<?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">OJFD</journal-id><journal-title-group><journal-title>Open Journal of Fluid Dynamics</journal-title></journal-title-group><issn pub-type="epub">2165-3852</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/ojfd.2016.61001</article-id><article-id pub-id-type="publisher-id">OJFD-64275</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  Numerical Study on the Effects of Contraction Ratio in a Two-Phase Flow Injection Nozzle
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>aider</surname><given-names>Ali</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>Kyung</surname><given-names>Won Kim</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>Jae</surname><given-names>Sik Kim</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Jong</surname><given-names>Yun Choi</given-names></name><xref ref-type="aff" rid="aff3"><sup>3</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Cheol</surname><given-names>Woo Park</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, Kyungpook National University, Daegu, Korea</addr-line></aff><aff id="aff3"><addr-line>B.C.M. Co., Ltd., 81 Yeomsaekgongdancheon-Ro, Seo-Gu, Daegu, Korea</addr-line></aff><aff id="aff2"><addr-line>Podomaul Co., Ltd., 1190 Kumchang-Ro, Daechang-Myon, Yeongcheon-Si, Korea</addr-line></aff><pub-date pub-type="epub"><day>08</day><month>03</month><year>2016</year></pub-date><volume>06</volume><issue>01</issue><fpage>1</fpage><lpage>10</lpage><history><date date-type="received"><day>24</day>	<month>November</month>	<year>2015</year></date><date date-type="rev-recd"><day>accepted</day>	<month>5</month>	<year>March</year>	</date><date date-type="accepted"><day>8</day>	<month>March</month>	<year>2016</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>
 
 
  The Euler-Euler numerical method was used to investigate the effects of contraction ratio on twophase flow mixing with mass transfer in the flow injection nozzle. The geometric shape of the nozzle was modified to improve carbonation efficiency. A gas inlet hole was created to increase the flow mixing of CO2 with water. A nozzle throat was also introduced to increase the gas dissolution by increasing flow rates. Various contraction ratios of nozzle throat, inlet gas and liquid velocities, and gas bubble sizes were employed to determine their effects on gas hold-up, gas concentration, and mass transfer coefficient. Results revealed that the flow injection nozzle with high contraction ratios improved carbonation because of high gas hold-up. Gas concentration was directly related to contraction ratio and gas flow velocities. Carbonation reduced when high liquid velocities and large gas bubbles were employed because of inefficient flow mixing. This study indicated that flow injection nozzle with large contraction ratios were suitable for carbonation because of their ability to increase gas hold-up, gas concentration, and mass transfer coefficient.
 
</p></abstract><kwd-group><kwd>Flow Injection Nozzle</kwd><kwd> Nozzle Throat</kwd><kwd> Contraction Ratio</kwd><kwd> Gas-Liquid Flow</kwd><kwd> Mass Transfer</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Carbonated beverages are prepared by dissolving CO<sub>2</sub> in water with minimum amount of gas bubbles produced. Carbonating machines generally employ a flow injection nozzle to supply water during continuous carbonation. Carbonation efficiency can be increased by improving the dissolution of CO<sub>2</sub> in water. However, CO<sub>2</sub> is not completely dissolved in the carbonating tank because of high gas and water flow rates. Therefore, a small opening is created in the flow injection nozzle to allow CO<sub>2</sub> to enter into the nozzle and mix effectively with water. The aforementioned geometrical modification helps to increase gas dissolution by increasing the interaction time of gas with water. The gas bubbles tend to rise vertically and gather in the center of the nozzle at high gas flow rates, thereby leading to liquid circulation. Radial gas accumulation causes flow recirculation in the nozzle. Flow recirculation is essential for carbonation because it facilitates gas dissolution [<xref ref-type="bibr" rid="scirp.64275-ref1">1</xref>] [<xref ref-type="bibr" rid="scirp.64275-ref2">2</xref>] .