<?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">MME</journal-id><journal-title-group><journal-title>Modern Mechanical Engineering</journal-title></journal-title-group><issn pub-type="epub">2164-0165</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/mme.2017.72005</article-id><article-id pub-id-type="publisher-id">MME-76071</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></subj-group></article-categories><title-group><article-title>
 
 
  Numerical Study of Heat Transfer and Flow Bifurcation of CuO Nanofluid in Sudden Expansion Microchannel Using Two-Phase Model
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Farhad</surname><given-names>A. Abbassi</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Mohsen</surname><given-names>Nazari</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Mohammad</surname><given-names>Mohsen Shahmardan</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>School of Mechanical Engineering, Shahrood University, Shahrood, Iran</addr-line></aff><pub-date pub-type="epub"><day>10</day><month>05</month><year>2017</year></pub-date><volume>07</volume><issue>02</issue><fpage>57</fpage><lpage>72</lpage><history><date date-type="received"><day>March</day>	<month>13,</month>	<year>2017</year></date><date date-type="rev-recd"><day>Accepted:</day>	<month>May</month>	<year>7,</year>	</date><date date-type="accepted"><day>May</day>	<month>10,</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>
 
 
  In this paper, laminar forced convection of CuO nanofluid is numerically investigated in sudden expansion microchannel with isotherm walls and different expansion ratios (ER). An Eulerian two-fluid model is considered to simulate the nanofluid flow inside the microchannel and the governing mass, momentum and energy equations for both phases are solved using the finite volume method. Eulerian-Eulerian two-phase model is very efficient because of considering the relative velocity and temperature of the phases and the nanoparticle concentration distribution. In solving the flow equations for both phases, the SIMPLE algorithm is modified for the coupling of the velocity and pressure and the continuity equations for both phases are combined in order to create the pressure correction equations. However, the Eulerian-Eulerian modeling results show higher heat transfer enhancement in comparison to pure water, so that for a 2% copper-water nanofluid, it has been observed a 35% increase of the heat transfer. The heat transfer enhancement increases with increase in Reynolds number and nanoparticle volume concentration, while the pressure drop increases only slightly. An investigation of the expansion ratio of microchannel shows that the average Nusselt number increases with decrease in expansion ratio as well as with increase in Reynolds number. Also, the Bifurcation has been occurred in higher Reynolds number that is different for each expansion ratio of the microchannel.
 
</p></abstract><kwd-group><kwd>Heat Transfer</kwd><kwd> Nanofluid</kwd><kwd> Sudden Expansion Microchannel</kwd><kwd> Two-Phase</kwd><kwd> Eulerian-Eulerian</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The term nanofluid was used by Choi [<xref ref-type="bibr" rid="scirp.76071-ref1">1</xref>] for the first time. After that many researchers continued his works and focused on the modeling of the thermal conductivity of nanofluid [<xref ref-type="bibr" rid="scirp.76071-ref2">2</xref>] [<xref ref-type="bibr" rid="scirp.76071-ref3">3</xref>] [<xref ref-type="bibr" rid="scirp.76071-ref4">4</xref>] . Recently, the concentration is on the heat transfer and fluid flow behavior of nanofluid.</p><p>Most experimental studies for nanofluid are done on macro and micro-scales [<xref ref-type="bibr" rid="scirp.76071-ref5">5</xref>] [<xref ref-type="bibr" rid="scirp.76071-ref6">6</xref>] [<xref ref-type="bibr" rid="scirp.76071-ref7">7</xref>] [<xref ref-type="bibr" rid="scirp.76071-ref8">8</xref>] . Wen and Ding [<xref ref-type="bibr" rid="scirp.76071-ref5">5</xref>] studied the heat transfer of Al<sub>2</sub>O<sub>3</sub> -water nanofluid in a copper tube under the constant heat flux. Their measurements in the heat transfer of Al<sub>2</sub>O<sub>3</sub> -water nanofluid showed an enhancement in the entrance region of the tube. They explained that the particle migration reduces the thickness of the thermal boundary layer and causes this behavior in the heat transfer of the nanofluid. Heris et al. [<xref ref-type="bibr" rid="scirp.76071-ref6">6</xref>] investigated CuO-water and Al<sub>2</sub>O<sub>3</sub> -wa- ter nanofluids in an annular tube. They compared the results of the experimental study and the homogeneous model and realized the under-estimation of the homogeneous model in the heat transfer enhancement, especially in higher nanoparticle volume concentration. Homogeneous (single phase) and two-phase models are commonly used in the numerical study of the heat transfer and fluid flow of the nanofluid. In single phase model, the velocity and temperature of the base fluid and the particles are the same. Most studies in this field are done by using the single phase model [<xref ref-type="bibr" rid="scirp.76071-ref3">3</xref>] [<xref ref-type="bibr" rid="scirp.76071-ref9">9</xref>] [<xref ref-type="bibr" rid="scirp.76071-ref10">10</xref>] . In the two-phase model, the base fluid and particles are considered as two different phases in despite of the single phase model and both phases have different velocities and temperatures. Also, the interactions between the phases are so important in the governing equations of the two-phase models.