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							                                                         International Journal of Advances in Science and Technology,
                                                                                                    Vol. 3, No.1, 2011

   Chemical Reaction and Heat source effects on MHD Free Convection
      Flow past a Vertical Plate under Oscillatory Suction Velocity
                         V.Bhagya Lakshmi1, S.V.K.Varma2 and N.Ch.S.Iyengar3
                 1
                   Department of Mathematics, Sri Venkateswara University, Tirupati, Andhra Pradesh, India
                                                  svulakshmi@gmail.com
                 2
                   Department of Mathematics, Sri Venkateswara University, Tirupati, Andhra Pradesh, India
                                            svijayakumarvarma@yahoo.co.in
                 3
                   School of Computing Science and Engineering, VIT University, Vellore, Tamilnadu, India
                                               nchsniyengar48@gmail.com

                                                        Abstract

The objective of this paper is to analyze effects of Chemical reaction and Heat source on MHD flow past a
vertical plate under oscillatory suction velocity. It is assumed the permeability of the porous medium fluctuates
with time. The governing equations of the flow field are solved by using perturbation technique. The expressions
for the velocity, temperature and concentration fields are obtained. Skin friction, the rate of heat and mass
transfer in terms of Nusslet number and Sherwood number are also derived. The effects of the flow parameters
such as Grashoff number for heat transfer and mass transfer (Gr,Gc), Heat source parameter (Q), Prandtl
number (Pr), Magnetic parameter (M), Schmidt number (Sc) and Chemical reaction parameter Kr on the
velocity, temperature, concentration, skin-friction, nusslet number and Sherwood number have been analyzed
through the graphs and Tables.

Keywords: Heat and Mass Transfer, Chemical Reaction, Oscillating suction velocity, Magnetic field.

1. Introduction
          A number of scholars have developed their extensive research on the study of heat and mass transfer due to
its day-to-day applications in science and technology. The phenomenon of heat and mass transfer are observed in
buoyancy induced motions in the atmosphere, in water bodies, quasi-solid bodies such as earth and so on. In many
transport processes in nature and in industrial applications in which heat and mass transfer are a consequence of
buoyancy effects caused by diffusing of heat and chemical species. The study of such processes is useful for
improving a number of chemical technologies, such as polymer production, chemical oil recovery, underground
energy transform, manufacturing of ceramic and food processing.
          Raptis and Kafoussias (1) have studied the influence of a magnetic field upon the steady free convection
flow through a porous medium bounded by an infinite vertical plate with constant suction velocity, and when the
plate temperature is also constant. Raptis (2) has studied mathematically the case of time-varying two- dimensional
natural convective heat transfer of an incompressible, electrically-conducting viscous fluid via a highly porous
medium bounded by an infinite vertical porous plate. Vajravelu and Hadyinicolaou (3) investigated the convective
heat transfer in an electrically conducting fluid at stretching surface with uniform stream velocity.
          The present trend in the field of chemical reaction analysis is to give a mathematical model for the system
to predict the reactor performance. Many researches are being carried out across the globe. The study of heat and
mass transfer with chemical reaction is given primary importance in chemical and hydrometallurgical industries.
A study of the first order chemical reaction on the flow past an impulsively started vertical plate with uniform heat
and mass flux by P. Ganesan and R. Muthucumaraswamy (4). The same type of problem with inclusion of constant
wall suction was studied by Makinde.O.D. And P. Sibanda (5), J.R. Fan et.al (6) studied the same problem over a
horizontal moving plate. R. Kandasamy and S.P. Anjalidevi (7) investigated the effect of chemical reaction of the
flow over a wedge. Atul Kumar Singh (8) analyzed the MHD free convection and mass transfer flow with heat
source and thermal diffusion. The paper deals with the study of free convection and mass transfer flow of an
incompressible, viscous and electrically conducting fluid past a continuously moving infinite vertical plate in the
presence of large suction and under the influence of uniform magnetic field considering heat source and thermal
diffusion. Processes involving the mass transfer effect have long been recognized as important principal in chemical
processing equipment. Recently, Mohammad Ferdows, et.al (9) have studied the effect of similarity solution for
MHD flow through vertical porous plate with suction.




Special Issue                                         Page 53 of 89                                          ISSN 2229 5216
                                                               International Journal of Advances in Science and Technology,
                                                                                                          Vol. 3, No.1, 2011

         In the above stated studies, the oscillatory suction in the presence of time dependent velocity along the
influence of uniform magnetic fields are not studied while such flows are encountered in geophysical problems,
astrophysical problems, soil sciences and so on. Therefore, the aim of the present investigation is to study the
chemical reaction and heat source effects on MHD convective flow past a vertical plate under oscillatory suction
velocity in the presence of a uniform transverse magnetic field. The permeability of the porous medium is
considered to be      K  t '   K0 1   ein 't '  and the suction velocity is assumed to be   t '   0 1   ein 't ' 
where   0  0   and     0    is a positive constant.


2. Mathematical Formulation

          Consider in an unsteady flow of an incompressible, electrically conducting and viscous fluid past an
infinite vertical porous plate under the oscillatory suction velocity in the presence of chemical reaction and heat
source. In Cartesian coordinate system, let „x‟-axis be along the plate in the direction of the flow and y-axis normal
to it. A uniform magnetic field is applied normal to direction of flow. In the analysis, we assume that the magnetic
Reynolds‟s number is much less than unity so that the induced magnetic field is neglected in comparison to the
applied magnetic field. Further, all the fluid properties are assumed constant except that of the influence of density
variation with temperature. Therefore, the basic flow in the medium is entirely due to buoyancy plate as well as fluid
is assumed to be at the same temperature and the concentration of species is very low so that Soret and Dufer effects
                                                                                                                      '
are neglected. When t>0, the temperature of the plate is instantaneously raised (or lowered) to Tw and the
                                                           '
concentration of species is raised (or lowered) to Cw .
          Following the analysis and dimensionless parameters of (10), the governing equations become
1 u                 u  2u
      1   eint 
                                               u
                        2  GrT  GmC                  M 2u
                                         K0 1   e 
                                                                                                                            (1)
4 t                 y y                          int


1 T           int T   1  2T
      1   e               Q T                                                                                      (2)
4 t               y pr y 2
 1 C                 C 1  2T
       1   eint             Kr  C                                                                                  (3)
 4 t                 y SC y 2
               K         Q
Where K r  1 , Q  12
                  2
                v0        v0
The corresponding boundary conditions in dimensionless form are
u  0 , T  1   eint , C  1   eint at y  0
u  0 ,T  0 , C  0                 as y                                                                                 (4)

3. Method of Solution

In order to solve the System of equations (1), (2) & (3) under the boundary conditions (4) we assume
u  y, t   u0  y    u1  y  eint
T  y, t   T0  y    T1  y  eint                                                                                     (5)
C  y, t   C0  y    C1  y  e   int


Substituting (5) in to the equations (1), (2) & (3) and equating the harmonic and non-harmonic terms, we get
u0  u0  a1u0  GrT0  GmC0
 ''   '
                                                                                                                            (6)




Special Issue                                              Page 54 of 89                                       ISSN 2229 5216
                                                                                International Journal of Advances in Science and Technology,
                                                                                                                           Vol. 3, No.1, 2011

                                                           u0
u1''  u1'  a2u1  GrT1  GmC1  u0 
                                    '
                                                                                                                                        (7)
                                                           K0
T0''  PT0'  PT0  0
        r      r                                                                                                                        (8)
T1''  PT1'  a3T1   PT0'
        r               r                                                                                                                (9)
C0  ScC0  SC C0  0
 ''     '
                                                                                                                                        (10)
C  ScC  a4C1  ScC
  ''
  1
              '
              1
                                         '
                                         0                                                                                              (11)
The corresponding boundary conditions are:
u0  u1  0, T0  T1  0, C0  C1  0 at y  0
u0  u1  0, T0  T1  1, C0  C1  1 as y                                                                                            (12)

Solving equations (6)-(11) with the help of boundary conditions (12)
u  y, t   9  a7  a8  e
                                     m10 y
                                               a7e m2 y  a8e m6 y ] 
 [a19e m y  a14e m y  a15e m y  a10e m10 y  a17e m y  a18e m y ]eint
             12                 4                8                                   2               6

                                                                                                                                        (13)

T  y, t   e
                   m2 y
                             [(1  a5 )e m4 y  a5e m2 y ]eint                                                                      (14)

C  y, t   e
                   m6 y
                             [(1  a6 )e m8 y  a6e m6 y ]eint                                                                      (15)
To obtain the fluctuating parts of the transient velocity, temperature and concentration are:
 u  y, t   u0  y     M r Cosnt  M i Sinnt                                                                                     (16)

T  y, t   T0  y     Kr Cosnt  Ki Sinnt                                                                                        (17)

C  y, t   C0  y     Lr Cosnt  Li Sinnt                                                                                        (18)
Where
M r   N15CosB3 y  N16 SinB3 y  e A3 y   N5CosB1 y  N6 SinB1 y  e A1 y 
       N7CosB2 y  N8 SinB2 y  e A2 y  N9em y  N11em y  N13em y   10                2           6



M i   N16CosB3 y  N15 SinB3 y  e A y   N6CosB1 y  N5 SinB1 y  e A y 
                                                          3                                                  1



         N8CosB2 y  N7 SinB2 y  e A2 y  N10em y  N12em y  N14em y     10               2               6



Kr   1  N1  CosB1 y  N2 SinB1 y  e A y  Ne m y      1                  2



Ki   1  N1  SinB1 y  N2CosB1 y  e A y  Ne m y       1                  2



Lr   1  N3  CosB2 y  N4 SinB2 y  e A y  N3e m y         1                  6



Li    1  N3  SinB2 y  N4CosB2 y  e A y  N4e m y            1                  6



The expressions for transient velocity, temperature and concentration fields for nt   / 2 are
         
u ( y,   )  u0  y    M i                                                                                                           (19)
      2n
      
T ( y, )  T0  y    Ki                                                                                                              (20)
      2n
         
C ( y,        )  C0  y    Li                                                                                                       (21)
         2n




Special Issue                                                             Page 55 of 89                                     ISSN 2229 5216
                                                          International Journal of Advances in Science and Technology,
                                                                                                     Vol. 3, No.1, 2011

4. Skin Friction, Nusselt Number and Sherwood Number

The Skin friction coefficient       at the plate, in terms of amplitude and phase is

           u 
        =  0   X Cos  nt                                                                                   (22)
          y  y 0
The Rate of heat transfer coefficient  Nu  at the plate in terms of amplitude and phase is

             T 
     Nu        = m2   Y Cos  nt                                                                             (23)
             y  y 0
The Rate of Mass transfer coefficient  Sh  at the plate in terms of amplitude and phase is

            C 
   Sh         = m6   Z Cos  nt                                                                              (24)
            y  y 0
Where  0  m2 a7  m6 a8  m10  a7  a8 
                           Xi                            Y                         Z
X  X r  X i , Tan          , Y  Yi  Yr , Tan  i , Z  Zi  Z r , Tan  i
                           Xr                            Yr                        Zr
X r   A3 N15  B3 N16  A1 N5  B1 N6  A2 N7  B2 N8  m10 N9  m2 N11  m6 N13
X i   A3 N16  B3 N15  A1 N6  B1 N5  A2 N8  B2 N7  m10 N10  m2 N12  m6 N14
Yr  A1 1  N1   B1 N2  m2 N1 , Yi  B1 1  N1   A1 N2  m2 N2
Zr  A2 1  N3   B2 N4  m6 N3 , Zi  B2 1  N3   A2 N4  m6 N4

5. Results and Discussion
      Numerical calculations have been carried out for transient velocity, transient temperature and species
concentration distributions for different values of parameters are displayed in figures (1)-(10). From figures (1)-(4)
we noticed that the maximum velocity attains near the plate in the neighborhood of the point y=2 for y>0 the
velocity decrease and tends to zero as y   .
      Figs (1) and (2) display the effect of heat source parameter Q on the velocity field for the cases of cooling and
heating of the plates respectively. From (1) it is observed that the transient velocity decreases with an increase in
heat source parameter Q. The reverse effect is observed from the fig (2) in the case of heating of the plate.
       Figs (3) & (4) represent the transient velocity profiles due to variations in chemical reaction parameter Kr in
case of cooling and heating of the plate respectively. It is noticed that an increases in Kr the velocity decreases. The
reverse phenomenon is observed from the fig (4) in the case of heating of the plate.
                                                                                                                  0
       Fig (5) shows temperature field due to variations in Prandtl number Pr for air, mercury, water at 4 c at
  0.002 and n=5.0. It is seen that an increase in Pr decreases the transient temperature field indicating that
temperature falls more rapidly for water in comparison to air.
       Fig (6) shows transient temperature due to variations in heat source parameter Q. It is observed that the
transient temperature decreases with increases in Q values
       Fig(7) display the concentration due to variations in Schmidt number Sc for the bases Hydrogen, Helium,
Water - Vapor, Oxygen and Ammonia at   0.002 ,n=5.0 It is observed that concentration field falls slowly and
steadily for hydrogen and helium but falls rapidly to oxygen and ammonia in comparison to water - vapor.
       From fig (8) it is observed that the transient concentration decreases with an increase in chemical reaction
parameter Kr.
       Figs(9) & (10) shows the in the absence of Chemical reaction and heat source for the cases of cooling and
heating , the results of the present paper are reduced to those obtained by Athul Kumar Singh, Ajay Kumar Singh
and N.P. Singh(13)




Special Issue                                          Page 56 of 89                                  ISSN 2229 5216
                                                            International Journal of Advances in Science and Technology,
                                                                                                       Vol. 3, No.1, 2011

       Table-I represents the numerical values of Skin friction coefficient  in terms of amplitude X , phase
Tan , Skin friction coefficient  m due to steady part of velocity and Skin friction coefficient  for variations in
Gr,Gm,Pr,Sc,M,Ko,n,Q and Kr respectively due to cooling of the plate. It is noticed that an increase in Gr or Gm or
Sc or Ko or Q as increase in the value of amplitude X          and decreases the amplitude X as increase in Pr or M or
n or Kr. The phase Tan decreases due to increase in Gr or Pr Sc or Q while increases due to increase in Gm or
M or Ko or n or Kr. It is also seen that  m ,  decreases due to increases in Pr or M while an increases in Gr or Gm
or Sc or Ko or N or Q or Kr.
      Table-II shows the numerical values of Skin friction coefficient  in terms of amplitude X , phase Tan
Skin friction coefficient    m     due to steady part of velocity and Skin friction coefficient         for variations in
Gr,Gm,Pr,Sc,M,Ko,n,Q and Kr respectively due to heating of the plate. It is observed that decrease in Gr or Gm
leads to an increases the value of amplitude X Also it is observed that an increase in Sc or Ko or Q leads to an
increase the value of X while an increase in Pr or M or n or Kr leads to decrease in the value of X . The value of
Tan decreases due to increases in Pr or Sc or n or Q while an increase due to increases in M or Ko or Kr. It is
also we noticed that decrease Tan with decrease in Gr and decreases in Gm in the increases the value of Tan .
It is noticed that  m ,  decrease due to increases in Pr or Sc or M or n and decreases in Gr or Gm values due to
decreases the values of  m ,  .
       Table-III shows the effects of parameters Pr, Q and n on amplitude Y , phase Tan and rate of heat

transfer in terms of Nusselt number N u at         0.002 , nt   / 2 . It is observed that the values the amplitude Y ,
Nusselt number N u increases due to increases in Pr while to decreases Y , N u leads to increase in Q or n. The
value ofTan decreases due to increase in Q or n while decreases due to an increase in Pr.
      Table-IV represents the effects of parameters Sc, Kr and n on amplitude Z , phase Tan and rate of mass
transfer in terms of Sher-wood number S h at     0.002 , nt   / 2 . It is noticed that the Sher-wood number S h
increases as increase in Sc or Kr or n. The phase Tan increases with increase in Sc or Kr or n. It is also observed
that the value amplitude Z increases as increase in Kr or n and it increases with increase in Sc values.


                 10

                                                                                         Gr=5.0
                   8                                                                     Gm=5.0
                                                   Kr=0.07
                                                                                         Pr=0.71
                                                                                         Sc=0.22
                                                            Kr=0.08                      M=0.5
                   6
                                                                                         Ko=0.1
                                                                        Kr=0.09          n=5.0
                                                                                         Q=0.4
           U




                   4                                                                     E =0.002


                   2



                   0



                  -2
                       0     2         4       6        8       10      12      14      16      18        20
                                                                Y
                Figure1: Velocity profiles variation with Chemical reaction parameter Kr (Gr, Gm>0)




Special Issue                                           Page 57 of 89                                     ISSN 2229 5216
                                                        International Journal of Advances in Science and Technology,
                                                                                                   Vol. 3, No.1, 2011


                0.1

                  0

                -0.1
                                                                                          Kr=0.07
                -0.2                                                                      Kr=0.08

                                                                                         Kr=0.09
                -0.3
         U


                                                                                      Gr=-5.0
                -0.4
                                                                                      Gm=-5.0
                                                                                      Pr=0.71
                -0.5                                                                  Sc=0.22
                                                                                      M=0.5
                -0.6                                                                  Ko=10.0
                                                                                      n=5.0
                -0.7                                                                  Q=0.4
                                                                                      E =0.002
                -0.8
                       0   2       4        6      8        10      12      14      16      18      20
                                                            Y
                Figure 2: Velocity profiles variation with Chemical reaction parameter Kr (Gr, Gm<0)


                 0.6
                                                                             Q=4
                                                                                Q=6
                 0.5                                                               Q=6.5
                                                                                            Q=7

                 0.4


                 0.3
          U




                                 Gr=5.0
                 0.2             Gm=5.0
                                 Pr=0.71
                                 Sc=0.22
                 0.1             M=0.5
                                 Ko=5.0
                                 E =0.005
                   0             Kr=5
                                 n=5.0

                -0.1
                       0   0.1     0.2     0.3    0.4       0.5     0.6     0.7     0.8     0.9      1
                                                             Y
                   Figure 3: Velocity profiles variation with Heat source parameter Q (Gr, Gm>0)
                0.1

                                       Gr= -5.0
                  0                    Gm= -5.0
                                       Pr=0.71
                                       Sc=0.22
                -0.1                   M=0.5
                                       Ko=5.0
                                       E =0.005
                -0.2                   Kr=5
                                       n=5.0
          U




                -0.3


                                                                                           Q=7
                -0.4
                                                                                         Q=6.5

                -0.5                                                                Q=6
                                                                                 Q=5.5
                -0.6
                       0   0.1    0.2     0.3     0.4       0.5    0.6     0.7     0.8      0.9     1
                                                            Y

                   Figure 4: Velocity profiles variation with Heat source parameter Q (Gr, Gm<0)




Special Issue                                      Page 58 of 89                                    ISSN 2229 5216
                                                            International Journal of Advances in Science and Technology,
                                                                                                       Vol. 3, No.1, 2011


                1.2
                                                        Q=10
                  1                                                       Q=1
                                                                                      Q=5

                0.8                                                                           Q=15

                0.6

                0.4
                                                                                            Q=20

                0.2
         T



                  0

                -0.2
                              Pr=0.78
                -0.4          E =0.005
                              n=5.0
                -0.6

                -0.8
                       0      0.1    0.2     0.3      0.4       0.5    0.6      0.7     0.8      0.9    1
                                                                Y
                           Figure 5: Temperature profiles variation with Heat source parameter Q


                1.4


                1.2                                 Pr=0.25
                                                                                       Pr=0.71

                  1


                0.8
          T




                                                    Pr11.0
                0.6
                                                                Pr=7.00


                0.4
                                                                                       Q=1.0
                                                                                       E =0.005
                0.2                                                                    n=5.0


                  0
                   0                 0.2              0.4              0.6              0.8             1
                                                                Y


                              Figure 6: Temperature profiles variation with Prandtl number Pr


                1.2

                  1

                0.8

                0.6
                                Kr=0.2

                0.4
          C




                                            Kr=10.0
                0.2

                  0
                                                      Kr=5.0
                             Sc=0.6
                -0.2         n =5.0
                                                                Kr=2.0
                             E=0.005
                -0.4

                -0.6
                       0      0.1     0.2     0.3     0.4       0.5    0.6      0.7     0.8      0.9    1
                                                                Y
                   Figure 7: Concentration profiles variation with Chemical reaction parameter Kr




Special Issue                                          Page 59 of 89                                    ISSN 2229 5216
                                                        International Journal of Advances in Science and Technology,
                                                                                                   Vol. 3, No.1, 2011


                1.2


                  1                                Sc=0.66                   Sc=0.30


                0.8                                                Sc=0.60                     Sc=0.22


                                                                                               Sc=0.78
                0.6
         C



                0.4
                            Kr=1.0
                            E=0.005
                0.2         n =5.0



                  0


                -0.2
                       0           0.5              1                  1.5                 2                2.5
                                                             Y
                           Figure 8: Concentration profiles variation with Schmidt number Sc
                0.7
                                                     curve   Gr Gm M             n Ko   Pr        Sc
                0.6                                    I     2   2 2             5 5   0.7      0.22
                                                       II     5  5  2             5 5  0.7      0.22
                                                       III    2   2 2             5 5   7.0      0.22
                0.5                                    IV     2  2 2              5 5  0.7      0.66
                                                        V    2   2 2             5  5   0.7      0.22
                                                       VI     2  2 2             10 10 0.7       0.22
                0.4

                                                          VI
                0.3
          U




                                                                   I
                                                                       III
                0.2
                                                                             V
                                                                                 IV
                0.1                                                                            II


                  0


                -0.1
                       0                       5                              10                            15
                                                             Y

            Figure 9: Velocity profiles variation with different parameters when Kr=0, Q=0(Gr, Gm>0)

                0.1


                  0

                                                                                      VI
                -0.1                                                    V
                                                             III
                -0.2
                                                          IV
                                                    I
                -0.3
           U




                                                                   II

                -0.4                                curve Gr Gm M n               Ko   Pr           Sc
                                                      I   -2  -2 2               5 5    0.7         0.22
                                                      II   -5 -5  2               5 5   0.7         0.22
                -0.5                                  III  -2  -2 2               5 5    7.0         0.22
                                                      IV   -2 -2 2                5 5   0.7         0.66
                -0.6                                   V  -2  -2 2               5   5   0.7         0.22
                                                      VI   -2 -2 2               10 10 0.7           0.22

                -0.7
                       0                       5                              10                            15
                                                             Y

           Figure 10: Velocity profiles variation with different parameters when Kr=0, Q=0(Gr, Gm<0)




Special Issue                                       Page 60 of 89                                           ISSN 2229 5216
                                                          International Journal of Advances in Science and Technology,
                                                                                                     Vol. 3, No.1, 2011

                                                        TABLE-I
        Values of Amplitude X , phase Tan and Skin-friction coefficients              due to cooling of the plate

                    Pr      Sc                                                 X       Tan
                                                                                                              2.5396
  2.0       2.0     7.0    0.66     0.5     5.0     5.0       1.0    0.08    2.2049    0.0814     2.5400

  2.0       5.0     7.0    0.66     0.5     5.0     5.0       1.0    0.08    2.6220    -0.6362    3.0295      3.0323

