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<front>
<journal-meta>
<journal-id journal-id-type="pmc">FDMP</journal-id>
<journal-id journal-id-type="nlm-ta">FDMP</journal-id>
<journal-id journal-id-type="publisher-id">FDMP</journal-id>
<journal-title-group>
<journal-title>Fluid Dynamics &#x0026; Materials Processing</journal-title>
</journal-title-group>
<issn pub-type="epub">1555-2578</issn>
<issn pub-type="ppub">1555-256X</issn>
<publisher>
<publisher-name>Tech Science Press</publisher-name>
<publisher-loc>USA</publisher-loc>
</publisher>
</journal-meta>
<article-meta>
<article-id pub-id-type="publisher-id">58295</article-id>
<article-id pub-id-type="doi">10.32604/fdmp.2024.058295</article-id>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Article</subject>
</subj-group>
</article-categories>
<title-group>
<article-title>Numerical Simulation of Gas-LiquId Flow in a Horizontal Elbow</article-title><alt-title alt-title-type="left-running-head">Numerical Simulation of Gas-LiquId Flow in a Horizontal Elbow</alt-title><alt-title alt-title-type="right-running-head">Numerical Simulation of Gas-LiquId Flow in a Horizontal Elbow</alt-title>
</title-group>
<contrib-group>
<contrib id="author-1" contrib-type="author">
<name name-style="western"><surname>Ma</surname><given-names>Lihui</given-names></name>
<xref ref-type="aff" rid="aff-1">1</xref>
</contrib>
<contrib id="author-2" contrib-type="author">
<name name-style="western"><surname>Li</surname><given-names>Wei</given-names></name>
<xref ref-type="aff" rid="aff-1">1</xref>
</contrib>
<contrib id="author-3" contrib-type="author">
<name name-style="western"><surname>Wang</surname><given-names>Yuanyuan</given-names></name>
<xref ref-type="aff" rid="aff-1">1</xref>
</contrib>
<contrib id="author-4" contrib-type="author">
<name name-style="western"><surname>Zhang</surname><given-names>Pan</given-names></name>
<xref ref-type="aff" rid="aff-1">1</xref>
</contrib>
<contrib id="author-5" contrib-type="author">
<name name-style="western"><surname>Wang</surname><given-names>Lina</given-names></name>
<xref ref-type="aff" rid="aff-1">1</xref>
</contrib>
<contrib id="author-6" contrib-type="author">
<name name-style="western"><surname>Liu</surname><given-names>Xinying</given-names></name>
<xref ref-type="aff" rid="aff-1">1</xref>
</contrib>
<contrib id="author-7" contrib-type="author">
<name name-style="western"><surname>Dong</surname><given-names>Meiqin</given-names></name>
<xref ref-type="aff" rid="aff-2">2</xref>
</contrib>
<contrib id="author-8" contrib-type="author">
<name name-style="western"><surname>Cao</surname><given-names>Xuewen</given-names></name>
<xref ref-type="aff" rid="aff-2">2</xref>
</contrib>
<contrib id="author-9" contrib-type="author" corresp="yes">
<name name-style="western"><surname>Bian</surname><given-names>Jiang</given-names></name>
<xref ref-type="aff" rid="aff-3">3</xref><email>bj@yangtzeu.edu.cn</email>
</contrib>
<aff id="aff-1"><label>1</label><institution>Technical Inspection Center, Sionpec Shengli Oilfield Company</institution>, <addr-line>Dongying, 257000, China</addr-line></aff>
<aff id="aff-2"><label>2</label><institution>College of Pipeline and Civil Engineering, China University of Petroleum (East China)</institution>, <addr-line>Qingdao, 266580, China</addr-line></aff>
<aff id="aff-3"><label>3</label><institution>School of Petroleum Engineering, Yangtze University</institution>, <addr-line>Wuhan, 430100</addr-line>, <country>China</country></aff>
</contrib-group><author-notes><corresp id="cor1"><label>&#x002A;</label>Corresponding Author: Jiang Bian. Email: <email>bj@yangtzeu.edu.cn</email></corresp></author-notes>
<pub-date date-type="collection" publication-format="electronic">
<year>2025</year>
</pub-date>
<pub-date date-type="pub" publication-format="electronic">
<day>24</day><month>1</month><year>2025</year>
</pub-date>
<volume>21</volume>
<issue>1</issue>
<fpage>107</fpage>
<lpage>119</lpage>
<history>
<date date-type="received"><day>09</day><month>9</month><year>2024</year></date>
<date date-type="accepted"><day>03</day><month>12</month><year>2024</year></date>
</history>
<permissions>
<copyright-statement>&#x00A9; 2025 The Authors.</copyright-statement>
<copyright-year>2025</copyright-year>
<copyright-holder>Published by Tech Science Press.</copyright-holder>
<license xlink:href="https://creativecommons.org/licenses/by/4.0/">
<license-p>This work is licensed under a <ext-link ext-link-type="uri" xlink:type="simple" xlink:href="https://creativecommons.org/licenses/by/4.0/">Creative Commons Attribution 4.0 International License</ext-link>, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.</license-p>
</license>
</permissions>
<self-uri content-type="pdf" xlink:href="TSP_FDMP_58295.pdf"></self-uri>
<abstract><p>
Gas-liquid flow (GLF), especially slug and annular flows in oil and gas gathering and transportation pipelines, become particularly complex inside elbows and can easily exacerbate pipeline corrosion and damage. In this study, FLUENT was used to conduct 3D simulations of slug and annular flow in elbows for different velocities to assess the ensuing changes in terms of pressure. In particular, the multifluid VOF (Volume of Fraction) model was chosen. The results indicate that under both slug and annular flow conditions, the pressure inside the elbow is lower than the outside. As the superficial velocity of liquid and gas increase, the pressure and liquid flow velocity at different positions of the elbow also increase, while the secondary flow weakens. Under annular flow conditions, the liquid film on the outer side of the elbow is thicker than that on the inner side, and the liquid velocity in the main liquid film zone is the lowest.</p>
</abstract>
<kwd-group kwd-group-type="author">
<kwd>Gas-liquid flow</kwd>
<kwd>elbow</kwd>
<kwd>CFD</kwd>
<kwd>VOF model</kwd>
</kwd-group>
<funding-group>
<award-group id="awg1">
<funding-source>Ministry of Industry and Information Technology High Tech Ship Special Project</funding-source>
<award-id>CBG3N21-2-6</award-id>
</award-group>
</funding-group>
</article-meta>
</front>
<body>
<sec id="s1">
<label>1</label>
<title>Introduction</title>
<p>Gas-liquid flow (GLF) widely occurs in petroleum and natural gas engineering. Slug and annular flows are two common flow patterns [<xref ref-type="bibr" rid="ref-1">1</xref>] occurring at high gas and low liquid flow rates [<xref ref-type="bibr" rid="ref-2">2</xref>]. In slug flow, fluctuations in parameters such as velocity and pressure may affect the safe transportation of pipelines. In an annular flow, the liquid phase flows in the form of a liquid film on the pipe wall, the gas phase flows in the center of the pipe, and some of the liquid film flows in the form of droplets in the gas phase owing to the shear effect of the airflow. When an annular flow flows through an elbow, a secondary flow and flow separation occur, and changes in the flow parameters can cause corrosion and damage to the pipeline. Therefore, studying the slug and annular flow characteristics of elbows is crucial for designing and maintaining piping systems [<xref ref-type="bibr" rid="ref-3">3</xref>].</p>
<p>Several studies have been conducted on the properties of slugs and annular flow. Yin et al. [<xref ref-type="bibr" rid="ref-4">4</xref>] experimentally and numerically investigated the gas-liquid slug flow in a hilly terrain pipeline at low superficial liquid velocities and explained the evolutionary process of slug flow in a corrugated pipeline through pressure drop fluctuations, liquid-holding rates, and phase distributions. Widodo et al. [<xref ref-type="bibr" rid="ref-5">5</xref>] discussed the flow law of a 45&#x00B0; vertical&#x2013;upward horizontal pipe. The frequency of the slug flow increased with gas velocity, whereas the pressure drop decreased. Akhlaghi et al. [<xref ref-type="bibr" rid="ref-6">6</xref>] studied the slug flow in a pipeline and observed that the SGV (superficial gas velocity) had a greater effect on the start position of the slug and the fully developed length of the slug than the SLV (superficial liquid velocity), and that an increase in the SLV decreased the slug length and liquid film thickness, whereas the liquid slug length and lateral slug velocity increased. Gourma et al. [<xref ref-type="bibr" rid="ref-7">7</xref>] numerically investigated the forces and loads of the slug flow in an elbow using a VOF (Volume of Fraction) model. Abdulkadir et al. [<xref ref-type="bibr" rid="ref-8">8</xref>] conducted studies on slug flow and reported that CFD (Computational Fluid Dynamics) simulations can predict the flow pattern before and after the elbow. Kesana et al. [<xref ref-type="bibr" rid="ref-9">9</xref>] and Parsi et al. [<xref ref-type="bibr" rid="ref-10">10</xref>] reported that the erosion rate of the slug flow increased with increasing grain size, SGV, and SLV. Al-Lababidi et al. [<xref ref-type="bibr" rid="ref-11">11</xref>,<xref ref-type="bibr" rid="ref-12">12</xref>] investigated the movement of sand particles in a slug flow in a pipe.</p>
<p>Researchers have also studied annular-flow liquid films in both vertical and horizontal tubes. Jing et al. [<xref ref-type="bibr" rid="ref-13">13</xref>] conducted experiments on oil&#x2013;water flow in a pipeline with a 90&#x00B0; elbow and assessed the effect of the elbow on the stability of annular flow evolution by comparative analysis of the flow pattern and friction pressure gradient in the upstream and downstream sections; however, they lacked a detailed characterization of the distribution characteristics of the different phases in the pipeline cross-section. L&#x00F3;pez et al. [<xref ref-type="bibr" rid="ref-14">14</xref>] conducted indoor experiments and numerical simulations of gas-liquid annular flow in a 180&#x00B0; elbow and described the effects of the radius of curvature and SGV on the behavior of the liquid film and the flow characteristics of the annular flow. Tkaczyk et al. [<xref ref-type="bibr" rid="ref-15">15</xref>] simulated gas-liquid annular flow in an elbow based on a modified fluid volume method using the finite volume method. Bandyopadhyay et al. [<xref ref-type="bibr" rid="ref-16">16</xref>] studied annular flow in four types of U-shaped elbows and compared the results calculated using FLUENT with the experimental results. Ribeiro et al. [<xref ref-type="bibr" rid="ref-17">17</xref>] investigated the droplet size in a two-phase horizontal annular flow at different gas-liquid ratios. The experimental results showed that the droplets enlarged after passing through the elbow. Abdulkadir et al. [<xref ref-type="bibr" rid="ref-18">18</xref>] experimentally investigated the liquid-film thickness distribution in a 180&#x00B0; reflux elbow. The experimental results revealed that, at higher liquid flow rates, the liquid film thickness in the inner part of the elbow was relatively high. Li et al. [<xref ref-type="bibr" rid="ref-19">19</xref>] experimentally investigated the effects of the superficial velocity on the slug and annular flow characteristics at micro-T junctions. Wu et al. [<xref ref-type="bibr" rid="ref-20">20</xref>] investigated the hydrodynamic characteristics of an annular flow in a 90&#x00B0; elbow using a VOF model.</p>