</p><p>Behzadmehr et al. [<xref ref-type="bibr" rid="scirp.76071-ref11">11</xref>] studied the turbulent convection of the nanofluid in a circular tube by using a two phase mixture model. After comparing their results with an experimental study, they reported that the mixture model has more coincidence to the experimental study compared to the homogeneous model. Mirmasoumi and Behzadmehr [<xref ref-type="bibr" rid="scirp.76071-ref12">12</xref>] also used the two phase mixture model for studying the mixed convection of the nanofluid in a tube. Mirmasoumi and Behzadmehr [<xref ref-type="bibr" rid="scirp.76071-ref13">13</xref>] and Akbarinia and Laur [<xref ref-type="bibr" rid="scirp.76071-ref14">14</xref>] studied the effect of the nanoparticle size on the mixed convection of the nanofluid by the mixture model. An increase in the heat transfer of the nanofluid with decrease in the nanoparticle size was observed in both studies. Kurowski et al. [<xref ref-type="bibr" rid="scirp.76071-ref15">15</xref>] simulated the nanofluid flow by three different mixtures, homogeneous and Eulerian-Lagrangian models in a minichannel. The results of all models were almost the same. Fard et al. [<xref ref-type="bibr" rid="scirp.76071-ref16">16</xref>] used single and two-phase models for studying the heat transfer of the nanofluid inside a tube. They investigated a 0.2% CuO-water and compared the results with experimental ones and reported that the average relative error between the two-phase model and experimental data was 8% while it was 16% for the single phase model.</p><p>Mohammad Kalteh et al. [<xref ref-type="bibr" rid="scirp.76071-ref17">17</xref>] investigated the nanofluid forced convection experimentally and numerically inside a wide microchannel heat sink. They used two-phase Eulerian-Eulerian model in numerical method and reported that the average Nusselt number increases with increase in Reynolds number and nanoparticle volume concentration. Keshavarz and Mohammadi [<xref ref-type="bibr" rid="scirp.76071-ref18">18</xref>] investigated the thermal performance of Al<sub>2</sub>O<sub>3</sub> -water nanofluid in minichannel heat sink by using single and two-phase models. In their study, it has been observed that the two-phase models have more coincidence with the experimental results in comparison to the single phase model, however, it is not sensible in low volume concentration but by increasing the particle volume concentration up to 1% or in high Reynolds number, the deviation between the single phase model and the experimental data increases. Shariat et al. [<xref ref-type="bibr" rid="scirp.76071-ref19">19</xref>] studied the impact of nanoparticle mean diameter and the buoyancy force on laminar mixed convection nanofluid flow in an elliptic duct by using two-phase mixture model. They reported that in certain Reynolds and Richardson numbers, the average Nusselt number increases with decrease in the nanoparticle diameter as well as with increase in Richardson number.</p><p>In this paper, the nanofluid flow and laminar forced convection in a sudden expansion microchannel with different expansion ratio and isotherm walls are studied by using the Eulerian-Eulerian two-phase model. The governing equations of mass, momentum and energy are discretized using the finite volume method and the modified SIMPLE algorithm is used for solving the flow equations of both phases. Also, the effects of the nanoparticle size and volume concentration and Reynolds number on the average Nusselt number are investigated. Considering the importance of the microfluidic systems and the field of nanofluid heat transfer, the investigation of the flow and heat transfer of nanofluid in a microfluidic device like a sudden expansion microchannel can be so important and practical. In expansion microchannels, the effective hydraulic diameter decreases because of the vortex creation that increases the resistance of the fluid flow. In fact, the sudden expansion microchannels can be used as a microfluidic rectifier, like: Tesla rectifier, simple nozzle/diffuser structures and cascaded nozzle/diffuser structures. These rectifiers are valveless and do the rectification with different flow resistance in the forward flow and the reverse one. On the other hand, two-phase models are proper substitution for a single phase model. Among two-phase models, the Eulerian-Eulerian model has good efficiency because of considering the relative velocity and temperature between phases and the nanoparticle volume concentration distribution.</p><p>Numerical investigation of nanofluid flow and heat transfer in a sudden expansion microchannel by using the Eulerian-Eulerian two-phase model and applying the modified SIMPLE algorithm is a new work in the field of nanofluid heat transfer in a microfluidic system.</p></sec><sec id="s2"><title>2. Governing Equations</title><p>In this study, the geometry is the sudden expansion microchannel with different expansion ratios. <xref ref-type="fig" rid="fig1">Figure 1</xref> is a schematic of the sudden expansion microchannel. The laminar flow of the mixture of water and copper nanoparticles, enters the microchannel with uniform velocity and temperature and the heat transfer</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> The sudden expansion microchannel</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1860330x2.png"/></fig><p>occurs between the nanofluid and the isothermal walls of the microchannel. The upstream length and height of the microchannel<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x3.png" xlink:type="simple"/></inline-formula>, the downstream length and height of microchannel <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x4.png" xlink:type="simple"/></inline-formula> and the reattachment length after the expansion region (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x5.png" xlink:type="simple"/></inline-formula> ) are shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>.