Abstract

For the flow over curved surfaces, an extra wall-normal pressure gradient is imposed to the flow through excessive surface pressure, such that the flow turns in alignment with the surface. In turn, turbulent fluctuations are suppressed over the convex surface; whereas, they are enhanced over the concave. Recently, the direct numerical simulation (DNS) of turbulent channel flow experiencing a 60 degree circular bend shows highly complex flow phenomena. Particularly, the mean flow properties are directly related to the channel geometry; in the impulse response of the mean flow to the step change of streamline curvature, sudden changes in mean strain rate and extra rates of strain emerge. This mean flow process is prior to the response of the turbulence structures. Due to the large streamline curvature, the underlying turbulence lagging mechanism and the stress strain misalignment are difficult to model. For this, the new DNS data for the wall bounded flow with high streamline curvature and large integral length scales is used to explore RANS performance. For eddy-viscosity models, this leads to the Boussinesq approximation being questionable. Also, for a Reynolds-stress model (RSM) with closure approximations applicable to homogeneous turbulent flows that are nearly in equilibrium, the current case can result in substantial predictive error. This is because of, for example, the linear approximation for the rapid pressure–strain correlation. To help move towards better turbulence modelling, Reynolds-averaged Navier–Stokes (RANS) predictions are compared for the same flow configuration as the DNS, using some popular turbulent models. These models include the second-order closure with the stress-ω formulation, the standard k−ω and the Menter’s shear-stress transport (SST) models, the standard Spalart–Allmaras (S-A) model with and without the corresponding strain–vorticity correction. As expected, overall, the RSM provides closer predictions to the DNS data than the selected eddy-viscosity models, even though the predictive accuracy needs to be further improved. Potentially, a non-linear constitutive relation or second-order closure, incorporating a relaxation approximation for the lagging mechanism, may lead to a remedy for the current non-equilibrium flow. Moreover, all models would also benefit from sensitisation to the impact of the large integral length scales.

Highlights

  • Relative to flow over a flat surface, when experiencing curved boundaries, more complexity emerges from the turbulence structures

  • In this figure and the following, the full-line represents the Direct Numerical Simulation (DNS) data, the dash-dot line is for the laminar profile that gives the same wall shear for the upstream fully developed region, and the Reynolds-averaged Navier–Stokes (RANS) results are given by symbols (◦ the RSM, the k − ω SST, the k − ω standard, the S-A with the strain–vorticity correction, the S-A standard, and + the HYDRA S-A with the strain–vorticity correction)

  • The Reynolds-averaged Navier–Stokes simulations have been performed for a turbulent channel flow experiencing a 60 degree circular bend

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Summary

Introduction

Relative to flow over a flat surface, when experiencing curved boundaries, more complexity emerges from the turbulence structures. Depending on the shape of such a viscous surface, extra momentum is imposed to the flow through an excessive wall pressure distribution. In such a way, the flow is forced to turn in alignment with the solid boundary. The flow is forced to turn in alignment with the solid boundary This usually results in static pressure gradient and dynamic head variation. The shear layer structures are distorted due to extra strain rates. Efforts on this subject are reviewed by Bradshaw [1,2,3]

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