Vortical Flow past Axisymmetric Bluff Bodies

Hiroshi Higuchi

Mechanical, Aerospace and Manufacturing Engineering
Syracuse University

Abstract-
Fluid-structure interactions and their control in many practical applications rely on the understanding of the wake behind bluff bodies. The experimental study presented is motivated by so-called wake-recontact problems with high-performance parachutes; it examines the evolution of the wake structure behind a disk and other bluff-bodies. Behind the impulsively started disk, the growth of the wake size and circulation time history scaled with the velocity and the disk diameter over a wide range of the Reynolds numbers tested. The maximum normalized circulation reached an asymptotic value after which the vortex started to deform and eventually shed downstream asymmetrically. This maximum circulation is analogous to the formation number for the vortex ring (Gharib et al, 1998.) The results will be compared with those behind the uniformly accelerated disk and a flat plate. [The wake study is currently being extended to supersonic speeds as well as to the wake behind a magnetically suspended model.] The talk will conclude with related wake structure interaction problems in sports aerodynamics pertaining to the knuckleball and flying disk.


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