<?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">AM</journal-id><journal-title-group><journal-title>Applied Mathematics</journal-title></journal-title-group><issn pub-type="epub">2152-7385</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/am.2015.66082</article-id><article-id pub-id-type="publisher-id">AM-56788</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>
 
 
  Unsteady Hydro-Magnetic Heat and Mass Transfer Flow of a Non-Newtonian Power-Law Fluid past a Flat Plate in the Presence of Homogeneous Chemical Reaction
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>tishree</surname><given-names>Swain</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>Hadibandhu</surname><given-names>Pattanayak</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref></contrib></contrib-group><aff id="aff2"><addr-line>Department of Mathematics, Institute of Mathematics and Applications, Bhubaneswar, India</addr-line></aff><aff id="aff1"><addr-line>Department of Mathematics, Krupajal Engineering School, Bhubaneswar, India</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>h.pattnayak@gmail.com(TS)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>29</day><month>05</month><year>2015</year></pub-date><volume>06</volume><issue>06</issue><fpage>899</fpage><lpage>907</lpage><history><date date-type="received"><day>11</day>	<month>May</month>	<year>2015</year></date><date date-type="rev-recd"><day>accepted</day>	<month>26</month>	<year>May</year>	</date><date date-type="accepted"><day>29</day>	<month>May</month>	<year>2015</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>
 
 
  This paper investigates the flow, heat andmass transfer of a power law fluid from a vertical plate in presence of a magnetic field. The resulting non-linear partial differential equations governing the flow together with the boundary conditions are reduced to non-dimensional form. The governing equations are discretized using implicit finite difference scheme and solved numerically. The velocity, temperature and concentration profile are presented graphically while the skin friction, local Nusselt number and the Sherwood number are presented in tabular form for different values of parameters of the problem.
 
</p></abstract><kwd-group><kwd>Power Law Fluid</kwd><kwd> Chemical Reaction</kwd><kwd> Thermal Diffusion</kwd><kwd> Magnetic Field</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The fluids which are encountered in chemical and allied processing applications are known as non-Newtonian- fluids. The study of non-Newtonian fluid flows has considerable interest for their numerous engineering appli- cations. During the past four decades the study of non-Newtonian fluids has gained interest because of their nu- merous technological applications, including manufacturing of the plastic sheets, performance of lubricants and</p><p>movement of biological fluids. To explain the behavior of non-Newtonian fluid different models have been proposed. Among these the power law fluid has gained importance. The order of chemical reactions depends on several factors. One of the simplest chemical reactions is the first order reaction in which the rate of reaction is directly proportional to the species concentration. Now a days, due to the growing use of these non-Newtonian substances in various manufacturing and processing industries, considerable efforts have been directed towards understanding their friction and heat transfer characteristics. By the application of a magnetic field hydromagnetic techniques are used for the purification of molten metal. The problem of steady flow and heat transfer in power law fluid by free convection along a vertical plate has been investigated by many researchers. Vujanovic et al. [<xref ref-type="bibr" rid="scirp.56788-ref1">1</xref>] investigated a variational solution of the Rayleigh problem for a power law non-Newtonian conducting fluid. Padhy &amp; Pattnayak [<xref ref-type="bibr" rid="scirp.56788-ref2">2</xref>] studied the mass transfer and free convective effects of a power law fluid past an impulsively started vertical plate. Murthy [<xref ref-type="bibr" rid="scirp.56788-ref3">3</xref>] investigated effects of double dispersion on mixed convection heat and mass transfer in a non-Darcy porous medium. Muthucumaraswamy et al. [<xref ref-type="bibr" rid="scirp.56788-ref4">4</xref>] discussed on diffusion and first order chemical reaction on impulsively started infinite vertical plate with variable temperature. Naseer [<xref ref-type="bibr" rid="scirp.56788-ref5">5</xref>] investigated the problem of unsteady free convection with heat &amp; mass transfer from an isothermal vertical flat plate to a non-Newtonian power law fluid immersed in a saturated porous medium. Chamkha et al. [<xref ref-type="bibr" rid="scirp.56788-ref6">6</xref>] investigated unsteady natural convective power law fluid flow past a vertical plate embedded in a non-Darcian porous medium in the presence of a homogeneous chemical reaction. Khan et al. [<xref ref-type="bibr" rid="scirp.56788-ref7">7</xref>] discussed non-Newtonian MHD mixed convective power law fluid flow over a vertical stretching sheet with thermal radiation, heat generation and chemical reaction effects. Olajuwon et al. [<xref ref-type="bibr" rid="scirp.56788-ref8">8</xref>] studied convection heat mass transfer in a power law fluid with non-constant relaxation time past a vertical porous plate in the presence of thermo and thermal diffusion. Olajuwon [<xref ref-type="bibr" rid="scirp.56788-ref9">9</xref>] examined effects of thermo diffusion and chemical reaction on heat and mass transfer in a power law fluid over a flat plate with heat generation. Then in 2014 many researchers had shown interest to examine on the subject heat and mass transfer in a non-Newtonian fluid. Uwanta et al. [<xref ref-type="bibr" rid="scirp.56788-ref10">10</xref>] investigated heat and mass transfer flow past an infinite vertical plate with variable thermal conductivity heat source and chemical reaction. Jothimani and Vidhya [<xref ref-type="bibr" rid="scirp.56788-ref11">11</xref>] studied non-Newtonian fluid flow and heat transfer over a non-linearly stretching surface along with porous plate in porous medium. Recently Madhu et al. [<xref ref-type="bibr" rid="scirp.56788-ref12">12</xref>] studied effect of viscous dis- sipation and thermal stratification on chemical reacting fluid flow over a vertical stretching surface with heat source.</p><p>The aim of the present work is to investigate the unsteady hydro magnetic non-Newtonian power law fluid past a flat plate with heat and mass transfer effect. The governing equations, describing the model are highly nonlinear coupled partial differential equations in nature. Hence closed form solutions are not possible. Suitable implicit finite difference scheme has been used to get the solution of the problem. Graphs have been plotted against various flow parameters to study the characteristics of velocity, temperature and concentration of the fluid.</p></sec><sec id="s2"><title>2. Formulation of the Problem</title><p>There exist different types of non-Newtonian fluids but the simplest and most common type is the power-law fluid for which the rheological equation of the state between stress components and strain rate components defined by Vujanovic is</p><disp-formula id="scirp.56788-formula98"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-7402748x5.png"  xlink:type="simple"/></disp-formula><p>where, P is the pressure, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x6.png" xlink:type="simple"/></inline-formula>is the Kronecker delta, K and n are the consistency and flow behavior indices of the fluid respectively. When n &gt; 1 the fluid is described as dilatant, n &lt; 1 as pseudo-plastic and when n = 1 it is known as the Newtonian fluid.</p><p>Consider the unsteady free convection heat and mass transfer flow of a two-dimensional, viscous, incompressible, electrically conducting and chemically reactive non-Newtonian power-law fluid along an infinite non- conducting vertical flat plate in the presence of a uniform magnetic field B<sub>0</sub> applied in a transverse direction to fluid flow. Let x′-axis be along the plate in upward direction, y′-axis is normal to it &amp; z′-axis is normal to x′y′-plane. Initially, at time<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x7.png" xlink:type="simple"/></inline-formula>, the fluid and plate are at rest and at a uniform temperature<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x8.png" xlink:type="simple"/></inline-formula>. When <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x9.png" xlink:type="simple"/></inline-formula> the plate is maintained at constant temperature <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x10.png" xlink:type="simple"/></inline-formula> and constant species concentration<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x11.png" xlink:type="simple"/></inline-formula>. Since the plate is of infinite extent in x′ direction and is electrically non-conducting, except pressure all other physical quantities are functions of y′ and t′ only. The governing equations describing the model are</p><disp-formula id="scirp.56788-formula99"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-7402748x12.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.56788-formula100"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-7402748x13.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.56788-formula101"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-7402748x14.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.56788-formula102"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-7402748x15.png"  xlink:type="simple"/></disp-formula><p>where g is acceleration due to gravity, α represents the thermal diffusivity, β<sub>T</sub> is coefficient of thermal expansion of fluid, β<sub>C</sub> is volumetric coefficient of expansion or contraction, k is thermal conductivity of the fluid, ρ is fluid density, n is power law index, u′ &amp; v′ are stream wise and transverse velocity respectively.