Abstract

The predictive accuracy of wall-modelled LES is influenced by a combination of the subgrid model, the wall model, the numerical dissipation induced primarily by the convective numerical scheme, and also by the density and topology of the computational grid. The latter factor is of particular importance for industrial flow problems, where unstructured grids are typically employed due to the necessity to handle complex geometries. Here, a systematic simulation-based study is presented, investigating the effect of grid-cell type on the predictive accuracy of wall-modelled LES in the framework of a general-purpose finite-volume solver. Following standard practice for meshing near-wall regions, it is proposed to use prismatic cells. Three candidate shapes for the base of the prisms are considered: a triangle, a quadrilateral, and an arbitrary polygon. The cell-centre distance is proposed as a metric to determine the spatial resolution of grids with different cell types. The simulation campaign covers two test cases with attached boundary layers: fully-developed turbulent channel flow, and a zero-pressure-gradient flat-plate turbulent boundary layer. A grid construction strategy is employed, which adapts the grid metric to the outer length scale of the boundary layer. The results are compared with DNS data concerning mean wall shear stress and profiles of flow statistics. The principle outcome is that unstructured simulations may provide the same accuracy as simulations on structured orthogonal hexahedral grids. The choice of base shape of the near-wall cells has a significant impact on the computational cost, but in terms of accuracy appears to be a factor of secondary importance.

Highlights

  • The majority of the computational fluid dynamics (CFD) solvers used for tackling flow problems occurring in applications are based on finite volume discretization of the governing equations

  • For the majority of the quantities of interest, the obtained profiles will be presented in terms of the relative error, in percent, with respect to the reference direct numerical simulation (DNS)

  • Since the size of WMLES cells are quite large at low δ/d, the reference value at each cell centre is obtained by averaging the DNS profile across the wall-normal extent of the corresponding cell

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Summary

Introduction

The majority of the computational fluid dynamics (CFD) solvers used for tackling flow problems occurring in applications are based on finite volume discretization of the governing equations. Scale-resolving turbulence modelling approaches, such as direct numerical simulation (DNS) and large-eddy simulation (LES), have until recently mainly been used in academic studies of canonical flows The domains of such flows are well-suited for discretization with a high-quality structured grid. Based on analysis of integral length scales, it is typically recommended that in the TBL the spanwise resolution should be about twice as high as the streamwise Such a recommendation can be quite difficult to follow for a flow where the direction of the stream is subject to change, and for certain cell shapes may lead to deterioration of quality.

Unstructured grid generation
Grid resolution metrics
Boundary layer meshing algorithm
Selection of surface meshing algorithms
Computational fluid dynamics methods
Numerical experiments
Fully developed turbulent channel flow
Flat-plate turbulent boundary layer
Conclusions
Declaration of Competing Interest
Full Text
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