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<front>
<journal-meta>
<journal-id journal-id-type="publisher-id">Front. Mater.</journal-id>
<journal-title>Frontiers in Materials</journal-title>
<abbrev-journal-title abbrev-type="pubmed">Front. Mater.</abbrev-journal-title>
<issn pub-type="epub">2296-8016</issn>
<publisher>
<publisher-name>Frontiers Media S.A.</publisher-name>
</publisher>
</journal-meta>
<article-meta>
<article-id pub-id-type="publisher-id">862601</article-id>
<article-id pub-id-type="doi">10.3389/fmats.2022.862601</article-id>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Materials</subject>
<subj-group>
<subject>Original Research</subject>
</subj-group>
</subj-group>
</article-categories>
<title-group>
<article-title>Numerical Modeling and Experimental Validation of TiC Nanoparticle Distribution During the Ultrasonic Casting Process of 2219 Aluminum Matrix Nanocomposites</article-title>
<alt-title alt-title-type="left-running-head">Yi-Long et al.</alt-title>
<alt-title alt-title-type="right-running-head">TiC /2219 Nanocomposites</alt-title>
</title-group>
<contrib-group>
<contrib contrib-type="author">
<name>
<surname>Yi-Long</surname>
<given-names>Yang</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
</contrib>
<contrib contrib-type="author" corresp="yes">
<name>
<surname>Yun</surname>
<given-names>Zhang</given-names>
</name>
<xref ref-type="aff" rid="aff2">
<sup>2</sup>
</xref>
<xref ref-type="aff" rid="aff3">
<sup>3</sup>
</xref>
<xref ref-type="corresp" rid="c001">&#x2a;</xref>
<uri xlink:href="https://loop.frontiersin.org/people/1564352/overview"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Hao-Ming</surname>
<given-names>Zhang</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Xu-He</surname>
<given-names>Liu</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
</contrib>
</contrib-group>
<aff id="aff1">
<sup>1</sup>
<institution>School of Mechanical Engineering</institution>, <institution>Henan University of Engineering</institution>, <addr-line>Zhengzhou</addr-line>, <country>China</country>
</aff>
<aff id="aff2">
<sup>2</sup>
<institution>College of Mechanical and Electrical Engineering</institution>, <institution>Central South University</institution>, <addr-line>Changsha</addr-line>, <country>China</country>
</aff>
<aff id="aff3">
<sup>3</sup>
<institution>State Key Laboratory of High Performance Complex Manufacturing</institution>, <institution>Central South University</institution>, <addr-line>Changsha</addr-line>, <country>China</country>
</aff>
<author-notes>
<fn fn-type="edited-by">
<p>
<bold>Edited by:</bold> <ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/1435935/overview">Peng Cao</ext-link>, The University of Auckland, New Zealand</p>
</fn>
<fn fn-type="edited-by">
<p>
<bold>Reviewed by:</bold> <ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/939066/overview">Rajkumar Kaliyamoorthy</ext-link>, SSN College of Engineering, India</p>
<p>
<ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/1677327/overview">Shenglu Lu</ext-link>, RMIT University, Australia</p>
</fn>
<corresp id="c001">&#x2a;Correspondence: Zhang Yun, <email>yun_zhang66@163.com</email>
</corresp>
<fn fn-type="other">
<p>This article was submitted to Structural Materials, a section of the journal Frontiers in Materials</p>
</fn>
</author-notes>
<pub-date pub-type="epub">
<day>13</day>
<month>04</month>
<year>2022</year>
</pub-date>
<pub-date pub-type="collection">
<year>2022</year>
</pub-date>
<volume>9</volume>
<elocation-id>862601</elocation-id>
<history>
<date date-type="received">
<day>26</day>
<month>01</month>
<year>2022</year>
</date>
<date date-type="accepted">
<day>21</day>
<month>03</month>
<year>2022</year>
</date>
</history>
<permissions>
<copyright-statement>Copyright &#xa9; 2022 Yi-Long, Yun, Hao-Ming and Xu-He.</copyright-statement>
<copyright-year>2022</copyright-year>
<copyright-holder>Yi-Long, Yun, Hao-Ming and Xu-He</copyright-holder>
<license xlink:href="http://creativecommons.org/licenses/by/4.0/">
<p>This is an open-access article distributed under the terms of the Creative Commons Attribution License (CC BY). The use, distribution or reproduction in other forums is permitted, provided the original author(s) and the copyright owner(s) are credited and that the original publication in this journal is cited, in accordance with accepted academic practice. No use, distribution or reproduction is permitted which does not comply with these terms.</p>
</license>
</permissions>
<abstract>
<p>In this work, a two-dimensional model of 0.9&#xa0;wt% TiC nanoparticle-reinforced 2219 aluminum nanocomposites fabricated by a high-intensity ultrasonic casting technique was established. The TiC nanoparticle distribution in 2219 aluminum melts was investigated using the multiphase computational fluid dynamics ultrasonic cavitation model accounting for turbulent flow. And the variable interaction between nanoparticles and melts was analyzed by Ansys&#x2019;s Fluent Dense Discrete phase Model According to the simulation results, the ultrasonic power had a significant effect on the distribution of TiC nanoparticles in aluminum melt. The appropriate ultrasonic power has a promoting effect on the dispersion of nanoparticles. Due to the impact of ultrasonic streaming, the number of nanoparticles in the center position was lower than that in the edge position of the molten pool. Moreover, casting experiments were carried out to verify the efficacy and accuracy of the simulation. The average grain size in the center position was smaller than that in the edge position. TEM and SEM were used to analyze the distribution of TiC nanoparticles. They were more evenly distributed in the center position of the ingot than those in the edge part. Besides more nanoparticles were agglomerated in the edge. The experimental results were mostly consistent with the simulation results.</p>
</abstract>
<kwd-group>
<kwd>aluminum matrix nanocomposite</kwd>
<kwd>CFD ultrasonic cavitation model</kwd>
<kwd>TiC nanoparticle distribution</kwd>
<kwd>experiment</kwd>
<kwd>microstructure</kwd>
</kwd-group>