<p>Horizontal 90&#x00B0; elbows are widely used in natural-gas-gathering pipelines and constitute one of the most severely eroded and worn locations in pipeline systems. The erosion rate of the elbow section was much higher than that of the straight pipe section, with a magnitude approximately 50 times that of the straight pipe section. The elbow section is the weakest link in a mixed-flow pipeline and is the most susceptible to erosion and damage. Therefore, studying the flow characteristics of the slug and annular flows in the elbow section is helpful for studying elbow erosion and erosion resistance. Therefore, CFD numerical simulation methods were used to study the phase, pressure, and velocity distributions inside pipelines under different velocity conditions as well as the influence of elbows on the slug and annular flow laws. The aim of this research is to provide a more accurate and comprehensive description of the characteristic parameters of slug and annular flow at elbows and to provide theoretical guidance for the study of erosion mechanisms, elbow design, and protection of elbows to provide a theoretical basis and assistance for the study of oil and gas mixed transportation technology and multiphase-flow elbow erosion and corrosion, ultimately ensuring the economic and safe production and operation of oil and gas fields.</p>
</sec>
<sec id="s2">
<label>2</label>
<title>Numerical Methods</title>
<sec id="s2_1">
<label>2.1</label>
<title>Geometric Model</title>
<p>The simulated elbow was a 90&#x00B0; elbow, the pipe diameter <italic>D</italic> &#x003D; 50 mm, and the bending ratio <italic>R</italic>/<italic>D</italic> &#x003D; 5, which was the same as that in the experiment. Because the numerical simulation in this study involves transient calculation, to ensure the full development of the GLF in the pipe while considering the calculation consumption of the model, the lengths of the inlet of the elbow is 100<italic>D</italic>, the length of the outlet is 30<italic>D</italic>, the length of the inlet of the elbow is 30<italic>D</italic>, and the length of the outlet is 20<italic>D</italic>. The geometric model is shown in <xref ref-type="fig" rid="fig-1">Fig. 1</xref>.</p>
<fig id="fig-1">
<label>Figure 1</label>
<caption>
<title>Geometric model of a 90&#x00B0; horizontal elbow</title></caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FDMP_58295-fig-1.tif"/>
</fig>
</sec>
<sec id="s2_2">
<label>2.2</label>
<title>Mesh Generation</title>
<p>A quadrilateral mesh was adopted to divide the faces of the elbows, an O-block was used at the entrances and exits, and the grid density near the boundary was relatively high. After meshing, the hexahedral structured mesh is converted into an unstructured mesh in ICEM and exported for storage. To check the grid dependence, different numbers of grids were generated, and the grid independence verification results are shown in <xref ref-type="table" rid="table-1">Table 1</xref>. The number of grid nodes of the slug and annular flows in this study were 463,375 and 193,775, respectively; the numbers of grids were 439,680 and 183,680, respectively; and the mesh quality was 0.642. The details of the meshing division are shown in <xref ref-type="fig" rid="fig-2">Fig. 2</xref>.</p>
<table-wrap id="table-1"><label>Table 1</label>
<caption>
<title>Grid independence verification results</title></caption>
<table><colgroup>
<col/>
<col/>
<col/>
<col/>
</colgroup>
<thead>
<tr>
<th>Geometric model</th>
<th>Number of grids</th>
<th>Pressure at the center of the outlet section/Pa</th>
<th>Deviation/%</th>
</tr>
</thead>
<tbody>
<tr>
<td rowspan="4">For slug flow</td>
<td>144,518</td>
<td>10,850</td>
<td>5.85</td>
</tr>
<tr>
<td>235,341</td>
<td>11,354</td>
<td>1.48</td>
</tr>
<tr>
<td>463,375</td>
<td>11,458</td>
<td>0.57</td>
</tr>
<tr>
<td>889,155</td>
<td>11,524</td>
<td>/</td>
</tr>
<tr>
<td rowspan="4">For annular flow</td>
<td>39,984</td>
<td>10,951</td>
<td>8.60</td>
</tr>
<tr>
<td>85,223</td>
<td>11,705</td>
<td>2.30</td>
</tr>
<tr>
<td>193,775</td>
<td>11,902</td>
<td>0.66</td>
</tr>
<tr>
<td>412,517</td>
<td>11,981</td>
<td>/</td>
</tr>
</tbody>
</table>
</table-wrap><fig id="fig-2">
<label>Figure 2</label>
<caption>
<title>Elbow mesh division</title></caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FDMP_58295-fig-2.tif"/>
</fig>
</sec>
<sec id="s2_3">
<label>2.3</label>
<title>Physical Model</title>
<p>The flow of the GLF is modeled by a numerical solution of a set of equations describing the broadest case of medium movement. The numerical models (including the mass and momentum equations) of the GLF are as follows [<xref ref-type="bibr" rid="ref-21">21</xref>]:</p>
<p>(1) Continuity equation<disp-formula id="eqn-1"><label>(1)</label>
