<?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">WJM</journal-id><journal-title-group><journal-title>World Journal of Mechanics</journal-title></journal-title-group><issn pub-type="epub">2160-049X</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/wjm.2016.611032</article-id><article-id pub-id-type="publisher-id">WJM-72001</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Engineering</subject><subject> Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  Characteristics of Nanofluids over a Non-Linearly Stretched Sheet under the Influence of Thermal Radiation and Magnetic Field
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Shiva</surname><given-names>Prasad Rayapole</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>Anand</surname><given-names>Rao Jakkula</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Department of Mathematics, Osmania University, Hyderabad, India</addr-line></aff><pub-date pub-type="epub"><day>25</day><month>10</month><year>2016</year></pub-date><volume>06</volume><issue>11</issue><fpage>456</fpage><lpage>471</lpage><history><date date-type="received"><day>October</day>	<month>5,</month>	<year>2016</year></date><date date-type="rev-recd"><day>Accepted:</day>	<month>November</month>	<year>12,</year>	</date><date date-type="accepted"><day>November</day>	<month>15,</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>
 
 
  Recent studies carried out in terms of viscous flow and heat transfer of nano-fluids on the non-linear sheets. In this paper, detailed studies to understand the characteristics such as viscous flow and heat transfer of nano-fluids under the influence of thermal radiation and magnetic fields are studied using Keller-Box method. Various governing parameters affecting the viscous flow and heat transfers are drawn based on quantitative results. The raise in temperature affected the velocity to a negative value; however, the same observation was made even for the increasing magnetic field. The impact of radiation parameter is proportional seems to be proportional to temperature and it is observed to be inversely proportional with concentration.
 
</p></abstract><kwd-group><kwd>Nano-Fluids</kwd><kwd> Thermal Radiation</kwd><kwd> Magnetic Field</kwd><kwd> Keller-Box</kwd><kwd> Viscous Flow</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>A nanofluid is a fluid which contains nanometer sized solid particles. Nanometer-size solid particles have unique chemical and physical properties. Since suspending nanometer-size particles to the conventional heat transfer fluids lead a better heat transfer, nanofluids are proposed to be employed in several applications such as transportation, nuclear reactors and electronics [<xref ref-type="bibr" rid="scirp.72001-ref1">1</xref>] .</p><p>Many engineering processing applications use the characteristics obtained by the flow studies over stretched surfaces includes extrusion, hot rolling, etc. For example, polymer sheets and filaments, in general use continuous extrusion of polymer form a die to the windup roller that is almost placed at a finite distance. The velocity in stretched surfaces almost differs from the plain surfaces and it will be proportional to the distance from orifice [<xref ref-type="bibr" rid="scirp.72001-ref2">2</xref>] . In a recent research conducted by various authors revealed that the mass and heat transfer in stretched and constant surfaces differs in various aspects [<xref ref-type="bibr" rid="scirp.72001-ref3">3</xref>] . Stretching problem on a permeable wall with incompressible fluid is studied by Magyari and Keller [<xref ref-type="bibr" rid="scirp.72001-ref4">4</xref>] . However, Vajravelu also studied the effect of flow and heat transfers in viscous fluids on a nonlinear stretched sheet under the absence of viscous dissipation [<xref ref-type="bibr" rid="scirp.72001-ref5">5</xref>] . All the above study cases are limited to linear stretching of sheets and nonlinear sheet stretching is not considered. However, the above authors highlighted exponential and nonlinear stretching. On the other side, a study on heat transfer characteristics of viscoelastic and viscous fluids on exponential stretched sheets are studied by various authors [<xref ref-type="bibr" rid="scirp.72001-ref6">6</xref>] [<xref ref-type="bibr" rid="scirp.72001-ref7">7</xref>] .</p><p>Apart from these, due to advancement of technology and introduction of nanotechnology the size of materials reduced to nanometres possesses special physical and chemical characteristics [<xref ref-type="bibr" rid="scirp.72001-ref8">8</xref>] . Chio used nano-fluids for the first time with a combination of nano-scaled particles along with fluids [<xref ref-type="bibr" rid="scirp.72001-ref8">8</xref>] . Further, these fluids are used on stretched materials and on vertical plates to experiment thermal conductivity and convective heat transfer properties [<xref ref-type="bibr" rid="scirp.72001-ref9">9</xref>] [<xref ref-type="bibr" rid="scirp.72001-ref10">10</xref>] [<xref ref-type="bibr" rid="scirp.72001-ref11">11</xref>] . In this paper, the study is being conducted to test the flow characteristics on a vertical plate and to study the nonlinearly stretching sheet with respect to viscous flow of nano fluids and heat transfer with magnetic field and thermal radiation.