<contract-sponsor id="cn001">Science and Technology Program of Hunan Province<named-content content-type="fundref-id">10.13039/501100019081</named-content>
</contract-sponsor>
<contract-sponsor id="cn002">Natural Science Foundation of Hunan Province<named-content content-type="fundref-id">10.13039/501100004735</named-content>
</contract-sponsor>
</article-meta>
</front>
<body>
<sec id="s1">
<title>Introduction</title>
<p>Metal matrix nanocomposites (MMNCs) have been widely applied in aerospace, automation, transportation, and military industries. The research on aluminum matrix composites has been going on several decades. Compared with ordinary aluminum alloys, aluminum matrix composites have higher hardness, strength, better corrosion resistance, and wear resistance (<xref ref-type="bibr" rid="B10">Hong Yang et al., 2019</xref>; <xref ref-type="bibr" rid="B5">Ding Yuan et al., 2021</xref>; <xref ref-type="bibr" rid="B32">Zhang et al., 2021</xref>; <xref ref-type="bibr" rid="B15">Liu et al., 2020</xref>). What&#x2019;s more, the performance of the composite can be further improved by reducing the size of the reinforcements. Nanoparticles reinforced aluminum matrix composites exhibit greater mechanical properties and ductility than microparticles reinforced aluminum matrix composites. Various reinforced phases have been investigated, including Al<sub>2</sub>O<sub>3</sub> (<xref ref-type="bibr" rid="B17">Malaki et al., 2019</xref>; <xref ref-type="bibr" rid="B13">Li et al., 2021</xref>), TiB<sub>2</sub> (<xref ref-type="bibr" rid="B12">Jie Yuan et al., 2021</xref>; <xref ref-type="bibr" rid="B4">Chi et al., 2021</xref>), TiC (<xref ref-type="bibr" rid="B31">Zhang et al., 2020</xref>; <xref ref-type="bibr" rid="B20">Peter et al., 2020</xref>), SiC (<xref ref-type="bibr" rid="B16">Ma et al., 2020</xref>; <xref ref-type="bibr" rid="B18">Mao et al., 2022</xref>), AlN (<xref ref-type="bibr" rid="B29">Yilong Yang et al., 2019</xref>), and carbon nanotubes (<xref ref-type="bibr" rid="B9">Guo et al., 2017</xref>). The composite materials can be prepared by different methods, including casting (<xref ref-type="bibr" rid="B29">Yilong Yang et al., 2019</xref>), <italic>in situ</italic> synthesis (<xref ref-type="bibr" rid="B4">Chi et al., 2021</xref>), power metallurgy (<xref ref-type="bibr" rid="B19">Nayak and Date, 2021</xref>), and additive manufacturing (<xref ref-type="bibr" rid="B24">Shangqin Yuan et al., 2021</xref>).</p>
<p>Casting is the most popular of the above preparation method due to its economy and variability. Ultrasonic melt treatment (UST) is thought to be a particularly effective method (<xref ref-type="bibr" rid="B6">Emadi et al., 2021</xref>; <xref ref-type="bibr" rid="B23">Rao, 2021</xref>). It is challenging to produce a homogeneous nanoparticle distribution in the melt due to the poor wettability and large surface volume ratio of nanoparticles. Nanoparticles tend to agglomerate during the fabrication process. The acoustic cavitation produced by ultrasonication can effectively promote the fragmentation of dendrites and increase the wettability between the nanoparticles and melts. Moreover, the instantaneous high pressure created by collapsing cavitation bubbles is also conducive to the dispersion of agglomerated nanoparticles. Thus, more nanoparticles act as heterogeneous nucleation cores, which significantly promote the grain refinement effect (<xref ref-type="bibr" rid="B12">Jie Yuan et al., 2021</xref>; <xref ref-type="bibr" rid="B3">Balasubramani et al., 2021</xref>).</p>
<p>However, the major studies about the ultrasonication were based on experiments. <xref ref-type="bibr" rid="B7">Eskin and Eskin (2003)</xref> revealed that the size and distribution of ceramic particles in Al-Si alloy matrix composites were significantly improved under the ultrasonic cavitation effect. However, the nanoparticle distribution in the melt simulated by numerical models was limited. <xref ref-type="bibr" rid="B2">Ayyar et al. (2008)</xref> explored the effect of particle spatial distribution and strength on the tensile behavior of particle-reinforced composites by numerical simulation method. <xref ref-type="bibr" rid="B26">Shashi (2020)</xref> also applied numerical simulation to analyze the debonding behavior of fiber reinforced metal matrix composites. <xref ref-type="bibr" rid="B30">Zhang and Nastac (2014)</xref> studied the effect of the model parameters, including nanoparticle size, ultrasonic probe position, fluid flow, and initial location where nanoparticles were released into the melt. However, these studies only performed the simulation analysis. No verification experiment was carried out to support the simulation results. Few scholars have combined numerical simulation analysis with experimental data to investigate the nanoparticle distribution in melts based on the aforesaid analysis. Therefore, it is a challenge to simulate the distribution of TiC nanoparticles in 2219 alloy melt and verify the simulation results with experimental results.</p>
<p>In this study, Fluent 17.0 software (<xref ref-type="bibr" rid="B8">Fluent, 2018</xref>) was used to simulate the distribution of TiC nanoparticle distribution. The Dense Discrete phase Model (DDPM) (<xref ref-type="bibr" rid="B11">Jain et al., 2017</xref>; <xref ref-type="bibr" rid="B1">Adnan et al., 2021</xref>) was modified. The turbulent flow, variable interaction between nanoparticles and melts were taken into account in this multiphase flow model. The purpose of this paper was to simulate the distribution of TiC nanoparticles in 2219 aluminum melt and analyze the effect of ultrasonic power on the TiC nanoparticle distribution. Subsequently, casting experiments were carried out by performing ultrasonic cavitation treatment of 2219 Al composites reinforced by 0.9&#xa0;wt% TiC nanoparticles to compare the numerical simulation results.</p>
</sec>
<sec id="s2">
<title>Simulation of TIC Nanoparticle Distribution in 2219 AL Melts</title>
<sec id="s2-1">
<title>Model Description</title>
<p>
