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E. Omokhuale, I. J. Uwanta, A. A. Momoh, A. Tahir. / International Journal of Engineering
              Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com
                        Vol. 2, Issue5, September- October 2012, pp.885-892
The Effects of Concentration and Hall Current on Unsteady Flow
              of a Viscoelastic Fluid in a Fixed Plate
                 1
                     E. Omokhuale, 1I. J. Uwanta,2A. A.Momoh, 2 A. Tahir.
            1
            Department of Mathematics, UsmanuDanfodiyo University, P. M. B. 2346, Sokoto, Nigeria
.2
     Department of Mathematics, Modibbo Adama University of Technology, P.M.B. 2076, Yola. Adamawa State.
                                                 Nigeria

ABSTRACT
         The present Study deals with the effects        numerically. Kai- Long (2010) studied Heat and
of concentration and Hall current on                     mass transfer for a viscous flow with radiation effect
unsteadyflow of a viscoelastic fluid in a fixed          past a non-linear stretching sheet. Hall Effect on
plate. The resultant equations have been solved          MHD mixed convective flow of a viscous
analytically. The velocity, temperature and              incompressible fluid past a vertical porous plate
concentration distributions are derived, and their       immersed in a porous medium with Heat
profiles for various physical parameters are             Source/Sink was studied by Sharma et al. (2007).
shown through graphs. The coefficient of Skin            Salehet al. (2010) examined Heat and mass transfer
friction, Nusselt number and Sherwood number             in MHD viscoclastic fluid flow through a porous
at the plate are derived and their numerical             medium over a stretching sheet with chemical
values for various physical parameters are               reaction. Das and Jana (2010) examined Heat and
presented through tables. The influence of               Mass transfer effects on unsteady MHD free
various parameters such as the thermal Grashof           convection flow near a moving vertical plate in a
number, mass Grashof number, Schmidt                     porous medium. The effects of chemical reaction,
number, Prandtl number, Hall Parameter,                  Hall current and Ion – Slip currents on MHD
Hartmann       number,     Chemical       Reaction       micropolar fluid flow with thermal Diffusivity using
parameter and the frequency of oscillation on the        Novel Numerical Technique was studied by Motsa
flow field are discussed. It is seen that, the           and Shateyi (2012). Aboeldahab and Elbarby (2001)
velocity increases with the increase in Gc and           examined        Hall       current      effect      on
Gr,and it decreases with increase in Sc, M, m, Kc,       Magnetohydrodynamics free convection flow past a
and Pr, temperature decreases with increase in           Semi – infinite vertical plate with mass transfer. Hall
Pr, Also, the concentration decreases with the           current effect with simultaneous thermal and mass
increase in Sc and Kc.                                   diffusion on unsteady hydromagnetic flow near an
                                                         accelerated vertical plate was investigated Acharyaet
KEY WORDS: Hall Current, Viscoelastic, Porous            al. (2001). Takhar (2006) studied Unsteady flow free
medium, Magnetohydrodynamics.                            convective flow over an infinite vertical porous
                                                         platedue to the combined effects of thermal and
1.0 INTRODUCTION                                         mass diffusion, magnetic field and Hall current.
         There exist flows which are caused not only     Exact Solution of MHD free convection flow and
by temperature differences but also by concentration     Mass Transfer near a moving vertical porous plate in
differences. There are several engineering situations    the presence of thermal radiation was investigated
wherein combined heat and mass transport arise           by Das (2010). Anjali Devi and Ganga examined
such as dehumidifiers, humidifiers, desert coolers,      effects of viscous and Joules dissipation and MHD
and chemical reactors etc. Magnetohydrodynamics is       flow, heat and mass transfer past a Stretching porous
currently undergoing a period of great enlargement       surface embedded in a porous medium. Sonthet al.
and differentiation of subject matter. It is important   (2012) studied Heat and Mass transfer in a
in the design of MHD generators and accelerators in      viscoelastic fluid over an accelerated surface with
geophysics, underground water storage system, soil       heat source/sink and viscous dissipation. Shateyiet
sciences, astrophysics, nuclear power reactor, solar     al. (2010) investigated The effects of thermal
structures, and so on.                                   Radiation, Hall currents, Soret and Dufour on MHD
         Moreso, the interest in these new problems      flow by mixed convection over vertical surface in
generates from their importance in liquid metals,        porous medium. Effect of Hall currents and
electrolytes and ionized gases. On account of their      Chemical reaction and Hydromagnetic flow of a
varied importance, these flows have been studied by      stretching vertical surface with internal heat
several authors – notable amongst them are Singh         generation / absorption was examined by Salem and
and Singh (2012) they investigated MHD flow of           El-Aziz (2008).
Viscous Dissipation and Chemical Reaction over a
Stretching porous plate in a porous medium               2.0 MATHEMATICAL FORMULATION




                                                                                                885 | P a g e
E. Omokhuale, I. J. Uwanta, A. A. Momoh, A. Tahir. / International Journal of Engineering
                         Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com
                                   Vol. 2, Issue5, September- October 2012, pp.885-892
                      We consider the unsteady flow of a viscous                volume        expansion, k 0 is      the       kinematic
            incompressible      and    electrically    conducting
            viscoelastic fluid over afixed porous plate with                    viscoelasticity,  is the density,  is the viscosity,
            oscillating temperature. The x- axis is assumed to be               is the kinematic viscosity, KT is the thermal
            oriented vertically upwards along the plate and the                 conductivity, Cp is the specific heat in the fluid at
            y-axis is taken normal to the plane of the plate. It is             constant pressure,  is the electrical conductivity of
            assumed that the plate is electrically non –                        the fluid,  e is the magnetic permeability, D is the
            conducting and a uniform magnetic field of straight
                                                                                molecular diffusivity, T0 is the temperature of the
             B0 is applied normal to the plate. The induced
            magnetic field is assumed constant. So that                         plane and Td is the temperature of the fluid far away
             
             B   0, B0 ,0 ,. The plate is subjected to a constant            from plane. C 0 is the concentration of the plane and
         suction velocity.                                          Cd is the concentration of the fluid far away from
1.
   The equation of conservation of charge J  0, gives constant. the plane.
                                                                   And v  v0 , the negative sign indicate that the
                                       Pe                  suction is towards the plane.
         2.
               J  e e ( J  E )   V  B        (1)         Introducing the following non-dimensionless
                                                ene 
                                                                                parameters
            Equation (1) reduces to                                                    v0 y      v 2t    u     *    T  T       C  C                
                        B0                                                              , t  0 , u  ,   ,          ,C                        
                           2 
             J x*              mu*   *                                                      4     v0    v0    T  T      C  C               
                    (1  m )                
                                                                                    g  (T  T )          g  c (C  C )       B0 2        Cp 
                                                                                                                                                        
                       B0                                                      Gr                   , Gc                     ,M          , Pr      
             J y* 
                    (1  m2 )
                               u  m 
                                 *      *             (2)                                 v0 2
                                                                                                                      v0 2
                                                                                                                                       v0 2
                                                                                                                                                     KT 
                                                                                                                                                       
                                                                                              k1v0 2     k *v0 2
            Where                                                               Sc  , K  2 , k  2                                                    
                                                                                     D          4                                                     
                                                                                                                                                        
             m  e e
            is the Hall parameter.                                                                                       (8)
            The governing equations for the momentum, energy                    Substituting the dimensionless variables in (8) into
            and concentration are as follows;                                   (3) to (6), we get (dropping the bars)

   u u u         3u      (u  m )                                     u   1 u u  2u K  3u M (u  m ) u
      v0    k1 2   B02             g  (T  Td )  g  * (C  Cd )  *                                    Gr  GcC
   t y y y t             (1  m )
                                     2
                                                                           k    4 t   2 4 2 t   (1  m 2 )  k
                                                                                                                   
                        (3)                                                     (9)
              2     3       (  mu ) u                                1    2 K  3 M (  mu ) u
       v0      2  k1 2   B0 2                                                                           
   t      y    y     y t        (1  m 2 ) k *                            4 t   2 4 2 t   (1  m 2 )   k
                                                                   (4)
                                                                                           (10)
             T      T  K T             2
                 v0     T                                                     1   1  2
             t      y  Cp y 2                                                     
                                                                                4 t  Pr  2
                                              (5)                                                              (11)
             C      C    C         2
                                                                                1 C C 1  C           2
                 v0     D 2  KrC                                                   
             t      y    y                                                   4 t  Sc  2
                                     (6)                                        (12)
            The boundary conditions of the problem are:                         The corresponding boundary conditions are
   u  0,   0, T  Td  (T0  Td )eit , C  Cd  (C0  Cd )eit aty  0      u(0, t )  0,  (0, t )  0, (0, t )  eit , C (0, t )eit aty  0
   u  0,   0, T  0, C  0aty  1                                            u(1, t )   (1, t )   (1, t )  C (1, t )  0aty  1
              (7)                                                                          (13)
            Where u and v are the components of velocity in the
            x and y direction respectively, g is the acceleration               Equations (9) and (10) can be combined into a single
            due to gravity,          and  are the coefficient of
                                              *
                                                                                equation by introducing the complex velocity.



