<?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">JAMP</journal-id><journal-title-group><journal-title>Journal of Applied Mathematics and Physics</journal-title></journal-title-group><issn pub-type="epub">2327-4352</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/jamp.2016.42038</article-id><article-id pub-id-type="publisher-id">JAMP-63797</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>
 
 
  Effect of Nonlinear Thermal Radiation on Boundary Layer Flow of Viscous Fluid over Nonlinear Stretching Sheet with Injection/Suction
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>.</surname><given-names>Vijaya Laxmi</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Bandari</surname><given-names>Shankar</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><aff id="aff2"><addr-line>Department of Mathematics, Osmania University, Hyderabad, India</addr-line></aff><aff id="aff1"><addr-line>Department of Mathematics, M.V.S. Govt. Arts &amp;amp; Science College, Mahabubnagar, India</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>vijaya9966998024@rediffmail.com(.VL)</email>;<email>bandarishankar@gmail.co.in(BS)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>17</day><month>02</month><year>2016</year></pub-date><volume>04</volume><issue>02</issue><fpage>307</fpage><lpage>319</lpage><history><date date-type="received"><day>7</day>	<month>January</month>	<year>2016</year></date><date date-type="rev-recd"><day>accepted</day>	<month>22</month>	<year>February</year>	</date><date date-type="accepted"><day>25</day>	<month>February</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>
 
 
  The present study reveals the effect of nonlinear thermal radiation and magnetic field on a boundary layer flow of a viscous fluid over a nonlinear stretching sheet with suction or an injection. Using suitable similarity transformations, governing partial differential equations were reduced to higher order ordinary differential equations and further these are solved numerically using of Keller-Box method. Effect of flow controlling parameter on velocity, temperature and nanoparticle fluid concentration, local skin friction coefficient, local Nusselt number and local Sherwood numbers are discussed. It is found that the dimensionless velocity decreases and temperature, concentration are increased with the increasing of magnetic parameter. The temperature profile is an increasing function of thermal radiation when it is increasing.
 
</p></abstract><kwd-group><kwd>Nonlinear Thermal Radiation</kwd><kwd> Stretching Sheet</kwd><kwd> Boundary Layer</kwd><kwd> Keller-Box Method</kwd><kwd> Suction/Injection</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Boundary layer behaviour with the heat and mass transfer over a nonlinear stretching sheet in the presence of thermal radiation is very important for various engineering and industrial applications. These applications involve the cooling of continuous strips or filaments by drawing them through a quiescent fluid. Flow past a stretching surface with different stretching velocity has been addressed previously. Grubka et al. [<xref ref-type="bibr" rid="scirp.63797-ref1">1</xref>] studied the effect of heat transfer characteristics of a boundary layer flow of fluids flow over a linear continuous stretching surface. Chen et al. [<xref ref-type="bibr" rid="scirp.63797-ref2">2</xref>] studied the heat transfer effect of a boundary layer flow over a linear stretching sheet which was subjected to suction/blowing in the present of the sheet with prescribed wall temperature and heat flux. Kumaran and his group [<xref ref-type="bibr" rid="scirp.63797-ref3">3</xref>] examined the transition effect of boundary layer flow due to a presence and an absence of magnetic field over a viscous flow past a stretching sheet and analyzed the task numerically by implicit finite difference technique (Crank-Nicholson method). Bakar et al. [<xref ref-type="bibr" rid="scirp.63797-ref4">4</xref>] investigated the steady laminar flow over a stretching sheet with a convective boundary condition by the considering of the effect of partial slip. Krishnamurthy et al. [<xref ref-type="bibr" rid="scirp.63797-ref5">5</xref>] investigated the effect of viscous dissipation on hydromagnetic fluid flow and heat transfer of nanofluid over an exponentially stretching sheet with fluid-particle suspension. However, studies on heat and mass, transfer in the laminar boundary layer flow over a non-linear stretching sheet is very less. It is well known to the all research community that the stretching is not necessarily linear in many industrial applications. Many authors analysed flow, heat and mass transfer transport of both Netonian and non-Newtonian fluid over nonlinear stretching surfaces. Rana and Bhargava [<xref ref-type="bibr" rid="scirp.63797-ref6">6</xref>] numerically investigated, steady, laminar boundary fluid flow which results from the non-linear stretching of a flat surface in a nanofluid. Khan et al. [<xref ref-type="bibr" rid="scirp.63797-ref7">7</xref>] studied three-dimensional flow of nanofluid over an elastic sheet stretched non-linearly in two lateral directions and the results of their study reveal that penetration depths of temperature and nanoparticle volume fraction are decreasing functions of the power-law index. Pal and Mandal [<xref ref-type="bibr" rid="scirp.63797-ref8">8</xref>] obtained numerical solution by fifth-order Runge-Kutta-Fehlberg method with shooting technique for magnetohydrodynamic boundary layer flow of an electrically conducting convective nanofluids induced by a non-linear vertical stretching/shrinking sheet with viscous dissipation, thermal radiation, and Ohmic heating. Mabood et al. [<xref ref-type="bibr" rid="scirp.63797-ref9">9</xref>] obtained numerical results for MHD laminar boundary layer flow with heat and mass transfer of an electrically conducting water-based nanofluid over a nonlinear stretching sheet with viscous dissipation effect. Das [<xref ref-type="bibr" rid="scirp.63797-ref10">10</xref>] performed a numerical investigation, to study the problem of boundary layer flow of a nanofluid over non-linear permeable stretching sheet at prescribed surface temperature in the presence of partial slip.