Spectral analysis of the boundary layer on a plunging airfoil

dc.contributor.authorSoltani, M. R.
dc.contributor.authorRasi, Marzabadi F.
dc.date.accessioned2015-06-24T07:56:34Z
dc.date.available2015-06-24T07:56:34Z
dc.date.issued2010
dc.description.abstractPaper presented at the 7th International Conference on Heat Transfer, Fluid Mechanics and Thermodynamics, Turkey, 19-21 July, 2010.en_ZA
dc.description.abstractThe effects of periodic unsteady flow through plunging motion on the boundary layer transition along the suction surface of a typical wind turbine blade section are experimentally investigated The state of the boundary layer at different conditions was determined using multiple hot-film sensors through the frequency domain analysis. The appearance of laminar/turbulent spikes at dominated frequencies revealed the boundary layer characteristics. Power spectral of the hot­-film signals showed that the transition locations as well as the separation region were a function of the reduced frequency and mean angle of attack.
dc.description.librarianej2015en_ZA
dc.format.extent5 pagesen_ZA
dc.format.mediumPDFen_ZA
dc.identifier.citationSoltani, MR & Rasi MF 2010, 'Spectral analysis of the boundary layer on a plunging airfoil', Paper presented to the 7th International Conference on Heat Transfer, Fluid Mechanics and Thermodynamics, Turkey, 19-21 July 2010.en_ZA
dc.identifier.urihttp://hdl.handle.net/2263/45755
dc.language.isoenen_ZA
dc.publisherInternational Conference on Heat Transfer, Fluid Mechanics and Thermodynamicsen_ZA
dc.relation.ispartofHEFAT 2010en_US
dc.rightsUniversity of Pretoriaen_ZA
dc.subjectSpectral analysisen_ZA
dc.subjectPlunging airfoilen_ZA
dc.titleSpectral analysis of the boundary layer on a plunging airfoilen_ZA
dc.typePresentationen_ZA

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