<?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">ACES</journal-id><journal-title-group><journal-title>Advances in Chemical Engineering and Science</journal-title></journal-title-group><issn pub-type="epub">2160-0392</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/aces.2017.74026</article-id><article-id pub-id-type="publisher-id">ACES-78727</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Chemistry&amp;Materials Science</subject></subj-group></article-categories><title-group><article-title>
 
 
  Numerical Simulation of the Shell-and-Tube Heat Exchanger: Influence of the Lower Flows and the Baffles on a Fluid Dynamics
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Sebastião</surname><given-names>José dos Santos Filho</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>Josedite</surname><given-names>Saraiva de Souza</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>Antonio</surname><given-names>Gilson Barbosa de Lima</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><aff id="aff2"><addr-line>Departament of Mechanical Engineering, Federal University of Campina Grande, Campina Grande, Brazil</addr-line></aff><aff id="aff1"><addr-line>Departament of Mechanical Engineering, UNINASSAU, Campina Grande, Brazil</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>ssgr98@yahoo.com.br(SJDSF)</email>;<email>eng.josedite@hotmail.com(JSDS)</email>;<email>antonio.gilson@dem.ufcg.edu.br(AGBDL)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>14</day><month>08</month><year>2017</year></pub-date><volume>07</volume><issue>04</issue><fpage>349</fpage><lpage>361</lpage><history><date date-type="received"><day>June</day>	<month>20,</month>	<year>2017</year></date><date date-type="rev-recd"><day>Accepted:</day>	<month>August</month>	<year>22,</year>	</date><date date-type="accepted"><day>August</day>	<month>25,</month>	<year>2017</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>
 
 
  This project proposes the numerical reproduction development of the water flow in a shell-and-tube heat exchanger 2:1 according to the CLASS C TEMA standard (for moderate operation conditions, with commercial application). With baffles in aluminum and copper tube for the cold fluid flow, the shell is in acrylic, and with thermal analysis efficiencies with regard to the presence or not of the baffles, that is to analyze the efficiency with only, the tubes and the shell and soon after the analysis with tubes and baffles. Heat exchangers are widely used equipment on an industrial and commercial scale, the application of these equipments on an industrial scale represents innovative processing solutions reflecting the processes efficiency, producing significant savings and lower cost, supporting the business success, and consequently offering opportunities, social responsibility, which are the pillars of sustainability. For the development of this work the methodology was used to calculate effectiveness, following the design parameters and contour conditions, it was analyzed the fluids behavior in the shell and the tube, through computational fluid dynamics (CFD) using the software ANSYS CFX 15.0. The results were compared with Excel generated worksheets calculated using the existing equations and correlations.
 
</p></abstract><kwd-group><kwd>Heat Exchanger</kwd><kwd> CFD</kwd><kwd> Baffles</kwd><kwd> ANSYS</kwd><kwd> CFX</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Heat transfer is thermal energy in transit, occurs due to a temperature difference in the medium and can happen by conduction, convection or irradiation. The thermal exchange process is defined as any operation or operations sequence performed on one or more materials aiming at varying its energy, composition, size or any other physicochemical properties [<xref ref-type="bibr" rid="scirp.78727-ref1">1</xref>] .</p><p>The heat exchange process between two fluids that are at different temperature gradients and are separated by a solid wall occurs in many applications within the engineering, and the equipment for this process is called a heat exchanger. Heat transfer in a heat exchanger usually involves the convection process in each fluid and conduction through the wall separating the two fluids [<xref ref-type="bibr" rid="scirp.78727-ref2">2</xref>] .</p><p>There are several types of heat exchanger, such as concentric tube heat exchangers, parallel flow, counter current, cross flow, with fin and both unmixed fluids, shell and tube heat exchanger with baffles, which is referenced in this project.</p><p>Several methods are used to analyze the shell-and-tube heat exchanger variables. Some of them belong to technical literature, such as the Kern method [<xref ref-type="bibr" rid="scirp.78727-ref3">3</xref>] , which focuses mainly on the load losses and the laminar flow process, Bell [<xref ref-type="bibr" rid="scirp.78727-ref3">3</xref>] , which focuses on the experimental data being the best in relation to the literature methods and Tinker, which focuses on the flow division for the heat transfer analysis and loss of charge in each series. Others occur through advanced software, which allows more accurate results, such as HTRI (Heat Transfer Research Inc, in USA) and HTFS (Heat Transfer and Fluid Flow Service, in England).</p><p>Given their wide use on an industrial scale, heat exchangers are highly important equipment in any global scenario, as they are responsible for the greatest energy demands, as well as they are process equipment, responsible for all industry processing such as footwear, beverage and other industries. Their wide spread application can be attributed to ease of manufacture from a variety of materials. Moreover, there is no limit on the operating temperature and pressure [<xref ref-type="bibr" rid="scirp.78727-ref4">4</xref>] .</p><p>Looking for ways that will make these equipment’s more efficient, increasing their capacity for thermal exchange and reducing the investment necessary for their construction are the study object of various researches. However, its use is not restricted only to the industrial environment, being present in the daily of people in various forms such as: refrigerators, heaters, electric showers air conditioners, among others, forcing even more researchers to create sustainable projects that have to be efficient, affordable and less costly.</p><p>The performance of these exchangers can be optimized by inserting baffles in the shell to direct the flow of fluid across the tubes on shell side [<xref ref-type="bibr" rid="scirp.78727-ref5">5</xref>] presented a heat exchanger to be able to the heat recovery from geothermal brine for additional power generation. The results indicated that the heat exchanger can be applied for the evaporator of the model Organic Rankine Cycle power plant.</p><p>[<xref ref-type="bibr" rid="scirp.78727-ref6">6</xref>] presented an experimental analysis of the performance on the shell-and-tube type heat exchanger containing segmental baffles at three angular orientations (θ), the authors concluded that, when angle inclination increases from 0˚ to 60˚, the heat transfer coefficient value increases due to increase in swirl.</p><p>In this sense, this project aims to reproduce numerically the water flow in a 2:1 shell-tube exchanger. Initially the analysis of the mass flow rates variation in the shell and the tube and its effects on the thermal exchange is made. Later, baffles are added to verify how they act on the thermal exchange efficiency. The results are compared to the heat exchanger design using the Transfer Unit Number (NUT) method to provide credibility to the mathematical modeling used.</p></sec><sec id="s2"><title>2. Methodology</title><sec id="s2_1"><title>2.1. Study Domain</title><p>The study domain is defined by shell-and-tube heat exchangers (<xref ref-type="fig" rid="fig1">Figure 1</xref> and <xref ref-type="fig" rid="fig2">Figure 2</xref>). In the first one the domain dimensions are high-lighted, and in the second one the dimensions are the same to the previous. Details of baffles are show in the <xref ref-type="fig" rid="fig3">Figure 3</xref>, and they are in a distance of 4.88 cm.</p><p>Using the ANSYS CFX software was constructed on the domains tetrahedral mesh, with 625,398 and 1,828,214 tetrahedral elements, according to <xref ref-type="fig" rid="fig4">Figure 4</xref> and <xref ref-type="fig" rid="fig5">Figure 5</xref>.</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Domain geometry without baffles</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-3700835x2.png"/></fig><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Domain geometry with baffles</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-3700835x3.png"/></fig><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Details of a baffle</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-3700835x4.png"/></fig><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Tetrahedral mesh on domain without baffles containing 625,398 tetrahedral elements</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-3700835x5.png"/></fig><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Tetrahedral mesh on domain with baffles containing 1,828,214 tetrahedral elements</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-3700835x6.png"/></fig></sec><sec id="s2_2"><title>2.2. Mathematical Modeling</title><sec id="s2_2_1"><title>2.2.1. Simulation Considerations</title><p>The studied flow is based on the following considerations:</p><p>1) Permanent and turbulent flow;</p><p>2) The fluid is Newtonian and incompressible and the physicochemical properties are constants;</p><p>3) Non-isothermal process;</p><p>4) There is no occurrence of chemical reactions;</p><p>5) It was not considered the gravitational effect;</p><p>6) No mass and momentum transfer at the interface;</p><p>7) The interfacial drag forces (forces of lift, wall lubrication, virtual mass, pressure and turbulent dispersion of solid) were neglected;</p><p>8) The fluid circulating in the shell and in the tube is water.