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    Film Cooling Effectiveness in High-Turbulence Flow

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 003::page 479
    Author:
    G. W. Jumper
    ,
    R. B. Rivir
    ,
    W. C. Elrod
    DOI: 10.1115/1.2927899
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The mechanisms influencing film cooling effectiveness on a flat plate in high free-stream turbulence using a single row of 30 deg slant-hole injectors are examined. The primary area of focus is the area within 40 diameters downstream of injection. Of interest are blowing ratios for optimum film cooling effectiveness within 10 diameters downstream of injection, and the decay of film cooling effectiveness down the plate. Film cooling flow Reynolds numbers. Re, from 24,700 to 86,600 and free-stream turbulence intensities from 14 to 17 percent were examined. Changes in Reynolds number or free-stream turbulence broadened and increased the blowing ratios for optimum film cooling effectiveness. In comparison with tests conducted at 0.5 percent free-stream turbulence, higher free-stream turbulence causes a faster decay in film cooling effectiveness, or a reduction in the effective cooling length, and a reduction of the level of cooling effectiveness at the higher Reynolds numbers.
    keyword(s): Flow (Dynamics) , Cooling , Turbulence , Reynolds number , Ejectors , Flat plates AND Mechanisms ,
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      Film Cooling Effectiveness in High-Turbulence Flow

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/109393
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    • Journal of Turbomachinery

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    contributor authorG. W. Jumper
    contributor authorR. B. Rivir
    contributor authorW. C. Elrod
    date accessioned2017-05-08T23:36:57Z
    date available2017-05-08T23:36:57Z
    date copyrightJuly, 1991
    date issued1991
    identifier issn0889-504X
    identifier otherJOTUEI-28613#479_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109393
    description abstractThe mechanisms influencing film cooling effectiveness on a flat plate in high free-stream turbulence using a single row of 30 deg slant-hole injectors are examined. The primary area of focus is the area within 40 diameters downstream of injection. Of interest are blowing ratios for optimum film cooling effectiveness within 10 diameters downstream of injection, and the decay of film cooling effectiveness down the plate. Film cooling flow Reynolds numbers. Re, from 24,700 to 86,600 and free-stream turbulence intensities from 14 to 17 percent were examined. Changes in Reynolds number or free-stream turbulence broadened and increased the blowing ratios for optimum film cooling effectiveness. In comparison with tests conducted at 0.5 percent free-stream turbulence, higher free-stream turbulence causes a faster decay in film cooling effectiveness, or a reduction in the effective cooling length, and a reduction of the level of cooling effectiveness at the higher Reynolds numbers.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFilm Cooling Effectiveness in High-Turbulence Flow
    typeJournal Paper
    journal volume113
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2927899
    journal fristpage479
    journal lastpage483
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsCooling
    keywordsTurbulence
    keywordsReynolds number
    keywordsEjectors
    keywordsFlat plates AND Mechanisms
    treeJournal of Turbomachinery:;1991:;volume( 113 ):;issue: 003
    contenttypeFulltext
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