</p><p>Considering the Eulerian-Eulerian two-phase model and the steady state, laminar and two-dimensional flow of nanofluid, the governing equations for the base liquid and nanoparticle phases can be written as follows.</p><sec id="s2_1"><title>2.1. Continuity Equations</title><p>Continuity equations for solid and liquid phases in the cartesian coordinate system are as follows [<xref ref-type="bibr" rid="scirp.76071-ref20">20</xref>] [<xref ref-type="bibr" rid="scirp.76071-ref21">21</xref>] :</p><disp-formula id="scirp.76071-formula51"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x6.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.76071-formula52"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x7.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x8.png" xlink:type="simple"/></inline-formula> , ρ and φ are velocity vector, density and volume concentration, respectively. Subscripts l and p show the base liquid and nanoparticle phases, respectively. Also, for volume concentration of the phases we have</p><disp-formula id="scirp.76071-formula53"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x9.png"  xlink:type="simple"/></disp-formula></sec><sec id="s2_2"><title>2.2. Momentum Equations</title><p>Momentum equations for solid and liquid phases in cartesian coordinate system are as follows:</p><disp-formula id="scirp.76071-formula54"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x10.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.76071-formula55"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x11.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x12.png" xlink:type="simple"/></inline-formula> , <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x13.png" xlink:type="simple"/></inline-formula> , <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x14.png" xlink:type="simple"/></inline-formula> , P and &#181; are the particle-particle interaction, drag, virtual mass (added mass) forces, pressure and viscosity, respectively. Here, the lift force between the phases can be neglected because of the small size of the nanoparticles and the gravitational force is neglected because of the small size of the microchannel.</p><p>The force terms in the momentum equations are defined as</p><disp-formula id="scirp.76071-formula56"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x15.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.76071-formula57"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x16.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.76071-formula58"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x17.png"  xlink:type="simple"/></disp-formula><p>The friction coefficient β, drag coefficient<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x18.png" xlink:type="simple"/></inline-formula>, the particle-particle interaction modulus G and the particle Reynolds namber are</p><disp-formula id="scirp.76071-formula59"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x19.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.76071-formula60"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x20.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.76071-formula61"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x21.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.76071-formula62"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x22.png"  xlink:type="simple"/></disp-formula><p>Here, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x23.png" xlink:type="simple"/></inline-formula> is the nanoparticle diameter.</p><p>Equation (9) is valid for <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x24.png" xlink:type="simple"/></inline-formula> . Also, it should be considered that Equations (8)-(14) are not obtained for nano-sized particles. But, they can be used for nanoparticles because of the lack of the proper correlations for nano-sized particles [<xref ref-type="bibr" rid="scirp.76071-ref22">22</xref>] .</p></sec><sec id="s2_3"><title>2.3. Energy Equations</title><p>The base fluid and particle phases are considered as incompressible fluids and the viscous dissipation and radiation are neglected. So, the energy equations in cartesian coordinate system can be written as</p><disp-formula id="scirp.76071-formula63"><label>(13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x25.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.76071-formula64"><label>(14)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x26.png"  xlink:type="simple"/></disp-formula><p>Here, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x27.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x28.png" xlink:type="simple"/></inline-formula> , <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x29.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x30.png" xlink:type="simple"/></inline-formula> are the temperature, effective thermal conductivity, heat capacity at constant pressure and volume interphase heat transfer coefficient, respectively. For spherical nanoparticles <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x28.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x29.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x30.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x31.png" xlink:type="simple"/></inline-formula> can be calculated as</p><disp-formula id="scirp.76071-formula65"><label>(15)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x32.png"  xlink:type="simple"/></disp-formula><p>Here, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x33.png" xlink:type="simple"/></inline-formula> is the fluid-particle heat transfer coefficient that is obtained from experimental correlations.