Sohail Nadeem1, Changhoon Lee. 1. Department of Mathematics, Quaid-i-Azam University, 45320, Islamabad 44000, Pakistan. snqau@hotmail.com.
Abstract
The steady boundary layer flow of nanofluid over an exponential stretching surface is investigated analytically. The transport equations include the effects of Brownian motion parameter and thermophoresis parameter. The highly nonlinear coupled partial differential equations are simplified with the help of suitable similarity transformations. The reduced equations are then solved analytically with the help of homotopy analysis method (HAM). The convergence of HAM solutions are obtained by plotting h-curve. The expressions for velocity, temperature and nanoparticle volume fraction are computed for some values of the parameters namely, suction injection parameter α, Lewis number Le, the Brownian motion parameter Nb and thermophoresis parameter Nt.
The steady boundary layer flow of nanofluid over an exponential stretching surface is investigated analytically. The transport equations include the effects of Brownian motion parameter and thermophoresis parameter. The highly nonlinear coupled partial differential equations are simplified with the help of suitable similarity transformations. The reduced equations are then solved analytically with the help of homotopy analysis method (HAM). The convergence of HAM solutions are obtained by plotting h-curve. The expressions for velocity, temperature and nanoparticle volume fraction are computed for some values of the parameters namely, suction injection parameter α, Lewis number Le, the Brownian motion parameter Nb and thermophoresis parameter Nt.
During the last many years, the study of boundary layer flow and heat transfer over a
stretching surface has achieved a lot of success because of its large number of
applications in industry and technology. Few of these applications are materials
manufactured by polymer extrusion, drawing of copper wires, continuous stretching of
plastic films, artificial fibers, hot rolling, wire drawing, glass fiber, metal
extrusion and metal spinning etc. After the pioneering work by Sakiadis [1], a large amount of literature is available on boundary
layer flow of Newtonian and non-Newtonian fluids over linear and nonlinear stretching
surfaces [2-10]. However, only a limited attention has been paid to the study of
exponential stretching surface. Mention may be made to the works of Magyari and Keller
[11], Sanjayanand and Khan [12], Khan and Sanjayanand [13], Bidin and Nazar [14]
and Nadeem et al. [15,16].More recently, the study of convective heat transfer in nanofluids has achieved great
success in various industrial processes. A large number of experimental and theoretical
studies have been carried out by numerous researchers on thermal conductivity of
nanofluids [17-22]. The theory of nanofluids has presented several fundamental
properties with the large enhancement in thermal conductivity as compared to the base
fluid [23].In this study, we have discussed the boundary layer flow of nanofluid over an
exponentially stretching surface with suction and injection. To the best of our
knowledge, the nanofluid over an exponentially stretching surface has not been discussed
so far. However, the present paper is only a theoretical idea, which is not checked
experimentally. The governing highly nonlinear partial differential equation of motion,
energy and nanoparticle volume fraction has been simplified by using suitable similarity
transformations and then solved analytically with the help of HAM [24-39]. The convergence of HAM solution has been discussed
by plotting h-curve. The effects of pertinent parameters of nanofluid have been
discussed through graphs.
2 Formulation of the problem
Consider the steady two-dimensional flow of an incompressible nanofluid over an
exponentially stretching surface. We are considering Cartesian coordinate system in such
a way that x-axis is taken along the stretching surface in the direction of the
motion and y-axis is normal to it. The plate is stretched in the x-direction
with a velocity U= U0 exp
(x/l). defined at y = 0. The flow and heat transfer
characteristics under the boundary layer approximations are governed by the following
equationswhere (u, v) are the velocity components in (x, y)
directions, ρis the fluid density of base fluid, ν
is the kinematic viscosity, T is the temperature, C is the
nanoparticle volume fraction, (ρc)is the effective
heat capacity of nanoparticles, (ρc)is the heat
capacity of the fluid, α = k/(ρc)is the thermal diffusivity of the fluid, Dis the
Brownian diffusion coefficient and Dis the thermophoretic
diffusion coefficient.The corresponding boundary conditions for the flow problem arein which U0 is the reference velocity, β(x)
is the suction and injection velocity when β(x) > 0 and
β(x) < 0, respectively, Tand
T∞ are the temperatures of the sheet and the ambient fluid,
C, C∞ are the nanoparticles volume
fraction of the plate and the fluid, respectively.We are interested in similarity solution of the above boundary value problem; therefore,
we introduce the following similarity transformationsMaking use of transformations (6), Eq. (1) is identically satisfied and Equations
(2)-(4) take the formwhereThe physical quantities of interest in this problem are the local skin-friction
coefficient C, Nusselt number Nuand the local
Sherwood number Sh, which are defined aswhere Re= U/ν is the local
Renolds number.
