<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article  PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd"><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article"><front><journal-meta><journal-id journal-id-type="publisher-id">AJCM</journal-id><journal-title-group><journal-title>American Journal of Computational Mathematics</journal-title></journal-title-group><issn pub-type="epub">2161-1203</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/ajcm.2016.61005</article-id><article-id pub-id-type="publisher-id">AJCM-65175</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  MHD Stagnation Point Flow of a Casson Fluid over a Nonlinearly Stretching Sheet with Viscous Dissipation
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>onica</surname><given-names>Medikare</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Sucharitha</surname><given-names>Joga</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Kishore</surname><given-names>Kumar Chidem</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Department of Mathematics, Osmania University, Hyderabad, India</addr-line></aff><aff id="aff2"><addr-line>Department of Mathematics, Nizam College, Osmania University, Hyderabad, India</addr-line></aff><pub-date pub-type="epub"><day>23</day><month>02</month><year>2016</year></pub-date><volume>06</volume><issue>01</issue><fpage>37</fpage><lpage>48</lpage><history><date date-type="received"><day>6</day>	<month>February</month>	<year>2016</year></date><date date-type="rev-recd"><day>accepted</day>	<month>27</month>	<year>March</year>	</date><date date-type="accepted"><day>30</day>	<month>March</month>	<year>2016</year></date></history><permissions><copyright-statement>&#169; Copyright  2014 by authors and Scientific Research Publishing Inc. </copyright-statement><copyright-year>2014</copyright-year><license><license-p>This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/</license-p></license></permissions><abstract><p>
 
 
  Study to analyze the 
  MHD stagnation point flow of a Casson fluid over a nonlinearly stretching sheet with viscous dissipation was carried out. The partial differential equations governing this phenomenon were transformed into coupled nonlinear ordinary differential equations with suitable similarity transformations. These equations were then solved by finite difference technique known as Keller Box method. The various parameters such as Prandtl number (
  Pr
  ), Eckert number (
  Ec
  ), Magnetic parameter (
  M
  ), Casson parameter (
  β
  ) and non linear stretching parameter (
  n
  ) determining the velocity and temperature distributions, the local Skin friction coefficient and the local Nusselt number governing such a flow were also analyzed. On analysis it was found that the Casson fluid parameter (
  β
  ) decreased both the fluid velocity and temperature whereas an increase in (
  β
  ) increased both the heat transfer rate and wall skin-friction coefficient.
 
</p></abstract><kwd-group><kwd>Stagnation Point</kwd><kwd> Casson Fluid</kwd><kwd> MHD</kwd><kwd> Viscous Dissipation</kwd><kwd> Nonlinear Stretching Sheet</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The study of boundary layer flow over a stretching sheet has been a great challenge for researchers and it has immense applications in various industrial processes such as extraction of polymer sheet, paper production, wire drawing, glass-ﬁber production etc. The flow of incompressible fluid over a linearly stretching sheet was first investigated by Crane [<xref ref-type="bibr" rid="scirp.65175-ref1">1</xref>] . The Mass Transfer with suction or blowing over a stretching sheet was investigated by Gupta and Gupta [<xref ref-type="bibr" rid="scirp.65175-ref2">2</xref>] . The heat transfer over a stretching sheet of a hydromagnetic flow has been studied by Chakrabarthi and Gupta [<xref ref-type="bibr" rid="scirp.65175-ref3">3</xref>] . The flow over a stretching surface in three diemsional was discussed by Wang [<xref ref-type="bibr" rid="scirp.65175-ref4">4</xref>] . The MHD flow characteristics over a stretching sheet of a viscoelastic fluid was demonstrated by Andersson [<xref ref-type="bibr" rid="scirp.65175-ref5">5</xref>] . Later his work was extended by M. I. Char [<xref ref-type="bibr" rid="scirp.65175-ref6">6</xref>] with mass transfer.</p><p>The numerical analysis of magnetic field on Eyring-Powell fluid flow towards a stretching sheet has been discussed by N S Akbar [<xref ref-type="bibr" rid="scirp.65175-ref7">7</xref>] .