Abstract

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.

Highlights

  • We are concerned with approximating incompressible wall-bounded flows including several examples of channel flow and wall boundary layers, as sketched in figure 1

  • At high Reynolds number, the flow over a flat plate is accurately described by the boundary layer approximation

  • While there is no first-principles theory that leads to the turbulent boundary layer velocity profile, the wall-wake formulation introduced by Coles (1956) in his landmark paper provides a very good correlation that accurately reflects the relative balance between viscous and turbulent stresses across most of the layer and can be used to compare flows at different Reynolds numbers

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Summary

Introduction

We are concerned with approximating incompressible wall-bounded flows including several examples of channel flow and wall boundary layers, as sketched in figure 1 These flows are governed by the two-dimensional, stationary, Reynolds-averaged Navier–Stokes (RANS) equations (1.1a,b):. The average effect of this balance of viscous and convective stresses is to produce a well-defined wall layer with a very steep mean velocity gradient at the wall over a length scale comparable to the scale of the eddies just described. Viscous stresses become small and momentum transport is dominated by turbulent eddying motions over a length scale comparable to the thickness of the boundary layer. The velocity variation over this outer wake layer scales with the aptly named defect velocity (ue − uτ )

The wall-wake formulation
The universal velocity profile
The universal velocity profile shape function
Channel flow
The adverse pressure gradient boundary layer
Findings
Conclusions
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