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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:321/89  |  提交时间:2021/08/03
Hypersonic boundary layer  Stability  Transition  Thermal protection  
A Sufficient and Necessary Condition of the Existence of WENO-Like Linear Combination for Finite Difference Schemes 期刊论文
COMMUNICATIONS IN COMPUTATIONAL PHYSICS, 2021, 卷号: 29, 期号: 2, 页码: 534-570
作者:  Kang J(康健);  Li XL(李新亮)
Adobe PDF(403Kb)  |  收藏  |  浏览/下载:271/52  |  提交时间:2021/03/03
Finite difference  WENO  sufficient and necessary condition  proof  
Study on turbulence drag reduction of riblet plate in hypersonic turbulent flows 期刊论文
INTERNATIONAL JOURNAL OF MODERN PHYSICS C, 2020, 卷号: 31, 期号: 3, 页码: 11
作者:  Zhou H(周浩);  Li XL(李新亮);  Yu ZP(于长平)
Adobe PDF(3698Kb)  |  收藏  |  浏览/下载:265/84  |  提交时间:2020/05/18
Hypersonic  turbulence control  numerical simulation  riblet plate  
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:352/111  |  提交时间:2020/04/07
Shock wave  Turbulent boundary layer  Unsteadiness  Expansion corner