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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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Date Issued:2017
Author:李新亮
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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.
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View/Download:470/166
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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 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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View/Download:594/184
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Submit date:2017/04/26