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    Heat Transfer in Rotating, Trailing Edge, Converging Channels With Partial Length Pin-Fins

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 006::page 061009-1
    Author:
    Sahin, Izzet
    ,
    Chen, I-Lun
    ,
    Wright, Lesley M.
    ,
    Han, Je-Chin
    ,
    Xu, Hongzhou
    ,
    Fox, Michael
    DOI: 10.1115/1.4050241
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the current study, the heat transfer and pressure drop characteristics of a rotating, partial pin-finned, cooling channel that has a trapezoidal cross section and converges from the hub to tip in both the streamwise and spanwise directions are experimentally investigated. To model the geometry of an internal trailing edge cooling passage, the channel is oriented with respect to the direction of rotation (β = 120 deg). Isolated copper plates are used to obtain regionally averaged heat transfer coefficients on the leading and trailing surfaces. Pressure drop is measured using pressure taps placed at the inlet and outlet of the channel. Utilizing Dp = 5 mm diameter pins, a staggered array is created. For this array, the streamwise pin-spacing, Sy/Dp = 2.1, was kept constant; however, the spanwise pin-spacing, Sx/Dp, was varied from the hub to tip between 3 and 2.6 due to the channel convergence. Experiments were conducted for two partial pin-fin sets having pin length-to-diameter ratios of Sz/Dp = 0.4 and 0.2. The rotation number was varied from 0 to 0.21 by ranging the inlet Reynolds number from 10,000 to 40,000 and rotation speed from 0 to 300 rpm. A significant decrease in pressure loss and a slight reduction in heat transfer enhancement are observed with the use of partial pin-fins compared with the previously reported full pin-fin converging channel study. This provides better thermal performances of the partial pin-fin arrays compared with the full pin-fin array, in the converging channels.
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      Heat Transfer in Rotating, Trailing Edge, Converging Channels With Partial Length Pin-Fins

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4277003
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    • Journal of Turbomachinery

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    contributor authorSahin, Izzet
    contributor authorChen, I-Lun
    contributor authorWright, Lesley M.
    contributor authorHan, Je-Chin
    contributor authorXu, Hongzhou
    contributor authorFox, Michael
    date accessioned2022-02-05T22:08:47Z
    date available2022-02-05T22:08:47Z
    date copyright4/8/2021 12:00:00 AM
    date issued2021
    identifier issn0889-504X
    identifier otherturbo_143_6_061009.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4277003
    description abstractIn the current study, the heat transfer and pressure drop characteristics of a rotating, partial pin-finned, cooling channel that has a trapezoidal cross section and converges from the hub to tip in both the streamwise and spanwise directions are experimentally investigated. To model the geometry of an internal trailing edge cooling passage, the channel is oriented with respect to the direction of rotation (β = 120 deg). Isolated copper plates are used to obtain regionally averaged heat transfer coefficients on the leading and trailing surfaces. Pressure drop is measured using pressure taps placed at the inlet and outlet of the channel. Utilizing Dp = 5 mm diameter pins, a staggered array is created. For this array, the streamwise pin-spacing, Sy/Dp = 2.1, was kept constant; however, the spanwise pin-spacing, Sx/Dp, was varied from the hub to tip between 3 and 2.6 due to the channel convergence. Experiments were conducted for two partial pin-fin sets having pin length-to-diameter ratios of Sz/Dp = 0.4 and 0.2. The rotation number was varied from 0 to 0.21 by ranging the inlet Reynolds number from 10,000 to 40,000 and rotation speed from 0 to 300 rpm. A significant decrease in pressure loss and a slight reduction in heat transfer enhancement are observed with the use of partial pin-fins compared with the previously reported full pin-fin converging channel study. This provides better thermal performances of the partial pin-fin arrays compared with the full pin-fin array, in the converging channels.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHeat Transfer in Rotating, Trailing Edge, Converging Channels With Partial Length Pin-Fins
    typeJournal Paper
    journal volume143
    journal issue6
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4050241
    journal fristpage061009-1
    journal lastpage061009-11
    page11
    treeJournal of Turbomachinery:;2021:;volume( 143 ):;issue: 006
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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