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    Thermodynamic Effect on a Cavitating Inducer—Part II: On-Board Measurements of Temperature Depression Within Leading Edge Cavities

    Source: Journal of Fluids Engineering:;2010:;volume( 132 ):;issue: 002::page 21304
    Author:
    Jean-Pierre Franc
    ,
    Éric Janson
    ,
    Pierre Ramina
    ,
    Guillaume Boitel
    ,
    Michel Riondet
    ,
    Claude Rebattet
    DOI: 10.1115/1.4001007
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Temperature 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.
    keyword(s): Temperature , Cavitation , Blades AND Cavities ,
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      Thermodynamic Effect on a Cavitating Inducer—Part II: On-Board Measurements of Temperature Depression Within Leading Edge Cavities

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/143542
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    • Journal of Fluids Engineering

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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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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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