</p><p>All the above investigations are restricted for the flow over a linearly stretching sheet but it is not necessary that the stretching sheet has to be linear. Vajravelu [<xref ref-type="bibr" rid="scirp.65175-ref8">8</xref>] analyzed the viscous flow over a nonlinearly stretching sheet. The heat transfer characteristics of a viscous fluid over a non linear stretching sheet was later introduced by Cortell [<xref ref-type="bibr" rid="scirp.65175-ref9">9</xref>] . A great number of studies for the boundary layer flow over a non linear stretching sheet under different aspects of heat and mass transfer, slip and convective boundary conditions etc., are presented in the literature [<xref ref-type="bibr" rid="scirp.65175-ref10">10</xref>] - [<xref ref-type="bibr" rid="scirp.65175-ref16">16</xref>] .</p><p>The study of stagnation point flow towards a stationary semi infinite wall was first introduced by Hiemenz [<xref ref-type="bibr" rid="scirp.65175-ref17">17</xref>] in a two dimensional case. In his work he reduced the Navier-Stokes equations into non linear ordinary differential equations with the help of similarity transformations. The same problem was extended by Homann [<xref ref-type="bibr" rid="scirp.65175-ref18">18</xref>] . Chiam [<xref ref-type="bibr" rid="scirp.65175-ref19">19</xref>] combined the works of Hiemenz and Crane i.e., the stagnation point flow towards a stretching sheet when the stretching rate of the plate is equal to the strain rate of the stagnation point flow and he found no boundary layer structure near the plate. El-Dab [<xref ref-type="bibr" rid="scirp.65175-ref20">20</xref>] obtained numerical solution of MHD flow of micropolar fluid with heat and mass transfer towards a stagnation point on a vertical plate.</p><p>In all these attempts, stagnation point flow due to the stretching sheet was analyzed. The boundary layer flow over a shrinking sheet was ﬁrst investigated by Wang [<xref ref-type="bibr" rid="scirp.65175-ref21">21</xref>] . He dealt with stagnation point flow on a two dimensional shrinking sheet and axi symmetric stagnation point flow on a axisymmetric shrinking sheet. In contrast, Lok et al. [<xref ref-type="bibr" rid="scirp.65175-ref22">22</xref>] numerically studied non orthogonal stagnation point flow towards a stretching sheet. In his work, he determined that the obliqueness of a free stream line causes the shifting of the stagnation point towards the incoming flow.</p><p>Many fluids in industries resemble non-Newtonian behaviour. Non-Newtonian fluids are more appropriate than Newtonian fluids because of their varied industrial applications like petroleum drilling, polymer engineering, certain separation processes, food manufacturing etc.</p><p>For non-Newtonian fluids, the relationship between stress and the rate of strain is not linear and it is difficult to express all these properties in a single constitutive equation. Consequently, these fluid models [<xref ref-type="bibr" rid="scirp.65175-ref23">23</xref>] - [<xref ref-type="bibr" rid="scirp.65175-ref31">31</xref>] have been proposed depending on various physical characters.</p><p>Casson fluid is one such type of such non-Newtonian fluid, which behaves like an elastic solid, with a yield shear stress existing in the constitutive equation. This ﬂuid model has its origin in modelling of ﬂow of many biological ﬂuids especially blood. Examples of such fluids include foams, yoghurt, molten chocolate, cosmetics, nail polish, tomato puree etc. Casson [<xref ref-type="bibr" rid="scirp.65175-ref32">32</xref>] introduced this model to predict the flow behaviour of pigment oil suspensions of the printing ink type. Later on, several researchers studied Casson fluid pertaining to different flow situations. The unsteady boundary layer flow and heat transfer of a Casson fluid over a moving flat plate with a parallel free stream was studied by Mustafa et al. [<xref ref-type="bibr" rid="scirp.65175-ref33">33</xref>] . The exact solution for boundary layer flow of Casson fluid over a permeable stretching/shrinking sheet with and without external magnetic field was discussed by Bhattacharyya et al. [<xref ref-type="bibr" rid="scirp.65175-ref34">34</xref>] [<xref ref-type="bibr" rid="scirp.65175-ref35">35</xref>] . The Casson ﬂuid has an inﬁnite viscosity at zero rate of shear and a yield stress below which no ﬂow occurs and a zero velocity at an inﬁnite shear rate [<xref ref-type="bibr" rid="scirp.65175-ref36">36</xref>] [<xref ref-type="bibr" rid="scirp.65175-ref37">37</xref>] . An excellent collection of articles can be found in [<xref ref-type="bibr" rid="scirp.65175-ref38">38</xref>] - [<xref ref-type="bibr" rid="scirp.65175-ref40">40</xref>] .</p><p>Motivated by the above investigations on non-Newtonian fluids and its wide applications, the objective of the present study is to analyze MHD stagnation point flow of a Casson fluid over a non linear stretching sheet with viscous dissipation. We have extended the works of Vajravelu [<xref ref-type="bibr" rid="scirp.65175-ref8">8</xref>] by considering magnetic field, stagnation point and viscous dissipation effects to the flow regime for more physical implications. In addition to this, the roles of the other parameters are explained in brief. The results are displayed in figures and tables. A parametric study of the physical parameters is conducted and a representative set of numerical results for the velocity and temperature profiles as well as the skin friction coefficient and local Nusselt number is illustrated graphically to show interesting features of the solutions. Here the governing partial differential equations were transformed into coupled non linear ordinary differential equations using appropriate similarity tranformations. The transformed ODE’s were then solved by Keller Box method. However, to the best of our knowledge no work has been carried out yet to analyze the present result. The layout of this paper is as follows.</p><p>In Section 2 the problem is formulated and similarity transformation has been employed to transform the partial differential equation into a non linear ordinary differential equations. In Section 3 a numerical solution using Keller box method has been discussed. In Section 4 the numerical results have been discussed graphically. Finally, the main concluding observations are mentioned in Section 5.</p></sec><sec id="s2"><title>2. Mathematical Formulation</title><p>Consider the steady two-dimensional stagnation point ﬂow of an incompressible Casson ﬂuid located at y = 0. The flow being confined in the region y &gt; 0. We take the non-linear stretching sheet in the XOY plane (see <xref ref-type="fig" rid="fig1">Figure 1</xref>). Along the x-axis, two equal and opposite forces are being applied. The surface is stretched in the x-di- rection such that the x-component of the velocity varies non-linearly along it, i.e. <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x6.png" xlink:type="simple"/></inline-formula>where c &gt; 0 is constant of proportionality and n is a power index. A magnetic ﬁeld of uniform strength <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x7.png" xlink:type="simple"/></inline-formula> is applied perpendicular to the surface. The magnetic Reynolds number is taken to be small enough so that the induced magnetic ﬁeld can be neglected in comparison to the applied magnetic field. It is also assumed that the ambient ﬂuid is moved with a velocity<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x8.png" xlink:type="simple"/></inline-formula>, where a &gt; 0 is a constant. The rheological equation of state for an isotropic and incompressible ﬂow of the Casson ﬂuid [Nakamura and Sawada [<xref ref-type="bibr" rid="scirp.65175-ref34">34</xref>] , Mustafa et al. [<xref ref-type="bibr" rid="scirp.65175-ref31">31</xref>] is given by</p><disp-formula id="scirp.65175-formula1308"><graphic  xlink:href="http://html.scirp.org/file/5-1100503x9.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x10.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x11.png" xlink:type="simple"/></inline-formula> are the plastic dynamic viscosity, yield stress of the fluid respectively. Similarly <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x12.png" xlink:type="simple"/></inline-formula> is the product of the component of deformation rate with itself, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x13.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x14.png" xlink:type="simple"/></inline-formula>is the (i, j)-th component of the deformation rate and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x15.png" xlink:type="simple"/></inline-formula> is a critical value of this product based on the non-Newtonian model.</p><p>The continuity, momentum and energy equations governing the fluid flow are given by</p><disp-formula id="scirp.65175-formula1309"><graphic  xlink:href="http://html.scirp.org/file/5-1100503x16.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.65175-formula1310"><graphic  xlink:href="http://html.scirp.org/file/5-1100503x17.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.65175-formula1311"><graphic  xlink:href="http://html.scirp.org/file/5-1100503x18.png"  xlink:type="simple"/></disp-formula><p>where u, v are the velocity components in x, y direction respectively, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x19.png" xlink:type="simple"/></inline-formula>is the kinematic viscosity, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x20.png" xlink:type="simple"/></inline-formula>is the viscosity,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x21.png" xlink:type="simple"/></inline-formula> is the Casson fluid parameter, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x22.png" xlink:type="simple"/></inline-formula>is the thermal diffusivity of the fluid, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x23.png" xlink:type="simple"/></inline-formula>is thespecific heat and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x24.png" xlink:type="simple"/></inline-formula> is the magnetic field.</p><p>The suitable boundary conditions are given by</p><fig-group id="fig1"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Physical sketch of the given problem.</title></caption><fig id ="fig1_1"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-1100503x25.png"/></fig></fig-group><disp-formula id="scirp.65175-formula1312"><graphic  xlink:href="http://html.scirp.org/file/5-1100503x26.png"  xlink:type="simple"/></disp-formula><p>Here, c (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x27.png" xlink:type="simple"/></inline-formula>) is the surface stretching sheet related parameter. <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x28.png" xlink:type="simple"/></inline-formula>are the uniform temperature at the sheet, free stream temperature respectively and n is the power index related to the surface stretching speed.</p><p>With the help of following similarity transformations</p><disp-formula id="scirp.65175-formula1313"><graphic  xlink:href="http://html.scirp.org/file/5-1100503x29.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.65175-formula1314"><graphic  xlink:href="http://html.scirp.org/file/5-1100503x30.png"  xlink:type="simple"/></disp-formula><p>The Equations (1), (2) and (3) are transformed into coupled non linear ordinary differential equations as follows.</p><disp-formula id="scirp.65175-formula1315"><graphic  xlink:href="http://html.scirp.org/file/5-1100503x31.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.65175-formula1316"><graphic  xlink:href="http://html.scirp.org/file/5-1100503x32.png"  xlink:type="simple"/></disp-formula><p>and the boundary conditions are transformed into</p><disp-formula id="scirp.65175-formula1317"><graphic  xlink:href="http://html.scirp.org/file/5-1100503x33.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.65175-formula1318"><graphic  xlink:href="http://html.scirp.org/file/5-1100503x34.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x35.png" xlink:type="simple"/></inline-formula> is the Prandtl Number, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x35.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x36.png" xlink:type="simple"/></inline-formula>is the magnetic parameter,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x37.png" xlink:type="simple"/></inline-formula>is the Eckert number and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x37.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x38.png" xlink:type="simple"/></inline-formula> is the velocity ratio parameter.</p><p>where prime denotes the differentiation with respect to<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x39.png" xlink:type="simple"/></inline-formula>.</p><p>The quantities of practical interest are the Skin friction coefficient <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x40.png" xlink:type="simple"/></inline-formula> and the Local Nusselt number <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x40.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x41.png" xlink:type="simple"/></inline-formula> which are defined as</p><disp-formula id="scirp.65175-formula1319"><graphic  xlink:href="http://html.scirp.org/file/5-1100503x42.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x43.png" xlink:type="simple"/></inline-formula> is the shear stress or skin friction along the stretching sheet and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x43.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x44.png" xlink:type="simple"/></inline-formula> is the heat flux from the sheet.</p><p>Hence the dimensionless form of Skin friction <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x45.png" xlink:type="simple"/></inline-formula> and the Local Nusselt number <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x45.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x46.png" xlink:type="simple"/></inline-formula> are given by</p><disp-formula id="scirp.65175-formula1320"><graphic  xlink:href="http://html.scirp.org/file/5-1100503x47.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x48.png" xlink:type="simple"/></inline-formula> is the local Reynolds number.</p></sec><sec id="s3"><title>3. Numerical Solution</title><p>The numerical solution for the above coupled ordinary differential equations for different values of governing parameters is obtained using finite difference scheme called Keller-box method. This method involves the four main steps which are as follows:</p><p>1) Reduce the equation or system of equations to a first order system.</p><p>2) Write the difference equations using central differences.</p><p>3) Linearize the resulting algebraic equations (if they are non-linear) by Newton’s method.</p><p>4) Write them in matrix-vector form and use the block-tridiagonal-elimination technique to solve the linear system.