</p><p>Heat transfer, influenced by thermal radiation has applications in many technological processes, including nuclear power plants, gas turbines and the various propulsion devices for aircraft, missiles, satellites and space vehicles. But a linear radiation is not valid for high temperature difference and also dimensionless parameter that is used in the linearized Rosseland approximation is only the effective Prandtl number [<xref ref-type="bibr" rid="scirp.63797-ref11">11</xref>] , Pntokratoras [<xref ref-type="bibr" rid="scirp.63797-ref12">12</xref>] investigated the effect of linear or non-linear Rosseland radiation on steady laminar natural convection along a vertical isothermal plate by using a new radiation parameter called film radiation parameter. Hayat et al. [<xref ref-type="bibr" rid="scirp.63797-ref13">13</xref>] analysed the effect of nonlinear thermal radiation and constant applied magnetic field on magnetohydrodynamic three-dimensional flow of couple stress nanofluid and viscous nanofluid in the presence of thermophoresis and Brownian motion effects. Shehzad et al. [<xref ref-type="bibr" rid="scirp.63797-ref14">14</xref>] have explored the characteristics of thermophoresis and Brownian motion in magnetohydrodynamic three-dimensional flow of nano Jeffrey fluid in the presence of nonlinear thermal radiation.</p><p>Another important aspect, which influences heat transfer processes is effects of injection or suction. It is well- known that the effects of injection on the boundary layer flow are of interest in reducing the drag force. Many of the authors have studied heat transfer by considering an uniform and non-uniform heat source/sink effects, which are crucial in controlling the heat transfer. Jalilpour et al. [<xref ref-type="bibr" rid="scirp.63797-ref15">15</xref>] presented a theoretical study to analyze the effect of heat generation/absorption on magnetohydrodynamic stagnation point flow and heat transfer over a porous stretching surface, with prescribed surface heat flux. Cao et al. [<xref ref-type="bibr" rid="scirp.63797-ref16">16</xref>] have investigated the magnetohydrodynamic (MHD) Maxwell fluid past a stretching plate with suction/injection in the presence of nanoparticles. By considering investigates steady laminar boundary layer flow of power law fluids past a flat surface with suction or injection and magnetic effects Lin et al. [<xref ref-type="bibr" rid="scirp.63797-ref17">17</xref>] investigates steady laminar boundary layer flow of power law fluids past a flat surface with suction or injection and magnetic effects.</p><p>The main aim of the present paper is to solve the problem of magnetohydrodynamics (MHD) studies on boundary layer flow over nonlinear stretching sheet with injection/suction and nonlinear thermal radiation of a viscous fluid by adopting the well known Keller-Box method. I have verified the obtained numerical results with earlier work and a very good agreement has been established.</p></sec><sec id="s2"><title>2. Formulation of the Problem</title><p>Consider a two dimensional steady laminar boundary layer flow over a permeable nonlinear stretching sheet in the presence of applied magnetic in an incompressible viscous fluid. Presume sheet direction is horizontal with the x-axis and y-axis is the direction normal to the stretching sheet. Present flow is restricted to <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x7.png" xlink:type="simple"/></inline-formula> and is due to the simultaneous effect of two equal and opposite forces along the direction of the x-axis and maintained the origin is fixed. The sheet coincides with the plane <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x8.png" xlink:type="simple"/></inline-formula> and its velocity is assumed as <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x9.png" xlink:type="simple"/></inline-formula> , where “a” and “n” are positive constant values. The flow configuration is given in <xref ref-type="fig" rid="fig1">Figure 1</xref>. The boundary layer equations, under the Boussinesq approximations and for steady state flow conditions are given by:</p><disp-formula id="scirp.63797-formula1788"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1720485x10.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.63797-formula1789"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1720485x11.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.63797-formula1790"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1720485x12.