Boundary Layer Stagnation-Point Flow of Second Grade Fluid over an Exponentially Stretching Sheet
Abdul Rehman1,, Ghulam Farooq1, Israr Ahmed1, Muhammad Naseer2, Muhammad Zulfiqar3
1Department of Mathematics, University of Balochistan, Quetta, Pakistan
2Department of Mathematics, Quaid-i-Azam University, Islamabad, Pakistan
3Department of Mathematics, GC University, Lahore, Pakistan
Abstract | |
1. | Introduction |
2. | Formulation |
3. | Analytical Solution of the Problem |
4. | Numerical Solution |
5. | Results and Discussion |
References |
Abstract
In this paper, the steady boundary layer stagnation point flow and heat transfer of a second grade fluid over an exponentially stretching sheet is investigated. The solutions are obtained through homotopy analysis method (HAM) and the Keller-box technique. Comparisons of both the solutions are given graphically as well as in tabular form. The effects of second grade parameter β Prandtl number Pr and other important physical parameters are presented through graphs and the salient features are discussed.
Keywords: boundary layer flow, heat transfer, second grade fluid, exponential stretching/shrinking, homotopy analysis method, keller-box technique
Copyright © 2015 Science and Education Publishing. All Rights Reserved.Cite this article:
- Abdul Rehman, Ghulam Farooq, Israr Ahmed, Muhammad Naseer, Muhammad Zulfiqar. Boundary Layer Stagnation-Point Flow of Second Grade Fluid over an Exponentially Stretching Sheet. American Journal of Applied Mathematics and Statistics. Vol. 3, No. 6, 2015, pp 211-219. https://pubs.sciepub.com/ajams/3/6/1
- Rehman, Abdul, et al. "Boundary Layer Stagnation-Point Flow of Second Grade Fluid over an Exponentially Stretching Sheet." American Journal of Applied Mathematics and Statistics 3.6 (2015): 211-219.
- Rehman, A. , Farooq, G. , Ahmed, I. , Naseer, M. , & Zulfiqar, M. (2015). Boundary Layer Stagnation-Point Flow of Second Grade Fluid over an Exponentially Stretching Sheet. American Journal of Applied Mathematics and Statistics, 3(6), 211-219.
- Rehman, Abdul, Ghulam Farooq, Israr Ahmed, Muhammad Naseer, and Muhammad Zulfiqar. "Boundary Layer Stagnation-Point Flow of Second Grade Fluid over an Exponentially Stretching Sheet." American Journal of Applied Mathematics and Statistics 3, no. 6 (2015): 211-219.
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At a glance: Figures
1. Introduction
Boundary layer flow due to stretching and stagnation point flows have achieved considerable attention due to its applications in industry and manufacturing processes. A large number of researchers are engaged with this area. Mention may be made to the works of [1-15][1]. In the analysis mentioned above simple stretching and stagnation flow have been used. However some researchers have used the exponential stretching because of its engineering applications. Sanjayanad and Khan [16] and Khan and Sanjayanad [17] have discussed the boundary layer flow of viscoelastic fluid due to exponential stretching sheet with and without heat transfer analysis. Later on, the idea of exponential stretching have further discussed by Nadeem et al [18, 19] for considering different non-Newtonian fluid models. Recently, Wei et al [20] have considered the stagnation point flow over an exponentially stretching/shrinking sheet for the viscous fluids.
Motivated from the above analysis, the aim of the present paper is to discuss the boundary layer flow of second grade fluid over an exponential stretching sheet. To the best of author’s knowledge only a single attempt is available which discussed the exponential stagnation with the exponential stretching when fluid is taken as Newtonian. However, this analysis has not been discussed so far for non-Newtonian fluids. Therefore, in this paper we have discussed both the analytical and numerical solutions of the second grade fluid with exponential stagnation point flow with exponential stretching in the presence of mixed convection heat transfer. It is also worth able to mention here that we have discussed the two strong solution techniques together. The analytical solutions are carried out with the help of homotopy analysis method [21-28][21]. For validity of the solution we have also provided numerical solutions obtained with the of Keller-box technique [29, 30, 31]. The physical features of embedding parameters are discussed through graphs.
2. Formulation
Let us consider a stagnation point flow of an incompressible second grade fluid over a stretching sheet. The stretching and stagnation point is assumed to be of exponential type. The Cartesian coordinates (x, y) are used such that x is along the surface of the sheet, while y is taken normal to it. The related boundary layer equations of second grade fluid in the presence of heat transfer take the following form
![]() | (1) |
![]() | (2) |
![]() | (3) |
Here are the velocity components along the
axes,
is the fluid density,
is the second grade parameter,
is the kinematic viscosity,
is temperature,
is the thermal diffusivity,
is pressure and
is the free-stream velocity. The corresponding boundary conditions for the problem are
![]() | (4) |
![]() | (5) |
where the free-stream velocity , the stretching velocity
, and the surface temperature
, are defined as
![]() | (6) |
in which and
are constant velocities,
is constant temperature and
is the reference length. Defining the following similarity transformations:
![]() | (7) |
![]() | (8) |
With the help of transformations defined in
and
,
is identically satisfied and
and
take the form
![]() | (9) |
![]() | (10) |
in which is the nondimensional second grade fluid parameter and
is the Prandtl number. The boundary conditions in nondimensional form can be written as
![]() | (11) |
![]() | (12) |
where .
The shear stress on the surfaces , the frictional drag coefficient
the heat flux at the surface
and the local Nusselt numbers
in dimensionless form are defined as
![]() | (13) |
![]() | (14) |
![]() | (15) |
![]() | (16) |
where , and
is the local Reynolds number.
