中文版 | English

在结果中检索

IMECH-IR

浏览/检索结果: 共48条，第1-10条 帮助

限定条件    
已选(0)清除 条数/页：   排序方式：
Numerical simulation of 30p30n multi-element airfoil using delayed detached-eddy simulation 会议论文
AIAA AVIATION 2020 FORUM, 15 June 2020 through 19 June 2020
作者:  Jin Y;  廖飞, Cai JS
Adobe PDF(4611Kb)  |  收藏  |  浏览/下载：192/104  |  提交时间：2021/06/11
Investigation of high-order cell-centered finite difference method for aeroacoustics 会议论文
25th AIAA/CEAS Aeroacoustics Conference, 2019, Delft, Netherlands, May 20, 2019 - May 23, 2019
作者:  Jin Y;  Liao F(廖飞);  Cai JS;  Morris PJ
Adobe PDF(2986Kb)  |  收藏  |  浏览/下载：204/73  |  提交时间：2020/11/20
Investigation of shock attenuation in a shock tube using DSMC method 会议论文
31st International Symposium on Rarefied Gas Dynamics, RGD 2018, University of StrathclydeGlasgow; United Kingdom;, 23 July 2018 ~ 27 July 2018
作者:  Xue XW(薛晓薇);  Chen S;  Sun QH(孙泉华)
Adobe PDF(1688Kb)  |  收藏  |  浏览/下载：155/71  |  提交时间：2020/11/20
Prediction of kerosene properties at supercritical pressures by Artificial Neural Network 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018
作者:  Li B;  Lee YC(李亚超);  Yao W(姚卫);  Lu Y(陆阳);  Fan XJ(范学军)
Adobe PDF(1813Kb)  |  收藏  |  浏览/下载：298/80  |  提交时间：2018/12/26
Real-gas Effect Accounted for by the Principle of Extended Corresponding States in Modeling Supersonic Kerosene Jet 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018
作者:  Wang Y;  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(1120Kb)  |  收藏  |  浏览/下载：481/102  |  提交时间：2018/12/26
Prediction of kerosene properties at supercritical pressures by Artificial Neural Network 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio., July 9-11, 2018
作者:  Li B(李波);  Lee YC(李亚超);  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(1813Kb)  |  收藏  |  浏览/下载：167/61  |  提交时间：2020/08/27
DYNAMIC RESPONSE ANALYSIS ON THE INTERACTION BETWEEN FLEXIBLE BODIES OF LARGE-SIZED WIND TURBINE UNDER RANDOM WIND LOADS 会议论文
37th ASME International Conference on Ocean, Offshore and Arctic Engineering, Madrid, SPAIN, JUN 17-22, 2018
作者:  Li YL;  Guo SX(郭双喜);  Li M;  Chen WM(陈伟民);  Kong Y
Adobe PDF(1944Kb)  |  收藏  |  浏览/下载：269/56  |  提交时间：2018/12/12
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)
Adobe PDF(1377Kb)  |  收藏  |  浏览/下载：275/112  |  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)
Adobe PDF(1358Kb)  |  收藏  |  浏览/下载：416/104  |  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  
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)
Adobe PDF(566Kb)  |  收藏  |  浏览/下载：321/68  |  提交时间：2018/01/16
Boundary Layer Flow  Boundary Layers  Spacecraft  Wind Tunnels