THERMAL RADIATION AND MASS TRANSFER EFFECTS ON FREE CONVECTION FLOW PAST A SEMI-INFINITE VERTICAL...
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Transcript of THERMAL RADIATION AND MASS TRANSFER EFFECTS ON FREE CONVECTION FLOW PAST A SEMI-INFINITE VERTICAL...
IJMA
THERMAL RADIATION AND MASS TRANSFEREFFECTS ON FREE CONVECTION FLOW PAST A
SEMI-INFINITE VERTICAL MOVING POROUSPLATE WITH CHEMICAL REACTION
T. Sankar Reddy1, S. Mohammed Ibrahim2 and N. Bhaskar Reddy3
ABSTRACT: The combined free convection boundary layer flow with
radiation and mass transfer past a semi-infinite vertical moving porous plate
in the presence of chemical reaction is studied when the plate moves in its
own plane. The Rosseland approximation is used to describe radiative heat
transfer in the limit of optically thick fluids. The dimensionless governing
equations for this investigation are solved analytically using two-term
harmonic and non-harmonic functions. Numerical evaluation of the analytical
results is performed and some graphical results for the results for the velocity,
temperature and concentration profiles within the boundary layer and
tabulated results for the skin-friction coefficient, Nusselt number and the
Sherwood number are presented and discussed.
Keywords: Free convection; Radiation; Heat and Mass transfer; Chemical
reaction.
1. INTRODUCTION
The study of convection with heat and mass is very useful in fields such aschemistry, agriculture and oceanography. A few representative fields of interest
in which combined heat and mass transfer play an important role are the design
of chemical processing equipment, formation and dispersion of fog, distribution
of temperature and moisture over agriculture fields and groves of fruit trees,
damage of crops due to freezing, and pollution of the environment. This technique
is used in the cooling processes of plastic sheets, polymer fibres, glass materials,
and in drying processes of paper. Gebhart and Pera [1] studied the nature of
vertical natural convection flows resulting from the combined buoyancy effects
of thermal and mass diffusion. Radiative flows are encountered in countless
industrial and environment processes e.g. heating and cooling chambers fossil
fuel and combustion energy processes, evaporation from large open water
reservoirs, astrophysical flows, and solar power technology and space vehiclere-entry. Abdus Sattar and Hamid Kalim [2] investigated the unsteady free
convection interaction with thermal radiation in a boundary layer flow past a
vertical plate. Makinde [3] examined the transient free convection interaction
with thermal radiation of an absorbing -emitting fluid along moving vertical
permeable plate. Muthucumaraswamy and Senthil Kumar [4] presented heat and
mass transfer effects on moving vertical plate in the presence of thermal radiation.
Cogley et al. [5] showed that in the optically thin limit, the fluid does not absorb
its own emitted radiation, but the fluid does absorb radiation emitted by the
boundaries. Recently, Ibrahim et al. [6] have studied nonclassical thermal effects
in strokes second problem for micropolar fluids. Ghaly and Elbarbary [7] reported
the effect of radiation on free convection flow on MHD along a stretching surface
with uniform free stream. Sattar and Hamid [8] investigated the unsteady free
convection interaction with thermal radiation in a boundary layer flow past avertical porous plate.
Combined hat and mass transfer with chemical reaction are of importance in
many processes and have, therefore, received a considerable amount of attention
in recent years. In processes such as drying, evaporation at the surface of a water
body, energy transfer in a wet cooling tower and the flow in a desert cooler, heat
and mass transfer occur simultaneously. We are particularly interested in cases inwhich diffusion and chemical reaction occur at the roughly the same speed. When
diffusion is much faster than chemical reaction, then only chemical factors
influence the chemical reaction rat; when diffusion is not much faster than reaction,
the diffusion and kinematics and kinetics interact to produce very different effects.
Chambre and Young [9] have presented a first order chemical reaction in the
neighbourhood of a horizontal plate. Deka et al. [10] analyzed the effect of the
first order homogeneous chemical reaction on the process of an unsteady flow
past an infinite vertical plate with a constant heat and mass transfer.
Muthucumaraswamy and Ganesan [11] studied effect of the chemical reaction
and injection on the flow characteristics in an unsteady upward motion of an
isothermal plate.
The objective of this paper is to consider unsteady simultaneous convective
heat and mass transfer flow along a vertical moving porous plate in the presence
of thermal radiation and chemical reaction. It is assumed that the plate moves
with constant velocity in the flow direction. In addition, it is assumed temperature
and concentration at the wall as well as the suction velocity are exponentially
varying with time.
2. MATHEMATICAL ANALYSIS
An unsteady two-dimensional laminar free convection with mass transfer flow
of a viscous incompressible fluid past a semi-infinite vertical moving porous
plate in the presence of thermal radiation and chemical reaction is considered.