<mml:math id="mml-eqn-1" display="block"><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03C1;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>t</mml:mi></mml:mrow></mml:mfrac></mml:mrow><mml:mo>+</mml:mo><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mo>&#x22C5;</mml:mo><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mi>&#x03C1;</mml:mi><mml:mover><mml:mrow><mml:msub><mml:mi>u</mml:mi><mml:mi>l</mml:mi></mml:msub></mml:mrow><mml:mo>&#x2192;</mml:mo></mml:mover></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:mstyle></mml:math>
</disp-formula>where <inline-formula id="ieqn-1">
<mml:math id="mml-ieqn-1"><mml:mi>&#x03C1;</mml:mi><mml:mo>=</mml:mo><mml:mrow><mml:msub><mml:mi>&#x03C1;</mml:mi><mml:mi>l</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>&#x03B1;</mml:mi><mml:mi>l</mml:mi></mml:msub></mml:mrow><mml:mo>+</mml:mo><mml:mo stretchy="false">(</mml:mo><mml:mn>1</mml:mn><mml:mo>&#x2212;</mml:mo><mml:mrow><mml:msub><mml:mi>&#x03B1;</mml:mi><mml:mi>l</mml:mi></mml:msub></mml:mrow><mml:mo stretchy="false">)</mml:mo><mml:mrow><mml:msub><mml:mi>&#x03C1;</mml:mi><mml:mi>g</mml:mi></mml:msub></mml:mrow></mml:math>
</inline-formula>, <italic>&#x03C1;</italic><sub><italic>l</italic></sub> and <italic>&#x03C1;</italic><sub><italic>g</italic></sub> represent the density of liquid and gas, <italic>&#x03B1;</italic><sub><italic>l</italic></sub> represents the phase volume fraction of liquid, <inline-formula id="ieqn-2">
<mml:math id="mml-ieqn-2"><mml:mover><mml:mi>u</mml:mi><mml:mo>&#x2192;</mml:mo></mml:mover></mml:math>
</inline-formula> is the velocity vector, and <italic>t</italic> is the time.</p>
<p>(2) Momentum conservation equation<disp-formula id="eqn-2"><label>(2)</label>
<mml:math id="mml-eqn-2" display="block"><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mi>&#x03C1;</mml:mi><mml:mrow><mml:msub><mml:mi>u</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:mrow><mml:mo>)</mml:mo></mml:mrow></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>t</mml:mi></mml:mrow></mml:mfrac></mml:mrow><mml:mo>+</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mi>&#x03C1;</mml:mi><mml:mrow><mml:msub><mml:mi>u</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>u</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:mrow><mml:mo>)</mml:mo></mml:mrow></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>p</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow><mml:mo>+</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:msub><mml:mi>&#x03C4;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow><mml:mo>+</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msubsup><mml:mi>&#x03C4;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mrow><mml:mi>Re</mml:mi></mml:mrow></mml:mrow></mml:msubsup></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow><mml:mo>+</mml:mo><mml:mi>&#x03C1;</mml:mi><mml:mrow><mml:msub><mml:mi>g</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:mstyle></mml:mstyle></mml:mstyle></mml:mstyle></mml:mstyle></mml:math>
</disp-formula>where <italic>p</italic>, <italic>&#x03C1;</italic>, <italic>&#x03C4;</italic><sub><italic>ij</italic></sub> and <inline-formula id="ieqn-3">
<mml:math id="mml-ieqn-3"><mml:msubsup><mml:mi>&#x03C4;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mrow><mml:mi>Re</mml:mi></mml:mrow></mml:mrow></mml:msubsup></mml:math>
</inline-formula> represent the static pressure, the density of a combined phase, the stress tensor, and the turbulent stress, respectively. <italic>g</italic><sub><italic>i</italic></sub> represents the gravitational volume force in the <italic>i</italic>-direction.</p>
<p>(3) Turbulence model</p>
<p>The standard <italic>k&#x2013;&#x03B5;</italic> turbulence model is used in this study, and the <italic>k</italic> and <italic>&#x03B5;</italic> equations are expressed as follows:<disp-formula id="eqn-3"><label>(3)</label>
<mml:math id="mml-eqn-3" display="block"><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mi>p</mml:mi><mml:mi>k</mml:mi></mml:mrow><mml:mo>)</mml:mo></mml:mrow></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>t</mml:mi></mml:mrow></mml:mfrac></mml:mrow><mml:mo>+</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mi>p</mml:mi><mml:mi>k</mml:mi><mml:mrow><mml:msub><mml:mi>u</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:mrow><mml:mo>)</mml:mo></mml:mrow></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow><mml:mo>=</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow><mml:mrow><mml:mo>[</mml:mo><mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mi>&#x03BC;</mml:mi><mml:mo>+</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mrow><mml:msub><mml:mi>&#x03BC;</mml:mi><mml:mi>t</mml:mi></mml:msub></mml:mrow></mml:mrow><mml:mrow><mml:mi>&#x03C3;</mml:mi><mml:mi>k</mml:mi></mml:mrow></mml:mfrac></mml:mrow></mml:mstyle></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>k</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow></mml:mstyle></mml:mrow><mml:mo>]</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mrow><mml:msub><mml:mi>G</mml:mi><mml:mi>K</mml:mi></mml:msub></mml:mrow><mml:mo>+</mml:mo><mml:mrow><mml:msub><mml:mi>G</mml:mi><mml:mi>b</mml:mi></mml:msub></mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mi>p</mml:mi><mml:mi>&#x03B5;</mml:mi><mml:mo>&#x2212;</mml:mo><mml:mrow><mml:msub><mml:mi>Y</mml:mi><mml:mi>M</mml:mi></mml:msub></mml:mrow><mml:mo>+</mml:mo><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mi>k</mml:mi></mml:msub></mml:mrow></mml:mstyle></mml:mstyle></mml:mstyle></mml:math>
