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Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 5, 页码: 350-363
Authors:  Tong FL(童福林);  Sun D(孙栋);  Li XL(李新亮)
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Direct numerical simulation  Low-frequency unsteadiness  Shock waves  Turbulent boundary layer  Wavy-wall  
Subgrid-scale model based on the vorticity gradient tensor for rotating turbulent flows 期刊论文
ACTA MECHANICA SINICA, 2020, 页码: 9
Authors:  Qi H(齐涵);  Li XL(李新亮);  Yu ZP(于长平)
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Large-eddy simulation  Subgrid-scale model  Rotating turbulent channel flow  
超声速膨胀角入射激波/湍流边界层干扰直接数值模拟研究 期刊论文
航空学报, 2019, 页码: 21
Authors:  童福林;  孙东;  袁先旭;  李新亮
View  |  Adobe PDF(1603Kb)  |  Favorite  |  View/Download：201/69  |  Submit date：2019/12/16
激波/湍流边界层干扰  膨胀角  本征正交分解  直接数值模拟  
Effects of dimensional wall temperature on velocity-temperature correlations in supersonic turbulent channel flow of thermally perfect gas 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2019, 卷号: 62, 期号: 6, 页码: AR64711
Authors:  Chen XP;  Li XL(李新亮);  Zhu ZC
View  |  Adobe PDF(1844Kb)  |  Favorite  |  View/Download：322/101  |  Submit date：2019/04/11
direct numerical simulation  velocity-temperature correlation  supersonic flow  channel flow  thermally perfect gas  strong Reynolds analogy  
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
View  |  Adobe PDF(1011Kb)  |  Favorite  |  View/Download：396/120  |  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  
分辨率优化的混合WENO格式 期刊论文
计算物理, 2017, 卷号: 35, 期号: 4, 页码: 397-404
Authors:  郭元;  田奇;  梁贤;  李新亮
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混合格式  数值耗散  色散  保单调  优化  
Effect of uniform blowing or suction on hypersonic spatially developing turbulent boundary layers 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2016, 卷号: 59, 期号: 6, 页码: 664702
Authors:  Chen Z(陈哲);  Yu ZP(于长平);  Li L(李理);  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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转捩对压缩拐角激波/边界层干扰分离泡的影响 期刊论文
航空学报, 2016, 卷号: 37, 期号: 10, 页码: 2909-2921
Authors:  童福林;  李新亮;  唐志共;  朱兴坤;  黄江涛
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Transition  Compression Ramp  Shock Wave/boundary Layer Interaction  Separation Bubble  Direct Numerical Simulation  
比熵增概念及其在湍流模型中的应用 期刊论文
空气动力学学报, 2013, 卷号: 31, 期号: 3, 页码: 381-387
Authors:  赵瑞;  阎超;  李新亮;  蒋海军
Adobe PDF(705Kb)  |  Favorite  |  View/Download：864/233  |  Submit date：2013/10/11
熵  比熵增  Badwin-lomax湍流模型  计算流体力学  
Improvement of Baldwin-Lomax turbulence model for supersonic complex flows 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2013, 卷号: 26, 期号: 3, 页码: 529–534
Authors:  Zhao R(赵瑞);  Yan C(阎超);  Yu J(于剑);  Li XL(李新亮);  Yan, C (reprint author), Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China.
Adobe PDF(1609Kb)  |  Favorite  |  View/Download：884/289  |  Submit date：2013/09/21
Baldwin-lomax Model  Boundary Layers  Computational Aerodynamics  Entropy  Supersonic Flows  Turbulence Models