</p><p>Carbonation significantly depends on the solubility of CO<sub>2</sub> in water. As such, mass transfer in these systems must be assessed for design optimization. The mass transfer coefficient of CO<sub>2</sub> must be estimated in the flow injection nozzle to quantify mass transfer rate between the gas and liquid interface boundary [<xref ref-type="bibr" rid="scirp.64275-ref3">3</xref>] . Deckwer et al. [<xref ref-type="bibr" rid="scirp.64275-ref4">4</xref>] reported that mass transfer coefficient depends on the geometric shape of the sparger or nozzle used for flow injection. The mass transfer coefficient increases with increasing gas flow rates but decreases when gas and liquid are mixed together with a mechanical agitation device [<xref ref-type="bibr" rid="scirp.64275-ref5">5</xref>] . Several numerical studies were conducted on various industrial applications of two-phase flow by using the famous Euler-Euler two-fluid model because of the complexity and immense cost involved in the experimental work. Chakraborty et al. [<xref ref-type="bibr" rid="scirp.64275-ref6">6</xref>] used the Euler-Euler model to examine the influence of gas flow velocity, reactor geometry, and sparger arrangement on the hydrodynamic properties of the reactor. The results suggested the use of low gas flow rates and uniformly distributed gas spargers to improve the performance of the two-phase reactor [<xref ref-type="bibr" rid="scirp.64275-ref6">6</xref>] . Therefore, the design of the gas sparger or injecting nozzle is of considerable importance for increasing mass transfer coefficient and gas hold-up to enhance carbonation. Moreover, the throat of the flow injection nozzle is considerably important, and the throat area (contraction ratio) can be varied to enhance carbonation by increasing gas dissolution in water. Alves et al. [<xref ref-type="bibr" rid="scirp.64275-ref7">7</xref>] investigated the effect of contraction ratio on the overall features of different flow types; they reported that liquid recirculation strongly depended on contraction ratio and increased with decreasing contraction ratio [<xref ref-type="bibr" rid="scirp.64275-ref7">7</xref>] . Evan and Walters [<xref ref-type="bibr" rid="scirp.64275-ref8">8</xref>] studied the effect of three different contraction ratios. Liquid recirculation is formed and dominated in the case of high contraction ratios [<xref ref-type="bibr" rid="scirp.64275-ref8">8</xref>] . Therefore, contraction ratio is an important parameter in the design of flow injection nozzles and can be used to enhance carbonation. We previously investigated flow mixing in the carbonating tank to improve carbonation with the use of the same Euler-Euler methodology [<xref ref-type="bibr" rid="scirp.64275-ref9">9</xref>] . However, flow mixing in the injecting nozzle and the effect of contraction ratio on hydrodynamic properties were not considered in our previous work.</p><p>The study investigates the effect of contraction ratio on gas-liquid turbulent flow with mass transfer in the flow injection nozzle. An inlet hole for CO<sub>2</sub> gas was constructed in the nozzle to increase the interaction time of gas with water. The shape of the water nozzle was further modified by introducing a nozzle throat to enhance gas dissolution. The throat area of the nozzle was varied to examine the effect of contraction ratio on the flow mixing phenomenon. Various contraction ratios of nozzle throat, inlet gas and liquid velocities, and gas bubble sizes were employed to determine their effects on gas hold-up, liquid velocity, gas concentration, and mass transfer coefficient.</p></sec><sec id="s2"><title>2. Mathematical Modeling</title><p>A 2D model of the flow injection nozzle with a length (L) of 0.055 m and a diameter ( ) of 0.006 m is presented in <xref ref-type="fig" rid="fig1">Figure 1</xref>. The inlet for CO<sub>2</sub> gas possesses a length of 0.003 m. A nozzle throat with a length (l) of 0.009 m and a diameter (d) of 0.0023 m was introduced to enhance gas dissolution. <xref ref-type="fig" rid="fig1">Figure 1</xref> demonstrates the nozzle bend with the inner (r) and outer (R) radii of curvatures of 0.0078 and 0.0015 m, respectively. The geometrical effects of nozzle were studied using a dimensionless number, namely, contraction ratio (CR), which is given below:</p><disp-formula id="scirp.64275-formula4"><label>. (1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-2320260x6.png"  xlink:type="simple"/></disp-formula><p>The study considered three CRs (i.e., 2, 3, and 4) with different gas and water flow rates and gas bubble sizes to examine the effect of CRs on the flow mixing process of CO<sub>2</sub> gas with water in the flow injection nozzle.