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The combined influences of Hall currents and rotation on the MHD Couette flow of a viscous incompressible electrically conducting fluid between two infinite horizontal parallel porous plates channel in a rotating system in the presence of a uniform transverse magnetic field have been carried out. The solutions for the velocity field as well as shear stresses have been obtained for small time as well as for large times by Laplace transform technique. It is found that for large times the Hall currents accelerates primary flow whereas it retards secondary flow while the rotation retards the primary flow whereas it accelerates the secondary flow. It is also found that the velocity components converge more rapidly for small time solution than the general solution. The asymptotic behavior of the solution is analyzed for small as well as large values of magnetic parameter <i>M</i><sup>2</sup>, rotation parameter <i>K</i><sup>2</sup> and Reynolds number <i>R</i><sub><i>e</i></sub>. It is observed that a thin boundary layer is formed near the moving plate of the channel and the thicknesses of the layer increases with increase in either Hall parameter <i>m</i> or Reynolds number <i>R</i><sub><i>e</i></sub> while it decreases with increase in Hartmann number <i>M</i>. It is interesting to note that for large values of <i>M</i><sup>2</sup> , the boundary layer thickness is independent of the rotation parameter.

In most of the cases, the Hall term is ignored by applying Ohm’s law as it has no marked effect for small magnetic fields. However, to study the effects of strong magnetic fields on the electrically conducting fluid flow, we see that the influence of the electromagnetic force is noticeable and causes anisotropic electrical conductivity in the plasma. This anisotropy in the electrical conductivity of the plasma produces a current known as the Hall current. The Hall effect is important when the magnetic field is strong or when the collision frequency is low, causing the Hall parameter to be significant (Sutton and Sherman [

In the present paper we have studied the combined effects of Hall current and rotation on the MHD Couette flow of a viscous incompressible electrically conducting fluid between two infinite horizontal parallel porous plates channel in a rotating system when one of the plate moving with uniform velocity and the other one held at rest. The solutions for the velocity distributions as well as shear stresses have been obtained for small times as well as for large times by Laplace transform technique. It is found that for large times the primary velocity increases while the magnitude of the secondary velocity decreases with increase in Hall parameter. It is also found that for large times the primary velocity decreases while the magnitude of the secondary velocity increases with an increase in rotation parameter. Further, the velocity components converge more rapidly for small time solution than the general solution. The asymptotic behavior of the solution is analyzed for small as well as large values of magnetic parameter, rotation parameter and Reynolds number. It is observed that a thin boundary layer is formed near the stationary plate and the thicknesses of the layer increases with increase in either Hall parameter or Reynolds number while it decreases with increase in Hartmann number. It is interesting to note that for large values of, the boundary layer thickness is independent of the rotation parameter.

Consider unsteady MHD flow of a viscous incompressible electrically conducting fluid between two infinite parallel porous plates separated by a distance when both the fluid and channel rotate in unison about an axis normal to the plates with a uniform angular velocity. Choose a cartesian co-ordinate system with -axis along the lower stationary plate in the direction of the flow, the -axis is normal to the plates and the -axis perpendicular to -plane. A uniform magnetic field imposed perpendicular to the plates. The flow within the channel is induced due to the movement of the upper plate parallel to itself in -direction with a uniform velocity. Initially (), fluid as well as plates of the channel are assumed to be at rest. When time, the upper plate starts to move with uniform velocity along - direction in its own plane while the lower plate (z = 0) is kept fixed. Let the velocity components be relative to a frame of reference rotating with the fluid. Since the plates of the channel are infinite long and directions and are electrically nonconducting all physical quantities, except pressure, will be functions of and only. Suction/

injection of the fluid takes place through the porous plates of the channel with uniform velocity which is for suction and is for injection. The equation of continuity then gives everywhere in the fluid.

Neglecting ion-slip and thermoelectric effects, the generalised Ohm’s law for partially ionized gas is [see Cowling[

where, , , , , and are respectively, the magnetic field vector, the electric field vector, the fluid velocity vector, the current density vector, the conductivity of the fluid, the cyclotron frequency and the electron collision time.

We shall assume that the magnetic Reynolds number for the flow is small so that the induced magnetic field can be neglected in comparison to the applied one. This assumption is justified since the magnetic Reynolds number is generally very small for metallic liquids and partially ionized fluids. The solenoidal relation for the magnetic field gives constant constant everywhere in the fluid where. The equation of conservation of charge gives constant. This constant is zero since at the plates which are electrically non-conducting. Thus everywhere in the flow. Since the induced magnetic field is neglected, the Maxwell’s equation

becomes which gives and. This implies that constant and constant everywhere in the flow.

In view of the above assumption and on taking, Equation (1) gives

where is the Hall parameter. Solving for and, we get

On the use of Equations (4) and (5), the equations of motion along -and -directions are

where, and are respectively the fluid density, the kinematic coefficient of viscosity and the modified fluid pressure including centrifugal force.