3 Solution by homotopy analysis method
For HAM solutions, the initial guesses and the linear operators L(i = 1 - 3) areThe operators satisfy the following propertiesin which C1 to C7 are constants. From Equations
(7) to (9), we can define the following zeroth-order deformation problemsIn Equations (17)-(22), ħ1, ħ2, and
ħ3 denote the non-zero auxiliary parameters,
H1, H2 and H3 are the
non-zero auxiliary function (H1 = H2 =
H3 = 1) andObviouslyWhen p varies from 0 to 1, then ,
,
vary from
initial guesses f0 (η), θ0
(η) and g0 (η) to the final
solutions f (η), θ (η) and g
(η), respectively. Considering that the auxiliary parameters
ħ1, ħ2 and ħ3
are so properly chosen that the Taylor series of ,
and expanded
with respect to an embedding parameter converge at p = 1, hence Equations
(17)-(19) becomeThe mth-order problems are defined as followwhereEmploying MATHEMATICA, Equations (35)-(40) have the following solutionsin which ,
,
,
are the constants and the numerical data of above solutions are shown through graphs in
the following section.
4 Results and discussion
The numerical data of the solutions (45)-(47), which is obtained with the help of
Mathematica, have been discussed through graphs. The convergence of the series solutions
strongly depends on the values of non-zero auxiliary parameters ħ(i = 1, 2, 3, h1 = h2 =
h3), which can adjust and control the convergence of the
solutions. Therefore, for the convergence of the solution, the ħ-curves is
plotted for velocity field in Figure 1. We have found the
convergence region of velocity for different values of suction injection parameter
v. It is seen that with the increase in suction parameter
v, the convergence region become smaller and smaller. Almost
similar kind of convergence regions appear for temperature and nanoparticle volume
fraction, which are not shown here. The non-dimensional velocity f′
against η for various values of suction injection parameter is shown in
Figure 2. It is observed that velocity field increases with the
increase in v. Moreover, the suction causes the reduction of the
boundary layer. The temperature field θ for different values of Prandtle
number Pr, Brownian parameter Nb, Lewis number Le and thermophoresis
parameter Nt is shown in Figures 3, 4, 5 and 6. In Figure 3, the temperature is plotted for different values of Pr. It is
observed that with the increase in Pr, there is a very slight change in temperature;
however, for very large Pr, the solutions seem to be unstable, which are not shown here.
The variation of Nb on θ is shown in Figure 4. It is depicted that with the increase in Nb, the temperature
profile increases. There is a minimal change in θ with the increase in
Le (see Figure 5). The results remain unchanged for
very large values of Le. The effects of Nt on θ are seen
in Figure 6. It is seen that temperature profile increases with
the increase in Nt; however, the thermal boundary layer thickness reduces. The
nanoparticle volume fraction g for different values of Pr, Nb, Nt
and Le is plotted in Figures 7, 8, 9 and 10. It is observed from
Figure 7 that with the increase in Nb, g decreases and
boundary layer for g also decreases. The effects of Pr on g are
minimal. (See Figure 8). The effects of Le on g
are shown in Figure 9. It is observed that g
decreases as well as layer thickness reduces with the increase in Le.
However, with the increase in Nt, g increases and layer thickness
reduces (See Figure 10).
Figure 1
.
Figure 2
Velocity for different values of suction and injection parameter.
Figure 3
Variation of temperature for different values of Pr when .
Figure 4
Variation of temperature for different values of .
Figure 5
Variation of temperature for different values of .
Figure 6
Variation of temperature for different values of .
Figure 7
Variation of nanoparticle fraction .
Figure 8
Variation of nanoparticle fraction .
Figure 9
Variation of nanoparticle fraction .
Figure 10
Variation of nanoparticle fraction .
.Velocity for different values of suction and injection parameter.Variation of temperature for different values of Pr when .Variation of temperature for different values of .Variation of temperature for different values of .Variation of temperature for different values of .Variation of nanoparticle fraction .Variation of nanoparticle fraction .Variation of nanoparticle fraction .Variation of nanoparticle fraction .
Competing interests
This is just the theoretical study, every experimentalist can check it experimentally
with our consent.
Authors' contributions
SN done the major part of the article; however, the funding and computational
suggestions and proof reading has been done by CL. All authors read and approved the
final manuscript.