</p><p>To study these aspects, Keller-Box method is used and is known to be one of the best numerical methods included with mixed finite volume that considers the average of conservation laws and related constitutive laws [<xref ref-type="bibr" rid="scirp.72001-ref12">12</xref>] . Earlier the applications of this method were used by Hamad et al. [<xref ref-type="bibr" rid="scirp.72001-ref13">13</xref>] for the steady boundary layer similarity solutions for studying viscous flow and heat transfer characteristics on stretching sheets along with thermal radiation [<xref ref-type="bibr" rid="scirp.72001-ref13">13</xref>] . The importance of this paper is to understand the thermal radiation effect on stretched sheets along with various other factors discussed by previous researchers.</p></sec><sec id="s2"><title>2. Mathematical Formulation</title><p>In this paper, the properties of viscous flow with respect to nano-fluid on a stretching sheets is considered. Generally the flow is possible when the condition<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x2.png" xlink:type="simple"/></inline-formula>. Here, the term y is the normal coordinate with respect to the stretching sheet. Practically the steady uniform stretching leads to equal and opposite forces along x-axis; hence the sheets will be stretched by fixing the origin.</p><p>The following assumptions are made before getting into more mathematical formulations. Assume the temperature at stretching surface as a function of x (see Equation (5)), ambient temperature T as constant and at the sheet nano particle fraction C as a constant with a value<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x3.png" xlink:type="simple"/></inline-formula>. Now assume that the sheet is extended by stretching with a nonlinearity parameter n along with a velocity of<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x4.png" xlink:type="simple"/></inline-formula>. Here x is the stretching surface coordinate where the measurement is being taken place.</p><p>Now consider a nanofluid is flowing at <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x5.png" xlink:type="simple"/></inline-formula> and consider fluid to be under the influence of electrical conduction because of the magnetic field<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x6.png" xlink:type="simple"/></inline-formula>, which is normal to stretching sheet. Make a note that at stretching surface the <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x7.png" xlink:type="simple"/></inline-formula> (wall temperature) and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x8.png" xlink:type="simple"/></inline-formula> are considered to be constant. The ambient value of temperature <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x9.png" xlink:type="simple"/></inline-formula> and nanoparticle fraction <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x10.png" xlink:type="simple"/></inline-formula> are denoted when y tends to infinity. The physical system considered for this study included for nano-technical fabrication and thermal material processing. In the <xref ref-type="fig" rid="fig1">Figure 1</xref>, coordinate system and flow models are shown and governing equations are given below:</p><disp-formula id="scirp.72001-formula7"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-4900446x11.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.72001-formula8"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-4900446x12.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.72001-formula9"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-4900446x13.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.72001-formula10"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-4900446x14.png"  xlink:type="simple"/></disp-formula><p>The boundary conditions for parameters velocity, temperature and nano-particle fraction are given below:</p><disp-formula id="scirp.72001-formula11"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-4900446x15.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.72001-formula12"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-4900446x16.png"  xlink:type="simple"/></disp-formula><p>where,</p><p>u and v are the velocity components in x and y directions,</p><p>a is acceleration of components.</p><p>Thermal Diffusivity <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x17.png" xlink:type="simple"/></inline-formula></p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x18.png" xlink:type="simple"/></inline-formula>is electrical conductivity,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x19.png" xlink:type="simple"/></inline-formula>is the kinematic viscosity,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x20.png" xlink:type="simple"/></inline-formula>is the density,</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> The Physical model and corresponding coordinate systems</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-4900446x21.png"/></fig><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x22.png" xlink:type="simple"/></inline-formula>is the Brown Diffusion Coefficient,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x23.png" xlink:type="simple"/></inline-formula>is the thermo phoresis diffusion coefficient.