</disp-formula></p>
<p><disp-formula id="eqn-4"><label>(4)</label>
<mml:math id="mml-eqn-4" display="block"><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mi>p</mml:mi><mml:mi>&#x03B5;</mml:mi></mml:mrow><mml:mo>)</mml:mo></mml:mrow></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>t</mml:mi></mml:mrow></mml:mfrac></mml:mrow><mml:mo>+</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mi>p</mml:mi><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:msub><mml:mi>u</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:mrow><mml:mo>)</mml:mo></mml:mrow></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow><mml:mo>=</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow><mml:mrow><mml:mo>[</mml:mo><mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mi>&#x03BC;</mml:mi><mml:mo>+</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mrow><mml:msub><mml:mi>&#x03BC;</mml:mi><mml:mi>t</mml:mi></mml:msub></mml:mrow></mml:mrow><mml:mrow><mml:mi>&#x03C3;</mml:mi><mml:mi>e</mml:mi></mml:mrow></mml:mfrac></mml:mrow></mml:mstyle></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03B5;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow></mml:mstyle></mml:mrow><mml:mo>]</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mrow><mml:msub><mml:mi>C</mml:mi><mml:mrow><mml:mn>1</mml:mn><mml:mi>&#x03B5;</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mi>&#x03B5;</mml:mi><mml:mi>k</mml:mi></mml:mfrac></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mrow><mml:msub><mml:mi>G</mml:mi><mml:mi>k</mml:mi></mml:msub></mml:mrow><mml:mo>+</mml:mo><mml:mrow><mml:msub><mml:mi>G</mml:mi><mml:mrow><mml:mn>3</mml:mn><mml:mi>&#x03B5;</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>G</mml:mi><mml:mi>b</mml:mi></mml:msub></mml:mrow></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mrow><mml:msub><mml:mi>C</mml:mi><mml:mrow><mml:mn>2</mml:mn><mml:mi>&#x03B5;</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mi>p</mml:mi><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mrow><mml:msup><mml:mi>&#x03B5;</mml:mi><mml:mn>2</mml:mn></mml:msup></mml:mrow></mml:mrow><mml:mi>k</mml:mi></mml:mfrac></mml:mrow><mml:mo>+</mml:mo><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mi>&#x03B5;</mml:mi></mml:msub></mml:mrow></mml:mstyle></mml:mstyle></mml:mstyle></mml:mstyle></mml:mstyle></mml:math>
</disp-formula>where <inline-formula id="ieqn-4">
<mml:math id="mml-ieqn-4"><mml:mrow><mml:msub><mml:mi>Y</mml:mi><mml:mi>M</mml:mi></mml:msub></mml:mrow></mml:math>
</inline-formula> is the diffusion loss, <italic>&#x03C3;</italic><sub><italic>k</italic></sub> and <italic>&#x03C3;</italic><sub><italic>e</italic></sub> are the Prandtl numbers of <italic>k</italic> and <italic>&#x03B5;</italic> equations, respectively, and <inline-formula id="ieqn-5">
<mml:math id="mml-ieqn-5"><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mi>k</mml:mi></mml:msub></mml:mrow></mml:math>
</inline-formula> and <inline-formula id="ieqn-6">
<mml:math id="mml-ieqn-6"><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mi>&#x03B5;</mml:mi></mml:msub></mml:mrow></mml:math>
</inline-formula> are user-defined terms. <inline-formula id="ieqn-7">
<mml:math id="mml-ieqn-7"><mml:mrow><mml:msub><mml:mi>G</mml:mi><mml:mi>k</mml:mi></mml:msub></mml:mrow></mml:math>
</inline-formula> is the turbulent kinetic energy obtained from <inline-formula id="ieqn-8">
<mml:math id="mml-ieqn-8"><mml:mrow><mml:msub><mml:mi>G</mml:mi><mml:mi>k</mml:mi></mml:msub></mml:mrow><mml:mo>=</mml:mo><mml:mrow><mml:msub><mml:mi>&#x03BC;</mml:mi><mml:mi>t</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:msup><mml:mi>S</mml:mi><mml:mn>2</mml:mn></mml:msup></mml:mrow></mml:math>
</inline-formula>. <inline-formula id="ieqn-9">
<mml:math id="mml-ieqn-9"><mml:mi>S</mml:mi></mml:math>
</inline-formula> is the coefficient of the stress tensor, which can be obtained using <inline-formula id="ieqn-10">
<mml:math id="mml-ieqn-10"><mml:mi>S</mml:mi><mml:mo>=</mml:mo><mml:msqrt><mml:mn>2</mml:mn><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:msqrt></mml:math>
</inline-formula>. <inline-formula id="ieqn-11">
<mml:math id="mml-ieqn-11"><mml:mrow><mml:msub><mml:mi>G</mml:mi><mml:mi>b</mml:mi></mml:msub></mml:mrow></mml:math>
</inline-formula> is the turbulent kinetic energy generated by buoyancy, which can be obtained using <inline-formula id="ieqn-12">
<mml:math id="mml-ieqn-12"><mml:mrow><mml:msub><mml:mi>G</mml:mi><mml:mi>b</mml:mi></mml:msub></mml:mrow><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mi>g</mml:mi><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mrow><mml:msub><mml:mi>&#x03BC;</mml:mi><mml:mi>t</mml:mi></mml:msub></mml:mrow></mml:mrow><mml:mrow><mml:mi>&#x03C1;</mml:mi><mml:mi>P</mml:mi><mml:mrow><mml:msub><mml:mi>r</mml:mi><mml:mi>t</mml:mi></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>p</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow></mml:mstyle></mml:mstyle></mml:math>
</inline-formula> and <inline-formula id="ieqn-13">
<mml:math id="mml-ieqn-13"><mml:mi>P</mml:mi><mml:mrow><mml:msub><mml:mi>r</mml:mi><mml:mi>t</mml:mi></mml:msub></mml:mrow><mml:mo>=</mml:mo><mml:mn>0.85</mml:mn></mml:math>
</inline-formula>. <inline-formula id="ieqn-14">
<mml:math id="mml-ieqn-14"><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math>
</inline-formula> is the mean strain rate obtained via <inline-formula id="ieqn-15">
