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contributor authorJean-Pierre Franc
contributor authorÉric Janson
contributor authorPierre Ramina
contributor authorGuillaume Boitel
contributor authorMichel Riondet
contributor authorClaude Rebattet
date accessioned2017-05-09T00:38:20Z
date available2017-05-09T00:38:20Z
date copyrightFebruary, 2010
date issued2010
identifier issn0098-2202
identifier otherJFEGA4-27408#021304_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/143542
description abstractTemperature depression within the leading edge cavities on a space inducer is measured in Refrigerant 114 using miniature thermocouples mounted on the rotating blades. Time-averaged values of cavity temperature depression are determined all along the descent in cavitation number and correlated with the extent of cavities. In addition to mean values, temperature fluctuations are analyzed with respect to the onset of cavitation instabilities, namely, alternate blade cavitation and supersynchronous rotating cavitation. Temperature spectra relative to a rotating frame of reference are compared with pressure spectra obtained in a fixed frame of reference. Temperature oscillations issued from different blades are compared, and phase shifts between consecutive and opposite blades are evaluated in the case of the supersynchronous instability regime.
publisherThe American Society of Mechanical Engineers (ASME)
titleThermodynamic Effect on a Cavitating Inducer—Part II: On-Board Measurements of Temperature Depression Within Leading Edge Cavities
typeJournal Paper
journal volume132
journal issue2
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.4001007
journal fristpage21304
identifier eissn1528-901X
keywordsTemperature
keywordsCavitation
keywordsBlades AND Cavities
treeJournal of Fluids Engineering:;2010:;volume( 132 ):;issue: 002
contenttypeFulltext


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