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dc.contributor.authorHaans, Wouter-
dc.contributor.authorSant, Tonio-
dc.contributor.authorvan Kuik, Gijs-
dc.contributor.authorvan Bussel, Gerard-
dc.date.accessioned2017-03-27T07:29:15Z-
dc.date.available2017-03-27T07:29:15Z-
dc.date.issued2005-
dc.identifier.citationHaans, W., Sant, T., van Kuik, G., & van Bussel, G. (2005). Measurement and modelling of tip vortex paths in the wake of a HAWT under yawed flow conditions. 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno. 7575-7584.en_GB
dc.identifier.urihttps://www.um.edu.mt/library/oar//handle/123456789/17851-
dc.description.abstractTip vortex locations have been measured in the wake of a model rotor in both axial flow and yaw using quantitative flow visualisation. For each setting, the axial force coefficient has been derived as well from measurements. The results seem to agree well with those previously published on the Delft University of technology model rotor. The main interest is to determine the tip vortex pitch, wake skew angle and wake expansion and to physically interpret the data. The results should also help to validate and construct models. The tip vortex locations data complement the existing skewed wake velocity data from hot-wire anemometry, making it a valuable experimental database.en_GB
dc.language.isoenen_GB
dc.publisherAmerican Institute of Aeronautics and Astronautics, Inc.en_GB
dc.rightsinfo:eu-repo/semantics/restrictedAccessen_GB
dc.subjectHorizontal axis wind turbinesen_GB
dc.subjectWind poweren_GB
dc.subjectWind turbinesen_GB
dc.subjectAnemometeren_GB
dc.subjectAxial flowen_GB
dc.subjectRotorsen_GB
dc.titleMeasurement and modelling of tip vortex paths in the wake of a HAWT under yawed flow conditionsen_GB
dc.typeconferenceObjecten_GB
dc.rights.holderThe copyright of this work belongs to the author(s)/publisher. The rights of this work are as defined by the appropriate Copyright Legislation or as modified by any successive legislation. Users may access this work and can make use of the information contained in accordance with the Copyright Legislation provided that the author must be properly acknowledged. Further distribution or reproduction in any format is prohibited without the prior permission of the copyright holder.en_GB
dc.bibliographicCitation.conferencename43rd AIAA Aerospace Sciences Meeting and Exhibiten_GB
dc.bibliographicCitation.conferenceplaceReno, United States, 10-13/01/2005en_GB
dc.description.reviewedpeer-revieweden_GB
dc.identifier.doi10.1115/1.2037092-
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