<xref ref-type="fig" rid="F1">Figure 1</xref> shows the two-dimensional mesh model. The diameter of the ultrasonic probe was 39&#xa0;mm, and it was inserted 15&#xa0;mm below the melt surface. The liquid aluminum was 2219 Al alloy with a density of the melt was 2.69&#xa0;g/cm<sup>3</sup> and viscosity of 1.0 &#xd7; 10<sup>&#x2013;3</sup>&#xa0;kg/(ms) when the temperature ranging from 750&#xb0;C to 800&#xb0;C (<xref ref-type="bibr" rid="B28">Yang et al., 2017</xref>; <xref ref-type="bibr" rid="B21">Plevachuk et al., 2008</xref>). The inert TiC nanoparticles have an average diameter of 60&#xa0;nm and density of 4.5&#xa0;g/cm<sup>3</sup> (<xref ref-type="bibr" rid="B10">Hong Yang et al., 2019</xref>). For the convenience of observation, it was assumed that 0.9&#xa0;wt% TiC nanoparticles were injected 20&#xa0;mm above the bottom of the molten pool, and the injection was completed within 1&#xa0;s. ICEM software was used to partition the grid of this two-dimensional model for easy calculation. The model grid was divided into quadrilateral elements. To lessen the computation burden, the calculation model was scaled in proportion to the actual experimental equipment. The actual experimental crucible was 297&#xa0;mm in height and 207&#xa0;mm in width. The geometric parameters of the model are provided in <xref ref-type="fig" rid="F1">Figure 1</xref> and <xref ref-type="table" rid="T1">Table 1</xref>.</p>
<fig id="F1" position="float">
<label>FIGURE 1</label>
<caption>
<p>2D mesh model of the ultrasonic treatment process.</p>
</caption>
<graphic xlink:href="fmats-09-862601-g001.tif"/>
</fig>
<table-wrap id="T1" position="float">
<label>TABLE 1</label>
<caption>
<p>Calculation model and boundary setting.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="left">Boundary</th>
<th align="center">Length/mm</th>
<th align="center">Boundary Conditions</th>
<th align="center">Boundary Type</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="left">ab</td>
<td align="center">15</td>
<td align="center">out</td>
<td align="left">Pressure-outlet</td>
</tr>
<tr>
<td align="left">bc</td>
<td align="center">15</td>
<td align="center">Wall 1</td>
<td align="left">wall</td>
</tr>
<tr>
<td align="left">cd</td>
<td align="center">39</td>
<td align="center">inlet</td>
<td align="left">Pressure-inlet</td>
</tr>
<tr>
<td align="left">de</td>
<td align="center">15</td>
<td align="center">Wall 2</td>
<td align="left">wall</td>
</tr>
<tr>
<td align="left">ef</td>
<td align="center">15</td>
<td align="center">out</td>
<td align="left">Pressure-outlet</td>
</tr>
<tr>
<td align="left">fg</td>
<td align="center">99</td>
<td align="center">Wall 3</td>
<td align="left">wall</td>
</tr>
<tr>
<td align="left">gh</td>
<td align="center">69</td>
<td align="center">Wall 4</td>
<td align="left">wall</td>
</tr>
<tr>
<td align="left">ha</td>
<td align="center">99</td>
<td align="center">Wall 5</td>
<td align="left">wall</td>
</tr>
</tbody>
</table>
</table-wrap>
</sec>
<sec id="s2-2">
<title>Establishment of Mathematical Models</title>
<p>For easy calculation, some hypotheses were proposed. Firstly, the heat convection was ignored, and the preparation device was adiabatic. Secondly, the aluminum alloy melt was an incompressible melt; and finally, the density of the aluminum melt and TiC nanoparticles remained constant. Two-phase flow mixing model, DDPM, and <italic>k-&#x3c9;</italic> turbulence model (<xref ref-type="bibr" rid="B8">Fluent, 2018</xref>) were applied to investigate the nanoparticle distribution in the melt under ultrasonic treatment. Each phase was treated by Eulerian. Additionally, the nanoparticles were regarded as the particle phases in the Eulerian DDPM multiphase model. It was assumed that the wave propagation was linear and the shear stress was ignored. The acoustic pressure can be calculated by the wave equation (<xref ref-type="bibr" rid="B25">Shao et al., 2011</xref>):<disp-formula id="e1">
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<mml:mo>&#x2b;</mml:mo>
<mml:msub>
<mml:mi>a</mml:mi>
<mml:mtext>q</mml:mtext>
</mml:msub>
<mml:msub>
<mml:mi>&#x3c1;</mml:mi>
<mml:mtext>q</mml:mtext>
</mml:msub>
<mml:mi>g</mml:mi>
<mml:mo>&#x2b;</mml:mo>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mrow>
<mml:mi>D</mml:mi>
<mml:mi>P</mml:mi>
<mml:mi>M</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mrow>
<mml:mi>o</mml:mi>
<mml:mi>t</mml:mi>
<mml:mi>h</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
<label>(3)</label>
</disp-formula>
</p>
<p>Here, <inline-formula id="inf2">
<mml:math id="m5">
<mml:mrow>
<mml:msub>
<mml:mi>a</mml:mi>
<mml:mtext>q</mml:mtext>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the volume fraction of the phase, <inline-formula id="inf3">
<mml:math id="m6">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3c1;</mml:mi>
<mml:mtext>q</mml:mtext>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the density of the phase, <inline-formula id="inf4">
<mml:math id="m7">
<mml:mrow>
<mml:msub>
<mml:mtext>u</mml:mtext>
<mml:mtext>q</mml:mtext>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the velocity, <inline-formula id="inf5">
<mml:math id="m8">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3bc;</mml:mi>
<mml:mtext>q</mml:mtext>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the molecular viscosity, and <inline-formula id="inf6">
<mml:math id="m9">
<mml:mtext>P</mml:mtext>
</mml:math>
</inline-formula> is the pressure shared by all phases. <inline-formula id="inf7">
<mml:math id="m10">
<mml:mrow>
<mml:msub>
<mml:mrow>
<mml:mover accent="true">
<mml:mi>m</mml:mi>
<mml:mo>.</mml:mo>
</mml:mover>
</mml:mrow>
<mml:mrow>
<mml:mtext>pq</mml:mtext>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> represents the mass transfer from the <inline-formula id="inf8">
<mml:math id="m11">
<mml:mrow>
<mml:mtext>pth</mml:mtext>
</mml:mrow>
</mml:math>
</inline-formula> phase to the <inline-formula id="inf9">
<mml:math id="m12">
<mml:mrow>
<mml:mtext>qth</mml:mtext>
</mml:mrow>
</mml:math>
</inline-formula> phase. <inline-formula id="inf10">
<mml:math id="m13">
<mml:mrow>
<mml:msub>
<mml:mrow>
<mml:mover accent="true">
<mml:mi>m</mml:mi>
<mml:mo>.</mml:mo>
</mml:mover>
</mml:mrow>
