<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article  PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd"><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article"><front><journal-meta><journal-id journal-id-type="publisher-id">JAMP</journal-id><journal-title-group><journal-title>Journal of Applied Mathematics and Physics</journal-title></journal-title-group><issn pub-type="epub">2327-4352</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/jamp.2014.28087</article-id><article-id pub-id-type="publisher-id">JAMP-47817</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>A Mixed Convection Boundary Layer Flow over a Vertical Wall in a Porous Medium, with Exponentially Varying Fluid Viscosity</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Eunice</surname><given-names>Mureithi</given-names></name><xref ref-type="aff" rid="aff1"><sub>1</sub></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><aff id="aff1"><label>1</label><addr-line>Department of Mathematics, University of Dar es Salaam, Dar es Salaam, Tanzania</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>ewambui02@gmail.com</email></corresp></author-notes><pub-date pub-type="epub"><day>27</day><month>06</month><year>2014</year></pub-date><volume>02</volume><issue>08</issue><fpage>795</fpage><lpage>802</lpage><history><date date-type="received"><day>20</day>	<month>May</month>	<year>2014</year></date><date date-type="rev-recd"><day>18</day>	<month>June</month>	<year>2014</year>	</date><date date-type="accepted"><day>3</day>	<month>July</month>	<year>2014</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 study investigates a mixed convection boundary layer flow over a
vertical wall embedded in a highly porous medium. The fluid viscosity is
assumed to decrease exponentially with temperature. The boundary layer
equations are transformed into a non-similar form using an appropriate non-similar
variable ξ and a
pseudo-similar variable η. The non-similar
equations are solved using an efficient local non-similarity method. The effect
of viscosity variation parameter on the heat transfer, skin friction and the
velocity and temperature distribution within the boundary layer is
investigated. The viscosity variation parameter, the viscous dissipation
parameter and non-simi-larity variable are shown to have a significant effect
on velocity and thermal boundary layer and also on the skin friction
coefficient and heat transfer at the wall. 
</p></abstract><kwd-group><kwd>Porous Medium</kwd><kwd> Non-Darcy</kwd><kwd> Mixed Convection Boundary Layer</kwd><kwd> Temperature Dependent Viscosity</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Mixed convection boundary layer flow through a porous medium is of primary importance due to its applications in industry such as geothermal operations (for example dynamics of hot springs), terrestrial heat flow through an aquifer, flow of moisture through porous industrial material etc. Engineering applications include porous thermal insulation and heat exchangers with fluidized beds etc.</p><p>Reviews on convective heat transfer in porous medium are well documented in the books by Nield and Bejan, [<xref ref-type="bibr" rid="scirp.47817-ref1">1</xref>] and Pop and Ingham [<xref ref-type="bibr" rid="scirp.47817-ref2">2</xref>] , Kaviany [<xref ref-type="bibr" rid="scirp.47817-ref3">3</xref>] and in the handbook of porous media edited by Vafai [<xref ref-type="bibr" rid="scirp.47817-ref4">4</xref>] . Numerous studies on mixed convection boundary through a porous media using the Darcy model and extended Darcy models have been carried out, by others, by Karabis et al. [<xref ref-type="bibr" rid="scirp.47817-ref5">5</xref>] investigated a mixed forced-free convection boundary layer flow over a vertical wall in a highly porous medium, Chen [<xref ref-type="bibr" rid="scirp.47817-ref6">6</xref>] who looked at a boundary layer flow over a horizontal in a saturated porous medium. Using the model developed by Vafai and Tien [<xref ref-type="bibr" rid="scirp.47817-ref7">7</xref>] , Hong et al. [<xref ref-type="bibr" rid="scirp.47817-ref8">8</xref>] investigated the non-Darcian effects on a flow over a vertical plate in porous media.</p><p>Most fluids used in engineering have temperature varying viscosity. A study by Hossain and Munir [<xref ref-type="bibr" rid="scirp.47817-ref9">9</xref>] investigated a mixed convection boundary layer with temperature dependent viscosity where it was shown that the viscosity variation parameter has an effect on the wall skin friction coefficient and wall heat transfer coefficient. Jayanthi and Kumari [<xref ref-type="bibr" rid="scirp.47817-ref10">10</xref>] studied the effects of variable viscosity on a non-Darcy flow of a non-Newtonian fluid over a vertical surface in porous medium. They showed that variable viscosity parameter has a significant effect on the fluid flow properties.