</p></sec><sec id="s2_2_2"><title>2.2.2. Calculation Memory of the Heat Exchanger</title><p>For the calculation of the Nusselt coefficient on the tubes side, the correlation proposed by Petukhov, found in [<xref ref-type="bibr" rid="scirp.78727-ref7">7</xref>] , were used, which is valid for the Reynolds range of 10 ≤ Re ≤ 5 &#215; 10 and Prandtl 0.5 ≤ Pr ≤ 2000, in the way:</p><disp-formula id="scirp.78727-formula29"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x7.png"  xlink:type="simple"/></disp-formula><p>where f is the friction factor.</p><p>The Nusselt number is a dimensionless one that relates the convective heat transfer with diffusive transfer being defined as:</p><disp-formula id="scirp.78727-formula30"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x8.png"  xlink:type="simple"/></disp-formula><p>where h is the heat transfer coefficient (W・m<sup>−2</sup>・K<sup>−1</sup>), D is the diameter (m) and K is the thermal conductivity of the material (W・m<sup>−</sup><sup>1</sup>・K<sup>−1</sup>).</p><p>The friction factor defined for flow in smooth tubes according to the correlation proposed by Petukhov [<xref ref-type="bibr" rid="scirp.78727-ref7">7</xref>] and valid for a range of Reynolds number of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-3700835x9.png" xlink:type="simple"/></inline-formula> it is given by:</p><disp-formula id="scirp.78727-formula31"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x10.png"  xlink:type="simple"/></disp-formula><p>On the shell side, the correlation proposed by Mcadms [<xref ref-type="bibr" rid="scirp.78727-ref8">8</xref>] was used for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-3700835x11.png" xlink:type="simple"/></inline-formula>:</p><disp-formula id="scirp.78727-formula32"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x12.png"  xlink:type="simple"/></disp-formula><p>where the Reynolds number is defined as the equivalent diameter on the shell side, which takes into consideration the wet perimeter and the free area for the flow.</p><p>The equivalent diameter varies according to the arrangement of tubes, which may be triangular or square, and is calculated by the equation below [<xref ref-type="bibr" rid="scirp.78727-ref8">8</xref>] :</p><disp-formula id="scirp.78727-formula33"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x13.png"  xlink:type="simple"/></disp-formula><p>where d<sub>0</sub> (m) is the tubes outer diameter.</p><p>Thus, the Reynolds number on the shell side becomes:</p><disp-formula id="scirp.78727-formula34"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x14.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-3700835x15.png" xlink:type="simple"/></inline-formula> (kg/s) is the total mass flow defined as a function of the cross-sectional area of the flow direction which is free to flow.</p><p>The area <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-3700835x16.png" xlink:type="simple"/></inline-formula> of the external surface of the tubes is defined as:</p><disp-formula id="scirp.78727-formula35"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x17.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-3700835x18.png" xlink:type="simple"/></inline-formula> (m) is the shell diameter, B (m) is the spacing between the baffles and C (m) and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-3700835x19.png" xlink:type="simple"/></inline-formula> (m) are the distances between the tubes edges and the distance between the center of one tube and the center of the other, respectively, determined according to the arrangement chosen.</p><p>It can be easily verified that the spacing between the baffles relates to the baffles quantity by the following equation, since the baffle length is fixed:</p><disp-formula id="scirp.78727-formula36"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x20.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-3700835x21.png" xlink:type="simple"/></inline-formula> is the baffles number and L (m) is the shell length.</p><p>From the individual exchange coefficients and knowing the steel thermal conductivity, the global heat transfer coefficient was determined with the following equation:</p><disp-formula id="scirp.78727-formula37"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x22.png"  xlink:type="simple"/></disp-formula><p>where D<sub>i</sub> (m) is the tubes inside diameter.</p><p>In some cases, it is necessary to take into account the flux resistance exerted by fouling, both of the tube and the case, for the heat transfer overall coefficient. However, as treated water is used in the present study, these resistances are dispensed without causing great interference to the design.