<mml:mrow>
<mml:mtext>qp</mml:mtext>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> represents the mass transfer from the <inline-formula id="inf11">
<mml:math id="m14">
<mml:mrow>
<mml:mtext>qth</mml:mtext>
</mml:mrow>
</mml:math>
</inline-formula> phase to the <inline-formula id="inf12">
<mml:math id="m15">
<mml:mrow>
<mml:mtext>pth</mml:mtext>
</mml:mrow>
</mml:math>
</inline-formula> phase. <inline-formula id="inf13">
<mml:math id="m16">
<mml:mrow>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mrow>
<mml:mi>D</mml:mi>
<mml:mi>P</mml:mi>
<mml:mi>M</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the momentum exchange term, which is only considered in the initial phase equation. <inline-formula id="inf14">
<mml:math id="m17">
<mml:mrow>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mrow>
<mml:mi>o</mml:mi>
<mml:mi>t</mml:mi>
<mml:mi>h</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the source item, which includes the actual mass force, buoyancy, turbulence dispersion, etc. We can see that <xref ref-type="disp-formula" rid="e2">Eqs 2</xref>, <xref ref-type="disp-formula" rid="e3">3</xref> cannot solve the velocity field and volume fraction of the discrete phase. Their values are got from the Lagrangian tracking equation. The particle tracking model can be described below.</p>
<p>The trajectory of discrete phase particles was predicted by integrating the equilibrium force of discrete phase particles in the melt. It can be calculated as follows:<disp-formula id="e4">
<mml:math id="m18">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:msub>
<mml:mrow>
<mml:mtext>du</mml:mtext>
</mml:mrow>
<mml:mtext>p</mml:mtext>
</mml:msub>
</mml:mrow>
<mml:mrow>
<mml:mtext>dt</mml:mtext>
</mml:mrow>
</mml:mfrac>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mi>F</mml:mi>
<mml:mi>D</mml:mi>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:msub>
<mml:mi>F</mml:mi>
<mml:mi>G</mml:mi>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:msub>
<mml:mi>F</mml:mi>
<mml:mi>B</mml:mi>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:msub>
<mml:mi>F</mml:mi>
<mml:mrow>
<mml:mi>v</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>r</mml:mi>
<mml:mi>t</mml:mi>
<mml:mi>u</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>l</mml:mi>
<mml:mo>-</mml:mo>
<mml:mi>m</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>s</mml:mi>
<mml:mi>s</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:msub>
<mml:mi>F</mml:mi>
<mml:mrow>
<mml:mi>p</mml:mi>
<mml:mi>r</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>s</mml:mi>
<mml:mi>s</mml:mi>
<mml:mi>u</mml:mi>
<mml:mi>r</mml:mi>
<mml:mi>e</mml:mi>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>g</mml:mi>
<mml:mi>r</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>d</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>n</mml:mi>
<mml:mi>t</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:msub>
<mml:mi>F</mml:mi>
<mml:mrow>
<mml:mi>l</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>f</mml:mi>
<mml:mi>t</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:msub>
<mml:mi>F</mml:mi>
<mml:mrow>
<mml:mi>i</mml:mi>
<mml:mi>n</mml:mi>
<mml:mi>t</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>r</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>c</mml:mi>
<mml:mi>t</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>o</mml:mi>
<mml:mi>n</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
<label>(4)</label>
</disp-formula>where <inline-formula id="inf15">
<mml:math id="m19">
<mml:mrow>
<mml:msub>
<mml:mtext>u</mml:mtext>
<mml:mtext>p</mml:mtext>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the velocity in the melt, <inline-formula id="inf16">
<mml:math id="m20">
<mml:mrow>
<mml:msub>
<mml:mi>F</mml:mi>
<mml:mi>D</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the drag force, <inline-formula id="inf17">
<mml:math id="m21">
<mml:mrow>
<mml:msub>
<mml:mi>F</mml:mi>
<mml:mi>G</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the gravitational force, <inline-formula id="inf18">
<mml:math id="m22">
<mml:mrow>
<mml:msub>
<mml:mi>F</mml:mi>
<mml:mi>B</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the buoyancy force, <inline-formula id="inf19">
<mml:math id="m23">
<mml:mrow>
<mml:msub>
<mml:mi>F</mml:mi>
<mml:mrow>
<mml:mi>v</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>r</mml:mi>
<mml:mi>t</mml:mi>
<mml:mi>u</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>l</mml:mi>
<mml:mo>-</mml:mo>
<mml:mi>m</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>s</mml:mi>
<mml:mi>s</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the virtual mass force, <inline-formula id="inf20">
<mml:math id="m24">
<mml:mrow>
<mml:msub>
<mml:mi>F</mml:mi>
<mml:mrow>
<mml:mi>p</mml:mi>
<mml:mi>r</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>s</mml:mi>
<mml:mi>s</mml:mi>
<mml:mi>u</mml:mi>
<mml:mi>r</mml:mi>
<mml:mi>e</mml:mi>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>g</mml:mi>
<mml:mi>r</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>d</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>n</mml:mi>
<mml:mi>t</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the additional force produced by the pressure gradient, <inline-formula id="inf21">
<mml:math id="m25">
<mml:mrow>
<mml:msub>
<mml:mi>F</mml:mi>
<mml:mrow>
<mml:mi>l</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>f</mml:mi>
<mml:mi>t</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the Saffman&#x2019;s lift force produced by the local velocity gradients across the particle, and <inline-formula id="inf22">
<mml:math id="m26">
<mml:mrow>
<mml:msub>
<mml:mi>F</mml:mi>
<mml:mrow>
<mml:mi>i</mml:mi>
<mml:mi>n</mml:mi>
<mml:mi>t</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>r</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>c</mml:mi>
<mml:mi>t</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>o</mml:mi>
<mml:mi>n</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the additional acceleration caused by the interaction between particles. The above variables were obtained by the following equations:<disp-formula id="e5">