</p><disp-formula id="scirp.76071-formula66"><label>(16)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x34.png"  xlink:type="simple"/></disp-formula><p>where Pr is the base liquid Prandtl number.</p><p>The effective thermal conductivities for both phases are</p><disp-formula id="scirp.76071-formula67"><label>(17)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x35.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.76071-formula68"><label>(18)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x36.png"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.76071-formula69"><label>(19)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x37.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.76071-formula70"><label>(20)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x38.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.76071-formula71"><label>(21)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x39.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.76071-formula72"><label>(22)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x40.png"  xlink:type="simple"/></disp-formula><p>For spherical nanoparticles</p><disp-formula id="scirp.76071-formula73"><label>(23)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x41.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.76071-formula74"><label>(24)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x42.png"  xlink:type="simple"/></disp-formula><p>Equations (18)-(25) are not obtained for nano-sized particles. But these correlations are used because of the lack of the appropriate correlations for nano- sized particles [<xref ref-type="bibr" rid="scirp.76071-ref22">22</xref>] .</p><p>The Nusselt number is calculated from the temperature difference between the nanofluid mean temperature and the microchannel walls:</p><disp-formula id="scirp.76071-formula75"><label>(25)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x43.png"  xlink:type="simple"/></disp-formula><p>Here, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x44.png" xlink:type="simple"/></inline-formula> , <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x44.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x45.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x44.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x45.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x46.png" xlink:type="simple"/></inline-formula> are the wall convective heat transfer flux, convective heat transfer coefficient and the microchannel hydraulic diameter, respectively. The mean temperature of the nanofluid is calculated as follow</p><disp-formula id="scirp.76071-formula76"><label>(26)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x47.png"  xlink:type="simple"/></disp-formula><p>where the integration is applied on the microchannel cross section.</p><p>According to the Equations (15) and (16), the wall convective heat transfer flux can be obtained as</p><disp-formula id="scirp.76071-formula77"><label>(27)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x48.png"  xlink:type="simple"/></disp-formula><p>Considering the local heat transfer coefficient, the average heat transfer coefficient is</p><disp-formula id="scirp.76071-formula78"><label>(28)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x49.png"  xlink:type="simple"/></disp-formula></sec><sec id="s2_4"><title>2.4. Non-Dimensionalization</title><p>The non-dimensional parameters using in converting the governing equations are as follows:</p><disp-formula id="scirp.76071-formula79"><label>(29)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x50.png"  xlink:type="simple"/></disp-formula><p>where i = l, p indicates the liquid and particle phases.</p></sec><sec id="s2_5"><title>2.5. Boundary Conditions</title><p>At the inlet, the mixture of water and copper nanoparticles enters the sudden expansion microchannel with the same uniform axial velocity. At the outlet, the velocity boundary condition is considered for the outflow of the both phases. In this study, the non-slip boundary condition at the walls is assumed for both phases.</p><p>For thermal boundary conditions, the microchannel walls are isothermal and the outflow temperature boundary condition is considered for both phases. Because the length of the microchannel is too long, the variations of the outflow velocity and temperature are assumed as follow</p><disp-formula id="scirp.76071-formula80"><label>(30)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x51.png"  xlink:type="simple"/></disp-formula></sec></sec><sec id="s3"><title>3. Numerical Method</title><p>In this study, the non-dimensional forms of the governing equations are discretized by the finite volume method. The first order upwind scheme is used for discretizing the convection-diffusion term. After discretization, the governing equations are converted to a set of algebric equations that is solved iteratively and the SIMPLE algorithm is used for the pressure-velocity coupling [<xref ref-type="bibr" rid="scirp.76071-ref23">23</xref>] [<xref ref-type="bibr" rid="scirp.76071-ref24">24</xref>] . For using this algorithm, the pressure correction equation is obtained from the combination of the continuity equations of the base fluid and particle phases. In fact, combining the continuity equations for both phases causes a new pressure correction equation that modifies the SIMPLE algorithm and the under-relaxa- tion coefficients are used for velocity and pressure in order to accelerate the convergence of the algorithm. In this algorithm, the source term of the pressure correction equation is considered as the convergence criterion. In this study, the iteration is continued until the convergence criterion becomes smaller than 10<sup>−6</sup> in all cells.