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contributor authorDuquesne, Pierre
contributor authorDombard, Jerome
contributor authorPoujol, Nicolas
contributor authorGiauque, Alexis
date accessioned2024-12-24T18:43:46Z
date available2024-12-24T18:43:46Z
date copyright5/8/2024 12:00:00 AM
date issued2024
identifier issn0889-504X
identifier otherturbo_146_10_101011.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4302636
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.
publisherThe American Society of Mechanical Engineers (ASME)
titleAn Open–Closed Flow Separation in a Compressor Radial Diffuser
typeJournal Paper
journal volume146
journal issue10
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4065413
journal fristpage101011-1
journal lastpage101011-8
page8
treeJournal of Turbomachinery:;2024:;volume( 146 ):;issue: 010
contenttypeFulltext


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