<?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.2013.42050</article-id><article-id pub-id-type="publisher-id">AM-28204</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>
 
 
  Exact Solutions of a Power Law Fluid Model in Posttreatment Analysis of Wire Coating with Linearly Varying Boundary Temperature
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>ehan</surname><given-names>Ali Shah</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>Saeed</surname><given-names>Islam</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Abdul</surname><given-names>Majeed Siddiqui</given-names></name><xref ref-type="aff" rid="aff3"><sup>3</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Tahira</surname><given-names>Haroon</given-names></name><xref ref-type="aff" rid="aff4"><sup>4</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Department of Basic Sciences and Islamiat, University of Engineering and Technology, Peshawar, Pakistan</addr-line></aff><aff id="aff3"><addr-line>Department of Mathematics, Pennsylvania State University, York Campus, York, USA</addr-line></aff><aff id="aff4"><addr-line>Department of Mathematics, COMSATS Institute of Information Technology, Islamabad, Pakistan</addr-line></aff><aff id="aff2"><addr-line>Department of Mathematics, Abdul Wali Khan University, Mardan, Pakistan</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>mmrehan79@yahoo.com(EAS)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>22</day><month>02</month><year>2013</year></pub-date><volume>04</volume><issue>02</issue><fpage>330</fpage><lpage>337</lpage><history><date date-type="received"><day>April</day>	<month>19,</month>	<year>2012</year></date><date date-type="rev-recd"><day>January</day>	<month>11,</month>	<year>2013</year>	</date><date date-type="accepted"><day>January</day>	<month>18,</month>	<year>2013</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>
 
 
   In this paper, analysis of post-treatment of wire coating is presented. Coating material satisfies power law fluid model. Exact solutions for the velocity field, volume flow rate and average velocity are obtained. Moreover, the heat transfer results are presented for different cases of linearly varying on the boundaries. The variations of velocity, volume flow rate, radius of coated wire, shear rate and the force on the total wire are presented graphically and discussed. 
 
</p></abstract><kwd-group><kwd>Exact Solution; Wire Coating; Power Law Fluid Model; Linearly Varying Temperature at Boundaries</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The wire coating process is basically an extrusion operation in which either the molten polymer, in the form of tubing, is extruded continuously over axially moving wire, or the wire is pulled through the extruded molten polymer. Polymer extrudate is an important industrial process used for coating a wire for primary insulation of conducting wires with molten polymers for mechanical strength and environmental protection purposes. Wire coating have many application in the field of chemical and industrial engineering. Many authors have studied the wire coating phenomena.</p><p>&#160;</p><p>The basic concept of modeling the wire coating for viscous fluid is given in the books by Denn and middleman [1,2]. McKelvey [<xref ref-type="bibr" rid="scirp.28204-ref3">3</xref>] and Paton et al. [<xref ref-type="bibr" rid="scirp.28204-ref4">4</xref>] have analyzed the flow of Newtonian and power law fluid model in wire coating process, and obtained expressions for the flow rate, shear rate and the velocity distribution along the radial direction. Gagley and storey [<xref ref-type="bibr" rid="scirp.28204-ref5">5</xref>] provided numerical simulations for a Newtonian fluid in the form of dimensionless parameters characterizing the wire speed, die dimensions, radial position, shear rate, and melt viscosity. Akhter and Hashmi [6,7] have developed the mathematical model for wire coating using power law model and investigated the effect of the change in viscosity. A.M Siddiqui, T.Haroon and H. Khan [<xref ref-type="bibr" rid="scirp.28204-ref8">8</xref>] studied the wire coating extrusion in a pressure-type die in flow of third grade fluid. Fenner and Williams [<xref ref-type="bibr" rid="scirp.28204-ref9">9</xref>] carried out an analysis of the flow in the tapering section of a pressure type die. They obtained the numerical solutions for the pressure and velocity profiles in the die. M. Sajjid et al. [<xref ref-type="bibr" rid="scirp.28204-ref10">10</xref>] studied the wire coating with Oldroyd 8-constant fluid and gave the solution for velocity field in the series form.