Numerical investigation of stagnation point flow over a stretching sheet with convective boundary conditions

  • Muhammad Khairul Anuar Mohamed1,

    Affiliated with

    • Mohd Zuki Salleh2Email author,

      Affiliated with

      • Roslinda Nazar3 and

        Affiliated with

        • Anuar Ishak3

          Affiliated with

          Boundary Value Problems20132013:4

          DOI: 10.1186/1687-2770-2013-4

          Received: 31 August 2012

          Accepted: 26 December 2012

          Published: 16 January 2013

          Abstract

          In this study, the mathematical modeling for stagnation point flow over a stretching surface with convective boundary conditions is considered. The transformed boundary layer equations are solved numerically using the shooting method. Numerical solutions are obtained for the skin friction coefficient, the surface temperature as well as the velocity profiles. The features of the flow and heat transfer characteristics for various values of the Prandtl number, stretching parameter and conjugate parameter are analyzed and discussed.

          Keywords

          convective boundary conditions mathematical modeling stagnation point flow stretching sheet

          1 Introduction

          Problems related to convection boundary layer flows are important in engineering and industrial activities. Such flows are applied to manage thermal effects in many industrial outputs, for example, in electronic devices, computer power supply and also in an engine cooling system such as a heatsink in a car radiator. Sakiadis [1] was the first to study the boundary layer flow on a continuous solid surface moving at a constant speed. Due to entrainment of the ambient fluid, this boundary layer flow is quite different from the Blasius flow past a flat plate. Sakiadis’s theoretical predictions for Newtonian fluids were later corroborated experimentally by Tsou et al. [2]. Flow of a viscous fluid past a stretching sheet is a classical problem in fluid dynamics. Crane [3] was the first to study the convection boundary layer flow over a stretching sheet. The heat and mass transfer on a stretching sheet with suction or blowing was investigated by Gupta and Gupta [4]. They considered an isothermal moving plate and obtained the temperature and concentration distributions. Chen and Char [5] studied the laminar boundary layer flow and heat transfer from a linearly stretching, continuous sheet subjected to suction or blowing with prescribed wall temperature and heat flux. Stagnation flow towards a shrinking sheet was then investigated by Wang [6] who considered the prescribed wall temperature case. Ishak et al. [79] studied the MHD stagnation point flow towards a stretching sheet, mixed convection towards a vertical and continuosly stretching sheet and post stagnation-point towards a vertical and linearly stretching sheet. This type of problem was then extended to viscous fluids, viscoelastic fluids or micropolar fluids by many investigators by considering the usually applied boundary conditions, either prescribed wall temperature or prescribed wall heat flux. Recently, Mohamed et al. [10] studied the stagnation point flow over a stretching sheet and Hayat et al. [11] investigated the flow of a second grade fluid over a stretching surface with Newtonian heating.

          On the other hand, Merkin [12] has shown that in general, there are four common heating processes specifying the wall-to-ambient temperature distributions, namely (i) constant or prescribed wall temperature; (ii) constant or prescribed surface heat flux; (iii) Newtonian heating (NH); and (iv) convective/conjugate boundary conditions (CBC), where heat is supplied through a bounding surface of finite thickness and finite heat capacity. The interface temperature is not known a priori but depends on the intrinsic properties of the system, namely the thermal conductivity of the fluid or solid. Recent demands in heat transfer engineering have requested researchers to develop various new types of heat transfer equipments with superior performance, especially compact and light-weight ones. With the increasing need for small-size units, focus has been cast on the effects of the interaction between developments of thermal boundary layers in both fluid streams and of axial wall conduction, which usually affects the heat exchanges performance. Since the early paper by Luikov et al. [13], many contributions to the topic of conjugate heat transfer have been made. The conjugate/convective boundary condition has been used only quite recently by Aziz [14] who studied the laminar thermal boundary layer over a flat plate. This Blasius flow with the conjugate boundary condition then has been revisited by Rashidi and Erfani [15] and Magyari [16]. Makinde and Aziz [17] considered the hydromagnetic heat and mass transfer over a vertical plate. Ishak et al. [18, 19] have studied the thermal boundary layer flow on a moving plate (Sakiadis flow) with radiation effects. Recently, Merkin and Pop [20], Yao et al. [21], Yacob et al. [22] and Yacob and Ishak [23] investigated the boundary layer flow past a shrinking/stretching sheet with convective boundary conditions in a viscous fluid, nanofluid or micropolar fluid, respectively. Excellent reviews of the topics of convective heat transfer problems can be found in the books by Kimura et al. [24] and Martynenko and Khramtsov [25].

