<?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.2012.23015</article-id><article-id pub-id-type="publisher-id">WJM-19984</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>
 
 
  Mathematical Analysis of Unsteady MHD Blood Flow through Parallel Plate Channel with Heat Source
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>slam</surname><given-names>M. Eldesoky</given-names></name><xref ref-type="aff" rid="aff1"><sub>1</sub></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><aff id="aff1"><label>1</label><addr-line>Basic Engineering Sciences Department, Faculty of Engineering, Elmenoufia University, Shibin El Kom, Egypt</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>eldesokyi@yahoo.com</email></corresp></author-notes><pub-date pub-type="epub"><day>20</day><month>06</month><year>2012</year></pub-date><volume>02</volume><issue>03</issue><fpage>131</fpage><lpage>137</lpage><history><date date-type="received"><day>March</day>	<month>6,</month>	<year>2012</year></date><date date-type="rev-recd"><day>April</day>	<month>5,</month>	<year>2012</year>	</date><date date-type="accepted"><day>April</day>	<month>20,</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>
 
 
  In the present study, a mathematical model of unsteady blood flow through parallel plate channel under the action of an applied constant transverse magnetic field is proposed. The model is subjected to heat source. Analytical expressions are obtained by choosing the axial velocity; temperature distribution and the normal velocity of the blood depend on y and t only to convert the system of partial differential equations into system of ordinary differential equations under the conditions defined in our model. The model has been analyzed to find the effects of various parameters such as, Hartmann number, heat source parameter and Prandtl number on the axial velocity, temperature distribution and the normal velocity. The numerical solutions of axial velocity, temperature distributions and normal velocity are shown graphically for better understanding of the problem. Hence, the present mathematical model gives a simple form of axial velocity, temperature distribution and normal velocity of the blood flow so that it will help not only people working in the field of Physiological fluid dynamics but also to the medical practitioners.
 
</p></abstract><kwd-group><kwd>Blood Flow; Parallel Plate Channel; Boundary Layer; Heat Source; Magnetic Field</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The study of blood flow has been carried out by several authors. During the last decades extensive research work has been done on the fluid dynamics of biological fluids in the presence of magnetic field. For multiple reasons, applications of magnetohydrodynamics in physiological flow problems are of growing interest. Many researchers have reported that the blood is an electrically conducting fluid [1-4]. The electromagnetic force (Lorentz force) acts on the blood and this force opposes the motion of blood and there by flow of blood is impeded, so that the external magnetic field can be used in the treatment of some kinds of diseases like cardiovascular diseases and in the diseases with accelerated blood circulation such as hemorrhages and hypertension.</p><p>In general, biological systems are affected by an application of external magnetic field on blood flow through human arterial system. Many mathematical models have already been investigated by several research workers to explore the nature of blood flow under the influence of an external magnetic field. Tzirtzilakis [<xref ref-type="bibr" rid="scirp.19984-ref5">5</xref>] studied a mathematical model of biomagnetic fluid dynamics (BFD), suitable for the description of the Newtonian blood flow under the action of magnetic field. This model is consistent with the principles of ferrodynamics and magnetohydrodynamics and takes into account both magnetization and electrical conductivity of blood. Ramamurthy and shanker [<xref ref-type="bibr" rid="scirp.19984-ref6">6</xref>] studied magnetohydrodynamic effects on blood flow through a porous channel. They considered the blood a Newtonian fluid and conducting fluid.