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Wall-modeled large-eddy simulation of the flow past a rod-airfoil tandem by the Lattice Boltzmann method

Emmanuel Leveque (LMFA – Laboratoire de Mécanique des Fluides et d’Acoustique, CNRS, Ecole Centrale de Lyon, Ecully, France)
Hatem Touil (BU AESI, C-S Systèmes d’Information, Lyon, France)
Satish Malik (LMFA – Laboratoire de Mécanique des Fluides et d’Acoustique, CNRS, Ecole Centrale de Lyon, Ecully, France)
Denis Ricot (Renault CAE Division, Guyancourt, France)
Alois Sengissen (Department of Acoustics and Environment, Airbus Operations SAS, Toulouse, France)

International Journal of Numerical Methods for Heat & Fluid Flow

ISSN: 0961-5539

Article publication date: 8 May 2018

222

Abstract

Purpose

The Lattice Boltzmann (LB) method offers an alternative to conventional computational fluid dynamics (CFD) methods. However, its practical use for complex turbulent flows of engineering interest is still at an early stage. This paper aims to outline an LB wall-modeled large-eddy simulation (WMLES) solver.

Design/methodology/approach

The solver is dedicated to complex high-Reynolds flows in the context of WMLES. It relies on an improved LB scheme and can handle complex geometries on multi-resolution block structured grids.

Findings

Dynamic and acoustic characteristics of a turbulent airflow past a rod-airfoil tandem are examined to test the capabilities of this solver. Detailed direct comparisons are made with both experimental and numerical reference data.

Originality/value

This study allows assessing the potential of an LB approach for industrial CFD applications.

Keywords

Acknowledgements

LB simulations have been performed on the local HPC facilities at Ecole Centrale de Lyon (PMCS2I) and Ecole Normale Supérieure de Lyon (PSMN). These HPC facilities are supported by their academic host institutions, the Auvergne-Rhône-Alpes region (GRANT CPRT07-13 CIRA) and the national Equip@Meso grant (ANR-10-EQPX-29-01). The research work has been financially supported by the French Ministry of Industry and Bpifrance in the framework of the “Programme d’Investissement d’Avenir: Calcul Intensif et Simulation Numérique.” F. Chevillotte and F.-X. Bécot (Matelys research Lab) have helped for the development of dynamic sponge zones in the LaBS solver. We thank Basile Bazin (CS-SI) for his help in the mesh setting.

Citation

Leveque, E., Touil, H., Malik, S., Ricot, D. and Sengissen, A. (2018), "Wall-modeled large-eddy simulation of the flow past a rod-airfoil tandem by the Lattice Boltzmann method", International Journal of Numerical Methods for Heat & Fluid Flow, Vol. 28 No. 5, pp. 1096-1116. https://doi.org/10.1108/HFF-06-2017-0258

Publisher

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Emerald Publishing Limited

Copyright © 2018, Emerald Publishing Limited

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