          Motivated by the works of Wang [6] and Yacob and Ishak [23], we aim in this study to investigate the problem of stagnation point flow over a stretching sheet with convective boundary conditions. The governing nonlinear partial differential equations are first transformed into a system of ordinary differential equations by a similarity transformation before being solved numerically using the shooting method (see Salleh et al. [26] for more details about this method).

          2 Mathematical formulation

          A steady two-dimensional stagnation-point flow over a stretching/shrinking plate immersed in an incompressible viscous fluid of ambient temperature T http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq1_HTML.gif is considered. It is assumed that the external velocity u e ( x ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq2_HTML.gif and the stretching velocity u w ( x ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq3_HTML.gif are of the forms u e ( x ) = a x http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq4_HTML.gif and u w ( x ) = b x http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq5_HTML.gif, where a and b are constants. The physical model and coordinate system of this problem are shown in Figure 1. It is further assumed that the plate is subjected to a conjugate boundary condition. The boundary layer equations are
          http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Equ1_HTML.gif
          (1)
          http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Equ2_HTML.gif
          (2)
          http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Equ3_HTML.gif
          (3)
          subject to the boundary conditions (Salleh et al. [27] and Aziz [14])
          http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Equ4_HTML.gif
          (4)
          where u and v are the velocity components along the x and y directions, respectively. Further, T is temperature, T f http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq6_HTML.gif is the temperature of the hot fluid, ν is the kinematic viscosity, k is the thermal conductivity, α is the thermal diffusivity and h f http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq7_HTML.gif is the heat transfer coefficient.
          http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Fig1_HTML.jpg
          Figure 1

          Physical model and the coordinate system.

          We now introduce the following similarity variables (see Salleh et al. [27] and Aziz [14]):
          η = ( u e ν x ) 1 / 2 y , ψ = ( ν x u e ) 1 / 2 f ( η ) , θ ( η ) = T T T  (NH) or θ ( η ) = T T T f T  (CBC) , http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Equ5_HTML.gif
          (5)
          where ψ is the stream function defined as u = ψ y http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq8_HTML.gif and v = ψ x http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq9_HTML.gif, which identically satisfies Equation (1). Thus, we have
          u = a x f ( η ) , v = ( a ν ) 1 / 2 f ( η ) , http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Equ6_HTML.gif
          (6)
          where prime denotes differentiation with respect to η. Substituting (5) and (6) into Equations (2) and (3), we obtain the following nonlinear ordinary differential equations:
          http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Equ7_HTML.gif
          (7)
          http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Equ8_HTML.gif
          (8)
          where Pr = ν α http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq10_HTML.gif is the Prandtl number. The boundary conditions (4) become
          http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Equ9_HTML.gif
          (9)
          http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Equ10_HTML.gif
          (10)
          where ε = b a 0 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq11_HTML.gif is the stretching parameter. Further, γ = h f ( ν a ) 1 / 2 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq12_HTML.gif (NH) or γ = h f ( ν a ) 1 / 2 k 1 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq13_HTML.gif (CBC) is the conjugate parameter for the convective boundary condition. It is noticed that γ = 0 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq14_HTML.gif is for the insulated plate and γ http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq15_HTML.gif is when the surface temperature is prescribed. The physical quantities of interest are the skin friction coefficient C f http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq16_HTML.gif and the local Nusselt number Nu x http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq17_HTML.gif which are given by
          C f = τ w ρ u e 2 , Nu x = x q w k ( T w T ) , http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Equ11_HTML.gif
          (11)
          where ρ is the fluid density. The surface shear stress τ w http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq18_HTML.gif and the surface heat flux q w http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq19_HTML.gif are given by
          τ w = μ ( u y ) y = 0 , q w = k ( T y ) y = 0 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Equ12_HTML.gif
          (12)
          with μ = ρ ν http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq20_HTML.gif and k being the dynamic viscosity and the thermal conductivity, respectively. Using the similarity variables in (5) gives
          C f Re x 1 / 2 = f ( 0 ) , Nu x Re x 1 / 2 = γ ( 1 θ ( 0 ) + 1 )  (NH) , Nu x Re x 1 / 2 = γ ( 1 θ ( 0 ) 1 )  (CBC) , http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Equ13_HTML.gif
          (13)

          where Re x = u e x ν http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq21_HTML.gif is the local Reynolds number and Nu x http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq17_HTML.gif is the local Nusselt number.

