<?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.2011.12003</article-id><article-id pub-id-type="publisher-id">WJM-4668</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>
 
 
  Visco-Elastic Boundary Layer Flow past a Stretching Plate and Heat Transfer with Variable Thermal Conductivity
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>aseem</surname><given-names>Ahmad</given-names></name><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><author-notes><corresp id="cor1">* E-mail:<email>naseem_mt@yahoo.com</email></corresp></author-notes><pub-date pub-type="epub"><day>19</day><month>04</month><year>2011</year></pub-date><volume>01</volume><issue>02</issue><fpage>15</fpage><lpage>20</lpage><history><date date-type="received"><day>February</day>	<month>11,</month>	<year>2011</year></date><date date-type="rev-recd"><day>March</day>	<month>6,</month>	<year>2011</year>	</date><date date-type="accepted"><day>March</day>	<month>11,</month>	<year>2011</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 the present paper, the boundary layer flow of Walters Liquid B Model over a stretching plate has been considered to solve heat flow problem with variable conductivity. First, using similarity transformation, the velocity components of velocity have been obtained. Then, the heat flow problem has been considered in two ways: 1) prescribed surface temperature (PST), and 2) prescribed stretching plate heat flux (PHF) in case of variable conductivity. Due to variable conductivity, temperature profile has its two part- one mean tempera-ture and other temperature profile induced due to variable conductivity. The related results have been dis-cussed with the help of graphs.
 
</p></abstract><kwd-group><kwd>Boundary Layer Flow</kwd><kwd> Similarity Solution</kwd><kwd> Variable Thermal Conductivity</kwd><kwd> Prandtl Number</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Due to number of applications in industrial manufacturing process, the problem of boundary layer flow past a stretching plate has attracted considerable attention of researchers during the past few decades. Examples of such technological process are hot rolling, wire drawing, glassfiber and paper production. In the process of drawing artificial fibers the polymer solution emerges from orifice with a speed which increases from almost zero at the orifice up to a plateau value at which it remains constant. The moving fiber, which is of great technical importance, is governed by the rate at which the fiber is cooled and this, in turn affects the final properties of the yarn. A number of works are presently available that follow the pioneering classical work of Sakiadis [<xref ref-type="bibr" rid="scirp.4668-ref1">1</xref>], F. K. Tsou, E. M. Sparrow, R. J. Goldstein [<xref ref-type="bibr" rid="scirp.4668-ref2">2</xref>] and Crane [<xref ref-type="bibr" rid="scirp.4668-ref3">3</xref>]. The following <xref ref-type="table" rid="table">Table </xref>lists some relevant works that pertain to cooling liquids, i.e., heat transfer for stretching surface:</p><p>There are liquid metals whose thermal conductivity varies with temperature in an approximately linear manner in the range from 0˚ F to 400˚ F. In 1996, T. C. Chiam [<xref ref-type="bibr" rid="scirp.4668-ref22">22</xref>] considered heat transfer problem with variable thermal conductivity in stagnation-point flow towards stretching sheet. N. Ahmad and K. Marwah [16,17] also studied boundary layer flow of Walters Liquid B Model with heat transfer for linear stretching plate with variable thermal conductivity numerically.</p><p>In almost all the flow problems over stretching sheet with heat transfer referred so far where closed form solution is obtained, the thermal conductivity of liquid has been taken constant. In this paper, we try to solve the boundary layer flow of Walters Liquid B Model over a stretching plate and heat transfer with variable thermal conductivity in the following two cases:</p><p>1) prescribed surface temperature (PST), and 2) prescribed stretching plate heat flux (PHF). The temperature field has been obtained in each case and the effect on it, of Visco-elasticity and Prandtl number has been discussed graphically.</p></sec><sec id="s2"><title>2. Mathematical Formation and Solution</title><p>The problem considered here is the steady boundary layer flow due to a moving flat plate in a quiescent Walters Liquid B Model. The flow is two dimensional where x-axis is along the plane of moving plate and y-axis is normal to it, respectively. We assume that the surface is moving continuously with the velocity <img src="1-4900010\804fdaa2-84e3-45fe-abd5-9843defb4b75.jpg" /> in the positive x-direction. Under these assumptions, the boundary layer along moving plate is governed by the equations:</p><disp-formula id="scirp.4668-formula7070"><label>(1)</label><graphic position="anchor" xlink:href="1-4900010\bfb2afb0-9d8b-4459-a274-135b6e4109f3.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4668-formula7071"><label>(2)</label><graphic position="anchor" xlink:href="1-4900010\70d845bf-a191-425c-ae7e-235a882b6ca1.jpg"  xlink:type="simple"/></disp-formula><p>where u, the horizontal velocity component; v, the vertical velocity component;<img src="1-4900010\cf8e699a-36c3-4f60-a356-8a600a18cb69.jpg" />, the kinematic viscosity; k<sub>0</sub>, the coefficient of visco-elasticity The relevant boundary conditions are:</p><p><img src="1-4900010\2273fe11-d217-422a-b076-ee49bcfe36e5.jpg" /></p><p>Introducing the dimensionless variables</p><p><img src="1-4900010\309943f9-a64f-4e83-8c91-835cd46f9b72.jpg" /></p><p>the Equations (1) and (2) reduce to</p><disp-formula id="scirp.4668-formula7072"><label>(3)</label><graphic position="anchor" xlink:href="1-4900010\d8300a0b-eec8-4fe2-a61b-5382b863998e.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4668-formula7073"><label>(4)</label><graphic position="anchor" xlink:href="1-4900010\ad0f5b09-bd2a-4a01-8f79-c3d18d984524.jpg"  xlink:type="simple"/></disp-formula><p>where k<sub>1</sub>=<img src="1-4900010\d29e1d7e-b1b2-4e51-ae94-0600b230d91a.jpg" />with boundary conditions</p><disp-formula id="scirp.4668-formula7074"><label>(5)</label><graphic position="anchor" xlink:href="1-4900010\6694ffd6-5fb9-48c9-b7aa-15b757627803.jpg"  xlink:type="simple"/></disp-formula><p>where bar has been dropped for convenience.</p><p>Setting the similarity solution of the form<img src="1-4900010\73464220-58e9-4c7f-a5bb-74df0b9992a6.jpg" />, we have</p><disp-formula id="scirp.4668-formula7075"><label>(6)</label><graphic position="anchor" xlink:href="1-4900010\68de348b-8886-45f6-9ed6-0eee4166ef18.jpg"  xlink:type="simple"/></disp-formula><p>Putting u and v in the Equation (2), we have</p><disp-formula id="scirp.4668-formula7076"><label>(7)</label><graphic position="anchor" xlink:href="1-4900010\cd7e8e29-ebb1-4438-92b7-65d259e556c9.jpg"  xlink:type="simple"/></disp-formula><p>which is non-linear differential equation of order three.</p><p>The boundary conditions (5) reduce to</p><disp-formula id="scirp.4668-formula7077"><label>(8)</label><graphic position="anchor" xlink:href="1-4900010\8e79dfdc-65cd-4baf-8da5-6a7e76c84d53.