Analysis of an airfoil using a transition and turbulence model

In order to evaluate the performance of airfoils with computational fluid dynamics (CFD) tools, modelling of transitional region in the boundary layer is very critical. Currently, there are several classes of transition-based turbulence model which are based on different methods. Among these, the k-...

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Main Authors: Islam, Mazharul, Fürst, Jiri, Wood, David H., Ani, Farid Nasir
Format: Article
Language:English
Published: Trans Tech Publications Ltd 2016
Subjects:
Online Access:http://irep.iium.edu.my/56511/
http://irep.iium.edu.my/56511/1/16_AnalysisOfAnAirfoilUsingATransitionAndTurbulenceModel-MazharEtAl2016.pdf
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author Islam, Mazharul
Fürst, Jiri
Wood, David H.
Ani, Farid Nasir
author_facet Islam, Mazharul
Fürst, Jiri
Wood, David H.
Ani, Farid Nasir
author_sort Islam, Mazharul
building IIUM Repository
collection Online Access
description In order to evaluate the performance of airfoils with computational fluid dynamics (CFD) tools, modelling of transitional region in the boundary layer is very critical. Currently, there are several classes of transition-based turbulence model which are based on different methods. Among these, the k-kL- ω, which is a three equation turbulence model, is one of the prominent ones which is based on the concept of laminar kinetic energy. This model is phenomenological and has several advantageous features. Over the years, different researchers have attempted to modify the original version which was proposed by Walter and Cokljat in 2008 to enrich the modelling capability. In this article, a modified form of k-kL-ω transitional turbulence model has been used with the help of OpenFOAM for an investigative CFD analysis of a NACA 4-digit airfoil at range of angles of attack.
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spelling iium-565112017-04-19T02:10:54Z http://irep.iium.edu.my/56511/ Analysis of an airfoil using a transition and turbulence model Islam, Mazharul Fürst, Jiri Wood, David H. Ani, Farid Nasir TL500 Aeronautics In order to evaluate the performance of airfoils with computational fluid dynamics (CFD) tools, modelling of transitional region in the boundary layer is very critical. Currently, there are several classes of transition-based turbulence model which are based on different methods. Among these, the k-kL- ω, which is a three equation turbulence model, is one of the prominent ones which is based on the concept of laminar kinetic energy. This model is phenomenological and has several advantageous features. Over the years, different researchers have attempted to modify the original version which was proposed by Walter and Cokljat in 2008 to enrich the modelling capability. In this article, a modified form of k-kL-ω transitional turbulence model has been used with the help of OpenFOAM for an investigative CFD analysis of a NACA 4-digit airfoil at range of angles of attack. Trans Tech Publications Ltd 2016-01 Article PeerReviewed application/pdf en http://irep.iium.edu.my/56511/1/16_AnalysisOfAnAirfoilUsingATransitionAndTurbulenceModel-MazharEtAl2016.pdf Islam, Mazharul and Fürst, Jiri and Wood, David H. and Ani, Farid Nasir (2016) Analysis of an airfoil using a transition and turbulence model. Applied Mechanics and Materials, 819. pp. 356-360. ISSN 1662-7482 https://www.scientific.net/AMM.819.356 10.4028/www.scientific.net/AMM.819.356
spellingShingle TL500 Aeronautics
Islam, Mazharul
Fürst, Jiri
Wood, David H.
Ani, Farid Nasir
Analysis of an airfoil using a transition and turbulence model
title Analysis of an airfoil using a transition and turbulence model
title_full Analysis of an airfoil using a transition and turbulence model
title_fullStr Analysis of an airfoil using a transition and turbulence model
title_full_unstemmed Analysis of an airfoil using a transition and turbulence model
title_short Analysis of an airfoil using a transition and turbulence model
title_sort analysis of an airfoil using a transition and turbulence model
topic TL500 Aeronautics
url http://irep.iium.edu.my/56511/
http://irep.iium.edu.my/56511/
http://irep.iium.edu.my/56511/
http://irep.iium.edu.my/56511/1/16_AnalysisOfAnAirfoilUsingATransitionAndTurbulenceModel-MazharEtAl2016.pdf