</p><p>Similarly x′ and y′ are stream wise and transverse co-ordinate. T' is temperature of the fluid and t′ is time, D is the coefficient of mass diffusivity, k<sub>c</sub> is the rate of chemical reaction, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x16.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x17.png" xlink:type="simple"/></inline-formula> are the free stream temperature and concentration of the fluid respectively, and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x18.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x19.png" xlink:type="simple"/></inline-formula> are the temperature and concentration at the wall respectively.</p><p>The initial and boundary conditions are</p><disp-formula id="scirp.56788-formula103"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-7402748x20.png"  xlink:type="simple"/></disp-formula><p>The dimensionless variables are defined as follows:</p><disp-formula id="scirp.56788-formula104"><graphic  xlink:href="http://html.scirp.org/file/1-7402748x21.png"  xlink:type="simple"/></disp-formula><p>where, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x22.png" xlink:type="simple"/></inline-formula>and l is the suitable length scale. Substituting the above non-dimensional variables into</p><p>Equations (2)-(5) yield the following dimensionless equations</p><disp-formula id="scirp.56788-formula105"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-7402748x23.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.56788-formula106"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-7402748x24.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.56788-formula107"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-7402748x25.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.56788-formula108"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-7402748x26.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x27.png" xlink:type="simple"/></inline-formula> is the Reynold number, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x28.png" xlink:type="simple"/></inline-formula>is the Grashof number, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x29.png" xlink:type="simple"/></inline-formula>is the modified Grashof number,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x30.png" xlink:type="simple"/></inline-formula> is the Prandtl number, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x31.png" xlink:type="simple"/></inline-formula>is the Schmidt number, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x32.png" xlink:type="simple"/></inline-formula>is the magnetic parameter, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x33.png" xlink:type="simple"/></inline-formula>is the chemical reaction parameter, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x33.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x34.png" xlink:type="simple"/></inline-formula>is the specific heat at constant pressure, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x33.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x34.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x35.png" xlink:type="simple"/></inline-formula>is the kinematic viscosity and &#181; is the constant viscosity of the fluid in boundary layer region.</p><p>Accordingly, the initial and boundary conditions will be reduced to</p><disp-formula id="scirp.56788-formula109"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-7402748x36.png"  xlink:type="simple"/></disp-formula><p>The special significance of this type of flow with heat and mass transfer situation are the skin-friction coefficient C<sub>f</sub>, the local Nusselt number N<sub>u</sub> and Sherwood number S<sub>h</sub>. These physical quantities are defined in non- dimensional form, respectively, as follows:</p><disp-formula id="scirp.56788-formula110"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-7402748x37.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.56788-formula111"><label>(13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-7402748x38.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.56788-formula112"><label>(14)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-7402748x39.png"  xlink:type="simple"/></disp-formula></sec><sec id="s3"><title>3. Solution of the Problem</title><p>The Equations (7)-(10) are solved by implicit finite difference method. For discretization in space and time a uniform mesh of step <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x40.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x40.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x41.png" xlink:type="simple"/></inline-formula> along x &amp; y direction respectively and time <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x40.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x41.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x42.png" xlink:type="simple"/></inline-formula> are employed so that the grid points are <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x40.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x41.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x42.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x43.png" xlink:type="simple"/></inline-formula> for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x40.