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Prediction of Transition Locations in Regions of the Minor Axis of Hypersonic Elliptic Cones using the BiGlobal-eN Method 期刊论文
ADVANCES IN APPLIED MATHEMATICS AND MECHANICS, 2024, 页码: 28
作者:  Zhao, Lei;  Zhou, Wenqiang;  Li XL(李新亮);  Zhang, Shaolong;  Zhang, Yongming
收藏  |  浏览/下载：33/0  |  提交时间：2024/02/19
BiGlobal stability  transition  boundary layer  hypersonic elliptic cone  minor axis.  
Experimental study on the evolution of mode waves in laminar boundary layer on a large-scale flat plate 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 1, 页码: 16
作者:  Liu MK(刘美宽);  Han GL(韩桂来);  Jiang ZL(姜宗林)
Adobe PDF(5472Kb)  |  收藏  |  浏览/下载：240/39  |  提交时间：2022/03/05
Statistical characteristics of turbulent mixing in spherical and cylindrical converging Richtmyer-Meshkov instabilities 期刊论文
JOURNAL OF FLUID MECHANICS, 2021, 卷号: 928, 页码: 32
作者:  Li XL(李新亮);  Fu YW(符耀威);  Yu ZP(于长平);  Li, Li
Adobe PDF(1452Kb)  |  收藏  |  浏览/下载：222/39  |  提交时间：2022/01/12
compressible turbulence  shock waves  turbulent mixing  
Theoretical, numerical and experimental study of hypersonic boundary layer transition: Blunt circular cone 期刊论文
APPLIED THERMAL ENGINEERING, 2021, 卷号: 194, 页码: 14
作者:  Chen, Jianqiang;  Yi, Shihe;  Li XL(李新亮);  Han GL(韩桂来);  Zhang, Yifeng;  Yang, Qiang;  Yuan, Xianxu
Adobe PDF(11175Kb)  |  收藏  |  浏览/下载：325/91  |  提交时间：2021/08/03
Hypersonic boundary layer  Stability  Transition  Thermal protection  
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
作者:  Tong FL(童福林);  Sun D(孙栋);  Li XL(李新亮)
Adobe PDF(4402Kb)  |  收藏  |  浏览/下载：198/45  |  提交时间：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
作者:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  收藏  |  浏览/下载：327/169  |  提交时间：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Incident shock wave and supersonic turbulent boundarylayer interactions near an expansion corner 期刊论文
COMPUTERS & FLUIDS, 2020, 卷号: 198, 页码: 18
作者:  Tong FL(童福林);  Li XL(李新亮);  Yuan XX;  Yu ZP(于长平)
浏览  |  Adobe PDF(7909Kb)  |  收藏  |  浏览/下载：356/113  |  提交时间：2020/04/07
Shock wave  Turbulent boundary layer  Unsteadiness  Expansion corner