</p><p>The current study focuses on a boundary layer flow over a vertical wall embedded in a highly porous medium and with variable viscosity. The non-similar boundary layer equations are solved using the local non-similarity method due to Sparrow et al. [<xref ref-type="bibr" rid="scirp.47817-ref11">11</xref>] and Sparrow and Yu [<xref ref-type="bibr" rid="scirp.47817-ref12">12</xref>] . In Section 2 the mixed convection boundary layer flow equations are formulated and transformed to the non-similar form, in Section 3 the equations are solved and the results presented and discussed in Section 4. Conclusions are drawn in Section 5.</p></sec><sec id="s2"><title>2. Mixed Convection Boundary Layer Flow in a Porous Medium</title><p>A steady, two-dimensional flow of a viscous incompressible fluid over a heated semi-infinite vertical wall embedded in a highly porous medium is studied. The <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\a328faab-a8fa-496c-9b4f-a1b46db385ab.png" xlink:type="simple"/></inline-formula>-axis is taken along the wall and the <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\fba96967-4fc2-4c13-b28c-a8e998056521.png" xlink:type="simple"/></inline-formula>-axis as the normal axis to <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\9a092afa-9568-48e9-97e0-5c2dd189587c.png" xlink:type="simple"/></inline-formula>-axis. The free-stream velocity and temperature are taken as <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\dc9d239d-104b-4b4b-9a18-7530432c2682.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\f8dd17a9-9963-4b51-b374-589018f3369f.png" xlink:type="simple"/></inline-formula> respectively and the wall temperature as<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\cb84a047-16e6-437b-aac2-b7682cb4ddc3.png" xlink:type="simple"/></inline-formula>. The fluid viscosity <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\ab216a90-3713-4e4a-b30e-7e98703495bf.png" xlink:type="simple"/></inline-formula> is assumed to decrease exponentially with temperature. Under the boundary layer approximation for a flow through a porous medium and the Boussinesq's approximation, the mixed convection boundary layer equations through a porous media take the form:</p><disp-formula id="scirp.47817-formula1"><label>(2.1)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\7666d08d-31cb-4ac9-824a-95c2128ec3ee.png"/></disp-formula><disp-formula id="scirp.47817-formula2"><label>(2.2)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\3ef518af-cf20-4cad-9fea-f6e96851e801.png"/></disp-formula><disp-formula id="scirp.47817-formula3"><label>(2.3)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\0aba9451-bc1b-4f92-9b8e-fb10ba8c7290.png"/></disp-formula><p>The appropriate boundary conditions for the flow are:</p><disp-formula id="scirp.47817-formula4"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\7d8aad45-53fc-4d8a-9bb4-361852a2ba62.png"/></disp-formula><p>Here <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\0e2f52c6-17d5-4195-8466-7b7565f00663.png" xlink:type="simple"/></inline-formula> is the gravitational acceleration, <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\1603c757-c4a9-4a8f-8aef-982c9ffa6552.png" xlink:type="simple"/></inline-formula>is the coefficient of thermal expansion, <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\cd7b180d-b423-4195-b523-940da5021a0a.png" xlink:type="simple"/></inline-formula>is the thermal con- ductivity, <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\0a794f7e-0230-409a-8198-cb2e8d0caec1.png" xlink:type="simple"/></inline-formula>is the specific heat at constant pressure, <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\bf7ee3b6-4728-44dd-ac1e-2698ffac3cd7.png" xlink:type="simple"/></inline-formula>is the fluid density at reference temperature <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\6327b3fa-a413-424b-bca0-746b68b3903e.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\17f9fcdf-d2d7-4ee6-ad47-025bf4065ae0.png" xlink:type="simple"/></inline-formula> is the permeability of the porous medium. The wall temperature <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\c4a05f92-cf13-4455-931e-ad866f4be6f0.png" xlink:type="simple"/></inline-formula> is assumed to be a constant. Most com- mon fluids have dynamic viscosity that varies exponentially with temperature. Here we use Arrhenius model which takes the exponential form</p><disp-formula id="scirp.47817-formula5"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\16dca867-e12d-4744-8f5b-814ff56f3d40.png"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\f7b26fca-5926-40a3-a826-c15dfbfe852c.png" xlink:type="simple"/></inline-formula> is reference viscosity at reference temperature <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\5f22b383-9f6d-4976-9a89-1aa708b70dea.