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    The Effects of Free-Stream Turbulence Intensity and Velocity Distribution on Heat Transfer to Curved Surfaces

    Source: Journal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 001::page 159
    Author:
    A. Brown
    ,
    R. C. Burton
    DOI: 10.1115/1.3446312
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes a novel method for measuring the local heat-transfer distribution over a curved surface. The effect of free-stream turbulence intensity, ranging in value from 0.016 to 0.092, on local heat transfer is investigated for a range of Reynolds numbers from 2.0 × 105 to 7.7 × 105 . The geometry of the rig was modified to consider three free-stream velocity distributions covering distributions currently in use on suction surfaces of turbine blades. The results are compared with other workers’ experimental results and with available prediction techniques for heat transfer in laminar and turbulent boundary layers. Special attention is paid to the region of boundary-layer transition.
    keyword(s): Heat transfer , Turbulence , Suction , Reynolds number , Turbine blades , Boundary layers , Boundary layer turbulence AND Geometry ,
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      The Effects of Free-Stream Turbulence Intensity and Velocity Distribution on Heat Transfer to Curved Surfaces

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/91038
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorA. Brown
    contributor authorR. C. Burton
    date accessioned2017-05-08T23:04:47Z
    date available2017-05-08T23:04:47Z
    date copyrightJanuary, 1978
    date issued1978
    identifier issn1528-8919
    identifier otherJETPEZ-26739#159_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/91038
    description abstractThis paper describes a novel method for measuring the local heat-transfer distribution over a curved surface. The effect of free-stream turbulence intensity, ranging in value from 0.016 to 0.092, on local heat transfer is investigated for a range of Reynolds numbers from 2.0 × 105 to 7.7 × 105 . The geometry of the rig was modified to consider three free-stream velocity distributions covering distributions currently in use on suction surfaces of turbine blades. The results are compared with other workers’ experimental results and with available prediction techniques for heat transfer in laminar and turbulent boundary layers. Special attention is paid to the region of boundary-layer transition.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Effects of Free-Stream Turbulence Intensity and Velocity Distribution on Heat Transfer to Curved Surfaces
    typeJournal Paper
    journal volume100
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3446312
    journal fristpage159
    journal lastpage168
    identifier eissn0742-4795
    keywordsHeat transfer
    keywordsTurbulence
    keywordsSuction
    keywordsReynolds number
    keywordsTurbine blades
    keywordsBoundary layers
    keywordsBoundary layer turbulence AND Geometry
    treeJournal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian