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    An Experimental Convective Heat Transfer Investigation Around a Film-Cooled Gas Turbine Blade

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 003::page 497
    Author:
    C. Camci
    ,
    T. Arts
    DOI: 10.1115/1.2927685
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present paper deals with an experimental convective heat transfer investigation around a film-cooled, high-pressure gas turbine rotor blade mounted in a stationary, linear cascade arrangement. The measurements were performed in the von Karman Institute Isentropic Light Piston Compression Tube facility. The test blade was made of Macor glass ceramic and was instrumented with thin film gages. The coolant flow was ejected simultaneously through the leading edge (three rows of holes), the suction side (two rows of holes), and the pressure side (one row of holes). The effects of overall mass weight ratio, coolant to free-stream temperature ratio, and free-stream turbulence were successively investigated.
    keyword(s): Convection , Gas turbines , Blades , Coolants , Cascades (Fluid dynamics) , High pressure (Physics) , Rotors , Compression , Pistons , Weight (Mass) , Pressure , Thin films , Flow (Dynamics) , Temperature , Ceramics , Glass , Measurement , Gages , Turbulence AND Suction ,
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      An Experimental Convective Heat Transfer Investigation Around a Film-Cooled Gas Turbine Blade

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/107740
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    • Journal of Turbomachinery

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    contributor authorC. Camci
    contributor authorT. Arts
    date accessioned2017-05-08T23:34:06Z
    date available2017-05-08T23:34:06Z
    date copyrightJuly, 1990
    date issued1990
    identifier issn0889-504X
    identifier otherJOTUEI-28604#497_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107740
    description abstractThe present paper deals with an experimental convective heat transfer investigation around a film-cooled, high-pressure gas turbine rotor blade mounted in a stationary, linear cascade arrangement. The measurements were performed in the von Karman Institute Isentropic Light Piston Compression Tube facility. The test blade was made of Macor glass ceramic and was instrumented with thin film gages. The coolant flow was ejected simultaneously through the leading edge (three rows of holes), the suction side (two rows of holes), and the pressure side (one row of holes). The effects of overall mass weight ratio, coolant to free-stream temperature ratio, and free-stream turbulence were successively investigated.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Experimental Convective Heat Transfer Investigation Around a Film-Cooled Gas Turbine Blade
    typeJournal Paper
    journal volume112
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2927685
    journal fristpage497
    journal lastpage503
    identifier eissn1528-8900
    keywordsConvection
    keywordsGas turbines
    keywordsBlades
    keywordsCoolants
    keywordsCascades (Fluid dynamics)
    keywordsHigh pressure (Physics)
    keywordsRotors
    keywordsCompression
    keywordsPistons
    keywordsWeight (Mass)
    keywordsPressure
    keywordsThin films
    keywordsFlow (Dynamics)
    keywordsTemperature
    keywordsCeramics
    keywordsGlass
    keywordsMeasurement
    keywordsGages
    keywordsTurbulence AND Suction
    treeJournal of Turbomachinery:;1990:;volume( 112 ):;issue: 003
    contenttypeFulltext
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