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.63797-formula1791"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1720485x13.png"  xlink:type="simple"/></disp-formula><p>We assume that the variable magnetic field <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x14.png" xlink:type="simple"/></inline-formula> and is of the form <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x15.png" xlink:type="simple"/></inline-formula> [<xref ref-type="bibr" rid="scirp.63797-ref18">18</xref>] -[<xref ref-type="bibr" rid="scirp.63797-ref20">20</xref>] . The boundary conditions for velocity, temperature and concentration are considered are</p><disp-formula id="scirp.63797-formula1792"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1720485x16.png"  xlink:type="simple"/></disp-formula><p>Unlike the linearized Rosseland approximation, we use nonlinear Rosseland diffusion approximation from which one can obtain results for both small and large differences between <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x17.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x18.png" xlink:type="simple"/></inline-formula> .</p><p>Using Rosseland (Rosseland, 1931) approximation for radiation, the radiative heat flux is simplified as,</p><disp-formula id="scirp.63797-formula1793"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1720485x19.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x20.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x21.png" xlink:type="simple"/></inline-formula> are the Stefan-Boltzmann constant and mean absorption coefficient respectively and where T is the temperature across the boundary layer.</p><p>For a boundary layer flow over a horizontal flat plate, from Equation (2.6) we get,</p><disp-formula id="scirp.63797-formula1794"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1720485x22.png"  xlink:type="simple"/></disp-formula><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Flow organization with coordinate system</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1720485x23.png"/></fig><p>In view to Equation (6), energy Equation (3) takes the form</p><disp-formula id="scirp.63797-formula1795"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1720485x24.png"  xlink:type="simple"/></disp-formula><p>where<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x25.png" xlink:type="simple"/></inline-formula>, k being the thermal conductivity.</p><p>The following shifts are used to transform the governing partial differential equations into a scheme of ordinary differential equations.</p><disp-formula id="scirp.63797-formula1796"><graphic  xlink:href="http://html.scirp.org/file/9-1720485x26.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.63797-formula1797"><graphic  xlink:href="http://html.scirp.org/file/9-1720485x27.png"  xlink:type="simple"/></disp-formula><p>where<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x28.png" xlink:type="simple"/></inline-formula>, the temperature ratio parameter.</p><p>The similarity variable <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x29.png" xlink:type="simple"/></inline-formula> and dimensionless stream function <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x30.png" xlink:type="simple"/></inline-formula> satisfy the continuity equation. With the similarity variable <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x31.png" xlink:type="simple"/></inline-formula> , the Equations (2), (4) and (8) reduces to the following ordinary differential equations, respectively</p><disp-formula id="scirp.63797-formula1798"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1720485x32.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.63797-formula1799"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1720485x33.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.63797-formula1800"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1720485x34.png"  xlink:type="simple"/></disp-formula><p>Using the similarity transformation and the boundary conditions which are mentioned in equation (5), the transformed boundary conditions are;</p><disp-formula id="scirp.63797-formula1801"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1720485x35.png"  xlink:type="simple"/></disp-formula><p>Here <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x36.png" xlink:type="simple"/></inline-formula> is the suction/injection parameter and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x36.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x37.png" xlink:type="simple"/></inline-formula> belongs to injection, suction and impermeability cases respectively. Magnetic parameter of<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x36.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x37.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x38.png" xlink:type="simple"/></inline-formula>. The physical quantities of importance from the engineering point of observation are the skin friction coefficient, the local Nusselt number <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x36.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x37.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x38.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x39.png" xlink:type="simple"/></inline-formula> and the local Sherwood number <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x36.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x37.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x38.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x39.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x40.png" xlink:type="simple"/></inline-formula> which are defined as</p><disp-formula id="scirp.63797-formula1802"><label>(13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1720485x41.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.63797-formula1803"><label>(14)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1720485x42.