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    Interference Between Two Circular Cylinders of Finite Height Vertically Immersed in a Turbulent Boundary Layer

    Source: Journal of Fluids Engineering:;1982:;volume( 104 ):;issue: 004::page 529
    Author:
    S. Taniguchi
    ,
    H. Sakamoto
    ,
    M. Arie
    DOI: 10.1115/1.3241901
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Measurements were made of the circumferential pressure distributions around two cylinders of finite height h and diameter d, spaced a distance s apart and vertically immersed in a turbulent boundary layer. The angle of attack φ and the dimensionless spacing s/d were varied. Drag and lift characteristics of both cylinders were classified into three regions divided by two zero-lift lines, namely 0 ≲ φ ≲ 30 deg, 30 ≲ φ ≲ 120 deg, and 120 ≲ φ ≲ 180 deg, in which interference between the two cylinders was found to be almost negligible for s/d ≳ 4.0, except for an influence in the wake region of the upstream cylinder.
    keyword(s): Boundary layer turbulence , Circular cylinders , Cylinders , Pressure , Measurement , Drag (Fluid dynamics) AND Wakes ,
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      Interference Between Two Circular Cylinders of Finite Height Vertically Immersed in a Turbulent Boundary Layer

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/95947
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    • Journal of Fluids Engineering

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    contributor authorS. Taniguchi
    contributor authorH. Sakamoto
    contributor authorM. Arie
    date accessioned2017-05-08T23:13:35Z
    date available2017-05-08T23:13:35Z
    date copyrightDecember, 1982
    date issued1982
    identifier issn0098-2202
    identifier otherJFEGA4-26990#529_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/95947
    description abstractMeasurements were made of the circumferential pressure distributions around two cylinders of finite height h and diameter d, spaced a distance s apart and vertically immersed in a turbulent boundary layer. The angle of attack φ and the dimensionless spacing s/d were varied. Drag and lift characteristics of both cylinders were classified into three regions divided by two zero-lift lines, namely 0 ≲ φ ≲ 30 deg, 30 ≲ φ ≲ 120 deg, and 120 ≲ φ ≲ 180 deg, in which interference between the two cylinders was found to be almost negligible for s/d ≳ 4.0, except for an influence in the wake region of the upstream cylinder.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInterference Between Two Circular Cylinders of Finite Height Vertically Immersed in a Turbulent Boundary Layer
    typeJournal Paper
    journal volume104
    journal issue4
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3241901
    journal fristpage529
    journal lastpage536
    identifier eissn1528-901X
    keywordsBoundary layer turbulence
    keywordsCircular cylinders
    keywordsCylinders
    keywordsPressure
    keywordsMeasurement
    keywordsDrag (Fluid dynamics) AND Wakes
    treeJournal of Fluids Engineering:;1982:;volume( 104 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian