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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：230/58  |  Submit date：2021/06/07
Direct numerical simulation  Low-frequency unsteadiness  Shock waves  Turbulent boundary layer  Wavy-wall  
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  Favorite  |  View/Download：357/178  |  Submit date：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
High-speed unsteady flows past two-body configurations 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2018, 卷号: 31, 期号: 1, 页码: 54-64
Authors:  Xue XP;  Nishiyama Y;  Nakamura Y;  Mori K;  Wang YP(汪运鹏);  Wen CY
Adobe PDF(2278Kb)  |  Favorite  |  View/Download：218/70  |  Submit date：2018/10/30
Compressible flow  Shock/shock interaction  Two-body configurations  Unsteady flow  Wake/shock interaction