</p></sec><sec id="s4"><title>4. Grid Independence Study</title><p>To investigate that the results are independent from the number of grid points, the average Nusselt number is calculated for various numbers of grid points and Reynolds numbers. <xref ref-type="table" rid="table1">Table 1</xref> and <xref ref-type="fig" rid="fig2">Figure 2</xref> show the average Nusselt numbers for four different numbers of grid points and Re = 100. It can be seen that the average Nusselt numbers between the 3 and 4 grids have a negligible difference, so the grid 3 is selected for this study.</p><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> The average Nusselt number versus number of grid points</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1860330x52.png"/></fig><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Grid-independency study results for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x53.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x53.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x54.png" xlink:type="simple"/></inline-formula>and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x53.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x54.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x55.png" xlink:type="simple"/></inline-formula></title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Grid</th><th align="center" valign="middle" >1 <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x56.png" xlink:type="simple"/></inline-formula></th><th align="center" valign="middle" >2 <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x57.png" xlink:type="simple"/></inline-formula></th><th align="center" valign="middle" >3 <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x58.png" xlink:type="simple"/></inline-formula></th><th align="center" valign="middle" >4 <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x59.png" xlink:type="simple"/></inline-formula></th></tr></thead><tr><td align="center" valign="middle" >Part1</td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x60.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x61.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x62.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x63.png" xlink:type="simple"/></inline-formula></td></tr><tr><td align="center" valign="middle" >Part2</td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x64.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x65.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x66.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x67.png" xlink:type="simple"/></inline-formula></td></tr><tr><td align="center" valign="middle" >All cells</td><td align="center" valign="middle" >1500</td><td align="center" valign="middle" >10,000</td><td align="center" valign="middle" >30,000</td><td align="center" valign="middle" >48,000</td></tr><tr><td align="center" valign="middle" >Average Nusselt</td><td align="center" valign="middle" >7. 214875</td><td align="center" valign="middle" >7. 654121</td><td align="center" valign="middle" >7. 988713</td><td align="center" valign="middle" >8. 014657</td></tr></tbody></table></table-wrap></sec><sec id="s5"><title>5. Validation</title><p>Because of the lack of the experimental studies for nanofluid flow in a sudden expansion microchannels, the reattachment length for the pure water (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x68.png" xlink:type="simple"/></inline-formula>) at different Reynolds numbers is calculated and compared to Scott et al. [<xref ref-type="bibr" rid="scirp.76071-ref25">25</xref>] results in order to investigate the accuracy of the code. <xref ref-type="table" rid="table2">Table 2</xref> and <xref ref-type="fig" rid="fig3">Figure 3</xref> show the reasonable coincidence between the different amounts of the reattachment length of these two studies for ER = 3 and the maximum deviation is less than 4%.</p></sec><sec id="s6"><title>6. Results and Discussion</title><sec id="s6_1"><title>6.1. The Viscosity of the Solid Phase</title><p>One of the important parameter in this two phase study is the solid viscosity (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x69.png" xlink:type="simple"/></inline-formula> ). In fact, the solid viscosity is the virtual viscosity that must be defined correctly in this model. There is not much experimental data for this viscosity in a solid-liquid two phase mixture, so the trial and error method is used for obtaining the proper value for the solid viscosity. This viscosity appears in the Reynolds number of the solid phase, thus <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x69.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x70.png" xlink:type="simple"/></inline-formula> is calculated for the different Reynolds number of the solid phase until the velocity profile of this numerical solu-</p><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Comparison between reattachment length of this study and Scott’s one for different Reynolds number</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1860330x71.png"/></fig><table-wrap id="table2" ><label><xref ref-type="table" rid="table2">Table 2</xref></label><caption><title> Comparison between reattachment length of this study and Scott’s one</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Reynolds number (Re)</th><th align="center" valign="middle" >Reattachment length <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x72.png" xlink:type="simple"/></inline-formula></th><th align="center" valign="middle" >Reattachment length <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x73.png" xlink:type="simple"/></inline-formula> [<xref ref-type="bibr" rid="scirp.76071-ref25">25</xref>]</th></tr></thead><tr><td align="center" valign="middle" >50</td><td align="center" valign="middle" >5.3</td><td align="center" valign="middle" >5.1</td></tr><tr><td align="center" valign="middle" >100</td><td align="center" valign="middle" >9.3</td><td align="center" valign="middle" >9.7</td></tr><tr><td align="center" valign="middle" >150</td><td align="center" valign="middle" >14.6</td><td align="center" valign="middle" >15</td></tr><tr><td align="center" valign="middle" >200</td><td align="center" valign="middle" >20</td><td align="center" valign="middle" >20</td></tr></tbody></table></table-wrap><p>tion has an appropriate coincidence with it’s analytical solution profile. Consequently, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x74.png" xlink:type="simple"/></inline-formula> is obtained from the trial and error method and the Reynolds number of the solid phase. <xref ref-type="table" rid="table3">Table 3</xref> shows the sensitivity of the Nusselt number to the solid viscosity for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x74.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x75.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x74.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x75.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x76.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x74.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x75.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x76.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x77.png" xlink:type="simple"/></inline-formula>and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x74.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x75.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x76.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x77.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x78.png" xlink:type="simple"/></inline-formula>.</p><p>It can be seen that the changes of the Nusselt number is small when <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x79.png" xlink:type="simple"/></inline-formula> changes. So, the amount of the solid viscosity is not so effective on the results and it is not necessary to find the exact amount of this viscosity. Also, Saffaraval et al. [<xref ref-type="bibr" rid="scirp.76071-ref18">18</xref>] reported the same result about the particle viscosity. The amount of the solid viscosity is considered to be 0.089 Pa.s in this study.</p></sec><sec id="s6_2"><title>6.2. Force Terms in the Momentum Equations</title><p>The momentum equation has three interphase forces including virtual mass, particle-particle interaction and drag forces. In <xref ref-type="table" rid="table4">Table 4</xref>, the average Nusselt number is investigated for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x80.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x80.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x81.png" xlink:type="simple"/></inline-formula>and different conditions of the force terms. It can be seen that the particle-particle interaction and vitual mass forces are not effective on the average Nusselt number, however, the drag force changes the average Nusselt number slightly. Neglecting the drag term causes the average Nusselt number increase, especially in the higher nanoparticle</p><table-wrap id="table3" ><label><xref ref-type="table" rid="table3">Table 3</xref></label><caption><title> Average Nusselt number on the solid viscosity for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x82.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x82.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x83.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x82.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x83.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x84.png" xlink:type="simple"/></inline-formula>and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x82.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x83.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x84.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x85.png" xlink:type="simple"/></inline-formula></title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Solid viscosity</th><th align="center" valign="middle" >Average Nusselt</th></tr></thead><tr><td align="center" valign="middle" >0.001</td><td align="center" valign="middle" >7.889133</td></tr><tr><td align="center" valign="middle" >0.005</td><td align="center" valign="middle" >7.964714</td></tr><tr><td align="center" valign="middle" >0.008</td><td align="center" valign="middle" >7.892112</td></tr><tr><td align="center" valign="middle" >0.01</td><td align="center" valign="middle" >7.938243</td></tr><tr><td align="center" valign="middle" >0.03</td><td align="center" valign="middle" >7.953711</td></tr><tr><td align="center" valign="middle" >0.07</td><td align="center" valign="middle" >7.981838</td></tr><tr><td align="center" valign="middle" >0.089</td><td align="center" valign="middle" >7.988713</td></tr><tr><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >8.004554</td></tr></tbody></table></table-wrap><table-wrap id="table4" ><label><xref ref-type="table" rid="table4">Table 4</xref></label><caption><title> Effect of the force terms on the average Nusselt number for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x86.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x86.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x87.png" xlink:type="simple"/></inline-formula>and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x86.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x87.