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\3274990b-2acd-432f-9dde-08b9489e720f.png" xlink:type="simple"/></inline-formula> is a viscosity variation number defined as</p><disp-formula id="scirp.47817-formula6"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\92f70a83-3b86-434f-ab11-f26c082f749a.png"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\1ff44dfd-305b-4320-a29b-f081b89708f6.png" xlink:type="simple"/></inline-formula> with be <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\e4a938e7-8dc8-480b-a216-d20f070043ec.png" xlink:type="simple"/></inline-formula> being the fluid viscosity at the wall temperature<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\a8118bb4-c646-42cf-a3c2-e291f4444c08.png" xlink:type="simple"/></inline-formula>. For gases <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\ee34a74d-f635-4d6d-8eb0-361287c140fd.png" xlink:type="simple"/></inline-formula> and for liquids it is positive. For small values of <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\3c618c27-164e-413a-a68d-d08845a0d079.png" xlink:type="simple"/></inline-formula> Taylor expansion leads to the linear or the inverse relation of viscosity with temperature.</p><sec id="s2_1"><title>Non-Similar Boundary Layer Equations</title><p>The equations are rendered non-dimensional by introducing a boundary layer pseudo-similarity variable <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\4e4cac01-5aa9-432b-a90d-1621b61da93c.png" xlink:type="simple"/></inline-formula> and a non-similar variable<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\c438f51e-3161-4373-b990-8933fa41b6ee.png" xlink:type="simple"/></inline-formula>, defined respectively as</p><disp-formula id="scirp.47817-formula7"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\b0acbdf8-e938-481b-83c1-f560338dbfbd.png"/></disp-formula><p>with <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\b6ccfc86-3dea-4e27-a4eb-f9c6f08da6f7.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\45c31051-85d6-4488-bfd1-7e23e5af0c6b.png" xlink:type="simple"/></inline-formula> being the local Grash of number and the local Reynolds number, defined as</p><disp-formula id="scirp.47817-formula8"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\c5c09a02-7c44-4cdf-af37-33f7e01b6cae.png"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\3d7118f2-37cb-4c1b-a682-1fa43b817882.png" xlink:type="simple"/></inline-formula> is the kinematic viscosity.</p><p>We use the scaling</p><disp-formula id="scirp.47817-formula9"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\578b29c8-2326-4a28-a82a-724b134ab2a9.png"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\6aff51ec-6a9c-40e4-9d3f-f32ad3f5fb94.png" xlink:type="simple"/></inline-formula> is the dimensionless viscosity and<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\d230dfd4-cbe0-437d-9fa9-ce588d7b7965.png" xlink:type="simple"/></inline-formula>.</p><p>From the equation of continuity:</p><disp-formula id="scirp.47817-formula10"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\e943000e-082b-4149-bbb8-8a5f42bf0e69.png"/></disp-formula><p>with</p><disp-formula id="scirp.47817-formula11"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\aa741cf8-5ab2-41d6-b15e-61a4a40eebf6.png"/></disp-formula><p>Assuming power law variation in the free-stream velocity<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\33c971c3-3b99-47c5-b9e3-c6f46a5c9993.png" xlink:type="simple"/></inline-formula>, we have<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\464bf216-7d1c-4f3c-8705-70a97148ddd1.png" xlink:type="simple"/></inline-formula>. The non-similar boun- dary layer equations take the form:</p><disp-formula id="scirp.47817-formula12"><label>(2.4)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\ec3d0018-9d2c-439a-bedc-1382770eaaad.png"/></disp-formula><disp-formula id="scirp.47817-formula13"><label>(2.5)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\a3269504-2534-404e-ae72-5830f92abc42.png"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\db10ffdc-7aaa-486c-a6c7-a2c59d26d0e0.png" xlink:type="simple"/></inline-formula> is the dimensionless local permeability parameter, <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\bad417a4-ae4f-4eb0-9596-6264189e0470.png" xlink:type="simple"/></inline-formula>is the Prandtl number and <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\a6925ee6-d225-4c59-81f6-d3bebaaa4353.png" xlink:type="simple"/></inline-formula> is the local Eckert number, defined respectively as</p><disp-formula id="scirp.47817-formula14"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\af1cc804-2a11-4fef-bc07-e89739dc227c.png"/></disp-formula><p>The boundary conditions, in non-dimensional form, are:</p><disp-formula id="scirp.47817-formula15"><label>(2.6)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\17c6dca8-0604-4fcf-82f1-bb60d3c3c7f5.png"/></disp-formula><p>The shear stress and the heat transfer at the wall can be represented using the local skin friction coefficient and the local Nusselt number, defined by</p><disp-formula id="scirp.47817-formula16"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\c0903ab5-7a63-4de2-9313-2fe6def641f3.png"/></disp-formula></sec></sec><sec id="s3"><title>3. Numerical Solutions of the Non-Similar Boundary Layer Equations</title><p>The system of Equations (2.4)-(2.6) is solved using the non-similar method of Sparrow et al. [<xref ref-type="bibr" rid="scirp.47817-ref11">11</xref>] . This method has been used extensively in solving non-similar mixed convection boundary layer equations by among other Sparrow and Yu [<xref ref-type="bibr" rid="scirp.47817-ref12">12</xref>] , Gorla et al. [<xref ref-type="bibr" rid="scirp.47817-ref13">13</xref>] , Mureithi and Mason [<xref ref-type="bibr" rid="scirp.47817-ref14">14</xref>] , B&#233;g et al. [<xref ref-type="bibr" rid="scirp.47817-ref15">15</xref>] etc. The method involves approximating the solutions at different levels of truncation. We introduce the notation:</p><disp-formula id="scirp.47817-formula17"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\8cf9d31c-ddf4-49b1-bc79-ed677cb38a32.png"/></disp-formula><p>The first level of approximation involves solving the local similarity equations, where all terms involving the <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\3da17970-a90b-4e7f-b233-3ad9014c9dc7.png" xlink:type="simple"/></inline-formula> and its derivatives (that is the non-similar terms,<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\e51d5c24-eafb-4fd3-810f-15db3ccf1574.png" xlink:type="simple"/></inline-formula>) in the Equations (2.4)-(2.6) are neglected.</p><p>At the second level of truncation, the method involves solving the system (2.4)-(2.6) together with the auxiliary system obtained by differentiating (2.4)-(2.6) partially with respect <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\81fb436e-8e75-42d4-b903-3df81a33eba9.png" xlink:type="simple"/></inline-formula> and neglecting all terms involving second order differentiation with respect to 𝜉 (that is <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\8fed8cb3-a348-4548-a6ed-b806b4e4522c.png" xlink:type="simple"/></inline-formula> The auxiliary system takes the form:</p><disp-formula id="scirp.47817-formula18"><label>(2.7)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\a753f68f-9c99-426d-937c-e47ba334c0c9.png"/></disp-formula><disp-formula id="scirp.47817-formula19"><label>(2.8)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\f2f21d15-5977-49c2-a95a-d4e57c0698a8.png"/></disp-formula><disp-formula id="scirp.47817-formula20"><label>(2.9)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\384e192a-d771-4dda-bf1f-9c152d84e353.png"/></disp-formula><p>The system (2.4)-(2.9) solved as if it is an ordinary differential system, with <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\006d6a42-ee5e-4dcf-a964-02e840e5880c.png" xlink:type="simple"/></inline-formula> being treated as a parameter. The results obtained are a better approximation than those obtained at the first level of approximation.</p><p>An even better approximation can be obtained at the third order level of approximation, where the system (2.4)-(2.9) are solved together with an of auxiliary system obtained by further differentiating Equations (2.7)-(2.9) partially with respect to <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\6282e34a-8d94-40a0-b3db-ee74f445fd00.png" xlink:type="simple"/></inline-formula> and all terms containing third order partials with respect to <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\d7299303-822c-4263-b0a0-d7540a9d6ee8.png" xlink:type="simple"/></inline-formula> are neglected.</p></sec><sec id="s4"><title>4. Discussion of Results</title><p>We approximate the solution of (2.4)-(2.6) using the second level of approximation. The system of Equations (2.4)-(2.9) is solved using the fourth order Runge-Kutta method combined with a Newton root refinement scheme. Computations were carried out for the case when <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\484c501e-ddf1-4752-86d3-e98509529386.png" xlink:type="simple"/></inline-formula> (air) and viscosity that increases exponentially with increase in temperature<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\922dff39-5ee9-44f0-8568-0c784b50432d.png" xlink:type="simple"/></inline-formula>.</p><p><xref ref-type="fig" rid="fig1">Figure 1</xref> show the effect varying the non-similar parameter <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\cc89431e-794c-4c0d-ba67-a66a957af449.png" xlink:type="simple"/></inline-formula> on the scaled stream-wise velocity, <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\cb9ad0e3-39f8-4e01-8789-897629e7a0ab.png" xlink:type="simple"/></inline-formula>, and viscosity, <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\46f94fa2-0389-4717-b513-367f543f013c.png" xlink:type="simple"/></inline-formula>, distribution in the boundary layer. At a fixed stream-wise location, <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\e0de88be-5224-4fa7-948d-b6a6ca7378bd.png" xlink:type="simple"/></inline-formula>becomes a buoyancy- related parameter. As <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\d844b112-21a4-404c-9f4a-4d5224368a47.png" xlink:type="simple"/></inline-formula> increases velocity overshoots (exceeding free-stream velocity) are observed within the boundary layer. The maximum values of the super-velocities increase with increase in <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\3436f021-9ba7-498a-aaae-d82f89ddb8aa.png" xlink:type="simple"/></inline-formula> Results in figure 1also show that increasing <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\d79d2568-781c-4657-b3ed-ef3517961b0d.png" xlink:type="simple"/></inline-formula> has the effect of decreasing the thickness of the viscosity boundary layer.</p><p>The effect of varying the viscous dissipation parameter <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\139edf4f-8398-4e89-895f-094b1a0517fd.png" xlink:type="simple"/></inline-formula> was investigated and the results are presented in <xref ref-type="fig" rid="fig2">Figure 2</xref>. The results indicate that as <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\78efdf13-d575-4593-9035-277dae778cc5.png" xlink:type="simple"/></inline-formula> increases, the amplitude of the super-velocities increase. Temperature is also shown to increase with increase in <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\50748846-7ebb-4a4d-82d7-2c085d810c43.png" xlink:type="simple"/></inline-formula> and for high enough values of <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\cdcb90b8-73dc-4741-9ad0-56ad4ce9d1da.png" xlink:type="simple"/></inline-formula> (in this case<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\b933c3aa-2992-42e2-9ad5-09e19468dfc3.png" xlink:type="simple"/></inline-formula>) there is a small region adjacent to the wall, where temperature exceeds its wall value of one. It follows that viscosity function also has positive gradient in that small region. This is an indication that increasing <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\67dfb5c1-6901-41c4-a90d-a6a6d6d1ded1.png" xlink:type="simple"/></inline-formula> results in increased heat transfer from the wall to the fluid.</p><p><xref ref-type="fig" rid="fig3">Figure 3</xref> shows stream-wise velocity and viscosity distributions within the boundary layer for different values of<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\e83a5d0c-495b-41a8-95f9-219bf2272b4e.png" xlink:type="simple"/></inline-formula>. The results show that at a fixed value of <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\1b113130-7454-4a82-91ff-13ae385384c4.png" xlink:type="simple"/></inline-formula> velocity overshoots increase with increase in<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\23ff822b-d194-46ad-887c-755326c832d5.png" xlink:type="simple"/></inline-formula>. On the con- trary, viscosity decreases with increase in<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\b13e8a00-7322-4490-8f8a-c24d2978a1a5.png" xlink:type="simple"/></inline-formula>.