<?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.2012.37102</article-id><article-id pub-id-type="publisher-id">AM-19873</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 Thermal Shock-Chemical Reactive Problem in Flow of Viscoelastic Fluid with Thermal Relaxation
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>agdy</surname><given-names>A. Ezzat</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>Wisam</surname><given-names>Khatan</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Department of Mathematics and Sciences, Faculty of sciences and letters in Al Bukayriyyah, Al-Qassim University, Al-Qassim, Saudi Arabia</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>maezzat2000@yahoo.com(AAE)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>30</day><month>07</month><year>2012</year></pub-date><volume>03</volume><issue>07</issue><fpage>685</fpage><lpage>698</lpage><history><date date-type="received"><day>April</day>	<month>20,</month>	<year>2012</year></date><date date-type="rev-recd"><day>May</day>	<month>20,</month>	<year>2012</year>	</date><date date-type="accepted"><day>May</day>	<month>27,</month>	<year>2012</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>
 
 
  Effects of thermal and species diffusion with one relaxation time on the boundary layer flow of a viscoelastic fluid bounded by a vertical surface in the presence of transverse magnetic field have been studied. The state space approach developed by Ezzat [1] is adopted for the solution of one-dimensional problem for any set of boundary conditions. The resulting formulation together with the Laplace transform techniques are applied to a thermal shock-chemical reactive problem. The inversion of the Laplace transforms is carried out using a numerical approach. The numerical results of dimensionless temperature, concentration, velocity, and induced magnetic and electric fields distributions are given and illustrated graphically for the problem.
 
</p></abstract><kwd-group><kwd>MHD; Heat and Mass Transfer; Boundary Layer Theory; Viscoelastic Fluid; State Space Approach; Lord-Shulman Theory; Numerical Results</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Viscoelastic flows are encountered in numerous areas of petrochemical, biomedical and environmental engineering including polypropylene coalescence sintering [<xref ref-type="bibr" rid="scirp.19873-ref2">2</xref>] and geological flows [<xref ref-type="bibr" rid="scirp.19873-ref3">3</xref>]. A wide range of mathematical models have been developed to simulate the nonlinear stress-strain characteristics of such fluids which exhibit both viscous and elastic properties [<xref ref-type="bibr" rid="scirp.19873-ref4">4</xref>].</p><p>In nature and many industrial applications, there are plenty of transport processes where simultaneous heat and mass transfer is a common phenomenon. Its application is found in many diverse fields but not limited to cleaning operations, curing of plastics, manufacturing of pulp-insulated cables, many chemical processes such as analysis of polymers in chemical engineering, condensation and frosting of heat exchangers [<xref ref-type="bibr" rid="scirp.19873-ref5">5</xref>]. The study of convection reduces to the determination of convective heat and mass transfer coefficients. Convective heat and mass transfer coefficients are important parameters, which are a measure of the resistance to heat and mass transfer between a surface and the fluid flowing over that surface. The convective coefficients depend on the hydrodynamic, thermal and concentration boundary layers. In many of the internal flows, both forced and natural convection play major roles in the heat and mass transfer processes. Whereas in the entrance section of a duct, forced convection becomes dominant, as the flow moves towards the downstream section, natural convection could dominate over forced convection and finally in the thermally developed region natural convection becomes negligible. Natural convection may be due to a temperature or concentration gradient or both. If the buoyancy forces are due to temperature and concentration gradients that act in the same direction, both the heat and mass transfer will increase. However, if the temperature and concentration gradients act in the opposite direction, both heat and mass transfer reduce [<xref ref-type="bibr" rid="scirp.19873-ref6">6</xref>].</p><p>In recent years, the study of viscoelastic fluid flow is an important type of flow occurring in several engineering processes. Such processes are wire drawing, glass fiber and paper production, crystal growing, drawing of plastic sheets, among which we also cite many applications in petroleum in drilling, manufacturing of foods and slurry transporting. The boundary layer concept of such fluids is of special importance due to its applications to many engineering problems among which we cite the possibility of reducing frictional drag on the hulls of ships and submarines.</p><p>A great deal of works has been carried out on various aspects of momentum and heat transfer characteristics in a viscoelastic boundary layer fluid flow over a stretching plastic boundary [<xref ref-type="bibr" rid="scirp.19873-ref7">7</xref>] since the pioneering work of Sakiadis [<xref ref-type="bibr" rid="scirp.19873-ref8">8</xref>]. Ezzat and Zakaria [<xref ref-type="bibr" rid="scirp.19873-ref9">9</xref>] studied the effects of free convection currents with one relaxation time on the flow of a viscoelastic fluid through a porous medium. Khan and Sanjayanand [<xref ref-type="bibr" rid="scirp.19873-ref10">10</xref>] studied heat and mass transfer in a viscoelastic boundary layer flow over exponentially stretching sheet.</p><p>In this work, we use a more general model of MHD mixed convection flow of conducting viscoelastic fluid which also includes both the relaxation time in the heat and concentration equation and the electric permeability of the electromagnetic field. The unsteady free convection heat and mass transfer flow of electrically conducting incompressible viscoelastic fluid past an infinite vertical plate in the presence of a transverse magnetic field and chemical reaction using the state space approach and Laplace transforms technique. The inversion of the Laplace transform is carried out using a numerical technique [<xref ref-type="bibr" rid="scirp.19873-ref11">11</xref>].</p></sec><sec id="s2"><title>2. Formulation of the Problem</title><p>The electro-magnetic quantities satisfy Maxwell’s equations [<xref ref-type="bibr" rid="scirp.19873-ref12">12</xref>]:</p><disp-formula id="scirp.19873-formula61940"><label>(1)</label><graphic position="anchor" xlink:href="2-7400814\0cf4f49b-f1a0-483a-9add-29155e3cd7a9.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19873-formula61941"><label>(2)</label><graphic position="anchor" xlink:href="2-7400814\eeb49ba0-3643-4630-8829-4f2907b1d338.jpg"  xlink:type="simple"/></disp-formula><p><img src="2-7400814\1b169fd2-a74e-4713-a48c-f797ff4ae9ce.jpg" />,<img src="2-7400814\c2bc333b-fd50-4fc2-8399-3966ea5820b1.jpg" /> (3)</p><p><img src="2-7400814\3943f36b-a307-49ce-82f4-b9031b68f14a.jpg" />,<img src="2-7400814\0a2701bb-9701-4c48-b314-8b7ebcb6cd46.jpg" /> (4)</p><p>These equations are supplemented by Ohm’s law</p><disp-formula id="scirp.19873-formula61942"><label>(5)</label><graphic position="anchor" xlink:href="2-7400814\21f34e5e-7af1-4479-a8f6-f4c4465ed2d1.jpg"  xlink:type="simple"/></disp-formula><p>Consider an unsteady free convection flow of electrically conducting incompressible, viscoelastic fluid past an infinite vertical plate. The x-axis is taken in the vertical direction along the plate and y-axis normal to it. Let u be the component of the velocity of the fluid in the x direction and a constant magnetic field acts in the y direction of strength<img src="2-7400814\033860a3-fa7c-4003-bad7-6b8430e0d477.jpg" />. This produces an induced magnetic field <img src="2-7400814\f20530a1-e288-45a6-8bc0-4b47ffe0009f.jpg" /> and an induced electric field <img src="2-7400814\d033a02c-3672-4a36-8f3c-97b3d85583d0.jpg" /> as well as a conduction current density<img src="2-7400814\08deb0ac-878d-4066-ac02-ec99d9238270.jpg" />. All the considered functions will depend on y and the time t only.</p><p>Equation (5) reduces to</p><disp-formula id="scirp.19873-formula61943"><label>. (6)</label><graphic position="anchor" xlink:href="2-7400814\9d54b52c-1e16-4b9d-8ac2-9cd3c9432bb2.jpg"  xlink:type="simple"/></disp-formula><p>The vector Equations (1) and (2) reduced to the following scalar equation</p><disp-formula id="scirp.19873-formula61944"><label>(7)</label><graphic position="anchor" xlink:href="2-7400814\7471bb8f-10d8-47b4-a7ee-da0d3ef2c232.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19873-formula61945"><label>(8)</label><graphic position="anchor" xlink:href="2-7400814\2d7a6693-5e02-4770-8c4d-6c061872816a.jpg"  xlink:type="simple"/></disp-formula><p>Eliminating J between Equations (6) and (7) we obtain</p><disp-formula id="scirp.19873-formula61946"><label>(9)</label><graphic position="anchor" xlink:href="2-7400814\51cac265-c8ce-4008-84bd-7a245b5a685e.jpg"  xlink:type="simple"/></disp-formula><p>Eliminating E between Equations (8) and (9) we obtain</p><disp-formula id="scirp.19873-formula61947"><label>(10)</label><graphic position="anchor" xlink:href="2-7400814\30aff1cf-0898-46e8-a69b-50752bb45bc3.jpg"  xlink:type="simple"/></disp-formula><p>The Lorentz force has a non-vanishing component in the x-direction, given by:</p><disp-formula id="scirp.19873-formula61948"><label>(11)</label><graphic position="anchor" xlink:href="2-7400814\c9b2101a-0d60-4462-89d6-60dd84a922b9.jpg"  xlink:type="simple"/></disp-formula><p>Assume that the viscoelastic fluid contains some chemically reactive diffusive species then the equations describing the flow in the boundary layer reduce to:</p><disp-formula id="scirp.19873-formula61949"><label>(12)</label><graphic position="anchor" xlink:href="2-7400814\a84b7fad-f642-4b73-bb04-9b4e47a84653.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19873-formula61950"><label>(13)</label><graphic position="anchor" xlink:href="2-7400814\aaa61b4e-3b51-4ca9-8100-4bbf6f5e30d7.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19873-formula61951"><label>(14)</label><graphic position="anchor" xlink:href="2-7400814\0da542d9-20e6-43cc-ab4c-95c61105140f.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19873-formula61952"><label>(15)</label><graphic position="anchor" xlink:href="2-7400814\b0324f5d-35e8-4bcd-a598-bb010e5dccd4.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19873-formula61953"><label>(16)</label><graphic position="anchor" xlink:href="2-7400814\94d0d559-136c-4aa9-a67c-cfff3626ad52.jpg"  xlink:type="simple"/></disp-formula><p>Introduce the non-dimensional quantities.</p><disp-formula id="scirp.19873-formula61954"><label>(17)</label><graphic position="anchor" xlink:href="2-7400814\c82b3d32-1a8d-471a-aeb3-ef1255536eee.jpg"  xlink:type="simple"/></disp-formula><p>With the help of the non-dimensional quantities above Equations (12)-(16) reduced to the non-dimensional equations</p><disp-formula id="scirp.19873-formula61955"><label>(18)</label><graphic position="anchor" xlink:href="2-7400814\a90dd706-f015-427e-98e3-081a5e4f52b9.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19873-formula61956"><label>(19)</label><graphic position="anchor" xlink:href="2-7400814\71c8517e-1624-4ec8-9c2a-ac03934f35b9.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19873-formula61957"><label>(20)</label><graphic position="anchor" xlink:href="2-7400814\fc1d4ff5-e712-4360-b979-52f83a5c95c3.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19873-formula61958"><label>(21)</label><graphic position="anchor" xlink:href="2-7400814\388db5b4-9307-435b-8a2b-5d5864c1250d.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19873-formula61959"><label>(22)</label><graphic position="anchor" xlink:href="2-7400814\ade40517-07c9-4e02-92b0-9d29afb062cb.jpg"  xlink:type="simple"/></disp-formula><p>where<img src="2-7400814\5a97c890-2561-468f-aeda-868ea92cd0fb.jpg" />,<img src="2-7400814\9847a134-60f5-45db-9960-e6defaf41595.jpg" />.</p><p>To simplify the algebra, only problems with zero initial conditions are considered. Taking Laplace transform of Equations (18)-(22) and writing the resulting equations in matrix form results in (23).</p><p>where</p><p><img src="2-7400814\3d7a2a90-4eb4-4df0-aced-fdd3d7480082.jpg" /></p><p><img src="2-7400814\a59f7cf7-a534-4ca2-8a96-9e243b8b9ae2.jpg" /></p><p><img src="2-7400814\fb760e1e-af81-4b43-a452-8df2f417d7ea.jpg" /></p><p><img src="2-7400814\a96babd0-1fd1-4416-a8fb-59883e51f8f7.jpg" /></p><p>and</p><p><img src="2-7400814\c3323b08-bce1-437f-9fbb-674d960fdf81.jpg" />.</p><p>In Equation (23) the overbar denotes the Laplace transform and the prime indicates differentiations with respect to y.</p><disp-formula id="scirp.19873-formula61960"><label>(23)</label><graphic position="anchor" xlink:href="2-7400814\db9adc2f-c7a3-497c-9066-3fa9779c6159.jpg"  xlink:type="simple"/></disp-formula><p>Equation (23) can be written in constracted form as</p><disp-formula id="scirp.19873-formula61961"><label>(24)</label><graphic position="anchor" xlink:href="2-7400814\6d4668b0-489f-4626-8f6a-b7157bbc7cef.jpg"  xlink:type="simple"/></disp-formula><p>The formal solution can be expressed as:</p><disp-formula id="scirp.19873-formula61962"><label>(25)</label><graphic position="anchor" xlink:href="2-7400814\f4307bf7-4588-4c14-b221-8fdbe93a0a03.jpg"  xlink:type="simple"/></disp-formula><p>The characteristic equation of the matrix <img src="2-7400814\cd538806-9388-4aa0-b5c1-ef31ec2ff6be.jpg" /> is</p><disp-formula id="scirp.19873-formula61963"><label>(26)</label><graphic position="anchor" xlink:href="2-7400814\616e60d0-7bd2-4c97-bf08-1047ff34d310.jpg"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.19873-formula61964"><label>(27)</label><graphic position="anchor" xlink:href="2-7400814\6e3b6a04-7b75-4eb0-b024-04a52c8ab47f.jpg"  xlink:type="simple"/></disp-formula><p>The roots<img src="2-7400814\5bcb351f-8192-42e6-8744-fa10e336ff10.jpg" />, <img src="2-7400814\67ec557e-fbe1-44cc-9e40-e2ed0eba27f3.jpg" />, <img src="2-7400814\0afa0396-4769-4dcf-8792-f63d4632fe63.jpg" />and <img src="2-7400814\07759885-d585-46f5-8bca-7c780dc537ce.jpg" /> of Equation (25) satisfy the relations:</p><disp-formula id="scirp.19873-formula61965"><label>(28)</label><graphic position="anchor" xlink:href="2-7400814\c60116dd-73d7-4162-9aa5-dca9897da504.jpg"  xlink:type="simple"/></disp-formula><p>Two of the roots, say <img src="2-7400814\8849fb90-4109-4a7d-8586-5994379218eb.jpg" /> and <img src="2-7400814\ee0fc3c9-86e4-4a8a-a9bf-c7ed2c5b3a4f.jpg" /> have simple expression given by</p><disp-formula