Vortex Flows and Related Numerical Methods II
ESAIM: Proceedings,
Vol. 1, 1996, pp. 307-323
Computational Investigation of Drag Reduction
on a Rotationally Oscillating Cylinder
D. Shiels and A. Leonard
Graduate Aeronautical Laboratories
California Institute of Technology
Pasadena, CA 91125, USA
A. Stagg
Cray Research, Inc.
c/o Jet Propulsion Laboratories
MS 301-455, 4800 Oak Grove Drive
Pasadenaa, CA 91109, USA
Abstract
The reduction of drag on a circular cylinder in two-dimensional
incompressible flow, achieved using oscillatory body rotation, is
investigated to reveal the physics responsible for the force reduction.
Flow is computationally simulated at Reynolds numbers of 100, 300, and
15000 for a small group of sinusoidal body rotations to gain an
understanding of the mechanisms which can control forces in such
situations. It is observed that, for certain rotational parameters, drag
is reduced over a range of Reynolds numbers from the two-dimensional base
flow. At Re=15000, an interesting boundary layer instability is
observed which could explain the dramatic drag reduction previously noted
in an experiment on this flow. Simulations are performed with a
high-resolution viscous vortex method which utilizes the particle strength
exchange technique for diffusion and multipole expansions for fast
summations. Different approaches for computing and analyzing forces will
be discussed as well as a "hybridization" applied to the scheme to allow
particle merging in the far wake.
Vortex Flows and Related
Numerical Methods II
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