</p><p>Arterial MHD pulsatile flow of blood under periodic body acceleration has been studied by Das and Saha [<xref ref-type="bibr" rid="scirp.19984-ref7">7</xref>]. The blood flow in very narrow capillaries under the effect of transverse magnetic field has been investigated by Madhu et al. [<xref ref-type="bibr" rid="scirp.19984-ref8">8</xref>]. In this investigation; it is assumed that there is a lubricating layer between red blood cells and tube wall. A pulsatile flow of blood which is considered as a couple stress fluid through a porous medium under the influence of periodic body acceleration in the presence of magnetic field has been investigated by Rathod and Tanveer [<xref ref-type="bibr" rid="scirp.19984-ref9">9</xref>]. Singh and Rathee [<xref ref-type="bibr" rid="scirp.19984-ref10">10</xref>] gave an analytical solution of two-dimensional model of blood flow with variable viscosity through an indented artery due to low density lipoprotein effect in the presence of magnetic field. The investigation shows that hypertensive patients are more adequate to have heart circulatory problems. The effect of uniform transverse magnetic field on its pulsatile motion through an axi-symmetric tube is analyzed by Dulal and Ananda [<xref ref-type="bibr" rid="scirp.19984-ref11">11</xref>]. Zamir and Roach [<xref ref-type="bibr" rid="scirp.19984-ref12">12</xref>] studied Blood flow downstream of a two-dimensional bifurcation with a symmetrical steady flow.</p><p>Heat transfer in biological systems is relevant in many diagnostic and therapeutic applications that involve changes in temperature. As we know, the cardiovascular system is sensitive to changes in the environment, and flow characteristics of blood are modified to satisfy changing demands of the orgasm. In addition to transporting of oxygen, metabolites and other dissolved sub stances to and from the tissues, blood flow alters heat transfer within the body. Adhikary and Misra [<xref ref-type="bibr" rid="scirp.19984-ref13">13</xref>] pre sented an exact solution of the problem of oscillatory flow of a fluid and heat transfer along a porous oscillating channel in presence of an external magnetic field. The influence of blood flow in large vessels on the temperature distribution in hyperthermia has been developed by Lagendijk [<xref ref-type="bibr" rid="scirp.19984-ref14">14</xref>]. The blood flow in a small tube was modeled by the two-fluid model by Wang [<xref ref-type="bibr" rid="scirp.19984-ref15">15</xref>]. The flow is fully developed, constant heat flux convective heat transfer.</p><p>In the present investigation, a mathematical model for the unsteady blood flow through a very narrow parallel plate channel with heat source and external transverse magnetic field is presented. This work is an extensive study of Madhu et al. [<xref ref-type="bibr" rid="scirp.19984-ref8">8</xref>] with heat transfer under the conditions defined in our model. The main aim of this work is to obtain analytical expressions for axial velocity, temperature distribution and normal velocity using new boundary conditions and with converting the system of partial differential equations into system of ordinary differential equations. Also to study the effect of magnetic field (Hartmann number (Ha)), heat source parameter (<img src="1-4900111\8aabdf50-2446-4119-a69e-d74fc3896ee0.jpg" />) and Prandtl number (Pr) on the axial velocity, temperature distribution and normal velocity. Hence, the present mathematical model gives a simple form of axial velocity, temperature distribution and normal velocity of the blood flow so that it will help not only people working in the field of Physiological fluid dynamics but also to the medical practitioners. In fact, we studied the mathematical model in [<xref ref-type="bibr" rid="scirp.19984-ref2">2</xref>] with few modifications, also we checked the analytical solution and modified the results.</p></sec><sec id="s2"><title>2. Formulation of the Problem</title><p>Consider flow between non-conducting two parallel plates as shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>.</p><p>Here blood is supposed to be Newtonian, incompressible, homogenous and viscous fluid. Also, the viscosity of blood is considered to be constant. The effect of mag netic field is considered in this model which is applied in a direction perpendicular to the flow of blood.