</p><p>Heat transfer at the wall (represented by the Nusselt number, <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\72fb8588-7bf2-4d4f-a929-e4f60145469e.png" xlink:type="simple"/></inline-formula>and shear stress at the wall (repre- sented by skin friction coefficient, <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\36894bc0-bf65-4432-8129-b4d37bcf1cb3.png" xlink:type="simple"/></inline-formula>were investigated as functions of the effect of <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\d6c93d3a-162a-4c41-8f41-8d7f9d4e8364.png" xlink:type="simple"/></inline-formula> and various values of <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\9c318c1f-5a69-4f37-809e-7e8d7d16813d.png" xlink:type="simple"/></inline-formula> <xref ref-type="fig" rid="fig4">Figure 4</xref> shows that the skin friction coefficient and Nusselt number increase with increase in<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\6c7e5119-342f-4050-9eea-18a32c57ef76.png" xlink:type="simple"/></inline-formula>. The skin friction coefficient increases linearly with <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\3349451e-1c3c-430d-a84a-a587b06010cf.png" xlink:type="simple"/></inline-formula> while the Nusselt number decreases with increase in<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\e66f2807-a541-4a24-8be1-a4352c0d16d3.png" xlink:type="simple"/></inline-formula>.</p><p>Similar results showing the effect of <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\7e6c9739-925d-4d5a-a1a2-862de59d6673.png" xlink:type="simple"/></inline-formula> on both the skin friction and the Nusselt number are presented in <xref ref-type="fig" rid="fig5">Figure 5</xref>. The results show that the skin friction increases linearly with increase in <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\af092fa2-5c26-42e7-ad67-0071196c0fda.png" xlink:type="simple"/></inline-formula> while the Nusselt number decrease with increase in<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\9136ff68-1a00-4569-a665-57992f90e3ed.png" xlink:type="simple"/></inline-formula>. On the other hand, increase <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\eb9d97e1-fd09-42c2-a0c7-abcc094484f3.png" xlink:type="simple"/></inline-formula> results in increase in the skin friction coeffi-</p><fig-group id="fig1"> <caption><title>Figure 1</title><p> The effect of varying <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\f3b622ef-8b7d-4828-9e0a-992707283fe1.png" xlink:type="simple"/></inline-formula> on (a) scaled stream-wise velocity <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\d52a7347-622b-44dd-8184-5af00f7b85e5.png" xlink:type="simple"/></inline-formula>and (b) viscosity <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\f6090a2a-6687-4196-820c-c79d18539cac.png" xlink:type="simple"/></inline-formula>for the case when<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\f3106037-321f-4970-83c0-bb7c4801dd01.png" xlink:type="simple"/></inline-formula></p></caption><fig id ="fig1_1"><label>(a)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\cda331db-d28a-489a-bb90-db9a7c912ae6.png"/></fig><fig id ="fig1_2"><label>(b)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\6c2f47c0-67ee-41ec-8fa7-1f4443727e2a.png"/></fig></fig-group><fig-group id="fig2"><caption><title>Figure 2</title><p> Effect of varying <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\d3d278ae-c808-430d-8f8f-2f611ac0cbcb.png" xlink:type="simple"/></inline-formula> on (a)<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\64d155cb-5edc-4d7d-be01-f5c2b7556eb7.png" xlink:type="simple"/></inline-formula>, (b) <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\3db391e1-27a8-4a67-8898-51ef9d0ca9d9.png" xlink:type="simple"/></inline-formula>and (c) <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\b164b406-2199-4657-998b-d7844f2cf35e.png" xlink:type="simple"/></inline-formula>for the case when <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\626621df-03f0-4eee-b08b-d09f1dca38c3.png" xlink:type="simple"/></inline-formula>  <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\e6c8b546-ce61-4602-945c-c21c00273cef.png" xlink:type="simple"/></inline-formula></p></caption><fig id ="fig2_1"><label>(a)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\9ddebcd6-06e5-44d3-b1b2-77ff8bdb039b.png"/></fig><fig id ="fig2_2"><label>(b) (c)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\bbfdd222-3919-4ea1-8e99-0d9e5479680d.png"/></fig><fig id ="fig2_3"><label>(b) (c)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\1d5c7808-d122-4bf0-b0a1-c82f2dd4eb61.png"/></fig></fig-group><fig-group id="fig3"> <caption><title>Figure 3</title><p> Effect of varying viscosity variation parameter <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\df51c53d-d224-419d-aab5-3a0ff942f736.png" xlink:type="simple"/></inline-formula> on (a) <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\eede90bf-5227-4727-ba20-405605843e71.png" xlink:type="simple"/></inline-formula>and (b) <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\a9390c22-909b-4b4d-8391-6cb4678563c3.png" xlink:type="simple"/></inline-formula>for the case when <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\2d1ab874-e129-4295-99a5-41ad3af311dc.png" xlink:type="simple"/></inline-formula>  <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\a928fd86-d731-4684-913c-1cf5bab311bb.png" xlink:type="simple"/></inline-formula></p></caption><fig id ="fig3_1"><label>(a)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\7b8310be-7972-43b2-8244-0ee14f3dc88a.png"/></fig><fig id ="fig3_2"><label>(b)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\cea62e06-4c93-426b-8c74-ecd4dccc15e4.png"/></fig></fig-group><fig-group id="fig4"> <caption><title>Figure 4</title><p> The effect of varying <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\98642ffb-b861-4e6d-b1d2-78b17f986992.