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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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李新亮 [14]
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Indexed By:CSCD
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Decomposition of mean skin friction in incident shock wave/turbulent boundary layer interaction flows at Mach 2.25
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 9, 页码: 178-194
Authors:
Duan JY(段俊亦)
;
Tong FL(童福林)
;
Li XL(李新亮)
;
Liu HW(刘洪伟)
Adobe PDF(6039Kb)
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View/Download:131/10
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Submit date:2023/11/13
Compressible flow
Boundary layers
Direct numerical simulation
Shock waves
Skin friction
Turbulent flow
A new dynamic subgrid-scale model using artificial neural network for compressible flow
期刊论文
THEORETICAL AND APPLIED MECHANICS LETTERS, 2022, 卷号: 12, 期号: 4
Authors:
Qi H(齐涵)
;
Li XL(李新亮)
;
Luo, Ning
;
Yu ZP(于长平)
Adobe PDF(2851Kb)
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View/Download:67/17
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Submit date:2024/01/15
Subgrid-scale kinetic energy
Eddy-viscosity model
Compressible flow
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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View/Download:229/57
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Submit date:2021/06/07
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)
Adobe PDF(2084Kb)
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Submit date:2020/07/06
Large-eddy simulation
Subgrid-scale model
Rotating turbulent channel flow
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
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View/Download:330/102
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Submit date:2019/04/11
direct numerical simulation
velocity-temperature correlation
supersonic flow
channel flow
thermally perfect gas
strong Reynolds analogy
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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Submit date:2016/09/14
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
Direct Numerical Simulation of Chemical Non-equilibrium Turbulent Flow
期刊论文
Chinese Physics Letters, 2013, 卷号: 30, 期号: 6, 页码: 064702/1-064702/5
Authors:
Chen XP(陈小平)
;
Li XL(李新亮)
;
Li, XL (reprint author), Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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View/Download:877/379
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Submit date:2013/09/21
Channel Flows
Turbulent Flows
Non-equilibrium Turbulent Flow
Chemical Reactions
Direct Numerical Simulation
Direct Numerical Simulation of Shock/Turbulent Boundary Layer Interaction in a Supersonic Compression Ramp
期刊论文
SCIENCE CHINA: Physics, Mechanics & Astronomy, 2010, 卷号: 53, 期号: 9, 页码: 1651-1658
Authors:
Li XL(李新亮)
;
Fu DX(傅德薰)
;
Ma YW(马延文)
;
Liang X(梁贤)
;
Li XL(李新亮)
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Adobe PDF(951Kb)
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View/Download:1621/369
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Submit date:2010/10/25
compression Ramp
Shock/turbulent Boundary Layer Interaction
Direct Numerical Simulation
Shock Oscillation
Acoustic Calculation for Supersonic Turbulent Boundary Layer Flow
期刊论文
Chinese Physics Letters, 2009, 卷号: 26, 期号: 9, 页码: 094701-1-4
Authors:
Li XL(李新亮)
;
Fu DX(傅德薰)
;
Ma YW(马延文)
;
Gao H(高慧)
Adobe PDF(1149Kb)
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View/Download:1101/322
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Submit date:2010/03/07
Direct Numerical-simulation
Sound