</p><p>The coated wire after leaving the die is effected by the quality of the material used in coating process, the wire drawing velocity and the temperature. There are very few disclosures presenting theoretical analysis of flow in the posttreatment process subsequent to the die.</p><p>The analysis of the drag flow of the coated polymer outside pressure die was carried out by Kasajima and Katsuhiko Ito [<xref ref-type="bibr" rid="scirp.28204-ref11">11</xref>]. They derived the expression for velocity and temperature field. Moreover, they found the volume flow rate, average velocity and discussed some cases for constant velocity and constant temperature on the boundaries. We work under the same geometry as by Masayuki Kasajima and Katsuhiko with the assumption that the polymer obeys the power law fluid model and derived the velocity field, volume flow rate, thickness of coated wire, average velocity, the force on the total wire surface and linearly varying temperature distribution in the direction of flow. As the posttreatment problem is mainly concern with temperature for cooling the coated wire therefore due to its importance and realization of physical problem we discussed some cases of linearly varying temperature for analysis of temperature distribution as follows:</p><p>• Temperature of the wire is constant while it is varying linearly on the surface of the coated wire.</p><p>• Temperature of the wire varying linearly while it is constant on the surface of the coated wire.</p><p>• Temperature of the wire and the surface of coated wire are varying linearly at the same temperature gradient.</p><p>The non-linear differential equations governing the model are made dimensionless and solved for velocity and temperature distribution. Theoretical analysis on the drag flow mechanism of polymer extrudate, in the heat treatment process, is presented.</p></sec><sec id="s2"><title>2. Basic Governing Equations</title><p>The basic equations governing the flow of an incompressible fluid with thermal effects are:</p><disp-formula id="scirp.28204-formula18871"><label>, (1)</label><graphic position="anchor" xlink:href="10-7400812\8482e4ae-252e-4a71-be47-29a054ff2dca.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.28204-formula18872"><label>, (2)</label><graphic position="anchor" xlink:href="10-7400812\aff859dc-c4a2-44d7-b90b-5ff61a2b938c.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.28204-formula18873"><label>(3)</label><graphic position="anchor" xlink:href="10-7400812\c2c0096a-1994-4316-a588-7d9e98f9f31d.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="10-7400812\e44be09f-71cf-4058-b1d9-ee859c0df238.jpg" /> is the velocity vector, <img src="10-7400812\2a674ea7-6bc4-40ac-bd18-67a50e09ef50.jpg" />is the constant density, <img src="10-7400812\6544123c-c015-4f67-9437-9959a39e53e5.jpg" />is the body force, <img src="10-7400812\23304e2f-2718-4525-8175-e5e32f2dc509.jpg" />is the Cauchy stress tensor, <img src="10-7400812\5b9e56c9-ad1a-42f4-9047-da660cee435f.jpg" />denote the material derivative, <img src="10-7400812\3dc6f9f8-07b5-4dc0-99a0-d51f7e11d7ab.jpg" />is the fluid temperature, <img src="10-7400812\c396a304-e2ef-470f-99b2-0c5a475da4dc.jpg" />is the thermal conductivity, <img src="10-7400812\95667488-1690-4cf4-b838-00f2c2d1cb48.jpg" />is the specific heat and <img src="10-7400812\0e8595ee-f49f-4bf6-a02d-8aac74b74971.jpg" /> is the gradient of velocity vector<img src="10-7400812\af3e6b74-a2b1-47fb-9305-86392bb3d8d6.jpg" />.</p><p>The Cauchy stress tensor <img src="10-7400812\71f815cd-6f1f-4295-97b5-478141ef3a9f.jpg" /> is defined as</p><disp-formula id="scirp.28204-formula18874"><label>, (4)</label><graphic position="anchor" xlink:href="10-7400812\720bfbf0-7652-4f5e-b504-2fcf78beb57a.jpg"  xlink:type="simple"/></disp-formula><p>In which <img src="10-7400812\3da193df-365a-4fbf-a593-1902f7c6005d.jpg" /> is the pressure, <img src="10-7400812\6d0e76f8-f20d-46ad-bf54-6889c7996a8d.jpg" />is the identity tensor and <img src="10-7400812\f2ccadf9-c198-429e-8c47-1fc1ca9712a7.jpg" /> is the extra stress tensor. For power law fluid model <img src="10-7400812\e943b4fd-2ab8-45ee-86eb-85e732ae957a.jpg" /> is defined as</p><p><img src="10-7400812\32dd7cdc-f2f7-4e55-93fe-49b4194f4400.jpg" /><img src="10-7400812\23158e88-e263-424b-9599-bdf673baa828.jpg" />, (5)</p><p>where</p><disp-formula id="scirp.28204-formula18875"><label>(6)</label><graphic position="anchor" xlink:href="10-7400812\4b3f7cd6-16ae-4d80-b508-f77d0190ffd8.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="10-7400812\98559b71-d0d8-407d-b68a-4f4758ad138d.jpg" /> is the scalar invariant, <img src="10-7400812\f1ce860d-bae9-4e25-8975-6c21eeb85370.jpg" />is the coefficient of viscosity of the fluid, <img src="10-7400812\b4e0ad0e-94fd-4ac5-9fcc-8b33eeefa276.jpg" />in superscript denotes the transpose of the matrix<img src="10-7400812\f49bae85-4f5d-4693-b9c6-8f4b81493bc3.jpg" />, <img src="10-7400812\544aa272-1553-4429-b3c7-8fcaeeb11361.jpg" />is the consistency index and <img src="10-7400812\30c097e3-d299-4139-8aae-d3510e9f7f88.jpg" /> is the power law index. The index <img src="10-7400812\b07cf683-3aa5-472a-908c-1b6f7e268a6a.jpg" /> is non-dimensional and the dimension of <img src="10-7400812\8a1c6364-ec80-4333-8c9b-61ed2d7febf7.jpg" /> depends on the value of<img src="10-7400812\14bd688b-6756-4dc9-aa71-6b0d16a61e19.jpg" />. The parameter <img src="10-7400812\88a5d55e-9188-4b0f-8f33-704405740797.jpg" /> subdivide fluids into pseudoplastic fluids<img src="10-7400812\56ae76d0-468f-4061-b9bc-9935888ed5cc.jpg" />, dilatant fluids<img src="10-7400812\35be0c4a-53f6-46a3-9089-7d18f6c87663.jpg" /> and Newtonian fluid For<img src="10-7400812\2d90c947-2d9c-4e0c-9faa-fe28bcd735ae.jpg" />. Therefore the deviation of <img src="10-7400812\ecb900e2-e49f-412b-85af-e280ba9c314b.jpg" /> from unity indicates the degree of deviation from Newtonian behavior [<xref ref-type="bibr" rid="scirp.28204-ref12">12</xref>].</p></sec><sec id="s3"><title>3. Formulation and Solution of the Problem</title><p>In wire coating process, the quality of the polymer and wire drawing velocity are important within the die, after leaving the die temperature and the shape of the transverse sectioning is also very important. Consider the flow of the polymer extrudate given in <xref ref-type="fig" rid="fig1">Figure 1</xref>, denoted by the solid line. To analyze the flow behavior of a polymer used in wire coating, it is convenient to divide the flow transversely into many short sections as shown by broken lines in <xref ref-type="fig" rid="fig1">Figure 1</xref> with the assumption that each section has almost the same shape, we analyze only one section because each section can be assumed to be approximately of the shape shown in <xref ref-type="fig" rid="fig2">Figure 2</xref> and readily analyzable.</p><p>Consider the wire of radius <img src="10-7400812\37b4953c-8aba-4b2a-a6d5-10112234ffcc.jpg" /> is dragged in the <img src="10-7400812\a3cd5e49-5e0e-4b93-bba8-8995b79f2798.jpg" /> direction with velocity <img src="10-7400812\17d6c13d-c24a-4e34-88f8-8286a3b9c9ed.jpg" /> through an incompressible polymer satisfying power law fluid model (II) and the gas (III) surrounding the polymer (II) is flowing with a velocity <img src="10-7400812\4fa5dabc-1285-4e8d-adda-24ccb42339e7.jpg" />in the <img src="10-7400812\e4848c6e-fe75-49cc-99ee-5195245ae7db.jpg" /> direction.</p><p>Consider the cylindrical coordinates <img src="10-7400812\04b11a37-b496-4d33-854e-451e826f1542.jpg" /> such that <img src="10-7400812\81dbbd47-b5bc-4f86-b618-18862fc8108c.jpg" /> is perpendicular to the direction of flow.</p><p>Assume that:</p><p>1) The flow is incompressible due to the high viscosity of the polymer.</p><p>2) Polymer II holds the power law fluid model for shear rate.</p><p>3) In <xref ref-type="fig" rid="fig2">Figure 2</xref> the wire I, the polymer II and gas III are in contact with each other and consider no slippage occurs along the contacting surfaces of the wire, polymer, and the gas.</p><p>Also assume that the flow is steady, laminar, unidirectional and axisymmetric:</p><p>We seek the velocity field of the form</p><disp-formula id="scirp.28204-formula18876"><label>. (7)</label><graphic position="anchor" xlink:href="10-7400812\1df1c52a-1861-4265-a3e7-4677406fec0b.jpg"  xlink:type="simple"/></disp-formula><p>then the boundary conditions for the problem become</p><disp-formula id="scirp.28204-formula18877"><label>(8)</label><graphic position="anchor" xlink:href="10-7400812\c63183b0-b4af-45bf-8ee8-4defad551366.jpg"  xlink:type="simple"/></disp-formula><p>In the flow through the tube, the scalar invariant is:</p><disp-formula id="scirp.28204-formula18878"><label>(9)</label><graphic position="anchor" xlink:href="10-7400812\f3ffb5c8-b868-478f-8722-5647fc296db4.jpg"  xlink:type="simple"/></disp-formula><p>Substituting Equation (9) into Equation (6) one obtains:</p><disp-formula id="scirp.28204-formula18879"><label>. (10)</label><graphic position="anchor" xlink:href="10-7400812\79ebab9a-49d0-4f2f-9270-c4ec03f75efe.jpg"  xlink:type="simple"/></disp-formula><p>Using the velocity field (7) the continuity Equation (1) is satisfied identically, and the non zero components of Equation (5) with the help of Equation (10) become:</p><disp-formula id="scirp.28204-formula18880"><label>(11)</label><graphic position="anchor" xlink:href="10-7400812\3755775e-510e-437d-a846-f7273046b227.jpg"  xlink:type="simple"/></disp-formula><p>Substituting the velocity field and Equation (11) in the momentum Equation (2) neglecting the body force take the form:</p><disp-formula id="scirp.28204-formula18881"><label>(12)</label><graphic position="anchor" xlink:href="10-7400812\427a12d1-cf74-456c-a039-2e68dff6611b.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.28204-formula18882"><label>(13)</label><graphic position="anchor" xlink:href="10-7400812\bbe06944-a15a-41fc-8b3a-19f21363606e.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.28204-formula18883"><label>(14)</label><graphic position="anchor" xlink:href="10-7400812\7dc9314d-69ea-444e-887d-303cd100b332.jpg"  xlink:type="simple"/></disp-formula><p>If the z-axis is chosen correspond to the direction of increasing pressure, polymer (II) moves in the minus direction of the z-axis and the shear rate<img src="10-7400812\ad24c160-ff3b-47eb-a9f9-fb485905915e.jpg" />becomes plus for all value of <img src="10-7400812\b76a3255-836d-4faa-82b9-56c448162f1c.jpg" /> Therefore, the absolute value of Equation (5) can be discarded.</p><p>Equation (14) represents the flow due to pressure gradient. After leaving the die, there is only drag flow. Hence, we consider</p><disp-formula id="scirp.28204-formula18884"><label>(15)</label><graphic position="anchor" xlink:href="10-7400812\f442f775-d14b-497a-8038-e8c6eb6b5bd3.jpg"  xlink:type="simple"/></disp-formula><p>and the energy Equation (3) becomes:</p><disp-formula id="scirp.28204-formula18885"><label>(16)</label><graphic position="anchor" xlink:href="10-7400812\9ae165cb-3881-4872-ab6d-4daf74a16d36.jpg"  xlink:type="simple"/></disp-formula><p>For linearly varying temperature, consider</p><disp-formula id="scirp.28204-formula18886"><label>, (17)</label><graphic position="anchor" xlink:href="10-7400812\f9237705-5cff-4ca1-b09c-dc2aa4f59f77.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="10-7400812\de88cbb0-3408-44c2-b449-7f5a2265942e.jpg" /> is the temperature gradient.</p><p>Substituting Equation (17) into Equation (16), we have</p><disp-formula id="scirp.28204-formula18887"><label>(18)</label><graphic position="anchor" xlink:href="10-7400812\edaa2f4d-71da-4520-9145-18ca2f416ef6.jpg"  xlink:type="simple"/></disp-formula><p>Now first the velocity field is determined from Equation (15) and then the temperature distribution can be easily calculated using Equation (18).</p><p>The average velocity is</p><disp-formula id="scirp.28204-formula18888"><label>(19)</label><graphic position="anchor" xlink:href="10-7400812\71b9d501-4f39-4492-b7c1-a98e1899baf0.jpg"  xlink:type="simple"/></disp-formula><p>At some control surface downstream, the volume flow rate of coating is</p><disp-formula id="scirp.28204-formula18889"><label>(20)</label><graphic position="anchor" xlink:href="10-7400812\e030c14c-5219-4704-ab57-c4e7f02c0a4c.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="10-7400812\be97e685-5281-42f3-a793-fadea7715432.jpg" /> is the radius of the coated wire.</p><p>The volume flow rate of the polymer is</p><disp-formula id="scirp.28204-formula18890"><label>(21)</label><graphic position="anchor" xlink:href="10-7400812\d96a0b9a-9e5b-424e-b918-f17761c85b96.jpg"  xlink:type="simple"/></disp-formula><p>The thickness of the coated wire can be obtained from Equations (16) and (17) as</p><disp-formula id="scirp.28204-formula18891"><label>(22)</label><graphic position="anchor" xlink:href="10-7400812\43ce6323-e12c-4426-a3db-07f3ae6687c5.jpg"  xlink:type="simple"/></disp-formula><p>The force on the wire is computed by determining the shear stress at the wire surface. This is given by</p><disp-formula id="scirp.28204-formula18892"><label>(23)</label><graphic position="anchor" xlink:href="10-7400812\ce09147a-7b8d-4572-98e5-7455bbfef77b.jpg"  xlink:type="simple"/></disp-formula><p>The force on the total wire surface is</p><disp-formula id="scirp.28204-formula18893"><label>(24)</label><graphic position="anchor" xlink:href="10-7400812\2a163694-6e49-403a-a6bf-2a8a8c387b7f.jpg"  xlink:type="simple"/></disp-formula><p>Introduce the dimensionless parameters</p><disp-formula id="scirp.28204-formula18894"><label>(25)</label><graphic position="anchor" xlink:href="10-7400812\aaf2fd19-04e8-49b6-a525-59e59867bee8.jpg"  xlink:type="simple"/></disp-formula><p>Equations (8), (15) and (18)-(25) after dropping the “<img src="10-7400812\41b2991b-3035-4825-ae8d-0b3b5d8bf394.jpg" />” take the following form:</p><disp-formula id="scirp.28204-formula18895"><label>, (26)</label><graphic position="anchor" xlink:href="10-7400812\34817bcf-6a89-4013-a46a-3c39d2fb7d12.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.28204-formula18896"><label>, (27)</label><graphic position="anchor" xlink:href="10-7400812\198358f4-2deb-4389-88f9-33b961306511.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.28204-formula18897"><label>, (28)</label><graphic position="anchor" xlink:href="10-7400812\73d4e979-27b4-494c-a2b7-e99d5839a00c.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.28204-formula18898"><label>, (29)</label><graphic position="anchor" xlink:href="10-7400812\65cf2446-b3cb-4e8f-9a6e-6954fd32b9bc.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.28204-formula18899"><label>, (30)</label><graphic position="anchor" xlink:href="10-7400812\9ce4ac7e-40a1-4acf-9d89-d6877e27a5a0.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.28204-formula18900"><label>(31)</label><graphic position="anchor" xlink:href="10-7400812\004bf1c7-e082-4a47-8480-a12edfe3fb53.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.28204-formula18901"><label>(32)</label><graphic position="anchor" xlink:href="10-7400812\dfa38893-1027-4481-a1d0-58a2766b56a1.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.28204-formula18902"><label>(33)</label><graphic position="anchor" xlink:href="10-7400812\4ed1fde8-ed03-4da2-bc5a-7647ac691d07.jpg"  xlink:type="simple"/></disp-formula><p>The solution to (26) corresponding to the boundary conditions (27) are:</p><disp-formula id="scirp.28204-formula18903"><label>(34)</label><graphic position="anchor" xlink:href="10-7400812\dcaa30f1-521b-4109-92f2-67c0d7d5c5f6.jpg"  xlink:type="simple"/></disp-formula><p>For<img src="10-7400812\966ce00c-e15d-4620-9cf5-7a358516b401.jpg" />, the velocity field can be obtain from Equation (26).</p><disp-formula id="scirp.28204-formula18904"><label>(35)</label><graphic position="anchor" xlink:href="10-7400812\f1da6665-acad-4e12-8260-8267fcd40e58.jpg"  xlink:type="simple"/></disp-formula><p>where the superscript “<img src="10-7400812\791733dc-8531-44bf-abe9-ca36d1e56676.jpg" />” means the case of<img src="10-7400812\dbf1382b-7bec-4c4f-bbb7-300910b08a4c.jpg" />.</p><p>For <img src="10-7400812\3ab61a77-f062-4dae-a414-adb3beed8381.jpg" />the average velocity is obtained from Equations (29) and (34):</p><disp-formula id="scirp.28204-formula18905"><label>(36)</label><graphic position="anchor" xlink:href="10-7400812\27100fd5-208a-4d78-8680-f7cc2c5e9562.jpg"  xlink:type="simple"/></disp-formula><p>For <img src="10-7400812\00d6df1c-1c85-41c4-b4b3-f4db321a0e40.jpg" /> the average velocity is obtained from Equations (29) and (35):</p><disp-formula id="scirp.28204-formula18906"><label>(37)</label><graphic position="anchor" xlink:href="10-7400812\7df14841-64e1-4ce1-862a-93560d836b45.jpg"  xlink:type="simple"/></disp-formula><p>For <img src="10-7400812\a9cd4533-2652-40fe-b546-aa3a7e069b70.jpg" /> the shear rate can be obtained from Equation (34):</p><disp-formula id="scirp.28204-formula18907"><label>(38)</label><graphic position="anchor" xlink:href="10-7400812\0cecc669-9e39-4d4b-82c9-6e82efbd94f6.jpg"  xlink:type="simple"/></disp-formula><p>For <img src="10-7400812\eb3b8733-d677-428c-abe5-d770b0b94b82.jpg" /> the shear rate is obtained from Equation (35) as:</p><disp-formula id="scirp.28204-formula18908"><label>(39)</label><graphic position="anchor" xlink:href="10-7400812\798a5df6-488e-4adf-9a72-998250a9c31b.jpg"  xlink:type="simple"/></disp-formula><p>The thickness of the coated wire for <img src="10-7400812\201f1623-c1cc-4530-835f-432290a0c02a.jpg" /> is obtained from Equations (31) and (34):</p><disp-formula id="scirp.28204-formula18909"><label>(40)</label><graphic position="anchor" xlink:href="10-7400812\e545c891-b88f-45e1-95e7-6985b0201242.jpg"  xlink:type="simple"/></disp-formula><p>Similarly, the thickness of the coated wire for <img src="10-7400812\bd2d8cd2-f69c-4522-92d2-93e0e1bc59f2.jpg" /> is obtained from Equations (31) and (35):</p><disp-formula id="scirp.28204-formula18910"><label>(41)</label><graphic position="anchor" xlink:href="10-7400812\1c70835d-2229-40b4-b594-652bd43a952a.jpg"  xlink:type="simple"/></disp-formula><p>In a similar manner, the force on the total wire surface for power law index <img src="10-7400812\b605cbf5-c718-43c0-8b56-5a6445cac1b9.jpg" /> is not equal to 1 is</p><disp-formula id="scirp.28204-formula18911"><label>, (42)</label><graphic position="anchor" xlink:href="10-7400812\17d75c00-6d1f-4a69-94a3-af9396a366e3.jpg"  xlink:type="simple"/></disp-formula><p>and the force on the total wire surface for the case when the power law index <img src="10-7400812\6c36d183-c310-4b7c-a6ba-5d8b13c91aac.jpg" /> is equal to 1 is given by</p><disp-formula id="scirp.28204-formula18912"><label>. (43)</label><graphic position="anchor" xlink:href="10-7400812\1f6c6d42-ce9a-4b41-bd2d-655a39b75e2a.jpg"  xlink:type="simple"/></disp-formula><p>In dimensionless form the volume flow rate for <img src="10-7400812\4b3d7529-f664-4c9e-89bb-05a3380fc49e.jpg" /> is or is not equal to 1are the same as the average velocity in Equations (37) and (36) respectively.</p><p>In case of transformation of our problem to original parameters the results of velocity field, volume flow rate, average velocity and rate of shear stress are transformed to the results of Kasajima and Katsuhiko Ito [<xref ref-type="bibr" rid="scirp.28204-ref11">11</xref>] for <img src="10-7400812\5c22dd27-e518-41ab-83c3-c35403b4d336.jpg" /> is or is not equal to 1.</p><p><xref ref-type="fig" rid="fig3">Figure 3</xref> illustrates the well known effect of <img src="10-7400812\b5865b61-9808-4511-a582-3ad4622a6903.jpg" /> on the velocity profile; i.e. for pseudoplastic the profile becomes progressively flatter; and for dilatant fluids the profile becomes progressively linear.</p><p>Keeping the importance of temperature in our problem we are seeking the temperature distribution with different cases.</p><p>Case 1. Temperature of the wire is constant while it is varying linearly on the surface of the coated wire:</p><p>Here, consider the temperature of the wire is<img src="10-7400812\f22066a8-08aa-4644-890c-e204a576ba83.jpg" />, and it is <img src="10-7400812\ca9c53bd-aef2-4d81-b077-d9e19b3e8ba5.jpg" /> on the surface of the coated wire, so from Equation (17) we have</p><disp-formula id="scirp.28204-formula18913"><label>(44)</label><graphic position="anchor" xlink:href="10-7400812\6dd9db98-c0b7-4ad3-8506-53a7c2c30f2b.jpg"  xlink:type="simple"/></disp-formula><p>After transformation we obtain</p><disp-formula id="scirp.28204-formula18914"><label>(45)</label><graphic position="anchor" xlink:href="10-7400812\7ed34806-ef62-4c39-a770-c43da0552c6f.jpg"  xlink:type="simple"/></disp-formula><p>where</p><p><img src="10-7400812\ea921e76-56c9-4cb8-9df2-37b1db4f217f.jpg" />.</p><p>For <img src="10-7400812\08fe30e5-d5be-45ef-9dba-da0788b666c2.jpg" /> the velocity field from Equation (23) is substitute in Equation (22) and solved corresponding to the boundary conditions (45), we obtain the expression for temperature distribution in form of <img src="10-7400812\d38c6666-c2ce-4bb3-9403-414181eb11c1.jpg" /> as:</p><disp-formula id="scirp.28204-formula18915"><label>(46)</label><graphic position="anchor" xlink:href="10-7400812\3556b1a6-1f57-4972-b89d-91b4fbf99b8b.jpg"  xlink:type="simple"/></disp-formula><p>For <img src="10-7400812\279892e6-2ae9-4390-8876-6f2aee26168e.jpg" /> the velocity field from Equation (24) is substitute in Equation (22) and solved corresponding to the boundary conditions (45), the explicit function for <img src="10-7400812\5ae9e1e1-949c-4e56-a018-7b0aeb189a7f.jpg" /> is obtained for temperature field as:</p><disp-formula id="scirp.28204-formula18916"><label>(47)</label><graphic position="anchor" xlink:href="10-7400812\96b0a347-9473-4e5c-933c-369a335a637f.jpg"  xlink:type="simple"/></disp-formula><p>Case 2. Temperature of the wire varying linearly while it is constant on the surface of the coated wire:</p><p>In this case, consider the temperature at the surface of wire is<img src="10-7400812\b3850e37-2ac8-4cdc-8b7b-cdd14314dd90.jpg" />, and <img src="10-7400812\a081904b-3861-424f-81bf-a87eddbda58a.jpg" /> on the surface of continuum.</p><p>Under the above consideration Equation (17) gives</p><disp-formula id="scirp.28204-formula18917"><label>(48)</label><graphic position="anchor" xlink:href="10-7400812\e92c06ec-bd79-49f5-87cf-d9f9665e6864.jpg"  xlink:type="simple"/></disp-formula><p>After transformation of the boundary conditions (48) for the non-dimensional temperature distribution <img src="10-7400812\02eacd44-6194-46c6-956e-861e205eea48.jpg" /> takes the following form</p><disp-formula id="scirp.28204-formula18918"><label>(49)</label><graphic position="anchor" xlink:href="10-7400812\574aa93e-163d-4c7a-a03e-9c7e4865ee55.jpg"  xlink:type="simple"/></disp-formula><p>where</p><p><img src="10-7400812\38e542c4-a308-45a3-ba91-d894c997ba81.jpg" />.</p><p>For <img src="10-7400812\43761288-0218-4ce2-b46f-c053053bed40.jpg" /> the velocity field from Equation (22) is substitute in Equation (22) and solved corresponding to the boundary conditions (49), we have</p><disp-formula id="scirp.28204-formula18919"><label>(50)</label><graphic position="anchor" xlink:href="10-7400812\c046c626-87e4-49b7-8244-0234ef660a96.jpg"  xlink:type="simple"/></disp-formula><p>For <img src="10-7400812\2ece02ef-0907-4cb4-a855-94f8a2ba13d3.jpg" /> the velocity field from Equation (24) is substitute in Equation (22) and solved corresponding to the boundary conditions (49), we have</p><disp-formula id="scirp.28204-formula18920"><label>(51)</label><graphic position="anchor" xlink:href="10-7400812\e6c7c911-9851-4151-a686-386fda1742b7.jpg"  xlink:type="simple"/></disp-formula><p>Case 3. Temperature of the wire and the surface of coated wire are varying linearly at the same temperature gradient:</p><p>Consider the temperatures at the surface of wire and on the surface of continuum are<img src="10-7400812\afef1800-2e48-4f83-b244-d9ab7257f136.jpg" />.