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x41.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x42.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x43.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x44.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x40.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x41.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x42.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x43.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x44.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x45.png" xlink:type="simple"/></inline-formula>&amp;<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x40.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x41.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x42.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x43.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x44.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x45.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x46.png" xlink:type="simple"/></inline-formula>. The discretized form of Equation (7), (8), (9) and (10) are obtained respectively as,</p><disp-formula id="scirp.56788-formula113"><label>(15)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-7402748x47.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.56788-formula114"><label>(16)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-7402748x48.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.56788-formula115"><label>(17)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-7402748x49.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.56788-formula116"><label>(18)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-7402748x50.png"  xlink:type="simple"/></disp-formula><p>The above discretized Equations (15)-(18) are solved iteratively using the following algorithm.</p><p>Step I</p><p>Initialize <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x51.png" xlink:type="simple"/></inline-formula></p><p>Step II</p><p>For <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x52.png" xlink:type="simple"/></inline-formula></p><p>For <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x53.png" xlink:type="simple"/></inline-formula></p><p>For <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x54.png" xlink:type="simple"/></inline-formula></p><disp-formula id="scirp.56788-formula117"><graphic  xlink:href="http://html.scirp.org/file/1-7402748x55.png"  xlink:type="simple"/></disp-formula><p>Step III</p><disp-formula id="scirp.56788-formula118"><graphic  xlink:href="http://html.scirp.org/file/1-7402748x56.png"  xlink:type="simple"/></disp-formula><p>Step IV</p><disp-formula id="scirp.56788-formula119"><graphic  xlink:href="http://html.scirp.org/file/1-7402748x57.png"  xlink:type="simple"/></disp-formula><p>Step V</p><disp-formula id="scirp.56788-formula120"><graphic  xlink:href="http://html.scirp.org/file/1-7402748x58.png"  xlink:type="simple"/></disp-formula><p>The Steps (II)-(V) are repeated until the relative errors of two consecutive values of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x59.png" xlink:type="simple"/></inline-formula> are less than a given tolerance.</p></sec><sec id="s4"><title>4. Results &amp; Discussion</title><p>The non-linear governing Equations (7)-(10) with the boundary conditions (11) are solved using finite difference method. The velocity, temperature, and concentration of the fluid for different Reynold numbers are shown in Figures 1(a)-(c). The velocity, temperature and concentration decrease as R<sub>e</sub> increases.</p><p>The velocity and temperature of the fluid for different Prandtl numbers are shown in <xref ref-type="fig" rid="fig2">Figure 2</xref>(a) and <xref ref-type="fig" rid="fig2">Figure 2</xref>(b). Prandtl number increases the viscous diffusivity of the fluid at the surface which enhanced the velocity of the fluid near the surface as depicted in <xref ref-type="fig" rid="fig2">Figure 2</xref>(a), increase in P<sub>r</sub> implies flow of liquid with low thermal diffusivity and high viscous stress, which increases thermal boundary layer thickness near the surface as shown in <xref ref-type="fig" rid="fig2">Figure 2</xref>(b).</p><p>In <xref ref-type="fig" rid="fig3">Figure 3</xref>(a) and <xref ref-type="fig" rid="fig3">Figure 3</xref>(b) we have seen as chemical reaction parameter increases the velocity and species concentration decrease, but it is reverse in the case of Schmidt number. The velocity and species concentration increase as S<sub>c</sub> increases it is reflected through <xref ref-type="fig" rid="fig4">Figure 4</xref>(a) and <xref ref-type="fig" rid="fig4">Figure 4</xref>(b).</p><p>It is evident from <xref ref-type="fig" rid="fig5">Figure 5</xref> that the presence of transverse magnetic field has a retarding effect on velocity field. But from Figures 6-8 it is observed that with an increase in G<sub>r</sub>, G<sub>m</sub> or N the velocity increases.