id="scirp.19873-formula61966"><label>(29a)</label><graphic position="anchor" xlink:href="2-7400814\fe1f444e-7c9b-4f67-87eb-9aed77357a14.jpg"  xlink:type="simple"/></disp-formula><p>The other two roots <img src="2-7400814\c4b2c42e-72ad-4248-9c99-1641cdcfda7d.jpg" /> and <img src="2-7400814\06988986-35ec-4403-8ac0-b4e576e5cc3f.jpg" /> satisfy the relation</p><disp-formula id="scirp.19873-formula61967"><label>(29b)</label><graphic position="anchor" xlink:href="2-7400814\6afb5bb4-3da3-44af-9b46-a063a1630866.jpg"  xlink:type="simple"/></disp-formula><p>The Maclaurin series expansion of <img src="2-7400814\055bb2d4-1803-4629-95f3-3faaf6445cd8.jpg" /> is given by</p><p><img src="2-7400814\db91e0b5-0d3a-4c98-b967-242b6159bfca.jpg" />.</p><p>Using the Cayley-Hamilton theorem, the infinite series can be truncated to the following form</p><disp-formula id="scirp.19873-formula61968"><label>(30)</label><graphic position="anchor" xlink:href="2-7400814\5f949281-175e-4e62-999a-d1c8e15e7f7a.jpg"  xlink:type="simple"/></disp-formula><p>where I is the unit matrix of order 8 and a<sub>0</sub> – a<sub>7</sub> are some parameters depending on s and y.</p><p>The characteristic roots<img src="2-7400814\d71c43ca-50d4-4aa1-bbfd-e7afe4a72202.jpg" />, <img src="2-7400814\9e21d3f3-7d5c-4680-800a-35124cf9f850.jpg" />, <img src="2-7400814\e6ad79ea-5649-4f18-b2f9-4e3b9b6d9134.jpg" />and <img src="2-7400814\17a4b3b4-f8c3-48a2-bc03-7765e225749f.jpg" /> of the matrix A must satisfy the equations.</p><p><img src="2-7400814\2e00d884-6bed-494b-ae57-df0607e55070.jpg" /></p><p><img src="2-7400814\cbef6115-1d3c-41a4-b1d7-b4317ac059d4.jpg" /></p><p><img src="2-7400814\2f0ea963-8a52-4bfc-84de-269104d038fe.jpg" /></p><p><img src="2-7400814\ad6fdbdb-a94a-4276-80e9-07e3bf158cc1.jpg" /></p><p>The solution of this system of linear equations is given in Appendix A:</p><p>Substituting for the parameters a<sub>0</sub> - a<sub>7</sub> into Equation (30) and computing A<sup>2</sup>, A<sup>3</sup>, A<sup>4</sup>, A<sup>5</sup>, A<sup>6</sup> and A<sup>7</sup>, we get, the elements (ℓ<sub>ij</sub> i, j = 1, 2, 3, 4, 5, 6, 7, 8) of the matrix L(y, s) which listed in Appendix B.</p><p>It should be noted here that, we have used Equation (29) in order to write these entries in the simplest possible form. It should also be noted that this is a formal expression for the matrix exponential. In the physical problem<img src="2-7400814\b7d53989-bc97-4df0-9a02-5134a9fd0263.jpg" />, we should suppress the positive exponential which are unbounded at infinity. Thus we should replace each <img src="2-7400814\b72c41d4-062e-4ae6-8e51-36a322c05091.jpg" /> by <img src="2-7400814\ebb129df-4a15-4879-9330-76630931b092.jpg" /> and each <img src="2-7400814\0884b2d3-4456-4a05-88f5-6808afdf6e8a.jpg" /> by<img src="2-7400814\0df54a8e-e487-4a3a-892f-0139265cd733.jpg" />.</p><p>It is now possible to solve broad class problems in the Laplace transform domain.</p></sec><sec id="s3"><title>3. Thermal Shock-Chemical Reactive Problem</title><p>Consider the free convection flow of an incompressible viscoelastic fluid in the presence of magnetic field occupying a semi-infinite region y &#179; 0 of the space bounded by an infinite vertical plate y = 0 with quiescent initial state. A thermal-concentration shock is applied to the boundary plane y = 0 in the form</p><disp-formula id="scirp.19873-formula61969"><label>(31)</label><graphic position="anchor" xlink:href="2-7400814\b02cb27d-87a0-48d1-8054-9f7b4f495b3d.jpg"  xlink:type="simple"/></disp-formula><p>and the mechanical boundary conditions on the plate is taken as</p><disp-formula id="scirp.19873-formula61970"><label>(32)</label><graphic position="anchor" xlink:href="2-7400814\0ba127b1-2e45-49f0-a691-24ad10a2b947.