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    Impingement/Effusion Cooling: The Influence of the Number of Impingement Holes and Pressure Loss on the Heat Transfer Coefficient

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 003::page 467
    Author:
    A. M. Al Dabagh
    ,
    G. E. Andrews
    ,
    R. A. A. Abdul Husain
    ,
    C. I. Husain
    ,
    A. Nazari
    ,
    J. Wu
    DOI: 10.1115/1.2927682
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Measurements of the overall heat transfer coefficient within an impingement/effusion cooled wall are presented. The FLUENT CFD computer code has been applied to the internal aerodynamics to demonstrate the importance of internal recirculation in the impingement gap. This generates a convective heat transfer to the impingement jet. Measurements of this heat transfer plate coefficient are presented that show it to be approximately half of the impingement/effusion heat transfer coefficient. The influence of the relative pressure loss or X/D between the impingement and effusion walls was investigated, for an effusion X/D of 4.67 and a Z of 8 mm, and shown to be only significant at high G where a reduction in h of 20 percent occurred. Increasing the number of holes N in the impingement/effusion array at a constant Z of 8 mm reduced h by 20 percent, mainly due to the higher Z/D for the smaller holes at high N. Reduced numbers of impingement holes relative to the effusion holes, in a ratio of 1 to 4, were shown to have a small influence on h with a maximum reduction in h of 20 percent at high G and a negligible effect at low G.
    keyword(s): Cooling , Pressure , Heat transfer coefficients , Measurement , Computational fluid dynamics , Convection , Computers , Aerodynamics AND Heat transfer ,
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      Impingement/Effusion Cooling: The Influence of the Number of Impingement Holes and Pressure Loss on the Heat Transfer Coefficient

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/107737
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    • Journal of Turbomachinery

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    contributor authorA. M. Al Dabagh
    contributor authorG. E. Andrews
    contributor authorR. A. A. Abdul Husain
    contributor authorC. I. Husain
    contributor authorA. Nazari
    contributor authorJ. Wu
    date accessioned2017-05-08T23:34:06Z
    date available2017-05-08T23:34:06Z
    date copyrightJuly, 1990
    date issued1990
    identifier issn0889-504X
    identifier otherJOTUEI-28604#467_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107737
    description abstractMeasurements of the overall heat transfer coefficient within an impingement/effusion cooled wall are presented. The FLUENT CFD computer code has been applied to the internal aerodynamics to demonstrate the importance of internal recirculation in the impingement gap. This generates a convective heat transfer to the impingement jet. Measurements of this heat transfer plate coefficient are presented that show it to be approximately half of the impingement/effusion heat transfer coefficient. The influence of the relative pressure loss or X/D between the impingement and effusion walls was investigated, for an effusion X/D of 4.67 and a Z of 8 mm, and shown to be only significant at high G where a reduction in h of 20 percent occurred. Increasing the number of holes N in the impingement/effusion array at a constant Z of 8 mm reduced h by 20 percent, mainly due to the higher Z/D for the smaller holes at high N. Reduced numbers of impingement holes relative to the effusion holes, in a ratio of 1 to 4, were shown to have a small influence on h with a maximum reduction in h of 20 percent at high G and a negligible effect at low G.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleImpingement/Effusion Cooling: The Influence of the Number of Impingement Holes and Pressure Loss on the Heat Transfer Coefficient
    typeJournal Paper
    journal volume112
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2927682
    journal fristpage467
    journal lastpage476
    identifier eissn1528-8900
    keywordsCooling
    keywordsPressure
    keywordsHeat transfer coefficients
    keywordsMeasurement
    keywordsComputational fluid dynamics
    keywordsConvection
    keywordsComputers
    keywordsAerodynamics AND Heat transfer
    treeJournal of Turbomachinery:;1990:;volume( 112 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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