                                                                                                                          886 | P a g e
E. Omokhuale, I. J. Uwanta, A. A. Momoh, A. Tahir. / International Journal of Engineering
                    Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com
                              Vol. 2, Issue5, September- October 2012, pp.885-892
         U  u , t   i , t                                                       Solving (20) to (22) under the boundary
                                                                                conditions (23) and (25).And substituting the
                                                          (14)                  obtained solutions into (17) to (19) respectively.
                                                                                Then
         Where                                                                  the velocity distribution can be expressed as
         i  1                                                                 U (, t )   A5em5  A6em6  A8em3  A9em4  A10em1  A11em2   eint
                                                                                                                                                      
         Thus,                                                                  (24)
1 U U  2U K  3U M (1  im)U U                                               And, the temperature field is given by
                                 Gr  GcC
4 t   2 4 2 t   (1  m 2 )  k                                            ( , t )   A3em   A4e m    ei t
                                                                                                     3           4


                                                                    (15)        (25)
         With boundary conditions:                                              Similarly, the concentration distribution gives
    t  0 : U (0, t )  0, (0, t )  eit , C (0, t )eit at  0
     *
                                                                                C ( , t )   A1em1  A2e m2   ei t
   U (1, t )   (1, t )  C (1, t )  0, at  1                                                                      (26)
                                                                                       The Skin friction, Nusselt number and
                                                      (16)                      Sherwood number is obtained by differentiating (24)
                 where Gr is the thermal Grashof number,
                                                                                to (26) and at
                                                                                                 evaluated at   0 respectively. .
         Gc is the mass Grashof number, Sc is the Schmidt
         number, Pr is the Prandtl number, Rm is the Reynold                        U ( , t )
         number, K is the viscoelastic Parameter and S is the                                    m5 A5  m6 A6  m3 A8  m4 A9  m1 A10  m2 A11   ei t
         pearmeability.                                                                 0
                                                                                                                                  (27)
         3.0 METHOD OF SOLUTIONS                                                     ( , t )
         To solve (11), (12) and (15) subject to the boundary                                    m3 A3  m4 A4   ei  t
         conditions (16), we assume solutions of the form                               0
         U (, t )  U1    eit                                                                      (28)
                                                                                    C ( , t )
                                                                   (17)
                                                                                                 m1 A1  m2 A2 
          ( , t )  1 ( ) e   i t
                                                                                        0
                                                                   (18)                                                          (29)
         C(, t )  C1    e       it
                                            (19)
                                                                                4.0 RESULTS AND DISCUSSION
         where U1      1             and      C1   are   to      be            The effects of concentration and Hall
         determined.                                                            current on unsteady flow of a viscoelastic fluid in a
         Substituting (17) to (19) into (11), (12) and (15),                    fixed plate has been formulated and solved
         Comparing harmonic and non harmonic terms, we                          analytically. In order to understand the flow of the
         obtain                                                                 fluid, computations are performed for different
                                                                                parameters such as Gr, Gc, Sc, Pr,  , Kc, M, and
                  U            Gr         GcC
         U         L3U         it
                                                                               m.
                  L1           4 L1e       4 L1eit
                                                                                4.1 Velocity profiles
                                              (20)                                       Figures 1 to 7connote the velocity profiles;
                          1
         1  Pr 1  i1  0
                                                                                figure 8 depicts the temperature profiles and
                                                                                figures9& 10display the concentration profiles with
                          4
                                                                                varying parameters respectively.
                              (21)                                                       The effect of velocity for different values of
                      1                                                         (Pr = 0.71, 1, 3) is displayed in figure 1, the graph
         C1 ScC1  iC1  KcScC1  0                                        show that velocity decreases with increase in Pr.
                      4                  (22)                                   The effect of velocity for different values of (Sc =
         and boundary conditions give                                           0.18, 0.78, 2.01, 2.65) is given in figure 2, the graph
           0 : U1 (0)   (0)  C (0)  1                                    show that velocity decreases with the increase in Sc.
                                                                                Figure 3 denotes the effect of velocity for different
                                               
           1: U1 (1)  0, (1)  0, C (1)  0                                values of (m = 2, 4, 6, 10), it is seen that velocity
                                                                                decreases with the increase in m.
                              (23)
                                                                                The effect of velocity for different values of (M = 1,
         where the primes connotes differentiation with
         respect to  .
                                                                                3, 6, 10) is shown in figure 4, it depict that velocity
                                                                                decreases with increase in M.



                                                                                                                             887 | P a g e
E. Omokhuale, I. J. Uwanta, A. A. Momoh, A. Tahir. / International Journal of Engineering
           Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com
                     Vol. 2, Issue5, September- October 2012, pp.885-892
Figure 5 depicts the effect of velocity for (Gr = 1, 2,       The effect of velocity for different values of (Kc = 1,
3, 5), the graph connote that velocity increases with         2, 3, 4) is displayed in figure 7, it is clear that
the increase in Gr.                                           velocity decreases with the increase in Kc.
          The effect of velocity for different values of
(Gc = 2, 3, 4, 8) is presented in figure 6, it is seen
that velocity increases with the increase in Gc.




         Figure 1. Velocity profiles for different values of Pr.




         Figure 2. Velocity profiles for different values of Sc.




                                                                                                     888 | P a g e
E. Omokhuale, I. J. Uwanta, A. A. Momoh, A. Tahir. / International Journal of Engineering
           Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com
                     Vol. 2, Issue5, September- October 2012, pp.885-892




Figure 3. Velocity profiles for different values of m.




                  Figure       4.      Velocity          profiles   for     different   values       of     M
                  .




