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    Revisiting Dimensionless Parameters Quantifying Film Cooling

    Source: Journal of Turbomachinery:;2025:;volume( 147 ):;issue: 010::page 101004-1
    Author:
    Lee, Chien-Shing
    ,
    Shih, Tom I-P.
    ,
    Straub, Douglas
    ,
    Weber, Justin
    DOI: 10.1115/1.4067931
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The adiabatic effectiveness of film cooling (η) has been characterized by the density (DRh) and blowing (BRh) ratios. In this study, dimensional analysis and computations based on Reynolds-averaged Navier–Stokes (RANS) were performed to identify and examine parameters needed to quantify η, where film cooling is crossflow-fed instead of plenum-fed. The test problem studied is film cooling of a flat plate, where the cooling air, issuing through 30-deg inclined circular holes, is fed from a cooling channel whose flow direction is perpendicular to the direction of the hot-gas flow. For this test problem, dimensional analysis shows an additional blowing ratio is needed, denoted as BRc, to quantify η, where BRc is the ratio of the mass flux through the film-cooling hole to the mass flux in the cooling channel upstream of the film-cooling hole. RANS results with and without conjugate heat transfer obtained by varying the mass flowrate in the cooling channel, while keeping DRh and BRh constant (DRh = 1.9 and BRh was either 0.75 or 1.0), show reducing mass flowrate in the cooling channel by one-half, which doubles BRc (from 2.6 to 5.2) to slightly affect the discharge coefficient through the film-cooling holes (<5%) but up to 85% on laterally averaged η and up to 25% on overall cooling effectiveness. RANS results also show the flow mechanisms induced by BRc that affect η. The RANS results of this study were validated by comparing with experimental data.
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      Revisiting Dimensionless Parameters Quantifying Film Cooling

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    contributor authorLee, Chien-Shing
    contributor authorShih, Tom I-P.
    contributor authorStraub, Douglas
    contributor authorWeber, Justin
    date accessioned2025-08-20T09:14:47Z
    date available2025-08-20T09:14:47Z
    date copyright2/28/2025 12:00:00 AM
    date issued2025
    identifier issn0889-504X
    identifier otherturbo-24-1389.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4307969
    description abstractThe adiabatic effectiveness of film cooling (η) has been characterized by the density (DRh) and blowing (BRh) ratios. In this study, dimensional analysis and computations based on Reynolds-averaged Navier–Stokes (RANS) were performed to identify and examine parameters needed to quantify η, where film cooling is crossflow-fed instead of plenum-fed. The test problem studied is film cooling of a flat plate, where the cooling air, issuing through 30-deg inclined circular holes, is fed from a cooling channel whose flow direction is perpendicular to the direction of the hot-gas flow. For this test problem, dimensional analysis shows an additional blowing ratio is needed, denoted as BRc, to quantify η, where BRc is the ratio of the mass flux through the film-cooling hole to the mass flux in the cooling channel upstream of the film-cooling hole. RANS results with and without conjugate heat transfer obtained by varying the mass flowrate in the cooling channel, while keeping DRh and BRh constant (DRh = 1.9 and BRh was either 0.75 or 1.0), show reducing mass flowrate in the cooling channel by one-half, which doubles BRc (from 2.6 to 5.2) to slightly affect the discharge coefficient through the film-cooling holes (<5%) but up to 85% on laterally averaged η and up to 25% on overall cooling effectiveness. RANS results also show the flow mechanisms induced by BRc that affect η. The RANS results of this study were validated by comparing with experimental data.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleRevisiting Dimensionless Parameters Quantifying Film Cooling
    typeJournal Paper
    journal volume147
    journal issue10
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4067931
    journal fristpage101004-1
    journal lastpage101004-14
    page14
    treeJournal of Turbomachinery:;2025:;volume( 147 ):;issue: 010
    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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