CFD Analysis of a SD 7003 Airfoil with a Local Correlation Based Transition and Turbulence Model
CFD Analysis of a SD 7003 Airfoil with a Local Correlation Based Transition and Turbulence Model
The SD 7003 has been investigated quite extensively in the past at different Reynolds numbers. At moderate Reynolds numbers and low angles of attack its upper surface is dominated by a large laminar separation bubble which provides a demanding test case for RANS-based transition models. In this article, a widely used open-source Computational Fluid Dynamics (CFD) toolbox has been used mainly to investigate the (i) aerodynamics coefficients and (ii) boundary layer transitional behaviors of a SD 7003 airfoil using a local correlation-based γ - Reθt SST [1] transition and turbulence model. Several researchers have proposed different correlations which can be used in the γ - Reθt SST. In this article, five such correlations have been investigated for the SD 7003 at low Reynolds number which is particularly challenging for CFD analysis.
Islam, Mazharul
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Langfeldt, Felix
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Fürst, Jiří
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Wood, David H.
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3 April 2017
Islam, Mazharul
c8fc8371-fd66-42e5-917c-b35f32dd29c9
Langfeldt, Felix
2bf86877-f2cd-4c35-be0f-e38a718a915c
Fürst, Jiří
cbaee291-20c9-465d-bcf2-a106b9ae325e
Wood, David H.
01e8a94b-abc8-4661-ae85-3024e4d15131
Islam, Mazharul, Langfeldt, Felix, Fürst, Jiří and Wood, David H.
(2017)
CFD Analysis of a SD 7003 Airfoil with a Local Correlation Based Transition and Turbulence Model.
IOP Conference Series: Materials Science and Engineering, 184, [012067].
(doi:10.1088/1757-899X/184/1/012067).
Abstract
The SD 7003 has been investigated quite extensively in the past at different Reynolds numbers. At moderate Reynolds numbers and low angles of attack its upper surface is dominated by a large laminar separation bubble which provides a demanding test case for RANS-based transition models. In this article, a widely used open-source Computational Fluid Dynamics (CFD) toolbox has been used mainly to investigate the (i) aerodynamics coefficients and (ii) boundary layer transitional behaviors of a SD 7003 airfoil using a local correlation-based γ - Reθt SST [1] transition and turbulence model. Several researchers have proposed different correlations which can be used in the γ - Reθt SST. In this article, five such correlations have been investigated for the SD 7003 at low Reynolds number which is particularly challenging for CFD analysis.
Text
Islam_2017_IOP_Conf._Ser.__Mater._Sci._Eng._184_012067
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Published date: 3 April 2017
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© Published under licence by IOP Publishing Ltd.
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Copyright 2017 Elsevier B.V., All rights reserved.
Venue - Dates:
3rd International Conference on Mechanical, Automotive and Aerospace Engineering, ICMAAE 2016, , Kuala Lumpur, Malaysia, 2016-07-25 - 2016-07-27
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Local EPrints ID: 455134
URI: http://eprints.soton.ac.uk/id/eprint/455134
ISSN: 1757-8981
PURE UUID: a3bfeaba-0113-456b-bf6b-768ed31aa2df
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Date deposited: 10 Mar 2022 17:51
Last modified: 06 Jun 2024 02:12
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Author:
Mazharul Islam
Author:
Jiří Fürst
Author:
David H. Wood
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