LBM-LES modelling of low-Reynolds number turbulent flow over NACA0012 aerofoil
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 owin...
| Main Authors: | , , |
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| Other Authors: | |
| Format: | Book Chapter |
| Published: |
Springer Berlin Heidelberg
2016
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| Online Access: | http://hdl.handle.net/20.500.11937/16709 |
| _version_ | 1848749253675974656 |
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| author | Nadim, Nima Chandratilleke, Tilak Krause, M. |
| author2 | Zhou Y |
| author_facet | Zhou Y Nadim, Nima Chandratilleke, Tilak Krause, M. |
| author_sort | Nadim, Nima |
| building | Curtin Institutional Repository |
| collection | Online Access |
| description | 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. |
| first_indexed | 2025-11-14T07:18:00Z |
| format | Book Chapter |
| id | curtin-20.500.11937-16709 |
| institution | Curtin University Malaysia |
| institution_category | Local University |
| last_indexed | 2025-11-14T07:18:00Z |
| publishDate | 2016 |
| publisher | Springer Berlin Heidelberg |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | curtin-20.500.11937-167092023-02-27T07:34:28Z LBM-LES modelling of low-Reynolds number turbulent flow over NACA0012 aerofoil Nadim, Nima Chandratilleke, Tilak Krause, M. Zhou Y Lucey AD Liu Y Huang L 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. 2016 Book Chapter http://hdl.handle.net/20.500.11937/16709 10.1007/978-3-662-48868-3_33 Springer Berlin Heidelberg restricted |
| spellingShingle | Nadim, Nima Chandratilleke, Tilak Krause, M. LBM-LES modelling of low-Reynolds number turbulent flow over NACA0012 aerofoil |
| title | LBM-LES modelling of low-Reynolds number turbulent flow over NACA0012 aerofoil |
| title_full | LBM-LES modelling of low-Reynolds number turbulent flow over NACA0012 aerofoil |
| title_fullStr | LBM-LES modelling of low-Reynolds number turbulent flow over NACA0012 aerofoil |
| title_full_unstemmed | LBM-LES modelling of low-Reynolds number turbulent flow over NACA0012 aerofoil |
| title_short | LBM-LES modelling of low-Reynolds number turbulent flow over NACA0012 aerofoil |
| title_sort | lbm-les modelling of low-reynolds number turbulent flow over naca0012 aerofoil |
| url | http://hdl.handle.net/20.500.11937/16709 |