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    Flow and Heat Transfer in a Ribbed Converging-Diverging U-Duct Under Rotating and Non-Rotating Conditions

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 003::page 31005-1
    Author:
    Kim, Wanjae
    ,
    Shih, Tom I-P.
    ,
    Dalton, Richard P.
    ,
    Bryden, Kenneth Mark
    ,
    Chang, Sung Yong
    ,
    Park, Gyu Sang
    DOI: 10.1115/1.4066567
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A numerical study based on steady Reynolds-averaged-Navier–Stokes (RANS) with the shear stress transport (SST) turbulence model was performed to investigate the flow and heat transfer in a ribbed U-duct with a rectangular cross section that converges linearly in the radially outward direction and diverges linearly in the radially inward direction under rotating and nonrotating conditions. Parameters examined include rotation number (Roi = 0, 0.0219, 0.0336, 0.0731), Reynolds number (Rei = 46,000, 100,000, and 154,000), and the duct's taper angle (α = 0 deg and 1.41 deg) under conditions relevant to gas turbines used for electric power generation. Results obtained show that increasing the taper angle from 0 deg to 1.41 deg, which appears negligibly small, significantly increases both the friction coefficient and the Nusselt number whether there is rotation or not. With rotation at Roi = 0.0336 and Rei = 100,000, the maximum increase in the average friction coefficient and Nusselt number was found to be 41.7% and 36.6%, respectively. Without rotation at Rei = 46,000, those are 11.5% and 14.7%, respectively.
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      Flow and Heat Transfer in a Ribbed Converging-Diverging U-Duct Under Rotating and Non-Rotating Conditions

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4305519
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    • Journal of Turbomachinery

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    contributor authorKim, Wanjae
    contributor authorShih, Tom I-P.
    contributor authorDalton, Richard P.
    contributor authorBryden, Kenneth Mark
    contributor authorChang, Sung Yong
    contributor authorPark, Gyu Sang
    date accessioned2025-04-21T10:06:46Z
    date available2025-04-21T10:06:46Z
    date copyright10/14/2024 12:00:00 AM
    date issued2024
    identifier issn0889-504X
    identifier otherturbo_147_3_031005.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4305519
    description abstractA numerical study based on steady Reynolds-averaged-Navier–Stokes (RANS) with the shear stress transport (SST) turbulence model was performed to investigate the flow and heat transfer in a ribbed U-duct with a rectangular cross section that converges linearly in the radially outward direction and diverges linearly in the radially inward direction under rotating and nonrotating conditions. Parameters examined include rotation number (Roi = 0, 0.0219, 0.0336, 0.0731), Reynolds number (Rei = 46,000, 100,000, and 154,000), and the duct's taper angle (α = 0 deg and 1.41 deg) under conditions relevant to gas turbines used for electric power generation. Results obtained show that increasing the taper angle from 0 deg to 1.41 deg, which appears negligibly small, significantly increases both the friction coefficient and the Nusselt number whether there is rotation or not. With rotation at Roi = 0.0336 and Rei = 100,000, the maximum increase in the average friction coefficient and Nusselt number was found to be 41.7% and 36.6%, respectively. Without rotation at Rei = 46,000, those are 11.5% and 14.7%, respectively.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFlow and Heat Transfer in a Ribbed Converging-Diverging U-Duct Under Rotating and Non-Rotating Conditions
    typeJournal Paper
    journal volume147
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4066567
    journal fristpage31005-1
    journal lastpage31005-15
    page15
    treeJournal of Turbomachinery:;2024:;volume( 147 ):;issue: 003
    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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