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    A Numerical Solution for the Laminar Wake Behind a Finite Flat Plate

    Source: Journal of Applied Mechanics:;1968:;volume( 035 ):;issue: 004::page 625
    Author:
    A. Plotkin
    ,
    I. Flügge-Lotz
    DOI: 10.1115/1.3601283
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A finite-difference solution is presented for the laminar, two-dimensional, viscous, incompressible wake behind a finite flate plate. The plate is infinitely thin and is aligned parallel to a uniform stream. The Reynolds number based on plate length is assumed large enough to allow the formation of boundary layers on the top and bottom of the plate. The wake is formed by the merging of these boundary layers at the trailing edge. The upstream influence of the trailing-edge disturbance necessitates solving the complete Navier-Stokes equations in the trailing-edge region. As yet, no satisfactory solution to the problem exists. The aim of this investigation is to calculate an improved first approximation to the solution in the trailing-edge region for high values of the Reynolds number. The solution can be continued in the downstream direction. Solutions are obtained for Reynolds numbers larger than 105 . The behavior of the flow variables in the immediate neighborhood of the trailing edge indicates the existence of a singularity at the edge. The exact nature of this singularity has not, as yet, been determined.
    keyword(s): Wakes , Flat plates , Reynolds number , Boundary layers , Approximation , Flow (Dynamics) AND Navier-Stokes equations ,
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      A Numerical Solution for the Laminar Wake Behind a Finite Flat Plate

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    http://yetl.yabesh.ir/yetl1/handle/yetl/123578
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    contributor authorA. Plotkin
    contributor authorI. Flügge-Lotz
    date accessioned2017-05-09T00:02:13Z
    date available2017-05-09T00:02:13Z
    date copyrightDecember, 1968
    date issued1968
    identifier issn0021-8936
    identifier otherJAMCAV-25882#625_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/123578
    description abstractA finite-difference solution is presented for the laminar, two-dimensional, viscous, incompressible wake behind a finite flate plate. The plate is infinitely thin and is aligned parallel to a uniform stream. The Reynolds number based on plate length is assumed large enough to allow the formation of boundary layers on the top and bottom of the plate. The wake is formed by the merging of these boundary layers at the trailing edge. The upstream influence of the trailing-edge disturbance necessitates solving the complete Navier-Stokes equations in the trailing-edge region. As yet, no satisfactory solution to the problem exists. The aim of this investigation is to calculate an improved first approximation to the solution in the trailing-edge region for high values of the Reynolds number. The solution can be continued in the downstream direction. Solutions are obtained for Reynolds numbers larger than 105 . The behavior of the flow variables in the immediate neighborhood of the trailing edge indicates the existence of a singularity at the edge. The exact nature of this singularity has not, as yet, been determined.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Numerical Solution for the Laminar Wake Behind a Finite Flat Plate
    typeJournal Paper
    journal volume35
    journal issue4
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3601283
    journal fristpage625
    journal lastpage630
    identifier eissn1528-9036
    keywordsWakes
    keywordsFlat plates
    keywordsReynolds number
    keywordsBoundary layers
    keywordsApproximation
    keywordsFlow (Dynamics) AND Navier-Stokes equations
    treeJournal of Applied Mechanics:;1968:;volume( 035 ):;issue: 004
    contenttypeFulltext
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