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    Second Order Boundary Layer Solutions on a Curved Surface

    Source: Journal of Fluids Engineering:;1972:;volume( 094 ):;issue: 003::page 649
    Author:
    W. F. Van Tassell
    ,
    D. B. Taulbee
    DOI: 10.1115/1.3425521
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Solutions of the second order longitudinal curvature boundary layer equations near the stagnation point of a two-dimensional circular cylinder are presented. Four cases corresponding to 1 first order locally similar solutions, 2 first order nonsimilar solutions, 3 second order locally similar solutions, and 4 second order nonsimilar solutions are considered. For each of the four cases, results for four different altitudes are given. The only second order effect considered is longitudinal curvature. Based on the numerical results, it is concluded that similarity and curvature assumptions can alter the skin friction calculations significantly. The heat transfer calculations are much less sensitive to the various assumptions, at least for the cases studied in this paper.
    keyword(s): Boundary layers , Circular cylinders , Equations , Heat transfer AND Skin friction (Fluid dynamics) ,
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      Second Order Boundary Layer Solutions on a Curved Surface

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/162022
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    contributor authorW. F. Van Tassell
    contributor authorD. B. Taulbee
    date accessioned2017-05-09T01:31:45Z
    date available2017-05-09T01:31:45Z
    date copyrightSeptember, 1972
    date issued1972
    identifier issn0098-2202
    identifier otherJFEGA4-27397#649_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/162022
    description abstractSolutions of the second order longitudinal curvature boundary layer equations near the stagnation point of a two-dimensional circular cylinder are presented. Four cases corresponding to 1 first order locally similar solutions, 2 first order nonsimilar solutions, 3 second order locally similar solutions, and 4 second order nonsimilar solutions are considered. For each of the four cases, results for four different altitudes are given. The only second order effect considered is longitudinal curvature. Based on the numerical results, it is concluded that similarity and curvature assumptions can alter the skin friction calculations significantly. The heat transfer calculations are much less sensitive to the various assumptions, at least for the cases studied in this paper.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSecond Order Boundary Layer Solutions on a Curved Surface
    typeJournal Paper
    journal volume94
    journal issue3
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3425521
    journal fristpage649
    journal lastpage654
    identifier eissn1528-901X
    keywordsBoundary layers
    keywordsCircular cylinders
    keywordsEquations
    keywordsHeat transfer AND Skin friction (Fluid dynamics)
    treeJournal of Fluids Engineering:;1972:;volume( 094 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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