LBM-LES modelling of low-Reynolds number turbulent flow over NACA0012 aerofoil
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Authors
Nadim, Nima
Chandratilleke, Tilak
Krause, M.
Date
2016Type
Book Chapter
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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.
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
Department
Department of Mechanical Engineering
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