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dc.contributor.authorUruba, Václav
dc.contributor.authorPátek, Zdeněk
dc.contributor.authorProcházka, Pavel
dc.contributor.authorSkála, Vladislav
dc.contributor.authorZacho, David
dc.contributor.authorKulhánek, Robert
dc.date.accessioned2019-03-26T09:11:22Z-
dc.date.available2019-03-26T09:11:22Z-
dc.date.issued2018
dc.identifier.citationURUBA, V., PÁTEK, Z., PROCHÁZKA, P., SKÁLA, V., ZACHO, D., KULHÁNEK, R. Flow Structure behind a Wing at High Reynolds Numbers. In EFM17 – Experimental Fluid Mechanics 2017. COUTABOEUF: EDP Sciences, 2018. s. 1-7. ISSN: 2101-6275.en
dc.identifier.issn2101-6275
dc.identifier.uri2-s2.0-85049387855
dc.identifier.urihttp://hdl.handle.net/11025/33774
dc.format7 s.cs
dc.format.mimetypeapplication/pdf
dc.language.isoenen
dc.publisherEDP Sciencesen
dc.relation.ispartofseriesEFM17 – Experimental Fluid Mechanics 2017en
dc.rights© EDP Sciencesen
dc.titleFlow Structure behind a Wing at High Reynolds Numbersen
dc.typekonferenční příspěvekcs
dc.typeconferenceObjecten
dc.rights.accessopenAccessen
dc.type.versionpublishedVersionen
dc.description.abstract-translatedThe stereo PIV measurement were performed behind a wing in the plane perpendicular to the flow to study the vortical structures oriented in the streamwise direction, which take place both in suction and pressure sides of the wing. The Reynolds numbers during the experiments in the 3 m wind tunnel range from 0.5 million up to 1.5 million.en
dc.subject.translatedFlow Structureen
dc.subject.translatedWingen
dc.subject.translatedHigh Reynolds Numbersen
dc.identifier.doi10.1051/epjconf/201817002111
dc.type.statusPeer-revieweden
dc.identifier.document-number454317800112
dc.identifier.obd43925517
dc.project.IDSGS-2016-045/Zvyšování účinnosti, spolehlivosti a životnosti energetických strojů a zařízení 4cs
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