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    Asymmetrical Boundary Layer Separation at the Base of a Two Cylinder Geometry

    Source: Journal of Fluids Engineering:;1989:;volume( 111 ):;issue: 004::page 443
    Author:
    M. T. Boyle
    ,
    L. S. Langston
    DOI: 10.1115/1.3243666
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper reports on the experimental description of the three-dimensional horseshoe vortex system occurring at the base of two cylinders mounted side by side on an endwall. The spacing between the two cylinders is adjusted to generate a family of viscous flows. Flow visualization performed in a water tunnel provides a qualitative understanding of the flow over a range of flow variables. A detailed wind tunnel experiment, provides a quantitative description of the flow at a single test condition. The flow is described by the use of a five-hole pressure probe and by cylinder and endwall surface static pressure measurements. At ReD = 2.5 × 105 the measurements show an asymmetrical primary vortex with a wide flat cross section. A small counter rotating vortex is found between the primary vortex and the cylinder leading edge.
    keyword(s): Separation (Technology) , Boundary layers , Cylinders , Geometry , Flow (Dynamics) , Vortices , Pressure , Measurement , Pressure measurement , Flow visualization , Water tunnels , Probes AND Wind tunnels ,
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      Asymmetrical Boundary Layer Separation at the Base of a Two Cylinder Geometry

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    https://yetl.yabesh.ir/yetl1/handle/yetl/105543
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    contributor authorM. T. Boyle
    contributor authorL. S. Langston
    date accessioned2017-05-08T23:30:15Z
    date available2017-05-08T23:30:15Z
    date copyrightDecember, 1989
    date issued1989
    identifier issn0098-2202
    identifier otherJFEGA4-27046#443_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/105543
    description abstractThis paper reports on the experimental description of the three-dimensional horseshoe vortex system occurring at the base of two cylinders mounted side by side on an endwall. The spacing between the two cylinders is adjusted to generate a family of viscous flows. Flow visualization performed in a water tunnel provides a qualitative understanding of the flow over a range of flow variables. A detailed wind tunnel experiment, provides a quantitative description of the flow at a single test condition. The flow is described by the use of a five-hole pressure probe and by cylinder and endwall surface static pressure measurements. At ReD = 2.5 × 105 the measurements show an asymmetrical primary vortex with a wide flat cross section. A small counter rotating vortex is found between the primary vortex and the cylinder leading edge.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAsymmetrical Boundary Layer Separation at the Base of a Two Cylinder Geometry
    typeJournal Paper
    journal volume111
    journal issue4
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3243666
    journal fristpage443
    journal lastpage448
    identifier eissn1528-901X
    keywordsSeparation (Technology)
    keywordsBoundary layers
    keywordsCylinders
    keywordsGeometry
    keywordsFlow (Dynamics)
    keywordsVortices
    keywordsPressure
    keywordsMeasurement
    keywordsPressure measurement
    keywordsFlow visualization
    keywordsWater tunnels
    keywordsProbes AND Wind tunnels
    treeJournal of Fluids Engineering:;1989:;volume( 111 ):;issue: 004
    contenttypeFulltext
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