IMECH-IR

Browse/Search Results:  1-10 of 236 Help

Selected(0)Clear Items/Page:    Sort:
A new high-order RKDG method based on the TENO-THINC scheme for shock-capturing 期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2025, 卷号: 520, 页码: 20./通讯作者:Fu, Lin
Authors:  Huang, Haohan;  Li XL(李新亮);  Fu, Lin
Favorite  |  View/Download:18/0  |  Submit date:2024/11/14
PDEs  Runge-Kutta discontinuous Galerkin methods  TENO  WENO  Hyperbolic conservation laws  
Extremely high wall pressure events in shock wave and turbulent boundary layer interactions using DNS data 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2024, 卷号: 37, 期号: 11, 页码: 81-93./通讯作者:Tong FL
Authors:  Limei, Junjie;  Yuan, Xianxu;  Dong, Siwei;  Li XL(李新亮);  Tong FL(童福林)
Favorite  |  View/Download:6/0  |  Submit date:2024/12/02
Wall pressure fluctuations  Extreme pressure events  Shock wave  Turbulent boundary layer  Direct numerical simulation  
高超声速旋转钝锥边界层稳定性与转捩研究 期刊论文
中国科学:物理学 力学 天文学, 2024, 卷号: 54, 期号: 10, 页码: 34-49./通讯作者:于长平
Authors:  宋德培;  于长平;  李新亮
Adobe PDF(1187Kb)  |  Favorite  |  View/Download:97/41  |  Submit date:2024/10/18
高超声速  边界层转捩  直接数值模拟  钝锥  
Helicity transfer in compressible turbulent flows 期刊论文
PHYSICAL REVIEW FLUIDS, 2024, 卷号: 9, 期号: 9, 页码: 25./通讯作者:Wang, Lifeng, Yu, Changping
Authors:  Yan Z(闫政);  Wu, Junfeng;  Lei, Zhu;  Wang, Jianchun;  Wang, Lifeng;  Li XL(李新亮);  Yu ZP(于长平)
Favorite  |  View/Download:34/0  |  Submit date:2024/10/14
Effects of wall temperature on hypersonic shock wave/turbulent boundary layer interactions 期刊论文
JOURNAL OF FLUID MECHANICS, 2024, 卷号: 990, 页码: 35./通讯作者:Li, Xinliang
Authors:  Zhang J(张吉);  Guo TB(郭同彪);  Dang GL(党冠麟);  Li XL(李新亮)
Favorite  |  View/Download:70/0  |  Submit date:2024/09/18
hypersonic flow  shock waves  turbulent boundary layers  
Prediction of Transition Locations in Regions of the Minor Axis of Hypersonic Elliptic Cones Using the 期刊论文
ADVANCES IN APPLIED MATHEMATICS AND MECHANICS, 2024, 卷号: 16, 期号: 4, 页码: 805-832./通讯作者:Zhang, Yongming
Authors:  Zhao, Lei;  Zhou, Wenqiang;  Li XL(李新亮);  Zhang, Shaolong;  Zhang, Yongming
Favorite  |  View/Download:89/0  |  Submit date:2024/08/01
BiGlobal stability  transition  boundary layer  hypersonic elliptic cone  minor axis  
Investigations on the turbulent/non-turbulent interface in supersonic compressible plate turbulent boundary layer 期刊论文
JOURNAL OF FLUID MECHANICS, 2024, 卷号: 988, 页码: 32./通讯作者:Wang, Jinjun
Authors:  Su, Shuhuai;  Long, Yanguang;  Wang, Jinjun;  Li XL(李新亮)
Favorite  |  View/Download:40/0  |  Submit date:2024/06/27
turbulent boundary layers  compressible turbulence  compressible boundary layers  
Wall skin friction analysis in a hypersonic turbulent boundary layer over a compression ramp 期刊论文
JOURNAL OF FLUID MECHANICS, 2024, 卷号: 988, 页码: 32./通讯作者:Li, Xinliang
Authors:  Guo TB(郭同彪);  Zhang J(张继);  Zhu YH(朱艳华);  Li XL(李新亮)
Favorite  |  View/Download:52/0  |  Submit date:2024/06/27
hypersonic flow  shock waves  turbulent boundary layers  
压缩拐角强激波边界层干扰直接数值模拟研究 期刊论文
空天防御, 2024, 卷号: 7, 期号: 02, 页码: 29-35./通讯作者:李新亮
Authors:  郭同彪;  张吉;  李新亮
Adobe PDF(1519Kb)  |  Favorite  |  View/Download:66/21  |  Submit date:2024/07/05
激波/湍流边界层干扰  直接数值模拟  流动结构  流动分离  湍动能  
一种基于能流相似性的新型大涡模拟方法及装置 专利
发明专利. 一种基于能流相似性的新型大涡模拟方法及装置, 专利号: CN112131800B, 申请日期: 2020-07-20,
Inventors:  于长平;  齐涵;  李新亮
Adobe PDF(971Kb)  |  Favorite  |  View/Download:2/1  |  Submit date:2024/12/10