          3 Numerical method

          The system of boundary value problem (BVP) (7)-(10) was solved numerically via the shooting technique [2833] by converting it into an equivalent initial value problem (IVP). In this technique, we choose a suitable finite value of η http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq22_HTML.gif (where η http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq22_HTML.gif corresponds to η http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq23_HTML.gif) which depends on the values of the parameters considered. First, the system of equations (7) and (8) is reduced to a first-order system (by introducing new variables) as follows:
          http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Equ14_HTML.gif
          (14)
          http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Equ15_HTML.gif
          (15)
          with the boundary conditions
          f ( 0 ) = 0 , p ( 0 ) = ε , r ( 0 ) = γ [ 1 + θ ( 0 ) ]  (NH) or r ( 0 ) = γ [ 1 θ ( 0 ) ]  (CBC) , p ( η ) = 1 , θ ( η ) = 0 . http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Equ16_HTML.gif
          (16)
          Now, we have a set of ‘partial’ initial conditions
          f ( 0 ) = 0 , p ( 0 ) = ε , q ( 0 ) = α 1 , θ ( 0 ) = α 2 , r ( 0 ) = γ [ 1 + α 2 ]  (NH) or r ( 0 ) = γ [ 1 α 2 ]  (CBC) . http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Equa_HTML.gif

          The Runge-Kutta-Fehlberg method will be adopted to solve the applicable initial value problem. In order to integrate Equations (14) and (15) as an IVP, we require a value for f ( 0 ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq24_HTML.gif and θ ( 0 ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq25_HTML.gif, i.e., α 1 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq26_HTML.gif and α 2 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq27_HTML.gif respectively. Since these values are not given in the boundary conditions (16), suitable guess values for f ( 0 ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq24_HTML.gif and θ ( 0 ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq25_HTML.gif are made and integration is carried out. Then, we compare the calculated values for f ( η ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq28_HTML.gif and θ ( η ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq29_HTML.gif at η http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq22_HTML.gif with the given boundary conditions f ( η ) = 1 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq30_HTML.gif and θ ( η ) = 0 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq31_HTML.gif respectively and adjust the estimated values of f ( 0 ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq24_HTML.gif, θ ( 0 ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq25_HTML.gif and η http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq22_HTML.gif to give a better approximation for the solution. This computation is done with the aid of shootlib file in Maple software. In this study, the boundary layer thickness η http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq22_HTML.gif between 2 and 8 was used in the computation, depending on the values of the parameters considered so that the boundary condition at ‘infinity’ is achieved.

          4 Results and discussion

          Equations (7) and (8) subject to the boundary conditions (9) and (10) were solved numerically using the shooting method with three parameters considered, namely the Prandtl number Pr, the conjugate parameter γ and the stretching parameter ε. From the numerical solution, it is known that the boundary layer thicknesses η http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq22_HTML.gif from 2 to 8 is suitable to provide accurate numerical results. Due to the decoupled boundary layer equations (7) and (8), for ε = 0 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq32_HTML.gif, it has been found that there is a unique value of the skin friction coefficient, f ( 0 ) = 1.2325877 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq33_HTML.gif, which is in very good comparison with the classical value f ( 0 ) = 1.232588 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq34_HTML.gif reported by Hiemenz [34]. Table 1 presents the comparison between the present results with the previously reported results by Wang [6] and Yacob and Ishak [23] for various values of the stretching parameter ε. It has been found that they are in good-agreement. We can conclude that this method works efficiently for the present problem, and we are also confident that the results presented here are accurate.
          Table 1

          Comparison for the values of f ( 0 ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq24_HTML.gif with previously published results

          ε

          Wang [6]

          Yacob and Ishak [23]

          Present

          f ( 0 ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq35_HTML.gif

          2

          −1.88731

          −1.887307

          −1.8873066

          1

          0

          0

          0

          0.5

          0.71330

          0.713295

          0.7132949

          0

          1.232588

          1.232588

          1.2325877

          Figure 2 illustrates the variation of the surface temperature θ ( 0 ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq25_HTML.gif with ε when Pr = 0.72 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq36_HTML.gif and γ = 0.1 , 1 ,  and  1.5 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq37_HTML.gif. To get a physically acceptable solution, ε must be greater than or equal to a critical value, say εc, i.e., ε ε c http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq38_HTML.gif. It can be seen from this figure that θ ( 0 ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq25_HTML.gif bounded to 1 as ε approaches the critical value ε c 1.2460 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq39_HTML.gif.
          http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Fig2_HTML.jpg
          Figure 2

          Variation of the plate temperature θ ( 0 ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq40_HTML.gif with ε when Pr = 0.72 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq41_HTML.gif and γ = 0.1 , 1 , 1.5 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq42_HTML.gif .