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.63797-formula1804"><label>(15)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1720485x43.png"  xlink:type="simple"/></disp-formula><p>Here the wall heat flux <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x44.png" xlink:type="simple"/></inline-formula> <sub></sub>and the mass flux <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x44.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x45.png" xlink:type="simple"/></inline-formula> <sub></sub>are given as:</p><disp-formula id="scirp.63797-formula1805"><graphic  xlink:href="http://html.scirp.org/file/9-1720485x46.png"  xlink:type="simple"/></disp-formula><p>Using of similarity variable, the Equations (13), (14) and (15) becomes:</p><disp-formula id="scirp.63797-formula1806"><label>(16)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1720485x47.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.63797-formula1807"><label>(17)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1720485x48.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.63797-formula1808"><label>(18)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/9-1720485x49.png"  xlink:type="simple"/></disp-formula><p>Here <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x50.png" xlink:type="simple"/></inline-formula> is the Reynolds number.</p></sec><sec id="s3"><title>3. Numerical Procedure</title><p>The ordinary differential Equations (9), (10), (11) with the boundary conditions (12) are solved numerically by using of Keller-Box method with MATLAB, as revealed by (19), the following few steps are involved to achieve Numerical solutions:</p><p> Reduce the above mentioned higher order ordinary differential equations into a system of first order ordinary differential equations;</p><p> Write the finite differences for the first order equations.</p><p> Linearize the algebraic equations by Newton’s method, and write them in matrix-vector form; and</p><p> Solve the linear system by the block tri-diagonal elimination technique.</p><p> To get the accuracy of this method the appropriate initial guesses have been chosen. The following initial guesses are chosen.</p><p> <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x51.png" xlink:type="simple"/></inline-formula></p></sec><sec id="s4"><title>4. Results and Discussion</title><p>To have a check on the accuracy of the numerical procedure used, first test computations for <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x52.png" xlink:type="simple"/></inline-formula> are carried out for viscous fluid for various values of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x52.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x53.png" xlink:type="simple"/></inline-formula> and compared with the available published results of Goyal and Bhargava (2014), Gorla and Sidawi (1994) and Nadeem and Hussain (2013) in <xref ref-type="table" rid="table1">Table 1</xref> and they are found to be in excellent agreement. The parameters for the present study are magnetic parameter M , Prandtl number (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x52.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x53.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x54.png" xlink:type="simple"/></inline-formula>) , Schmidt number (S<sub>c</sub>), suction/injection parameter s radiation parameter (Rd) , and the nonlinear stretching sheet parameter (h).</p><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Comparison table for viscous case <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x55.png" xlink:type="simple"/></inline-formula> for <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x55.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x56.png" xlink:type="simple"/></inline-formula> </title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Pr</th><th align="center" valign="middle" >Nadeem and Hussain (HAM method) (2013)</th><th align="center" valign="middle" >Gorla and Sidawi (1994)</th><th align="center" valign="middle" >Goyal and Bhargava (FEM Method) (2014)</th><th align="center" valign="middle" >Present (RKF45 Method)</th></tr></thead><tr><td align="center" valign="middle" >0.2</td><td align="center" valign="middle" >0.169</td><td align="center" valign="middle" >0.1691</td><td align="center" valign="middle" >0.1691</td><td align="center" valign="middle" >0.170259788</td></tr><tr><td align="center" valign="middle" >0.7</td><td align="center" valign="middle" >0.454</td><td align="center" valign="middle" >0.5349</td><td align="center" valign="middle" >0.4539</td><td align="center" valign="middle" >0.454447258</td></tr><tr><td align="center" valign="middle" >2</td><td align="center" valign="middle" >0.911</td><td align="center" valign="middle" >0.9114</td><td align="center" valign="middle" >0.9113</td><td align="center" valign="middle" >0.911352755</td></tr><tr><td align="center" valign="middle" >7</td><td align="center" valign="middle" ></td><td align="center" valign="middle" >1.8905</td><td align="center" valign="middle" >1.8954</td><td align="center" valign="middle" >1.895400395</td></tr><tr><td align="center" valign="middle" >20</td><td align="center" valign="middle" ></td><td align="center" valign="middle" >3.3539</td><td align="center" valign="middle" >3.3539</td><td align="center" valign="middle" >3.353901838</td></tr></tbody></table></table-wrap><p>A parametric study is carried out to demonstrate the effects of governing parameters on velocity, temperature and concentration profiles. <xref ref-type="fig" rid="fig2">Figure 2</xref> and <xref ref-type="fig" rid="fig3">Figure 3</xref> illustrate the effect of magnetic and nonlinear stretching parameters on the dimensionless velocity. It is evidently observed that the velocity profile of the viscous fluid is insignificantly reduced with increasing values of M and h . The velocity is reduced strongly as the results of increased magnetic field, and is due to the fact that the magnetic field commences a retarding body force which will acts transverse to the direction of the functional magnetic field, and is well known as Lorentz force, which will decelerate the boundary layer flow and the thickness of the momentum boundary layer. Hence, this will encourage an increase of the velocity gradient at its surface as clearly expressed in figures.