LBM-LES modelling of low-Reynolds number turbulent flow over NACA0012 aerofoil

Nadim, Nima; Chandratilleke, Tilak; Krause, M.

doi:10.1007/978-3-662-48868-3_33

Access Status

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Authors

Nadim, Nima

Chandratilleke, Tilak

Krause, M.

Date

2016

Type

Book Chapter

Metadata

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Citation

Nadim, N. and Chandratilleke, T. and Krause, M. 2016. LBM-LES modelling of low-Reynolds number turbulent flow over NACA0012 aerofoil. In Fluid-Structure-Sound Interactions and Control: Proceedings of the 3rd Symposium on Fluid-Structure-Sound Interactions and Control, ed. Zhou Y, Lucey AD, Liu Y, Huang L, 205-210. Berlin: Springer Berlin Heidelberg.

Source Title

Fluid-Structure-Sound Interactions and Control: Proceedings of the 3rd Symposium on Fluid-Structure-Sound Interactions and Control

DOI

10.1007/978-3-662-48868-3_33

ISBN

978-3-662-48866-9

School

Department of Mechanical Engineering

URI

http://hdl.handle.net/20.500.11937/16709

Collection

Curtin Research Publications

Abstract

Contemporary evolution of numerical methods in fluid dynamics includes a growing application of lattice Boltzmann modelling (LBM) for turbulent flows. Large eddy simulation, implemented on LBM framework, is established as a competent alternative for the finite volume turbulence modelling method owing to enhanced feasibility of parallelism and the transient nature of LBM equations. This work utilises a simple Smagorinsky SGS model to investigate fundamental characteristics of a turbulent flow over NACA0012 aerofoil for a range of low Reynolds number in a turbulent flow.