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x88.png" xlink:type="simple"/></inline-formula></title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Volume concentration (%)</th><th align="center" valign="middle" >Considering all force term</th><th align="center" valign="middle" >Neglecting <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x89.png" xlink:type="simple"/></inline-formula></th><th align="center" valign="middle" >Neglecting <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x90.png" xlink:type="simple"/></inline-formula></th><th align="center" valign="middle" >Neglecting <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x91.png" xlink:type="simple"/></inline-formula></th></tr></thead><tr><td align="center" valign="middle" >1</td><td align="center" valign="middle" >7.988713</td><td align="center" valign="middle" >8.02481</td><td align="center" valign="middle" >7.98862</td><td align="center" valign="middle" >7.98864</td></tr><tr><td align="center" valign="middle" >2</td><td align="center" valign="middle" >8.193648</td><td align="center" valign="middle" >8.28713</td><td align="center" valign="middle" >8.19353</td><td align="center" valign="middle" >8.19349</td></tr><tr><td align="center" valign="middle" >3</td><td align="center" valign="middle" >8.411941</td><td align="center" valign="middle" >8.54164</td><td align="center" valign="middle" >8.41193</td><td align="center" valign="middle" >8.41191</td></tr><tr><td align="center" valign="middle" >4</td><td align="center" valign="middle" >8.633981</td><td align="center" valign="middle" >8.81341</td><td align="center" valign="middle" >8.63378</td><td align="center" valign="middle" >8.63392</td></tr><tr><td align="center" valign="middle" >5</td><td align="center" valign="middle" >8.856696</td><td align="center" valign="middle" >9.09733</td><td align="center" valign="middle" >8.85658</td><td align="center" valign="middle" >8.85668</td></tr></tbody></table></table-wrap><p>volume concentrations. According to <xref ref-type="table" rid="table4">Table 4</xref>, by neglecting the drag term at<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x92.png" xlink:type="simple"/></inline-formula>, the average Nusselt number increases 0.03 and it increases 0.24 at<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x92.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x93.png" xlink:type="simple"/></inline-formula>. Consequently, the particle-particle interaction and virtual mass forces can be neglected in the mathematical models of nanofluid.</p></sec><sec id="s6_3"><title>6.3. Enhancement of the Nanofluid Heat Transfer in Comparison to the Pure Water</title><p><xref ref-type="fig" rid="fig4">Figure 4</xref> shows the increase of the average Nusselt number of the nanofluid in comparison to the pure water for different nanoparticle volume concentration. The results show the non-linearly increase in the nanofluid heat transfer enhancement when the nanoparticle volume concentration increases. In fact, the nanofluid heat transfer enhancement is caused by the presence of the copper nanoparticles that increases the thermal conductivity coefficient of the fluid. At <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x94.png" xlink:type="simple"/></inline-formula> it has been observed that the percentage enhancement in the average Nusselt number at Re = 100 is 7.6% more than the corresponding percentage at Re = 50.</p><p>The enhancement of the nanofluid heat transfer in comparison to the pure water can be seen from <xref ref-type="fig" rid="fig5">Figure 5</xref> that the coefficient of performance (COP) increases with an increase in the nanoparticle volume concentration for every Reynolds number. Another important observation in <xref ref-type="fig" rid="fig5">Figure 5</xref> is that the lower</p><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Comparison of percentage enhancement in average Nusselt number with respect to pure water for different volume concentrations and ER = 3</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1860330x95.png"/></fig><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Coefficient of performance of the nanofluid versus Reynolds number for different nanoparticle volume concentration, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x97.png" xlink:type="simple"/></inline-formula>and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x97.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x98.png" xlink:type="simple"/></inline-formula></title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1860330x96.png"/></fig><p>Reynolds number affects more on increasing the COP for a definite nanoparticle volume concentration. Here, the COP of the nanofluid is obtained as</p><disp-formula id="scirp.76071-formula81"><label>(31)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1860330x99.png"  xlink:type="simple"/></disp-formula><p>where subscripts nf and pw show the nanofluid and pure water, respectively.</p></sec><sec id="s6_4"><title>6.4. Expansion Ratio Effect on the Nanofluid Heat Transfer and Flow</title><p><xref ref-type="fig" rid="fig6">Figure 6</xref> illustrates the pressure drop for <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x100.png" xlink:type="simple"/></inline-formula> when the expansion ratio of the microchannel changes. From <xref ref-type="fig" rid="fig6">Figure 6</xref> it has been observed that the</p><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> Non-dimensional pressure drop versus Reynolds number for different expansion ratio and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x102.png" xlink:type="simple"/></inline-formula></title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1860330x101.png"/></fig><p>pressure drop increases with decrease of the expansion ratio of the microchannel but it is small for all Reynolds numbers.