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Electromagnetically driven anticyclonic rotation in spherical Couette flow

Published online by Cambridge University Press:  24 April 2023

D. Proal
Affiliation:
Instituto de Investigación en Ciencias Básicas y Aplicadas – Universidad Autónoma del Estado de Morelos, Cuernavaca, Morelos 62209, Mexico
D.R. Domínguez-Lozoya
Affiliation:
Instituto de Energías Renovables – Universidad Nacional Autónoma de Mexico, Temixco, Morelos 62209, Mexico
A. Figueroa*
Affiliation:
CONACYT-Centro de Investigación en Ciencias-Universidad Autónoma del Estado de Morelos, Cuernavaca, Morelos 62209, Mexico
M. Rivero
Affiliation:
Instituto de Investigaciones en Materiales, Unidad Morelia, Universidad Nacional Autónoma de México, 58190 Morelia, Michoacán, Mexico
S. Piedra
Affiliation:
CONACYT – Centro de Ingeniería y Desarrollo Industrial, Querétaro, Querétaro 76270, Mexico
J. Núñez
Affiliation:
Escuela Nacional de Estudios Superiores, Unidad Morelia, Universidad Nacional Autónoma de México, 58190 Morelia, Michoacán, Mexico
*
†Email address for correspondence: alfil@uaem.mx

Abstract

The electromagnetically driven anticyclonic flow in the wide gap of a rotating concentric spheres system is studied experimentally and numerically in the laminar regime. The working fluid is an electrolyte contained in the spherical gap. The outer sphere rotates at constant angular speed, and the inner sphere is at rest. The electromagnetic stirring is generated due to the interaction of a direct current, which is injected radially through ring-shaped electrodes located at the equatorial zone of each sphere, and a dipolar magnetic field produced by a permanent magnet located inside the inner sphere. Experimental velocity fields in the equatorial plane were obtained with particle image velocimetry. Additionally, full three-dimensional numerical simulations were performed. The high shearing at the equatorial region promotes an instability that can be perceived as a triggering mechanism of four tornado-like vortical structures tilted and entangled in the polar direction. The instability structure rotates in either the cyclonic or the anticyclonic direction, depending on the flow parameters, namely, the angular velocity of the outer sphere and the applied electric current. To the best knowledge of the authors, this is the first time the phenomenon under study is reported with electromagnetic forcing. The numerical results agree quantitatively with the experimental observations.

Information

Type
JFM Papers
Copyright
© The Author(s), 2023. Published by Cambridge University Press
Figure 0

Figure 1.An electrolytic solution fills the gap between the outer and inner spheres with radii $r_o$ and $r_i$, respectively. The outer sphere rotates at constant angular speed $\boldsymbol {\varOmega }$. The inner sphere is at rest and encloses a cylindrical permanent magnet, which produces the imposed dipolar magnetic field $\boldsymbol {B}^{0}$. The DC electric current $\boldsymbol {j}^{0}$ is mainly radial and is injected through two copper ring electrodes located at the equator of the spheres. The main direction of the Lorentz force is denoted by $\boldsymbol {F}^0$. The flow is visualized in a section of the equatorial plane with PIV. (a) Three-dimensional model of the experimental set-up. (b) Physical model (not drawn to scale).

Figure 1

Figure 2.Electromagnetic stirring and rotating external sphere. (a) Time-averaged velocity field of the flow at the equator ($\phi ={\rm \pi} /2$); experimental PIV observation. (b) Radial profile of the azimuthal velocity $u_{\theta }$ as function of the $r$-coordinate at the equator. The markers and the continuous line denote experimental measurements and numerical results, respectively. Here, $E_k=8.12 \times 10^{-4}$ and $\varLambda _L=2.15 \times 10^{-2}$ ($I=50$ mA, $\varOmega =0.251\,{\rm rad}\,{\rm s}^{-1}$).