</p><p>Impact of Prandtl number on the temperature profile is given in <xref ref-type="fig" rid="fig4">Figure 4</xref>, and it indicates that increasing the Prandtl number decrease the temperature profile. A similar conclusion can be drawn to the effect of Schmidt</p><p>number <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x57.png" xlink:type="simple"/></inline-formula> on the species concentration in the presence of magnetic field as it is indicated in the <xref ref-type="fig" rid="fig5">Figure 5</xref>. <xref ref-type="fig" rid="fig6">Figure 6</xref> and <xref ref-type="fig" rid="fig7">Figure 7</xref> respectively shows the effect of thermal radiation parameter (Rd) and temperature ratio</p><p>parameter <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x58.png" xlink:type="simple"/></inline-formula> on temperature profiles. It is observed that, the temperature profile increases for increasing values of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x58.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x59.png" xlink:type="simple"/></inline-formula> . Further it shows that, the temperature profiles increase with increase in Rd. This is because, in-</p><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Effect of M on velocity profile</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1720485x60.png"/></fig><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Effect of stretching sheet parameter h on velocity profile</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1720485x61.png"/></fig><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Effect of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x63.png" xlink:type="simple"/></inline-formula> on temperature profile</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1720485x62.png"/></fig><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Effect of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x65.png" xlink:type="simple"/></inline-formula> on concentration profile</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1720485x64.png"/></fig><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> Effect of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x67.png" xlink:type="simple"/></inline-formula> on temperature profile</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1720485x66.png"/></fig><fig id="fig7"  position="float"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> Effect of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x69.png" xlink:type="simple"/></inline-formula> on temperature profile</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1720485x68.png"/></fig><p>crease in the radiation parameter provides more heat to fluid that cause an enhancement in the temperature and thermal boundary layer thickness. Figures 8-10 depicts the effect the suction/injection parameter s on velocity, temperature and concentration profiles, respectively. These plots shows that velocity decreases significantly with increasing suction parameter whereas fluid velocity is found to increase with injection and temperature decreases with increasing suction parameter whereas it increases due to blowing.</p><p>Now, we focus on the variations of quantities of the physical interest from an engineering point of view. That is, local skin friction<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x70.png" xlink:type="simple"/></inline-formula>, the local Nusselt number <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x70.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x71.png" xlink:type="simple"/></inline-formula> and the local Sherwood number<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x70.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x71.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x72.png" xlink:type="simple"/></inline-formula>. Figure</p><p>11 indicates of that for the larger values of magnetic parameter M, the skin friction coefficient shows the increasing behaviour correspond to the raise in the values of nonlinear stretching parameter h. This means fluid motion on the wall of the sheet is accelerated when we strengthen the effect of parameters.</p><p><xref ref-type="fig" rid="fig1">Figure 1</xref>2 depicts the variation of heat transfer rate with the magnetic field at different Prandtl number. It is experimental that the Nusselt numbers decrease with the increase in magnetic parameter and Prandtl number values. <xref ref-type="fig" rid="fig1">Figure 1</xref>3 and <xref ref-type="fig" rid="fig1">Figure 1</xref>4 illustrates the effect of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x73.png" xlink:type="simple"/></inline-formula> and Rd on coefficient of local Nusselt number. It is observed that heat transfer rate decreases with <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x73.