</p><p>From Equation (17), we have</p><disp-formula id="scirp.28204-formula18921"><label>(52)</label><graphic position="anchor" xlink:href="10-7400812\d57e3718-78d8-4784-8fd5-e06b5868ee19.jpg"  xlink:type="simple"/></disp-formula><p>After simplification according to demand of our problem, we obtain</p><disp-formula id="scirp.28204-formula18922"><label>(53)</label><graphic position="anchor" xlink:href="10-7400812\2e018bee-ecf6-46d5-b352-5c088af97fd1.jpg"  xlink:type="simple"/></disp-formula><p>For <img src="10-7400812\62463832-c0e0-4903-ba9a-431a146c5e78.jpg" /> the velocity field from Equation (22) is substitute in Equation (22) and solved corresponding to the boundary conditions (53), we have</p><disp-formula id="scirp.28204-formula18923"><label>(54)</label><graphic position="anchor" xlink:href="10-7400812\105db739-507a-47f0-92fe-5b6bbf5806a1.jpg"  xlink:type="simple"/></disp-formula><p>For <img src="10-7400812\437851cf-3575-47da-b31a-f5dbdb66dcf8.jpg" /> the velocity field from Equation (24) is substitute in Equation (22) and solved corresponding to the boundary conditions (53), after simplification we have</p><disp-formula id="scirp.28204-formula18924"><label>(55)</label><graphic position="anchor" xlink:href="10-7400812\50e1ba5d-d91f-4b9c-bea8-22c374918942.jpg"  xlink:type="simple"/></disp-formula></sec><sec id="s4"><title>4. Conclusion</title><p>The posttreatment of wire coating analysis are carried out for power law model fluid. The velocity field, volume flow rate, average velocity, force on the total wire, thickness of coated wire and shear rate have been derived for <img src="10-7400812\9c5fea58-fe03-4f68-bb4d-09f9059e88a4.jpg" /> is or is not equal to 1. In posttreatment problem the temperature is extremely important for cooling the wire. Therefore, regarding the importance of temperature we have discussed three cases for linearly varying temperature. Expression for temperature distributions in non-dimensional form are obtained for <img src="10-7400812\45974cda-f062-427d-90b9-90eaddb9bca0.jpg" /> and<img src="10-7400812\eee8653e-b80f-4015-9764-8d3527057525.jpg" />. The interpretations of the results are carried out under the influence of non-dimensional parameters. It is concluded that the velocity decreases as the power law index <img src="10-7400812\bb960add-1f01-41ea-899a-80f580ff6f6a.jpg" /> increases. In addition, the non-Newtonian parameter<img src="10-7400812\223a8528-6516-4c15-ba76-112118402a2d.jpg" /> decrease the fluid velocity. Also, it is concluded that the force on the coated wire increases as the velocity ratio increases and decreases while increases<img src="10-7400812\50c61e0c-ceed-4c12-a71d-70cb84304d1d.jpg" />. It is observed that for <img src="10-7400812\90513144-f2c7-440d-af75-7916d353a905.jpg" /> the thickness of coated wire increases. Moreover, with a linearly varying wall temperature along the direction of flow the highest temperature rise in the centre of the channel depends on the dimensionless number<img src="10-7400812\ec1b304f-2c47-42c8-bb3c-d584401260a2.jpg" />. One can see the behavior of the physical quantities such as velocity function, non-dimensional function of temperature profile and the differential form of these functions from Figures 3-15.</p></sec><sec id="s5"><title>5. Acknowledgements</title><p>The first author is thankful to higher education commission of Pakistan for funding in MS leading to PhD studies under the 5000 indigenous scholarship scheme BatchIV.</p></sec><sec id="s6"><title>REFERENCES</title></sec><sec id="s7"><title>NOTES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.28204-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">M. M. Denn, “Process Fluid Mechanics,” Prentice-Hall, Upper Saddle River, 1980.</mixed-citation></ref><ref id="scirp.28204-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">S. 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