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    Heat Transfer to an Airfoil in Oscillating Flow

    Source: Journal of Engineering for Gas Turbines and Power:;1971:;volume( 093 ):;issue: 004::page 461
    Author:
    J. A. Miller
    ,
    P. F. Pucci
    DOI: 10.1115/1.3445607
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Local heat transfer coefficients to an airfoil in an oscillating stream have been measured for a range of frequencies and oscillation amplitudes. Results at moderate angles of attack are in agreement with previously reported findings. However, at large angles of attack, including those associated with stall in steady flow, a strong periodic starting vortex shed from the leading edge leads to a dramatic reattachment of the flow and consequent increase in local Nusselt Numbers of as much as five-fold. These effects are shown to be amplified by increasing oscillation frequency and amplitude.
    keyword(s): Flow (Dynamics) , Heat transfer , Airfoils , Oscillations , Vortices , Frequency AND Heat transfer coefficients ,
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      Heat Transfer to an Airfoil in Oscillating Flow

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/150878
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorJ. A. Miller
    contributor authorP. F. Pucci
    date accessioned2017-05-09T00:56:15Z
    date available2017-05-09T00:56:15Z
    date copyrightOctober, 1971
    date issued1971
    identifier issn1528-8919
    identifier otherJETPEZ-26696#461_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/150878
    description abstractLocal heat transfer coefficients to an airfoil in an oscillating stream have been measured for a range of frequencies and oscillation amplitudes. Results at moderate angles of attack are in agreement with previously reported findings. However, at large angles of attack, including those associated with stall in steady flow, a strong periodic starting vortex shed from the leading edge leads to a dramatic reattachment of the flow and consequent increase in local Nusselt Numbers of as much as five-fold. These effects are shown to be amplified by increasing oscillation frequency and amplitude.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHeat Transfer to an Airfoil in Oscillating Flow
    typeJournal Paper
    journal volume93
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3445607
    journal fristpage461
    journal lastpage468
    identifier eissn0742-4795
    keywordsFlow (Dynamics)
    keywordsHeat transfer
    keywordsAirfoils
    keywordsOscillations
    keywordsVortices
    keywordsFrequency AND Heat transfer coefficients
    treeJournal of Engineering for Gas Turbines and Power:;1971:;volume( 093 ):;issue: 004
    contenttypeFulltext
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