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    A Theory for Boundary Layer Growth on the Blades of a Radial Impeller Including Endwall Influence

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 003::page 403
    Author:
    H. Ekerol
    ,
    J. W. Railly
    DOI: 10.1115/1.3227429
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental data on the wall shear stress of a turbulent boundary layer on the suction side of a blade in a two-dimensional radial impeller is compared with the predictions of a theory which takes account of rotation and curvature effects as well as the three-dimensional influence of the endwall boundary layers. The latter influence is assumed to arise mainly from mainstream distortion due to secondary flows created by the endwall boundary layers, and it appears as an extra term in the momentum integral equation of the blade boundary layer which has allowance, also for the Coriolis effect; an appropriate form of the Head entrainment equation is derived to obtain a solution and a comparison made. A comparison of the above theory with the Patankar-Spalding prediction method, modified to include the effects of Coriolis (including mixing length modification, MLM), is also made.
    keyword(s): Boundary layers , Blades , Impellers , Shear (Mechanics) , Clearances (Engineering) , Boundary layer turbulence , Equations , Integral equations , Momentum , Rotation , Flow (Dynamics) , Coriolis force , Suction AND Stress ,
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      A Theory for Boundary Layer Growth on the Blades of a Radial Impeller Including Endwall Influence

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/97043
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorH. Ekerol
    contributor authorJ. W. Railly
    date accessioned2017-05-08T23:15:25Z
    date available2017-05-08T23:15:25Z
    date copyrightJuly, 1983
    date issued1983
    identifier issn1528-8919
    identifier otherJETPEZ-26783#403_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/97043
    description abstractExperimental data on the wall shear stress of a turbulent boundary layer on the suction side of a blade in a two-dimensional radial impeller is compared with the predictions of a theory which takes account of rotation and curvature effects as well as the three-dimensional influence of the endwall boundary layers. The latter influence is assumed to arise mainly from mainstream distortion due to secondary flows created by the endwall boundary layers, and it appears as an extra term in the momentum integral equation of the blade boundary layer which has allowance, also for the Coriolis effect; an appropriate form of the Head entrainment equation is derived to obtain a solution and a comparison made. A comparison of the above theory with the Patankar-Spalding prediction method, modified to include the effects of Coriolis (including mixing length modification, MLM), is also made.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Theory for Boundary Layer Growth on the Blades of a Radial Impeller Including Endwall Influence
    typeJournal Paper
    journal volume105
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3227429
    journal fristpage403
    journal lastpage411
    identifier eissn0742-4795
    keywordsBoundary layers
    keywordsBlades
    keywordsImpellers
    keywordsShear (Mechanics)
    keywordsClearances (Engineering)
    keywordsBoundary layer turbulence
    keywordsEquations
    keywordsIntegral equations
    keywordsMomentum
    keywordsRotation
    keywordsFlow (Dynamics)
    keywordsCoriolis force
    keywordsSuction AND Stress
    treeJournal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 003
    contenttypeFulltext
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