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dc.contributor.authorDuquesne, Pierre
dc.contributor.authorDombard, Jerome
dc.contributor.authorPoujol, Nicolas
dc.contributor.authorGiauque, Alexis
dc.date.accessioned2024-12-24T18:43:46Z
dc.date.available2024-12-24T18:43:46Z
dc.date.copyright5/8/2024 12:00:00 AM
dc.date.issued2024
dc.identifier.issn0889-504X
dc.identifier.otherturbo_146_10_101011.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4302636
dc.description.abstractLarge eddy simulations (LES) results are used to track flow separation zones in a splittered vaned radial diffuser near the compressor best efficiency at high rotation speed. The topology analysis reveals some closed separations at the corner of the blade and hub or shroud surface. In addition, an open–closed flow separation at the main blade pressure side is observed for the first time. The surface separation has the shape of a sheet at the blade mid-span, and the associated separation line is delimited only at its downstream extremity by a trailing edge node. This flow separation process is robust to a small shift in operating condition, and the separation surface remains essentially unchanged. A large flowrate variation converts the open–closed separation into a more classic closed separation. The evolution in time of the separation surface is also observed, and the authors conclude to the unsteady existence of the open–closed separation.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleAn Open–Closed Flow Separation in a Compressor Radial Diffuser
dc.typeJournal Paper
dc.journal.volume146
dc.journal.issue10
dc.journal.titleJournal of Turbomachinery
dc.identifier.doi10.1115/1.4065413
dc.journal.fristpage101011-1
dc.journal.lastpage101011-8
dc.page8
dc.treeJournal of Turbomachinery:;2024:;volume( 146 ):;issue: 010
dc.contenttypeFulltext


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