</p><sec id="s2_1"><title>2.1. Gas-Liquid Flow Modeling</title><p>The study used the Euler-Euler methodology to model two-phase flow in the flow injection nozzle because of</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Computational models of the flow injection nozzle</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-2320260x7.png"/></fig><p>the ability to track average phase concentration [<xref ref-type="bibr" rid="scirp.64275-ref10">10</xref>] [<xref ref-type="bibr" rid="scirp.64275-ref11">11</xref>] . The governing equations of continuity and momentum transport are as follows:</p><disp-formula id="scirp.64275-formula5"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-2320260x8.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.64275-formula6"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-2320260x9.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.64275-formula7"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-2320260x10.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x11.png" xlink:type="simple"/></inline-formula> represents the hold-up (m<sup>3</sup>/m<sup>3</sup>), <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x12.png" xlink:type="simple"/></inline-formula>is the density (kg/m<sup>3</sup>), <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x13.png" xlink:type="simple"/></inline-formula>is the velocity (m/s), <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x14.png" xlink:type="simple"/></inline-formula>is the pressure (Pa), <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x15.png" xlink:type="simple"/></inline-formula>is the dynamic viscosity (Pa∙s), g is the gravity vector (9.81 m/s<sup>2</sup>), subscripts l and g are the liquid and gas phases, respectively, and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x16.png" xlink:type="simple"/></inline-formula> is the mass transfer rate from gas to liquid (kg/m<sup>3</sup>∙s).</p><p>Ideal gas law was used to calculate gas density [<xref ref-type="bibr" rid="scirp.64275-ref12">12</xref>] .</p><disp-formula id="scirp.64275-formula8"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-2320260x17.png"  xlink:type="simple"/></disp-formula><p>where M denotes the molecular weight of CO<sub>2</sub> (44.01 kg/kmol), R is the ideal gas constant (0.1889 kJ/kg-K), <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x18.png" xlink:type="simple"/></inline-formula>is the reference pressure (1 &#215; 10<sup>5</sup> Pa), and T is the CO<sub>2</sub> temperature (298 K).</p><p>The k-ε turbulence model with additional source terms was used to model turbulence between gas bubbles and the liquid. The governing equations for the turbulent kinetic energy k and the dissipation rate <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x19.png" xlink:type="simple"/></inline-formula> are respectively given as follows:</p><disp-formula id="scirp.64275-formula9"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-2320260x20.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.64275-formula10"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-2320260x21.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.64275-formula11"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-2320260x22.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x23.png" xlink:type="simple"/></inline-formula> represents the dynamic viscosity (Pa∙s), <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x24.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x25.png" xlink:type="simple"/></inline-formula> are the turbulent Prandtl numbers, and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x25.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x26.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x25.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x27.png" xlink:type="simple"/></inline-formula> are the first and second experimental model constants, respectively. These constants are set as follows:<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x25.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x28.png" xlink:type="simple"/></inline-formula>.</p><p>The source term <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x29.png" xlink:type="simple"/></inline-formula> for the bubble-induced turbulence (W/m<sup>3</sup>) is presented as:</p><disp-formula id="scirp.64275-formula12"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-2320260x30.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x31.png" xlink:type="simple"/></inline-formula> denotes the gas hold-up (m<sup>3</sup>/m<sup>3</sup>) and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x32.png" xlink:type="simple"/></inline-formula> is the slip velocity (m/s). The bubble-induced turbulence parameter (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x33.png" xlink:type="simple"/></inline-formula>) was set as 0.505.