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    Effect of Streamline Curvature on Film Cooling

    Source: Journal of Engineering for Gas Turbines and Power:;1977:;volume( 099 ):;issue: 001::page 77
    Author:
    R. E. Mayle
    ,
    M. F. Blair
    ,
    D. A. Bailey
    ,
    F. C. Kopper
    DOI: 10.1115/1.3446255
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of streamline curvature on film cooling effectiveness are discussed. Experiments for air discharged through a slot and into a turbulent boundary layer along a flat, convex, and concave surface are described. Adiabatic wall effectiveness measurements on each surface for several blowing rates are presented. Boundary-layer velocity and temperature measurements are also presented for one of the blowing rates. Compared to the results for the flat surface, convex curvature is found to increase the adiabatic wall effectiveness whereas concave curvature is found to be detrimental.
    keyword(s): Cooling , Measurement , Temperature measurement , Boundary layers AND Boundary layer turbulence ,
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      Effect of Streamline Curvature on Film Cooling

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/89848
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorR. E. Mayle
    contributor authorM. F. Blair
    contributor authorD. A. Bailey
    contributor authorF. C. Kopper
    date accessioned2017-05-08T23:02:50Z
    date available2017-05-08T23:02:50Z
    date copyrightJanuary, 1977
    date issued1977
    identifier issn1528-8919
    identifier otherJETPEZ-26730#77_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/89848
    description abstractThe effects of streamline curvature on film cooling effectiveness are discussed. Experiments for air discharged through a slot and into a turbulent boundary layer along a flat, convex, and concave surface are described. Adiabatic wall effectiveness measurements on each surface for several blowing rates are presented. Boundary-layer velocity and temperature measurements are also presented for one of the blowing rates. Compared to the results for the flat surface, convex curvature is found to increase the adiabatic wall effectiveness whereas concave curvature is found to be detrimental.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffect of Streamline Curvature on Film Cooling
    typeJournal Paper
    journal volume99
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3446255
    journal fristpage77
    journal lastpage82
    identifier eissn0742-4795
    keywordsCooling
    keywordsMeasurement
    keywordsTemperature measurement
    keywordsBoundary layers AND Boundary layer turbulence
    treeJournal of Engineering for Gas Turbines and Power:;1977:;volume( 099 ):;issue: 001
    contenttypeFulltext
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