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    Improved Spatiotemporal Distributions of Sweeping Jet Film Cooling With a Shaped Exit Design

    Source: Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 003::page 31011-1
    Author:
    Wang, Kechen
    ,
    Zhou, Wenwu
    ,
    Wen, Xin
    ,
    Peng, Di
    ,
    Liu, Yingzheng
    DOI: 10.1115/1.4064078
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Sweeping jet (SJ) is a self-excited flow control device that can generate continuous and periodic flow, which makes it a promising geometry for film cooling. However, the cooling performance of current SJ configurations is not significantly better than that of 777-shaped holes. This paper presents two modified SJ configurations, named shaped SJ1 and shaped SJ2, which possess distinct shaped exit geometries. The spatiotemporal coolant distributions were comprehensively quantified for the 777-shaped hole, the compact SJ (with compact geometry), the shaped SJ1, and the shaped SJ2. The instantaneous cooling effectiveness distributions of the four configurations at blowing ratios (M) ranging from 0.5 to 3.0 were measured using the fast pressure-sensitive paint technique. The shaped SJ2 integrated the cooling characteristics of the 777-shaped hole and SJ. It maintained stability at a relatively low M, while began to oscillate when M was increased above 1.5. The shaped SJ design exhibited superior cooling effectiveness at both low and high M of 0.5 to 3.0. A proper orthogonal decomposition analysis and simulations illustrated the oscillation processes and flow structures within the SJ configuration. The shaped SJ2 showed a reduced outlet momentum and a more even distribution of film coverage than the 777-shaped hole, resulting in considerably improved cooling performance.
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      Improved Spatiotemporal Distributions of Sweeping Jet Film Cooling With a Shaped Exit Design

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    contributor authorWang, Kechen
    contributor authorZhou, Wenwu
    contributor authorWen, Xin
    contributor authorPeng, Di
    contributor authorLiu, Yingzheng
    date accessioned2024-04-24T22:50:04Z
    date available2024-04-24T22:50:04Z
    date copyright12/14/2023 12:00:00 AM
    date issued2023
    identifier issn0889-504X
    identifier otherturbo_146_3_031011.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4295953
    description abstractSweeping jet (SJ) is a self-excited flow control device that can generate continuous and periodic flow, which makes it a promising geometry for film cooling. However, the cooling performance of current SJ configurations is not significantly better than that of 777-shaped holes. This paper presents two modified SJ configurations, named shaped SJ1 and shaped SJ2, which possess distinct shaped exit geometries. The spatiotemporal coolant distributions were comprehensively quantified for the 777-shaped hole, the compact SJ (with compact geometry), the shaped SJ1, and the shaped SJ2. The instantaneous cooling effectiveness distributions of the four configurations at blowing ratios (M) ranging from 0.5 to 3.0 were measured using the fast pressure-sensitive paint technique. The shaped SJ2 integrated the cooling characteristics of the 777-shaped hole and SJ. It maintained stability at a relatively low M, while began to oscillate when M was increased above 1.5. The shaped SJ design exhibited superior cooling effectiveness at both low and high M of 0.5 to 3.0. A proper orthogonal decomposition analysis and simulations illustrated the oscillation processes and flow structures within the SJ configuration. The shaped SJ2 showed a reduced outlet momentum and a more even distribution of film coverage than the 777-shaped hole, resulting in considerably improved cooling performance.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleImproved Spatiotemporal Distributions of Sweeping Jet Film Cooling With a Shaped Exit Design
    typeJournal Paper
    journal volume146
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4064078
    journal fristpage31011-1
    journal lastpage31011-12
    page12
    treeJournal of Turbomachinery:;2023:;volume( 146 ):;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
    yabeshDSpacePersian