</p><p>Considering u and v as velocity components in the directions of x and y respectively (axial and normal respectively) at time t in the flow field, we may write the two dimensional boundary layer equations in presence of transverse magnetic field as</p><disp-formula id="scirp.19984-formula7185"><label>(1)</label><graphic position="anchor" xlink:href="1-4900111\8247e51d-de69-4447-8332-45215429f0e9.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19984-formula7186"><label>(2)</label><graphic position="anchor" xlink:href="1-4900111\da8b90b7-bee2-469b-ab33-4bc721e295e8.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19984-formula7187"><label>(3)</label><graphic position="anchor" xlink:href="1-4900111\92962fa2-4520-4e1d-8880-7cb74e623dd2.jpg"  xlink:type="simple"/></disp-formula><p>Introduce the following non-dimensional variables</p><disp-formula id="scirp.19984-formula7188"><label>(4)</label><graphic position="anchor" xlink:href="1-4900111\3ab905ab-1c1a-43ea-b9d5-80e099c19d89.jpg"  xlink:type="simple"/></disp-formula><p>Substituting from Equation (4) into the Equations (1)- (3) we may write these equations after dropping the stars as</p><disp-formula id="scirp.19984-formula7189"><label>(5)</label><graphic position="anchor" xlink:href="1-4900111\4838afb0-0625-420b-9506-66dfc9351a67.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19984-formula7190"><label>(6)</label><graphic position="anchor" xlink:href="1-4900111\0d719356-ba8f-404f-ae9b-7032e1b086d0.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19984-formula7191"><label>(7)</label><graphic position="anchor" xlink:href="1-4900111\788c3f15-02aa-454f-9a4e-b77a5cd82217.jpg"  xlink:type="simple"/></disp-formula><p>From Equation (7) we can observe that the temperature distribution <img src="1-4900111\d2198b62-33f0-4493-a00f-0b9017b345df.jpg" /> has 1<sup>st</sup> derivative with respect to time t. From this observation and with the help of solution of partial differential equation by separation of vari ables technique we can get the following equation</p><p><img src="1-4900111\a86f656d-ac20-48bb-b6e6-ab2698fde3ef.jpg" /></p><p>It is observed that the solution of this equation will be on the form<img src="1-4900111\1a0c1f9b-0d8c-44d1-92e9-a1f96fba9c93.jpg" />.</p><p>Similarly, the axial velocity u has the same concept, and then the solution of the problem will take the form mentioned in Section 3 and the boundary conditions are taken as:</p><disp-formula id="scirp.19984-formula7192"><label>(8)</label><graphic position="anchor" xlink:href="1-4900111\12beb5b6-8908-4de2-a01c-2cdaf8632ee5.jpg"  xlink:type="simple"/></disp-formula></sec><sec id="s3"><title>3. Solution of the Problem</title><p>With the help of discussion in the previous section, let us choose the solutions of the Equations (5)-(7) respectively as</p><disp-formula id="scirp.19984-formula7193"><label>(9)</label><graphic position="anchor" xlink:href="1-4900111\59debaa4-dbbd-48b1-9956-7e37bda9374e.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19984-formula7194"><label>(10)</label><graphic position="anchor" xlink:href="1-4900111\a0562414-1f51-48ca-a5bd-dc5e87c01c41.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19984-formula7195"><label>(11)</label><graphic position="anchor" xlink:href="1-4900111\85324f7c-dff7-487f-a75c-49816cb7fe89.jpg"  xlink:type="simple"/></disp-formula><p>Substituting from Equations (9)-(11) into Equations (5)-(8) we obtain the following equations respectively</p><disp-formula id="scirp.19984-formula7196"><label>(12)</label><graphic position="anchor" xlink:href="1-4900111\ea3078b8-5f30-4b03-9649-526408da10f0.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="1-4900111\6188a23f-2490-4f73-ac36-95cfe5e6a293.jpg" /></p><disp-formula id="scirp.19984-formula7197"><label>(A constant)(13)</label><graphic position="anchor" xlink:href="1-4900111\6063ddd4-0532-41f3-b449-4327575ef06d.