</p><p>However,</p><disp-formula id="scirp.72001-formula13"><graphic  xlink:href="http://html.scirp.org/file/3-4900446x24.png"  xlink:type="simple"/></disp-formula><p>The <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x25.png" xlink:type="simple"/></inline-formula> is the ratio between effective heat capacity of the nanoparticle material and fluid.</p><p>Here,</p><p>c is volumetric volume coefficient,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x26.png" xlink:type="simple"/></inline-formula>is density of particles,</p><p>C is rescaled volume fraction of nanoparticles,</p><p>R is radiation parameter.</p><p>Now assume variable magnetic field <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x27.png" xlink:type="simple"/></inline-formula> is in the for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x28.png" xlink:type="simple"/></inline-formula>.</p><p>Using Rosseland approximation for radiation, we can write</p><disp-formula id="scirp.72001-formula14"><label>(7a)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-4900446x29.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x30.png" xlink:type="simple"/></inline-formula> is the absorption coefficient, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x31.png" xlink:type="simple"/></inline-formula>is the Stefan-Boltzman constant. Assuming the temperature difference within the flow is such that <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x32.png" xlink:type="simple"/></inline-formula> may be expanded in a Taylor series about <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x33.png" xlink:type="simple"/></inline-formula> and neglecting higher orders we get<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x33.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x34.png" xlink:type="simple"/></inline-formula>.</p><p>Hence, Equation (7a) becomes</p><disp-formula id="scirp.72001-formula15"><label>(7b)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-4900446x35.png"  xlink:type="simple"/></disp-formula><p>Hence</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x36.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x36.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x37.png" xlink:type="simple"/></inline-formula>,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x38.png" xlink:type="simple"/></inline-formula>,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x39.png" xlink:type="simple"/></inline-formula>,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x39.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x40.png" xlink:type="simple"/></inline-formula>. (7)</p><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x41.png" xlink:type="simple"/></inline-formula> represents stream functions and is defined as<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x41.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x42.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x41.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x42.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x43.png" xlink:type="simple"/></inline-formula>so that</p><p>Equation (1) is satisfied identical. The governing Equations (2)-(4) or reduced by Equations (7).</p><disp-formula id="scirp.72001-formula16"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-4900446x44.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.72001-formula17"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-4900446x45.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.72001-formula18"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-4900446x46.png"  xlink:type="simple"/></disp-formula><p>The transformed boundary conditions are</p><disp-formula id="scirp.72001-formula19"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-4900446x47.png"  xlink:type="simple"/></disp-formula><p>Here, primes in the above equation represent the differentiation with respect to η, which is known to be an involved physical parameter and it is defined as follows:</p><disp-formula id="scirp.72001-formula20"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-4900446x48.png"  xlink:type="simple"/></disp-formula><p>Here,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x49.png" xlink:type="simple"/></inline-formula>is Prandtl number,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x50.png" xlink:type="simple"/></inline-formula>is the Lewis number,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x51.png" xlink:type="simple"/></inline-formula>is the Brownian motion parameter,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x52.png" xlink:type="simple"/></inline-formula>is the thermophoresis parameter,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x53.png" xlink:type="simple"/></inline-formula>is magnetic parameter,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x54.png" xlink:type="simple"/></inline-formula>is the Eckert number,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x55.png" xlink:type="simple"/></inline-formula>is the porous term,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x56.png" xlink:type="simple"/></inline-formula>is the radiation parameters.