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dc.contributor.authorDuda, Daniel
dc.contributor.authorYanovych, Vitalii
dc.contributor.authorUruba, Václav
dc.contributor.authorŽitek, Pavel
dc.contributor.authorMilčák, Petr
dc.contributor.authorJelínek, Tomáš
dc.contributor.authorNěmec, Martin
dc.date.accessioned2021-11-01T11:00:38Z-
dc.date.available2021-11-01T11:00:38Z-
dc.date.issued2021
dc.identifier.citationDUDA, D. YANOVYCH, V. URUBA, V. ŽITEK, P. MILČÁK, P. JELÍNEK, T. NĚMEC, M. Experimental investigation of the unsteady stator/rotor wake characteristics downstream of an axial air turbine. International Journal of Turbomachinery, Propulsion and Power, 2021, roč. 6, č. 3, s. nestránkováno. ISSN: 2504-186Xcs
dc.identifier.issn2504-186X
dc.identifier.uri2-s2.0-85110477662
dc.identifier.urihttp://hdl.handle.net/11025/45651
dc.format25 s.cs
dc.format.mimetypeapplication/pdf
dc.language.isoenen
dc.publisherMDPIen
dc.relation.ispartofseriesInternational Journal of Turbomachinery, Propulsion and Poweren
dc.rights© authorsen
dc.titleExperimental investigation of the unsteady stator/rotor wake characteristics downstream of an axial air turbineen
dc.title.alternativeExperimentální výzkum nestacionárních charakteristik staorového/rotorového úplavu za axiální vzduchovou turbínoucs
dc.typepreprintcs
dc.typepreprinten
dc.rights.accessopenAccessen
dc.type.versiondraften
dc.description.abstract-translatedA feasibility study of velocity field measurements using the Particle Image Velocimetry (PIV) method in an axial air turbine model is presented. The wakes past the blades of the rotor wheel were observed using the PIV technique. Data acquisition was synchronized with the shaft rotation; thus, the wakes were phase averaged for statistical analysis. The interaction of the rotor blade wakes with the stator ones was investigated by changing the stator wheel’s angle. The measurement planes were located just behind the rotor blades, covering approximately 3 cm × 3 cm in axial × tangential directions. The spatial correlation function suggests that the resolution used is sufficient for the large-scale flow-patterns only, but not for the small ones. The scales of fluctuations correspond to the shear layer thickness at the mid-span plane but, close to the end-wall, they contain larger structures caused by the secondary flows. The length-scales of the fluctuations under off-design conditions display a dependence on the area of the stator and rotor wakes cross-sections, which, in turn, depend on their angle. The obtained experimental data are to be used for the validation of mathematical simulation results in the future.en
dc.subject.translatedLength-scaleen
dc.subject.translatedParticle Image Velocimetryen
dc.subject.translatedPIVen
dc.subject.translatedTurbineen
dc.subject.translatedTurbine test facilityen
dc.subject.translatedTurbomachineryen
dc.subject.translatedWakeen
dc.identifier.doi10.3390/ijtpp6030022
dc.identifier.obd43933487
dc.project.IDEF16_026/0008389/LoStr: Výzkumná spolupráce pro dosažení vyšší účinnosti a spolehlivosti lopatkových strojůcs
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Preprinty / Preprints (CEV)
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