          Figure 3 shows the variation of the surface temperature θ ( 0 ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq25_HTML.gif with the Prandtl number Pr, when ε = 1 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq43_HTML.gif and γ = 0.1 , 1  and  1.5 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq44_HTML.gif. It is noticed that the increasing value of the Prandtl number caused the decrease of surface temperature θ ( 0 ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq25_HTML.gif. From Figures 2 and 3, the same trend is observed for the variation of the surface temperature, i.e., the surface temperature increases as γ increases.
          http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Fig3_HTML.jpg
          Figure 3

          Variation of the plate temperature θ ( 0 ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq40_HTML.gif with Prandtl number Pr when ε = 1 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq45_HTML.gif and γ = 0.1 , 1 , 1.5 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq46_HTML.gif .

          Figure 4 presents the temperature profiles for various values of Pr. It has been found that as Pr increases, the temperature in the boundary layer decreases, and the thermal boundary layer thickness also decreases. This is because for small values of the Prandtl number, the fluid is highly thermal conductive. Physically, if Pr increases, the thermal diffusivity decreases, and this phenomenon leads to the decreasing of energy ability that reduces the thermal boundary layer.
          http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Fig4_HTML.jpg
          Figure 4

          Temperature profiles θ ( η ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq47_HTML.gif for various values of Pr when γ = 1 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq48_HTML.gif and ε = 1 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq45_HTML.gif (CBC).

          The temperature profiles with various values of ε are presented in Figure 5, and it has been found again that as ε increases, the temperature decreases, and the thermal boundary layer thickness also decreases, similar to the results presented in Figure 4. The temperature profiles presented in Figure 6 show that the temperature increases as the conjugate parameter increases, in contrast with the results presented in Figures 4 and 5 for the variation of Pr and ε.
          http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Fig5_HTML.jpg
          Figure 5

          Temperature profiles θ ( η ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq47_HTML.gif for various values of ε when γ = 1 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq48_HTML.gif and Pr = 0.72 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq41_HTML.gif (CBC).

          http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Fig6_HTML.jpg
          Figure 6

          Temperature profiles θ ( η ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq47_HTML.gif for various values of γ when ε = 1 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq45_HTML.gif and Pr = 0.72 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq41_HTML.gif (CBC).

          Lastly, Figure 7 shows the velocity profiles for different values of ε which produce f ( 0 ) = ε http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq49_HTML.gif and f ( η ) = 1 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq50_HTML.gif as η http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq23_HTML.gif. When ε > 1 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq51_HTML.gif, the flow has an inverted boundary layer structure and the thickness of the boundary layer decreases with ε. On the other hand, when ε < 1 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq52_HTML.gif, the flow has a boundary layer structure, which results from the fact that when b / a < 1 http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq53_HTML.gif, the external velocity ax of the surface exceeds the velocity bx of the stretching sheet. For this case, the thickness of the boundary layer increases with the increase of ε.
          http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_Fig7_HTML.jpg
          Figure 7

          Velocity profiles f ( η ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq54_HTML.gif for various values of ε .

          5 Conclusion

          In this paper, we have theoretically and numerically studied the problem of stagnation point flow over a stretching sheet with the convective boundary condition. It is shown how the Prandtl number Pr, stretching parameter ε and conjugate parameter γ affect the values of the surface temperature θ ( 0 ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq25_HTML.gif and skin friction coefficient f ( 0 ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq55_HTML.gif.

          We can conclude that the thermal boundary layer thickness depends strongly on these three parameters. Further, it is seen that an increase in the Prandtl number Pr and stretching parameter ε results in a decrease of the temperature. The reason is that smaller values of Pr are equivalent to increasing thermal conductivity and therefore, heat is capable of diffusing away from the heated wall more rapidly than at higher values of Pr. However, the increase of conjugate parameter γ leads to an increase of the surface temperature θ ( 0 ) http://static-content.springer.com/image/art%3A10.1186%2F1687-2770-2013-4/MediaObjects/13661_2012_Article_263_IEq25_HTML.gif.