3. Analytical Solution of the Problem
The analytical solution of the above boundary value problem is obtained with the help of HAM. For HAM solution we choose the initial guesses as
![]() | (17) |
The corresponding auxiliary linear operators are
![]() | (18) |
They satisfy
![]() | (19) |
where are arbitrary constants. The zeroth-order deformation equations are defined as
![]() | (20) |
![]() | (21) |
in which
![]() | (22) |
![]() | (23) |
The appropriate boundary conditions for the zeroth order system are
![]() | (24) |
![]() | (25) |
Further details of the HAM solution can be found in [21, 22].
4. Numerical Solution
For accuracy of the HAM solution the problem is also solved using the Keller-box technique. For Keller-box scheme the nonlinear system of differential equations is first converted into a first order system using appropriate substitution. This first order system is then approximated by difference equations using central difference. The resulting finite difference system is linearized by applying Newton's method, at the end the obtained linearized system is solved using block-elimination procedure.
5. Results and Discussion
The problem of stagnation point boundary layer flow of a second grade fluid over an exponentially stretching sheet is solved analytically as well as numerically. The analytical solutions of the system of ordinary differential equations subject to the boundary conditions
are obtained through homotopy analysis method (HAM). The convergence of the HAM solution is havily dependent upon the proper selection of
. To find appropriate values of
and
the convergence regions of
and
are plotted in Figure 1-Figure 3 for specified combinations of involved parameters. Figure 1 is displaying the convergence regions for
for different values of second grade parameter
when stretching parameter
It is observed that convergence region for viscous fluids
is
and convergence region is
for
that is with increase in
convergence region reduced. Figure 2 is graphed for convergence region of
for different values of
when second grade parameter
From Figure 2 it is observed that convergence region for rigid plat case
is
while for
convergence region is
Figure 3 is sketched to observe convergence region for the temperature gradient for specified vales of stretching parameter, second grade parameter and the Prandtl number. It is noted that convergence region is









































To check accuracy of the HAM solution, the problem is also solved with the help of second order implicit finite difference scheme Keller-box technique. Figure 4-Figure 6 are prepared for comparison of both the HAM and Keller-box solutions for specified values of involved parameters. Figure 4 is schemed to spot behavior of the HAM and Keller-box solutions for different values of when
It is noted that both solutions are in excellent contract. Figure 5 is organized to observe behavior of the two solutions for different values of second grade parameter
when
It is witnessed that both the solutions are in decent agreement. From Figure 5 it is also noted that an escalation in second grade parameter
demands a decrease in the velocity profile, this is due to the fact that higher
resembles to higher tensile stress between fluid layers, that in return corresponds to higher resistance to fluid motion. Figure 6 is drawn to check the behavior of the two solutions for the temperature profile
for different values of the Prandtl number
when
and
respectively. From Figure 6 it is seen that both the solutions are again in good agreement and that an increase in
demands a decline in the temperature profile
and also corresponds to decrease in thermal boundary layer thickness. This is due to the fact that large
corresponds to low thermal diffusivity, which in return corresponds to less energy transfer ability due to which thermal boundary layer decreases. Figure 7 is designed to observe influence of second grade parameter
over the velocity profile
for different values of
. From Figure 7 it is observed that
has a dual behavior for
for different
. That is, for
an increase in
implies decrease in
, whereas for
an increase in
corresponds to a decrease in
. From Figure 7 it is also noted that
has greater reliance over
when
is away from unity, but when
is near to unity, dependence of
over
is minimal. Figure 8 is plotted to perceive the effects of
for different values of
. From Figure 8 it is observed that as stretching parameter
increases the temperature profile decreases more rapidly with respect to
as compare to smaller
Figure 9 is drafted to observe the behavior of
with respect to
for different values of second grade parameter
. From Figure 8 it is observed that decrease in
with
is slow for larger values of
. Figure 10 is included to check the behavior of temperature profile against different
when
and
. It is perceived that
has a dual behavior against
for different
, that is when
, an increase in
produces increase in
, whereas when
, an increase in
gives opposite behavior. Figure 11 is affiliated to check behavior of second grade parameter
over skin-friction coefficient against Reynolds number
for different values of
. It is depicted from Figure 11 that with an increase in
skin-friction coefficient increases. The rate of increase in
against
decreases with an increase in
. It is also noted that skin-friction coefficient
has strong dependence over
and behavior of other involved parameters are noticeable only when
whereas,
shoots to infinity when
while
decays to zero for
Figure 12 portrays behavior of Nusselt numbers
for different values of local Reynolds number
against
. From Figure 12 an increase is observed in
with respect to
.



Table 1-Table 2 are prepared to compare the HAM and Keller-box solutions for velocity and temperature gradients at the surface of stretching sheet. From Table 1-Table 2 it is obvious that both the solutions are compatible. From Table 1 it is also predicted that wall shear stress at the surface decreases with
, when
, while
increases with
, when
. Whereas with respect to second grade parameter
wall shear stress
decreases. Table 2 contains values for temperature gradient at surface of stretching sheet. From Table 2 it is noted that with an increase in
and
the local heat flux decreases, whereas with an increase in
the heat transfer at the wall decrease.
Table 1. Comparison of behavior of wall shear stress at the surface τw, against different parameters. The tabulated values are the corresponding absolute values of f''(0)
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