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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
Authors:  Chen, Jianqiang;  Yi, Shihe;  Li XL(李新亮);  Han GL(韩桂来);  Zhang, Yifeng;  Yang, Qiang;  Yuan, Xianxu
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Hypersonic boundary layer  Stability  Transition  Thermal protection  
Direct numerical simulation of a supersonic turbulent boundary layer over a compression–decompression corner 期刊论文
Physics of Fluids, 2021, 卷号: 33, 页码: 065111
Authors:  段俊亦;  李欣;  李新亮;  刘洪伟
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Effect of wall temperature on the kinetic energy transfer in a hypersonic turbulent boundary layer 期刊论文
Journal of Fluid Mechanics, 2021, 卷号: 929, 页码: A33
Authors:  Xu DH(许得豪);  Wang JC(王健春);  Wan MP(万敏平);  Yu ZP(于长平);  Li XL(李新亮);  Chen SY(陈十一)
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Subgrid-scale model for large-eddy simulation of transition and turbulence in compressible flows 期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 12, 页码: 14
Authors:  Zhou H(周浩);  Li XL(李新亮);  Qi H(齐涵);  Yu ZP(于长平)
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Numerical studies of shock wave interactions with a supersonic turbulent boundary layer in compression corner:Turning angle effects 期刊论文
COMPUTERS & FLUIDS, 2017, 卷号: 149, 页码: 56-69
Authors:  Tong FL(童福林);  Yu ZP(于长平);  Tang ZG(唐志共);  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.;  Li, XL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
View  |  Adobe PDF(6937Kb)  |  Favorite  |  View/Download：476/168  |  Submit date：2017/10/27
Compression Corner  Low-frequency Oscillation  Coherent Vortex Structure  Power Spectrum  Turbulent Kinetic Energy Budget  Direct Numerical Simulation  
Direct Numerical Simulation on Mach Number and Wall Temperature Effects in the Turbulent Flows of Flat-Plate Boundary Layer 期刊论文
COMMUNICATIONS IN COMPUTATIONAL PHYSICS, 2015, 卷号: 17, 期号: 1, 页码: 189-212
Authors:  Liang X;  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Hypersonic  Directly Numerical Simulation  Compressibility Effects  Turbulent Boundary Layer  Strong Reynolds Analogy  
Acoustic Calculation for Supersonic Turbulent Boundary Layer Flow 期刊论文
Chinese Physics Letters, 2009, 卷号: 26, 期号: 9, 页码: 094701-1-4
Authors:  Li XL(李新亮);  Fu DX(傅德薰);  Ma YW(马延文);  Gao H(高慧)
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Direct Numerical-simulation  Sound