</p><p>Determining the thermal capacities by multiplying the flow by their respective specific heat capacities, where the efficiency calculation is based on the maximum heat that can be transferred to or from the current with less transfer capacity.</p><disp-formula id="scirp.78727-formula38"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x23.png"  xlink:type="simple"/></disp-formula><p>where T<sub>qi</sub> is the initial hot fluid temperature and T<sub>fi</sub> is the initial cold fluid temperature.</p><p>The NUT indicates the actual area of heat exchange, thus, for the same values of minimum transfer capacity and global coefficient, the larger the NUT, the larger the physical dimension of the equipment. The NUT is the measure of the size of the exchanger, determined by the equation below:</p><disp-formula id="scirp.78727-formula39"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x24.png"  xlink:type="simple"/></disp-formula><p>With NUT and C<sub>min</sub>, the effectiveness of the exchanger is [<xref ref-type="bibr" rid="scirp.78727-ref7">7</xref>] :</p><disp-formula id="scirp.78727-formula40"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x25.png"  xlink:type="simple"/></disp-formula><p>where C is the relationship between C<sub>min</sub> and C<sub>max</sub>.</p><p>Given the effectiveness and the maximum exchange capacity, it is possible to find the heat transfer between the currents and the thermal conditions of both at the outlet of the shell and tube heat exchanger, as well as the Mean Logarithm of Temperature Differences (MLDT).</p><disp-formula id="scirp.78727-formula41"><label>(13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x26.png"  xlink:type="simple"/></disp-formula><p>where the temperature differences are defined by:</p><disp-formula id="scirp.78727-formula42"><label>(14)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x27.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.78727-formula43"><label>(15)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x28.png"  xlink:type="simple"/></disp-formula><p>For the method (MLDT) the dimensionless parameters P and R are determined:</p><disp-formula id="scirp.78727-formula44"><label>(16)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x29.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.78727-formula45"><label>(17)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x30.png"  xlink:type="simple"/></disp-formula><p>where R is the ratio of the fluids heat capacities and P represents the thermal effectiveness with respect to the cold fluid.</p><p>As the flow is not totally countercurrent, it is necessary to use the (MLDT) in which the correction factor F is determined by the equation for exchangers with 2 passes in the tubes and one in the shell [<xref ref-type="bibr" rid="scirp.78727-ref9">9</xref>] :</p><disp-formula id="scirp.78727-formula46"><label>(18)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x31.png"  xlink:type="simple"/></disp-formula><p>where S is defined as:</p><disp-formula id="scirp.78727-formula47"><label>(19)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x32.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.78727-formula48"><label>(20)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x33.png"  xlink:type="simple"/></disp-formula><p>where n is the passes number in the tubes.</p><p>With this the final MLDT, corrected the effects of the flows against currents and cross flow is given by:</p><disp-formula id="scirp.78727-formula49"><label>(21)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x34.png"  xlink:type="simple"/></disp-formula><p>If the temperature difference is known, the required exchange area can be determinate so that the project condition is reached, verifying that the existing area is sufficient for the continuity of the process.</p><p>It was also carried out the calculation of the load losses in order to carry out the sizing of the pump system to be used in the experiment, so on the pipes side, the localized losses were considered, i.e. those generated due to the obstructions, Valves, knees, etc. As well as the losses distributed throughout the pipe.</p><p>On the shell side, besides the localized and distributed losses along the pipeline, a calculation is also necessary to consider the effects of the various factors of construction of the exchanger, such as the arrangement of the bundle of pipes, quantity and spacing between the baffles, baffles cuts, and others. The load loss inside the shell [<xref ref-type="bibr" rid="scirp.78727-ref9">9</xref>] can be determined by equation:</p><disp-formula id="scirp.78727-formula50"><label>(22)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x35.png"  xlink:type="simple"/></disp-formula><p>where φ<sub>S</sub> is:</p><disp-formula id="scirp.78727-formula51"><label>(23)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x36.png"  xlink:type="simple"/></disp-formula><p>The friction factor [<xref ref-type="bibr" rid="scirp.78727-ref8">8</xref>] valid for flow in shell and tube heat exchangers for the Reynolds range of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-3700835x37.png" xlink:type="simple"/></inline-formula> is given by the equation:</p><disp-formula id="scirp.78727-formula52"><label>(24)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x38.png"  xlink:type="simple"/></disp-formula></sec><sec id="s2_2_3"><title>2.2.3. Governing Equations</title><p>The permanent equations considered in the mathematical modeling were the conservation of linear momentum (Equation (25)), mass (Equation (26)) and energy (Equation (27)).