Figure 2

Figure 3.Time-averaged plot at the meridional plane. The arrows denote the sense of rotation of the vortices for the streamlines. Here, $E_k=8.12 \times 10^{-4}$ and $\varLambda _L=2.15 \times 10^{-2}$ ($I=50$ mA, $\varOmega =0.251\,{\rm rad}\,{\rm s}^{-1}$). Numerical simulations. (a) Azimuthal velocity $u_{\theta }$ map. (b) Poloidal streamlines.

Figure 3

Figure 4.Instantaneous velocity fields at the equatorial plane: (a) $t=300$ s, (b) $t=307$ s. Cyclonic rotation of the instability. Here, $E_k=8.12 \times 10^{-4}$ and $\varLambda _L=2.15 \times 10^{-2}$ ($I=50$ mA, $\varOmega =0.251\,{\rm rad}\,{\rm s}^{-1}$). Experimental observations.

Figure 4

Figure 5.Three-dimensional structure of the instability. Instantaneous streamlines plotted at the marked planes parallel to the equator: (a) $z=0$ m, (b) $z=0.01$ m, (c) $z=0.02$ m, and (d) $z=0.04$ m. Instantaneous three-dimensional streamlines coloured by the angular velocity: (e) isometric view, ( f) side view. Cyclonic rotation of the instability. Here, $E_k=8.12 \times 10^{-4}$ and $\varLambda _L=2.15 \times 10^{-2}$ ($I=50$ mA, $\varOmega =0.251\,{\rm rad}\,{\rm s}^{-1}$). The arrows denote the directions of rotation of the vortices for the streamlines. The red triangle and disc are markers for mapping the position between two-dimensional and three-dimensional figures. The streamlines are coloured according to the angular velocity $\omega$. Numerical simulations.

Figure 5

Figure 6.Instantaneous three-dimensional streamlines: (a) $Ro=1.7$, $E_k=6.5 \times 10^{-3}$, $\varLambda _L=1.38$ ($\varOmega =0.031\,{\rm rad}\,{\rm s}^{-1}$); (b) $Ro=0.85$, $E_k=3.25 \times 10^{-3}$, $\varLambda _L=0.345$ ($\varOmega =0.063\,{\rm rad}\,{\rm s}^{-1}$); (c) $Ro=0.426$, $E_k=1.62 \times 10^{-3}$, $\varLambda _L=8.62 \times 10^{-2}$ ($\varOmega =0.126\,{\rm rad}\,{\rm s}^{-1}$); (d) $Ro=0.284$, $E_k=1.08 \times 10^{-3}$, $\varLambda _L=3.83 \times 10^{-2}$ ($\varOmega =0.188\,{\rm rad}\,{\rm s}^{-1}$); (e) $Ro=0.213$, $E_k=8.12 \times 10^{-4}$, $\varLambda _L=2.15 \times 10^{-2}$ ($\varOmega =0.251\,{\rm rad}\,{\rm s}^{-1}$); ( f) $Ro=0.17$, $E_k=6.5 \times 10^{-4}$, $\varLambda _L=1.38 \times 10^{-2}$ ($\varOmega =0.314\,{\rm rad}\,{\rm s}^{-1}$). The streamlines are coloured according to the angular velocity $\omega$. For all cases, $I=50$ mA. Numerical simulations.

Figure 6

Figure 7.Instability map (regime diagram). (a) Dimensionless parameters $E_k$ and $\varLambda _L$. (b) Experimental parameters and their associated Reynolds numbers. Here, $\bullet$ indicates stable flow, $\odot$ indicates cyclonic rotation, ${_\bigtriangleup}$ indicates oscillation, $\square$ indicates anticyclonic rotation, $\blacksquare$ indicates internal vibration, and $\blacktriangle$ indicates external vibration. Numerical simulations.

Figure 7

Figure 8.Time-averaged meridional plane of the vorticity: (a) $r$-component, (b) $\theta$-component. Here, $E_k=8.12 \times 10^{-4}$ and $\varLambda _L=2.15 \times 10^{-2}$ ($I=50$ mA, $\varOmega =0.251\,{\rm rad}\,{\rm s}^{-1}$). Numerical simulations.

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