Let x* -axis be taken along the plate in the vertically upward direction and
y* -axis be taken normal to it. Since the semi-infinite plate in length, the flow
variables are functions of y* and t* only. Hence, under the usual Boussinesq’s
approximation, the equations of mass, linear momentum, micro-rotation, energyand diffusion can be written as follows:
continuity:*
*
v
y = 0 (1)
linear momentum:* *
** *
u uv
t y =
2 ** *
*2 ( ) ( )f c
ug T T g C C
y(2)
energy: ** *
T Tv
t y =
2 *
2 **
1 r
p p
k T q
c c yy(3)
diffusion:* *
** *
C Cv
t y =
2 ** *
*2 ( ),r
uD K C C
y(4)
where x*, y* and t* are the dimensional distances along and perpendicular to the
plate and dimensional time, respectively, u* and v* are the components of
dimensional velocities along x* and y* directions, respectively, C* and T are the
dimensional concentration and temperature, respectively, is the fluid density,
is the kinematic viscosity, cp is the specific heat at constant pressure, is fluid
electrical conductivity, g is the acceleration due to gravity, f is the volumetric-expansion coefficient due to temperature, c is the volumetric-expansion
coefficient due to concentration, D* is the chemical molecular diffusivity, Kr is
the chemical reaction parameter, and k is the fluid thermal conductivity. The
magnetic and viscous dissipations are neglected in this study. The magnetic and
viscous dissipations are neglected in this study. The second and third terms on
the right hand side of the momentum equation (2) denote the thermal and
concentration buoyancy effects, respectively. Also, the second on the right hand
side of the energy equation (3) represents thermal radiation. It is assumed that
the porous plate moves with a variable velocity in the direction of fluid flow. In
addition, it is also assumed that the temperature and the concentration at the
wall as well as the suction velocity are exponentially varying with time. The
radiative heat flux term is simplified by making use of the Rosseland
approximation as [12]
gr =4
*
4
3s
e
T
k y(5)
where s is the Stefan-Boltzman constant and ke is the mean absorption coefficient,
respectively. It should be noted that by Rosseland approximation we limit our
analysis to optically thick fluids. If the temperature differences with in the flow
are sufficiently small then Equation (5) can be linearized by expanding T4 into
the Taylor series about T and neglecting higher terms takes the form
T4 3 44 3T T T (6)
It is assumed that the permeable plate moves with constant velocity in the
direction of fluid flow. We also assume that the plate temperature and concentrationand suction velocity vary exponentially with time. Under these assumptions, the
appropriate boundary conditions for the velocity, microrotation, temperature and
concentration fields are
u* =* ** , ( ) ,n t
p w wu T T T T e
C* =* ** * *( ) n t
w wC C C e , at y* = 0,
u* T T , C* C* as y*
where u*p, C*
w and Tw are the wall dimensional velocity, concentration and
temperature, respectively. C* and T are the free stream dimensional concentration
and temperature, respectively, n* is constant.
It is clear from Equation (1) that the suction velocity normal to the plate iseither a constant or a function of time. Assuming that takes the following
exponential form:
v* =* *
0(1 )n tV Ae (8)
where A is a real positive constant, and A are small less than unity, and V0 is a
scale of suction velocity which has a non-zero positive constant. The negative
sign indicates that the suction is towards the plate.
In order to write the governing equations and the boundary conditions
dimensionless form, the following non-dimensional quantities are introduced.
u =*
0
,u
U
** * *0
20 0 0
, , , ,pp
uv V y nv y U n
V U V
t =* 2 * *
0* * 3, , ,
4e
w w s
t V T T C C kkC R
T T C C T
Sc = * 20
Pr p prr
C CKK
D V k k(9)
Gr = 20 0
( )f wg T T
U V,
* *
20 0
( )c wg C CGc
U V.
In view of Eqs. (5), (6), (8) and (9) the governing Eqs. (2)-(4) reduce to the
following dimensional form:
1 ntu uAe
t y =
2
2 r c
uG G C
y(10)
1 n tAet y
=2
2
1,
y(11)
1 n tC CAe
t y =
2
2
1r
CK C
Sc y
where =4
1 Pr3 4R
and Gc, Gr, Pr, R, Kr and Sc are denote the solutal Grashof number, thermal
Grashof number, Prandtl number, radiation parameter, chemical reaction parameter
and the Schmidt number, respectively.
The boundary conditions (7) are than given by the following dimensionless
equations:
u = 1 , 1nt nte C e , at y = 0
u 0 0, C 0 at y (13)
3. SOLUTION OF THE PROBLEM
In order to reduce the above system of partial differential equations to a system
of ordinary differential equations in dimensionless form, we may represent the
translational velocity, microrotation, temperature and concentration in the
neighbourhood of the plate as
u = 20 1( ) ( ) ( ) ...ntu y e u y O
= 20 1( ) ( ) ( ) ...nty e y O (14)
C = 20 1( ) ( ) ( ) ...ntC y e C y O
Substituting Eq. (14) into Eqs. (10)-(12), and equating the harmonic and
non-harmonic terms, and neglecting the higher-order terms of O( 2), we obtain
the following pairs of equations for (u0, 0, C0) and (u1, 1, C1).
