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    An Approximate Analysis of Gaseous Film Cooling With Constant Fluid Properties

    Source: Journal of Engineering for Gas Turbines and Power:;1971:;volume( 093 ):;issue: 004::page 357
    Author:
    J. L. Gaddis
    ,
    J. P. Lamb
    DOI: 10.1115/1.3445594
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Presented herein is an analysis of the velocity and temperature fields for a constant-property turbulent flow downstream of a step-type injection slot. The flow field is considered to be in a developing condition and is quantitatively described with a two-layer model in which the outer region is dominated by large-scale turbulence typical of free shear layers. An approximate solution for the outer region is appropriately joined to an inner profile determined by the usual “law of the wall” so that one obtains both the correct profile shape for the complete viscous layer and the proper spatial positioning of velocity and temperature profiles. The latter are obtained from a linearized energy equation with unit turbulent Prandtl number and are employed, along with the velocity profiles, in an energy balance to determine the longitudinal variation of the effectiveness. A successful calculation technique is discussed and typical results are compared with existing experimental data. The analysis is shown to be competitive in accuracy with available correlation expressions while also yielding considerable insight into the interaction of various design parameters.
    keyword(s): Flow (Dynamics) , Temperature , Cooling , Fluids , Turbulence , Energy budget (Physics) , Shear (Mechanics) , Design , Equations , Prandtl number , Shapes AND Temperature profiles ,
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      An Approximate Analysis of Gaseous Film Cooling With Constant Fluid Properties

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/150734
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorJ. L. Gaddis
    contributor authorJ. P. Lamb
    date accessioned2017-05-09T00:55:54Z
    date available2017-05-09T00:55:54Z
    date copyrightOctober, 1971
    date issued1971
    identifier issn1528-8919
    identifier otherJETPEZ-26696#357_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/150734
    description abstractPresented herein is an analysis of the velocity and temperature fields for a constant-property turbulent flow downstream of a step-type injection slot. The flow field is considered to be in a developing condition and is quantitatively described with a two-layer model in which the outer region is dominated by large-scale turbulence typical of free shear layers. An approximate solution for the outer region is appropriately joined to an inner profile determined by the usual “law of the wall” so that one obtains both the correct profile shape for the complete viscous layer and the proper spatial positioning of velocity and temperature profiles. The latter are obtained from a linearized energy equation with unit turbulent Prandtl number and are employed, along with the velocity profiles, in an energy balance to determine the longitudinal variation of the effectiveness. A successful calculation technique is discussed and typical results are compared with existing experimental data. The analysis is shown to be competitive in accuracy with available correlation expressions while also yielding considerable insight into the interaction of various design parameters.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Approximate Analysis of Gaseous Film Cooling With Constant Fluid Properties
    typeJournal Paper
    journal volume93
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3445594
    journal fristpage357
    journal lastpage365
    identifier eissn0742-4795
    keywordsFlow (Dynamics)
    keywordsTemperature
    keywordsCooling
    keywordsFluids
    keywordsTurbulence
    keywordsEnergy budget (Physics)
    keywordsShear (Mechanics)
    keywordsDesign
    keywordsEquations
    keywordsPrandtl number
    keywordsShapes AND Temperature profiles
    treeJournal of Engineering for Gas Turbines and Power:;1971:;volume( 093 ):;issue: 004
    contenttypeFulltext
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