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    On the Axisymmetric Vortex Flow Over a Flat Surface

    Source: Journal of Applied Mechanics:;1969:;volume( 036 ):;issue: 003::page 614
    Author:
    E. W. Schwiderski
    DOI: 10.1115/1.3564725
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The numerical study of the interaction of a potential vortex with a stationary surface recently published by Kidd and Farris [1] is extended through a transformation of the boundary-value problem to Volterra integral equations. The new calculations verified the results by Kidd and Farris and improved the bounds of the critical Reynolds number Nc , beyond which no self-similar vortex flows exist, to 5.5 < Nc < 5.6 The breakdown of the self-similar motions develops through an instability in the lower boundary layer, which is indicated by two inflection points in the tangential velocity profile. At the critical Reynolds number the lower inflection point reaches the surface and indicates the beginning of boundary-layer separation in the wake-type flow. If the Stokes linearization is applied, one arrives at a new Stokes paradox. However, this “paradox” can be resolved by correcting the free-stream pressure distortion of the Stokes approximation. The new slow-motion approximation is nonlinear and yields an integral which is also free of the Whitehead paradox. The properties of the new exact solution confirm the novel flow features previously detected in almost self-similar motions, which were constructed by adjustable local boundary-layer approximations.
    keyword(s): Vortex flow , Motion , Boundary layers , Approximation , Reynolds number , Flow (Dynamics) , Separation (Technology) , Wakes , Boundary-value problems , Volterra equations , Vortices AND Pressure ,
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      On the Axisymmetric Vortex Flow Over a Flat Surface

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    contributor authorE. W. Schwiderski
    date accessioned2017-05-09T00:16:14Z
    date available2017-05-09T00:16:14Z
    date copyrightSeptember, 1969
    date issued1969
    identifier issn0021-8936
    identifier otherJAMCAV-25895#614_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/131835
    description abstractThe numerical study of the interaction of a potential vortex with a stationary surface recently published by Kidd and Farris [1] is extended through a transformation of the boundary-value problem to Volterra integral equations. The new calculations verified the results by Kidd and Farris and improved the bounds of the critical Reynolds number Nc , beyond which no self-similar vortex flows exist, to 5.5 < Nc < 5.6 The breakdown of the self-similar motions develops through an instability in the lower boundary layer, which is indicated by two inflection points in the tangential velocity profile. At the critical Reynolds number the lower inflection point reaches the surface and indicates the beginning of boundary-layer separation in the wake-type flow. If the Stokes linearization is applied, one arrives at a new Stokes paradox. However, this “paradox” can be resolved by correcting the free-stream pressure distortion of the Stokes approximation. The new slow-motion approximation is nonlinear and yields an integral which is also free of the Whitehead paradox. The properties of the new exact solution confirm the novel flow features previously detected in almost self-similar motions, which were constructed by adjustable local boundary-layer approximations.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOn the Axisymmetric Vortex Flow Over a Flat Surface
    typeJournal Paper
    journal volume36
    journal issue3
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3564725
    journal fristpage614
    journal lastpage619
    identifier eissn1528-9036
    keywordsVortex flow
    keywordsMotion
    keywordsBoundary layers
    keywordsApproximation
    keywordsReynolds number
    keywordsFlow (Dynamics)
    keywordsSeparation (Technology)
    keywordsWakes
    keywordsBoundary-value problems
    keywordsVolterra equations
    keywordsVortices AND Pressure
    treeJournal of Applied Mechanics:;1969:;volume( 036 ):;issue: 003
    contenttypeFulltext
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