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Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp 期刊论文
PHYSICS OF FLUIDS, 2017, 卷号: 29, 期号: 12, 页码: 125101
Authors:  Tong FL(童福林);  Li XL(李新亮);  Duan YH;  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：460/164  |  Submit date：2017/10/27
Compression Corner  Low-frequency Oscillation  Coherent Vortex Structure  Power Spectrum  Turbulent Kinetic Energy Budget  Direct Numerical Simulation