2015
DOI: 10.1016/j.renene.2014.11.043
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Effects of vortex generators on a blunt trailing-edge airfoil for wind turbines

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Cited by 127 publications
(66 citation statements)
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“…In the work carried out by Gao et al [16] and Baldacchino et al [17] on a 30% thick DU97-W-300 airfoil (Delft University of Technology, Delft, The Nederlands), the maximum lift coefficient was substantially increased due to the implementation of passive VGs. When the angle of attack increases, both lift and drag coefficients rise up to values higher than the ones reached in steady state conditions.…”
Section: Introductionmentioning
confidence: 99%
“…In the work carried out by Gao et al [16] and Baldacchino et al [17] on a 30% thick DU97-W-300 airfoil (Delft University of Technology, Delft, The Nederlands), the maximum lift coefficient was substantially increased due to the implementation of passive VGs. When the angle of attack increases, both lift and drag coefficients rise up to values higher than the ones reached in steady state conditions.…”
Section: Introductionmentioning
confidence: 99%
“…Oye [162] studied the effect of VG on the performance of 1 MW rated capacity wind turbine and reported that the addition of VGs to the rotor blades significantly improved the performance of the turbine. To explore the extent of reduction in drag achieved using the VG, it was compared without VG numerically by Gao et al [163] taking into consideration a three-dimensional model which accurately predicts the rotating condition of the turbine blade. VG jets are the streams of fluid that enter through the wall of the blade in a cross flow direction and create a dominant streamwise vortex that stays in the boundary layer causing the flow to stick to the surface, Khan and Johnston [164].…”
Section: Active Flow Control Techniquesmentioning
confidence: 99%
“…Great care is also needed to be taken in Fernandez-Gamiz et al [10] and Urkiola et al [11] studied the behaviour of a rectangular VG on a flat plate and the streamwise vortices produced to investigate how the physics of the wake behind VGs in a negligible streamwise pressure gradient flow can be reproduced in CFD simulations. In the work carried by Gao et al [12] on a 30% thick DU97-W-300 airfoil (Delft University family airfoils, Delft, The Netherlands), the maximum lift coefficient was increased from 1.5 to approximately 2 due to the implementation of passive VGs. When the angle of attack increases, both the lift and drag coefficients rise to values higher than the ones reached in the steady state conditions.…”
Section: Introductionmentioning
confidence: 99%