                  Figure 5. Velocity profiles for different values of Gr.




                                                                                                 889 | P a g e
E. Omokhuale, I. J. Uwanta, A. A. Momoh, A. Tahir. / International Journal of Engineering
           Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com
                     Vol. 2, Issue5, September- October 2012, pp.885-892




Figure 6. Velocity profiles for different values of Gc.




Figure 7. Velocity profiles for different values of Kc.

4.2      Temperature profiles
In figure 8, the effect of temperature for different
values of (Pr = 0.71, 1, 3, 7) is given. The graph
show that temperature increases with increasing Pr.




         Figure 8. Temperature profiles for different values of Pr.



                                                                                 890 | P a g e
E. Omokhuale, I. J. Uwanta, A. A. Momoh, A. Tahir. / International Journal of Engineering
           Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com
                     Vol. 2, Issue5, September- October 2012, pp.885-892
4.3      Concentration profiles                                concentration for (Kc= 0, 0.5, 1, 3) is given in figure
Figure 9 depicts the effect of concentration for (Sc =         10, it is seen that concentration decreases with the
0.3, 0.78, 1, 2.01), it is seen that concentration             decrease in Kc.
increases with the increase in Sc. The effect of




Figure 9. Concentration profiles for different values of Sc.




Figure 10. Concentration profiles for different values of Kc.

Table 1 to 3 represent the Skin friction, Nusselt              Table 2: Nusselt number
number and Sherwood number respectively.                                       Pr                  Nu
Table 1 depicts that the Skin friction increases with          1                0.71                0.8181
increase in Gc and Grand decreases with increase in            4                0.71                0.7400
Sc, m, M, Kc, and Pr.                                          1                3                   0.7830
Table 2 represents that the Nusselt number decreases
with increase in Pr, and decreases with increase in           Table 3: Sherwood number
Table 3 shows that the Sherwood number decreases                              Sc                   Sh
with increase in Sc and  .                                    1               0.3                  0.4015
                                                               5               0.3                  0.3890
Table 1: Skin friction                                        4               0.6                  0.3977
 Gc Sc Kc Gr                M    Pr     M     
1    1     0.3 0.1 1         1    0.71   0.5   6.1082          5.0 SUMMARY AND CONCLUSION
3    1     0.3 0.1 1         1    0.71   0.5   5.5219                   We have examined and solved the
1    1     0.6 0.1 1         1    0.71   0.5   5.7548          governing equations for the effects of concentration
1    4     0.3 0.1 1         1    0.71   0.5   6.5671          and Hall current on unsteady flow of a viscoelastic
1    1     0.3 1        1    1    0.71   0.5   6.3654          fluid in a fixed plate analytically. In order to point
1    1     0.3 0.1 4         1    0.71   0.5   6.8760          out the effect of physical parameters namely;
1    1     0.3 0.1 1         3    3      0.5   5.9006          thermal Grashof number, mass Grashof number,
1    1     0.3 0.1 1         1    0.71   2     5.0126          Schmidt number, Prandtl number, Chemical reaction
1    1     0.3 0.1 1         1    0.71   0.5   6.8741          parameter, Hartmann number, Hall parameter and



                                                                                                      891 | P a g e
E. Omokhuale, I. J. Uwanta, A. A. Momoh, A. Tahir. / International Journal of Engineering
           Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com
                     Vol. 2, Issue5, September- October 2012, pp.885-892
the frequency of oscillation on the flow field and the   8.    Salem, A. M. and El-Aziz, M. Abd. (2008).
following conclusions are drawn:                               Effect of Hall currents and Chemical
*The velocity increases with the increase in Gc and            reaction and Hydromagnetic
Gr.                                                            flow of a stretching vertical surface with
*The velocity falls due to increasing in Sc,  , M, m,         internal heat generation / absorption.
Kc, and Pr.                                                    Applied Mathematical Modelling: 32, 1236
*The temperature decreases with increase in Pr,                – 1254.
*The concentration reduces with the increase in Sc       9.    Saleh, M.A.,Mohammed ,A.A.B. and
and Kc.                                                        Mahmoud S.E. (2010). Heat and mass
*The Skin friction increases with increase in Gc and           transfer in MHD viscoclastic fluid flow
Gr and decreases with increase in Sc, M, m,Kc, and             through a porous medium over a stretching
Pr.                                                            sheet with chemical reaction. Journal of
*The rate of heat transfer decreases with increase in          Applied Mathematics, 1, 446-455.
Pr and  ,
*The Sherwood number decreases with the increase         10.   Shateyi, S., Motsa, S. S. and Sibanda, P.
in Sc and  .                                                  (2010). The effects of thermal Radiation,
                                                               Hall currents, Soret and
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         AJMP.8(1). 29 – 41.                                   Heat and Mass Transfer. 39, 823 – 834.
  6.     Kai- Long, H. (2010). Heat and mass
         transfer for a viscous flow with radiation
         effect past a non-linear stretching sheet.
         World Academy of Science, Engineering
         and Technology, 62(3), 326-330.
  7.     Motsa, S. S. and Shateyi, S. (2012). The
         effects of chemical reaction, Hall current
         and Ion – Slip currents on
         MHD micropolar fluid flow with thermal
         Diffusivity using Novel Numerical
         Technique.Journal of Applied Mathematics.
         10. 115 – 1165.



