Turbulent heat transfer enhancement in a triangular duct using delta-winglet vortex generators

The augmentation of convective heat transfer of a turbulent flow using delta-winglet vortex generators (VG) in a triangular duct was experimentally investigated. Two side walls of the heated test section are electrically heated with a constant heat flux while the lower wall is indirectly heated. Sin...

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Main Authors: Althaher M.A., Abdul-Rassol A.A., Ahmed H.E., Mohammed H.A.
Other Authors: 54789484000
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Published: 2023
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Institution: Universiti Tenaga Nasional
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spelling my.uniten.dspace-304192023-12-29T15:47:38Z Turbulent heat transfer enhancement in a triangular duct using delta-winglet vortex generators Althaher M.A. Abdul-Rassol A.A. Ahmed H.E. Mohammed H.A. 54789484000 45861008800 54789424300 15837504600 Delta-winglet Heat transfer enhancement Triangular duct Turbulent flow Vortex generator Angle of attack Ducts Friction Heat convection Heat flux Heat transfer coefficients Nusselt number Reynolds number Transport aircraft Tribology Turbulent flow Constant heat flux Convective heat transfer Correlation equation Delta-winglet Friction factors Heat transfer enhancement Inclination angles Leading edge Side walls Test sections Turbulent heat transfer Vortex generators Vortex flow The augmentation of convective heat transfer of a turbulent flow using delta-winglet vortex generators (VG) in a triangular duct was experimentally investigated. Two side walls of the heated test section are electrically heated with a constant heat flux while the lower wall is indirectly heated. Single, double, and triple pairs of VG are utilized. Each pair of VG was punched on one wall of the test duct. The effects of the number of VG pairs, the VG angle of attack, the VG location from the leading edge of the test duct, the VG geometry, and Reynolds number are examined in this paper. The results indicate that the Nusselt number and friction factor are relatively proportional to the size, number, and the inclination angle of the VG. The Nusselt number increases and the friction factor decreases as the Reynolds number increases. The present results were compared with the available literature and they show good agreement. Correlation equations of Nusselt number and friction factor for turbulent flow are developed, for the cases studied, as a function of Reynolds number and VG angle of attack. � 2011 Wiley Periodicals, Inc. Final 2023-12-29T07:47:38Z 2023-12-29T07:47:38Z 2012 Article 10.1002/htj.20382 2-s2.0-84155189156 https://www.scopus.com/inward/record.uri?eid=2-s2.0-84155189156&doi=10.1002%2fhtj.20382&partnerID=40&md5=4503f38cadf445f30435252d5efb77ed https://irepository.uniten.edu.my/handle/123456789/30419 41 1 43 62 Scopus
institution Universiti Tenaga Nasional
building UNITEN Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Tenaga Nasional
content_source UNITEN Institutional Repository
url_provider http://dspace.uniten.edu.my/
topic Delta-winglet
Heat transfer enhancement
Triangular duct
Turbulent flow
Vortex generator
Angle of attack
Ducts
Friction
Heat convection
Heat flux
Heat transfer coefficients
Nusselt number
Reynolds number
Transport aircraft
Tribology
Turbulent flow
Constant heat flux
Convective heat transfer
Correlation equation
Delta-winglet
Friction factors
Heat transfer enhancement
Inclination angles
Leading edge
Side walls
Test sections
Turbulent heat transfer
Vortex generators
Vortex flow
spellingShingle Delta-winglet
Heat transfer enhancement
Triangular duct
Turbulent flow
Vortex generator
Angle of attack
Ducts
Friction
Heat convection
Heat flux
Heat transfer coefficients
Nusselt number
Reynolds number
Transport aircraft
Tribology
Turbulent flow
Constant heat flux
Convective heat transfer
Correlation equation
Delta-winglet
Friction factors
Heat transfer enhancement
Inclination angles
Leading edge
Side walls
Test sections
Turbulent heat transfer
Vortex generators
Vortex flow
Althaher M.A.
Abdul-Rassol A.A.
Ahmed H.E.
Mohammed H.A.
Turbulent heat transfer enhancement in a triangular duct using delta-winglet vortex generators
description The augmentation of convective heat transfer of a turbulent flow using delta-winglet vortex generators (VG) in a triangular duct was experimentally investigated. Two side walls of the heated test section are electrically heated with a constant heat flux while the lower wall is indirectly heated. Single, double, and triple pairs of VG are utilized. Each pair of VG was punched on one wall of the test duct. The effects of the number of VG pairs, the VG angle of attack, the VG location from the leading edge of the test duct, the VG geometry, and Reynolds number are examined in this paper. The results indicate that the Nusselt number and friction factor are relatively proportional to the size, number, and the inclination angle of the VG. The Nusselt number increases and the friction factor decreases as the Reynolds number increases. The present results were compared with the available literature and they show good agreement. Correlation equations of Nusselt number and friction factor for turbulent flow are developed, for the cases studied, as a function of Reynolds number and VG angle of attack. � 2011 Wiley Periodicals, Inc.
author2 54789484000
author_facet 54789484000
Althaher M.A.
Abdul-Rassol A.A.
Ahmed H.E.
Mohammed H.A.
format Article
author Althaher M.A.
Abdul-Rassol A.A.
Ahmed H.E.
Mohammed H.A.
author_sort Althaher M.A.
title Turbulent heat transfer enhancement in a triangular duct using delta-winglet vortex generators
title_short Turbulent heat transfer enhancement in a triangular duct using delta-winglet vortex generators
title_full Turbulent heat transfer enhancement in a triangular duct using delta-winglet vortex generators
title_fullStr Turbulent heat transfer enhancement in a triangular duct using delta-winglet vortex generators
title_full_unstemmed Turbulent heat transfer enhancement in a triangular duct using delta-winglet vortex generators
title_sort turbulent heat transfer enhancement in a triangular duct using delta-winglet vortex generators
publishDate 2023
_version_ 1806426183872544768