A universal velocity profile for turbulent wall flows including adverse pressure gradient boundary layers

被引:29
作者
Subrahmanyam, Matthew A. [1 ]
Cantwell, Brian J. [1 ]
Alonso, Juan J. [1 ]
机构
[1] Stanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USA
关键词
turbulence modelling; turbulence theory; turbulent boundary layers; DIRECT NUMERICAL-SIMULATION; CHANNEL FLOW; WAKE MODEL; CODE;
D O I
10.1017/jfm.2021.998
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A recently developed mixing length model of the turbulent shear stress in pipe flow is used to solve the streamwise momentum equation for fully developed channel flow. The solution for the velocity profile takes the form of an integral that is uniformly valid from the wall to the channel centreline at all Reynolds numbers from zero to infinity. The universal velocity profile accurately approximates channel flow direct numerical simulation (DNS) data taken from several sources. The universal velocity profile also provides a remarkably accurate fit to simulated and experimental flat plate turbulent boundary layer data including zero and adverse pressure gradient data. The mixing length model has five free parameters that are selected through an optimization process to provide an accurate fit to data in the range R-tau = 550 to R-tau = 17 207. Because the velocity profile is directly related to the Reynolds shear stress, certain statistical properties of the flow can be studied such as turbulent kinetic energy production. The examples presented here include numerically simulated channel flow data from R-tau = 550 to R-tau = 8016, zero pressure gradient (ZPG) boundary layer simulations from R-tau = 1343 to R-tau = 2571, zero pressure gradient turbulent boundary layer experimental data between R-tau = 2109 and R-tau = 17 207, and adverse pressure gradient boundary layer data in the range R-tau = 912 to R-tau = 3587. An important finding is that the model parameters that characterize the near-wall flow do not depend on the pressure gradient. It is suggested that the new velocity profile provides a useful replacement for the classical wall-wake formulation.
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页数:31
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共 40 条
[1]   Spanwise velocity statistics in high-Reynolds-number turbulent boundary layers [J].
Baidya, R. ;
Philip, J. ;
Hutchins, N. ;
Monty, J. P. ;
Marusic, I. .
JOURNAL OF FLUID MECHANICS, 2021, 913 (913)
[2]   Distance-from-the-wall scaling of turbulent motions in wall-bounded flows [J].
Baidya, R. ;
Philip, J. ;
Hutchins, N. ;
Monty, J. P. ;
Marusic, I. .
PHYSICS OF FLUIDS, 2017, 29 (02)
[3]   Velocity statistics in turbulent channel flow up to Reτ=4000 [J].
Bernardini, Matteo ;
Pirozzoli, Sergio ;
Orlandi, Paolo .
JOURNAL OF FLUID MECHANICS, 2014, 742 :171-191
[4]   A code for direct numerical simulation of turbulent boundary layers at high Reynolds numbers in BG/P supercomputers [J].
Borrell, Guillem ;
Sillero, Juan A. ;
Jimenez, Javier .
COMPUTERS & FLUIDS, 2013, 80 :37-43
[5]   AN EXPERIMENTAL-STUDY OF ENTRAINMENT AND TRANSPORT IN THE TURBULENT NEAR WAKE OF A CIRCULAR-CYLINDER [J].
CANTWELL, B ;
COLES, D .
JOURNAL OF FLUID MECHANICS, 1983, 136 (NOV) :321-374
[6]   Integral measures of the zero pressure gradient boundary layer over the Reynolds number range 0 ≤ Rτ < ∞ [J].
Cantwell, Brian J. .
PHYSICS OF FLUIDS, 2021, 33 (08)
[7]   A universal velocity profile for smooth wall pipe flow [J].
Cantwell, Brian J. .
JOURNAL OF FLUID MECHANICS, 2019, 878 :834-874
[8]   Criteria for assessing experiments in zero pressure gradient boundary layers [J].
Chauhan, Kapil A. ;
Monkewitz, Peter A. ;
Nagib, Hassan M. .
FLUID DYNAMICS RESEARCH, 2009, 41 (02)
[9]   Reynolds number scaling of the peak turbulence intensity in wall flows [J].
Chen, Xi ;
Sreenivasan, Katepalli R. .
JOURNAL OF FLUID MECHANICS, 2021, 908
[10]   Quantifying wall turbulence via a symmetry approach. Part 2. Reynolds stresses [J].
Chen, Xi ;
Hussain, Fazle ;
She, Zhen-Su .
JOURNAL OF FLUID MECHANICS, 2018, 850 :401-438