  5.0       2.0     7.0    0.66     0.5     5.0     5.0       1.0    0.08    5.8446    0.3712     5.8603      5.8563

  2.0       2.0    11.4    0.66     0.5     5.0     5.0       1.0    0.08    2.1861    -0.0060    2.4017      2.4018

  2.0       2.0     7.0    0.78     0.5     5.0     5.0       1.0    0.08    2.3740    0.0144     2.2754      2.2753

  2.0       2.0     7.0    0.66     1.0     5.0     5.0       1.0    0.08    1.4322    0.1695     1.8815      1.8810

  2.0       2.0     7.0    0.66     0.5    10.0     5.0       1.0    0.08    2.3745    0.1506     2.7066      2.7059

  2.0       2.0     7.0    0.66     0.5     5.0    10.0       1.0    0.08    1.6578    -0.1375    2.5400      2.5404

  2.0       2.0     7.0    0.66     0.5     5.0     5.0       1.5    0.08    2.2619    0.0197     2.6012      2.6011

  2.0       2.0     7.0    0.66     0.5     5.0     5.0       5.0    0.09    2.1978    0.0925     2.5757      2.5753

                                                      TABLE-II
         Values of Amplitude X , phase Tan and Skin-friction coefficients  m ,  due to heating of the plate

  Gr        Gm       Pr     Sc      M      Kop      n         Q       Kr       X       Tan         m          

  -2.0      -2.0    7.0    0.66     0.5     5.0     5.0       1.0    0.08    2.2047    0.0814     -2.5400    -2.5396

  -2.0      -5.0    7.0    0.66     0.5     5.0     5.0       1.0    0.08    2.6220    -0.6362    -3.0295    -3.3267

  -5.0      -2.0    7.0    0.66     0.5     5.0     5.0       1.0    0.08    5.8446    0.3712     -5.8603    -5.8644

  -2.0      -2.0    11.4   0.66     0.5     5.0     5.0       1.0    0.08    2.1861    -0.0060    -2.4017    -2.4017

  -2.0      -2.0    7.0    0.78     0.5     5.0     5.0       1.0    0.08    2.3740    0.0144     -2.2754    -2.2755

  -2.0      -2.0    7.0    0.66     1.0     5.0     5.0       1.0    0.08    1.4322    0.1695     -1.8815    -1.8819

  -2.0      -2.0    7.0    0.66     0.5    10.0     5.0       1.0    0.08    2.3745    0.1506     -2.7066    -2.7073

  -2.0      -2.0    7.0    0.66     0.5     5.0    10.0       1.0    0.08    1.6578    -0.1375    -2.5400    -2.5395

  -2.0      -2.0    7.0    0.66     0.5     5.0     5.0       1.5    0.08    2.2619    0.0197     -2.6012    -2.6013

  -2.0      -2.0    7.0    0.66     0.5     5.0     5.0       5.0    0.09    2.1978    0.0925     -2.5757    -2.5761




Special Issue                                       Page 61 of 89                                     ISSN 2229 5216
                                                          International Journal of Advances in Science and Technology,
                                                                                                     Vol. 3, No.1, 2011

                                                         TABLE-III
                                Amplitude of Y , phase Tan and rate heat transfer N u
       S.No             pr            n             Q                   Y            Tan                  Nu
        1              07.0           5.0          1.0            23.8247            -0.9794             5.8246
        2              11.4           5.0          1.0           145.6866            -3.5348             10.5728
        3              07.0           5.0          1.5            18.7427            -0.6948             4.8443

        4              07.0          10.0          1.0            21.4710             0.6608             5.8150


                                                         TABLE-IV
                               Amplitude of Z , Phase Tan and rate of mass transfer S h
       S.No              Sc                 n            Kr                   Z          Tan                Sh
        1               0.22              5.0            0.04               0.5398       0.8174            0.1403

        2               0.66              5.0            0.04               1.1000       0.6728            0.5933

        3               0.22              5.0            0.04               0.5371       0.8342            0.1157

