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dc.contributor.authorSchlipf, Davidde
dc.contributor.authorTrabucchi, Davidede
dc.contributor.authorBischoff, Oliverde
dc.contributor.authorHofsäß, Martinde
dc.contributor.authorMann, Jakobde
dc.contributor.authorMikkelsen, Torbende
dc.contributor.authorRettenmeier, Andreasde
dc.contributor.authorTrujillo, Juan Joséde
dc.contributor.authorKühn, Martinde
dc.date.accessioned2013-08-06de
dc.date.accessioned2016-03-31T08:07:23Z-
dc.date.available2013-08-06de
dc.date.available2016-03-31T08:07:23Z-
dc.date.issued2011de
dc.identifier.other392313294de
dc.identifier.urihttp://nbn-resolving.de/urn:nbn:de:bsz:93-opus-85870de
dc.identifier.urihttp://elib.uni-stuttgart.de/handle/11682/3932-
dc.identifier.urihttp://dx.doi.org/10.18419/opus-3915-
dc.description.abstractTaylor’s frozen turbulence hypothesis is tested in its applicability for wind turbine applications. In this research full field measurements are performed at a test site for multi-megawatt wind turbines by means of a pulsed LIDAR with a scanning device. The system is installed at the top of the nacelle of a 5MW wind turbine. It provides simultaneous wind speed, with a maximum sampling rate of 5 Hz, at different stations parallel to the mean wind. Measurements in a range between 0.4 and 1.6 rotor diameter are performed following several two and three dimensional trajectories. The spectral characteristics of measurements taken simultaneously at different separation distances are studied. The scanning strategy which maximizes the wavenumber region where results are consistent with Taylor’s hypothesis is assessed. The best results are achieved by a horizontal sliding trajectory with valid wavenumbers up to 0.125 rad/m.en
dc.language.isoende
dc.rightsinfo:eu-repo/semantics/openAccessde
dc.subject.classificationLidar , Windenergie , Turbulente Strömungde
dc.subject.ddc624de
dc.subject.otherlidar , wind energy , Taylor's Frozen Turbulence Hypothesisen
dc.titleTesting of frozen turbulence hypothesis for wind turbine applications with a scanning LIDAR systemen
dc.typeconferenceObjectde
dc.date.updated2013-08-15de
ubs.fakultaetFakultät Luft- und Raumfahrttechnik und Geodäsiede
ubs.fakultaetFakultätsübergreifend / Sonstige Einrichtungde
ubs.institutInstitut für Flugzeugbaude
ubs.institutSonstige Einrichtungde
ubs.opusid8587de
ubs.publikation.sourceISARS 2010 : 28-30 June, Parisde
ubs.publikation.typKonferenzbeitragde
Enthalten in den Sammlungen:06 Fakultät Luft- und Raumfahrttechnik und Geodäsie



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