                                                                                            892 | P a g e

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Er25885892

  • 1. E. Omokhuale, I. J. Uwanta, A. A. Momoh, A. Tahir. / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 2, Issue5, September- October 2012, pp.885-892 The Effects of Concentration and Hall Current on Unsteady Flow of a Viscoelastic Fluid in a Fixed Plate 1 E. Omokhuale, 1I. J. Uwanta,2A. A.Momoh, 2 A. Tahir. 1 Department of Mathematics, UsmanuDanfodiyo University, P. M. B. 2346, Sokoto, Nigeria .2 Department of Mathematics, Modibbo Adama University of Technology, P.M.B. 2076, Yola. Adamawa State. Nigeria ABSTRACT The present Study deals with the effects numerically. Kai- Long (2010) studied Heat and of concentration and Hall current on mass transfer for a viscous flow with radiation effect unsteadyflow of a viscoelastic fluid in a fixed past a non-linear stretching sheet. Hall Effect on plate. The resultant equations have been solved MHD mixed convective flow of a viscous analytically. The velocity, temperature and incompressible fluid past a vertical porous plate concentration distributions are derived, and their immersed in a porous medium with Heat profiles for various physical parameters are Source/Sink was studied by Sharma et al. (2007). shown through graphs. The coefficient of Skin Salehet al. (2010) examined Heat and mass transfer friction, Nusselt number and Sherwood number in MHD viscoclastic fluid flow through a porous at the plate are derived and their numerical medium over a stretching sheet with chemical values for various physical parameters are reaction. Das and Jana (2010) examined Heat and presented through tables. The influence of Mass transfer effects on unsteady MHD free various parameters such as the thermal Grashof convection flow near a moving vertical plate in a number, mass Grashof number, Schmidt porous medium. The effects of chemical reaction, number, Prandtl number, Hall Parameter, Hall current and Ion – Slip currents on MHD Hartmann number, Chemical Reaction micropolar fluid flow with thermal Diffusivity using parameter and the frequency of oscillation on the Novel Numerical Technique was studied by Motsa flow field are discussed. It is seen that, the and Shateyi (2012). Aboeldahab and Elbarby (2001) velocity increases with the increase in Gc and examined Hall current effect on Gr,and it decreases with increase in Sc, M, m, Kc, Magnetohydrodynamics free convection flow past a and Pr, temperature decreases with increase in Semi – infinite vertical plate with mass transfer. Hall Pr, Also, the concentration decreases with the current effect with simultaneous thermal and mass increase in Sc and Kc. diffusion on unsteady hydromagnetic flow near an accelerated vertical plate was investigated Acharyaet KEY WORDS: Hall Current, Viscoelastic, Porous al. (2001). Takhar (2006) studied Unsteady flow free medium, Magnetohydrodynamics. convective flow over an infinite vertical porous platedue to the combined effects of thermal and 1.0 INTRODUCTION mass diffusion, magnetic field and Hall current. There exist flows which are caused not only Exact Solution of MHD free convection flow and by temperature differences but also by concentration Mass Transfer near a moving vertical porous plate in differences. There are several engineering situations the presence of thermal radiation was investigated wherein combined heat and mass transport arise by Das (2010). Anjali Devi and Ganga examined such as dehumidifiers, humidifiers, desert coolers, effects of viscous and Joules dissipation and MHD and chemical reactors etc. Magnetohydrodynamics is flow, heat and mass transfer past a Stretching porous currently undergoing a period of great enlargement surface embedded in a porous medium. Sonthet al. and differentiation of subject matter. It is important (2012) studied Heat and Mass transfer in a in the design of MHD generators and accelerators in viscoelastic fluid over an accelerated surface with geophysics, underground water storage system, soil heat source/sink and viscous dissipation. Shateyiet sciences, astrophysics, nuclear power reactor, solar al. (2010) investigated The effects of thermal structures, and so on. Radiation, Hall currents, Soret and Dufour on MHD Moreso, the interest in these new problems flow by mixed convection over vertical surface in generates from their importance in liquid metals, porous medium. Effect of Hall currents and electrolytes and ionized gases. On account of their Chemical reaction and Hydromagnetic flow of a varied importance, these flows have been studied by stretching vertical surface with internal heat several authors – notable amongst them are Singh generation / absorption was examined by Salem and and Singh (2012) they investigated MHD flow of El-Aziz (2008). Viscous Dissipation and Chemical Reaction over a Stretching porous plate in a porous medium 2.0 MATHEMATICAL FORMULATION 885 | P a g e