</p><p>The relation for gas velocity is as follows:</p><disp-formula id="scirp.64275-formula13"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-2320260x34.png"  xlink:type="simple"/></disp-formula><p>where<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x35.png" xlink:type="simple"/></inline-formula>, , and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x35.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x37.png" xlink:type="simple"/></inline-formula> are the gas, liquid, and slip velocities (m/s), respectively.</p></sec><sec id="s2_2"><title>2.2. Gas Dissolution</title><p>Two-film theory was used to model mass transfer across gas and liquid interfaces during gas dissolution in the flow injection nozzle [<xref ref-type="bibr" rid="scirp.64275-ref10">10</xref>] [<xref ref-type="bibr" rid="scirp.64275-ref13">13</xref>] . This film theory uses Henry’s law to model the mass transfer rate (m<sub>gl</sub>) in Equation (3) during CO<sub>2</sub> dissolution in water.</p><disp-formula id="scirp.64275-formula14"><label>. (11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-2320260x38.png"  xlink:type="simple"/></disp-formula><p>The interfacial area (a) between the two phases is modeled by Euler-Euler method [<xref ref-type="bibr" rid="scirp.64275-ref14">14</xref>] .<sup> </sup></p><disp-formula id="scirp.64275-formula15"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-2320260x39.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x40.png" xlink:type="simple"/></inline-formula> represents the mass transfer coefficient (m/s), H is the Henry’s constant (2980 Pa∙m<sup>3</sup>/mol), c denotes the gas concentration in liquid (mol/m<sup>3</sup>), M is the molecular weight (44.01 kg/kmol), a shows the interfacial area per volume (1/m), n represents the bubbles per volume (1/m<sup>3</sup>), and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x40.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x41.png" xlink:type="simple"/></inline-formula> is the gas hold-up (m<sup>3</sup>/m<sup>3</sup>).</p><p>Higbie’s theory was used to model the mass transfer coefficient (k<sub>m</sub>) and is presented as follows [<xref ref-type="bibr" rid="scirp.64275-ref3">3</xref>] [<xref ref-type="bibr" rid="scirp.64275-ref9">9</xref>] [<xref ref-type="bibr" rid="scirp.64275-ref10">10</xref>] :</p><disp-formula id="scirp.64275-formula16"><label>(13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-2320260x42.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x43.png" xlink:type="simple"/></inline-formula> represents the mass transfer coefficient (m/s), D is the diffusion coefficient (m<sup>2</sup>/s), <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x43.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x44.png" xlink:type="simple"/></inline-formula>shows the relative velocity between gas and liquid (m/s), and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x43.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x44.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x45.png" xlink:type="simple"/></inline-formula> is the gas bubble diameter (m).</p><p>The growth of gas bubbles in the flow injection nozzle was modeled by using the population balance equation. The governing equation for gas bubbles population balance is as follows:</p><disp-formula id="scirp.64275-formula17"><label>(14)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-2320260x46.png"  xlink:type="simple"/></disp-formula><p>where n is the number of bubbles per volume (1/m<sup>3</sup>), and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x47.png" xlink:type="simple"/></inline-formula> represents gas velocity (m/s).</p><p>The transport equation for gas concentration is shown below:</p><disp-formula id="scirp.64275-formula18"><label>(15)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-2320260x48.png"  xlink:type="simple"/></disp-formula><p>where d shows the diffusion coefficient (m<sup>2</sup>/s), and c represents the dissolved gas concentration in liquid (mol/m<sup>3</sup>). The diffusion coefficient is estimated using the following equation:</p><disp-formula id="scirp.64275-formula19"><label>(16)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-2320260x49.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x50.png" xlink:type="simple"/></inline-formula> is the turbulent viscosity (Pa・s), and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x50.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2320260x51.png" xlink:type="simple"/></inline-formula> is the liquid density (kg/m<sup>3</sup>).