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x74.png" xlink:type="simple"/></inline-formula> and Rd but increases with<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x73.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x74.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x75.png" xlink:type="simple"/></inline-formula>.</p><p>The numerical values of skin friction, Nusselt number and Sherwood number for various flow controlling parameters are tabulated in <xref ref-type="table" rid="table2">Table 2</xref>. It clear from the <xref ref-type="table" rid="table2">Table 2</xref>, that the Nusselt number and Sherwood numbers are decreases and Skin friction coefficient is increases for increasing values of M. We can also observe that in the case of suction the skin friction, Nusselt number and Sherwood number are higher than that in the case of injection.</p></sec><sec id="s5"><title>5. Conclusions</title><p>MHD boundary layer and heat transfer of a viscous fluid over a nonlinear stretching sheet in the presence of nonlinear thermal radiation with suction/injection have been studied in the current paper. A similarity solution is presented to analyse the effect of Prandtl number, magnetic parameter, nonlinearlity of stretching sheet and nonlinear thermal radiation, Schmidt number, and suction/injection parameters on velocity, temperature and concentration profiles. The effects of skin friction coefficient and surface heat and mass transfer characteristics are discussed graphically and also numerically. The main observations of the present study are as follows:</p><p> The velocity profile of the viscous fluid is insignificantly reduced with increasing values of magnetic and nonlinearity parameters.</p><p> Rising of Prandtl number resulted in decreases the temperature of the fluid.</p><p> As Schmidt number increases the species concentration decreases.</p><p> Increasing the suction/injection parameter reduces the velocity profiles.</p><p> Increase of nonlinear stretching sheet parameter, magnetic field results in diminishing of skin friction coefficient.</p><fig id="fig8"  position="float"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> Effect of suction/injection parameter s on velocity profile</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1720485x76.png"/></fig><fig id="fig9"  position="float"><label><xref ref-type="fig" rid="fig9">Figure 9</xref></label><caption><title> Effect of suction/injection parameter s on temperature profile</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1720485x77.png"/></fig><fig id="fig10"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>0</label><caption><title> Effect of suction/injection parameters on concentration profile</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1720485x78.png"/></fig><fig id="fig11"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>1</label><caption><title> Effect of M and n on skin friction coefficient</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1720485x79.png"/></fig><fig id="fig12"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>2</label><caption><title> Variation of heat transfer rate with M and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x81.png" xlink:type="simple"/></inline-formula></title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1720485x80.png"/></fig><fig id="fig13"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>3</label><caption><title> Variation of heat transfer rate with n and Rd</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1720485x82.png"/></fig><fig id="fig14"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>4</label><caption><title> Variation of heat transfer rate with <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x84.png" xlink:type="simple"/></inline-formula> and Rd</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/9-1720485x83.png"/></fig><table-wrap id="table2" ><label><xref ref-type="table" rid="table2">Table 2</xref></label><caption><title> Values of skin friction coefficient, Nusselt number and Sherwood number for different values of parameters when<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x85.png" xlink:type="simple"/></inline-formula></title></caption><table><tbody><thead><tr><th align="center" valign="middle" >M</th><th align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x86.png" xlink:type="simple"/></inline-formula></th><th align="center" valign="middle" >s</th><th align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x87.png" xlink:type="simple"/></inline-formula></th><th align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x88.png" xlink:type="simple"/></inline-formula></th><th align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x89.png" xlink:type="simple"/></inline-formula></th></tr></thead><tr><td align="center" valign="middle" >1</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" >8.828382</td><td align="center" valign="middle" >16.89666</td><td align="center" valign="middle" >11.30631</td></tr><tr><td align="center" valign="middle" >2</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" >9.382812</td><td align="center" valign="middle" >16.84966</td><td align="center" valign="middle" >11.30162</td></tr><tr><td align="center" valign="middle" >3</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" >9.887555</td><td align="center" valign="middle" >16.80994</td><td align="center" valign="middle" >11.29749</td></tr><tr><td align="center" valign="middle" >3</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" ></td><td align="center" valign="middle" >8.00</td><td align="center" valign="middle" >13.72852</td><td