  • 2. E. Omokhuale, I. J. Uwanta, A. A. Momoh, A. Tahir. / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 2, Issue5, September- October 2012, pp.885-892 We consider the unsteady flow of a viscous volume expansion, k 0 is the kinematic incompressible and electrically conducting viscoelastic fluid over afixed porous plate with viscoelasticity,  is the density,  is the viscosity, oscillating temperature. The x- axis is assumed to be is the kinematic viscosity, KT is the thermal oriented vertically upwards along the plate and the conductivity, Cp is the specific heat in the fluid at y-axis is taken normal to the plane of the plate. It is constant pressure,  is the electrical conductivity of assumed that the plate is electrically non – the fluid,  e is the magnetic permeability, D is the conducting and a uniform magnetic field of straight molecular diffusivity, T0 is the temperature of the B0 is applied normal to the plate. The induced magnetic field is assumed constant. So that plane and Td is the temperature of the fluid far away  B   0, B0 ,0 ,. The plate is subjected to a constant from plane. C 0 is the concentration of the plane and suction velocity. Cd is the concentration of the fluid far away from 1. The equation of conservation of charge J  0, gives constant. the plane. And v  v0 , the negative sign indicate that the       Pe  suction is towards the plane. 2. J  e e ( J  E )   V  B   (1) Introducing the following non-dimensionless  ene  parameters Equation (1) reduces to v0 y v 2t u * T  T C  C   B0   , t  0 , u  ,   ,  ,C   2  J x*  mu*   *    4 v0 v0 T  T C  C  (1  m )   g  (T  T ) g  c (C  C )  B0 2 Cp    B0 Gr  , Gc  ,M  , Pr   J y*  (1  m2 )  u  m  * *  (2) v0 2 v0 2  v0 2 KT     k1v0 2 k *v0 2 Where Sc  , K  2 , k  2  D 4    m  e e is the Hall parameter. (8) The governing equations for the momentum, energy Substituting the dimensionless variables in (8) into and concentration are as follows; (3) to (6), we get (dropping the bars) u u u  3u (u  m ) u 1 u u  2u K  3u M (u  m ) u  v0    k1 2   B02  g  (T  Td )  g  * (C  Cd )  *       Gr  GcC t y y y t  (1  m ) 2 k 4 t   2 4 2 t (1  m 2 ) k (3) (9)    2  3 (  mu ) u 1    2 K  3 M (  mu ) u  v0   2  k1 2   B0 2       t y y y t  (1  m 2 ) k * 4 t   2 4 2 t (1  m 2 ) k (4) (10) T T K T 2  v0  T 1   1  2 t y  Cp y 2   4 t  Pr  2 (5) (11) C C C 2 1 C C 1  C 2  v0  D 2  KrC   t y y 4 t  Sc  2 (6) (12) The boundary conditions of the problem are: The corresponding boundary conditions are u  0,   0, T  Td  (T0  Td )eit , C  Cd  (C0  Cd )eit aty  0 u(0, t )  0,  (0, t )  0, (0, t )  eit , C (0, t )eit aty  0 u  0,   0, T  0, C  0aty  1 u(1, t )   (1, t )   (1, t )  C (1, t )  0aty  1 (7) (13) Where u and v are the components of velocity in the x and y direction respectively, g is the acceleration Equations (9) and (10) can be combined into a single due to gravity,  and  are the coefficient of * equation by introducing the complex velocity. 886 | P a g e
  • 3. E. Omokhuale, I. J. Uwanta, A. A. Momoh, A. Tahir. / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 2, Issue5, September- October 2012, pp.885-892 U  u , t   i , t  Solving (20) to (22) under the boundary conditions (23) and (25).And substituting the (14) obtained solutions into (17) to (19) respectively. Then Where the velocity distribution can be expressed as i  1 U (, t )   A5em5  A6em6  A8em3  A9em4  A10em1  A11em2   eint   Thus, (24) 1 U U  2U K  3U M (1  im)U U And, the temperature field is given by       Gr  GcC 4 t   2 4 2 t (1  m 2 ) k  ( , t )   A3em   A4e m    ei t 3 4 (15) (25) With boundary conditions: Similarly, the concentration distribution gives t  0 : U (0, t )  0, (0, t )  eit , C (0, t )eit at  0 * C ( , t )   A1em1  A2e m2   ei t U (1, t )   (1, t )  C (1, t )  0, at  1 (26) The Skin friction, Nusselt number and (16) Sherwood number is obtained by differentiating (24) where Gr is the thermal Grashof number, to (26) and at evaluated at   0 respectively. . Gc is the mass Grashof number, Sc is the Schmidt number, Pr is the Prandtl number, Rm is the Reynold U ( , t ) number, K is the viscoelastic Parameter and S is the    m5 A5  m6 A6  m3 A8  m4 A9  m1 A10  m2 A11   ei t pearmeability.   