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    Performance Evaluation of a Novel Film-Cooling Hole

    Source: Journal of Heat Transfer:;2012:;volume( 134 ):;issue: 010::page 101702
    Author:
    Ki-Don Lee
    ,
    Kwang-Yong Kim
    DOI: 10.1115/1.4006752
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a numerical investigation of the film-cooling performance of a novel film-cooling hole in comparison with a fan-shaped hole. The novel shaped hole is designed to increase the lateral spreading of coolant on the cooling surface. The film-cooling performance of the novel shaped hole is evaluated at a density ratio of 1.75 and the range of the blowing ratio of 0.5–2.5. The simulations were performed using three-dimensional Reynolds-averaged Navier–Stokes analysis with the SST k-ω model. The numerical results for the fan-shaped hole show very good agreement with the experimental data. For the blowing ratio of 0.5, the novel shaped film-cooling hole shows a similar cooling performance as the fan-shaped hole. However, as the blowing ratio increases, the novel shaped hole shows greatly improved lateral spreading of the coolant and the cooling performance in terms of the film-cooling effectiveness in comparison with the fan-shaped hole.
    keyword(s): Cooling AND Coolants ,
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      Performance Evaluation of a Novel Film-Cooling Hole

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    http://yetl.yabesh.ir/yetl1/handle/yetl/149337
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    contributor authorKi-Don Lee
    contributor authorKwang-Yong Kim
    date accessioned2017-05-09T00:51:57Z
    date available2017-05-09T00:51:57Z
    date copyrightOctober, 2012
    date issued2012
    identifier issn0022-1481
    identifier otherJHTRAO-926055#101702_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/149337
    description abstractThis paper presents a numerical investigation of the film-cooling performance of a novel film-cooling hole in comparison with a fan-shaped hole. The novel shaped hole is designed to increase the lateral spreading of coolant on the cooling surface. The film-cooling performance of the novel shaped hole is evaluated at a density ratio of 1.75 and the range of the blowing ratio of 0.5–2.5. The simulations were performed using three-dimensional Reynolds-averaged Navier–Stokes analysis with the SST k-ω model. The numerical results for the fan-shaped hole show very good agreement with the experimental data. For the blowing ratio of 0.5, the novel shaped film-cooling hole shows a similar cooling performance as the fan-shaped hole. However, as the blowing ratio increases, the novel shaped hole shows greatly improved lateral spreading of the coolant and the cooling performance in terms of the film-cooling effectiveness in comparison with the fan-shaped hole.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePerformance Evaluation of a Novel Film-Cooling Hole
    typeJournal Paper
    journal volume134
    journal issue10
    journal titleJournal of Heat Transfer
    identifier doi10.1115/1.4006752
    journal fristpage101702
    identifier eissn1528-8943
    keywordsCooling AND Coolants
    treeJournal of Heat Transfer:;2012:;volume( 134 ):;issue: 010
    contenttypeFulltext
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