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    Turbulent Boundary Layers on Centrifugal Compressor Blades: Prediction of the Effects of Surface Curvature and Rotation

    Source: Journal of Fluids Engineering:;1976:;volume( 098 ):;issue: 003::page 374
    Author:
    J. P. Johnston
    ,
    S. A. Eide
    DOI: 10.1115/1.3448327
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A method for calculation of turbulent boundary layers on curved, rotating surfaces is presented, and the applicability of the method to the prediction of attached flow over compressor rotor blades is indicated. Calculated results are compared to existing data sets. Additional sample calculations to study the effects of rotation are also presented. Correlations of these calculated results provide a simple method for estimation of the effects of rotation on skin friction, cf , and boundary-layer shape factor, H.
    keyword(s): Compressors , Rotation , Blades , Boundary layer turbulence , Shapes , Flow (Dynamics) , Skin friction (Fluid dynamics) , Boundary layers AND Rotors ,
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      Turbulent Boundary Layers on Centrifugal Compressor Blades: Prediction of the Effects of Surface Curvature and Rotation

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/88777
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    • Journal of Fluids Engineering

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    contributor authorJ. P. Johnston
    contributor authorS. A. Eide
    date accessioned2017-05-08T23:00:56Z
    date available2017-05-08T23:00:56Z
    date copyrightSeptember, 1976
    date issued1976
    identifier issn0098-2202
    identifier otherJFEGA4-26897#374_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/88777
    description abstractA method for calculation of turbulent boundary layers on curved, rotating surfaces is presented, and the applicability of the method to the prediction of attached flow over compressor rotor blades is indicated. Calculated results are compared to existing data sets. Additional sample calculations to study the effects of rotation are also presented. Correlations of these calculated results provide a simple method for estimation of the effects of rotation on skin friction, cf , and boundary-layer shape factor, H.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleTurbulent Boundary Layers on Centrifugal Compressor Blades: Prediction of the Effects of Surface Curvature and Rotation
    typeJournal Paper
    journal volume98
    journal issue3
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3448327
    journal fristpage374
    journal lastpage381
    identifier eissn1528-901X
    keywordsCompressors
    keywordsRotation
    keywordsBlades
    keywordsBoundary layer turbulence
    keywordsShapes
    keywordsFlow (Dynamics)
    keywordsSkin friction (Fluid dynamics)
    keywordsBoundary layers AND Rotors
    treeJournal of Fluids Engineering:;1976:;volume( 098 ):;issue: 003
    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
    yabeshDSpacePersian