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contributor authorHoriguchi
contributor authorHironori;Tsubouchi
contributor authorKota;Toyoshima
contributor authorMasakazu;Sugiyama
contributor authorKazuyasu
date accessioned2022-08-18T12:56:06Z
date available2022-08-18T12:56:06Z
date copyright6/28/2022 12:00:00 AM
date issued2022
identifier issn0098-2202
identifier otherfe_144_11_111204.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4287129
description abstractA circumferential groove with swirl breakers was designed and its effect on the suppression of cavitation instabilities in an inducer was investigated in experiments. The circumferential groove with the swirl breakers could suppress almost all cavitation instability phenomena effectively and improve suction performance. Observations of flow fields in CFD showed that the swirl breakers reduced the circumferential velocity of the flow near the blade tip at the inlet of the inducer. It was suggested that such a flow pattern succeeded in suppressing cavitation instability phenomena, including pressure fluctuations with high frequencies caused by the interaction of the blades with backflow vortices which were visible as backflow vortex cavities in low suction pressure.
publisherThe American Society of Mechanical Engineers (ASME)
titleSuppression of Cavitation Instabilities in an Inducer by the Circumferential Groove With Swirl Breakers
typeJournal Paper
journal volume144
journal issue11
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.4054706
journal fristpage111204-1
journal lastpage111204-14
page14
treeJournal of Fluids Engineering:;2022:;volume( 144 ):;issue: 011
contenttypeFulltext


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