<?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.2013.43081</article-id><article-id pub-id-type="publisher-id">AM-29098</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>
 
 
  MHD Slip Flow past a Shrinking Sheet
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>antosh</surname><given-names>Chaudhary</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>Pradeep</surname><given-names>Kumar</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Malaviya National Institute of Technology, Jaipur, Rajasthan, India</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>d11.santosh@yahoo.com(AC)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>21</day><month>03</month><year>2013</year></pub-date><volume>04</volume><issue>03</issue><fpage>574</fpage><lpage>581</lpage><history><date date-type="received"><day>November</day>	<month>28,</month>	<year>2012</year></date><date date-type="rev-recd"><day>January</day>	<month>18,</month>	<year>2013</year>	</date><date date-type="accepted"><day>January</day>	<month>26,</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>
 
 
   An analysis is made for the steady two-dimensional laminar boundary layer flow of a viscous, incompressible, electrically conducting fluid near a stagnation point past a shrinking sheet with slip in the presence of a magnetic field. The governing boundary layer equations are transformed to ordinary differential equations by taking suitable similarity variables and solved numerically by Shooting method. The effects of the various parameters such as velocity ratio parameter, slip parameter, Prandtl number, Eckert number and magnetic parameter for velocity and temperature distributions have been discussed in detail through graphical representation. 
 
</p></abstract><kwd-group><kwd>MHD; Boundary Layer; Slip Flow; Shrinking Sheet</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The viscous flow and heat transfer in the boundary layer region due to a stretching sheet has wide theoretical and technical applications in manufacturing process and in industries such as extraction of polymer sheet, paper production, wire drawing, glass-fiber production, the cooling and drying of paper and textiles. The study of heat transfer and flow field is necessary for determining the quality of the final products of such process. Crane [<xref ref-type="bibr" rid="scirp.29098-ref1">1</xref>] was first who considered steady boundary layer flow of a viscous incompressible fluid over a linearly stretching plate and gave an exact similarity solution in closed analytical form. The effects of heat and mass transfer and magnetic field under various physical conditions have been investigated by several authors such as Chen and Char [<xref ref-type="bibr" rid="scirp.29098-ref2">2</xref>], Chiam [<xref ref-type="bibr" rid="scirp.29098-ref3">3</xref>], Andersson [<xref ref-type="bibr" rid="scirp.29098-ref4">4</xref>], Ariel et al. [<xref ref-type="bibr" rid="scirp.29098-ref5">5</xref>], Jat and Chaudhary [6,7], Wang [<xref ref-type="bibr" rid="scirp.29098-ref8">8</xref>], Fang et al. [<xref ref-type="bibr" rid="scirp.29098-ref9">9</xref>], Nadeem et al. [<xref ref-type="bibr" rid="scirp.29098-ref10">10</xref>], Bhattacharyya and Layek [<xref ref-type="bibr" rid="scirp.29098-ref11">11</xref>] and recently Bhattacharyya et al. [<xref ref-type="bibr" rid="scirp.29098-ref12">12</xref>] studied the slip effects on boundary layer stagnation-point flow and heat transfer towards a shrinking sheet.</p><p>Based on the above mentioned investigations and applications, this paper is concerned with a steady, two dimensional stagnation flow of an electrically conducting fluid past a shrinking sheet in the presence of a magnetic field. The results of velocity and temperature distributions for different parameters such as the velocity ratio parameter, the slip parameter, the Prandtl number, the Eckert number and the magnetic parameter were obtained.