<mml:math id="m27">
<mml:mrow>
<mml:msub>
<mml:mtext>F</mml:mtext>
<mml:mtext>D</mml:mtext>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mn>18</mml:mn>
<mml:mi>&#x3bc;</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:msub>
<mml:mi>&#x3c1;</mml:mi>
<mml:mtext>p</mml:mtext>
</mml:msub>
<mml:msubsup>
<mml:mi>d</mml:mi>
<mml:mtext>p</mml:mtext>
<mml:mn>2</mml:mn>
</mml:msubsup>
</mml:mrow>
</mml:mfrac>
<mml:mfrac>
<mml:mrow>
<mml:msub>
<mml:mtext>C</mml:mtext>
<mml:mtext>D</mml:mtext>
</mml:msub>
<mml:mi>Re</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mn>24</mml:mn>
</mml:mrow>
</mml:mfrac>
<mml:mrow>
<mml:mo>(</mml:mo>
<mml:mrow>
<mml:mtext>u</mml:mtext>
<mml:mo>&#x2212;</mml:mo>
<mml:msub>
<mml:mtext>u</mml:mtext>
<mml:mtext>p</mml:mtext>
</mml:msub>
</mml:mrow>
<mml:mo>)</mml:mo>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(5)</label>
</disp-formula>where <inline-formula id="inf23">
<mml:math id="m28">
<mml:mtext>u</mml:mtext>
</mml:math>
</inline-formula> is the fluid velocity, <inline-formula id="inf24">
<mml:math id="m29">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3c1;</mml:mi>
<mml:mtext>p</mml:mtext>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the density of the particle, <inline-formula id="inf25">
<mml:math id="m30">
<mml:mrow>
<mml:msub>
<mml:mtext>d</mml:mtext>
<mml:mtext>p</mml:mtext>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the particle diameter, <inline-formula id="inf26">
<mml:math id="m31">
<mml:mrow>
<mml:mi>Re</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is the relative Reynolds number, which is defined as <inline-formula id="inf27">
<mml:math id="m32">
<mml:mrow>
<mml:mi>Re</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mi>&#x3c1;</mml:mi>
<mml:msub>
<mml:mtext>d</mml:mtext>
<mml:mtext>p</mml:mtext>
</mml:msub>
<mml:mrow>
<mml:mo>&#x7c;</mml:mo>
<mml:mrow>
<mml:mtext>u</mml:mtext>
<mml:mo>-</mml:mo>
<mml:mrow>
<mml:mrow>
<mml:msub>
<mml:mtext>u</mml:mtext>
<mml:mtext>p</mml:mtext>
</mml:msub>
</mml:mrow>
<mml:mo>&#x7c;</mml:mo>
</mml:mrow>
</mml:mrow>
</mml:mrow>
</mml:mrow>
<mml:mi>&#x3bc;</mml:mi>
</mml:mfrac>
</mml:mrow>
</mml:math>
</inline-formula>, <inline-formula id="inf28">
<mml:math id="m33">
<mml:mi>&#x3c1;</mml:mi>
</mml:math>
</inline-formula> is the density of the melt, and <inline-formula id="inf29">
<mml:math id="m34">
<mml:mrow>
<mml:msub>
<mml:mtext>C</mml:mtext>
<mml:mtext>D</mml:mtext>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the drag coefficient, which is defined as <inline-formula id="inf30">
<mml:math id="m35">
<mml:mrow>
<mml:msub>
<mml:mtext>C</mml:mtext>
<mml:mtext>D</mml:mtext>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mn>24</mml:mn>
</mml:mrow>
<mml:mrow>
<mml:mi>Re</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mrow>
<mml:mo>(</mml:mo>
<mml:mrow>
<mml:mn>1</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>0.15</mml:mn>
<mml:msup>
<mml:mrow>
<mml:mi>Re</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mn>0.687</mml:mn>
</mml:mrow>
</mml:msup>
</mml:mrow>
<mml:mo>)</mml:mo>
</mml:mrow>
</mml:mrow>
</mml:math>
</inline-formula>.<disp-formula id="e6">
<mml:math id="m36">
<mml:mrow>
<mml:msub>
<mml:mi>F</mml:mi>
<mml:mi>G</mml:mi>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:msub>
<mml:mi>F</mml:mi>
<mml:mi>B</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mi>g</mml:mi>
<mml:mrow>
<mml:mo>(</mml:mo>
<mml:mrow>
<mml:msub>
<mml:mi>&#x3c1;</mml:mi>
<mml:mtext>p</mml:mtext>
</mml:msub>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>&#x3c1;</mml:mi>
</mml:mrow>
<mml:mo>)</mml:mo>
</mml:mrow>
</mml:mrow>
<mml:mrow>
<mml:msub>
<mml:mi>&#x3c1;</mml:mi>
<mml:mtext>p</mml:mtext>
</mml:msub>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:math>
<label>(6)</label>
</disp-formula>
<disp-formula id="e7">
<mml:math id="m37">
<mml:mrow>
<mml:msub>
<mml:mi>F</mml:mi>
<mml:mrow>
<mml:mi>v</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>r</mml:mi>
<mml:mi>t</mml:mi>
<mml:mi>u</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>l</mml:mi>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>m</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>s</mml:mi>
<mml:mi>s</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mn>1</mml:mn>
<mml:mn>2</mml:mn>
</mml:mfrac>
<mml:mfrac>
<mml:mi>&#x3c1;</mml:mi>
<mml:mrow>
<mml:msub>
<mml:mi>&#x3c1;</mml:mi>
<mml:mtext>p</mml:mtext>
</mml:msub>
</mml:mrow>
</mml:mfrac>
<mml:mfrac>
<mml:mtext>d</mml:mtext>
<mml:mrow>
<mml:mtext>dt</mml:mtext>
</mml:mrow>
</mml:mfrac>
<mml:mrow>
<mml:mo>(</mml:mo>
<mml:mrow>
<mml:msub>
<mml:mrow>
<mml:mtext>u</mml:mtext>
<mml:mo>-</mml:mo>
<mml:mtext>u</mml:mtext>
</mml:mrow>
<mml:mtext>p</mml:mtext>
</mml:msub>
</mml:mrow>
<mml:mo>)</mml:mo>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(7)</label>
</disp-formula>
<disp-formula id="e8">
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</mml:math>
<label>(9)</label>
</disp-formula>where <inline-formula id="inf31">
<mml:math id="m40">
<mml:mrow>
<mml:mtext>K</mml:mtext>
<mml:mo>&#x3d;</mml:mo>
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</inline-formula> is the deformation tensor.<disp-formula id="e10">
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<mml:mo stretchy="true">&#xaf;</mml:mo>
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<label>(10)</label>
</disp-formula>where <inline-formula id="inf33">
<mml:math id="m43">
<mml:mrow>
<mml:mover accent="true">
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</mml:math>
</inline-formula> is the stress strain tensor of the particle.</p>
<p>The discrete random walk model is a random tracking model that considers the influence of turbulence on the particle trajectory:<disp-formula id="e11">
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</mml:mfrac>
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</mml:msqrt>
</mml:mrow>
</mml:math>
<label>(11)</label>
</disp-formula>where <inline-formula id="inf34">
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</mml:mover>
</mml:mrow>
</mml:math>
