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    The Additive Nature of Film Cooling From Rows of Holes

    Source: Journal of Engineering for Gas Turbines and Power:;1976:;volume( 098 ):;issue: 004::page 457
    Author:
    J. F. Muska
    ,
    M. Suo
    ,
    R. W. Fish
    DOI: 10.1115/1.3446214
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A method of superposition which predicts the cumulative effect of film cooling has been described in the literature by Sellers. This method predicts the magnitude and extent of film cooling downstream of multiple injection stations by accounting for the effectiveness level from each upstream station individually. Sellers compared the method with results from multiple slots and good agreement was demonstrated. Because of the simplicity of the method it was proposed as a method to predict the cumulative effect of film cooling from rows of holes. To substantiate this, experiments were conducted with film cooling schemes on flat plates and airfoils. The results of these experiments demonstrate that the method is satisfactory for design of film cooled airfoils in the required range of geometries and coolant flows.
    keyword(s): Cooling , Airfoils , Flow (Dynamics) , Coolants , Design AND Flat plates ,
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      The Additive Nature of Film Cooling From Rows of Holes

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/88534
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorJ. F. Muska
    contributor authorM. Suo
    contributor authorR. W. Fish
    date accessioned2017-05-08T23:00:30Z
    date available2017-05-08T23:00:30Z
    date copyrightOctober, 1976
    date issued1976
    identifier issn1528-8919
    identifier otherJETPEZ-26728#457_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/88534
    description abstractA method of superposition which predicts the cumulative effect of film cooling has been described in the literature by Sellers. This method predicts the magnitude and extent of film cooling downstream of multiple injection stations by accounting for the effectiveness level from each upstream station individually. Sellers compared the method with results from multiple slots and good agreement was demonstrated. Because of the simplicity of the method it was proposed as a method to predict the cumulative effect of film cooling from rows of holes. To substantiate this, experiments were conducted with film cooling schemes on flat plates and airfoils. The results of these experiments demonstrate that the method is satisfactory for design of film cooled airfoils in the required range of geometries and coolant flows.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Additive Nature of Film Cooling From Rows of Holes
    typeJournal Paper
    journal volume98
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3446214
    journal fristpage457
    journal lastpage463
    identifier eissn0742-4795
    keywordsCooling
    keywordsAirfoils
    keywordsFlow (Dynamics)
    keywordsCoolants
    keywordsDesign AND Flat plates
    treeJournal of Engineering for Gas Turbines and Power:;1976:;volume( 098 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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