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="2-7400814\39274473-2538-4063-88bd-2dd73b7e83f3.jpg" /> and <img src="2-7400814\398ac4a3-112b-4e2f-9ade-924608ae6779.jpg" /> are constant and H(t) is Heaviside unit step function.</p><p>Now we apply the state space approach described above to this problem.</p><p>Since the solution is bounded at infinity, then the expressions for <img src="2-7400814\b0279b89-94f9-4b0e-a702-0745cc013855.jpg" /> can be obtained by suppressing the positive exponential terms in Equation (30) which are not bounded at infinity. Thus for<img src="2-7400814\6463ecd4-2ad7-4590-9e42-fd0a487fe330.jpg" />, we should replace each <img src="2-7400814\830e41ed-c37b-4264-81ad-2469b7b5f1a6.jpg" /> by <img src="2-7400814\657293ae-f8b5-41cb-9573-cb3621169694.jpg" /> and each <img src="2-7400814\bdbc7c44-3cb9-47e6-80ff-10b6b67ec8ff.jpg" />by<img src="2-7400814\002c1466-b6d3-40ab-bfec-73710847d2a8.jpg" />.</p><p>The components of the transformed initial state vector <img src="2-7400814\6f27b8e3-e891-42a5-b3ca-6c2c792cfe70.jpg" /> are known name</p><disp-formula id="scirp.19873-formula61971"><label>(33)</label><graphic position="anchor" xlink:href="2-7400814\ee7eaad2-5f67-4560-9c12-575f586c4b85.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19873-formula61972"><label>(34)</label><graphic position="anchor" xlink:href="2-7400814\156c3d0d-c5ad-44fd-a85f-51e78564a1a1.jpg"  xlink:type="simple"/></disp-formula><p>In order to obtain the remaining four components<img src="2-7400814\33941696-e8d4-45c7-bf7f-940306d48511.jpg" />, <img src="2-7400814\cccc1c0b-9388-4478-9753-5487913f93cd.jpg" />, <img src="2-7400814\305d27d4-862e-4637-8d57-c30595c70034.jpg" />and <img src="2-7400814\6c6f62db-2b26-4df0-a3e0-18363542c806.jpg" /> we substitute y = 0 into Equations (31) and (32) to obtain the following linear system of equations:</p><disp-formula id="scirp.19873-formula61973"><label>(35)</label><graphic position="anchor" xlink:href="2-7400814\140c97e8-b63e-4841-848b-67a1f3414db6.jpg"  xlink:type="simple"/></disp-formula><p>By solving this system, we arrive at</p><disp-formula id="scirp.19873-formula61974"><label>(36)</label><graphic position="anchor" xlink:href="2-7400814\80116a6e-4f1b-486d-82fc-08c414e827f7.jpg"  xlink:type="simple"/></disp-formula><p>Finally substituting the above value into (25), we obtain the solution of the problem in the transformed domain as:</p><disp-formula id="scirp.19873-formula61975"><label>(37)</label><graphic position="anchor" xlink:href="2-7400814\7f41f18a-2d28-4638-b37f-bdba2dc1b8e3.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19873-formula61976"><label>(38)</label><graphic position="anchor" xlink:href="2-7400814\69cd95b3-db42-400e-bfa9-a03d965fac17.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19873-formula61977"><label>(39)</label><graphic position="anchor" xlink:href="2-7400814\af7fc5da-e80c-46fd-b99c-4dbad5162394.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19873-formula61978"><label>(40)</label><graphic position="anchor" xlink:href="2-7400814\54a8cf15-713b-483c-8688-aabb95a4ddc1.jpg"  xlink:type="simple"/></disp-formula><p>where the constants A<sub>i</sub>, i = 1, 2, 3, 4 are listed in Appendix C.</p><p>The induced electric field and current density take the following forms</p><disp-formula id="scirp.19873-formula61979"><label>(41)</label><graphic position="anchor" xlink:href="2-7400814\af7c0b7d-e59e-47f3-af82-e674953eda5a.