</inline-formula> is the average value of fluid velocity in particle trajectory <xref ref-type="disp-formula" rid="e4">Equation 4</xref>, <inline-formula id="inf35">
<mml:math id="m46">
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</inline-formula> is the number of random normal distributions and <inline-formula id="inf36">
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<mml:mi>k</mml:mi>
</mml:math>
</inline-formula> is the turbulent kinetic energy located locally.</p>
</sec>
<sec id="s2-3">
<title>Boundary Conditions and Solution Procedure</title>
<p>The end face of the ultrasonic probe was defined as the velocity inlet, which was described in the User Defined Function (UDF). Line cd represented the end face of the ultrasonic probe. Line ab, and ef represented the interface between the external shielding gas and aluminum alloy melt. The remaining lines were defined as walls (<xref ref-type="fig" rid="F1">Figure 1</xref>). All discrete phase BC types were set as reflect. The concrete values and boundary condition names of each part in <xref ref-type="fig" rid="F1">Figure 1</xref> were listed in <xref ref-type="table" rid="T1">Table 1</xref>.</p>
<p>According to the Rosin-Rammler equation, TiC nanoparticles were between 40 nm and 70&#xa0;nm in size. After solving the fluid velocity, the position of nanoparticles was calculated at each step. Unidirectional coupling was used due to the lower discrete phase volume fraction. In this situation, the influence of the discrete phase on fluid turbulence may be neglected, which is convenient for calculation.</p>
</sec>
</sec>
<sec sec-type="results|discussion" id="s3">
<title>Simulation Results and Discussion</title>
<p>
<xref ref-type="fig" rid="F2">Figure 2</xref> shows the flow direction of the fluid and the nanoparticle distribution under ultrasonic treatment. The ultrasonic power was 350&#xa0;W, and the ultrasonic vibration frequency was 19&#xa0;kHz. <xref ref-type="fig" rid="F2">Figure 2</xref> shows that the fluid flow in the center position of the melt is very strong, so at the beginning, most nanoparticles were scattered to the edge under the influence of intense convection. As 0.9&#xa0;wt% nanoparticles were injected into the molten alloy within 1 s, the nanoparticles dispersed from the center to the edge and afterwards from the bottom to the upper part under the influence of ultrasonication. However, a relatively larger number of particles existed in the edge than that in the center. It means that the uniformity of particle distribution was independent of ultrasonic power. While, the ultrasonic power was directly proportional to the fluid flow intensity. It was driven by acoustic streaming, and then promoted the motion of nanoparticles. These phenomena can be explained by in <xref ref-type="fig" rid="F2">Figure 2</xref>.</p>
<fig id="F2" position="float">
<label>FIGURE 2</label>
<caption>
<p>Fluid flow <bold>(A)</bold> and effect of ultrasonic vibration time on nanoparticle distribution: <bold>(B)</bold> 1 s, <bold>(C)</bold> 1.1 s, <bold>(D)</bold> 1.2 s, <bold>(E)</bold> 1.3 s, and <bold>(F)</bold> 3&#xa0;s.</p>
</caption>
<graphic xlink:href="fmats-09-862601-g002.tif"/>
</fig>
<p>Two kinds of ultrasonic powers (250 W and 350&#xa0;W) were applied to investigate the effect on the distribution of TiC particles, as shown in <xref ref-type="fig" rid="F3">Figure 3</xref>. The ultrasonic application time was 20&#xa0;s. And the acoustic streaming near the ultrasonic end face was stronger than that away from the ultrasonic end face. Attributed to the large viscosity of aluminum melt, the energy of acoustic streaming was dissipated during the propagation process. Fewer particles dispersed in the area where the acoustic pressure is strong, whereas more particles distributed in where the acoustic pressure was weak, as shown in <xref ref-type="fig" rid="F3">Figure 3B</xref>. More particles were found in the lower center of the molten pool than that in the upper position. Compared with the result shown in <xref ref-type="fig" rid="F3">Figure 3A</xref>, the strength of acoustic flow in the upper and lower regions of the center was decreased when the ultrasonic power was reduced to 250&#xa0;W, as illustrated in <xref ref-type="fig" rid="F3">Figure 3C</xref>. Here we need to emphasize that the particles in <xref ref-type="fig" rid="F3">Figure 3</xref> were not distributed individually, but agglomerated together. On the other hand, attributed to the strong convection effect in the center of the ingot, TiC particles were obviously depolymerized during casting process. While more agglomerated TiC particles were dispersed in the bottom of the ingot, especially near the edge positions. Therefore, higher power may be detrimental to the particle distribution. Regardless of the ultrasonic power, the nanoparticles in the center were always less than those in the edge. Compared with <xref ref-type="fig" rid="F2">Figure 2</xref> and <xref ref-type="fig" rid="F3">Figure 3</xref> we can see that, in the initial stage of the particle introduced into the melt, all particles were agglomerated. Thus, the depolymerization speed of initial particles changed from slow to fast with the gradual dispersion of particles. When it tended to be stable in <xref ref-type="fig" rid="F3">Figure 3</xref>, the velocity was fast under the influence of strong convection. Experimental verification was conducted to verify the phenomena and conclusions of the simulation calculation in <xref ref-type="sec" rid="s4">
<italic>section 4</italic>
</xref>
<italic>.</italic>
</p>
<fig id="F3" position="float">
<label>FIGURE 3</label>
<caption>
<p>Effect of different ultrasonic powers on particle distribution: <bold>(A,B)</bold>: 350&#xa0;W and <bold>(C,D)</bold>: 250&#xa0;W.</p>
</caption>
<graphic xlink:href="fmats-09-862601-g003.tif"/>
</fig>
</sec>
<sec id="s4">
<title>Experimental Validation</title>