</p><p>For the physical interest in view we found the influence of power law index, magnetic parameter, Prandtl number, Reynold number, Schmidt number, chemical reaction parameter, thermal Grashof number and modified</p><fig-group id="fig1"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Variation of R<sub>e</sub> on (a) fluid velocity, (b) temperature and (c) species concentration when N = 1; G<sub>r</sub> = 5; G<sub>m</sub> = 5; M = 1; P<sub>r</sub> = 1; S<sub>c</sub> = 0.5; K<sub>r</sub> = 1.</title></caption><fig id ="fig1_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-7402748x60.png"/></fig></fig-group><fig-group id="fig2"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Variation of P<sub>r</sub> on (a) fluid velocity and (b) temperature when N = 1; G<sub>r</sub> = 5; G<sub>m</sub> = 5; M = 1; R<sub>e</sub> = 1; S<sub>c</sub> = 0.5; K<sub>r</sub> = 1.</title></caption><fig id ="fig2_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-7402748x61.png"/></fig></fig-group><fig-group id="fig3"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Variation of K<sub>r</sub> on (a) Velocity and (b) species concentration when N = 1; G<sub>r</sub> = 5; G<sub>m</sub> = 5; M = 1; R<sub>e</sub> = 1; P<sub>r</sub> = 1; S<sub>c</sub> = 2.</title></caption><fig id ="fig3_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-7402748x62.png"/></fig></fig-group><p>Grashof number on the skin friction C<sub>f</sub>, local Nusselt number N<sub>u</sub> and Sherwood number S<sub>h</sub> is shown in the <xref ref-type="table" rid="table1">Table 1</xref>. It is interesting to note that the increase in magnetic parameter decreases the velocity of the fluid that helps to reduce the skin friction at the surface, but the local heat transfer and mass transfer are not influenced by the magnetic parameter. When the fluid is dilatant the skin friction at the surface decreases, but local Nusselt number does not change. As Prandtl number increases the skin friction increases, local Nusselt number decreases but</p><fig-group id="fig4"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Variation of S<sub>c</sub> on (a) fluid velocity and (b) species concentration when N = 1; G<sub>r</sub> = 5; G<sub>m</sub> = 5; M = 1; R<sub>e</sub> = 1; P<sub>r</sub> = 1; K<sub>r</sub> = 0.4.</title></caption><fig id ="fig4_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-7402748x63.png"/></fig></fig-group><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Variation of M on velocity when N = 1; G<sub>r</sub> = 5; G<sub>m</sub> = 5; P<sub>r</sub> = 1; S<sub>c</sub> = 0.6; K<sub>r</sub> = 1</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-7402748x64.png"/></fig><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> Variation of N on velocity when G<sub>r</sub> = 5, G<sub>m</sub> = 5, M = 1, R<sub>e</sub> = 2, P<sub>r</sub> = 1, S<sub>c</sub> = 0.6, K<sub>r</sub> = 1</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-7402748x65.png"/></fig><fig id="fig7"  position="float"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> Variation of G<sub>r</sub> on velocity when N = 1, G<sub>m</sub> = 5, M = 1, R<sub>e</sub> = 1, P<sub>r</sub> = 1, S<sub>c</sub> = 0.6, K<sub>r</sub> = 0.4</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-7402748x66.png"/></fig><fig id="fig8"  position="float"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> Variation of G<sub>m</sub> on velocity when N = 1; G<sub>r</sub> = 5; M = 1; R<sub>e</sub> = 1; P<sub>r</sub> = 1; S<sub>c</sub> = 0.6; K<sub>r</sub> = 0.4</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-7402748x67.png"/></fig><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Skin friction, Nusselt number and Sherwood number</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >n</th><th align="center" valign="middle" >M</th><th align="center" valign="middle" >P<sub>r</sub></th><th align="center" valign="middle" >R<sub>e</sub></th><th align="center" valign="middle" >S<sub>c</sub></th><th align="center" valign="middle" >K<sub>r</sub></th><th align="center" valign="middle" >G<sub>r</sub></th><th align="center" valign="middle" >G<sub>m</sub></th><th align="center" valign="middle" >C<sub>f</sub></th><th align="center" valign="middle" >N<sub>u</sub></th><th align="center" valign="middle" >S<sub>h</sub></th></tr></thead><tr><td align="center" valign="middle" >1.5</td><td align="center" valign="middle"  rowspan="3"  >2</td><td align="center" valign="middle"  rowspan="3"  >1</td><td align="center" valign="middle"  rowspan="3"  >1</td><td align="center" valign="middle"  rowspan="3"  >0.6</td><td align="center" valign="middle"  rowspan="3"  >1</td><td align="center" valign="middle"  rowspan="3"  >5</td><td align="center" valign="middle"  rowspan="3"  >5</td><td align="center" valign="middle" >0.4049</td><td align="center" valign="middle" >-</td><td align="center" valign="middle" >-</td></tr><tr><td align="center" valign="middle" >2</td><td align="center" valign="middle" >0.4046</td><td align="center" valign="middle" >-</td><td align="center" valign="middle" >-</td></tr><tr><td align="center" valign="middle" >4</td><td align="center" valign="middle" >0.4029</td><td align="center" valign="middle" >-</td><td