" '0 0u u = 0 0r cG G C (15)
" '1 1 1u u nu = '
0 1 1r cAu G G C (16)
'' '0 0 = 0 (17)
'' '1 1 1n = '
0A (18)
'' '0 0 0rC ScC ScK C = 0, (19)
'' '1 1 1rC ScC Sc n K = '
0AScC (20)
where the primes denote differentiation with respect to y only. The corresponding
boundary conditions can be written as
u0 = Up, u1 = 0, 0 = 1, 1 = 1, C0 = 1, C1 = 1, at y = 0
u0 = 0, u1 = 0, 0 0, 1 0, C0 0, C1 0, as y (21)
Without going into detail, the solutions of Eqs (15)-(20) and subjected to
Eq. (21) can be shown to be
u(y, t) = 21 2 3
m yy ya e a e a e
31 2 41 2 3 4 5 6( )m ym y m y m ynt y ye b e b e b e b e b e b e (22)
(y, t) = 1m yy nt y yAe e e e e
n(23)
C(y, t) = 3 32 22m y m ym y m yn t Ame e e e e
n(24)
where m1 =4
1 12
n,
m2 =4
1 12
rSc K
Sc,
m3 =4
1 12
rn KSc
Sc, m4 =
11 1 4
2n
and a1 = 2 3( )pU a a , a2 = 22 2
Gr
m m
a3 = 2
Gc,
b1 = 21 1
1A
Grn
m m n, b2 =
22 2
22 2
GcmA a m
nm m n
b3 =
2
23 3
1Am
Gcn
m m n, b4 = 1 2 3 5 6( )b b b b b
b5 =3
24 4
GrA a
nm m n
, b6 = 1Aa
n
The skin-friction, the Nusselt number and the Sherwood number are important
physical quantities for this type of boundary-layer flow. These parameters can be
defined and determined as follows:
Cf =*
*
0 0 0
w
y
u
U V y
= 1 2 2 3 1 1 2 2 3 3 4 4 5 6n ta a m a e b m b m b m b m b b
Nu =*
*
0 1 1
0
Re 1y n tx
w y
T y A A mx Nu e
T T y n n
Sh =*
*
0 1 2 2 32 2
0
Re 1y n tx
w y
C y C Am Am mx Sh m e m
C C y n n
Where Rex = V0x/v is the local Reynolds number.
4. RESULTS AND DISCUSSION
Numerical evaluation of the analytical results reported in the previous section
was performed and a representative set of results is reported graphically in
Figure. 1-5. These results are obtained to illustrate the influence of the Grashof
number and solutal Grashof number, Radiation parameter, Schmidt number and
chemical reaction parameter on the velocity, temperature and concentration
profiles, while the values of physical parameters are fixed at A = 0.5, = 0.01,
n = 0.1, Pr = 0.7 and t = 1.0.
Figure 1 displays the effect of the plate moving velocity Up in the direction of
the fluid flow on the velocity profiles across the boundary layer. It is observed
that the values of the velocity on the porous plate increase, as Up increases.
Figure 1: Velocity Profiles Against Coordinate y for Different Up
In Figure 2, the velocity profiles are shown for different values of the Grashof
number and solutal Grashof number, we conclude that there is rise in the velocity,
when Gr or Gc increases. Physically, this is possible because as the Grashof
number increases, the contribution from the buoyancy near the plate becomes
significant, and hence a short rise in the velocity near the plate is observed. Here
the positive values of Gr correspond to a cooling of the surface by natural
convection.
Figure 2: Velocity Profiles Against Coordinate y for Different Gr and Gc
For different values of the radiation parameter R, the velocity and temperatureare plotted in Figure 3. It is obvious that an increase in R results in a decreasing
velocity and temperature within the boundary layer.
Figure 4. Shows the velocity profiles for different values of the Schmidt
number Sc and chemical reaction parameter Kr. It is clear that the velocity
decreases with increasing values of Sc and Kr.
The concentration profiles for different values of the Schmidt number Sc and
chemical reaction parameter Kr are shown Figure 5. It is observed that the
concentration decreases with increasing Sc and Kr.
Figure 4: Velocity Profiles Against Coordinate y for Different Sc and Kr
Figure 5: Concentration Profiles Against Coordinate y for Different Sc and Kr
5. CONCLUSIONS
The dimensionless governing equations are solved by the perturbation technique.The effect of different parameters like plate moving velocity, Grashof number,solutal Grashof number, Radiation parameter, Schmidt number and chemicalreaction parameter
It was found the velocity profiles increased due to increases in plate movingvelocity. Conclusions of the study are as follows.