0 (27) 3.0 METHOD OF SOLUTIONS  ( , t ) To solve (11), (12) and (15) subject to the boundary    m3 A3  m4 A4   ei  t conditions (16), we assume solutions of the form   0 U (, t )  U1    eit (28) C ( , t ) (17)    m1 A1  m2 A2   ( , t )  1 ( ) e i t   0 (18) (29) C(, t )  C1    e it (19) 4.0 RESULTS AND DISCUSSION where U1   1   and C1   are to be The effects of concentration and Hall determined. current on unsteady flow of a viscoelastic fluid in a Substituting (17) to (19) into (11), (12) and (15), fixed plate has been formulated and solved Comparing harmonic and non harmonic terms, we analytically. In order to understand the flow of the obtain fluid, computations are performed for different parameters such as Gr, Gc, Sc, Pr,  , Kc, M, and U Gr GcC U    L3U   it  m. L1 4 L1e 4 L1eit 4.1 Velocity profiles (20) Figures 1 to 7connote the velocity profiles; 1 1  Pr 1  i1  0 figure 8 depicts the temperature profiles and figures9& 10display the concentration profiles with 4 varying parameters respectively. (21) The effect of velocity for different values of 1 (Pr = 0.71, 1, 3) is displayed in figure 1, the graph C1 ScC1  iC1  KcScC1  0 show that velocity decreases with increase in Pr. 4 (22) The effect of velocity for different values of (Sc = and boundary conditions give 0.18, 0.78, 2.01, 2.65) is given in figure 2, the graph   0 : U1 (0)   (0)  C (0)  1  show that velocity decreases with the increase in Sc. Figure 3 denotes the effect of velocity for different    1: U1 (1)  0, (1)  0, C (1)  0 values of (m = 2, 4, 6, 10), it is seen that velocity decreases with the increase in m. (23) The effect of velocity for different values of (M = 1, where the primes connotes differentiation with respect to  . 3, 6, 10) is shown in figure 4, it depict that velocity decreases with increase in M. 887 | P a g e
  • 4. E. Omokhuale, I. J. Uwanta, A. A. Momoh, A. Tahir. / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 2, Issue5, September- October 2012, pp.885-892 Figure 5 depicts the effect of velocity for (Gr = 1, 2, The effect of velocity for different values of (Kc = 1, 3, 5), the graph connote that velocity increases with 2, 3, 4) is displayed in figure 7, it is clear that the increase in Gr. velocity decreases with the increase in Kc. The effect of velocity for different values of (Gc = 2, 3, 4, 8) is presented in figure 6, it is seen that velocity increases with the increase in Gc. Figure 1. Velocity profiles for different values of Pr. Figure 2. Velocity profiles for different values of Sc. 888 | P a g e
  • 5. E. Omokhuale, I. J. Uwanta, A. A. Momoh, A. Tahir. / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 2, Issue5, September- October 2012, pp.885-892 Figure 3. Velocity profiles for different values of m. Figure 4. Velocity profiles for different values of M . Figure 5. Velocity profiles for different values of Gr. 889 | P a g e
  • 6. E. Omokhuale, I. J. Uwanta, A. A. Momoh, A. Tahir. / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 2, Issue5, September- October 2012, pp.885-892 Figure 6. Velocity profiles for different values of Gc. Figure 7. Velocity profiles for different values of Kc. 4.2 Temperature profiles In figure 8, the effect of temperature for different values of (Pr = 0.71, 1, 3, 7) is given. The graph show that temperature increases with increasing Pr. Figure 8. Temperature profiles for different values of Pr. 890 | P a g e
  • 7. E. Omokhuale, I. J. Uwanta, A. A. Momoh, A. Tahir. / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 2, Issue5, September- October 2012, pp.885-892 4.3 Concentration profiles concentration for (Kc= 0, 0.5, 1, 3) is given in figure Figure 9 depicts the effect of concentration for (Sc = 10, it is seen that concentration decreases with the 0.3, 0.78, 1, 2.01), it is seen that concentration decrease in Kc. increases with the increase in Sc. The effect of Figure 9. Concentration profiles for different values of Sc. Figure 10. Concentration profiles for different values of Kc. Table 1 to 3 represent the Skin friction, Nusselt Table 2: Nusselt number number and Sherwood number respectively.  Pr Nu Table 1 depicts that the Skin friction increases with 1 0.71 0.8181 increase in Gc and Grand decreases with increase in 4 0.71 0.7400 Sc, m, M, Kc, and Pr. 1 3 0.7830 Table 2 represents that the Nusselt number decreases with increase in Pr, and decreases with increase in  Table 3: Sherwood number Table 3 shows that the Sherwood number decreases  Sc Sh with increase in Sc and  . 