        4               0.22           10.0              0.05               0.7485       0.8946            0.1388


6. References

[1]         A. A. Raptis and N. Kafousias, “Heat transfer in flow through a porous medium bounded by an infinite
            vertical plate under action of a magnetic field”, Int. J. Energy res. Vol.6, pp.241-245, 1982.
[2]         A. A. Raptis “Flow through a porous medium in the presence of Magnetic field”, Int J.Energy. Res vol.10,
            pp.97-101,1986.
[3]         Vajravelu, K.K. and Hadyinicolaou. A. „Convective heat transfer in an electrical conducting fluid
            at stretching surface with uniform stream velocity. Int. J. Engg. Sci., Vol.35, Pp.1273-1284, 1997.
[4]         P.Ganesan and R. muthucumaraswamy. “First order Chemical Reaction on flow past an
            impulsively started vertical plate with uniform heat and mass flux”. Acta Mechanica 147, pp 45-
            57, 2001.
[5]         Mankinde.O.D. and P.sibanda, “MHD mixed-convective flow heat and mass transfer past a vertical
            plate in a porous medium with constant wall suction‟. Journal of Heat Transfer, 130, 112602/1-
            8, 2008.
[6]         J.R. Fan, J.M. Shi and X.A. Xu, “Similarity solution of mixed convection with diffusion and
            chemical reaction over a horizontal moving plate”. Acta Machanica 126,Pp 59-69,1998.
[7]         R. Kandasamy and S.P. Anjali devi, “Effects of chemical reaction, heat and mass transfer on non-
            linear laminar boundary later flow over a wedge with suction or injection. J. of Comp and Appl.
            Mechanics, 5 pp 21-31, 2004.
[8]         Atul Kumar Singh, “Free convection and mass transfer flow with heat source and thermal
            diffusion”. Journal of Energy Heat and Mass Transfer, 23 Pp 167-178, 2001.
[9]         Mohammad Ferdows, Masatiro Ota, Abdus Sattar and Mohamud Alan, “Similarity solution for
            MHD flow through vertical porous plate with suction”. Journal of Applied Mechanics, 6(1), Pp 15-25,
            2005.
[10]        Athul Kumar Singh, Ajay Kumar Singh and N.P. Singh. “Heat and mass transfer in MHD flow of
            a viscous fluid past a vertical plate under oscillatory suction velocity”. Indian J. Pure appl, Math, 34(3),
            429-442, March 2003.




Special Issue                                           Page 62 of 89                                  ISSN 2229 5216
                                      International Journal of Advances in Science and Technology,
                                                                                 Vol. 3, No.1, 2011



Authors Profile


                  V.Bhagya Lakshmi, (M.Sc., M.phil), is a research scholar, Department of
                  Mathematics, S. V. University, Tirupati, A.P. India.




                  Dr. S. Vijaya Kumar Varma(M.Sc. Ph.D) is currently working as professor in
                  Department of Mathematics in S.V. University, Tirupati, he has 24 years of
                  experience with various levels and 30 years of research experience. Fluid
                  dynamics, Heat and mass transfer in fluid flows and magneto hydro dynamics are
                  the areas of research of his interest. He published 60 papers in national and
                  international journals. Under his guidance 8students awarded PhDs and 20
                  students awarded M.Phil. He has attended several national and international
                  conferences and workshops.


                  Dr.N.Ch.S.N. Iyengar (M.Sc, M.E, Ph.D) is a Senior Professor at the School of
                  Computing Science and Engineering at VIT University, Vellore, Tamil Nadu,
                  India. His research interests include Agent based Distributed Computing, Data
                  Mining, Privacy, hiding, Security, Cryptography, Intelligent computational
                  methods and Bio informatics. He has authored several textbooks and had nearly
                  110 research Publications in International Journals. He chaired many international
                  conferences and d delivered invited/ technical lectures/ keynote addresses besides
                  being International programmer committee member.




Special Issue                      Page 63 of 89                                   ISSN 2229 5216

						
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