Contribution to Active and Passive Control of Flow around a Cylinder

This numerical study aims to develop a coupled,
passive and active control strategy of the flow around a cylinder of
diameter D, and Re=4000. The strategy consists to put a cylindrical
rod in front of a deforming cylinder. The quasi- elliptical deformation
of cylinder follow a sinusoidal law in order to reduce the drag force.
To analyze the evolution of unsteady vortices, the Large Eddy
Simulation approach is used in this 2D simulation, carried out using
ANSYS – Fluent. The movement of deformation is reproduced using
an internal subroutine, introduced in the form of a User Defined
Function UDF. Two diameters of the rod were tested for a rod placed
at a distance L = 3 ×d, with an amplitudes of deformation A = 5%, A
= 25% and A = 50% of the cylinder diameter, the frequency of
deformation take the values fd = 1fn, 5fn and 8fn, which fn
represents the naturel vortex shedding frequency. The results show
substantial changes in the flow behavior and for a rod of 6mm (1%
D) with amplitude A = 25%, and with a 2fn frequency, drag
reduction of 60% was recorded.





References:
[1] Taylor, HD. The elimination of diffuser separation by vortex generators.
United Aircraft Corporation Report No. R-4012-3 1947.
[2] Schubauer, GB.,Spangenberg, WG. Forced mixing in boundary layers. J
Fluid Mech 1960;8:10–32.
[3] Greenblatt D, Wygnanski IJ. The control of flow separation by periodic
excitation. Prog Aerospace Sci 2000;36:487–545.
[4] Mittal R., Kotapati R.B. et Cattafesta L. 2005. "Numerical study of
resonant interactions and flow control in a canonical separated flow".
AIAA Paper, No. 2005-1261.
[5] amotsu Igarashi. (1997) "Drag reduction of a square prism by flow
control using a small rod”. Journal of Wind Engineering and Industrial
Aerodynamics ;69 71 141-153.
[6] Hua Shan a, Li Jiang, Numerical study of passive and active flow
separation controlover a NACA0012 airfoil J. Computers & Fluids 37
(2008) 975–992.
[7] T. sutsui, , Igarashi, T.Drag reduction of a circular cylinder in an airstream
Journal of Wind Engineering and Industrial Aerodynamics 90
(2002) 527–541.