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| 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
Authors: Jin Y ; 廖飞, Cai JS
 Adobe PDF(4611Kb) |  Favorite | View/Download：229/115 | Submit date：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
Authors: Jin Y; Liao F(廖飞); Cai JS; Morris PJ
Adobe PDF(2986Kb) | Favorite | View/Download：233/79 | Submit date：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
Authors: Xue XW(薛晓薇); Chen S; Sun QH(孙泉华)
Adobe PDF(1688Kb) | Favorite | View/Download：176/76 | Submit date：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
Authors: Li B; Lee YC(李亚超); Yao W(姚卫); Lu Y(陆阳); Fan XJ(范学军)
 View |  Adobe PDF(1813Kb) | Favorite | View/Download：328/86 | Submit date：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
Authors: Wang Y; Yao W(姚卫); Fan XJ(范学军)
View | Adobe PDF(1120Kb) | Favorite | View/Download：506/109 | Submit date：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
Authors: Li B(李波); Lee YC(李亚超); Yao W(姚卫); Fan XJ(范学军)
View | Adobe PDF(1813Kb) | Favorite | View/Download：218/68 | Submit date：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
Authors: Li YL; Guo SX(郭双喜); Li M; Chen WM(陈伟民); Kong Y
View | Adobe PDF(1944Kb) | Favorite | View/Download：315/61 | Submit date：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
Authors: Lee YC(李亚超); Yao W(姚卫); Fan XJ(范学军)
View | Adobe PDF(1377Kb) | Favorite | View/Download：298/116 | Submit date：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
Authors: Lee YC; Yao W(姚卫); Fan XJ(范学军); Yao, Wei(weiyao@imech.ac.cn)
View | Adobe PDF(1358Kb) | Favorite | View/Download：440/112 | Submit date：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
Authors: Jia YN(贾轶南); Yue LJ(岳连捷); Zhang XY(张新宇); Jia, Yinan(yuelj@imech.ac.cn)
View | Adobe PDF(566Kb) | Favorite | View/Download：341/74 | Submit date：2018/01/16
Boundary Layer Flow Boundary Layers Spacecraft Wind Tunnels |
