Impact of Leakage Inlet Swirl Angle in a Rotor–Stator Cavity on Flow Pattern, Radial Pressure Distribution and Frictional Torque in a Wide Circumferential Reynolds Number Range

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datacite.relatedItem.firstPage7
datacite.relatedItem.issue2
datacite.relatedItem.relatedIdentifierTypeISSN
datacite.relatedItem.relatedItemIdentifier2504-186X
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datacite.relatedItem.titleIJTPP
datacite.relatedItem.volume5
dc.contributor.authorTilman Raphael Schröder
dc.contributor.authorHans-Josef Dohmen
dc.contributor.authorDieter Brillert
dc.contributor.authorFriedrich-Karl Benra
dc.date.accessioned2024-08-26T11:57:48Z
dc.date.available2024-08-26T11:57:48Z
dc.date.issued2020
dc.identifier.doihttps://doi.org/10.3390/ijtpp5020007
dc.identifier.otherjz000095-0015
dc.identifier.urihttps://tustorage.ulb.tu-darmstadt.de/handle/tustorage/9246
dc.publisherMDPI AG
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/
dc.subject.ddc620
dc.titleImpact of Leakage Inlet Swirl Angle in a Rotor–Stator Cavity on Flow Pattern, Radial Pressure Distribution and Frictional Torque in a Wide Circumferential Reynolds Number Range
dc.typeArticle
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