An experimental study of flow around a circular cylinder with and without end plates in ground effect


Nishino, Takafumi, Roberts, Graham T. and Zhang, Xin (2006) An experimental study of flow around a circular cylinder with and without end plates in ground effect. In, 36th AIAA Fluid Dynamics Conference, San Francisco, USA, 05 - 08 Jun 2006. USA, American Institute of Aeronautics and Astronautics.

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Description/Abstract

Flow and force characteristics have been experimentally studied for a circular cylinder,
with and without end plates, placed near and parallel to a moving ground, over which no
boundary layer developed to interfere with the cylinder. Mean drag and lift measurements,
surface oil-flow visualisation, and particle image velocimetry (PIV) measurements were
carried out at two upper-subcritical Reynolds numbers of 0.4 and 1.0×105 (based on the
cylinder diameter d) to investigate the effects of the gap ratio h/d, where h is the gap between
the cylinder and the ground. For the cylinder with end plates, the drag rapidly decreased as
h/d decreased to less than 0.5, but became constant for h/d of less than 0.35. This distinctive
drag behaviour was explained by a global change in the near wake: the Kármán-type vortex
shedding was found to be intermittent at h/d = 0.4, and then totally ceased (and instead two
nearly parallel shear layers were formed) at h/d = 0.3 and below. Meanwhile, for the cylinder
without end plates, no such a critical change in drag was observed as the Kármán-type
vortices were not generated in the near wake region for all h/d investigated.

Item Type: Conference or Workshop Item (Paper)
Additional Information: AIAA paper 2006-3551
Related URLs:
Keywords: circular cylinder, ground effect
Subjects: T Technology > TL Motor vehicles. Aeronautics. Astronautics
Q Science > QC Physics
Divisions: University Structure - Pre August 2011 > School of Engineering Sciences > Aerodynamics & Flight Mechanics
Item ID: 49001
Date Deposited: 19 Oct 2007
Last Modified: 02 Mar 2012 13:09
Contributors: Nishino, Takafumi (Author)
Roberts, Graham T. (Author)
Zhang, Xin (Author)
Date: June 2006
Additional Information: AIAA paper 2006-3551
Status: Published
Publisher: American Institute of Aeronautics and Astronautics
URI: http://eprints.soton.ac.uk/id/eprint/49001

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