1 0.3 0.4015 5 0.3 0.3890 Table 1: Skin friction  4 0.6 0.3977  Gc Sc Kc Gr M Pr M  1 1 0.3 0.1 1 1 0.71 0.5 6.1082 5.0 SUMMARY AND CONCLUSION 3 1 0.3 0.1 1 1 0.71 0.5 5.5219 We have examined and solved the 1 1 0.6 0.1 1 1 0.71 0.5 5.7548 governing equations for the effects of concentration 1 4 0.3 0.1 1 1 0.71 0.5 6.5671 and Hall current on unsteady flow of a viscoelastic 1 1 0.3 1 1 1 0.71 0.5 6.3654 fluid in a fixed plate analytically. In order to point 1 1 0.3 0.1 4 1 0.71 0.5 6.8760 out the effect of physical parameters namely; 1 1 0.3 0.1 1 3 3 0.5 5.9006 thermal Grashof number, mass Grashof number, 1 1 0.3 0.1 1 1 0.71 2 5.0126 Schmidt number, Prandtl number, Chemical reaction 1 1 0.3 0.1 1 1 0.71 0.5 6.8741 parameter, Hartmann number, Hall parameter and 891 | P a g e
  • 8. E. Omokhuale, I. J. Uwanta, A. A. Momoh, A. Tahir. / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 2, Issue5, September- October 2012, pp.885-892 the frequency of oscillation on the flow field and the 8. Salem, A. M. and El-Aziz, M. Abd. (2008). following conclusions are drawn: Effect of Hall currents and Chemical *The velocity increases with the increase in Gc and reaction and Hydromagnetic Gr. flow of a stretching vertical surface with *The velocity falls due to increasing in Sc,  , M, m, internal heat generation / absorption. Kc, and Pr. Applied Mathematical Modelling: 32, 1236 *The temperature decreases with increase in Pr, – 1254. *The concentration reduces with the increase in Sc 9. Saleh, M.A.,Mohammed ,A.A.B. and and Kc. Mahmoud S.E. (2010). Heat and mass *The Skin friction increases with increase in Gc and transfer in MHD viscoclastic fluid flow Gr and decreases with increase in Sc, M, m,Kc, and through a porous medium over a stretching Pr. sheet with chemical reaction. Journal of *The rate of heat transfer decreases with increase in Applied Mathematics, 1, 446-455. Pr and  , *The Sherwood number decreases with the increase 10. Shateyi, S., Motsa, S. S. and Sibanda, P. in Sc and  . (2010). The effects of thermal Radiation, Hall currents, Soret and REFERENCES Dufour on MHD flow by mixed convection 1. Aboeldahab, E. M. and Elbarby, E. M. E. over vertical surface in porous medium. (2001). Hall current effect on Mathematical Problem in Engineering, Magnetohydrodynamics free convection 2010, Article ID 627475. flow past a Semi – infinite vertical plate 11. Sharma, B. K., Jha, A. K. and Chaudary, R. with mass transfer. Int. Journ. of C. (2007). Hall Effect on MHD mixed Engineering Sciences. 39. 1641 – 1652. convective flow of a viscous 2. Acharya, M., Dash, G. C., Singh, L. P. incompressible fluid past a vertical porous (2001). Hall current effect with plate immersed in a porous medium with simultaneous thermal and mass diffusion Heat Source/Sink. Rom. Journ. Phys. 52 (5- on unsteady hydromagnetic flow near an 7), 487 - 503. accelerated vertical plate. Indian Journal of 12. Singh, P. K. and Singh, J. (2012). MHD Physics, 75B(1), 168. flow of Viscous Dissipation and Chemical 3. Anjali Devi, S. P. and Ganga, B., effects of Reaction over a Stretching viscous and Joules dissipation and MHD porous plate in a porous medium. flow, heat and mass International Journal of Engineering transfer past a Stretching porous surface Research and Applications.2(2). 1556 – embedded in a porous medium. Non – 1564. Linear Analysis: Modelling and Control. 13. Sonth, R, M., Khan, S. K., Abel, M. S. and 14(3). 303 - 314. Prasad, K. V. (2012). Heat and Mass 4. Das, K. and Jana, S. (2010). Heat and Mass transfer in a viscoelastic fluid transfer effects on unsteady MHD free over an accelerated surface with heat convection flow near a source/sink and viscous dissipation. Journal moving vertical plate in a porous medium. of Heat and Mass Transfer, 38, 213 – 220. Bull. Soc. Math. 17, 15 - 32. 14. Takhar (2006). Unsteady flow free 5. Das, K. (2010). Exact Solution of MHD convective flow over an infinite vertical free convection flow and Mass Transfer porous platedue to the combined near a moving vertical porous effects of thermal and mass diffusion, plate in the presence of thermal radiation. magnetic field and Hall current. Journal of AJMP.8(1). 29 – 41. Heat and Mass Transfer. 39, 823 – 834. 6. Kai- Long, H. (2010). Heat and mass transfer for a viscous flow with radiation effect past a non-linear stretching sheet. World Academy of Science, Engineering and Technology, 62(3), 326-330. 7. Motsa, S. S. and Shateyi, S. (2012). The effects of chemical reaction, Hall current and Ion – Slip currents on MHD micropolar fluid flow with thermal Diffusivity using Novel Numerical Technique.Journal of Applied Mathematics. 10. 115 – 1165. 892 | P a g e