</p></sec></sec><sec id="s3"><title>3. Numerical Method and Implementation</title><p>Commercial code COMSOL-Multiphysics (V 4.3) was used to model two-phase flow mixing with mass transport in the flow injection nozzle. Three CRs were simultaneously solved using the k-ε turbulence model and mass transport equations for dissolved gas. A time-dependent solver was used to simulate the two-phase flow with mass transfer for 40 s and at a time step of 0.001 s. Geometric models were discretized using a free triangular mesh type with 3472 domain and 275 boundary elements. All computations were performed on an Intel Core i7-3370 3.90 GHz processor with a 16 GB RAM operating system.</p></sec><sec id="s4"><title>4. Results and Discussion</title><sec id="s4_1"><title>4.1. Gas Hold-Up</title><p>The effect of CR on the average gas hold-up with variation in inlet gas velocities is presented in <xref ref-type="fig" rid="fig2">Figure 2</xref>. These results were estimated using an inlet liquid velocity of 0.0001 m/s and a gas bubble size of 0.002 m. Gas hold-up showed a direct relationship to the gas flow rates, that is, the gas hold-up increased with increasing inlet gas velocity. Higher gas flow rates enhanced the accumulation of gas bubbles in the nozzle, thereby increasing liquid circulation. This condition implies that carbonation is more effective at high gas flow rates because of high gas dissolution caused by improved liquid recirculation. The gas hold-up significantly increased when the nozzle throat area was reduced. The flow injection nozzle with the CR value of 4 considerably improved the liquid recirculation because of high amount of gas hold-up. Hence, the carbonation process in nozzles with larger CRs and inlet gas velocities increased because of the high volume of gas in liquid [<xref ref-type="bibr" rid="scirp.64275-ref1">1</xref>] [<xref ref-type="bibr" rid="scirp.64275-ref9">9</xref>] . Gas hold-up reduced with increasing liquid flow rates because of decreased liquid recirculation (<xref ref-type="fig" rid="fig3">Figure 3</xref>). The results were estimated using an inlet gas velocity of 0.0005 m/s and a gas bubble size of 0.002 m. Increasing liquid velocity decreased the gas dissolution process because of less effective flow mixing of gas with liquid. Therefore, nozzles with larger CRs values and less liquid velocities are suitable for preparing carbonated water because of the larger volume of gas accumulation and improved liquid recirculation [<xref ref-type="bibr" rid="scirp.64275-ref9">9</xref>] .</p></sec><sec id="s4_2"><title>4.2. Gas Concentration</title><p>The effect of inlet gas velocities with different CRs on average gas concentration is presented in <xref ref-type="fig" rid="fig4">Figure 4</xref>. The results were evaluated at an inlet liquid velocity of 0.0001 m/s and a constant gas bubble size of 0.002 m. Gas concentration showed an increasing slope with respect to gas flow rates because of improved liquid circulation in the nozzle. The maximum gas concentration in the liquid was observed at high gas velocities, showing that carbonation increased at high gas velocities because of increasing gas concentration in the liquid. Gas concentration also exhibited a direct relationship to nozzle CRs. The reduction in the nozzle throat increased gas dissolution by improving liquid recirculation, which in turn increased the gas concentration level in water. The nozzle with a CR of 4 exhibited the highest gas concentration magnitude and enhanced carbonation. These findings imply that the nozzle throat with high CRs and gas flow rates would increase carbonation because of high gas concentrations caused by effective liquid recirculation [<xref ref-type="bibr" rid="scirp.64275-ref5">5</xref>] [<xref ref-type="bibr" rid="scirp.64275-ref9">9</xref>] [<xref ref-type="bibr" rid="scirp.64275-ref15">15</xref>] .</p><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Gas hold-up (1) with variations in inlet gas velocity (m/s)</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-2320260x52.png"/></fig><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Gas hold-up (1) with variations in inlet liquid velocity (m/s)</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-2320260x53.png"/></fig><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Gas concentration (mol/m<sup>3</sup>) with variations in gas velocity (m/s)</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-2320260x54.png"/></fig><p><xref ref-type="fig" rid="fig5">Figure 5</xref> shows the average gas concentration with the effect of different CR values and liquid velocities at an inlet gas velocity of 0.0005 m/s and bubble size of 0.002 m. The results showed that increasing the water flow rates decreased gas concentration because of less effective liquid recirculation in the nozzle. The slope of gas concentration