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dc.contributor.authorNadim, Nima
dc.contributor.authorChandratilleke, Tilak
dc.contributor.authorKrause, M.
dc.contributor.editorZhou Y
dc.contributor.editorLucey AD
dc.contributor.editorLiu Y
dc.contributor.editorHuang L
dc.date.accessioned2017-01-30T11:57:17Z
dc.date.available2017-01-30T11:57:17Z
dc.date.created2016-11-16T19:30:22Z
dc.date.issued2016
dc.identifier.citationNadim, 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.
dc.identifier.urihttp://hdl.handle.net/20.500.11937/16709
dc.identifier.doi10.1007/978-3-662-48868-3_33
dc.description.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.

dc.publisherSpringer Berlin Heidelberg
dc.titleLBM-LES modelling of low-Reynolds number turbulent flow over NACA0012 aerofoil
dc.typeBook Chapter
dcterms.source.startPage205
dcterms.source.endPage210
dcterms.source.titleFluid-Structure-Sound Interactions and Control: Proceedings of the 3rd Symposium on Fluid-Structure-Sound Interactions and Control
dcterms.source.isbn978-3-662-48866-9
dcterms.source.placeBerlin
dcterms.source.chapter70
curtin.departmentDepartment of Mechanical Engineering
curtin.accessStatusFulltext not available


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