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    Unsteady Incompressible Three-Dimensional Asymmetric Stagnation-Point Boundary Layers

    Source: Journal of Applied Mechanics:;1980:;volume( 047 ):;issue: 002::page 241
    Author:
    M. Kumari
    ,
    G. Nath
    DOI: 10.1115/1.3153649
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The unsteady laminar incompressible boundary-layer flow near the three-dimensional asymmetric stagnation point has been studied under the assumptions that the free-stream velocity, wall temperature, and surface mass transfer vary arbitrarily with time. The partial differential equations governing the flow have been solved numerically using an implicit finite-difference scheme. It is found that in contrast with the symmetric flow, the maximum heat transfer occurs away from the stagnation point due to the decrease in the boundary-layer thickness. The effect of the variation of the wall temperature with time on heat transfer is strong. The skin friction and heat transfer due to asymmetric flow only are comparatively less affected by the mass transfer as compared to those of symmetric flow.
    keyword(s): Boundary layers , Flow (Dynamics) , Heat transfer , Mass transfer , Wall temperature , Partial differential equations , Thickness AND Skin friction (Fluid dynamics) ,
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      Unsteady Incompressible Three-Dimensional Asymmetric Stagnation-Point Boundary Layers

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    https://yetl.yabesh.ir/yetl1/handle/yetl/92877
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    contributor authorM. Kumari
    contributor authorG. Nath
    date accessioned2017-05-08T23:07:59Z
    date available2017-05-08T23:07:59Z
    date copyrightJune, 1980
    date issued1980
    identifier issn0021-8936
    identifier otherJAMCAV-26145#241_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/92877
    description abstractThe unsteady laminar incompressible boundary-layer flow near the three-dimensional asymmetric stagnation point has been studied under the assumptions that the free-stream velocity, wall temperature, and surface mass transfer vary arbitrarily with time. The partial differential equations governing the flow have been solved numerically using an implicit finite-difference scheme. It is found that in contrast with the symmetric flow, the maximum heat transfer occurs away from the stagnation point due to the decrease in the boundary-layer thickness. The effect of the variation of the wall temperature with time on heat transfer is strong. The skin friction and heat transfer due to asymmetric flow only are comparatively less affected by the mass transfer as compared to those of symmetric flow.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleUnsteady Incompressible Three-Dimensional Asymmetric Stagnation-Point Boundary Layers
    typeJournal Paper
    journal volume47
    journal issue2
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3153649
    journal fristpage241
    journal lastpage246
    identifier eissn1528-9036
    keywordsBoundary layers
    keywordsFlow (Dynamics)
    keywordsHeat transfer
    keywordsMass transfer
    keywordsWall temperature
    keywordsPartial differential equations
    keywordsThickness AND Skin friction (Fluid dynamics)
    treeJournal of Applied Mechanics:;1980:;volume( 047 ):;issue: 002
    contenttypeFulltext
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