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    Pressure Loss Coefficient of Impingement Cooled Leading Edge System of a Turbine Blade

    Source: Journal of Engineering for Gas Turbines and Power:;1976:;volume( 098 ):;issue: 004::page 554
    Author:
    D. K. Mukherjee
    DOI: 10.1115/1.3446236
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The pressure loss coefficient of an impingement cooled system similar to that often used to cool the leading edge of a turbine blade has been determined from model test. The influence of Reynolds number in the range tested is negligible. However, the influence of relative distance of the jet holes from the surface to be cooled is very significant.
    keyword(s): Pressure , Turbine blades AND Reynolds number ,
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      Pressure Loss Coefficient of Impingement Cooled Leading Edge System of a Turbine Blade

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    https://yetl.yabesh.ir/yetl1/handle/yetl/88550
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    contributor authorD. K. Mukherjee
    date accessioned2017-05-08T23:00:32Z
    date available2017-05-08T23:00:32Z
    date copyrightOctober, 1976
    date issued1976
    identifier issn1528-8919
    identifier otherJETPEZ-26728#554_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/88550
    description abstractThe pressure loss coefficient of an impingement cooled system similar to that often used to cool the leading edge of a turbine blade has been determined from model test. The influence of Reynolds number in the range tested is negligible. However, the influence of relative distance of the jet holes from the surface to be cooled is very significant.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePressure Loss Coefficient of Impingement Cooled Leading Edge System of a Turbine Blade
    typeJournal Paper
    journal volume98
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3446236
    journal fristpage554
    journal lastpage556
    identifier eissn0742-4795
    keywordsPressure
    keywordsTurbine blades AND Reynolds number
    treeJournal of Engineering for Gas Turbines and Power:;1976:;volume( 098 ):;issue: 004
    contenttypeFulltext
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