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    Heat Transfer and Skin Friction for Turbulent Boundary-Layer Flow Longitudinal to a Circular Cylinder

    Source: Journal of Applied Mechanics:;1963:;volume( 030 ):;issue: 001::page 37
    Author:
    E. M. Sparrow
    ,
    E. R. G. Eckert
    ,
    W. J. Minkowycz
    DOI: 10.1115/1.3630103
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An analysis has been carried out for the turbulent velocity and thermal boundary layers which develop along a cylinder whose axis is parallel to the free-stream flow. Local and average friction factors are calculated as functions of the length Reynolds number Rex for various cylinder sizes (characterized, by the radius Reynolds number Rer0 ). For corresponding flow conditions, the friction factor for a cylinder always exceeds that for the flat plate. Local heat-transfer coefficients corresponding to the case of uniform wall heat flux have been obtained for Prandtl numbers of 0.7 and 5. As with the friction factors, the cylinder heat-transfer coefficients exceed those for the flat plate. This effect of the cylindrical geometry on heat transfer diminishes with increasing Prandtl number.
    keyword(s): Skin friction (Fluid dynamics) , Boundary layers , Circular cylinders , Flow (Dynamics) , Heat transfer , Turbulence , Cylinders , Friction , Reynolds number , Flat plates , Functions , Geometry , Prandtl number , Heat flux AND Thermal boundary layers ,
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      Heat Transfer and Skin Friction for Turbulent Boundary-Layer Flow Longitudinal to a Circular Cylinder

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/93890
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    • Journal of Applied Mechanics

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    contributor authorE. M. Sparrow
    contributor authorE. R. G. Eckert
    contributor authorW. J. Minkowycz
    date accessioned2017-05-08T23:09:56Z
    date available2017-05-08T23:09:56Z
    date copyrightMarch, 1963
    date issued1963
    identifier issn0021-8936
    identifier otherJAMCAV-25700#37_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/93890
    description abstractAn analysis has been carried out for the turbulent velocity and thermal boundary layers which develop along a cylinder whose axis is parallel to the free-stream flow. Local and average friction factors are calculated as functions of the length Reynolds number Rex for various cylinder sizes (characterized, by the radius Reynolds number Rer0 ). For corresponding flow conditions, the friction factor for a cylinder always exceeds that for the flat plate. Local heat-transfer coefficients corresponding to the case of uniform wall heat flux have been obtained for Prandtl numbers of 0.7 and 5. As with the friction factors, the cylinder heat-transfer coefficients exceed those for the flat plate. This effect of the cylindrical geometry on heat transfer diminishes with increasing Prandtl number.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHeat Transfer and Skin Friction for Turbulent Boundary-Layer Flow Longitudinal to a Circular Cylinder
    typeJournal Paper
    journal volume30
    journal issue1
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3630103
    journal fristpage37
    journal lastpage43
    identifier eissn1528-9036
    keywordsSkin friction (Fluid dynamics)
    keywordsBoundary layers
    keywordsCircular cylinders
    keywordsFlow (Dynamics)
    keywordsHeat transfer
    keywordsTurbulence
    keywordsCylinders
    keywordsFriction
    keywordsReynolds number
    keywordsFlat plates
    keywordsFunctions
    keywordsGeometry
    keywordsPrandtl number
    keywordsHeat flux AND Thermal boundary layers
    treeJournal of Applied Mechanics:;1963:;volume( 030 ):;issue: 001
    contenttypeFulltext
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