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    Effect of Weak Swirling Flow on Film Cooling Performance

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 004::page 786
    Author:
    C. Gau
    ,
    W. B. Hwang
    DOI: 10.1115/1.2927722
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments have been performed in a large circular pipe to study and obtain the film cooling effectivenesses with the presence of weak swirling flow in the mainstream. The swirling flow is generated by a flat vane swirler situated upstream. Cooling film is injected from an annular slot formed by the pipe wall and the circular cover plate. The radial temperature distribution measurements at several axial locations were used to infer the rate of mixing of film jet with swirling flow. The swirl number, which increases with turbulence intensity and swirl velocity in the mainstream, can significantly increase the mixing rate of film jet with swirl flow and decrease the film cooling effectiveness. During the course of the experiments, the blowing ratio ranged from 0.5 to 1.75 and the swirl number ranged from 0 to 0.6. Correlation equations for the film cooling effectiveness, which account for the effect of swirling flow, are obtained.
    keyword(s): Cooling , Swirling flow , Pipes , Equations , Measurement , Turbulence , Temperature distribution AND Flow (Dynamics) ,
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      Effect of Weak Swirling Flow on Film Cooling Performance

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    http://yetl.yabesh.ir/yetl1/handle/yetl/107706
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    contributor authorC. Gau
    contributor authorW. B. Hwang
    date accessioned2017-05-08T23:34:04Z
    date available2017-05-08T23:34:04Z
    date copyrightOctober, 1990
    date issued1990
    identifier issn0889-504X
    identifier otherJOTUEI-28606#786_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107706
    description abstractExperiments have been performed in a large circular pipe to study and obtain the film cooling effectivenesses with the presence of weak swirling flow in the mainstream. The swirling flow is generated by a flat vane swirler situated upstream. Cooling film is injected from an annular slot formed by the pipe wall and the circular cover plate. The radial temperature distribution measurements at several axial locations were used to infer the rate of mixing of film jet with swirling flow. The swirl number, which increases with turbulence intensity and swirl velocity in the mainstream, can significantly increase the mixing rate of film jet with swirl flow and decrease the film cooling effectiveness. During the course of the experiments, the blowing ratio ranged from 0.5 to 1.75 and the swirl number ranged from 0 to 0.6. Correlation equations for the film cooling effectiveness, which account for the effect of swirling flow, are obtained.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffect of Weak Swirling Flow on Film Cooling Performance
    typeJournal Paper
    journal volume112
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2927722
    journal fristpage786
    journal lastpage791
    identifier eissn1528-8900
    keywordsCooling
    keywordsSwirling flow
    keywordsPipes
    keywordsEquations
    keywordsMeasurement
    keywordsTurbulence
    keywordsTemperature distribution AND Flow (Dynamics)
    treeJournal of Turbomachinery:;1990:;volume( 112 ):;issue: 004
    contenttypeFulltext
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