</p></sec><sec id="s2"><title>2. Formulation of the Problem</title><p>Consider the steady two-dimensional laminar flow of a viscous incompressible electrically conducting fluid towards a linearly shrinking sheet such that the sheet is shrinked in its own plane with velocity proportional to the distance from the stagnation point in the presence of an externally applied normal magnetic field of constant strength<img src="19-7401292\45a864cd-d09a-411c-98ab-102edf698847.jpg" />. The shrinking surface has a linear velocity <img src="19-7401292\04f5eeed-85d5-4643-8235-55ca4ed59ab2.jpg" /> and uniform temperature<img src="19-7401292\b123bf22-8786-48cf-b531-921b2ef54d61.jpg" />, while the velocity of the flow external to the boundary layer is <img src="19-7401292\8acbd886-0a00-47db-9639-38434eb90f0c.jpg" /> and temperature <img src="19-7401292\67eeb714-d358-4726-97c6-b92a1a649167.jpg" /> as shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>. Therefore, under the usual boundary layer approximations, the governing equations of motion are:</p><disp-formula id="scirp.29098-formula47090"><label>(1)</label><graphic position="anchor" xlink:href="19-7401292\70910355-9b35-4c9d-ae7f-30c45d193377.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.29098-formula47091"><label>(2)</label><graphic position="anchor" xlink:href="19-7401292\e4c71100-3de8-4948-8e6a-1a7c619b5de0.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.29098-formula47092"><label>(3)</label><graphic position="anchor" xlink:href="19-7401292\c29e3cb1-08b1-4c89-870a-f2ce87b1854e.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="19-7401292\f58f763b-3291-4fc6-80d7-3ef9e2c607d9.jpg" /> is the coefficient of kinematic viscosity, <img src="19-7401292\e9042c58-b999-457f-87d7-05f1fef168cf.jpg" />the electrical conductivity, <img src="19-7401292\f2d7aba5-039d-4d05-90b1-bfea8f0f7249.jpg" />the magnetic permeability, <img src="19-7401292\f86103c0-1ce0-437d-843b-197e8db24a64.jpg" />the density, <img src="19-7401292\a96e8d51-7b8c-4492-b8f6-e89c56ac99c3.jpg" />the specific heat at constant pressure, <img src="19-7401292\a601d295-036e-4f24-a6cb-10556b9aeca0.jpg" />the thermal conductivity and <img src="19-7401292\0306da9a-e78c-4333-bde5-f4b161e1ed2e.jpg" /> the coefficient of viscosity. The other symbols have their usual</p><p>meanings.</p><p>The boundary conditions are:</p><disp-formula id="scirp.29098-formula47093"><label>(4)</label><graphic position="anchor" xlink:href="19-7401292\134ec4c3-4549-4879-b073-4688df0d3fea.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="19-7401292\1880b578-737b-4bbb-bc0f-a49dc67af163.jpg" /> is a proportionality constant of the velocity of shrinking sheet, <img src="19-7401292\d0833d99-9f80-40d9-a65f-a8a399e415e8.jpg" />is a slip length and <img src="19-7401292\2f20be65-ec8b-4fab-8cf4-78c3a0086910.jpg" /> is a constant proportional to the free stream velocity for away from the sheet.</p></sec><sec id="s3"><title>3. Analysis of the Velocity and the Thermal Boundary Layers</title><p>The continuity Equation (1) is identically satisfied by stream function<img src="19-7401292\5dd1153f-fa72-41a0-aa16-e9801ac63071.jpg" />, defined as</p><disp-formula id="scirp.29098-formula47094"><label>(5)</label><graphic position="anchor" xlink:href="19-7401292\da9183c9-17fa-404b-ae72-1e509b11d8c5.jpg"  xlink:type="simple"/></disp-formula><p>For the solution of the momentum and the energy Equations (2) and (3), the following dimensionless variables are defined:</p><disp-formula id="scirp.29098-formula47095"><label>(6)</label><graphic position="anchor" xlink:href="19-7401292\526237e1-10c9-4665-adf3-825ab7e110c5.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.29098-formula47096"><label>(7)</label><graphic position="anchor" xlink:href="19-7401292\2cf7cf3c-1b70-4d97-8a10-49fc5c818595.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.29098-formula47097"><label>(8)</label><graphic position="anchor" xlink:href="19-7401292\dd1b7a43-5d38-4f44-9573-5bcbd77ae36e.jpg"  xlink:type="simple"/></disp-formula><p>Equations (5) to (8), transform Equations (2) and (3) into</p><disp-formula id="scirp.29098-formula47098"><label>(9)</label><graphic position="anchor" xlink:href="19-7401292\55333d87-f78e-4647-a624-59c5410760fd.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.29098-formula47099"><label>(10)</label><graphic position="anchor" xlink:href="19-7401292\f75b5a39-d584-4a22-9250-ec89ea2c871d.jpg"  xlink:type="simple"/></disp-formula><p>where a prime (<img src="19-7401292\d2d36a7b-787e-4b2e-ad19-d9eeab2b6edd.jpg" />) denotes differentiation with respect to</p><p><img src="19-7401292\c4ffa2e0-4b9d-46b5-a18f-097d41d26a96.jpg" />, <img src="19-7401292\e475511a-eb38-437b-b613-c2c5b5ad42c1.jpg" />is the Magnetic parameter,</p><p><img src="19-7401292\7695129e-2591-4a73-a246-e0078c27e1b5.jpg" />is the Prandtl number and <img src="19-7401292\cc51d383-1123-4d25-a249-6a3f165c7e68.jpg" /></p><p>is the Eckert number.</p><p>The corresponding boundary conditions are:</p><disp-formula id="scirp.29098-formula47100"><label>(11)</label><graphic position="anchor" xlink:href="19-7401292\7ba5568a-2e4e-4ec1-bedf-7334bbb7633f.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="19-7401292\27f57715-8abb-46bd-bced-d953ece91b80.jpg" /> is the velocity ratio parameter and</p><p><img src="19-7401292\bd86aa89-ed8e-4dab-b653-764aa8804883.jpg" />is the slip parameter.</p><p>For numerical solution of the Equations (9) and (10), we apply the following power series in a small magnetic parameter <img src="19-7401292\83239c05-8177-410f-8520-a28448870efd.jpg" /> as:</p><disp-formula id="scirp.29098-formula47101"><label>(12)</label><graphic position="anchor" xlink:href="19-7401292\a6acc84a-50ba-4fe6-92e1-b6fad899df00.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.29098-formula47102"><label>(13)</label><graphic position="anchor" xlink:href="19-7401292\7f347d23-0f5e-4c93-a4a0-36612d7e6e59.jpg"  xlink:type="simple"/></disp-formula><p>Substituting Equations (12) and (13) and its derivatives in Equations (9) and (10) and then equating the coefficients of like powers of<img src="19-7401292\852df2be-4bf0-4a2a-9fed-c4d71d05d973.jpg" />, we get the following set of equations:</p><disp-formula id="scirp.29098-formula47103"><label>(14)</label><graphic position="anchor" xlink:href="19-7401292\d85b2d95-bea1-4cd2-bbc9-823f4993d1f9.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.29098-formula47104"><label>(15)</label><graphic position="anchor" xlink:href="19-7401292\32ee59e0-94ba-4c16-9423-4ff0419bf8a6.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.29098-formula47105"><label>(16)</label><graphic position="anchor" xlink:href="19-7401292\a7dbf45c-802c-4daf-a586-da222f86ca78.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.29098-formula47106"><label>(17)</label><graphic position="anchor" xlink:href="19-7401292\1e567318-95ed-4397-8728-1de782e75d74.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.29098-formula47107"><label>(18)</label><graphic position="anchor" xlink:href="19-7401292\82d2eada-8f2a-454d-9201-72cce0a03b19.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.29098-formula47108"><label>(19)</label><graphic position="anchor" xlink:href="19-7401292\ec283b81-8575-4844-a85c-a490a2b456c4.jpg"  xlink:type="simple"/></disp-formula><p>with the boundary conditions:</p><disp-formula id="scirp.29098-formula47109"><label>(20)</label><graphic position="anchor" xlink:href="19-7401292\dc3f910e-4df1-4a79-9276-e435b80393b1.jpg"  xlink:type="simple"/></disp-formula></sec><sec id="s4"><title>4. Results and Discussion</title><p>The Equation (14) is that obtained by Bhattacharyya et al. [<xref ref-type="bibr" rid="scirp.29098-ref12">12</xref>] for the non-magnetic case and the remaining equations are ordinary linear differential equations and have been solved numerically by Newton’s shooting method with fourth-order Runge-Kutta integration scheme for various values of the parameters. The velocity and temperature distributions for various values of parameters are shown in Figures 2-6 respectively.</p><p>The velocity profiles <img src="19-7401292\f01c1938-9c89-4dd8-ac5f-d9bd9a820f30.jpg" /> for different values of the velocity ratio parameter<img src="19-7401292\6ad998ca-34df-4645-8134-d2b35d41e087.jpg" />, the slip parameter <img src="19-7401292\3775902e-d942-488c-9853-836fdfce0880.jpg" /></p><p>and the magnetic parameter <img src="19-7401292\7a90eb3f-17a0-4c20-b4a1-f54fa3ada53e.jpg" /> are shown in Figures 2-4. It is observed that the velocity boundary layer thickness increases with the increasing values of the velocity ratio parameter <img src="19-7401292\ae9bd044-ebb4-4d2c-b893-4ad52bc64baa.jpg" /> and the slip parameter<img src="19-7401292\38057091-3fdc-4cbc-b08f-14277400f13e.jpg" />, whereas it decreases as the magnetic parameter <img src="19-7401292\2cf0b6a0-bd14-45ff-a509-1bae01d803fc.jpg" /> increases for a fixed<img src="19-7401292\2f74b81c-9b33-4082-8137-191c1764783a.jpg" />.</p><p>The temperature profiles <img src="19-7401292\afcb36f1-1297-4a7c-984b-3a93bc5c1ce3.jpg" /> for different values of the velocity ratio parameter<img src="19-7401292\00fe3c57-6f89-486e-8094-71cbee937ecc.jpg" />, the slip parameter<img src="19-7401292\6231b81e-584f-411a-9af9-050807473f18.jpg" />the Prandtl number<img src="19-7401292\8973ef9f-42c3-4f3c-ac26-dd37e3c3236a.jpg" />, the Eckert number <img src="19-7401292\d05cffbe-871f-499a-945d-c9f6c2fa9079.jpg" /> and the magnetic parameter <img src="19-7401292\9ef9f00b-2fe2-4c3a-9d07-139ac9503054.jpg" /> are plotted in Figures 5 and 6. It is observed that for the slip parameter <img src="19-7401292\508224e2-3c3e-4729-bbc2-8d127b4fb74d.jpg" /> the thermal boundary layer thickness decreases with the increasing values of the velocity ratio parameter<img src="19-7401292\d543c93d-483e-471e-a02d-b3582cbba034.jpg" />, the Prandtl number <img src="19-7401292\0f4f5a5a-f1aa-4493-84ea-40caafcc5bc4.jpg" /> and the Eckert number <img src="19-7401292\b8ddaf4c-6070-4369-994d-82bb6d345a8e.jpg" /> and the reverse phenomenon is observed for the magnetic parameter<img src="19-7401292\1ed60449-2639-41e3-9ced-286f75ead841.jpg" />.</p></sec><sec id="s5"><title>5. Conclusions</title><p>In this paper, the stagnation flow for two-dimensional electrically conducting fluid past a shrinking sheet with slip boundaries in the presence of a magnetic field is studied. The similarity equations are derived and solved numerically. It is found that the velocity boundary layer thickness increases with the increasing values of the velocity ratio parameter, the slip parameter. Further we observed that the magnetic parameter decreases with the increasing value of the velocity boundary layer thickness but the reverse phenomenon occurs for thermal boundary layer thickness. Also it observed that the thermal boundary layer thickness decreases with increasing values of the velocity ratio parameter, the Prandtl number and the Eckert number.</p></sec><sec id="s6"><title>REFERENCES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.29098-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">L. J. Crane, “Flow Past a Stretching Plate,” Zeitschrift für angewandte Mathematik und Physik, Vol. 21, No. 4, 1970, pp. 645-647. doi:10.1007/BF01587695</mixed-citation></ref><ref id="scirp.29098-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">C. K. Chen and M. I. Char, “Heat Transfer of a Continuous, Stretching Surface with Suction or Blowing,” Journal of Mathematical Analysis and Applications, Vol. 135, No. 2, 1988, pp. 568-580.</mixed-citation></ref><ref id="scirp.29098-ref3"><label>3</label><mixed-citation publication-type="other" xlink:type="simple">T. C. Chiam, “Stagnation-Point Flow towards a Stretching Plate,” Journal of the Physical Society of Japan, Vol. 63, No. 6, 1994, pp. 2443-2444.  