</p><p>This boundary value problem is reduced to the classical problem of flow and heat and mass transfer due to a stretching surface in a viscous fluid when <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x57.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x57.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x58.png" xlink:type="simple"/></inline-formula> in Equations (9) and (10).</p><p>In this study the quantities of practical interest are listed below:</p><disp-formula id="scirp.72001-formula21"><label>(13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-4900446x59.png"  xlink:type="simple"/></disp-formula><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x60.png" xlink:type="simple"/></inline-formula>is local skin friction,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x61.png" xlink:type="simple"/></inline-formula>is Nusselt Number,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x62.png" xlink:type="simple"/></inline-formula>is Sherwood Number.</p><p>The heat and mass fluxes <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x63.png" xlink:type="simple"/></inline-formula> at different surfaces for the thermal conductivity (k) is given by</p><disp-formula id="scirp.72001-formula22"><label>(14)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-4900446x64.png"  xlink:type="simple"/></disp-formula><p>Substituting Equation (7) into Equations (13) and (14), we obtain</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x65.png" xlink:type="simple"/></inline-formula>,</p><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x66.png" xlink:type="simple"/></inline-formula> is the local Reynolds number.</p></sec><sec id="s3"><title>3. Results and Discussion</title><p>Exact analysis for the reduced Equations (8)-(11) are not possible as they are nonlinear and coupled. However using Keller-Box method these problems can be evaluated for different values and parameters such as Pr, Nb, T and Le. Various effects are investi-</p><p>gated in this paper such as dimensionless velocity, temperature, skin function, mass transfer and rate of heat.</p><p>Some of the principal steps of Keller Box methods are listed below:</p><p>1) Reducing higher order ODEs to the first order ODEs</p><p>Let <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x67.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x67.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x68.png" xlink:type="simple"/></inline-formula></p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x69.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x69.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x70.png" xlink:type="simple"/></inline-formula></p><p>Let <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x71.png" xlink:type="simple"/></inline-formula></p><disp-formula id="scirp.72001-formula23"><graphic  xlink:href="http://html.scirp.org/file/3-4900446x72.png"  xlink:type="simple"/></disp-formula><p>Let <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x73.png" xlink:type="simple"/></inline-formula></p><disp-formula id="scirp.72001-formula24"><graphic  xlink:href="http://html.scirp.org/file/3-4900446x74.png"  xlink:type="simple"/></disp-formula><p>In the following steps only first ODE statement will be considered for further steps to follow using Keller Box method.</p><p>2) First order ODEs are written into difference equations by using central differencing schemes</p><p>Let us apply the central differential equation for <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x75.png" xlink:type="simple"/></inline-formula></p><disp-formula id="scirp.72001-formula25"><graphic  xlink:href="http://html.scirp.org/file/3-4900446x76.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.72001-formula26"><graphic  xlink:href="http://html.scirp.org/file/3-4900446x77.png"  xlink:type="simple"/></disp-formula><p>3) Using the Newtons method to linearizing the difference equation for extending it into vector form</p><disp-formula id="scirp.72001-formula27"><graphic  xlink:href="http://html.scirp.org/file/3-4900446x78.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.72001-formula28"><graphic  xlink:href="http://html.scirp.org/file/3-4900446x79.png"  xlink:type="simple"/></disp-formula><p>4) And finally using block elimination method the system equations are solved to draw the corresponding matrices.</p><p>MATLAB software is used to solve the differential equations numerically. This software is very efficient for using with Keller Box method.</p><p>Various comparisons are presented in <xref ref-type="table" rid="table1">Table 1</xref> to validate the proposed method with respect to previous method for the equations <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x80.png" xlink:type="simple"/></inline-formula> and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x80.