significantly decreased because of less effective flow mixing caused by increasing liquid flow velocities. Carbonation was significantly reduced in the nozzles with smaller CR because of low liquid recirculation, which is due to high liquid flow rates. Flow mixing in the nozzle can be increased by increasing gas flow rates to improve liquid recirculation. The results suggest that larger CRs and low liquid velocities are necessary to increase carbonation efficiency by increasing the gas concentration magnitude in the liquid [<xref ref-type="bibr" rid="scirp.64275-ref5">5</xref>] [<xref ref-type="bibr" rid="scirp.64275-ref15">15</xref>] . Gas bubble size is an important parameter in the study of the two-phase flow system because this parameter can affect gas dissolution [<xref ref-type="bibr" rid="scirp.64275-ref15">15</xref>] . Therefore, the effect of gas bubble size on the average gas concentration with different CRs is illustrated in <xref ref-type="fig" rid="fig6">Figure 6</xref>. The results are evaluated with an inlet gas velocity of 0.0005 m/s, water velocity of 0.0001 m/s, and gas bubble size of 0.002 m. Gas concentration significantly decreased with the use of larger gas bubbles because of reduction in gas dissolution. The results depict the difficulty in dissolving larger gas bubbles in the liquid. Therefore, gas concentration level in the nozzle was reduced at larger gas bubble diameters. The nozzle with a CR of 4 showed high gas concentration magnitudes at different gas bubble sizes than the other models. Therefore, small gas bubbles and larger CR are suitable for carbonation because of high gas concentration in the nozzle [<xref ref-type="bibr" rid="scirp.64275-ref9">9</xref>] [<xref ref-type="bibr" rid="scirp.64275-ref15">15</xref>] .</p><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Gas concentration (mol/m<sup>3</sup>) with variations in liquid velocity (m/s)</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-2320260x55.png"/></fig><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> Gas concentration (mol/m<sup>3</sup>) with variations in gas bubble size (m)</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-2320260x56.png"/></fig></sec><sec id="s4_3"><title>4.3. Mass Transfer Coefficient</title><p>The effect of various gas velocities on the average mass transfer coefficient with a CR of 3, liquid velocity of 0.0001 m/s, and gas bubble size of 0.002 m is shown in <xref ref-type="fig" rid="fig7">Figure 7</xref>. The mass transfer coefficient showed higher magnitude in the lower part of the nozzle, particularly at low gas velocities, because of the presence of gas inlet in this section. Gas dissolution in liquid was higher in the lower region of the flow injection nozzle because of the higher magnitude of mass transfer coefficient in the area. Mass transfer between the two fluids was lower in the upper part and throat of the nozzle because of higher liquid velocity in these areas. High liquid velocity resulted in low carbonation because of less effective flow mixing. Increasing the gas velocities enhanced the mass transfer mechanism in the entire nozzle geometry. Mass transfer was observed in the upper and lower sections of the nozzle at a maximum gas velocity of 0.001 m/s. These findings show that carbonation is strong in the lower portion but weak in the throat and upper part of the flow injection nozzle [<xref ref-type="bibr" rid="scirp.64275-ref4">4</xref>] [<xref ref-type="bibr" rid="scirp.64275-ref5">5</xref>] . The average mass transfer coefficient was also estimated by determining the effect of different CRs and gas velocities at an inlet liquid velocity of 0.0001 m/s and a constant gas bubble size 0.002 m (<xref ref-type="fig" rid="fig8">Figure 8</xref>). The mass transfer coefficient almost linearly increased with increasing inlet gas velocities for all cases of CRs. The nozzle with high CR values yielded higher magnitudes of the mass transfer coefficient, indicating that mass transfer between gas and liquid is high</p><fig id="fig7"  position="float"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> Mass transfer coefficient (m/s) in the nozzle with CR = 3 at inlet gas and liquid velocities of 0.0005 and 0.0001 m/s, respectively</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-2320260x57.png"/></fig><fig id="fig8"  position="float"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> Mass transfer coefficient (m/s) with variations in gas velocity (m/s)</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-2320260x58.png"/></fig><p>in nozzles with smaller CR. This result suggests the dependence of mass transfer coefficient on gas flow rates and nozzle geometry (CR). Therefore, higher gas velocities and CR are recommended to increase carbonation efficiency [<xref ref-type="bibr" rid="scirp.64275-ref3">3</xref>] [<xref ref-type="bibr" rid="scirp.64275-ref15">15</xref>] .</p><p><xref ref-type="fig" rid="fig9">Figure 9</xref> shows the average mass transfer coefficient with the effect of different CRs and liquid velocities at an inlet gas velocity of 0.0005 m/s and a bubble size of 0.002 m. Mass transfer coefficient significantly decreased with increasing liquid flow velocities because of less effective flow mixing. Mass transfer between the two fluids reduced linearly in the nozzle of small CRs because high liquid velocities caused a reduction in liquid recirculation. Nozzles with larger CRs increased carbonation because of increased mass transfer coefficient. Therefore, larger CRs and lower water flow rates must be selected to enhance carbonation by improving the mass transfer mechanism between gas and liquid [<xref ref-type="bibr" rid="scirp.64275-ref3">3</xref>] [<xref ref-type="bibr" rid="scirp.64275-ref9">9</xref>] . The effect of gas bubble size on mass transfer coefficient with different CRs is presented in <xref ref-type="fig" rid="fig1">Figure 1</xref>0. The results were evaluated at an inlet gas velocity of 0.0005 m/s, water velocity of 0.0001 m/s, and gas bubble size of 0.002 m. The mass transfer coefficient decreased linearly with increasing gas bubble size because mass transfer between the gas and liquid phases with larger gas bubbles is difficult. Moreover, the nozzle with a CR of 4 yielded higher mass transfer coefficient magnitudes than other CR cases. These results suggest that larger CRs and an appropriate gas bubble size must be selected to enhance carbonation by improving the mass transfer mechanism in the flow injection nozzle [<xref ref-type="bibr" rid="scirp.64275-ref4">4</xref>] [<xref ref-type="bibr" rid="scirp.64275-ref5">5</xref>] .</p><fig id="fig9"  position="float"><label><xref ref-type="fig" rid="fig9">Figure 9</xref></label><caption><title> Mass transfer coefficient (m/s) with variations in liquid velocity (m/s)</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-2320260x59.png"/></fig><fig id="fig10"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref>0</label><caption><title> Mass transfer coefficient (m/s) with variations in gas bubble size (m)</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-2320260x60.png"/></fig></sec></sec><sec id="s5"><title>5. Conclusion</title><p>This study investigated the effects of contraction ratio on gas-liquid flow mixing with mass transfer in the flow injection nozzle. Euler-Euler two-fluid method was used to model the two-phase flow in the flow injection nozzle. The nozzle geometry was modified with the addition of a gas inlet hole and throat to enhance gas dissolution. Various contraction ratios of nozzle throat, inlet gas and liquid velocities, and gas bubble sizes were used to determine their effects on gas hold-up, gas concentration, and mass transfer coefficient.</p><p>The flow injection nozzle with the maximum CR improved liquid recirculation, which is caused by larger gas hold-up volume. Carbonation was enhanced at higher gas flow velocities because of enhanced gas dissolution. Gas hold-up decreased with increasing liquid flow velocities because of less liquid recirculation. Gas concentration increased linearly with increasing CRs and gas flow velocities. By contrast, gas concentration was reduced with increasing liquid velocities because of less effective flow mixing. Gas bubbles with larger size decreased gas concentration by reducing gas dissolution in liquid. The mass transfer coefficient was high in the lower part of the flow injection nozzle. High CR values resulted in higher magnitudes of the mass transfer coefficient, which showed inverse relationships to liquid flow rates and gas bubble sizes. High CRs of the flow injection nozzle with higher gas flow velocities, lower liquid velocities, and small gas bubbles are suitable for effective carbonation.</p></sec><sec id="s6"><title>Acknowledgements</title><p>This work was supported by the High Value-added Food Technology Development Program, Ministry of Agriculture, Food, and Rural Affairs (No. 314051-03-1-HD020), and the grant from the Priority Research Centers Program through the NRF as funded by MEST (No. 2010-0020089).</p></sec><sec id="s7"><title>Cite this paper</title><p>HaiderAli,Kyung WonKim,Jae SikKim,Jong YunChoi,Cheol WooPark, (2016) Numerical Study on the Effects of Contraction Ratio in a Two-Phase Flow Injection Nozzle. 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