YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Behavior of a Coolant Film With Two Rows of Holes Along the Pressure Side of a High-Pressure Nozzle Guide Vane

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 003::page 512
    Author:
    T. Arts
    ,
    A. E. Bourguignon
    DOI: 10.1115/1.2927687
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The purpose of this paper is to quantify the influence on external convective heat transfer of a coolant film whose position varies along the pressure side of a high-pressure turbine nozzle guide vane. The measurements were performed in the short-duration Isentropic Light Piston Compression Tube facility of the von Karman Institute. The effects of external and internal flow are considered in terms of Mach number, Reynolds number, free-stream turbulence intensity, blowing rate, and coolant to free-stream temperature ratio. The way to evaluate these results in terms of film cooling efficiency and heat transfer coefficient is finally discussed.
    keyword(s): Pressure , Coolants , High pressure (Physics) , Nozzles , Turbines , Compression , Pistons , Heat transfer coefficients , Internal flow , Convection , Mach number , Temperature , Cooling , Measurement , Turbulence AND Reynolds number ,
    • Download: (1.380Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Behavior of a Coolant Film With Two Rows of Holes Along the Pressure Side of a High-Pressure Nozzle Guide Vane

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/107742
    Collections
    • Journal of Turbomachinery

    Show full item record

    contributor authorT. Arts
    contributor authorA. E. Bourguignon
    date accessioned2017-05-08T23:34:06Z
    date available2017-05-08T23:34:06Z
    date copyrightJuly, 1990
    date issued1990
    identifier issn0889-504X
    identifier otherJOTUEI-28604#512_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107742
    description abstractThe purpose of this paper is to quantify the influence on external convective heat transfer of a coolant film whose position varies along the pressure side of a high-pressure turbine nozzle guide vane. The measurements were performed in the short-duration Isentropic Light Piston Compression Tube facility of the von Karman Institute. The effects of external and internal flow are considered in terms of Mach number, Reynolds number, free-stream turbulence intensity, blowing rate, and coolant to free-stream temperature ratio. The way to evaluate these results in terms of film cooling efficiency and heat transfer coefficient is finally discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleBehavior of a Coolant Film With Two Rows of Holes Along the Pressure Side of a High-Pressure Nozzle Guide Vane
    typeJournal Paper
    journal volume112
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2927687
    journal fristpage512
    journal lastpage520
    identifier eissn1528-8900
    keywordsPressure
    keywordsCoolants
    keywordsHigh pressure (Physics)
    keywordsNozzles
    keywordsTurbines
    keywordsCompression
    keywordsPistons
    keywordsHeat transfer coefficients
    keywordsInternal flow
    keywordsConvection
    keywordsMach number
    keywordsTemperature
    keywordsCooling
    keywordsMeasurement
    keywordsTurbulence AND Reynolds number
    treeJournal of Turbomachinery:;1990:;volume( 112 ):;issue: 003
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian