2018
DOI: 10.5194/wes-3-1-2018
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Extraction of the wake induction and angle of attack on rotating wind turbine blades from PIV and CFD results

Abstract: Abstract. The analysis of wind turbine aerodynamics requires accurate information about the axial and tangential wake induction as well as the local angle of attack along the blades. In this work we present a new method for obtaining them conveniently from the velocity field. We apply the method to the New Mexico particle image velocimetry (PIV) data set and to computational fluid dynamics (CFD) simulations of the same turbine. This allows the comparison of experimental and numerical results of the mentioned q… Show more

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Cited by 26 publications
(27 citation statements)
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“…The local tangential velocity extracted from the radial traverse corresponds to the local tangential wake induction after changing its sign. It is demonstrated in Ref [39] that this method can predict the AoA satisfactorily from the root until at least 92% of the blade length. For larger spanwise positions, other methods, like e.g.…”
Section: Control Point Locusmentioning
confidence: 97%
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“…The local tangential velocity extracted from the radial traverse corresponds to the local tangential wake induction after changing its sign. It is demonstrated in Ref [39] that this method can predict the AoA satisfactorily from the root until at least 92% of the blade length. For larger spanwise positions, other methods, like e.g.…”
Section: Control Point Locusmentioning
confidence: 97%
“…• Herráez Method: This method obtains the undisturbed flow rotor velocity by extracting them directly from a position in the rotor plane where the influence of the blade bound circulation from each blade is canceled out by the other blades [39]. In the case of axi-symmetric, homogeneous inflow, this position corresponds to the bisectrix of the angle between two arbitrary blades.…”
Section: Control Point Locusmentioning
confidence: 99%
“…Despite the possible validation for force and pressure coefficient, the proposal of an alternative model for rotational augmentation necessitates the capture of aerodynamic coefficient, thus, the AoA, or alternatively, the determination of the local velocity in the rotor plane without bound circulation [22], i.e. axial and angular induction factors.…”
Section: Validation Of the Simulationsmentioning
confidence: 99%
“…Clearly, deducing the value of the aerodynamic forces from both experiments or simulations required the estimation of the angle of attack (AoA). In a rotating blade, this aspect is directly connected with the determination of the local inflow velocity in the rotor plane which is free of bound circulation (local undisturbed velocity) [22]. There are several methods for calculating the angle of attack at the rotor, thus, the analyses of this work are restricted to three proposals: average azimuthal technique (AAT) [23], three-point (3P) [24] and zero gamma (ZG) [22].…”
Section: Introductionmentioning
confidence: 99%
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