1. Transverse and lateral confinement effects on the oscillations of a free cylinder in a viscous flow
- Author
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Gianorio, Luciano, d'Angelo, Maria Veronica, Cachile, Mario, Hulin, Jean-Pierre, Auradou, Harold, Grupo de Medios Porosos [Buenos Aires] (GMP), Facultad de Ingeniería [Buenos Aires] (FIUBA), Universidad de Buenos Aires [Buenos Aires] (UBA)-Universidad de Buenos Aires [Buenos Aires] (UBA), Fluides, automatique, systèmes thermiques (FAST), Université Paris-Sud - Paris 11 (UP11)-Université Pierre et Marie Curie - Paris 6 (UPMC)-Centre National de la Recherche Scientifique (CNRS), and LIA PMF
- Subjects
[PHYS.PHYS.PHYS-FLU-DYN]Physics [physics]/Physics [physics]/Fluid Dynamics [physics.flu-dyn] ,Physics::Fluid Dynamics ,instability ,Fluid Dynamics (physics.flu-dyn) ,FOS: Physical sciences ,Physics - Fluid Dynamics ,flow-structure interaction ,oscillation ,Hele Shaw flow ,fluttering ,single fiber - Abstract
International audience; The different types of instabilities of free cylinders (diameter $D$, length $L$) have been studied in a viscous flow (velocity $U$) between parallel vertical walls of horizontal width $W$ at a distance $H$: the influence of the confinement parameters $D/H$ and $L/W$ has been investigated. As $D/H$ increases, there is a transition from stable flow to oscillations transverse to the walls and then to a fluttering motion with oscillations of the angle of the axis with respect to the horizontal. The two types of oscillations may be superimposed in the transition domain. The frequency $f$ of the transverse oscillations is independent of the lateral confinement $L/W$ in the range: 0.055 \le L/W \le 0.94$ for a given cylinder velocity $V_{cx}$ and increases only weakly with $V_{cx}$. These results are accounted for by assuming a $2D$ local flow over the cylinder with a characteristic velocity independent of $L/W$ for a given $V_{cx}$ value. The experimental values of $f$ are also independent of the transverse confinement $D/H$. The frequency $f_f$ of the fluttering motion is significantly lower than $f$: $f_f$ is also nearly independent of the cylinder diameter and of the flow velocity but decreases significantly as $L/W$ increases. The fluttering instability is then rather a $3D$ phenomenon involving the full length of the cylinder and the clearance between its ends and the side walls.
- Published
- 2013
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