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4668-formula7078"><label>(9)</label><graphic position="anchor" xlink:href="1-4900010\3560c718-8996-4b7d-a1f6-e1345acdb638.jpg"  xlink:type="simple"/></disp-formula><p>Boundary conditions suggest that the velocity function may be of the form <img src="1-4900010\a45bc320-cca3-4283-b6ea-d3cb59b5d830.jpg" /> where r is complex number with positive real part. Thus,</p><p><img src="1-4900010\0f2efa8a-9bfd-4ddf-b5cf-eb3e2edbfce3.jpg" /></p><p>Now, from the Equation (7), we get<img src="1-4900010\83f56e45-1c2b-442d-bab4-502a33f66684.jpg" />.</p><p>Therefore, the velocity components become as follows:</p><disp-formula id="scirp.4668-formula7079"><label>(8)</label><graphic position="anchor" xlink:href="1-4900010\bf84f04a-2479-41e5-862d-66cb2ae82ecd.jpg"  xlink:type="simple"/></disp-formula></sec><sec id="s3"><title>3. Heat Transfer Problem</title><p>In absence of viscous dissipation and heat generation, the energy equation for two dimensional heat flow is given by</p><disp-formula id="scirp.4668-formula7080"><label>(9)</label><graphic position="anchor" xlink:href="1-4900010\77d8e30e-b0da-471e-9562-c947e718344d.jpg"  xlink:type="simple"/></disp-formula><p>subject to boundary conditions</p><disp-formula id="scirp.4668-formula7081"><label>(10)</label><graphic position="anchor" xlink:href="1-4900010\123a0116-af00-4347-b926-82fa4a6ec208.jpg"  xlink:type="simple"/></disp-formula><p>where T<sub>P</sub> is plate temperature, T<sub>&#165;</sub> is temperature of surrounding fluid, C<sub>P</sub> is specific heat at constant pressure and k is thermal conductivity.</p><sec id="s3_1"><title>3.1. Case A: Prescribed Power Law Surface Temperature (PST)</title><p>Let the surface temperature be of the form</p><p><img src="1-4900010\b503d746-ccd4-4e8f-a19d-9f938d69faa5.jpg" /></p><p>while the temperature out side the dynamic region be<img src="1-4900010\a2daeee9-8df4-47b2-bb4c-3845f8061d17.jpg" />. Now, we define the dimensionless temperature by</p><p><img src="1-4900010\7ee5455e-3904-449c-b2ee-dc1da743566d.jpg" /></p><p>where<img src="1-4900010\78a783a2-0267-4274-95d2-51e42fdab849.jpg" />.</p><p>For liquid metals, it has been found that the thermal conductivity varies with temperature in an approximately linear manner in the range from 0˚ F to 400˚ F. Therefore, we assume k as <img src="1-4900010\8356a4ff-a7af-4005-9aef-5d2394c325e0.jpg" /> where<img src="1-4900010\d948756f-9e9a-4163-953c-9fcfd5f8f766.jpg" />.</p><p>Now, substituting u and v and changing the independent variable y to<img src="1-4900010\4105eec7-c27a-464b-b401-dc803a6e4fa3.jpg" />, we have</p><disp-formula id="scirp.4668-formula7082"><label>(11)</label><graphic position="anchor" xlink:href="1-4900010\c21301c5-142d-45f5-adeb-df0250ac86a4.jpg"  xlink:type="simple"/></disp-formula><p>with boundary conditions</p><disp-formula id="scirp.4668-formula7083"><label>(12)</label><graphic position="anchor" xlink:href="1-4900010\2c605b0e-cd81-4bb0-a8e9-19a2b9da205f.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4668-formula7084"><label>(13)</label><graphic position="anchor" xlink:href="1-4900010\2a0c6a81-0bca-4a43-b53e-cd79dc7f601c.jpg"  xlink:type="simple"/></disp-formula><p>From Equation (11), we note that the heat transfer takes place in two parts, that is, one part of heat transfer is due to temperature difference and the other part is due to variable thermal conductivity. We denote the first part by q<sub>m</sub> and second by q<sub>v</sub>. Thus, equating the terms independent of e and the terms involving e, we have</p><disp-formula id="scirp.4668-formula7085"><label>(14)</label><graphic position="anchor" xlink:href="1-4900010\27ddf5f5-99b2-4333-8d16-8468cb8d8b5a.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4668-formula7086"><label>(15)</label><graphic position="anchor" xlink:href="1-4900010\98348640-03a3-4aa9-9139-c64118c6bae1.jpg"  xlink:type="simple"/></disp-formula><p>and</p><disp-formula id="scirp.4668-formula7087"><label>(16)</label><graphic position="anchor" xlink:href="1-4900010\a41e8086-feea-46c3-8bf6-b440e6281ef1.jpg"  xlink:type="simple"/></disp-formula><p><img src="1-4900010\6f946855-46c2-4017-b004-adf4278d2fa7.jpg" />, <img src="1-4900010\c527ec1a-1b92-49c7-8626-31eeb1e1e761.jpg" />as <img src="1-4900010\641e992e-b0aa-432e-a2ad-30b28d82c18a.jpg" />(17)</p><p>The solution of the Equation (14) is</p><disp-formula id="scirp.4668-formula7088"><label>(18)</label><graphic position="anchor" xlink:href="1-4900010\4087ad94-2218-4c96-a20a-360eb2802dcd.jpg"  xlink:type="simple"/></disp-formula><p>Equation (17) is a non-linear differential equation of order two. Let the solution of this equation be of the form</p><p><img src="1-4900010\1b0344aa-b047-4565-9f23-3b2c19f86623.jpg" /></p><p>Putting this solution in the Equation (18), we have</p><disp-formula id="scirp.4668-formula7089"><label>(19)</label><graphic position="anchor" xlink:href="1-4900010\3a6cf92e-efef-4802-a4b4-d6e32982767b.jpg"  xlink:type="simple"/></disp-formula><p>The roots of this equation are 0 and 1/2. Therefore,</p><disp-formula id="scirp.4668-formula7090"><label>(20)</label><graphic position="anchor" xlink:href="1-4900010\d055e1d6-34d4-4d51-93e8-d94451aca5f1.jpg"  xlink:type="simple"/></disp-formula><p>The general solution (20) of the Equation (16) is real only when<img src="1-4900010\d6dbd21e-8f75-405c-9e95-b31310c33ab6.jpg" />. Therefore, the heat transfer due to variable thermal conductively takes place within the dynamic region<img src="1-4900010\58bbc09c-d4be-4593-9f56-f4f693b888a1.jpg" />. Hence, the boundary conditions (17) may be presented as</p><disp-formula id="scirp.4668-formula7091"><label>(21)</label><graphic position="anchor" xlink:href="1-4900010\51a32aff-88dd-4b60-8534-4075c00c3f3c.jpg"  xlink:type="simple"/></disp-formula><p>The solution (20) finally reduces to</p><disp-formula id="scirp.4668-formula7092"><label>(22)</label><graphic position="anchor" xlink:href="1-4900010\923ed1be-c2cc-42f6-9972-3bb9bd5cea58.jpg"  xlink:type="simple"/></disp-formula></sec><sec id="s3_2"><title>3.2. Case B: Prescribed Power Law Surface Heat Flux (PHF Case)</title><p>The power law heat flux on the surface of stretching plate is considered to be a quadratic power of x in the form</p><p><img src="1-4900010\42391961-65f9-46ad-8219-537f0451bb2e.jpg" />at <img src="1-4900010\268fd6b6-f216-458f-88e5-f12b67a0bea7.jpg" />(23)</p><p><img src="1-4900010\6d751589-7e51-4400-bdda-2ebced7ca194.jpg" />, as <img src="1-4900010\8bb7ddd3-dd8e-452d-bc12-dabeb33a7f13.jpg" />(24)</p><p>where D is a constant, k is the thermal conductivity. Now we define dimensionless temperature <img src="1-4900010\352469f5-ec87-4117-925d-8818f6d2e0c0.jpg" /> by</p><disp-formula id="scirp.4668-formula7093"><label>(25)</label><graphic position="anchor" xlink:href="1-4900010\333b180e-1103-46c7-9bdc-311c0e2b40e3.jpg"  xlink:type="simple"/></disp-formula><p>where</p><p><img src="1-4900010\60d38e06-55a4-4830-b072-867d65ce1103.jpg" />when <img src="1-4900010\36853e20-9919-4813-99c4-4e5db43f3f3a.jpg" /></p><p>and<img src="1-4900010\36c5de1a-a194-47df-ac95-4532c1abbb2b.jpg" />.</p><p>Writing the Equation (11) in terms of<img src="1-4900010\ae408e1f-7264-42dd-a0fa-55234a5ff07f.jpg" />, we get the following differential equation</p><disp-formula id="scirp.4668-formula7094"><label>(26)</label><graphic position="anchor" xlink:href="1-4900010\5f62f890-72cb-492d-9eff-e8667d5e8ed4.jpg"  xlink:type="simple"/></disp-formula><p>together with boundary conditions:</p><disp-formula id="scirp.4668-formula7095"><label>(27)</label><graphic position="anchor" xlink:href="1-4900010\c149c9ca-5cb6-4a60-8eb5-f7d944234337.jpg"  xlink:type="simple"/></disp-formula><p>Equating the terms independent of <img src="1-4900010\1291c52a-e4bc-4f5f-a3f9-dba2170fc7e5.jpg" /> and the terms involving <img src="1-4900010\092bc991-8665-4f67-8c11-9f3a4e4f116d.jpg" /> from Equation (26), we get the following two boundary value problems:</p><disp-formula id="scirp.4668-formula7096"><label>(28a)</label><graphic position="anchor" xlink:href="1-4900010\d543d8ac-366a-43e5-8e90-41810c7de97c.jpg"  xlink:type="simple"/></disp-formula><p><img src="1-4900010\3f8dcad0-cef6-4d0a-b08f-4dc5943f6494.jpg" />, <img src="1-4900010\02b6d094-69c0-4435-a0a6-9d0980c55d2a.jpg" />as <img src="1-4900010\dc976bbd-fbb1-4d44-96db-8a432a8c341f.jpg" />(28b)</p><p>and,</p><disp-formula id="scirp.4668-formula7097"><label>(29a)</label><graphic position="anchor" xlink:href="1-4900010\5d5f077d-0440-4f09-8ab4-246cb53a8cd1.jpg"  xlink:type="simple"/></disp-formula><p><img src="1-4900010\d7bd829d-85fa-4869-b505-153d7fdbc960.jpg" />, <img src="1-4900010\4ee2d2b7-5fe6-4866-a699-dea2ca624436.jpg" />as <img src="1-4900010\cbb1602f-2b4b-49f9-9965-62b3d3965b66.jpg" />(29b)</p><p>The solution of the Equation (28a) together with boundary conditions (28b) is given by</p><disp-formula id="scirp.4668-formula7098"><label>(30)</label><graphic position="anchor" xlink:href="1-4900010\324cb8a6-ba67-422a-9a24-ab0bce6407c6.jpg"  xlink:type="simple"/></disp-formula><p>The general solution of the Equation (29a) is</p><disp-formula id="scirp.4668-formula7099"><label>(31)</label><graphic position="anchor" xlink:href="1-4900010\27ba68df-61c4-45e2-adc0-7b88c72833a1.jpg"  xlink:type="simple"/></disp-formula><p>where C and D are arbitrary constants to be determined. Here, we observe that the dynamic region for this temperature field is <img src="1-4900010\8c47d4d7-4f8b-4d6e-a220-03e3119726ae.jpg" /> as it was in PST case. Therefore, the boundary conditions may be taken as</p><disp-formula id="scirp.4668-formula7100"><label>(32)</label><graphic position="anchor" xlink:href="1-4900010\5e9dc852-e3f7-4204-b798-34ab3a11380a.jpg"  xlink:type="simple"/></disp-formula><p>Hence finally the solution becomes</p><disp-formula id="scirp.4668-formula7101"><label>(32)</label><graphic position="anchor" xlink:href="1-4900010\2c1038af-f026-4d37-a3a9-3b724c0b0b14.jpg"  xlink:type="simple"/></disp-formula></sec></sec><sec id="s4"><title>4. Discussion and Results</title><p>A boundary layer flow of visco-elastic fluid (Walters Liquid B Model) over a stretching plate and heat transfer has been analyzed through out this paper. The boundary layer equations of momentum and heat transfer have been solved analytically. Two different analytical expressions have been obtained for dimensionless temperature fields for two general cases of boundary conditions namely 1) PST case, and 2) PHF respectively. The equation governing the induced temperature field due to variable thermal conductivity has been solved with modified boundary conditions in both the cases PST and PHF The related results have been discussed in the subsequent paragraphs in detail.