IMECH-IR

Browse/Search Results:  1-4 of 4 Help

Filters                                
Selected(0)Clear Items/Page:    Sort:
Direct numerical simulation of hypersonic boundary layer transition over a lifting-body model HyTRV 期刊论文
Advances in Aerodynamics, 2021, 卷号: 3, 期号: 1
Authors:  Qi H(齐涵);  Li XL(李新亮);  Yu ZP(于长平);  Tong FL(童福林)
Adobe PDF(4454Kb)  |  Favorite  |  View/Download:286/40  |  Submit date:2021/11/01
Lifting body model  Hypersonic transition  Direct numerical simulation  
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
Authors:  Tong FL(童福林);  Li XL(李新亮);  Yuan XX;  Yu ZP(于长平)
Adobe PDF(7909Kb)  |  Favorite  |  View/Download:371/120  |  Submit date:2020/04/07
Shock wave  Turbulent boundary layer  Unsteadiness  Expansion corner  
高超声速激波湍流边界层干扰直接数值模拟研究 期刊论文
力学学报, 2018, 卷号: 50, 期号: 2, 页码: 197-208
Authors:  童福林;  李欣;  于长平;  李新亮
Adobe PDF(1011Kb)  |  Favorite  |  View/Download:400/123  |  Submit date:2018/10/24
高超声速  激波湍流边界层干扰  直接数值模拟  湍动能  低频振荡  
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.
Adobe PDF(6937Kb)  |  Favorite  |  View/Download:465/165  |  Submit date:2017/10/27
Compression Corner  Low-frequency Oscillation  Coherent Vortex Structure  Power Spectrum  Turbulent Kinetic Energy Budget  Direct Numerical Simulation