Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-3 of 3 Help

Filters                            
Selected(0)Clear Items/Page:    Sort:
Decomposition of mean skin friction in incident shock wave/turbulent boundary layer interaction flows at Mach 2.25 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 9, 页码: 178-194
Authors:  Duan JY(段俊亦);  Tong FL(童福林);  Li XL(李新亮);  Liu HW(刘洪伟)
Adobe PDF(6039Kb)  |  Favorite  |  View/Download：121/8  |  Submit date：2023/11/13
Compressible flow  Boundary layers  Direct numerical simulation  Shock waves  Skin friction  Turbulent flow  
Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 5, 页码: 350-363
Authors:  Tong FL(童福林);  Sun D(孙栋);  Li XL(李新亮)
Adobe PDF(4402Kb)  |  Favorite  |  View/Download：217/51  |  Submit date：2021/06/07
Direct numerical simulation  Low-frequency unsteadiness  Shock waves  Turbulent boundary layer  Wavy-wall  
Improvement of Baldwin-Lomax turbulence model for supersonic complex flows 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2013, 卷号: 26, 期号: 3, 页码: 529–534
Authors:  Zhao R(赵瑞);  Yan C(阎超);  Yu J(于剑);  Li XL(李新亮);  Yan, C (reprint author), Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China.
Adobe PDF(1609Kb)  |  Favorite  |  View/Download：889/293  |  Submit date：2013/09/21
Baldwin-lomax Model  Boundary Layers  Computational Aerodynamics  Entropy  Supersonic Flows  Turbulence Models