Velocity transformation for compressible wall-bounded turbulent flows with and without heat transfer

被引:106
作者
Griffin, Kevin Patrick [1 ]
Fu, Lin [1 ,2 ,3 ]
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
关键词
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.
引用
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页数:7
相关论文
共 23 条
[1]  
Carvin C., 1988, AIAA Paper No. 88-0136
[2]   A numerical study of turbulent supersonic isothermal-wall channel flow [J].
Coleman, GN ;
Kim, J ;
Moser, RD .
JOURNAL OF FLUID MECHANICS, 1995, 305 :159-183
[3]   Shock-induced heating and transition to turbulence in a hypersonic boundary layer [J].
Fu, Lin ;
Karp, Michael ;
Bose, Sanjeeb T. ;
Moin, Parviz ;
Urzay, Javier .
JOURNAL OF FLUID MECHANICS, 2021, 909 (909)
[4]   General method for determining the boundary layer thickness in nonequilibrium flows [J].
Griffin, Kevin Patrick ;
Fu, Lin ;
Moin, Parviz .
PHYSICAL REVIEW FLUIDS, 2021, 6 (02)
[5]   Compressible turbulent channel flows: DNS results and modelling [J].
Huang, PG ;
Coleman, GN ;
Bradshaw, P .
JOURNAL OF FLUID MECHANICS, 1995, 305 :185-218
[6]   VANDRIEST TRANSFORMATION AND COMPRESSIBLE WALL-BOUNDED FLOWS [J].
HUANG, PG ;
COLEMAN, GN .
AIAA JOURNAL, 1994, 32 (10) :2110-2113
[7]   Analysis of the equilibrium wall model for high-speed turbulent flows [J].
Iyer, Prahladh S. ;
Malik, Mujeeb R. .
PHYSICAL REVIEW FLUIDS, 2019, 4 (07)
[8]   Direct numerical simulation of turbulent channel flow up to Reτ ≈ 5200 [J].
Lee, Myoungkyu ;
Moser, Robert D. .
JOURNAL OF FLUID MECHANICS, 2015, 774 :395-415
[9]   Direct numerical simulation of supersonic pipe flow at moderate Reynolds number [J].
Modesti, Davide ;
Pirozzoli, Sergio .
INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2019, 76 :100-112
[10]   Reynolds and Mach number effects in compressible turbulent channel flow [J].
Modesti, Davide ;
Pirozzoli, Sergio .
INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2016, 59 :33-49