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    Predictions of Endwall Losses and Secondary Flows in Axial Flow Turbine Cascades

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 002::page 229
    Author:
    O. P. Sharma
    ,
    T. L. Butler
    DOI: 10.1115/1.3262089
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the development of a semi-empirical model for estimating end-wall losses. The model has been developed from improved understanding of complex endwall secondary flows, acquired through review of flow visualization and pressure loss data for axial flow turbomachine cascades. The flow visualization data together with detailed measurements of viscous flow development through cascades have permitted more realistic interpretation of the classical secondary flow theories for axial turbomachine cascades. The re-interpreted secondary flow theories together with integral boundary layer concepts are used to formulate a calculation procedure for predicting losses due to the endwall secondary flows. The proposed model is evaluated against data from published literature and improved agreement between the data and predictions is demonstrated.
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      Predictions of Endwall Losses and Secondary Flows in Axial Flow Turbine Cascades

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    contributor authorO. P. Sharma
    contributor authorT. L. Butler
    date accessioned2017-05-08T23:26:04Z
    date available2017-05-08T23:26:04Z
    date copyrightApril, 1987
    date issued1987
    identifier issn0889-504X
    identifier otherJOTUEI-28583#229_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103243
    description abstractThis paper describes the development of a semi-empirical model for estimating end-wall losses. The model has been developed from improved understanding of complex endwall secondary flows, acquired through review of flow visualization and pressure loss data for axial flow turbomachine cascades. The flow visualization data together with detailed measurements of viscous flow development through cascades have permitted more realistic interpretation of the classical secondary flow theories for axial turbomachine cascades. The re-interpreted secondary flow theories together with integral boundary layer concepts are used to formulate a calculation procedure for predicting losses due to the endwall secondary flows. The proposed model is evaluated against data from published literature and improved agreement between the data and predictions is demonstrated.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePredictions of Endwall Losses and Secondary Flows in Axial Flow Turbine Cascades
    typeJournal Paper
    journal volume109
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.3262089
    journal fristpage229
    journal lastpage236
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;1987:;volume( 109 ):;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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