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    The Optimal Distribution of Pin Fins for Blade Tip Cap Underside Cooling

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 001::page 11002
    Author:
    Ledezma, Gustavo A.
    ,
    Bunker, Ronald S.
    DOI: 10.1115/1.4028290
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This article presents a geometric optimization study to maximize the total heat transfer rate between an array of discrete pin fins and the surrounding serpentine cooling flow. The fins are installed on the tip cap underside of a highpressure turbine blade (HPTB) model. The study has three parts. In the first, the numerical model is validated against experimental data obtained with liquid crystal thermography. In the second part, the heat and fluid flow performance of the pin fin assembly is simulated numerically, using RANS turbulence models in the range 25,000 < Re < 100,000 and Pr ∼ 0.7. The effect of varying the spacing and the tip cap boundary condition is investigated. In the last part of the study, it is shown that the optimal spacing between the pin fins can be correlated following the same theoretical arguments derived in the previous investigations that used simpler geometries.
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      The Optimal Distribution of Pin Fins for Blade Tip Cap Underside Cooling

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    http://yetl.yabesh.ir/yetl1/handle/yetl/159870
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    contributor authorLedezma, Gustavo A.
    contributor authorBunker, Ronald S.
    date accessioned2017-05-09T01:24:19Z
    date available2017-05-09T01:24:19Z
    date issued2015
    identifier issn0889-504X
    identifier otherturbo_137_01_011002.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/159870
    description abstractThis article presents a geometric optimization study to maximize the total heat transfer rate between an array of discrete pin fins and the surrounding serpentine cooling flow. The fins are installed on the tip cap underside of a highpressure turbine blade (HPTB) model. The study has three parts. In the first, the numerical model is validated against experimental data obtained with liquid crystal thermography. In the second part, the heat and fluid flow performance of the pin fin assembly is simulated numerically, using RANS turbulence models in the range 25,000 < Re < 100,000 and Pr ∼ 0.7. The effect of varying the spacing and the tip cap boundary condition is investigated. In the last part of the study, it is shown that the optimal spacing between the pin fins can be correlated following the same theoretical arguments derived in the previous investigations that used simpler geometries.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Optimal Distribution of Pin Fins for Blade Tip Cap Underside Cooling
    typeJournal Paper
    journal volume137
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4028290
    journal fristpage11002
    journal lastpage11002
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2015:;volume( 137 ):;issue: 001
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian