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dc.contributor.authorAdebayo, David Shina
dc.contributor.authorRona, A
dc.date.accessioned2019-10-10T12:57:02Z
dc.date.available2019-10-10T12:57:02Z
dc.date.issued2015-02-28
dc.identifier.citationAdebayo, D. S. and Rona, A. (2015) PIV study of the flow across the meridional plane of rotating cylinders with wide gap, International Review of Aerospace Engineering,en
dc.identifier.issn1973-7459en
dc.identifier.doi10.15866/irease.v8i1.5290en
dc.identifier.urihttp://hdl.handle.net/2436/622819
dc.description.abstractThis study investigates by Particle Image Velocimetry (PIV) the wavy Taylor vortex flow that develops in the gap between concentric rotating cylinders of low aspect ratio and low radius ratio, which is a configuration relevant to oil bearing chambers in turbomachinery. The configuration is characterised by a larger annular gap width than in classical journal bearing and by a Taylor number (Ta) of 2.47 × 106, which is 1000 times higher than the first critical Taylor number. It is found that the non-uniform axial spacing of the vortex cores induces an asymmetric radial velocity profile and an inflected axial velocity profile close to the cylindrical walls. The outflow at the centre of each pair of Taylor vortices that make up a vortex cell is strong and it is characterised by a sharp radial velocity peak. The inflow between pairs of Taylor vortex cells is unconventional in that it is characterised by pairs of confluent streams from the outer cylinder that merge towards the inner cylinder. These results form a body of experimental evidence on the flow features that may occur in engineering practice in oil bearing chamber flows, with relevance to lubrication and wear.en
dc.formatapplication/PDFen
dc.language.isoenen
dc.publisherPraise Worthy Prizeen
dc.subjectparticle image velocimetryen
dc.subjectconcentric cylindersen
dc.subjectwide gapen
dc.subjectTaylor vorticesen
dc.subjectMeridional Plane PIVen
dc.subjecthigh Taylor number flowen
dc.titlePIV study of the flow across the meridional plane of rotating cylinders with wide gapen
dc.typeJournal articleen
dc.identifier.eissn1973-7440
dc.identifier.journalInternational Review of Aerospace Engineeringen
dc.date.updated2019-09-24T17:47:31Z
dc.date.accepted2015-01-01
rioxxterms.funderJiscen
rioxxterms.identifier.projectUOW10102019DAen
rioxxterms.versionAMen
rioxxterms.licenseref.urihttps://creativecommons.org/licenses/by-nc-nd/4.0/en
rioxxterms.licenseref.startdate2019-10-10en
dc.source.volume8
dc.source.issue1
dc.source.beginpage26
dc.source.endpage35
dc.description.versionPublished version
refterms.dateFCD2019-10-10T12:56:17Z
refterms.versionFCDAM
refterms.dateFOA2019-10-10T12:57:03Z


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