</p><p><xref ref-type="fig" rid="fig7">Figure 7</xref> depicts the effect of Reynolds number and the expansion ratio of the microchannel on the average Nusselt number for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x103.png" xlink:type="simple"/></inline-formula>. It has been observed that the average Nusselt number increases with increase in Reynolds number and decrease in the expansion ratio of the microchannel. Reynolds number increases the convection effects but the increase of the expansion ratio decreases the pressure drop and makes the larger recirculation zone that decreases the convection effects and causes the lower heat transfer.</p></sec><sec id="s6_5"><title>6.5. Bifurcation</title><p>The increasing of the Reynolds number increases the expansion pressure. The pressure forces dominate the viscous force in the critical Reynolds number where the viscous force cannot hold the flow structure in a symmetric couple of vortexes anymore. In this case, the reattachment length of the upper wall decreases when the reattachment length of the lower one increases and the bifurcation of the reattachment length occurs in the critical Reynolds number. <xref ref-type="fig" rid="fig8">Figure 8</xref> shows that the critical Reynolds number decreases with increase in expansion ratio of the microchannel and the bifurcation point moves to the left side. It can be seen from <xref ref-type="fig" rid="fig8">Figure 8</xref> that the trinity occurs in the second critical Reynolds number for the reattachment length with more increase in the Reynolds number.</p><p>The trend of the first critical Reynolds number versus expansion ratio is a straight line. In <xref ref-type="fig" rid="fig9">Figure 9</xref>, a correlation for the first critical Reynolds number and expansion ratio is obtained by using the linear regression.</p><p>The first and second critical Reynolds numbers for different expansion ratios are shown in <xref ref-type="table" rid="table5">Table 5</xref>.</p><fig id="fig7"  position="float"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> Average Nusselt number versus Reynolds number for different expansion ratio and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x105.png" xlink:type="simple"/></inline-formula></title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1860330x104.png"/></fig><fig id="fig8"  position="float"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> Comparison of the bifurcation for different expansion ratios</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1860330x106.png"/></fig><fig id="fig9"  position="float"><label><xref ref-type="fig" rid="fig9">Figure 9</xref></label><caption><title> Linear regression for the first critical Reynolds number</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1860330x107.png"/></fig><table-wrap id="table5" ><label><xref ref-type="table" rid="table5">Table 5</xref></label><caption><title> The first and second critical Reynolds numbers for different expansion ratios</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Critical Reynolds number</th><th align="center" valign="middle" >ER = 3</th><th align="center" valign="middle" >ER = 4</th><th align="center" valign="middle" >ER = 5</th></tr></thead><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x108.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >200</td><td align="center" valign="middle" >150</td><td align="center" valign="middle" >120</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1860330x109.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >275</td><td align="center" valign="middle" >205</td><td align="center" valign="middle" >175</td></tr></tbody></table></table-wrap></sec></sec><sec id="s7"><title>7. Conclusion</title><p>A two-phase model is considered to simulate the nanofluid flow inside the microchannel and among two-phase models, Eulerian-Eulerian model is very efficient because of considering the relative velocity and temperature of the phases and the nanoparticle concentration distribution. The governing mass, momentum and energy equations for both phases are solved using the finite volume method. In solving the flow equations for both phases, the SIMPLE algorithm is modified for the coupling of the velocity and pressure and the continuity equations for both phases are combined in order to create the pressure correction equations. However, the Eulerian-Eulerian modeling results show higher heat transfer enhancement in comparison to pure water, so that for a 2% copper-water nanofluid, it has been observed a 35% increase of the heat transfer. The average nusselt number increases with increase in Reynolds number and nanoparticle volume concentration and decrease of the expansion ratio of the microchannel. For a constant volume concentration, the lower Reynolds number causes the larger average Nusselt number ratio. The critical Reynolds number for bifurcation decreases with increase in the expansion ratio of the microchannel. The importance and developments of microfluidic devices, like expansion microchannel, has made the investigation of the flow and the heat transfer of nanofluid in sudden expansion microchannel so important and practical. On the other hand, the two-phase models can be used instead of single phase model very well.</p></sec><sec id="s8"><title>Cite this paper</title><p>Abbassi, F.A., Nazari, M. and Shahmardan, M.M. (2017) Numerical Study of Heat Transfer and Flow Bifurcation of CuO Nanofluid in Sudden Expansion Microchannel Using Two-Phase Model. 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