(1) The velocity as well as concentration decreases with increasingparameters Sc and Kr.
(2) The velocity as well as temperature decreases with increasing parameter R.
(3) The velocity increases with increasing parameters Gr or Gc.
Nomenclature
A suction velocity parameter
C dimensionless concentration
Cf skin friction coefficient.
Cp specific heat at constant pressure .
D mass diffusion coefficient.
g acceleration due to gravity.
Gr Grashof number.
Gc solutal Grashof number
k thermal conductivity
Kr chemical reaction parameter
n scalar constant
Nu Nusselt number.
p pressure.
Pr Prandtl number.
R Radiation parameter
Rex local Reynolds number
Sc Schmidt number
Sh Sherwood number
T temperature.
t time
u,v components of velocities along and perpendicular to the plate.
U0 scale of free stream velocity.
V0 scale of suction velocity.
x,y distances of along and perpendicular to the plate.
Greek Symbols
fluid thermal diffusivity
c coefficient of volumetric concentration expansion of the working fluid
f coefficient of volumetric thermal expansion of the working fluid
scalar constant (<<1)
dimensionless temperature
fluid dynamic viscosity
fluid density
electrical conductivity.
fluid kinematic viscosity
friction coefficient
angular velocity vector
Subscripts
w Wall condition
Free steam condition
Superscripts
() differentiation with respect to y.
* dimensional properties
REFERENCES
[1] Gebhart B and Pera L (1971), “The Nature of Vertical Natural Convection Flows
Resulting from the Combined Buoyancy Effects of Thermal and Mass Diffusion”,Int. J. Heat Mass Transfer, 14, pp. 2025-2050.
[2] Abdus Sattar M.D. and Hamid Kalim M.D. (1996), “Unsteady Free-ConvectionInteraction with Thermal Radiation in a Boundary Layer Flow Past a Vertical PorousPlate”, J. Math. Phys. Sci., 30(1), pp. 25-37.
[3] Makinde O.D. (2005), “Free Convection Flow with Thermal Radiation and MassTransfer Past a Moving Vertical Plate”, 32, pp. 1411-1419.
[4] Muthucumaraswamy R and Senthil Kumar G (2004), “Heat and Mass Transfer Effectson Moving Vertical Plate in the Presence of Thermal Radiation”, Theoretical Applied
Mechanics, 31(1), pp. 35-46.
[5] Cogley A.C., Vincenty W.E., Gilles S.E., (1968) “Differential Approximation forRadiation in a Non-Gray Gas near Equilibrium”, AIAA J, 6 pp. 551-563.
[6] Ibrihem F.S, Hassanien I.A, Bakr AA. (2005), “Nonclssical Thermal Effects in StokesSecond Problem for Micropolar Fluids”. ASME J. Appl.Mech. 72, pp. 468-474.
[7] Ghaly A. Y., and. Elbarbary E. M. E., (2002) “Radiation Effect on MHD FreeConvective Flow of a Gas Stretching Surface with a Uniform Free Steam”, Journal
of Applied Mathematics, 2(2), pp. 93-103.
[8] Abdus Sattar M.D. and Hamid K.M.D.(1996), “Unsteady Free-Convection Interactionwith Thermal Radiation in a Boundary Layer Flow Past a Vertical Porous Plate”,J. Math. Phys. Sci., 30, pp. 25-37.
[9] Chambre P.L and Young J.D (1958), “On the Diffusion of a Chemically ReactiveSpecies in a Laminar Boundary Layer Flow”, Phys. Fluids Flow, 1, pp. 48-54.
[10] Dekha R., Das U.N and Soundalgekar V.M (1994), “Effects on Mass Transfer onFlow Past an Impulsively Started Infinite Vertical Plate with Constant Heat Flux and
Chemical Reaction”, Forschungim Ingenieurwesen, 60, pp. 284-209.
[11] Muthucumaraswamy R and Ganesan (2001), “Effect of the Chemical Reaction and
Injection on the Flow Characteristics in an Unsteady Upward Motion of an IsothermalPlate”, J Appl. Mech. Tech. Phys., 42, pp. 665-671.
[12] Brewster M.Q. (1992), “Thermal Radiative Transfer and Properties”, John Wileyand Sons, New York.
T. Sankar Reddy
Department of Mathematics, Annamacharya Instituteof Technology and Sciences, C.K. Dinne (Village & mandal),Kadapa, YSR- 516003.
E-mail: [email protected]
S. Mohammed Ibrahimb
Department of Mathematics, Priyadarshini Collegeof Engineering & Technology, NELLORE- 524004
N. Bhaskar Reddy
Dept. of Mathematics, Sri Venkateswara University,TIRUPATI-517502.