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    Heat Transfer and Pressure Loss of Additively Manufactured Internal Cooling Channels With Various Shapes

    Source: Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 007::page 71011-1
    Author:
    Wildgoose, Alexander J.
    ,
    Thole, Karen A.
    DOI: 10.1115/1.4056775
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Additive manufacturing (AM) provides the ability to fabricate highly customized internal cooling passages that are relevant to gas turbine components. This experimental study examines the pressure loss and heat transfer performance of a range of fundamental channel shapes that were produced using direct metal laser sintering. Circular, hexagonal, pentagonal, elliptical, diamond, square, rectangular, trapezoidal, and triangular channel cross sections were investigated. To maintain the same convective surface area between shapes, the wetted perimeters of the channel cross sections were kept constant. Parallel computational fluid dynamic simulations were performed to understand the relationships in cooling performance between several channel shapes. Several characteristic length scales were evaluated to scale the pressure loss and heat transfer measurements. Among the channel shapes investigated, the diamond channel showed the lowest Nusselt number and friction factor. The pentagon exhibited a similar Nusselt number as the circular channel despite having a lower friction factor. There was no difference in scaling the friction factor or Nusselt number results of the different channel shapes between using the square root of cross-sectional area compared to hydraulic diameter as the characteristic length scale
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      Heat Transfer and Pressure Loss of Additively Manufactured Internal Cooling Channels With Various Shapes

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4291588
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    • Journal of Turbomachinery

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    contributor authorWildgoose, Alexander J.
    contributor authorThole, Karen A.
    date accessioned2023-08-16T18:11:30Z
    date available2023-08-16T18:11:30Z
    date copyright2/10/2023 12:00:00 AM
    date issued2023
    identifier issn0889-504X
    identifier otherturbo_145_7_071011.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4291588
    description abstractAdditive manufacturing (AM) provides the ability to fabricate highly customized internal cooling passages that are relevant to gas turbine components. This experimental study examines the pressure loss and heat transfer performance of a range of fundamental channel shapes that were produced using direct metal laser sintering. Circular, hexagonal, pentagonal, elliptical, diamond, square, rectangular, trapezoidal, and triangular channel cross sections were investigated. To maintain the same convective surface area between shapes, the wetted perimeters of the channel cross sections were kept constant. Parallel computational fluid dynamic simulations were performed to understand the relationships in cooling performance between several channel shapes. Several characteristic length scales were evaluated to scale the pressure loss and heat transfer measurements. Among the channel shapes investigated, the diamond channel showed the lowest Nusselt number and friction factor. The pentagon exhibited a similar Nusselt number as the circular channel despite having a lower friction factor. There was no difference in scaling the friction factor or Nusselt number results of the different channel shapes between using the square root of cross-sectional area compared to hydraulic diameter as the characteristic length scale
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHeat Transfer and Pressure Loss of Additively Manufactured Internal Cooling Channels With Various Shapes
    typeJournal Paper
    journal volume145
    journal issue7
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4056775
    journal fristpage71011-1
    journal lastpage71011-11
    page11
    treeJournal of Turbomachinery:;2023:;volume( 145 ):;issue: 007
    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
    yabeshDSpacePersian