</p><disp-formula id="scirp.78727-formula53"><label>(25)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x39.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.78727-formula54"><label>(26)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x40.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.78727-formula55"><label>(27)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x41.png"  xlink:type="simple"/></disp-formula><p>Using the NUT method, the maximum thermal exchange value, Q<sub>max</sub>, is obtained from the input temperature values of the fluids, and Mean Logarithm of Temperature Differences (MLDT) method allows to find the value of the Real thermal exchange, Q, using the inlet and outlet temperatures. The effectiveness, ε, is given by:</p><disp-formula id="scirp.78727-formula56"><label>(28)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x42.png"  xlink:type="simple"/></disp-formula><p>The relative error, E, is given from the V<sub>exp</sub> expected value and V<sub>obt</sub> values obtained by:</p><disp-formula id="scirp.78727-formula57"><label>(29)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-3700835x43.png"  xlink:type="simple"/></disp-formula></sec><sec id="s2_2_4"><title>2.2.4. Physical and Chemical Properties</title><p>The properties of the water used in the present work are:</p><p>・ Water viscosity: 8.899 E<sup>−4</sup> Pa・s;</p><p>・ Water Density: 997 kg/m<sup>3</sup>.</p></sec><sec id="s2_2_5"><title>2.2.5. Simulated Cases</title><p>The boundary conditions of the simulated cases are shown below (<xref ref-type="table" rid="table1">Table 1</xref>).</p></sec></sec></sec><sec id="s3"><title>3. Results and Discussion</title><p>The study to obtain the results of the numerical reproduction of the water flow in a shell-and-tube heat exchanger was analyzed in three fundamental phases (<xref ref-type="table" rid="table2">Table 2</xref>). The first analysis focused on the temperatures and flows of the water masses used as contour conditions without baffles generating cases 1 and 2. The second analysis without and with the baffles, comparing cases 2 and 3.</p><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Simulated cases</title></caption><table><tbody><thead><tr><th align="center" valign="middle" ></th><th align="center" valign="middle" ></th><th align="center" valign="middle" >Case 1</th><th align="center" valign="middle" >Case 2</th><th align="center" valign="middle" >Case 3</th></tr></thead><tr><td align="center" valign="middle"  rowspan="2"  >Shell Inlet</td><td align="center" valign="middle" >Temperature [˚C]</td><td align="center" valign="middle" >25</td><td align="center" valign="middle" >25</td><td align="center" valign="middle" >25</td></tr><tr><td align="center" valign="middle" >Mass Flow [kg/s]</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >1</td></tr><tr><td align="center" valign="middle" >Shell Outlet</td><td align="center" valign="middle" >Pressure [Pa]</td><td align="center" valign="middle" >101,325</td><td align="center" valign="middle" >101,325</td><td align="center" valign="middle" >101,325</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >Tube Inlet</td><td align="center" valign="middle" >Temperature [˚C]</td><td align="center" valign="middle" >40</td><td align="center" valign="middle" >80</td><td align="center" valign="middle" >80</td></tr><tr><td align="center" valign="middle" >Mass Flow [kg/s]</td><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >0.5</td></tr><tr><td align="center" valign="middle" >Tube Outlet</td><td align="center" valign="middle" >Pressure [Pa]</td><td align="center" valign="middle" >101,325</td><td align="center" valign="middle" >101,325</td><td align="center" valign="middle" >101,325</td></tr><tr><td align="center" valign="middle"  colspan="2"  >Baffles</td><td align="center" valign="middle" >Without</td><td align="center" valign="middle" >Without</td><td align="center" valign="middle" >With</td></tr></tbody></table></table-wrap><table-wrap id="table2" ><label><xref ref-type="table" rid="table2">Table 2</xref></label><caption><title> Average temperatures of the water in the sections of outlet, error and efficiency of the thermal exchange</title></caption><table><tbody><thead><tr><th align="center" valign="middle" ></th><th align="center" valign="middle" >Outlets</th><th align="center" valign="middle" >NUT</th><th align="center" valign="middle" >Numerical Results</th><th