          Declarations

          Acknowledgements

          The authors wish to thank the anonymous reviewers for their valuable comments and suggestions. The financial support received from the Universiti Malaysia Pahang (Project Codes: RDU110108 and RDU110390) and the Universiti Kebangsaan Malaysia (Project Code: DIP-2012-31) is gratefully acknowledged.

          Authors’ Affiliations

          (1)
          Faculty of Information and Interactive Technology, University College Shahputra
          (2)
          Faculty of Industrial Science and Technology, Universiti Malaysia Pahang, UMP
          (3)
          School of Mathematical Science, Faculty of Science and Technology, Universiti Kebangsaan Malaysia, UKM

          References

          1. Sakiadis BC: Boundary-layer behavior on continuous solid surfaces: I. Boundary-layer equations for two-dimensional and axisymmetric flow. AIChE J. 1961, 7(1):26-28. 10.1002/aic.690070108View Article
          2. Tsou FK, Sparrow EM, Goldstein RJ: Flow and heat transfer in the boundary layer on a continuous moving surface. Int. J. Heat Mass Transf. 1967, 10(2):219-235. 10.1016/0017-9310(67)90100-7View Article
          3. Crane LJ: Flow past a stretching plate. Z. Angew. Math. Phys. 1970, 21: 645-647. 10.1007/BF01587695View Article
          4. Gupta PS, Gupta AS: Heat and mass transfer on a stretching sheet with suction or blowing. Can. J. Chem. Eng. 1977, 55(6):744-746. 10.1002/cjce.5450550619View Article
          5. Chen CK, Char M: Heat transfer on a continuous, stretching surface with suction and blowing. J. Math. Anal. Appl. 1988, 135: 568-580. 10.1016/0022-247X(88)90172-2MATHMathSciNetView Article
          6. Wang CY: Stagnation flow towards a shrinking sheet. Int. J. Non-Linear Mech. 2008, 43(5):377-382. 10.1016/j.ijnonlinmec.2007.12.021View Article
          7. Ishak A, Nazar R, Pop I: Mixed convection on the stagnation point flow toward a vertical, continuously stretching sheet. J. Heat Transf. 2007, 129(8):1087-1090. 10.1115/1.2737482View Article
          8. Ishak A, Nazar R, Pop I: Post stagnation point boundary layer flow and mixed convection heat transfer over a vertical, linearly stretching sheet. Arch. Mech. 2008, 60: 303-322.MATHMathSciNet
          9. Ishak A, Jafar K, Nazar R, Pop I: MHD stagnation point flow towards a stretching sheet. Phys. A, Stat. Mech. Appl. 2009, 388(17):3377-3383. 10.1016/j.physa.2009.05.026View Article
          10. Mohamed MKA, Salleh MZ, Nazar R, Ishak A: Stagnation point flow over a stretching sheet with Newtonian heating. Sains Malays. 2012, 41(11):1467-1473.
          11. Hayat T, Iqbal Z, Mustafa M: Flow of a second grade fluid over a stretching surface with Newtonian heating. J. Mech. 2012, 28(1):209-216. 10.1017/jmech.2012.21View Article
          12. Merkin JH: Natural-convection boundary-layer flow on a vertical surface with Newtonian heating. Int. J. Heat Fluid Flow 1994, 15(5):392-398. 10.1016/0142-727X(94)90053-1View Article
          13. Luikov AV, Aleksashenko VA, Aleksashenko AA: Analytical methods of solution of conjugated problems in convective heat transfer. Int. J. Heat Mass Transf. 1971, 14(8):1047-1056. 10.1016/0017-9310(71)90203-1MATHView Article
          14. Aziz A: A similarity solution for laminar thermal boundary layer over a flat plate with a convective surface boundary condition. Commun. Nonlinear Sci. Numer. Simul. 2009, 14(4):1064-1068. 10.1016/j.cnsns.2008.05.003View Article
          15. Rashidi MM, Erfani E: A novel analytical solution of the thermal boundary-layer over a flat plate with a convective surface boundary condition using DTM-Pade. 2009 International Conference on Signal Processing Systems 2009.
          16. Magyari E: Comment on ‘A similarity solution for laminar thermal boundary layer over a flat plate with a convective surface boundary condition’ by A. Aziz, Comm. Nonlinear Sci. Numer. Simul. 2009, 14:1064-1068. Commun. Nonlinear Sci. Numer. Simul. 2010, 16: 599-601.View Article