align="center" valign="middle" >-</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle" >4</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle" >0.3692</td><td align="center" valign="middle" >-</td><td align="center" valign="middle" >-</td></tr><tr><td align="center" valign="middle" >8</td><td align="center" valign="middle" >0.3222</td><td align="center" valign="middle" >-</td><td align="center" valign="middle" >-</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle" >2</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle" >0.5662</td><td align="center" valign="middle" >3.8563</td><td align="center" valign="middle" >-</td></tr><tr><td align="center" valign="middle" >4</td><td align="center" valign="middle" >0.7651</td><td align="center" valign="middle" >2.7748</td><td align="center" valign="middle" >-</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle" >3</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle" >0.1658</td><td align="center" valign="middle" >7.5284</td><td align="center" valign="middle" >8.9185</td></tr><tr><td align="center" valign="middle" >6</td><td align="center" valign="middle" >0.0868</td><td align="center" valign="middle" >8.5764</td><td align="center" valign="middle" >9.4168</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle" >1.0</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle" >0.4709</td><td align="center" valign="middle" >-</td><td align="center" valign="middle" >6.6021</td></tr><tr><td align="center" valign="middle" >1.5</td><td align="center" valign="middle" >0.5386</td><td align="center" valign="middle" >-</td><td align="center" valign="middle" >5.8548</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle" >2</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle" >0.3659</td><td align="center" valign="middle" >-</td><td align="center" valign="middle" >8.1591</td></tr><tr><td align="center" valign="middle" >3</td><td align="center" valign="middle" >0.3425</td><td align="center" valign="middle" >-</td><td align="center" valign="middle" >8.5691</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle" >10</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle" >0.7066</td><td align="center" valign="middle" >5.2366</td><td align="center" valign="middle" >-</td></tr><tr><td align="center" valign="middle" >15</td><td align="center" valign="middle" >1.0146</td><td align="center" valign="middle" >5.2366</td><td align="center" valign="middle" >-</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >-</td><td align="center" valign="middle"  rowspan="2"  >5</td><td align="center" valign="middle" >10</td><td align="center" valign="middle" >0.5428</td><td align="center" valign="middle" >-</td><td align="center" valign="middle" >7.4954</td></tr><tr><td align="center" valign="middle" >20</td><td align="center" valign="middle" >0.8224</td><td align="center" valign="middle" >-</td><td align="center" valign="middle" >7.4954</td></tr></tbody></table></table-wrap><p>C<sub>f</sub> = Skin Friction :<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x68.png" xlink:type="simple"/></inline-formula>; N<sub>u</sub> = Local Nusselt Number:<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x68.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x69.png" xlink:type="simple"/></inline-formula>; S<sub>h</sub> = Local Nusselt Number:<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x68.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x69.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-7402748x70.png" xlink:type="simple"/></inline-formula>.</p><p>concentration does not change with it. It is evident from the table that with an increase in R<sub>e</sub> the skin friction decreases while a reverse effect is seen in case of Nusselt number N<sub>u</sub> and Sherwood number S<sub>h</sub> is very much affected by Reynold number.</p></sec><sec id="s5"><title>5. Conclusions</title><p>Unsteady free convective heat and mass transfer in the flow of a two dimensional viscous incompressible electrically conducting and chemically reactive non-Newtonian power-law fluid along an infinite non-conducting vertical flat plate in the presence of uniform magnetic field are studied. It is found that,</p><p>・ With an increase in R<sub>e</sub> velocity, temperature &amp; concentration of the fluid decrease.</p><p>・ With the increasing value of chemical reaction parameter fluid velocity &amp; concentration decrease near the plate, but the species concentration shows reverse characteristics as depicted in the skin friction table.</p><p>・ Magnetic field has a retarding effect on the fluid flow while the thermal radiation has a reverse effect on it.</p><p>The solutions obtained are well agreed with the Newtonian case and they give improved results, taking into consideration of the behaviour of the magnetic field. This method well suits for other non-Newtonian fluid flow problems.</p></sec></body><back><ref-list><title>References</title><ref id="scirp.56788-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Vujanovic, B., Stauss, A.M. and Djukic, D. J. 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