</p><p>This method has been widely used in laminar and turbulent boundary layer flows. It seems to be much faster, easier to program, more efficient and flexible to use than other methods.</p></sec><sec id="s4"><title>4. Results and Discussion</title><p>The numerical computations are carried out with the help of Keller box method. The effects of different parameters like Stagnation point, MHD, viscous dissipation on velocity and temperature profiles has been clearly analyzed including with its physical quantities of significance. The effect of Casson fluid parameter on skin friction and local Nusselt number has been examined. Apart from those the various quantities of non linear stretching parameter were also analyzed.</p><p>To verify the accuracy of the present results, comparison has been made with the previous results of Vajravelu and Cortell (<xref ref-type="table" rid="table1">Table 1</xref>).</p><p><xref ref-type="table" rid="table1">Table 1</xref> clearly shows the values of skin friction coefficient <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x49.png" xlink:type="simple"/></inline-formula> and heat transfer rate <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x49.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x50.png" xlink:type="simple"/></inline-formula> at the surface for different values of non linear stretching parameter n which are found to be in excellent agreement.</p><p>The effects of magnetic parameter M and velocity ratio parameter λ on the flow field velocity is displayed in <xref ref-type="fig" rid="fig2">Figure 2</xref>. It shows that the velocity of the fluid is not affected by various values of M for λ = 1 i.e., when the velocity of ambient fluid and the velocity of the sheet are same, where as for λ = 0.2 an increase in M decreases the velocity boundary layer thickness. However, with an increase in M the flow field velocity increases and boundary layer thickness decreases for λ = 2. Due to the Lorentz force induced by the action of magnetic field ,the thickness of boundary layer decreases for both λ = 0.2 and λ = 2.</p><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Values<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x51.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x51.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x52.png" xlink:type="simple"/></inline-formula>of with Ec = 0, M = 0</title></caption><table><tbody><thead><tr><th align="center" valign="middle"  rowspan="3"  >n</th><th align="center" valign="middle"  colspan="3"  >Vajravelu</th><th align="center" valign="middle" >Cortell</th><th align="center" valign="middle"  colspan="3"  >Present Study</th></tr></thead><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x53.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle"  colspan="2"  ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x54.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x55.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x56.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle"  colspan="2"  ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x57.png" xlink:type="simple"/></inline-formula></td></tr><tr><td align="center" valign="middle" >Pr</td><td align="center" valign="middle" >0.71</td><td align="center" valign="middle" >7.0</td><td align="center" valign="middle" ></td><td align="center" valign="middle" >Pr</td><td align="center" valign="middle" >0.71</td><td align="center" valign="middle" >7.0</td></tr><tr><td align="center" valign="middle" >1</td><td align="center" valign="middle" >−1.0000</td><td align="center" valign="middle" >−0.4590</td><td align="center" valign="middle" >−1.8953</td><td align="center" valign="middle" >−1.000000</td><td align="center" valign="middle" >−1.0000</td><td align="center" valign="middle" >−0.4590</td><td align="center" valign="middle" >−1.8954</td></tr><tr><td align="center" valign="middle" >5</td><td align="center" valign="middle" >−0.1945</td><td align="center" valign="middle" >−0.4394</td><td align="center" valign="middle" >−1.8610</td><td align="center" valign="middle" >−</td><td align="center" valign="middle" >−0.1945</td><td align="center" valign="middle" >−0.4395</td><td align="center" valign="middle" >−1.8616</td></tr><tr><td align="center" valign="middle" >10</td><td align="center" valign="middle" >−1.2348</td><td align="center" valign="middle" >−0.4357</td><td align="center" valign="middle" >−1.8541</td><td align="center" valign="middle" >−1.234875</td><td align="center" valign="middle" >−1.2348</td><td align="center" valign="middle" >−0.4356</td><td align="center" valign="middle" >−1.8547</td></tr></tbody></table></table-wrap><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Velocity profile for different values of M when λ = 0.2, 1, 2 and β = 2, n = 10, Pr = 0.71</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-1100503x58.png"/></fig><p><xref ref-type="fig" rid="fig3">Figure 3</xref> depicts the effect of the velocity ratio parameter on the flow field velocity. It can be observed that for λ &lt; 1 i.e., when the stretching velocity of the sheet exceeds the free stream velocity, the velocity of the fluid and the boundary layer thickness increases with an increase in λ. Moreover, for λ &gt; 1 i.e., when the free stream exceeds the stretching velocity, the flow velocity increases and the boundary layer thickness decreases with an increase in λ. If λ = 1 i.e., when the stretching and free stream velocities are equal, then there is no boundary layer of Casson fluid flow near the sheet.</p><p><xref ref-type="fig" rid="fig4">Figure 4</xref> and <xref ref-type="fig" rid="fig5">Figure 5</xref> indicates the effect of Casson parameter β on velocity and temperature profiles for a non linear stretching parameter n = 10. It can be observed from <xref ref-type="fig" rid="fig4">Figure 4</xref> that the fluid velocity decreases when β increases. Due to the increase of Casson parameter β, the yield stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x59.png" xlink:type="simple"/></inline-formula> reduces and hence the momentum boundary layer thickness decreases.</p><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Velocity profile for various values of λ when M = 1, β = 2, n = 10, Pr = 0.71 and Ec = 1</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-1100503x60.png"/></fig><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Velocity profile for various values of β</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-1100503x61.png"/></fig><p><xref ref-type="fig" rid="fig5">Figure 5</xref> shows that the temperature decreases with increase in β implying that the thermal boundary layer decreases. In the vicinity of the sheet the temperature profile curves for larger values of β are lower than for those with smaller values of β. However, as we move far from the sheet within the thermal boundary layer, viscous dissipation vanishes and the curves for larger values of β tend to override for smaller values of β. Hence the temperature profiles intersect each other at a point and the behaviour goes other way round at this point.</p><p><xref ref-type="fig" rid="fig6">Figure 6</xref> and <xref ref-type="fig" rid="fig7">Figure 7</xref> indicates the velocity and the temperature proﬁles for various values of nonlinear</p><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Temperature profile for various values of β</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-1100503x62.png"/></fig><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> Velocity profile for various values of n</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-1100503x63.png"/></fig><fig id="fig7"  position="float"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> Temperature profile for various values of n</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-1100503x64.png"/></fig><p>stretching parameter n. <xref ref-type="fig" rid="fig6">Figure 6</xref> shows that the velocity of the fluid decreases with an increase in power index n, while the temperature increases (<xref ref-type="fig" rid="fig7">Figure 7</xref>). From the above two figures no specific variations were observed</p><p>when n is large. This is because of the term <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x65.png" xlink:type="simple"/></inline-formula> which approximately approaches to 2 when n reaches infin-</p><p>ity, as mentioned in the subfigures. Therefore the observations for the large values of n is not a study of interest.</p><p><xref ref-type="fig" rid="fig8">Figure 8</xref> indicates the effect of magnetic parameter M on velocity and temperature profiles. The velocity of the fluid decreases with an increase in M. This causes retarding effect on the flow field leading to the prominent reduction in velocity due to Lorentz force effect. Therefore, the Lorentz force increases the opposition of the flow of fluid reducing the velocity of the flow.</p><p><xref ref-type="fig" rid="fig9">Figure 9</xref> shows the temperature profile for various values of Pr. It is clear that the dimensionless parameter θ</p><fig id="fig8"  position="float"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> Velocity profile for various values of M</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-1100503x66.png"/></fig><fig id="fig9"  position="float"><label><xref ref-type="fig" rid="fig9">Figure 9</xref></label><caption><title> Temperature profile for various values of Pr</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-1100503x67.png"/></fig><p>decreases with the increase in Prandtl number. Since the Prandtl number is the ratio of momentum diffusivity to thermal diffusivity; it reduces the thermal boundary layer thickness. In general the Prandtl number is used in heat transfer problems to reduce the relative thickening of the momentum and the thermal boundary layers.