Determination of the angle of attack on a research wind turbine rotor blade using surface pressure measurements

dc.contributor.authorSoto-Valle, Rodrigo
dc.contributor.authorBartholomay, Sirko
dc.contributor.authorAlber, Jörg
dc.contributor.authorManolesos, Marinos
dc.contributor.authorNayeri, Christian Navid
dc.contributor.authorPaschereit, Christian Oliver
dc.date.accessioned2021-01-04T14:25:27Z
dc.date.available2021-01-04T14:25:27Z
dc.date.issued2020-12-22
dc.description.abstractIn this paper, a method to determine the angle of attack on a wind turbine rotor blade using a chordwise pressure distribution measurement was applied. The approach used a reduced number of pressure tap data located close to the blade leading edge. The results were compared with the measurements from three external probes mounted on the blade at different radial positions and with analytical calculations. Both experimental approaches used in this study are based on the 2-D flow assumption; the pressure tap method is an application of the thin airfoil theory, while the probe method applies geometrical and induction corrections to the measurement data. The experiments were conducted in the wind tunnel at the Hermann Föttinger Institut of the Technische Universität Berlin. The research turbine is a three-bladed upwind horizontal axis wind turbine model with a rotor diameter of 3 m. The measurements were carried out at rated conditions with a tip speed ratio of 4.35, and different yaw and pitch angles were tested in order to compare the approaches over a wide range of conditions. Results show that the pressure tap method is suitable and provides a similar angle of attack to the external probe measurements as well as the analytical calculations. This is a significant step for the experimental determination of the local angle of attack, as it eliminates the need for external probes, which affect the flow over the blade and require additional calibration.en
dc.description.sponsorshipTU Berlin, Open-Access-Mittel – 2020en
dc.identifier.eissn2366-7451
dc.identifier.issn2366-7443
dc.identifier.urihttps://depositonce.tu-berlin.de/handle/11303/12337
dc.identifier.urihttp://dx.doi.org/10.14279/depositonce-11180
dc.language.isoenen
dc.relation.ispartof10.14279/depositonce-16447
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/en
dc.subject.ddc600 Technik, Technologiede
dc.subject.otherresearch wind turbineen
dc.subject.othersurface pressureen
dc.subject.otherrotor bladesen
dc.titleDetermination of the angle of attack on a research wind turbine rotor blade using surface pressure measurementsen
dc.typeArticleen
dc.type.versionpublishedVersionen
dcterms.bibliographicCitation.doi10.5194/wes-5-1771-2020en
dcterms.bibliographicCitation.issue4en
dcterms.bibliographicCitation.journaltitleWind Energy Scienceen
dcterms.bibliographicCitation.originalpublishernameCopernicusen
dcterms.bibliographicCitation.originalpublisherplaceGöttingenen
dcterms.bibliographicCitation.pageend1792en
dcterms.bibliographicCitation.pagestart1771en
dcterms.bibliographicCitation.volume5en
tub.accessrights.dnbfreeen
tub.affiliationFak. 5 Verkehrs- und Maschinensysteme::Inst. Strömungsmechanik und Technische Akustik (ISTA)::FG Experimentelle Strömungsmechanikde
tub.affiliation.facultyFak. 5 Verkehrs- und Maschinensystemede
tub.affiliation.groupFG Experimentelle Strömungsmechanikde
tub.affiliation.instituteInst. Strömungsmechanik und Technische Akustik (ISTA)de
tub.publisher.universityorinstitutionTechnische Universität Berlinen

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