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19873-formula61980"><label>(42)</label><graphic position="anchor" xlink:href="2-7400814\c8ca8746-5e31-421e-9036-8391ffda18ae.jpg"  xlink:type="simple"/></disp-formula><p>The shearing stress at the wall is given by</p><disp-formula id="scirp.19873-formula61981"><label>(43)</label><graphic position="anchor" xlink:href="2-7400814\efb37ed2-f621-4e54-af10-f33ba1ded40a.jpg"  xlink:type="simple"/></disp-formula></sec><sec id="s4"><title>4. Inversion of the Laplace Transforms</title><p>In order to invert the Laplace transform in the above equations, we adopt a numerical inversion method based on a Fourier series expansion [<xref ref-type="bibr" rid="scirp.19873-ref11">11</xref>]. In this method, the inverse g(t) of the Laplace transform <img src="2-7400814\3510d27d-e35a-4c41-9908-bc6be7b95040.jpg" /> is approximated by the relation</p><disp-formula id="scirp.19873-formula61982"><label>(44)</label><graphic position="anchor" xlink:href="2-7400814\81098a19-5d81-4333-bc6e-c487b351cf66.jpg"  xlink:type="simple"/></disp-formula><p>where N is a sufficiently large integer representing the number of terms in the truncated infinite Fourier series. N must chosen such that</p><p><img src="2-7400814\4a1f6e76-1e8b-487a-bdcb-3133d1ea0fce.jpg" />where <img src="2-7400814\a614f272-c33d-4b54-be92-e4f18fd6594a.jpg" /> is a persecuted small positive number that corresponds to the degree of accuracy to be achieved. The parameter c is a positive free parameter that must be greater than the real parts of all singularities of<img src="2-7400814\5aebef81-5fb3-4c2a-a110-2bdf12bf8df3.jpg" />. The optimal choice of c was obtained according to the criteria described in [<xref ref-type="bibr" rid="scirp.19873-ref11">11</xref>].</p></sec><sec id="s5"><title>5. Numerical Results and Discussion</title><p>The problem of free convective flow with heat and mass transfer of a viscous incompressible viscoelastic electrically conducting fluid past a vertical plate in presence of a transverse magnetic field has been considered. The solutions for velocity, temperature and concentration fields as well as the induced magnetic and electric fields are obtained by using the state space approach. The technique is applied to a thermal shock-chemical reactive problem without heat sources. The effects of flow parameters such as Grashof number for heat and mass transfer<img src="2-7400814\11a45789-c6ac-48ad-968a-b6488aea76ea.jpg" />, <img src="2-7400814\e6715a72-8672-4244-9328-0119318b56c4.jpg" />, Prandtl number<img src="2-7400814\d3c2f710-5151-44ef-97a0-9082ec88fa9c.jpg" />, Schmidt number<img src="2-7400814\37f02f8d-b51c-4238-98f1-0baaf8708059.jpg" />, chemical reaction parameter K, viscoelastic parameter <img src="2-7400814\57167a31-bbbc-4280-93a5-0a23d17cd63a.jpg" /> and relaxation time <img src="2-7400814\052c4cb2-ffe9-4c9f-af5d-b40deae44a06.jpg" /> have been studied analytically and presented with the help of Figures 1-8 for the considered problem.</p><sec id="s5_1"><title>5.1. Velocity Field (u)</title><p>The velocity of the flow field varies vastly with the variation of the flow parameters such as Grashof number for heat and mass transfer<img src="2-7400814\a307d640-5733-4292-be27-b764f0cca8c7.jpg" />, <img src="2-7400814\03fd510d-7bbd-460b-b6df-4d2786c26586.jpg" />, viscoelastic parameter<img src="2-7400814\b6b96743-c9eb-443c-bf9a-b3b2a0df8260.jpg" />, Prandtl number<img src="2-7400814\c31e9675-beab-4098-9c16-d24e6fcd3609.jpg" />, Schmidt number<img src="2-7400814\174c2cbd-c9ef-470f-af58-633c6a030f28.jpg" />, chemical reaction parameter K. The effects of these parameters on the velocity fluid of flow field have been presented in Figures 1-3.