<mml:math id="mml-ieqn-15"><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mo>=</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mn>1</mml:mn><mml:mn>2</mml:mn></mml:mfrac></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:msub><mml:mi>u</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow><mml:mo>+</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:msub><mml:mi>u</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow></mml:mstyle></mml:mstyle></mml:mrow><mml:mo>)</mml:mo></mml:mrow></mml:mstyle></mml:math>
</inline-formula>. The coefficients <italic>C</italic> and <italic>&#x03B7;</italic> are obtained using <inline-formula id="ieqn-16">
<mml:math id="mml-ieqn-16"><mml:mi>C</mml:mi><mml:mo>=</mml:mo><mml:mo movablelimits="true" form="prefix">max</mml:mo><mml:mrow><mml:mo>[</mml:mo><mml:mrow><mml:mn>0.43</mml:mn><mml:mo>,</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mi>&#x03B7;</mml:mi><mml:mo>+</mml:mo><mml:mn>5</mml:mn></mml:mrow></mml:mfrac></mml:mrow></mml:mstyle></mml:mrow><mml:mo>]</mml:mo></mml:mrow></mml:math>
</inline-formula>, <inline-formula id="ieqn-17">
<mml:math id="mml-ieqn-17"><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mo>=</mml:mo></mml:mrow><mml:mi>S</mml:mi><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mi>k</mml:mi><mml:mi>&#x03B5;</mml:mi></mml:mfrac></mml:mrow></mml:mstyle></mml:math>
</inline-formula>.</p>
</sec>
<sec id="s2_4">
<label>2.4</label>
<title>Numerical Simulation Solution Setting</title>
<p>The pressure-based unsteady state was chosen for the solution calculation, the <italic>Y</italic>-axis was set with a gravity of 9.81 m/s<sup>2</sup>, and the negative sign indicated that the gravity direction was along the negative direction of the <italic>Y</italic>-axis. The multifluid VOF model is activated, the explicit computation is selected, the Courant number is set to 0.25, the convergence condition is set to residuals of less than 10<sup>&#x2212;5</sup>, and the turbulence model is selected to be the standard <italic>k&#x2013;&#x03B5;</italic> model. Air and water were used as primary and secondary phases, respectively. The inlet was divided into two parts in FLUENT: the slug-flow simulation inlet was layered with a height ratio of 0.5, and the annular-flow simulation inlet was divided into a small circle with a radius of 20 mm and a ring, with air flowing through the red channel and water flowing through the blue channel, as shown in <xref ref-type="fig" rid="fig-3">Fig. 3</xref>. The inlet and outlet were set as the velocity and pressure outlet boundary conditions, respectively, and the wall adopted a no-slip wall boundary condition. The input GLF rate at the inlet needs to be recalculated according to the principle of mass flow conservation. For example, the value of the input flow rate at the liquid phase inlet is equal to the superficial flow rate of the liquid phase multiplied by the ratio of the cross-sectional area of the pipeline and the cross-sectional area of the liquid phase inlet. The input GLF rates for this slug flow simulation were twice the superficial flow rate, the input gas flow rate for the annular flow simulation was the value of the SGV divided by 0.64, the input liquid flow rate was the value of the SLV divided by 0.36, and the outlet pressures were all set to atmospheric pressure.</p>
<fig id="fig-3">
<label>Figure 3</label>
<caption>
<title>Inlet of gas-liquid two-phase</title></caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FDMP_58295-fig-3.tif"/>
</fig>
<p>In FLUENT, for the transient numerical simulation calculation of multiphase flow under the condition of convergence, to improve accuracy, the numerical simulation solution settings in this study are listed in <xref ref-type="table" rid="table-2">Table 2</xref>.</p>
<table-wrap id="table-2"><label>Table 2</label>
<caption>
<title>Settings of the solution methods for the numerical simulation</title></caption>
<table><colgroup>
<col/>
<col/>
<col/>
</colgroup>
<thead>
<tr>
<th>Solution method</th>
<th>Slug flow</th>
<th>Annular flow</th>
</tr>
</thead>
<tbody>
<tr>
<td>Pressure-velocity coupling</td>
<td>Phase coupled SIMPLE</td>
<td>Phase coupled SIMPLE</td>
</tr>
<tr>
<td>Spatial gradient discretization</td>
<td>Least squares cell based</td>
<td>Least squares cell based</td>
</tr>
<tr>
<td>Volume fraction discretization</td>
<td>Geo-reconstruct</td>
<td>Geo-reconstruct</td>
</tr>
<tr>
<td>Turbulent dissipation rate discretization</td>
<td rowspan="2"></td>
<td rowspan="2"></td>
</tr>
<tr>
<td>Concentration discretization in the interfacial region</td>
</tr>
<tr>
<td>Time step size</td>
<td>0.001</td>
<td>0.00001</td>
</tr>
</tbody>
</table>
</table-wrap>
</sec>
<sec id="s2_5">
<label>2.5</label>
<title>Determination of the Simulated GLF Rate</title>
<p>Numerical simulation research is an expansion and supplementation of experimental research. This study conducted numerical simulations under some experimental research conditions, and the conditions for the GLF rate are listed in <xref ref-type="table" rid="table-3">Table 3</xref>.</p>
<table-wrap id="table-3"><label>Table 3</label>
<caption>
<title>Numerical simulation of selected gas-liquid velocities</title></caption>
<table><colgroup>
<col/>
<col/>
<col/>
</colgroup>
<thead>
<tr>
<th>Flow pattern</th>
<th>SGV (m/s)</th>
<th>SLV (m/s)</th>
</tr>
</thead>
<tbody>
<tr>
<td rowspan="3">Slug flow</td>