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.19984-formula7198"><label>(14)</label><graphic position="anchor" xlink:href="1-4900111\e3d1b957-6bf5-4a0c-9a22-55715e6c503f.jpg"  xlink:type="simple"/></disp-formula><p>The boundary conditions become:</p><disp-formula id="scirp.19984-formula7199"><label>(15)</label><graphic position="anchor" xlink:href="1-4900111\e3a4922b-41bb-4662-a5ec-656fca90ae53.jpg"  xlink:type="simple"/></disp-formula><p>Solution of Equation (14) is as follows</p><disp-formula id="scirp.19984-formula7200"><label>(16)</label><graphic position="anchor" xlink:href="1-4900111\c8b24035-6560-4e5d-b42e-8c98817711bd.jpg"  xlink:type="simple"/></disp-formula><p>where<img src="1-4900111\b93cff59-cbe1-48ad-9248-7d8dfca94fca.jpg" />.</p><p>Using the boundary conditions Equation (15) we obtain</p><p><img src="1-4900111\e7f79e2b-8add-4750-ac1a-ed448e320885.jpg" /></p><p>Then the final form of H(y) is</p><disp-formula id="scirp.19984-formula7201"><label>(17)</label><graphic position="anchor" xlink:href="1-4900111\965f02dc-03ae-4fb1-a635-2ffa763d14a6.jpg"  xlink:type="simple"/></disp-formula><p>From Equation (11) and (17) then the temperature distribution is given by</p><disp-formula id="scirp.19984-formula7202"><label>(18)</label><graphic position="anchor" xlink:href="1-4900111\4e938c06-78b3-4c68-a36f-cf2fc6ce3972.jpg"  xlink:type="simple"/></disp-formula><p>Substituting from Equation (17) into Equation (12) we get</p><p><img src="1-4900111\75909309-c423-4931-97f2-1af915ec53a0.jpg" /></p><p>Solving the last equation to obtain F using the Equation (15) as follows The Homogenous solution:</p><p><img src="1-4900111\47317541-17eb-4b9c-8372-9dc00a59df36.jpg" /></p><p>Substitute from Equation (15) to calculate the constants <img src="1-4900111\f0bbf470-ac6d-4870-b6e4-be9008fd94e3.jpg" /></p><p><img src="1-4900111\c57f560a-df9b-48ad-8ade-7f90bb8de901.jpg" /></p><p><img src="1-4900111\d43719bf-2c35-4544-a73e-587699dc03a0.jpg" /></p><p>The particular solution is:</p><p><img src="1-4900111\581b9c91-fff2-48db-9cbb-fdb6202560a8.jpg" /></p><p>The general solution of F is</p><disp-formula id="scirp.19984-formula7203"><label>(19)</label><graphic position="anchor" xlink:href="1-4900111\6b3fe8d0-448c-45bd-a6a6-321406305cc8.jpg"  xlink:type="simple"/></disp-formula><p>From Equation (9) and Equation (19) the axial velocity of blood is given by</p><p><img src="1-4900111\f5a0aaa4-fd3f-42c1-ab29-ad790c681e00.jpg" /> (20)</p><p>Also, from Equations (10) and (13) the normal velocity is given by</p><disp-formula id="scirp.19984-formula7204"><label>(21)</label><graphic position="anchor" xlink:href="1-4900111\e2f9a2ee-327b-4d7b-b724-ab739ff4548a.jpg"  xlink:type="simple"/></disp-formula><p>where C is an arbitrary constant (C = 1).</p><p>Equations (18), (20) and (21) show the temperature distribution, the axial velocity and normal velocity respectively.</p></sec><sec id="s4"><title>4. Numerical Results and Discussion</title><p>The flow investigation has been carried out by studying the effect of individual factors like heat source and magnetic field. The main objective of the study is to find the role of heat source parameter, magnetic field (Hartmann number), Prandtl number and decay parameter on tem perature distribution, axial velocity and normal velocity. To observe these effects, numerical codes are developed for the numerical evaluations of the analytic results obtained.</p><p>In <xref ref-type="fig" rid="fig2">Figure 2</xref> we study the variation of temperature distribution versus y at <img src="1-4900111\d2d2d0b9-a6ea-4492-aeff-b7f2152468a2.jpg" /> with different values of the heat source parameter (<img src="1-4900111\f2d6c2b1-526b-4646-8e5d-9ed669a2b61f.jpg" />). We observe that for the same value of y the temperature field increases with increasing the value of heat source parameter<img src="1-4900111\2745a020-2109-45cd-bb67-d8b55f872c82.jpg" />. Also, the temperature field increases to reach at its maximum value at y = 0 then decreases.</p><p><xref ref-type="fig" rid="fig3">Figure 3</xref> gives the temperature field distribution for different values of Prandtl number (Pr = 0.50, 1.00, 3.00, 5.00, 7.00) at<img src="1-4900111\86265ad1-f45a-4781-8572-38ebce2ba760.jpg" />. It is observed that the temperature field increases with increasing the value of Prandtl number Pr. The effect of Prandtl number is the same as heat source parameter. The effect of decay parameter on the temperature field distribution at <img src="1-4900111\63dd3f8a-2185-4cd7-8e91-1f16be3494fc.jpg" /> is shown in <xref ref-type="fig" rid="fig4">Figure 4</xref>. It is shown that the temperature field decreases with increasing the decay parameter. The maximum effect of the decay parameter on the temperature field is at y = –1 and there is no effect approximately of the decay parameter on the temperature distribution at y = 1.