Computational modelling of TRIANGULAR sub-boundary-layer vortex generators

Vortex generators (VGs) are used increasingly more by the wind turbine manufacture industry as flow control devices to improve rotor blade aerodynamic performance. The VG height is usually designed with equal thickness of the local boundary layer at the VG position. Nevertheless, these conventional...

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Main Authors: Fernandez-Gamiz Unai, Ruiz de Loizaga Jon, Errasti Iñigo, Boyano Ana, Zulueta Ekaitz, Lopez-Guede Jose Manuel
Format: Article
Language:English
Published: EDP Sciences 2020-01-01
Series:MATEC Web of Conferences
Online Access:https://www.matec-conferences.org/articles/matecconf/pdf/2020/03/matecconf_icome2017-2018_01054.pdf
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spelling doaj-eebf96aca9d545dfa8b2c3428acc4c252021-08-05T13:49:16ZengEDP SciencesMATEC Web of Conferences2261-236X2020-01-013070105410.1051/matecconf/202030701054matecconf_icome2017-2018_01054Computational modelling of TRIANGULAR sub-boundary-layer vortex generatorsFernandez-Gamiz UnaiRuiz de Loizaga JonErrasti IñigoBoyano AnaZulueta EkaitzLopez-Guede Jose ManuelVortex generators (VGs) are used increasingly more by the wind turbine manufacture industry as flow control devices to improve rotor blade aerodynamic performance. The VG height is usually designed with equal thickness of the local boundary layer at the VG position. Nevertheless, these conventional VGs may produce excess residual drag in some applications. The so-called sub boundary layer VGs can provide enough momentum transfer over a region several times their own height for effective flow-separation control with much lower drag. The main objective is to investigate how well the simulations can reproduce the physics of the flow of the primary vortex generated by a triangular VG mounted on a flat plate with negligible pressure gradient with the angle of attack of the vane to the oncoming flow β= 18. Three different device heights H= 5mm, H1= 6,25mm, H2= 4,16mm have been studied and compared both qualitatively and quantitatively. To that end, computational simulations have been carried out using RANS method and at Reynolds number Re = 2600 based on the boundary layer momentum thickness θ= 2.4 mm at the VG position. The computational results show good agreement with the experimental data available in AVATAR project.https://www.matec-conferences.org/articles/matecconf/pdf/2020/03/matecconf_icome2017-2018_01054.pdf
collection DOAJ
language English
format Article
sources DOAJ
author Fernandez-Gamiz Unai
Ruiz de Loizaga Jon
Errasti Iñigo
Boyano Ana
Zulueta Ekaitz
Lopez-Guede Jose Manuel
spellingShingle Fernandez-Gamiz Unai
Ruiz de Loizaga Jon
Errasti Iñigo
Boyano Ana
Zulueta Ekaitz
Lopez-Guede Jose Manuel
Computational modelling of TRIANGULAR sub-boundary-layer vortex generators
MATEC Web of Conferences
author_facet Fernandez-Gamiz Unai
Ruiz de Loizaga Jon
Errasti Iñigo
Boyano Ana
Zulueta Ekaitz
Lopez-Guede Jose Manuel
author_sort Fernandez-Gamiz Unai
title Computational modelling of TRIANGULAR sub-boundary-layer vortex generators
title_short Computational modelling of TRIANGULAR sub-boundary-layer vortex generators
title_full Computational modelling of TRIANGULAR sub-boundary-layer vortex generators
title_fullStr Computational modelling of TRIANGULAR sub-boundary-layer vortex generators
title_full_unstemmed Computational modelling of TRIANGULAR sub-boundary-layer vortex generators
title_sort computational modelling of triangular sub-boundary-layer vortex generators
publisher EDP Sciences
series MATEC Web of Conferences
issn 2261-236X
publishDate 2020-01-01
description Vortex generators (VGs) are used increasingly more by the wind turbine manufacture industry as flow control devices to improve rotor blade aerodynamic performance. The VG height is usually designed with equal thickness of the local boundary layer at the VG position. Nevertheless, these conventional VGs may produce excess residual drag in some applications. The so-called sub boundary layer VGs can provide enough momentum transfer over a region several times their own height for effective flow-separation control with much lower drag. The main objective is to investigate how well the simulations can reproduce the physics of the flow of the primary vortex generated by a triangular VG mounted on a flat plate with negligible pressure gradient with the angle of attack of the vane to the oncoming flow β= 18. Three different device heights H= 5mm, H1= 6,25mm, H2= 4,16mm have been studied and compared both qualitatively and quantitatively. To that end, computational simulations have been carried out using RANS method and at Reynolds number Re = 2600 based on the boundary layer momentum thickness θ= 2.4 mm at the VG position. The computational results show good agreement with the experimental data available in AVATAR project.
url https://www.matec-conferences.org/articles/matecconf/pdf/2020/03/matecconf_icome2017-2018_01054.pdf
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