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李新亮 [9]
童福林 [6]
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Creator:李新亮
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Shock wave and turbulent boundary layer interaction in a double compression ramp
期刊论文
COMPUTERS & FLUIDS, 2021, 卷号: 229, 页码: 15
Authors:
Tong FL(童福林)
;
Duan JY(段俊亦)
;
Li XL(李新亮)
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Submit date:2021/11/01
Shock wave
Turbulent boundary layer
Double compression ramp
Direct numerical simulation
Characteristics of wall-shear stress fluctuations in shock wave and turbulent boundary layer interaction
期刊论文
JOURNAL OF TURBULENCE, 2021, 页码: 23
Authors:
Tong FL(童福林)
;
Duan JY(段俊亦)
;
Li XL(李新亮)
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Submit date:2021/11/01
Wall-shear stress
shock wave
turbulent boundary layers
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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Submit date:2021/06/07
Direct numerical simulation
Low-frequency unsteadiness
Shock waves
Turbulent boundary layer
Wavy-wall
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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Submit date:2021/11/23
Wall-shear stress fluctuations in a supersonic turbulent boundary layer over an expansion corner
期刊论文
JOURNAL OF TURBULENCE, 2020, 页码: 20
Authors:
Tong FL(童福林)
;
Chen JQ
;
Sun D
;
Li XL(李新亮)
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Submit date:2020/08/26
Wall-shear stress
expansion corner
supersonic turbulent boundary layer
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)
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Submit date:2020/04/07
Shock wave
Turbulent boundary layer
Unsteadiness
Expansion corner
Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp
会议论文
Meeting of the Institute-of-Non-Newtonian-Fluid-Mechanics (INNFM), Llanwddyn, WALES, 2017
Authors:
Tong FL(童福林)
;
Li XL(李新亮)
;
Duan, Yanhui
;
Yu ZP(于长平)
;
Yu, CP (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
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Submit date:2018/01/16
Concave Surface Curvature
Adverse Pressure-gradient
Large-eddy Simulation
Reynolds-number
Near-wall
Flows
Separation
Vortices
Models
Numerical Study on Wall Temperature Effects on Shock Wave/Turbulent Boundary-Layer Interaction
期刊论文
AIAA JOURNAL, 2017, 卷号: 55, 期号: 1, 页码: 131-140
Authors:
Zhu XK
;
Yu ZP(于长平)
;
Tong FL
;
Li XL(李新亮)
;
Li, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2017/04/26
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.
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Submit date:2013/09/21
Baldwin-lomax Model
Boundary Layers
Computational Aerodynamics
Entropy
Supersonic Flows
Turbulence Models