Flow characteristics around a wall-mounted spherical obstacle in a thin boundary layer

Flow characteristics around a wall-mounted spherical obstacle in a thin boundary layer The mean wake structures and turbulent flow fields of a wall-mounted spherical obstacle placed in a thin laminar boundary layer, of thickness 14 % of the sphere diameter, were investigated at a Reynolds number of 17,800. Digital particle image velocimetry was used to interrogate the flow in the vicinity of the obstacle, and thermal anemometry measurements were performed to characterize unsteadiness in the wake. Streamwise features observed in the mean wake flow included counter-rotating tip vortices inducing downwash, horseshoe vortices, weak vortices inducing upwash at the top of the near wake, and counter-rotating ‘lobe’ vortices formed by the somewhat unique convex geometry of the sphere near the base. Under the present flow conditions, the sphere base geometry also prevented the roll-up of a horseshoe system upstream of the obstacle. The wake flow field, including lobe structures, is consistent with a vortex skeleton model developed to describe the simpler wakes of low-aspect-ratio wall-mounted semi-ellipsoidal obstacles, with modifications due to the unique junction geometry. Point velocity measurements in the wake identified a weak dominant frequency close to the bed. Cross-spectral analysis of these data at symmetrically located points revealed that, on average, flow oscillations were in phase. The turbulent stress distribution in the wake of the sphere showed a region of high magnitude near the bed not observed for other geometries, and spatially consistent with the lobe structures. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Experiments in Fluids Springer Journals

Flow characteristics around a wall-mounted spherical obstacle in a thin boundary layer

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Springer Berlin Heidelberg
Copyright © 2014 by Springer-Verlag Berlin Heidelberg
Engineering; Engineering Fluid Dynamics; Fluid- and Aerodynamics; Engineering Thermodynamics, Heat and Mass Transfer
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