align="center" valign="middle" >Error (%)</th><th align="center" valign="middle" >Effectiveness (%)</th></tr></thead><tr><td align="center" valign="middle"  rowspan="2"  >Case 1 Without baffles</td><td align="center" valign="middle" >Tube</td><td align="center" valign="middle" >25.6˚C</td><td align="center" valign="middle" >27.1˚C</td><td align="center" valign="middle" >6%</td><td align="center" valign="middle"  rowspan="2"  >26.3%</td></tr><tr><td align="center" valign="middle" >Shell</td><td align="center" valign="middle" >28.9˚C</td><td align="center" valign="middle" >39.6˚C</td><td align="center" valign="middle" >37%</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >Case 2 With baffles</td><td align="center" valign="middle" >Tube</td><td align="center" valign="middle" >28.6˚C</td><td align="center" valign="middle" >32.7˚C</td><td align="center" valign="middle" >14%</td><td align="center" valign="middle"  rowspan="2"  >5.3%</td></tr><tr><td align="center" valign="middle" >Shell</td><td align="center" valign="middle" >35.8˚C</td><td align="center" valign="middle" >78.5˚C</td><td align="center" valign="middle" >119%</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >Case 3 With baffles</td><td align="center" valign="middle" >Tube</td><td align="center" valign="middle" >28.6˚C</td><td align="center" valign="middle" >42.3˚C</td><td align="center" valign="middle" >48%</td><td align="center" valign="middle"  rowspan="2"  >8.3%</td></tr><tr><td align="center" valign="middle" >Shell</td><td align="center" valign="middle" >35.8˚C</td><td align="center" valign="middle" >77.9˚C</td><td align="center" valign="middle" >117%</td></tr></tbody></table></table-wrap><p>About the stream lines, it can be stated that the turbulences inside the bafflesless heat exchanger exhibit similar behavior regardless of the mass flow rate of the flow, as shown in <xref ref-type="fig" rid="fig6">Figure 6</xref>(a) and <xref ref-type="fig" rid="fig6">Figure 6</xref>(b). The baffles presence has as its</p><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> Fluid velocity stream lines for cases (a) 1, (b) 2 and (c) 3</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-3700835x44.png"/></fig><p>main function to change the flow direction with the aim of increase the rate heat transfer and, as can be seen in <xref ref-type="fig" rid="fig6">Figure 6</xref>, the current lines are modified.</p><p>By analyzing the pressure fields on the exchanger shell, it is noticed that the increase of the mass flow rates results in a greater pressure in its structure, which is a point that must be considered in the exchanger design (<xref ref-type="fig" rid="fig7">Figure 7</xref>). Regarding</p><fig id="fig7"  position="float"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> Pressure field on the exchanger shell for cases (a) 1, (b) 2 and (c) 3</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-3700835x45.png"/></fig><p>the baffles presence, they interfere directly in the pressure field, with a greater distributed load loss occurring. From the temperature fields, it is been noticed that the increase in the temperature at the entrance of the shell increased the temperature gradient along the exchanger, according to <xref ref-type="fig" rid="fig8">Figure 8</xref>(a) and <xref ref-type="fig" rid="fig8">Figure 8</xref>(b). It is also observed that the baffles presence increased the thermal exchange.</p><fig id="fig8"  position="float"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> Temperature field for cases (a) 1, (b) 2 and (c) 3</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-3700835x46.png"/></fig></sec><sec id="s4"><title>4. Conclusions</title><p>As reported in the development of this article, the design of a shell-and-tube heat exchanger is quite complex, requiring a good knowledge regarding its variables mainly regarding their velocity. However, our focus was related to flow rates and temperatures aiming this study for a later work.</p><p>The conclusions about this work were:</p><p>・ Mathematical modeling describes with satisfaction the phenomenon of flow in shell-and-tube heat exchangers, according to the results in the tables presented.</p><p>・ Current lines, pressure and temperature fields behave as expected physically.</p><p>・ The increase of the mass flow rates results in a greater pressure.</p><p>・ The baffles presence significantly increases the thermal exchange efficiency.</p><p>・ The temperature increase at the shell entrance increased the temperature gradient along the exchanger.</p></sec><sec id="s5"><title>Acknowledgements</title><p>Thanks to Professor Antonio Gilson for the availability of the Computational Laboratory of Thermal and Fluids (LCTF-UFCG) and Professor Josedite Saraiva for the valuable lessons.</p></sec><sec id="s6"><title>Cite this paper</title><p>dos Santos Filho, S.J., de Souza, J.S. and de Lima, A.G.B. 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