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    Full-Coverage Film Cooling—Part II: Heat Transfer Data and Numerical Simulation

    Source: Journal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 004::page 1006
    Author:
    M. E. Crawford
    ,
    W. M. Kays
    ,
    R. J. Moffat
    DOI: 10.1115/1.3230335
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental research into heat transfer from full-coverage film-cooled surfaces with three injection geometries was described in Part I. This part has two objectives. The first is to present a simple numerical procedure for simulation of heat transfer with full-coverage film cooling. The second objective is to present some of the Stanton number data that was used in Part I of the paper. The data chosen for presentation are the low-Reynolds number, heated-starting-length data for the three injection geometries with five-diameter hole spacing. Sample data sets with high blowing ratio and with ten-diameter hole spacing are also presented. The numerical procedure has been successfully applied to the Stanton number data sets.
    keyword(s): Heat transfer , Cooling , Computer simulation AND Simulation ,
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      Full-Coverage Film Cooling—Part II: Heat Transfer Data and Numerical Simulation

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/93208
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorM. E. Crawford
    contributor authorW. M. Kays
    contributor authorR. J. Moffat
    date accessioned2017-05-08T23:08:35Z
    date available2017-05-08T23:08:35Z
    date copyrightOctober, 1980
    date issued1980
    identifier issn1528-8919
    identifier otherJETPEZ-26762#1006_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/93208
    description abstractExperimental research into heat transfer from full-coverage film-cooled surfaces with three injection geometries was described in Part I. This part has two objectives. The first is to present a simple numerical procedure for simulation of heat transfer with full-coverage film cooling. The second objective is to present some of the Stanton number data that was used in Part I of the paper. The data chosen for presentation are the low-Reynolds number, heated-starting-length data for the three injection geometries with five-diameter hole spacing. Sample data sets with high blowing ratio and with ten-diameter hole spacing are also presented. The numerical procedure has been successfully applied to the Stanton number data sets.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFull-Coverage Film Cooling—Part II: Heat Transfer Data and Numerical Simulation
    typeJournal Paper
    journal volume102
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3230335
    journal fristpage1006
    journal lastpage1012
    identifier eissn0742-4795
    keywordsHeat transfer
    keywordsCooling
    keywordsComputer simulation AND Simulation
    treeJournal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 004
    contenttypeFulltext
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