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    Effects of Wakes on Blade Endwall Heat Transfer in High Turbulence Intensity

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 002
    Author:
    Park, Sehjin
    ,
    Sohn, Ho-Seong
    ,
    Cho, Hyung Hee
    ,
    Moon, Hee Koo
    ,
    Han, Yang Seok
    ,
    Ueda, Osamu
    DOI: 10.1115/1.4045335
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed heat transfer measurements are necessary to protect the blades under harsh and complex flow conditions. Therefore, this study investigated the heat transfer characteristics on the blade endwall under flow conditions that simulate high turbulence intensity of the main flow and the generation of wakes by the trailing edge of the vane. The endwall heat transfer was measured using the naphthalene sublimation method. A turbulence generating grid was installed in a linear cascade to simulate the main flow with high turbulence intensity and a wake generator with a rod bundle was used to simulate the wakes generated by the trailing edge of the vane. In the case of high turbulence intensity without wakes, the main flow with high turbulence intensity (turbulence intensity, T.I = 7.5%) had little impact on the effect of the horseshoe vortex and passage vortex on the heat transfer characteristics. However, increasing turbulence caused the endwall heat transfer to decrease near the pressure side of the blade and increase near the suction side of the blade. On the other hand, the wakes resulted in heat transfer characteristics similar to high turbulence intensity but decreased heat transfer by horseshoe vortex and passage vortex. The endwall heat transfer distributions were similar regardless of the turbulence intensity (T.I = 1.2% and 7.5%) in the cases with wakes (rod passing Strouhal number, S = 0.3). The flow condition of S = 0.3 has a more significant influence on the endwall heat transfer than that of T.I = 7.5%.
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      Effects of Wakes on Blade Endwall Heat Transfer in High Turbulence Intensity

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4273308
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    • Journal of Turbomachinery

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    contributor authorPark, Sehjin
    contributor authorSohn, Ho-Seong
    contributor authorCho, Hyung Hee
    contributor authorMoon, Hee Koo
    contributor authorHan, Yang Seok
    contributor authorUeda, Osamu
    date accessioned2022-02-04T14:16:03Z
    date available2022-02-04T14:16:03Z
    date copyright2020/01/24/
    date issued2020
    identifier issn0889-504X
    identifier otherturbo_142_2_021002.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4273308
    description abstractDetailed heat transfer measurements are necessary to protect the blades under harsh and complex flow conditions. Therefore, this study investigated the heat transfer characteristics on the blade endwall under flow conditions that simulate high turbulence intensity of the main flow and the generation of wakes by the trailing edge of the vane. The endwall heat transfer was measured using the naphthalene sublimation method. A turbulence generating grid was installed in a linear cascade to simulate the main flow with high turbulence intensity and a wake generator with a rod bundle was used to simulate the wakes generated by the trailing edge of the vane. In the case of high turbulence intensity without wakes, the main flow with high turbulence intensity (turbulence intensity, T.I = 7.5%) had little impact on the effect of the horseshoe vortex and passage vortex on the heat transfer characteristics. However, increasing turbulence caused the endwall heat transfer to decrease near the pressure side of the blade and increase near the suction side of the blade. On the other hand, the wakes resulted in heat transfer characteristics similar to high turbulence intensity but decreased heat transfer by horseshoe vortex and passage vortex. The endwall heat transfer distributions were similar regardless of the turbulence intensity (T.I = 1.2% and 7.5%) in the cases with wakes (rod passing Strouhal number, S = 0.3). The flow condition of S = 0.3 has a more significant influence on the endwall heat transfer than that of T.I = 7.5%.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffects of Wakes on Blade Endwall Heat Transfer in High Turbulence Intensity
    typeJournal Paper
    journal volume142
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4045335
    page21002
    treeJournal of Turbomachinery:;2020:;volume( 142 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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