<td>2</td>
<td>1.00</td>
</tr>
<tr>
<td>2</td>
<td>1.75</td>
</tr>
<tr>
<td>5</td>
<td>1.00</td>
</tr>
<tr>
<td rowspan="3">Annular flow</td>
<td>20</td>
<td>0.20</td>
</tr>
<tr>
<td>35</td>
<td>0.20</td>
</tr>
<tr>
<td>35</td>
<td>0.35</td>
</tr>
</tbody>
</table>
</table-wrap>
</sec>
<sec id="s2_6">
<label>2.6</label>
<title>Model Validation</title>
<p>Using the experimental conditions of a superficial gas velocity of 35 m/s and a superficial liquid velocity of 0.20 m/s as examples, the gas content at the inlet and outlet of the bent pipe was obtained through WMS processing, and the simulation results based on the established model were compared with the experimental data (as shown in <xref ref-type="fig" rid="fig-4">Fig. 4</xref>). Because the length of the experimental pipeline is longer than that of the model, as well as because of factors such as fluctuations in the amount of incoming gas and liquid, the simulation results have slight deviations from the experimental results, but are generally close, and the trend of change is the same.</p>
<fig id="fig-4">
<label>Figure 4</label>
<caption>
<title>Comparison between experimental and simulated value of air content at the outlet of 90&#x00B0; elbow</title></caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FDMP_58295-fig-4.tif"/>
</fig>
</sec>
</sec>
<sec id="s3">
<label>3</label>
<title>Results and Discussion</title>
<sec id="s3_1">
<label>3.1</label>
<title>Simulation Results of Slug Flow in the Elbow Section</title>
<p>Transient numerical simulations were performed for three sets of conditions with superficial gas and liquid velocities of 2 and 1 m/s, 2 and 1.75 m/s, and 5 and 1 m/s, respectively, for the slug flow. Pressure cloud diagrams, liquid velocity cloud diagrams, and vector diagrams corresponding to the liquid slug in the pipe under different velocities in the horizontal pipe slug flow were obtained to analyze the flow characteristics of the slug flow in the horizontal pipe, such as pressure and liquid velocity, and to study the effects of changes in the GLF velocity.</p>
<sec id="s3_1_1">
<label>3.1.1</label>
<title>Pressure Cloud Diagram</title>
<p>The results of the transient simulation of the three sets of slug flows were processed via CFD-Post to obtain the pressure cloud diagrams in the elbow at different velocities (<xref ref-type="fig" rid="fig-5">Fig. 5</xref>).</p>
<fig id="fig-5">
<label>Figure 5</label>
<caption>
<title>Pressure diagrams of slug flow in elbow</title></caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FDMP_58295-fig-5.tif"/>
</fig>
<p>As shown in <xref ref-type="fig" rid="fig-5">Fig. 5</xref>, the pressure of the entire pipeline decreased because of the energy consumption of the fluid during the flow process. In the pressure cloud diagrams of the axial and radial sections, the pressure in the elbow was uneven. The pressure on the outer side of the elbow was greater than that on the inner side and gradually decreased from the outer to the inner part of the elbow. A centrifugal force inside the elbow causes air bubbles in the liquid slug to flow on the inner side of the elbow, resulting in a stepped radial pressure distribution in the elbow.</p>
</sec>
<sec id="s3_1_2">
<label>3.1.2</label>
<title>Liquid Velocity Cloud Diagram and Vector Diagram</title>
<p>The results of the transient simulation of the three sets of slug flows were processed using CFD-Post to obtain the liquid velocity cloud diagrams (<xref ref-type="fig" rid="fig-6">Fig. 6</xref>).</p>
<fig id="fig-6">
<label>Figure 6</label>
<caption>
<title>Liquid velocity cloud and vector diagrams of slug flow in elbows</title></caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FDMP_58295-fig-6.tif"/>
</fig>
<p>According to the velocity cloud diagram of the axial section shown in <xref ref-type="fig" rid="fig-6">Fig. 6</xref>, the liquid velocity in the liquid slug region is the highest. Because of the centrifugal force, the liquid velocity inside the elbow was uneven, and the liquid velocity on the outer side was larger than that on the inner side. As SLV and SGV increased, the liquid velocity in the slug flow also increased.</p>
<p>According to the axial and radial section velocity vector diagrams, the liquid was biased toward the outside of the elbow flow owing to the centrifugal force of the elbow. The secondary flow at the center and outlet sections of the elbow formed vortices; however, as the GLF velocity increased, the secondary flow weakened.</p>
</sec>
</sec>
<sec id="s3_2">
<label>3.2</label>
<title>Simulation Results of Annular Flow in an Elbow</title>
<p>Transient simulations were conducted for three sets of conditions with superficial gas and liquid velocities of 20 and 0.20 m/s, 35 and 0.20 m/s, and 35 and 0.35 m/s, respectively, for annular flow. Pressure distribution cloud diagrams, liquid velocity cloud diagrams, and vector diagrams corresponding to different flow velocities of the elbow annular flow were obtained to analyze the effects of varying the gas and liquid flow velocities on the flow characteristics of the annular flow.</p>
<sec id="s3_2_1">
<label>3.2.1</label>
<title>Pressure Cloud Diagram</title>
<p>The results of the three sets of annular flow transient simulations were processed using CFD-Post to obtain the pressure cloud diagrams of the annular flow (<xref ref-type="fig" rid="fig-7">Fig. 7</xref>).</p>
<fig id="fig-7">