The initial and the boundary conditions are

Introducing the non-dimensional variables

Equations (6) and (7) become

where is the Hartmann number, the rotation parameter and the Reynolds number.

Combing Equations (11) and (12), we have

where

The initial and the boundary conditions for are

For general solution, the method given in Batchelor [

where first term on the right hand side is the steady-state solution, shows the departure from the steady-state and

Now, satisfies the following differential equation

with

Taking Laplace’s transform of Equation (19), we get

where

The corresponding boundary conditions for are

The solution of the Equation (21) subject to the boundary conditions (23) is

where

Taking inverse Laplace’s transform of the Equation (24), we have

On the use of Equation (17), we have

where

On separating into real and imaginary parts and using Equation (10), we get

where

The solutions given by Equations (29) and (30) exist for both (corresponding to for the blowing at the plates) and (corresponding to for the suction at the plates). If and, then the above Equations (29) and (30) are identical with Equations (26) and (27) of Das et al. [

Following Carslaw and Jaegar [

where

(33)

The solution (32) can be written as

where

(35)

On separating into real and imaginary parts and using Equation (14), we get the velocity distributions for the primary and the secondary flow as

The Equations (36) and (37) describe the fluid velocities for small times. If and, the Equations (36) and (37) coincide with Equations (17) and (18) of Das et al. [

To study the effects of rotation, suction/blowing and Hall parameter on the velocity distributions we have presented the non-dimensional velocity components and against in Figures 2-6 for various values of magnetic parameter, the rotation parameter, Hall parameter, Reynolds number and time. It is seen from

(37) converges more rapidly than the general solution given by (29) and (30). Hence, we conclude that for small times, the numerical values of the velocity components can be evaluated from the Equations (36)

and (37) instead of Equations (29) and (30).

For large time, the non-dimensional shear stresses due to the primary and the secondary flows at the stationary plate are given by

On separating real and imaginary parts, we get the shear stress components due to the primary and secondary flows at the stationary plate () as

(39)

The numerical values of and are presented in Figs.9-12 against Hall parameter for various values of, , and. It is seen from

For small times, the non-dimensional shear stresses due to the primary and secondary flows at the stationary plate () are given by

where

(42)

On separating real and imaginary parts, we get the shear stress components due to the primary and secondary flow as

We shall now discuss the asymptotic behavior of the solutions (29) and (30) for small and large values of, and:

Case(i): When, and.

When is large, and are of small order of magnitude, the flow becomes boundary layer type. For the boundary layer flow near the upper plate, introducing the boundary layer coordinate, we obtain the velocity distributions from (29) and (30) as

where

(46)

It is evident from Equations (44)and (45) that there arises a single-deck boundary layer of thickness of order

near the moving plate () of the channel where is given by (46). The thickness of this boundary layer increases with increase in either Hall parameter or rotation parameter since decreases with increase in either or. On the other hand, it decreases with increase in either Hartmann number or as increases with increase in either or.

Case(ii): When, and.

In this case, the velocity distributions are obtained from the Equations (29) and (30) as

where

(49)

The Equations (47) and (48) reveal that there appears a single-decker boundary layer of thickness of the order

adjacent to the moving plate ()

of the channel where is given by (49). The thicknesses of the layer increases with increase in either Hall parameter or Reynolds number while it decreases with increase in Hartmann number. It is interesting to note that for large values of, the boundary layer thickness is independent of the rotation parameter.

Case(iii): When, and.

In this case, Equations (28) and (29) become

where

It is seen from Equations (50) and (51) that there exists a single-deck boundary layer of thickness of order

where is given by (52). It is seen that the thickness of this boundary layer increases with increase in either Hall parameter or Reynolds number since decreases with increase in either or. On the other hand, it decreases with increase in squared-Hartmann number as increases with increase in.

To study the effects of Hall current, rotation, magnetic field, suction/injection and time on the flow field, the primary and secondary velocities and shear stress at the stationary plate due to the primary and secondary flows are depicted graphically for various values of, , , and. It is found that for large time the primary velocity increases while the magnitude of the secondary velocity decreases with increase in Hall parameter. It is also found that for large time the primary velocity decreases while the magnitude of the secondary velocity increases with an increase in rotation parameter. It is also found that the solution for small time converges more rapidly than the general solution. The asymptotic behavior of the solution is analyzed for small as well as large values of magnetic parameter, rotation parameter and Reynolds number. It is observed that a thin boundary layer is formed near the stationary plate and the thicknesses of the layer increases with increase in either Hall parameter or Reynolds number while it decreases with increase in Hartmann number. It is interesting to note that for large values of, the boundary layer thickness is independent of the rotation parameter. The expression for the shear stress at the stationary plate due to the primary and secondary flows is obtained in both the cases.