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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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.identifier.urihttps://tustorage.ulb.tu-darmstadt.de/handle/tustorage/9247
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.typepdf
dspace.entity.typeDistribution
relation.isDatasetOfDistribution4a2ee1fe-b48d-4627-a139-766abe57d450
relation.isDatasetOfDistribution.latestForDiscovery4a2ee1fe-b48d-4627-a139-766abe57d450

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