  提交时间：2020/11/20
Aerothermal condition  Cooling effectiveness  Cooling performance  Thermal sensitivity  Turbine vane  
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：278/112  |  提交时间：2020/08/26
Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems  
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：422/107  |  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  
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
作者:  Wang YR(王育人);  Jiang H(姜恒);  Chen M(陈猛);  Guo, Yanhong
浏览  |  Adobe PDF(477Kb)  |  收藏  |  浏览/下载：339/103  |  提交时间：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
作者:  Lee YC;  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(1377Kb)  |  收藏  |  浏览/下载：480/91  |  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  
Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp 会议论文
Meeting of the Institute-of-Non-Newtonian-Fluid-Mechanics (INNFM), Llanwddyn, WALES, 2017
作者:  Tong FL(童福林);  Li XL(李新亮);  Duan, Yanhui;  Yu ZP(于长平);  Yu, CP (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(3818Kb)  |  收藏  |  浏览/下载：295/117  |  提交时间：2018/01/16
Concave Surface Curvature  Adverse Pressure-gradient  Large-eddy Simulation  Reynolds-number  Near-wall  Flows  Separation  Vortices  Models  
Comparison of drag prediction using RANS models and DDES for the DLR-F6 configuration using high order schemes 会议论文
54th AIAA Aerospace Sciences Meeting, 2016, San Diego, CA, United states, January 4, 2016 - January 8, 2016
作者:  Gan JY;  Shen YQ(申义庆);  Zha GC
浏览  |  Adobe PDF(555Kb)  |  收藏  |  浏览/下载：279/91  |  提交时间：2017/05/05
Central Differencing  Drag Prediction  Finite Difference Scheme  High  Order Scheme  Line Relaxation  Mesh Refinement  Trailing Edges  Turbulent Models  
Visualization of flow separation inside cut kerf during laser cutting of thick sections 会议论文
34th International Congress on Applications of Lasers and Electro-Optics (ICALEO), Atlanta, GA, OCT 18-22, 2015
作者:  Zhang C;  Wen P;  Yao ZH;  Yuan YM(袁越明);  Fan XJ(范学军);  Wen, P (reprint author), Tsinghua Univ, State Key Lab Tribol, Beijing 100084, Peoples R China.
浏览  |  Adobe PDF(1350Kb)  |  收藏  |  浏览/下载：306/107  |  提交时间：2016/06/28