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    Adiabatic Wall Temperature and Heat Transfer Downstream of Injection Through Two Rows of Holes

    Source: Journal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 002::page 303
    Author:
    M. Y. Jabbari
    ,
    R. J. Goldstein
    DOI: 10.1115/1.3446350
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Results of an experimental investigation of film cooling and heat transfer following injection through two staggered rows of holes are reported. The two staggered rows are considerably more effective in protecting the wall than a single row. The film cooling effectiveness at locations beyond about 30-hole dia downstream of injection is laterally uniform. The heat transfer coefficient is within a few percent of that without injection at low blowing rates, but it increases rapidly as the blowing rate increases above unity.
    keyword(s): Heat transfer , Wall temperature , Cooling AND Heat transfer coefficients ,
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      Adiabatic Wall Temperature and Heat Transfer Downstream of Injection Through Two Rows of Holes

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/91003
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorM. Y. Jabbari
    contributor authorR. J. Goldstein
    date accessioned2017-05-08T23:04:44Z
    date available2017-05-08T23:04:44Z
    date copyrightApril, 1978
    date issued1978
    identifier issn1528-8919
    identifier otherJETPEZ-26740#303_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/91003
    description abstractResults of an experimental investigation of film cooling and heat transfer following injection through two staggered rows of holes are reported. The two staggered rows are considerably more effective in protecting the wall than a single row. The film cooling effectiveness at locations beyond about 30-hole dia downstream of injection is laterally uniform. The heat transfer coefficient is within a few percent of that without injection at low blowing rates, but it increases rapidly as the blowing rate increases above unity.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAdiabatic Wall Temperature and Heat Transfer Downstream of Injection Through Two Rows of Holes
    typeJournal Paper
    journal volume100
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3446350
    journal fristpage303
    journal lastpage307
    identifier eissn0742-4795
    keywordsHeat transfer
    keywordsWall temperature
    keywordsCooling AND Heat transfer coefficients
    treeJournal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 002
    contenttypeFulltext
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