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\3d19623f-c47d-41db-9dd3-3f9efa2901bc.png" xlink:type="simple"/></inline-formula> on the (a) skin friction coefficient and (b) Nusselt number for <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\f5d11943-00fc-4566-ab26-1f8e0ae04e06.png" xlink:type="simple"/></inline-formula>  <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\db16e806-a2dd-4714-ab2b-819292238850.png" xlink:type="simple"/></inline-formula></p></caption><fig id ="fig4_1"><label>(a)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\5fb772c4-fb18-4b5c-8e36-25b303cacba8.png"/></fig><fig id ="fig4_2"><label>(b)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\71152090-0de4-4e25-a945-364ec57d07c2.png"/></fig></fig-group><fig-group id="fig5"> <caption><title>Figure 5</title><p> The variation of (a) skin friction coefficient and (b) Nusselt number with <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\b7ca1bdc-4cd0-426f-a431-ddcada91f6bf.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\4c830e1c-fdfa-427a-a17e-6914fa6d9f12.png" xlink:type="simple"/></inline-formula>  <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\04e8a9ea-d66e-442f-ba63-97b84638105a.png" xlink:type="simple"/></inline-formula></p></caption><fig id ="fig5_1"><label>(a)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\10b1b478-be10-4e84-a9e0-71b99a16362d.png"/></fig><fig id ="fig5_2"><label>(b)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\7c46381e-95d0-4686-82f0-66d0c6dcc945.png"/></fig></fig-group><p>cient and a decrease in the Nusselt number. The results for the heat transfer coefficient indicate that at a fixed value of <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\87bd4fde-ba13-46c5-8271-eacc969073a6.png" xlink:type="simple"/></inline-formula> there is a critical value of <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\e7693bd6-3ed0-4582-bb04-cfe76882509c.png" xlink:type="simple"/></inline-formula> beyond which the heat transfer coefficient changes sign from positive (heat flows from fluid to the wall) to negative (heat flows from wall to the fluid in the boundary layer).</p></sec><sec id="s5"><title>5. Conclusions</title><p>A non-Darcy mixed convection boundary layer flow has been investigated. The results have shown that the non-similarity parameter<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-1720167x\372c1c36-7e7a-47c1-97e8-602e161582cb.png" xlink:type="simple"/></inline-formula>, which at particular stream-wise location represents thermal buoyancy, has the effect of accelerating the scaled free-stream velocity, resulting in super-velocities within the boundary layer. This effect is exacerbated by increasing viscous dissipation parameter and the viscosity variation parameter. The temperature dependent viscosity decreases with increase in buoyancy-related parameter and viscosity variation parameter but increases with increase in the viscous dissipation parameter.</p><p>The skin friction coefficient increases with increase in the viscosity variation parameter, the viscous dissipation parameter and the buoyancy-related parameter. For flows with viscous dissipation effects, there is a critical value of the buoyancy related parameter, above which the Nusselt number changes sign from positive (wall extracts heat from fluid) to negative (fluid extracts heat from wall).</p></sec><sec id="s6"><title>Acknowledgements</title><p>The author would like to thank the East African Universities Mathematics Programme (EAUMP) for their financial support.</p></sec></body><back><ref-list><title>References</title><ref id="scirp.47817-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">NIELD, D.A. AND BEJAN, A. (2006) CONVECTION IN POROUS MEDIA. SPRINGER AND BUSINESS MEDIA, NEW YORK.</mixed-citation></ref><ref id="scirp.47817-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">POP, I.I. AND INGHAM, D.B., EDS. (2001) CONVECTIVE HEAT TRANSFER: MATHEMATICAL AND COMPUTATIONAL MODELLING OF VISCOUS FLUIDS AND POROUS MEDIA. 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