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    The Fluctuating Flow of a Gas Near a Stagnation Point on a Hot Wall

    Source: Journal of Applied Mechanics:;1971:;volume( 038 ):;issue: 004::page 820
    Author:
    R. J. Gribben
    DOI: 10.1115/1.3408960
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Solutions are given in series, valid for low and high frequencies, for the two-dimensional flow in the vicinity of a stagnation point due to an incident stream, assumed incompressible, which is fluctuating in amplitude about a steady mean. The wall is assumed to be hot so that compressibility effects may not be neglected within the laminar boundary layer itself. Numerical computations are carried out for the case of the wall-mainstream temperature ratio, χ, equal to unity (a warm wall) and χ = 2.003 (a typical hot wall). Calculation of the fluctuations in the skin-friction and heat-transfer rate at the wall support previous approximate results at low frequencies for these two values of χ and the effect of the hot wall is seen to enhance the phase lead (skin friction) over, and decrease the phase lag (heat transfer) behind, the main stream. The possibility of covering the whole frequency range by the two series is discussed.
    keyword(s): Flow (Dynamics) , Heat transfer , Skin friction (Fluid dynamics) , Frequency , Compressibility , Boundary layers , Computation , Fluctuations (Physics) AND Temperature ,
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      The Fluctuating Flow of a Gas Near a Stagnation Point on a Hot Wall

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    https://yetl.yabesh.ir/yetl1/handle/yetl/147645
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    contributor authorR. J. Gribben
    date accessioned2017-05-09T00:47:03Z
    date available2017-05-09T00:47:03Z
    date copyrightDecember, 1971
    date issued1971
    identifier issn0021-8936
    identifier otherJAMCAV-25950#820_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/147645
    description abstractSolutions are given in series, valid for low and high frequencies, for the two-dimensional flow in the vicinity of a stagnation point due to an incident stream, assumed incompressible, which is fluctuating in amplitude about a steady mean. The wall is assumed to be hot so that compressibility effects may not be neglected within the laminar boundary layer itself. Numerical computations are carried out for the case of the wall-mainstream temperature ratio, χ, equal to unity (a warm wall) and χ = 2.003 (a typical hot wall). Calculation of the fluctuations in the skin-friction and heat-transfer rate at the wall support previous approximate results at low frequencies for these two values of χ and the effect of the hot wall is seen to enhance the phase lead (skin friction) over, and decrease the phase lag (heat transfer) behind, the main stream. The possibility of covering the whole frequency range by the two series is discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Fluctuating Flow of a Gas Near a Stagnation Point on a Hot Wall
    typeJournal Paper
    journal volume38
    journal issue4
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3408960
    journal fristpage820
    journal lastpage828
    identifier eissn1528-9036
    keywordsFlow (Dynamics)
    keywordsHeat transfer
    keywordsSkin friction (Fluid dynamics)
    keywordsFrequency
    keywordsCompressibility
    keywordsBoundary layers
    keywordsComputation
    keywordsFluctuations (Physics) AND Temperature
    treeJournal of Applied Mechanics:;1971:;volume( 038 ):;issue: 004
    contenttypeFulltext
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