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    Effect of Acceleration on the Heat Transfer Coefficient on a Film-Cooled Surface

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 003::page 464
    Author:
    H. D. Ammari
    ,
    N. Hay
    ,
    D. Lampard
    DOI: 10.1115/1.2927897
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Results are presented of an experimental investigation into the influence of mainstream acceleration on the heat transfer coefficient downstream of injection through a row of 35 deg holes in a flat plate. A mass transfer analogue technique was used, with two uniform acceleration parameters, K ( = v(du∞ /dx)/u2 ∞ , of 1.9 × 10−6 and 5.0×10−6 in addition to the zero acceleration baseline case. Two injectants, air and carbon dioxide, were employed to give coolant-to-mainstream density ratios of 1.0 and 1.52, respectively. The blowing rate varied from 0.5 to 2.0. The heat transfer coefficient beneath the film decreased progressively as the acceleration increased, with maximum reductions from the zero acceleration datum case of about 27 percent. In the presence of acceleration, the heat transfer coefficient at a given blowing rate was dependent on the density ratio, an increase in the density ratio leading to a decrease in the heat transfer coefficient. An empirical correlation of the data over most of the range of densities and blowing rates of the experiments has been developed.
    keyword(s): Heat transfer coefficients , Density , Mass transfer , Coolants , Carbon dioxide AND Flat plates ,
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      Effect of Acceleration on the Heat Transfer Coefficient on a Film-Cooled Surface

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/109389
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    • Journal of Turbomachinery

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    contributor authorH. D. Ammari
    contributor authorN. Hay
    contributor authorD. Lampard
    date accessioned2017-05-08T23:36:56Z
    date available2017-05-08T23:36:56Z
    date copyrightJuly, 1991
    date issued1991
    identifier issn0889-504X
    identifier otherJOTUEI-28613#464_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109389
    description abstractResults are presented of an experimental investigation into the influence of mainstream acceleration on the heat transfer coefficient downstream of injection through a row of 35 deg holes in a flat plate. A mass transfer analogue technique was used, with two uniform acceleration parameters, K ( = v(du∞ /dx)/u2 ∞ , of 1.9 × 10−6 and 5.0×10−6 in addition to the zero acceleration baseline case. Two injectants, air and carbon dioxide, were employed to give coolant-to-mainstream density ratios of 1.0 and 1.52, respectively. The blowing rate varied from 0.5 to 2.0. The heat transfer coefficient beneath the film decreased progressively as the acceleration increased, with maximum reductions from the zero acceleration datum case of about 27 percent. In the presence of acceleration, the heat transfer coefficient at a given blowing rate was dependent on the density ratio, an increase in the density ratio leading to a decrease in the heat transfer coefficient. An empirical correlation of the data over most of the range of densities and blowing rates of the experiments has been developed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffect of Acceleration on the Heat Transfer Coefficient on a Film-Cooled Surface
    typeJournal Paper
    journal volume113
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2927897
    journal fristpage464
    journal lastpage471
    identifier eissn1528-8900
    keywordsHeat transfer coefficients
    keywordsDensity
    keywordsMass transfer
    keywordsCoolants
    keywordsCarbon dioxide AND Flat plates
    treeJournal of Turbomachinery:;1991:;volume( 113 ):;issue: 003
    contenttypeFulltext
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