</p><sec id="s5_1_1"><title>5.1.1. Effect of Viscoelastic Parameter (k<sub>o</sub>)</title><p><xref ref-type="fig" rid="fig1">Figure 1</xref> depicts the effect of viscoelastic parameter <img src="2-7400814\2d23a2db-082e-4e2b-ad41-3e449a3185de.jpg" /> on the velocity profiles of the flow field keeping other parameters of the flow field constant. The curve with viscoelastic parameter, <img src="2-7400814\9cc0a72e-4b15-4e11-a8c4-0989f95bc79f.jpg" />corresponds to Newtonian flow and in other two curves the viscoelastic parameter is taken in increasing order. The viscoelastic parameter is found to decelerate the velocity of the flow field. The above parameter is in good agreement with the result obtained in cases of Khan and Sanjayanand [<xref ref-type="bibr" rid="scirp.19873-ref10">10</xref>].</p></sec><sec id="s5_1_2"><title>5.1.2. Effect of Grashof Number for Heat (G<sub>T</sub>)</title><p>The values of Grashof number for heat <img src="2-7400814\5d7cfcfd-c220-4e29-aab3-7a96eab8cf9d.jpg" /> have been chosen as they are interesting from physical point of view. The free convection of heat is due to the temperature difference <img src="2-7400814\fb5bd22c-a05d-437f-82eb-8028f592f0b7.jpg" /> and hence <img src="2-7400814\1a24d9b2-e3c6-404a-85a3-e5fd63cb01c2.jpg" /> when <img src="2-7400814\b0e25920-8ef6-4223-bda9-6e5db5d0ab7f.jpg" /> which physically corresponds to cooling of the surface by free convection currents. Then <img src="2-7400814\d5047feb-e749-452d-bb03-3ab73cc72ce4.jpg" /> correspond to heating of the surface by free convection currents. In <xref ref-type="fig" rid="fig2">Figure 2</xref>, we observe that the effect of cooling and heating by free convection currents when <img src="2-7400814\65530686-2186-4629-a435-79140f3a1243.jpg" /> and <img src="2-7400814\220fba9a-248b-4df9-a5ca-da7386099ece.jpg" /> are in agreement with physical observations that cooling of the surface by free convection currents occurs for positive values of <img src="2-7400814\bda0082d-2877-4311-83aa-1417ce5dda5d.jpg" /> while heating corresponds to negative values of<img src="2-7400814\cdf2cd7c-75e6-40b7-9b73-5fdda78bfc61.jpg" />. It was also noticed that the velocity increase with the increase of<img src="2-7400814\b945e984-591f-475f-9464-8f1e5f00d8be.jpg" />.</p></sec><sec id="s5_1_3"><title>5.1.3. Effect of Different Parameters (G<sub>c</sub>, P<sub>r</sub>, S<sub>c</sub>, K)</title><p><xref ref-type="fig" rid="fig3">Figure 3</xref> present the effect of Grashof number for mass transfer<img src="2-7400814\f930b565-8ed4-4bb1-ab54-cb22ea0aa62b.jpg" />, Prandtl number<img src="2-7400814\859c7d48-5061-4396-a1cc-df2cb35f0736.jpg" />, Schmidt number <img src="2-7400814\6aa302bc-ba28-48c6-8a14-aa4ad2f81398.jpg" /> and chemical reaction parameter K on the velocity profiles of the flow fluid. Comparing the curve (1) and (2) of the figure, it is observed that the Grashof number for mass transfer is to enhance the velocity of the flow field at all points. The effect of both Prandtl number <img src="2-7400814\2db55365-e422-4576-85d5-e96c685ef954.jpg" /> and chemical reaction parameter K on the velocity field is shown by the curves (1), (3) and (5). It was found that the increasing of <img src="2-7400814\0e67ad01-0391-4dc6-84aa-4dc5e8c28798.jpg" /> and K lead to decelerate the velocity of the flow field. Curves (1) and (4) describe the effect of Schmidt number <img src="2-7400814\916cafcd-6054-4a9c-bbf2-e0180c8999eb.jpg" /> on the velocity profiles of the flow field which reveal that the presence of heavier diffusing species has a retarding effect on the velocity of the flow field. The effect of the above parameters has the same behavior as in case of Das et al. [<xref ref-type="bibr" rid="scirp.19873-ref13">13</xref>].</p></sec></sec></sec></body><back><ref-list><title>References</title><ref id="scirp.19873-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">M. A. 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