doi:10.1143/JPSJ.63.2443</mixed-citation></ref><ref id="scirp.29098-ref4"><label>4</label><mixed-citation publication-type="other" xlink:type="simple">H. I. Andersson, “Slip Flow Past a Stretching Surface,” Acta Mechanica, Vol. 158, No. 1-2, 2002, pp. 121-125.  
doi:10.1007/BF01463174</mixed-citation></ref><ref id="scirp.29098-ref5"><label>5</label><mixed-citation publication-type="other" xlink:type="simple">P. D. Ariel, S. Hayat and S. Asghar, “The Flow of an Elastico-Viscous Fluid Past a Stretching Sheet with Partial Slip,” Acta Mechanica, Vol. 187, No. 1, 2006, pp. 29-35. doi:10.1007/s00707-006-0370-3</mixed-citation></ref><ref id="scirp.29098-ref6"><label>6</label><mixed-citation publication-type="other" xlink:type="simple">R. N. Jat and S. Chaudhary, “MHD Stagnation Flows with Slip,” Il Nuovo Cimento, Vol. 122B, No. 8, 2007, pp. 823-831.</mixed-citation></ref><ref id="scirp.29098-ref7"><label>7</label><mixed-citation publication-type="other" xlink:type="simple">R. N. Jat and S. Chaudhary, “Magnetohydrodynamic Boundary Layer Flow near the Stagnation Point of a Stretching Sheet,” Il Nuovo Cimento, Vol. 123B, No. 5, 2008, pp. 555-566.</mixed-citation></ref><ref id="scirp.29098-ref8"><label>8</label><mixed-citation publication-type="other" xlink:type="simple">C. Y. Wang, “Stagnation Flow towards a Shrinking Sheet,” International Journal of Non-Linear Mechanics, Vol. 43, No. 5, 2008, pp. 377-382.  
doi:10.1016/j.ijnonlinmec.2007.12.021</mixed-citation></ref><ref id="scirp.29098-ref9"><label>9</label><mixed-citation publication-type="other" xlink:type="simple">T. Fang, S. Yao, A. Zhang and A. Aziz, “Viscous Flow over a Shrinking Sheet with a Second Order Slip Flow Model,” Communications in Nonlinear Science and Numerical Simulation, Vol. 15, No. 7, 2010, pp. 1831-1842.  
doi:10.1016/j.cnsns.2009.07.017</mixed-citation></ref><ref id="scirp.29098-ref10"><label>10</label><mixed-citation publication-type="other" xlink:type="simple">S. Nadeem, A. Hussain and M. Khan, “HAM Solutions for Boundary Layer Flow in the Region of the Stagnation Point towards a Stretching Sheet,” Communications in Nonlinear Science and Numerical Simulation, Vol. 15, No. 3, 2010, pp. 475-481.  
doi:10.1016/j.cnsns.2009.04.037</mixed-citation></ref><ref id="scirp.29098-ref11"><label>11</label><mixed-citation publication-type="other" xlink:type="simple">K. Bhattacharyya and G. C. Layek, “Effects of Suction/ Blowing on Steady Boundary Layer Stagnation-Point Flow and Heat Transfer towards a Shrinking Sheet with Thermal Radiation,” International Journal of Heat and Mass Transfer, Vol. 54, No. 1-3, 2011, pp. 302-307.  
doi:10.1016/j.ijheatmasstransfer.2010.09.043</mixed-citation></ref><ref id="scirp.29098-ref12"><label>12</label><mixed-citation publication-type="other" xlink:type="simple">K. Bhattacharyya, S. Mukhopadhyay and G. C. Layek, “Slip Effects on Boundary Layer Stagnation-Point Flow and Heat Transfer towards a Shrinking Sheet,” International Journal of Heat and Mass Transfer, Vol. 54, No. 1, 2011, pp. 308-313.  
doi:10.1016/j.ijheatmasstransfer.2010.09.041</mixed-citation></ref></ref-list></back></article>