          17. Makinde OD, Aziz A: MHD mixed convection from a vertical plate embedded in a porous medium with a convective boundary condition. Int. J. Therm. Sci. 2010, 49(9):1813-1820. 10.1016/j.ijthermalsci.2010.05.015View Article
          18. Ishak A: Similarity solutions for flow and heat transfer over a permeable surface with convective boundary condition. Appl. Math. Comput. 2010, 217(2):837-842. 10.1016/j.amc.2010.06.026MATHMathSciNetView Article
          19. Ishak A, Yacob N, Bachok N: Radiation effects on the thermal boundary layer flow over a moving plate with convective boundary condition. Meccanica 2011, 46(4):795-801. 10.1007/s11012-010-9338-4MATHMathSciNetView Article
          20. Merkin JH, Pop I: The forced convection flow of a uniform stream over a flat surface with a convective surface boundary condition. Commun. Nonlinear Sci. Numer. Simul. 2011, 16(9):3602-3609. 10.1016/j.cnsns.2011.01.007MATHMathSciNetView Article
          21. Yao S, Fang T, Zhong Y: Heat transfer of a generalized stretching/shrinking wall problem with convective boundary conditions. Commun. Nonlinear Sci. Numer. Simul. 2011, 16(2):752-760. 10.1016/j.cnsns.2010.05.028MATHView Article
          22. Yacob NA, Ishak A, Pop I, Vajravelu K: Boundary layer flow past a stretching/shrinking surface beneath an external uniform shear flow with a convective surface boundary condition in a nanofluid. Nanoscale Res. Lett. 2011, 6(1):1-7.View Article
          23. Yacob NA, Ishak A: Stagnation point flow towards a stretching/shrinking sheet in a micropolar fluid with a convective surface boundary condition. Can. J. Chem. Eng. 2012, 90(3):621-626. 10.1002/cjce.20517View Article
          24. Kimura S, Kiwata T, Okajima A, Pop I: Conjugate natural convection in porous media. Adv. Water Resour. 1997, 20: 111-126. 10.1016/S0309-1708(96)00025-5View Article
          25. Martynenko OG, Khramtsov PP: Free Convective Heat Transfer. Springer, Berlin; 2005.
          26. Salleh MZ, Mohamed N, Khairuddin R, Khasi’ie NS, Nazar R: Numerical study of free convection boundary layer flow on a vertical surface with prescribed wall temperature, heat flux and Newtonian heating using shooting method. Proceedings of the International Conference on Software Engineering and Computer Systems (ICSECS’09) UMP, Kuantan 19-21 October 2009, 94-98.
          27. Salleh MZ, Nazar R, Pop I: Boundary layer flow and heat transfer over a stretching sheet with Newtonian heating. J. Taiwan Inst. Chem. Eng. 2010, 41(6):651-655. 10.1016/j.jtice.2010.01.013View Article
          28. Bailey PB, Shampine LF, Waltman PE: Nonlinear Two Point Boundary Value Problems. Academic Press, New York; 1968.MATH
          29. Meade DB, Haran BS, White RE: The shooting technique for the solution of two-point boundary value problems. Maple Technol. 1996, 3: 85-93.
          30. Bhattacharyya K, Layek GC: Effects of suction/blowing on steady boundary layer stagnation-point flow and heat transfer towards a shrinking sheet with thermal radiation. Int. J. Heat Mass Transf. 2011, 54: 302-307. 10.1016/j.ijheatmasstransfer.2010.09.043MATHView Article
          31. Bhattacharyya K, Mukhopadhyay S, Layek GC: Slip effects on boundary layer stagnation-point flow and heat transfer towards a shrinking sheet. Int. J. Heat Mass Transf. 2011, 54: 308-313. 10.1016/j.ijheatmasstransfer.2010.09.041MATHView Article
          32. Ishak A: Thermal boundary layer flow over a stretching sheet in a micropolar fluid with radiation effect. Meccanica 2010, 45: 367-373. 10.1007/s11012-009-9257-4MATHView Article
          33. Bachok N, Ishak A, Pop I: Melting heat transfer in boundary layer stagnation-point flow towards a stretching/shrinking sheet. Phys. Lett. A 2010, 374: 4075-4079. 10.1016/j.physleta.2010.08.032MATHView Article
          34. Hiemenz K: Die Grenzschicht an einem in den gleichformigen Flussigkeitsstrom eingetauchten geraden Kreiszylinder. Dinglers Polytech. J. 1911, 32: 321-410.

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          © Mohamed et al.; licensee Springer. 2013

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