<p>TiC/2219 nanocomposites reinforced by 0.9&#xa0;wt% TiC nanoparticles were manufactured by the ultrasonic-assisted method for 20s. The effect of ultrasonic vibration on the microstructure of the nanocomposite was discussed. <xref ref-type="fig" rid="F4">Figure 4</xref> shows the prepared 0.9&#xa0;wt% TiC/2219 nanocomposite sample. Two pieces of round block with approximately 20&#xa0;mm in thickness were cut from the top and bottom of the samples. Four square blocks with a size of 20 &#xd7; 20 &#xd7; 20&#xa0;mm were selected from the center position and the edge position of the two round blocks, as shown in <xref ref-type="fig" rid="F4">Figure 4</xref>, to examine the microstructure of the nanocomposite. The square blocks located at the center were named as a and c, and the square blocks located at the edge were named as b and d, respectively. The grain size of the nanocomposite was analyzed by optical microscopy (OM; DSX50240, OLYMPUS). The samples for OM were mechanically ground, polished, and etched using Keller solution. What&#x2019;s more, the distribution of TiC nanoparticles was observed by scanning electron microscopy (SEM; JSM-7600F, JEOL). The clear TiC nanoparticle morphology in the matrix was observed by transmission electron microscopy (TEM; JEM2100, JEOL). These samples with an initial thickness of 0.5&#xa0;mm were grinded to 80&#x2013;100&#xa0;&#xb5;m thickness. Then, the slices were punched into 3&#xa0;mm diameter disks and thinned by an ion beam. X-ray diffraction (Rigaku 600) was used to identify the phase components of the TiC/2219Al nanocomposites. It was operated at a scanning rate of 0.02&#xb0;/s at 40&#xa0;kV with Cu<sub>
<italic>K&#x3b1;</italic>
</sub> radiation (wavelength &#x3bb;<sub>
<italic>K&#x3b1;</italic>
</sub> &#x3d; 1.54056&#xa0;&#xc5;).</p>
<fig id="F4" position="float">
<label>FIGURE 4</label>
<caption>
<p>Schematic illustration of sampling positions.</p>
</caption>
<graphic xlink:href="fmats-09-862601-g004.tif"/>
</fig>
<p>
<xref ref-type="fig" rid="F5">Figure 5</xref> shows the optical microscopy images of the square blocks located in <xref ref-type="fig" rid="F4">Figure 4</xref>. The grain morphologies of block a and block c were fine equiaxed crystals, and the average grain sizes were 91 &#x3bc;m and 105&#xa0;&#x3bc;m, respectively. However, most grains from block b and block d were dendritic crystals, with an average grain size of 96 &#x3bc;m and 113&#xa0;&#x3bc;m, respectively (<xref ref-type="fig" rid="F6">Figure 6</xref>). It is obvious that, the grain size of the upper part was smaller than that of the lower part. On one hand, the acoustic streaming near the end face of ultrasonic pressure was the strongest. Acoustic streaming could break larger dendrites into smaller equiaxed crystals (<xref ref-type="bibr" rid="B19">Liu et al., 2019</xref>; <xref ref-type="bibr" rid="B22">Priyadarshi et al., 2021</xref>). On the other hand, majority of TiC particles gathered in the edge position, resulting in more agglomerated clusters. It can also be seen from the simulation results shown in <xref ref-type="fig" rid="F3">Figure 3</xref>. Attributed to the uniformly dispersed nanoparticles more heterogeneous nucleation sites were generated, promoting the nucleation rates during solidification process. Therefore, the grain size was smaller. However, most of the nanoparticles gathered at the edge, which were harmful to the heterogeneous nucleation (<xref ref-type="bibr" rid="B10">Hong Yang et al., 2019</xref>). In summary, the reason for the grain refinement in the center was the interaction of acoustic streaming and particles which acted as heterogeneous nucleation sites.</p>
<fig id="F5" position="float">
<label>FIGURE 5</label>
<caption>
<p>Optical microscopy images of the TiC/2219 nanocomposite at the <bold>(A)</bold> upper center, <bold>(B)</bold> upper edge, <bold>(C)</bold> lower center, and <bold>(D)</bold> lower edge positions.</p>
</caption>
<graphic xlink:href="fmats-09-862601-g005.tif"/>
</fig>
<fig id="F6" position="float">
<label>FIGURE 6</label>
<caption>
<p>The grain sizes of block a, block b, block c, and block d.</p>
</caption>
<graphic xlink:href="fmats-09-862601-g006.tif"/>
</fig>
<p>
<xref ref-type="fig" rid="F7">Figure 7</xref> shows the SEM micrographs of the blocks cut from the sample. <xref ref-type="fig" rid="F7">Figures 7A,B</xref> show the SEM images of the center and edge position of the upper part of the nanocomposite, and <xref ref-type="fig" rid="F7">Figures 7C,D</xref> show the SEM micrographs of the center and edge of the lower part of the nanocomposite, respectively. The number of TiC nanoparticles in the center position shown in <xref ref-type="fig" rid="F7">Figure 7</xref> less than that in the edge position both in the upper part and in the lower part of the nanocomposite, as well as the number of Al<sub>2</sub>Cu phases. Besides, discontinuous fine Al<sub>2</sub>Cu phases were generated in the center position. While they were continuous and coarse in the edge position. Thanks to the intensest acoustic streaming in the center position, more dendrites were broken to fragments. Besides, discontinuous phases were formed around the grain boundary. The acoustic streaming propagated from the center to the edge, accelerated the movement of TiC nanoparticles. As a result, fewer nanoparticles were found in the center position than those in the edge. The results of SEM micrographs were consistent with the data of the simulation in <xref ref-type="fig" rid="F3">Figure 3</xref>. The white dots in <xref ref-type="fig" rid="F7">Figure 7</xref> were nanoparticles. EDS was used to identify the compositions of the white dots, as shown in <xref ref-type="fig" rid="F7">Figure 7F</xref>. XRD was applied to accurately research the phases in composites. The results indicated that some Al<sub>2</sub>Cu phases and &#x3b1;-Al in the matrix were observed in the samples, as shown in <xref ref-type="fig" rid="F8">Figure 8</xref>. In addition, it also contained more TiC nanoparticles and a minor amount of TiO<sub>2</sub>. It was difficult for XRD to detect nanoscale phases, the peaks of TiC shown in the figure may be the agglomerated TiC nanoparticles. The oxidation of TiC may result in the creation of TiO<sub>2</sub> (<xref ref-type="bibr" rid="B29">Yilong Yang et al., 2019</xref>). As a consequence of merging SEM&#x2013;EDS and XRD results, it was determined that the white spots in <xref ref-type="fig" rid="F7">Figure 7</xref> were TiC nanoparticles.</p>