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x81.png" xlink:type="simple"/></inline-formula>. This comparisons resulted to be excellent and are found to be excellent. At the same time various effects due to magnetic and viscous parameters are shown in the <xref ref-type="table" rid="table2">Table 2</xref>. The <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x80.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x81.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x82.png" xlink:type="simple"/></inline-formula> is decreasing with respect to M, Ec, n and Lewis numbers. However <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x80.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x81.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x82.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x83.png" xlink:type="simple"/></inline-formula> also is a decreasing function of with respect to parameters M, n and Nt but is found to be increasing with respect to Pr, Ec and Le. Increase in Le means the fluid is more viscous as similar to radiation parameter (R) which in turn increases the rate of mass transfer and raise in Le reduces the heat transfer.</p><p>The magnetic parameter (M) effect is shown in <xref ref-type="fig" rid="fig2">Figure 2</xref>, in which the tangential velocity of fluid is decreasing with a raise in the values of magnetic field. However Lorentz forces is introduced in an electrically conducting fluid due to the interrelation between</p><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Comparison of skin friction coefficient, Nusselt and Sherwood number for various Values of Ec when Pr = 10, n = 10, Le = 10 and Nt = 0.3</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Nb</th><th align="center" valign="middle" >Hamad</th><th align="center" valign="middle" >Present</th><th align="center" valign="middle" >Hamad</th><th align="center" valign="middle" >Present</th></tr></thead><tr><td align="center" valign="middle" ></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x84.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x85.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x86.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x87.png" xlink:type="simple"/></inline-formula></td></tr><tr><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >3.771628</td><td align="center" valign="middle" >3.7716</td><td align="center" valign="middle" >3.658830</td><td align="center" valign="middle" >3.5688</td></tr><tr><td align="center" valign="middle" >0.2</td><td align="center" valign="middle" >3.251502</td><td align="center" valign="middle" >3.2515</td><td align="center" valign="middle" >3.149618</td><td align="center" valign="middle" >3.1496</td></tr><tr><td align="center" valign="middle" >0.3</td><td align="center" valign="middle" >2.827929</td><td align="center" valign="middle" >2.8279</td><td align="center" valign="middle" >2.735630</td><td align="center" valign="middle" >2.7356</td></tr><tr><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >5.621979</td><td align="center" valign="middle" >5.6220</td><td align="center" valign="middle" >5.345776</td><td align="center" valign="middle" >5.3458</td></tr><tr><td align="center" valign="middle" >0.2</td><td align="center" valign="middle" >0.998139</td><td align="center" valign="middle" >0.9981</td><td align="center" valign="middle" >0.875024</td><td align="center" valign="middle" >0.8750</td></tr><tr><td align="center" valign="middle" >0.3</td><td align="center" valign="middle" >0.451703</td><td align="center" valign="middle" >0.4517</td><td align="center" valign="middle" >0.525092</td><td align="center" valign="middle" >0.5251</td></tr></tbody></table></table-wrap><table-wrap id="table2" ><label><xref ref-type="table" rid="table2">Table 2</xref></label><caption><title> Resulting table: Showing results of<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x88.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x88.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x89.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x88.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x89.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x90.png" xlink:type="simple"/></inline-formula>for the values of M, Ec, when Pr = 10, n = 10, Le = 10, Nt = 0.3, Nb = 0.3 and R = 0</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/3-4900446x91.png" xlink:type="simple"/></inline-formula></th><th align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x92.png" xlink:type="simple"/></inline-formula></th><th align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x93.png" xlink:type="simple"/></inline-formula></th><th align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-4900446x94.png" xlink:type="simple"/></inline-formula></th></tr></thead><tr><td align="center" valign="middle" >0.0</td><td align="center" valign="middle" >0</td><td align="center" valign="middle" >1.2352</td><td align="center" valign="middle" >2.8279</td><td align="center" valign="middle" >0.4517</td></tr><tr><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >0</td><td align="center" valign="middle" >1.2756</td><td align="center" valign="middle" >2.8310</td><td align="center" valign="middle" >0.4314</td></tr><tr><td align="center" valign="middle" >0.3</td><td align="center" valign="middle" >0</td><td align="center" valign="middle" >1.3527</td><td align="center" valign="middle" >2.8370</td><td align="center" valign="middle" >0.3925</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >0</td><td align="center" valign="middle" >1.4254</td><td align="center" valign="middle" >2.8426</td><td align="center" valign="middle" >0.3559</td></tr><tr><td align="center" valign="middle" >1.0</td><td align="center" valign="middle" >0</td><td align="center" valign="middle" >1.5921</td><td align="center" valign="middle" >2.8555</td><td align="center" valign="middle" >0.2719</td></tr><tr><td align="center" valign="middle" >0</td><td align="center" valign="middle" >0</td><td align="center" valign="middle" >1.2352</td><td align="center" valign="middle" >2.8279</td><td align="center" valign="middle" >0.4517</td></tr><tr><td align="center" valign="middle" >0</td><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >1.2352</td><td align="center" valign="middle" >2.7356</td><td align="center" valign="middle" >0.5251</td></tr><tr><td align="center" valign="middle" >0</td><td align="center" valign="middle" >0.3</td><td align="center" valign="middle" >1.2352</td><td align="center" valign="middle" >2.5492</td><td align="center" valign="middle" >0.6734</td></tr><tr><td align="center" valign="middle" >0</td><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >1.2352</td><td align="center" valign="middle" >2.3604</td><td align="center" valign="middle" >0.8239</td></tr><tr><td align="center" valign="middle" >0</td><td align="center" valign="middle" >1.0</td><td align="center" valign="middle" >1.2352</td><td align="center" valign="middle" >1.8772</td><td align="center" valign="middle" >1.2096</td></tr></tbody></table></table-wrap><p>both magnetic and electrical fields. The Lorentz force acts against the flow when magnetic field is applied normal to the direction. In such scenarios the resistive forces will slow down.</p><p>The positive changes in M allow increasing the temperature within the boundary layer as shown in <xref ref-type="fig" rid="fig3">Figure 3</xref>. These profiles cannot be observed in the graph due to the limitations of boundary layer. The temperature profiles are plotted for different values of M.</p><p>The influence of M, nonlinear stretching parameter n on dimensionless, and nanoparticle concentrations are shown in <xref ref-type="fig" rid="fig4">Figure 4</xref>. The increase in M will enhance the dimensionless concentration profiles can be observed in <xref ref-type="fig" rid="fig4">Figure 4</xref>. Lorentz forces are resistive in nature opposing the fluid motion and hence the result is the production of heat. In such scenarios, in the magnetic field, the thermal boundary layer and nanoparticle volume fraction boundary layers thickness will increase. The nonlinear stretching</p><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> The velocity profiles for M</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-4900446x95.png"/></fig><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> The temperature profiles for M</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-4900446x96.png"/></fig><p>parameter is slightly negligible for the variation of nanoparticle concentration. Note that these parameters are negligible for both positive and negative values of n.</p><p>The effect of R for fixed values of other parameters the dimensionless concentrations</p><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> The temperature profiles for R</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-4900446x97.png"/></fig><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> The concentration profiles for R</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-4900446x98.png"/></fig><p>are shown in <xref ref-type="fig" rid="fig5">Figure 5</xref>. Inhibit nanoparticle pieces diffusion is observed in <xref ref-type="fig" rid="fig5">Figure 5</xref> for the large values of R. However, there will be heavy reduction in concentration boundary layer thickness.</p><p>Behaviour of temperature with respect to different values of Pr numbers are shown in <xref ref-type="fig" rid="fig6">Figure 6</xref>. This shows the decrease in velocity with the raise in Pr which leads to a decrease in the thermal boundary layer thickness. In simple this can be understood due to the raise in thermal conductivity for small values of Pr and hence the heat will be</p><p>diffused away from the heated surface as compared with the high values of Pr. Therefore the smaller Pr number due to thermal boundary layer leads to a thicker and hence the transferred heat will be reduced.</p><p>The temperature profiles for different values of Ec are plotted in <xref ref-type="fig" rid="fig7">Figure 7</xref>. The increase in the values of Ec is due to the increases in temperature within the boundary layer.</p><p>The effect of Ec on dimensionless concentration for various fixed values of other parameters is shown in <xref ref-type="fig" rid="fig8">Figure 8</xref>. The larger values of Ec suppress concentration profiles and hence inhibit nanoparticle species diffusion is observed. However there is a much greater reduction in concentration boundary layer thickness.</p><p>For the plot between behaviour of temperature and different value of Le are shown in <xref ref-type="fig" rid="fig9">Figure 9</xref> shows that the increase in Le results to a decreasing velocity due to which thermal boundary layer thickness will be decreasing so that less average temperature within boundary layer is observed. Reasons for small values of Le allow the thermal conductivity of the fluid to increase. Hence it allows the heat to diffuse rapidly from the heated surface for high values of Le.</p><p>Effect of Le on dimensionless concentration for various fixed parameters is shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>0. Larger values of Le suppress concentration profiles and a greater reduction will be seen in the concentration of boundary layer thickness.</p><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> Temperature profiles for Pr</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-4900446x99.png"/></fig><fig id="fig7"  position="float"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> The temperature profiles for Ec</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-4900446x100.png"/></fig><fig id="fig8"  position="float"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> The concentration profiles for Ec</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-4900446x101.png"/></fig><p>Behaviour of temperature with respect to different values of Nb are showin in <xref ref-type="fig" rid="fig1">Figure 1</xref>1. The increasing Nb values results in a decreasing velocity. It also results for a decrease in the thermal boundary layer thickness and hence reduces the average temperatures within the boundary layers. The reason behind such scenario lies in the smaller</p><fig id="fig9"  position="float"><label><xref ref-type="fig" rid="fig9">Figure 9</xref></label><caption><title> The temperature profiles for Le</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-4900446x102.png"/></fig><fig id="fig10"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>0</label><caption><title> Concentration profiles for Le</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-4900446x103.png"/></fig><p>values of Nb will allow to an increase in thermal conductivity of fluids so that heat will be diffused from heated surface rapidly for higher values of Nb. Hence for smaller Nb the thermal boundary layer is thicker and rate of heat transfer will be reduced.</p><fig id="fig11"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>1</label><caption><title> The temperature profiles for Nb</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-4900446x104.png"/></fig><fig id="fig12"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>2</label><caption><title> The concentration profiles for Nb</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-4900446x105.png"/></fig><p>Effect of Nb for dimensionless concentration for various fixed values of other parameters is observed in <xref ref-type="fig" rid="fig1">Figure 1</xref>2. Here for higher values of Nb suppress the concentration profile and hence greater reduction in the thickness of the concentration boundary</p><fig id="fig13"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>3</label><caption><title> The temperature profiles for Nt</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-4900446x106.png"/></fig><fig id="fig14"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>4</label><caption><title> Concentration profiles for Nt</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/3-4900446x107.png"/></fig><p>layer.</p><p>The Nt on temperature and concentration profiles are shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>3. In this the temperature profile increases the concentration profile due to Nt inhibits the fluid for not to move freely in the boundary layer, which in turn leads the flow to increase</p><p>the thickness of thermal boundary layer.</p><p>Influence of Nt and n on dimensionless and nanoparticle concentrations are shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>4 and the dimensionless profiles are observed to be enhancing with the</p><p>increase of Nt. However Lorentz force opposes the fluid motion hence the heat is produced. Due to such conditions thermal boundary and nanoparticle volume fraction boundary layer thickness will become thicker for strong Nt.</p></sec><sec id="s4"><title>4. Conclusion</title><p>In this paper, various similarity solutions for viscous flow and heat transfer of nanofluids on nonlinear streached sheets under the influence of thermal radiation are shown in the results. However, similar solutions are depending on Pr, Le, M, n, Nb, T and Nt. The graphical representations of various governing parameters are obtained in different conditions to draw the importance of thermal radiation and some of the featured observations of the findings are listed below:</p><p>・ The velocity is decreasing with the increase in temperature.</p><p>・ Ec will increase proportionally with Eckert number.