Hostname: page-component-cd9895bd7-jkksz Total loading time: 0 Render date: 2024-12-19T01:26:26.159Z Has data issue: false hasContentIssue false

Liquid-metal flow in a thin conducting pipe near the end of a region of uniform magnetic field

Published online by Cambridge University Press:  21 April 2006

John S. Walker
Affiliation:
Department of Theoretical and Applied Mechanics, University of Illinois, Urbana, IL 61801, U.S.A.

Abstract

This paper treats the liquid-metal flow in a straight circular pipe with a thin metal wall. A strong magnetic field is applied by a magnet with parallel poles that end abruptly. In the plane midway between the magnet poles: (a) far upstream, the flow is uniform, fully developed in a uniform magnetic field; (b) as the flow enters the non-uniform magnetic field near the end of the magnet, the flow moves away from the central part of the pipe and becomes concentrated as two jets near the points where the magnetic field is tangential to the pipe wall; (c) further downstream where the magnetic field strength is O(c) compared with its value upstream, the flow migrates from these jets back towards a uniform flow distributed over the entire pipe cross-section. Here, c is the wall conductance ratio, which is assumed to be small. The analysis also applies to flow into the magnetic field, because inertial effects and induced magnetic fields are neglected. There are circulations of electric current in planes parallel to the magnet poles. These currents produce a pressure drop in addition to that for two fully developed flows in a uniform magnetic field and in no magnetic field, joined at the end of the magnet. This pressure drop is given by 0.9336 $\beta^{\frac{1}{3}}c^{\frac{2}{3}}\sigma$V0B20L, where β is a measure of the magnetic field gradient with a minimum value of 2/π, σ is the liquid metal's electrical conductivity, V0 is the average velocity, B0 is the strength of the uniform magnetic field, and L is the inside radius of the pipe. This three-dimensional pressure drop is $O(c^{-\frac{1}{3}}L) $ times the pressure gradient for the fully developed flow in the uniform magnetic field.

Type
Research Article
Copyright
© 1986 Cambridge University Press

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Branover, H. 1978 Magnetohydrodynamic Flow in Ducts. John Wiley.
Holroyd, R. J. 1980 An experimental study of the effects of wall conductivity, non-uniform magnetic fields and variable area ducts on liquid metal flows at high Hartmann number. 2. Ducts with conducting walls. J. Fluid Mech. 96, 355.Google Scholar
Holroyd, R. J. & Mitchell, J. T. D. 1984 Liquid lithium as a coolant for Tokamak fusion reactors. Nuclear Engineering and Design/Fusion 1, 17.Google Scholar
Holroyd, R. J. & Walker, J. S. 1978 A theoretical study of the effects of wall conductivity, non-uniform magnetic fields and variable-area ducts on liquid-metal flows at high Hartmann number. J. Fluid Mech. 84, 471.Google Scholar
Roberts, P. H. 1967 Singularities of Hartmann layers. Proc. R. Soc. Lond. A 300, 94.Google Scholar
Shercliff, J. A. 1956 The flow of conducting Fluids in circular pipes under transverse magnetic fields. J. Fluid Mech. 1, 644.Google Scholar
Shercliff, J. A. 1965 A Textbook of agnetohydrodynamics, Pergamon.
Walker, J. S. & Buckmaster, J. D. 1979 Ferrohydrodynamic thrust bearings. Intl J. Engng Sci. 17, 1171.Google Scholar