</p><p><xref ref-type="fig" rid="fig5">Figure 5</xref> gives the axial velocity distribution for different values of heat source parameter (<img src="1-4900111\57a8460d-36e4-49b0-b916-04edd0bfc213.jpg" />= 0.50, 0.75, 1.00, 1.25, 1.50) at <img src="1-4900111\26a94f12-f487-42ac-92e1-1082515b3739.jpg" /> <img src="1-4900111\dd325c8e-0ab4-451e-95d1-7f397886ca8b.jpg" /> <img src="1-4900111\f25ba6a8-3f3e-414f-8cf0-fecd614b9f1b.jpg" /> <img src="1-4900111\d38ed31d-5a9e-4fbf-aecf-13f47ccf89a9.jpg" /> h = 0.50 <img src="1-4900111\e6a14012-2276-4d8e-8ee4-b6966f5b68b4.jpg" /> and<img src="1-4900111\0b9ba86f-9d77-40a3-8ad6-9068d07ca8f1.jpg" />. It is observed that the axial velocity increases with increasing the heat source parameter<img src="1-4900111\8da8e692-32c2-4004-b16d-36a7356bba93.jpg" />.</p><p>The effect of magnetic field on the axial velocity for different values of Hartmann number (Ha = 1.00, 2.00, 3.00, 4.00, 6.00) is shown in <xref ref-type="fig" rid="fig6">Figure 6</xref> at <img src="1-4900111\840fae47-4585-4f32-bd0a-dbdefc1df52d.jpg" /> <img src="1-4900111\abbc47af-fc41-489d-b671-df5cc92b1e6a.jpg" />, <img src="1-4900111\5d943655-9871-4dbd-86a1-202d0d6c316e.jpg" /><img src="1-4900111\18774bd0-1264-4886-9d4a-0960b4564498.jpg" /><img src="1-4900111\c6251c63-6270-496a-a9ab-45112be735af.jpg" /><img src="1-4900111\67d930e8-f91a-47d3-acfe-f22921dcb01a.jpg" /><img src="1-4900111\8b6d0932-127c-4dbb-906c-ce066f10ac5c.jpg" />and<img src="1-4900111\1d0e29f6-1a50-4dcc-bfcb-f17031c40c62.jpg" />. It is shown that the magnetic field decreases the axial velocity. We can observe that the axial velocity at <img src="1-4900111\50a0dc94-e572-4df8-a792-3be035165a7a.jpg" /> increases from y = –1</p><p>and attains maximum at y = 0 then decreases until y = 1. While at <img src="1-4900111\b5da1d6e-0715-4972-b824-eb248c8a8756.jpg" /> we observe that the axial velocity decreases along y.</p><p><xref ref-type="fig" rid="fig7">Figure 7</xref> shows the effect of Prandtl number on the distribution of the axial velocity at <img src="1-4900111\06a9ac6d-b4d5-445a-9e53-cf30e3e825ea.jpg" /> <img src="1-4900111\c8d4253b-4b08-4240-ac21-da5af0d75593.jpg" /> <img src="1-4900111\1817160d-9eb8-477f-b08f-92a5ecdc7d98.jpg" /> <img src="1-4900111\45c2d181-9c76-4636-8e31-f567ec9d8d4f.jpg" /> g = 9.81, h = 0.50, <img src="1-4900111\23c514a1-dfdf-4ca3-ac01-5ac170d82fda.jpg" />and<img src="1-4900111\24cc2b75-6cf1-4b0e-b3c5-5b6a9defd6c7.jpg" />. It is shown that the axial velocity increases with increasing the prandtl number. The effect of decay parameter is indicated in <xref ref-type="fig" rid="fig8">Figure 8</xref> at t = 1.00, <img src="1-4900111\3415fc8b-b29f-4336-a62d-6a3ed479f651.jpg" /><img src="1-4900111\d54ad3f6-fb46-4f66-8856-90a8db94b7c4.jpg" /><img src="1-4900111\5cdebe13-ad29-453e-9581-cb94808dfadf.jpg" />g = 9.81, h = 0.50, <img src="1-4900111\24ddc435-55aa-4c7e-b310-73cc591e25b5.jpg" />and<img src="1-4900111\56abc03a-4321-4760-826c-2a5d62bb5003.jpg" />. The axial velocity decreases with increasing the decay parameter. The maximum effect of the decay parameter on the axial velocity is at y = –1 and the axial velocity approximately not affected by the decay parameter at y = 1.</p><p><xref ref-type="fig" rid="fig9">Figure 9</xref> indicates the effect of decay parameter on the normal velocity distribution. It is shown that the normal velocity decreases with increasing the decay parameter. The normal velocity is decreases slowly at low values of the decay parameter (<img src="1-4900111\2310725f-cef2-43df-972b-be609f9fffb5.jpg" />) while it is decreases very fast and tends to zero at high values of decay parameter (<img src="1-4900111\82206b2e-db0a-4397-bfcb-c998e1f6810c.jpg" />).