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    Pressure Loss Due to the Tip Clearance of Impeller Blades in Centrifugal and Axial Blowers

    Source: Journal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 001::page 32
    Author:
    Y. Senoo
    ,
    M. Ishida
    DOI: 10.1115/1.3239882
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The pressure loss based on the tip clearance of impeller blades consists of the pressure loss induced by the leakage flow through the clearance and the pressure loss for supporting fluid against the pressure gradient in the channels and in the thin annular clearance space between the shroud and the impeller. Equations to evaluate these losses are derived and the predicted efficiency drop is compared with experimental data for two types of centrifugal impellers. Furthermore, the equations are simplified for axial impellers as a special case, and the predicted efficiency drop is compared with the experimental data for seven cases in the literature. Fair agreement demonstrates plausibility of the present model.
    keyword(s): Pressure , Impellers , Clearances (Engineering) , Blades , Equations , Drops , Fluids , Channels (Hydraulic engineering) , Pressure gradient AND Leakage flows ,
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      Pressure Loss Due to the Tip Clearance of Impeller Blades in Centrifugal and Axial Blowers

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    http://yetl.yabesh.ir/yetl1/handle/yetl/101155
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorY. Senoo
    contributor authorM. Ishida
    date accessioned2017-05-08T23:22:31Z
    date available2017-05-08T23:22:31Z
    date copyrightJanuary, 1986
    date issued1986
    identifier issn1528-8919
    identifier otherJETPEZ-26630#32_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101155
    description abstractThe pressure loss based on the tip clearance of impeller blades consists of the pressure loss induced by the leakage flow through the clearance and the pressure loss for supporting fluid against the pressure gradient in the channels and in the thin annular clearance space between the shroud and the impeller. Equations to evaluate these losses are derived and the predicted efficiency drop is compared with experimental data for two types of centrifugal impellers. Furthermore, the equations are simplified for axial impellers as a special case, and the predicted efficiency drop is compared with the experimental data for seven cases in the literature. Fair agreement demonstrates plausibility of the present model.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePressure Loss Due to the Tip Clearance of Impeller Blades in Centrifugal and Axial Blowers
    typeJournal Paper
    journal volume108
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3239882
    journal fristpage32
    journal lastpage37
    identifier eissn0742-4795
    keywordsPressure
    keywordsImpellers
    keywordsClearances (Engineering)
    keywordsBlades
    keywordsEquations
    keywordsDrops
    keywordsFluids
    keywordsChannels (Hydraulic engineering)
    keywordsPressure gradient AND Leakage flows
    treeJournal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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