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A computational method for the load spectra of large-scale structures with a data-driven learning algorithm 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2023, 卷号: 66, 期号: 1, 页码: 141-154
作者:  Chen XJ(陈贤佳);  Yuan, Zheng;  Li, Qiang;  Sun, ShouGuang;  Wei YJ(魏宇杰)
Adobe PDF(2512Kb)  |  收藏  |  浏览/下载：257/80  |  提交时间：2023/02/09
load spectrum  computational mechanics  deep learning  data-driven modeling  gated recurrent unit neural network  
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：237/38  |  提交时间：2022/03/05
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  
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：322/169  |  提交时间：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
On the ideal weights for WENO/WENO-like finite difference schemes for the first derivative, I 期刊论文
INTERNATIONAL JOURNAL OF MODERN PHYSICS C, 2020, 卷号: 31, 期号: 7, 页码: 12
作者:  Kang J(康健);  Li XL(李新亮)
Adobe PDF(584Kb)  |  收藏  |  浏览/下载：179/48  |  提交时间：2020/09/07
Finite difference  weighted essentially non-oscillatory  ideal weights  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