The topology and evolution of three-dimensional flow past a cylinder of slenderness ratio SR=1 mounted in a wind tunnel is examined for 0.1≤Re≤325 (based on the diameter of the cylinder) where steady-state solutions have been obtained. Direct numerical simulations were computed using an in-house parallel finite element code. The three-dimensional theory of separation is used to analyze and interpret the flow phenomena. Results indicate that symmetry breaking occurs at Re=1, while the first prominent structure is a horseshoe vortex downstream from the cylinder. At Re=150, two foci are observed, indicating the formation of two tornadolike vortices downstream. Concurrently, another horseshoe vortex is formed upstream from the cylinder. For higher Reynolds numbers, the flow downstream is segmented to upper and lower parts, whereas the topology of the flow on the solid boundaries remains unaltered. Pressure distributions show that pressure, the key physical parameter in the flow, decreases everywhere except immediately upstream from the cylinder. In addition, creation of critical points from saddle-node-type bifurcations occur when the streamwise component of the pressure gradient changes sign. Finally, at Re=325, an additional horseshoe vortex is formed at the wake of the cylinder. In all computations, an absence of critical points was observed on the free end of the cylinder.


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    Titel :

    Three-Dimensional, Laminar Flow Past a Short, Surface-Mounted Cylinder



    Erschienen in:

    Erscheinungsdatum :

    2016




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :

    Klassifikation :

    BKL:    55.50 Luftfahrzeugtechnik / 55.60 Raumfahrttechnik / 55.60 / 50.93 / 55.50 / 50.93 Weltraumforschung
    Lokalklassifikation TIB:    770/7040




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