<label>Figure 7</label>
<caption>
<title>Pressure nephogram of annular flow in an elbow</title></caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FDMP_58295-fig-7.tif"/>
</fig>
<p>As shown in <xref ref-type="fig" rid="fig-7">Fig. 7</xref>, the pressure of the entire pipeline of the elbow annular flow shows a decreasing trend; although the pressure of the inner elbow is lower than that of the outer elbow, the difference in the inner and outer pressures is not significant. This is mainly because although the liquid film distribution on the inner and outer pipe walls of the annular flow in the elbow is uneven, it can lead to differences in the inner and outer pressures of the elbow; however, this difference is not obvious at high gas velocities. A comparison of the pressure distributions in the elbow at different GLF rates revealed that the pressure at different positions on the elbow increased with increasing SLV and SGV; however, a change in the SGV had a greater effect on the elbow pressure.</p>
</sec>
<sec id="s3_2_2">
<label>3.2.2</label>
<title>Liquid Velocity Cloud Diagram and Vector Diagram</title>
<p>The results of the three sets of annular flow transient simulations were processed using CFD-Post to obtain the liquid velocity cloud diagrams and vector diagrams of the annular flow (<xref ref-type="fig" rid="fig-8">Fig. 8</xref>).</p>
<fig id="fig-8">
<label>Figure 8</label>
<caption>
<title>Liquid velocity cloud and vector diagram of annular flow in an elbow</title></caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FDMP_58295-fig-8.tif"/>
</fig>
<p>According to the liquid velocity cloud diagrams of the axial and radial sections in shown <xref ref-type="fig" rid="fig-8">Fig. 8</xref>, the distribution of the annular flow liquid velocity inside the elbow was uneven, and the velocity in the main liquid film area was the smallest. With increasing SLV, the annular flow velocity inside the elbow increased; however, an increase in the liquid film outside the elbow decreased the liquid velocity outside the elbow. As the SGV increased, the annular liquid flow rate in the elbow increased, the liquid film outside the elbow decreased, and the liquid flow rate outside the elbow increased.</p>
</sec>
</sec>
</sec>
<sec id="s4">
<label>4</label>
<title>Conclusion</title>
<p>In this study, the multifluid VOF model was selected in FLUENT for the numerical simulation of the elbow section. The flow fields corresponding to different calculation conditions of the slug and annular flow in the elbow section were obtained to analyze the effects of gas and liquid flow rate changes.</p>
<p>(1) The bubbles in the slug flow liquid slug of the elbow move inside the elbow, and the pressure in the entire pipeline decreases. The pressure inside the elbow was lower than that outside. The liquid velocity inside the elbow was uneven, and the liquid velocity outside the elbow was greater than that inside the elbow. There is a secondary flow in the elbow section, which has a small impact on the inlet of the elbow and a large impact on the center and downstream of the bend pipe.</p>
<p>(2) The liquid film of annular flow at outside the elbow was thicker than that inside the elbow, the pressure of the entire pipeline showed a downward trend, the pressure on the outside of the elbow was greater than that on the inside, the liquid flow velocity in the elbow was uneven, and the liquid velocity in the main liquid film area was the lowest. With increasing SLV and SGV, the pressure and liquid flow velocity at different positions in the elbow increased, and the secondary flow in the elbow weakened.</p>
<p>The above conclusion accurately and comprehensively describes the characteristic parameters of slug and annular flows at elbows and provides theoretical guidance for the study of erosion mechanisms, elbow design, and elbow protection. It also provides a theoretical basis and assistance for research on oil and gas mixed transportation technology and multiphase-flow elbow erosion and corrosion, ultimately ensuring economic and safe production and operation of oil and gas fields.</p>
</sec>
</body>
<back>
<ack>
<p>Thanks to the State Key Laboratory of Low Carbon Catalysis and Carbon Dioxide Utilization for supporting this work.</p>
</ack>
<sec>
<title>Funding Statement</title>
<p>This work was supported by the Ministry of Industry and Information Technology High Tech Ship Special Project (Grant No. CBG3N21-2-6).</p>
</sec>
<sec>
<title>Author Contributions</title>
<p>The authors confirm contribution to the paper as follows: study conception and design: Lihui Ma, Wei Li; data collection: Yuanyuan Wang, Pan Zhang; analysis and interpretation of results: Lina Wang, Xinying Liu, Xuewen Cao; draft manuscript preparation: Lihui Ma, Meiqin Dong, Jiang Bian. All authors reviewed the results and approved the final version of the manuscript.</p>
</sec>
<sec sec-type="data-availability">
<title>Availability of Data and Materials</title>
<p>The datasets generated and/or analyzed during the current study are available from the corresponding author on reasonable request.</p>
</sec>
<sec>
<title>Ethics Approval</title>
<p>Not applicable.</p>
</sec>
<sec sec-type="COI-statement">
<title>Conflicts of Interest</title>
<p>The authors declare no conflicts of interest to report regarding the present study.</p>
</sec>
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