</p><p><xref ref-type="fig" rid="fig1">Figure 1</xref> is a graph drawn for mean temperature field <img src="1-4900010\fea56e19-cc85-43d9-b44a-dc736a75a61e.jpg" /> versus <img src="1-4900010\f7c32b26-3b82-4898-bd70-d43d18854364.jpg" /> in PST case taking different values of visco-elastic parameter<img src="1-4900010\ab17287d-90d3-4335-ace0-b35409d44de2.jpg" />. It is observed that the temperature <img src="1-4900010\89ca115b-e92e-400d-b9ee-c13aec3579f7.jpg" /> at the surface of stretching plate is invariant with respect to physical parameters. Further, we observe that as we move away the stretching plate within dynamic region, the temperature field increases as viscoelastic parameter <img src="1-4900010\e049e646-e135-4f40-86f7-d796e762e93d.jpg" /> increases. Physically, when <img src="1-4900010\f929fa63-f33f-4b7f-9a6b-3d0e764de13f.jpg" /> increases, the fluid absorbs more heat which causes the increase of temperature.</p><p><xref ref-type="fig" rid="fig2">Figure 2</xref> exhibits variation pattern of mean temperature field q<sub>m</sub>(h) with regard to Prandtl number Pr in PST case. We notice that as Prandtl number Pr increases, the mean temperature decreases.</p><p><xref ref-type="fig" rid="fig3">Figure 3</xref> exhibits the variation pattern of induced temperature field q<sub>v</sub> in PST case. This temperature field is independent of k<sub>0</sub> and Pr. We see that the induced temperature decreases as we move away the plate. The variation pattern is represented by a parabolic curve having focus at h = 1. q<sub>v</sub> decreases as we move away the stretching plate and it becomes almost zero at h = 1 which end upper edge of boundary layer thickness.</p><p><xref ref-type="fig" rid="fig4">Figure 4</xref> is the graph of mean temperature field <img src="1-4900010\4516f9ce-f977-4a74-8ff8-49893ac1a1d8.jpg" /> versus <img src="1-4900010\2b7d41bb-2e09-4cbc-9361-b2a847634bea.jpg" /> in PHF case. Here we observe that this temperature field attains the maximum value at the surface of stretching plate which is more than PST case. The reason of this maximum value is that the direction of heat flow is from fluid to stretching plate. Temperature field is approaching to zero asymptotically. The variation pattern is almost same as in PST case.</p><p><xref ref-type="fig" rid="fig5">Figure 5</xref> shows the graph of <img src="1-4900010\34e59437-2c5a-47db-a45e-bf95c447ffbb.jpg" /> versus <img src="1-4900010\50b4d92a-3369-4ec3-87ee-f3071cdc5501.jpg" /> for the different values of Prandtl number Pr in PHF case. It has been observed that as Pr increases, temperature field decreases absolutely. Temperature field is tending to zero asymptotically.</p><p>Equation (32) represents the temperature field induced by variable thermal conductivity in PHF case. The geometry of this equation is parabola having focus at h = 1. This temperature field is independent of k<sub>1</sub> and Pr. We see that the induced temperature decreases as we move away the plate. It varies from maximum at the plate to zero at the upper end of boundary layer.</p><p>Putting k<sub>0</sub> = 0, we get the results due to Naseem Ahmad, Z. U. Siddiqui and M. K. Mishra [<xref ref-type="bibr" rid="scirp.4668-ref23">23</xref>].</p></sec><sec id="s5"><title>5. Conclusion</title><p>The boundary layer flow of Walters Liquid B over linear stretching plate has been studied together with heat transfer with variable thermal conductivity. The heat transfer has been studied by considering two cases: PST and PHS. The effect of visco-elasticity k<sub>0</sub> has been looked upon in the Figures 1 and 2. This paper is an extension of the work due to Naseem Ahmad, Z. U. Siddiqui and M. K. Mishra [<xref ref-type="bibr" rid="scirp.4668-ref23">23</xref>].</p></sec><sec id="s6"><title>REFERENCES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.4668-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">B. C. 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