Velocity transformation for compressible wall-bounded turbulent flows with and without heat transfer
被引:91
作者:
Griffin, Kevin Patrick
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机构:
Stanford Univ, Ctr Turbulence Res, Stanford, CA 94305 USAStanford Univ, Ctr Turbulence Res, Stanford, CA 94305 USA
Griffin, Kevin Patrick
[1
]
Fu, Lin
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机构:
Stanford Univ, Ctr Turbulence Res, Stanford, CA 94305 USA
Hong Kong Univ Sci & Technol, Dept Mech & Aerosp Engn, Kowloon, Hong Kong, Peoples R China
Hong Kong Univ Sci & Technol, Dept Math, Kowloon, Hong Kong, Peoples R ChinaStanford Univ, Ctr Turbulence Res, Stanford, CA 94305 USA
Fu, Lin
[1
,2
,3
]
Moin, Parviz
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机构:
Stanford Univ, Ctr Turbulence Res, Stanford, CA 94305 USAStanford Univ, Ctr Turbulence Res, Stanford, CA 94305 USA
Moin, Parviz
[1
]
机构:
[1] Stanford Univ, Ctr Turbulence Res, Stanford, CA 94305 USA
[2] Hong Kong Univ Sci & Technol, Dept Mech & Aerosp Engn, Kowloon, Hong Kong, Peoples R China
[3] Hong Kong Univ Sci & Technol, Dept Math, Kowloon, Hong Kong, Peoples R China
turbulence;
wall modeling;
law of the wall;
mean velocity profile;
Mach invariance;
DIRECT NUMERICAL-SIMULATION;
REYNOLDS;
D O I:
10.1073/pnas.2111144118
中图分类号:
O [数理科学和化学];
P [天文学、地球科学];
Q [生物科学];
N [自然科学总论];
学科分类号:
07 ;
0710 ;
09 ;
摘要:
In this work, a transformation, which maps the mean velocity profiles of compressible wall-bounded turbulent flows to the incompressible law of the wall, is proposed. Unlike existing approaches, the proposed transformation successfully collapses, without specific tuning, numerical simulation data from fully developed channel and pipe flows, and boundary layers with or without heat transfer. In all these cases, the transformation is successful across the entire inner layer of the boundary layer (including the viscous sublayer, buffer layer, and logarithmic layer), recovers the asymptotically exact near-wall behavior in the viscous sublayer, and is consistent with the near balance of turbulence production and dissipation in the logarithmic region of the boundary layer. The performance of the transformation is verified for compressible wall-bounded flows with edge Mach numbers ranging from 0 to 15 and friction Reynolds numbers ranging from 200 to 2,000. Based on physical arguments, we show that such a general transformation exists for compressible wall-bounded turbulence regardless of the wall thermal condition.
机构:
Univ Roma La Sapienza, Dipartimento Ingn Meccan & Aerosp, Via Eudossiana 18, I-00184 Rome, ItalyUniv Roma La Sapienza, Dipartimento Ingn Meccan & Aerosp, Via Eudossiana 18, I-00184 Rome, Italy
Modesti, Davide
Pirozzoli, Sergio
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机构:
Univ Roma La Sapienza, Dipartimento Ingn Meccan & Aerosp, Via Eudossiana 18, I-00184 Rome, ItalyUniv Roma La Sapienza, Dipartimento Ingn Meccan & Aerosp, Via Eudossiana 18, I-00184 Rome, Italy
机构:
Univ Roma La Sapienza, Dipartimento Ingn Meccan & Aerosp, Via Eudossiana 18, I-00184 Rome, ItalyUniv Roma La Sapienza, Dipartimento Ingn Meccan & Aerosp, Via Eudossiana 18, I-00184 Rome, Italy
Modesti, Davide
Pirozzoli, Sergio
论文数: 0引用数: 0
h-index: 0
机构:
Univ Roma La Sapienza, Dipartimento Ingn Meccan & Aerosp, Via Eudossiana 18, I-00184 Rome, ItalyUniv Roma La Sapienza, Dipartimento Ingn Meccan & Aerosp, Via Eudossiana 18, I-00184 Rome, Italy