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    Experimental Study of the Three-Dimensional Flow Field in an Annular Turbine Nozzle Guidevane

    Source: Journal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;issue: 002::page 437
    Author:
    C. H. Sieverding
    ,
    W. Van Hove
    ,
    E. Boletis
    DOI: 10.1115/1.3239585
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The paper describes the experimental investigation of the three-dimensional flow through a low-speed, low aspect ratio, high turning annular turbine nozzel guide vane. The flow is explored by means of double-head, four-hole pressure probes in twelve axial planes from upstream to far downstream of the blade row. The results are presented under the form of contour plots and spanwise pitch-averaged distributions of losses, flow angles, and static pressure distributions. The concept of presenting the evolution of the endwall boundary layer under the form of streamwise and crossflow velocity components is discussed in detail.
    keyword(s): Nozzles , Turbines , Flow (Dynamics) , Pressure , Boundary layers , Blades AND Probes ,
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      Experimental Study of the Three-Dimensional Flow Field in an Annular Turbine Nozzle Guidevane

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/98449
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorC. H. Sieverding
    contributor authorW. Van Hove
    contributor authorE. Boletis
    date accessioned2017-05-08T23:17:51Z
    date available2017-05-08T23:17:51Z
    date copyrightApril, 1984
    date issued1984
    identifier issn1528-8919
    identifier otherJETPEZ-26604#437_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/98449
    description abstractThe paper describes the experimental investigation of the three-dimensional flow through a low-speed, low aspect ratio, high turning annular turbine nozzel guide vane. The flow is explored by means of double-head, four-hole pressure probes in twelve axial planes from upstream to far downstream of the blade row. The results are presented under the form of contour plots and spanwise pitch-averaged distributions of losses, flow angles, and static pressure distributions. The concept of presenting the evolution of the endwall boundary layer under the form of streamwise and crossflow velocity components is discussed in detail.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleExperimental Study of the Three-Dimensional Flow Field in an Annular Turbine Nozzle Guidevane
    typeJournal Paper
    journal volume106
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3239585
    journal fristpage437
    journal lastpage444
    identifier eissn0742-4795
    keywordsNozzles
    keywordsTurbines
    keywordsFlow (Dynamics)
    keywordsPressure
    keywordsBoundary layers
    keywordsBlades AND Probes
    treeJournal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;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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