<fig id="F7" position="float">
<label>FIGURE 7</label>
<caption>
<p>SEM micrographs of the TiC/2219 nanocomposite at the <bold>(A)</bold> upper center, <bold>(B)</bold> upper edge, <bold>(C)</bold> lower center, and <bold>(D)</bold> lower edge positions. <bold>(E, F)</bold> EDS results identifying the chemical compositions of Al<sub>2</sub>Cu phases and TiC nanoparticles.</p>
</caption>
<graphic xlink:href="fmats-09-862601-g007.tif"/>
</fig>
<fig id="F8" position="float">
<label>FIGURE 8</label>
<caption>
<p>XRD patterns of the TiC/2219 nanocomposite samples extracted from the center position.</p>
</caption>
<graphic xlink:href="fmats-09-862601-g008.tif"/>
</fig>
<p>The clear morphology of TiC nanoparticles in the matrix was observed by TEM. <xref ref-type="fig" rid="F9">Figure 9</xref> shows the detailed microstructures at the nanoscale. The TiC nanoparticles and their clusters were observed in the area where they were well embedded. The sample in <xref ref-type="fig" rid="F9">Figure 9A</xref> was selected from the edge position of the nanocomposite. <xref ref-type="fig" rid="F9">Figure 9A</xref> shows that TiC nanoparticles were scattered in the form of local agglomeration. The sample taken from the center position of the nanocomposite shows that several single TiC nanoparticles was dispersed in the matrix without excessive agglomeration. Attributed to the ultrasonic cavitation effect, cavitation bubbles were generated once the ultrasonication was applied to the molten aluminum alloy (<xref ref-type="bibr" rid="B28">Yang et al., 2017</xref>; <xref ref-type="bibr" rid="B21">Plevachuk et al., 2008</xref>), which were beneficial to the dispersion of nanoparticles. TEM-EDS was used to identify the nanoparticle composition. <xref ref-type="fig" rid="F9">Figure 9C</xref> was the magnified version of <xref ref-type="fig" rid="F9">Figure 9B</xref>. The interface between the TiC nanoparticles and the aluminum matrix was clearly visible, indicating that the TiC nanoparticles added to the aluminum matrix were firmly bound.</p>
<fig id="F9" position="float">
<label>FIGURE 9</label>
<caption>
<p>
<bold>(A)</bold> and <bold>(B)</bold> TEM images illustrating the TiC nanoparticle distribution within the a-Al matrix of TiC/2219 nanocomposites; <bold>(C)</bold> Enlarged area in b.</p>
</caption>
<graphic xlink:href="fmats-09-862601-g009.tif"/>
</fig>
</sec>
<sec sec-type="conclusion" id="s5">
<title>Conclusion</title>
<p>In this work, the process of ultrasonic treatment was simulated by numerical simulation of cavitation-based mixing and dispersion of 0.9&#xa0;wt% TiC nanoparticles in 2219 aluminum melt. The conclusions are as follows:<list list-type="simple">
<list-item>
<p>(1) The distribution of TiC nanoparticles in the aluminum melts (prepared by ultrasonic casting process) was investigated by the DDPM model coupled with the <italic>k-&#x3c9;</italic> turbulence model. Simulation results show that the nanoparticles were well distributed in the melt. However, due to the strongest acoustic streaming effect, minor of TiC nanoparticles distributed in the center position of the composite. And the edge section exhibited the opposite characteristics, for the majority of nanoparticles tended to agglomerate around the edge position.</p>
</list-item>
<list-item>
<p>(2) The effect of ultrasonic power on the dispersion of nanoparticles was theoretically explored. An optimum ultrasonic power was beneficial for the distribution of the TiC nanoparticles. Besides, the nanoparticles in the center position of the nanocomposite move to the edge position driven by the stronger acoustic streaming.</p>
</list-item>
<list-item>
<p>(3) A small number of nanoparticles uniformly distributed in the center position of the nanocomposite, but a great density of agglomerated nanoparticles were found at the edge. This was consistent well with the simulation results. It lays a solid foundation for further experimental analysis in the future (<xref ref-type="bibr" rid="B14">Liu et al., 2019</xref>; <xref ref-type="bibr" rid="B22">Priyadarshi et al., 2021</xref>; <xref ref-type="bibr" rid="B30">Zhang and Nastac, 2014</xref>).</p>
</list-item>
</list>
</p>
</sec>
</body>
<back>
<sec id="s6">
<title>Data Availability Statement</title>
<p>The raw data supporting the conclusions of this article will be made available by the authors, without undue reservation.</p>
</sec>
<sec id="s7">
<title>Author Contributions</title>
<p>YY-L Conceptualization, Simulation calculation, Wrighting-original draft preparation; ZY: Experiment, Wrighting&#x2014;original draft preparation, Foundation, Wrighting&#x2014;Revised draft. ZH-M and LX-H: Foundation, Wrighting&#x2014;Revised draft.</p>
</sec>
<sec id="s8">
<title>Funding</title>
<p>The authors are thankful for the financial support from the Science and Technology Innovation Program of Hunan Province (NO. 2020RC 2002); Natural Science Foundation of Hunan Province (NO. 2021JJ40774); Key Scientific Research Projects of Colleges and Universities in Henan Province (NO. 20A430007); Key Scientific and Technological Projects in Henan Province (NO. 212102210032) (NO. 222102230097), and Doctoral Foundation of Henan Institute of Engineering (NO. D2021008).</p>
</sec>
<sec sec-type="COI-statement" id="s9">
<title>Conflict of Interest</title>
<p>The authors declare that the research was conducted in the absence of any commercial or financial relationships that could be construed as a potential conflict of interest.</p>
</sec>
<sec sec-type="disclaimer" id="s10">
<title>Publisher&#x2019;s Note</title>
<p>All claims expressed in this article are solely those of the authors and do not necessarily represent those of their affiliated organizations, or those of the publisher, the editors, and the reviewers. Any product that may be evaluated in this article, or claim that may be made by its manufacturer, is not guaranteed or endorsed by the publisher.</p>
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