</p><p>The influence of Eckert number Ec for linearly/non linearly stretching parameters i.e., n = 1, n = 10 is depicted in <xref ref-type="fig" rid="fig1">Figure 1</xref>0. It illustrates that the temperature increases with an increase in Ec. The increase in temperature profile is higher for non linear stretching parameter than that for linear stretching parameter. The viscous dissipation produces heat due to drag between the fluid particles and this extra heat causes an increase of the initial fluid temperature, and these variations are clearly mentioned for linearly (n = 1) and nonlinearly stretching cases (n = 10). Both <xref ref-type="fig" rid="fig1">Figure 1</xref>0 and <xref ref-type="fig" rid="fig1">Figure 1</xref>1 reveal that the viscous dissipation may not only cause thermal reversal but also increase the thermal boundary layer whether <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x68.png" xlink:type="simple"/></inline-formula> or<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x68.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x69.png" xlink:type="simple"/></inline-formula>.</p><fig id="fig10"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>0</label><caption><title> Temperature profile for various values of Ec, λ = 0.2</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-1100503x70.png"/></fig><fig id="fig11"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>1</label><caption><title> Temperature profile for various values of Ec, λ = 1.5</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-1100503x71.png"/></fig><p><xref ref-type="fig" rid="fig1">Figure 1</xref>2 and <xref ref-type="fig" rid="fig1">Figure 1</xref>3 indicates the skin friction coefficient and Local Nusselt number with variations of Casson parameter β respectively. <xref ref-type="fig" rid="fig1">Figure 1</xref>2 depicts the variation of the skin-friction coefficient with β for two values of non linear stretching parameter n = 1, n = 10. It is found that as β increases the skin-friction coefﬁcient <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x72.png" xlink:type="simple"/></inline-formula> increases. From this ﬁgure, it can be observed that the shear stress at the wall is negative. Physically, a negative sign implies that a drag force has been exerted by the surface on the fluid, and a positive sign implies the opposite.</p><p><xref ref-type="fig" rid="fig1">Figure 1</xref>3 indicates the variation of heat transfer coefficient <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x73.png" xlink:type="simple"/></inline-formula> with Casson parameter β. As β increases, the heat transfer coefficient gradually increases. Wall temperature gradient <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x73.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/5-1100503x74.png" xlink:type="simple"/></inline-formula> decreases with increase in n.</p><fig id="fig12"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>2</label><caption><title> Skin friction coefficient for various values of Casson parameter β</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-1100503x75.png"/></fig><fig id="fig13"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>3</label><caption><title> Local Nusselt number for various values of Casson parameter β</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/5-1100503x76.png"/></fig></sec><sec id="s5"><title>5. Conclusion</title><p>In the present study, MHD stagnation point flow of a Casson fluid over a non linearly stretching sheet are investigated with viscous dissipation. The numerical solution is obtained by Keller box technique. The effects of various governing parameters on heat flow characteristics were analyzed. Briefly the above discussion can be summarized as follows.</p><p>・ The velocity boundary layer thickness reduces for magnetic parameter M.</p><p>・ An increase in Casson parameter β decreases the velocity of the fluid as well as the thermal boundary layer thickness.</p><p>・ The velocity of the fluid decreases and temperature increases with an increase in nonlinear stretching parameter..</p><p>・ The Eckert number increases the thermal boundary layer thickness where as the Prandtl number decreases it.</p><p>・ Both the skin friction coefficient and heat transfer coefficient increases with Casson parameter β.</p></sec><sec id="s6"><title>Cite this paper</title><p>Ojinga Gideon Omiunu,1 1,Monica Medikare,Sucharitha Joga,Kishore Kumar Chidem, (2016) MHD Stagnation Point Flow of a Casson Fluid over a Nonlinearly Stretching Sheet with Viscous Dissipation. 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