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dc.contributor.authorBém, Jindřich
dc.contributor.authorDuda, Daniel
dc.contributor.authorKovařík, Jiří
dc.contributor.authorYanovych, Vitalii
dc.contributor.authorUruba, Václav
dc.date.accessioned2021-03-29T10:00:17Z-
dc.date.available2021-03-29T10:00:17Z-
dc.date.issued2019
dc.identifier.citationBÉM, J. DUDA, D. KOVAŘÍK, J. YANOVYCH, V. URUBA, V. Visualization of secondary flow in a corner of a channel. In: AIP Conference Proceedings. [S. l.]: American Institute of Physics Inc., 2019. ISBN 978-0-7354-1936-0, ISSN 0094-243X.cs
dc.identifier.isbn978-0-7354-1936-0
dc.identifier.issn0094-243X
dc.identifier.uri2-s2.0-85076411702
dc.identifier.urihttp://hdl.handle.net/11025/43120
dc.format6 s.
dc.format.mimetypeapplication/pdf
dc.language.isoenen
dc.publisherAmerican Institute of Physics Inc.en
dc.relation.ispartofseriesAIP Conference Proceedingsen
dc.rights© American Institute of Physicsen
dc.titleVisualization of secondary flow in a corner of a channelen
dc.typekonferenční příspěvekcs
dc.typeconferenceObjecten
dc.rights.accessopenAccessen
dc.type.versionpublishedVersionen
dc.description.abstract-translatedWe report observation of secondary flow in one corner of developing channel air flow. Length of the channel, i.e. length of boundary layer, is 400?mm, which is 3.2 times the channel cross-sectional size. Three components of velocity are measured by using a Stereo Particle Image Velocimetry (PIV) technique in the measurement area of size 24×22?mm, which is perpendicular to the direction of main flow in the channel. The Reynolds number based on the length of the channel ranged from 4·104 to 8·105 and has been controlled via imposed velocity. At low Reynolds number we observe a laminar corner vortex having at all velocities the same orientation. This symmetry breaking is probably caused by an imperfectness of the experimental device. At Reynolds number around 8·104 this vortex starts to slightly variate its strength and position causing transition of boundary layers into turbulence at Re = 1.1·105. At higher Re this laminar vortex disappears from the instantaneous velocity fields, but it is still apparent in the averaged ones. It gets smaller and another oppositely oriented vortex forms; note that the second vortex is not observed in the instantaneous velocity fields, only in the ensemble average. At even higher Re, this secondary flow structure is smaller than the turbulent boundary layers, but its shape of a pair of counter-rotating vortices is conserved probably being a seed for secondary flow between fully developed boundary layers reported in the literature for longer channels with fully developed flow.en
dc.subject.translatedTurbulence, Secondary flow, Boundary layer, Particle Image Velocimetryen
dc.identifier.doi10.1063/1.5138615
dc.type.statusPeer-revieweden
dc.identifier.obd43930510
dc.project.IDSGS-2019-001/Komplexní podpora konstruování technických zařízení IV.cs
Appears in Collections:Konferenční příspěvky / Conference papers (CEV)
Konferenční příspěvky / Conference papers (KKE)
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