</p><p>・ The increase in M will lead to a decrease in velocity parameter.</p><p>・ The temperature will increase due to an increase in R.</p><p>・ The concentration will decrease due to an increase in R.</p></sec><sec id="s5"><title>Acknowledgements</title><p>I thank MHRD, Govt. of India for supporting my work through UGC-BSR Fellowship.</p></sec><sec id="s6"><title>Cite this paper</title><p>Rayapole, S.P. and Jakkula, A.R. (2016) Characteristics of Na- nofluids over a Non-Linearly Stretched Sheet under the Influence of Thermal Radiation and Magnetic Field. World Journal of Mechanics, 6, 456-471. http://dx.doi.org/10.4236/wjm.2016.611032</p></sec></body><back><ref-list><title>References</title><ref id="scirp.72001-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Hamad, M.A., Mahny, K.L. and Salam, M.R.A. (2011) Similarity Solution of Viscous Flow and Heat Transfer of a Nanofluid over a Nonlinearily Stretching Sheet. Middle-East Journal of Scientific Research, 8, 764-768.</mixed-citation></ref><ref id="scirp.72001-ref2"><label>2</label><mixed-citation publication-type="book" xlink:type="simple">Keller, H.B. (1971) A New Difference Scheme for Parabolic Problems. In: Hubbard, B., Ed., Numerical Solutions of Partial Differential Equations, Vol. 2, Academic Press, New York, 327-350.</mixed-citation></ref><ref id="scirp.72001-ref3"><label>3</label><mixed-citation publication-type="other" xlink:type="simple">Tiwari, R.K. and Das, M.K. (2007) Heat Transferaugmentation in a Two-Sided Lid-Driven Differentially Heated Square Cavity Utilizing Nanofluids. International Journal of Heat and Mass Transfer, 50, 2002-2018. http://dx.doi.org/10.1016/j.ijheatmasstransfer.2006.09.034</mixed-citation></ref><ref id="scirp.72001-ref4"><label>4</label><mixed-citation publication-type="other" xlink:type="simple">Maiga, S.E.B., Palm, S.J., Nguyen, C.T., Roy, G. and Galanis, N. (2005) Heat Transfer Enhancement by Using Nanofluids in Forced Convection Flow. International Journal of Heat and Fluid Flow, 26, 530-546. http://dx.doi.org/10.1016/j.ijheatfluidflow.2005.02.004</mixed-citation></ref><ref id="scirp.72001-ref5"><label>5</label><mixed-citation publication-type="other" xlink:type="simple">Choi, S.U.S., Zhang, Z.G., Yu, W., Lockwood, F.E. and Grulke, E.A. (2001) Anomalously Thermal Conductivity Enhancement in Nanotube Suspensions. Applied Physics Letters, 79, 2252-2254. http://dx.doi.org/10.1063/1.1408272</mixed-citation></ref><ref id="scirp.72001-ref6"><label>6</label><mixed-citation publication-type="other" xlink:type="simple">Choi, S.U.S. (1995) Enhancing Thermal Conductivity Offluids with Nanoparticles. Proceedings of the 1995 ASME International Mechanical Engineering Congress and Exposition, San Francisco, 99-105.</mixed-citation></ref><ref id="scirp.72001-ref7"><label>7</label><mixed-citation publication-type="other" xlink:type="simple">Partha, M.K., Murthy, P.V.S.N. and Rajasekhar, G.P. (2005) Effect of Viscous Dissipation on the Mixed Convection of Heat Transfer from an Exponential Stretching Surface. Heat and Mass Transfer, 41, 360-366. http://dx.doi.org/10.1007/s00231-004-0552-2</mixed-citation></ref><ref id="scirp.72001-ref8"><label>8</label><mixed-citation publication-type="other" xlink:type="simple">Sajid, M. and Hayat, T. (2008) Influence of Thermal Radiation on the Boundary Layer Flow Due to an Exponentially Stretching Sheet. International Communications in Heat and Mass Transfer, 35, 347-356. http://dx.doi.org/10.1016/j.icheatmasstransfer.2007.08.006</mixed-citation></ref><ref id="scirp.72001-ref9"><label>9</label><mixed-citation publication-type="other" xlink:type="simple">Vajravelu, K. (2001) Viscous Flow over a Nonlinearly Stretching Sheet. Applied Mathematics and Computation, 124, 281-288. http://dx.doi.org/10.1016/S0096-3003(00)00062-X</mixed-citation></ref><ref id="scirp.72001-ref10"><label>10</label><mixed-citation publication-type="other" xlink:type="simple">Magyari, E. and Keller, B. (2000) Exact Solutions for Self-Similar Boundary-Layer Flows Induced by Permeable Stretching Walls. European Journal of Mechanics-B/Fluids, 19, 109-122. http://dx.doi.org/10.1016/S0997-7546(00)00104-7</mixed-citation></ref><ref id="scirp.72001-ref11"><label>11</label><mixed-citation publication-type="other" xlink:type="simple">Gupta, P.S. and Gupta, A.S. (1977) Heat and Mass Transfer on a Stretching Sheet with Suction or Blowing. The Canadian Journal of Chemical Engineering, 55, 744-746. http://dx.doi.org/10.1002/cjce.5450550619</mixed-citation></ref><ref id="scirp.72001-ref12"><label>12</label><mixed-citation publication-type="other" xlink:type="simple">Vleggaar, J. (1977) Laminar Boundary-Layer Behaviour on Continuous, Accelerating Surfaces. Chemical Engineering Science, 32, 1517-1525. http://dx.doi.org/10.1016/0009-2509(77)80249-2</mixed-citation></ref><ref id="scirp.72001-ref13"><label>13</label><mixed-citation publication-type="other" xlink:type="simple">Saidura, R., Leong, K.Y. and Mohammad, H.A. (2011) A Review on Applications and Challenges of Nanofluids. Renewable and Sustainable Energy Reviews, 15, 1646-1668. http://dx.doi.org/10.1016/j.rser.2010.11.035</mixed-citation></ref></ref-list></back></article>