</p></sec><sec id="s5"><title>5. Conclusions</title><p>In the present investigation, a mathematical model for the unsteady blood flow through a very narrow parallel plate channel with heat source and external transverse magnetic field is presented. This work is an extensive study of Madhu et al. [<xref ref-type="bibr" rid="scirp.19984-ref8">8</xref>] with heat transfer under the conditions defined in our model. The effect of magnetic field, heat source seems to be significant.</p><p>The main conclusions of the present paper may be summarized as follows:</p><p>• The present mathematical model gives a simple form of axial velocity, temperature distribution and normal velocity of the blood flow. Analytical expressions are</p><p>obtained by choosing the axial velocity; temperature distribution and the normal velocity of blood depend on y and t only along with corresponding boundary conditions to convert the system of partial differential equations into system of ordinary differential equations.</p><p>• The temperature field increases with increasing the heat source parameter and Prandtl number while decreases with increasing the decay parameter.</p><p>• The axial velocity increases with increasing heat source parameter and Prandtl number while decreases with increasing the Hartmann number and decay parameter.</p><p>• The normal velocity decreases with increasing the decay parameter and tending to zero very fast for higher values of the decay parameter.</p><p>Hence, the present mathematical model gives a simple form of axial velocity, temperature distribution and normal velocity of the blood flow so that it will help not only people working in the field of Physiological fluid dynamics but also to the medical practitioners.</p></sec><sec id="s6"><title>6. Acknowledgements</title><p>The author would like to express deeply thankful to referee for providing valuable suggestions to improve the quality of the manuscript.</p></sec><sec id="s7"><title>REFERENCES</title></sec><sec id="s8"><title>Nomenclature</title><p><img src="1-4900111\552dbf93-e98e-43c8-8e8b-d6e085ae31f3.jpg" />: Density of blood</p><p><img src="1-4900111\21d77fc0-9ce9-4b83-8472-cef2dad78b51.jpg" />: Dynamic viscosity of the blood (constant)</p><p><img src="1-4900111\0317db0b-1aed-4b72-bf3d-baabaa886dbf.jpg" />: Pressure of blood</p><p><img src="1-4900111\fe6c6fd4-30d5-4ca8-8c52-c163a765e1ac.jpg" />: Electrical conductivity of the blood</p><p><img src="1-4900111\900103fd-3370-4ef9-aa6f-96ecf496fe0b.jpg" />: Intensity of the magnetic field</p><p><img src="1-4900111\02f49f72-7f84-4723-abd4-43b1bc8fac28.jpg" />: Gravitational acceleration</p><p><img src="1-4900111\bde8297a-b781-4e77-961f-9294a72d39d9.jpg" />: Coefficient of volume expansion due to temperature</p><p><img src="1-4900111\dabe5dc1-df1a-4f35-9c23-92503342def1.jpg" />: Temperature of blood</p><p><img src="1-4900111\eddc57e0-bc97-4f19-b68e-33a6f936691d.jpg" />: Temperature of the wall (fixed temperature)</p><p><img src="1-4900111\ed5e2cbf-2c33-4df2-a89e-7571d74852ac.jpg" />: Coefficient of the thermal conductivity</p><p><img src="1-4900111\93f3f43d-93a1-4fd6-9ee6-d2883533a8bd.jpg" />: Specific heat at constant pressure</p><p><img src="1-4900111\8fea4ce6-2064-48df-a0d5-26cbef3fad49.jpg" />: Quantity of heat</p><p><img src="1-4900111\d5361bfc-00b1-4f91-aa90-92c9da004357.jpg" />: Temperature distribution <img src="1-4900111\e8fafd2d-7319-4e5e-9b3d-3186f795facc.jpg" /></p><p><img src="1-4900111\fe777a22-c257-4d17-ac3b-f1b7933a4ac3.jpg" />: Decay parameter</p><p><img src="1-4900111\cbe2b62b-27be-498a-be9c-b27c8ad1bdfb.jpg" />: Kinematic viscosity <img src="1-4900111\1ddd5eb8-1d49-4615-8f01-2899176d46ba.jpg" /></p><p><img src="1-4900111\24a78aa8-013b-4f1c-8b7b-2964a2f2fcf7.jpg" />: Prandtl number <img src="1-4900111\affda564-017f-4082-a3cb-eaa9ca630997.jpg" /></p><p><img src="1-4900111\274342ac-892c-41eb-8267-46ef1747f149.jpg" />: Heat source parameter <img src="1-4900111\5178e8a6-1a0d-47d7-a2c7-62a25af48d6d.jpg" /></p><p><img src="1-4900111\010eb9bc-3e66-40c7-8a17-a9aa7db24765.jpg" />: Hartmann number <img src="1-4900111\7a2dfc5b-e564-4ae8-ac7c-83bd9fd353da.jpg" /></p></sec></body><back><ref-list><title>References</title><ref id="scirp.19984-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">J. 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