align="center" valign="middle" >9.224813</td></tr><tr><td align="center" valign="middle" ></td><td align="center" valign="middle" >2</td><td align="center" valign="middle" ></td><td align="center" valign="middle" >9.887555</td><td align="center" valign="middle" >7.318164</td><td align="center" valign="middle" >11.29749</td></tr><tr><td align="center" valign="middle" ></td><td align="center" valign="middle" >3</td><td align="center" valign="middle" ></td><td align="center" valign="middle" >11.46847</td><td align="center" valign="middle" >19.40817</td><td align="center" valign="middle" >13.0449</td></tr><tr><td align="center" valign="middle" ></td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >8.030919</td><td align="center" valign="middle" >10.26802</td><td align="center" valign="middle" >7.726226</td></tr><tr><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" >3</td><td align="center" valign="middle" >9.887555</td><td align="center" valign="middle" >16.80994</td><td align="center" valign="middle" >11.29749</td></tr><tr><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" >4</td><td align="center" valign="middle" >11.90432</td><td align="center" valign="middle" >23.54166</td><td align="center" valign="middle" >14.91149</td></tr></tbody></table></table-wrap></sec><sec id="s6"><title>Acknowledgements</title><p>The author T. Vijayalaxmi grateful to University Grants Commission (UGC), India for awarding Faculty Development Programme (FDP) and also thankful to CCE, Govt. of Telangana State and Principal, M.V.S. Govt. Arts &amp; Science College, Mahabubnagar, Telangana State.</p></sec><sec id="s7"><title>Cite this paper</title><p>T. VijayaLaxmi,BandariShankar, (2016) Effect of Nonlinear Thermal Radiation on Boundary Layer Flow of Viscous Fluid over Nonlinear Stretching Sheet with Injection/Suction. Journal of Applied Mathematics and Physics,04,307-319. doi: 10.4236/jamp.2016.42038</p></sec><sec id="s8"><title>Nomenclature</title><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x90.png" xlink:type="simple"/></inline-formula> -Velocity components along x, y axis.</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x91.png" xlink:type="simple"/></inline-formula> -Kinematic viscosity</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x92.png" xlink:type="simple"/></inline-formula> -Density of the fluid</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x93.png" xlink:type="simple"/></inline-formula> -Electrical conductivity of the fluid</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x94.png" xlink:type="simple"/></inline-formula> -Nanofluid temperature</p><p><sub><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x95.png" xlink:type="simple"/></inline-formula> </sub>-Ambient temperature as y tends to infinity</p><p><sub><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x96.png" xlink:type="simple"/></inline-formula> </sub>-Temperature at stretching surface</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x97.png" xlink:type="simple"/></inline-formula> -Concentration</p><p><sub><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x98.png" xlink:type="simple"/></inline-formula> </sub>-Concentration at stretching surface</p><p><sub><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x99.png" xlink:type="simple"/></inline-formula> </sub>-Ambient concentration as y tends to infinity</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x100.png" xlink:type="simple"/></inline-formula> -Skin friction coefficient</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x101.png" xlink:type="simple"/></inline-formula> -Prandtl number</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x102.png" xlink:type="simple"/></inline-formula> -Schmidt number</p><p><sub><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x103.png" xlink:type="simple"/></inline-formula> </sub>-Local Nusselt number</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x104.png" xlink:type="simple"/></inline-formula> -Local Sherwood number</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x105.png" xlink:type="simple"/></inline-formula> -Suction/injection parameter</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x106.png" xlink:type="simple"/></inline-formula> -Thermal radiation parameter</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x107.png" xlink:type="simple"/></inline-formula> -Non-linear stretching parameter</p><p><sub><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x108.png" xlink:type="simple"/></inline-formula> </sub>-Radiative heat flux</p><p><sub><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x109.png" xlink:type="simple"/></inline-formula> </sub>-Specific heat at constant pressure</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x110.png" xlink:type="simple"/></inline-formula> -Mass diffusivity</p><p><sub><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x111.png" xlink:type="simple"/></inline-formula> </sub>-Surface velocity</p><p><sub><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x112.png" xlink:type="simple"/></inline-formula> </sub>-Induced magnetic field</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x113.png" xlink:type="simple"/></inline-formula> -Magnetic parameter</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/9-1720485x114.png" xlink:type="simple"/></inline-formula> -Dimensionless concentration</p></sec><sec id="s9"><title>NOTES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.63797-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Grubka, L.G. and Bobba, K.M. 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