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<front>
<journal-meta>
<journal-id journal-id-type="pmc">FHMT</journal-id>
<journal-id journal-id-type="nlm-ta">FHMT</journal-id>
<journal-id journal-id-type="publisher-id">FHMT</journal-id>
<journal-title-group>
<journal-title>Frontiers in Heat and Mass Transfer</journal-title>
</journal-title-group>
<issn pub-type="epub">2151-8629</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">50814</article-id>
<article-id pub-id-type="doi">10.32604/fhmt.2024.050814</article-id>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Article</subject>
</subj-group>
</article-categories>
<title-group>
<article-title>Finite Element Analysis for Magneto-Convection Heat Transfer Performance in Vertical Wavy Surface Enclosure: Fin Size Impact</article-title>
<alt-title alt-title-type="left-running-head">Finite Element Analysis for Magneto-Convection Heat Transfer Performance in Vertical Wavy Surface Enclosure: Fin Size Impact</alt-title>
<alt-title alt-title-type="right-running-head">Finite Element Analysis for Magneto-Convection Heat Transfer Performance in Vertical Wavy Surface Enclosure: Fin Size Impact</alt-title>
</title-group>
<contrib-group>
<contrib id="author-1" contrib-type="author">
<name name-style="western"><surname>Fayz-Al-Asad</surname><given-names>Md.</given-names></name><xref ref-type="aff" rid="aff-1">1</xref><xref ref-type="aff" rid="aff-4">4</xref></contrib>
<contrib id="author-2" contrib-type="author" corresp="yes">
<name name-style="western"><surname>Mebarek-Oudina</surname><given-names>F.</given-names></name><xref ref-type="aff" rid="aff-2">2</xref><email>oudina2003@yahoo.fr</email></contrib>
<contrib id="author-3" contrib-type="author">
<name name-style="western"><surname>Vaidya</surname><given-names>H.</given-names></name><xref ref-type="aff" rid="aff-3">3</xref></contrib>
<contrib id="author-4" contrib-type="author">
<name name-style="western"><surname>Hasan</surname><given-names>Md. Shamim</given-names></name><xref ref-type="aff" rid="aff-4">4</xref></contrib>
<contrib id="author-5" contrib-type="author">
<name name-style="western"><surname>Sarker</surname><given-names>Md. Manirul Alam</given-names></name><xref ref-type="aff" rid="aff-4">4</xref></contrib>
<contrib id="author-6" contrib-type="author">
<name name-style="western"><surname>Ismail</surname><given-names>A. I.</given-names></name><xref ref-type="aff" rid="aff-5">5</xref></contrib>
<aff id="aff-1"><label>1</label><institution>Department of Mathematics, American International University&#x2013;Bangladesh, Kuratoli</institution>, <addr-line>Khilkhet, Dhaka, 1229</addr-line>, <country>Bangladesh</country></aff>
<aff id="aff-2"><label>2</label><institution>Department of Physics, Faculty of Sciences, University of 20 Ao&#x00FB;t 1955-Skikda</institution>, <addr-line>Skikda, 21000</addr-line>, <country>Algeria</country></aff>
<aff id="aff-3"><label>3</label><institution>Department of Mathematics, Vijayanagara Sri Krishnadevaraya University, Vinayaka Nagar</institution>, <addr-line>Ballari, Karnataka, 583105</addr-line>, <country>India</country></aff>
<aff id="aff-4"><label>4</label><institution>Department of Mathematics, Bangladesh University of Engineering and Technology (BUET)</institution>, <addr-line>Dhaka, 1000</addr-line>, <country>Bangladesh</country></aff>
<aff id="aff-5"><label>5</label><institution>Mechanical Engineering Department, College of Engineering and Islamic Architecture, Umm Al-Qura University, P.O. Box 5555</institution>, <addr-line>Makkah</addr-line>, <country>Saudi Arabia</country></aff>
</contrib-group>
<author-notes>
<corresp id="cor1"><label>&#x002A;</label>Corresponding Author: F. Mebarek-Oudina. Email: <email>oudina2003@yahoo.fr</email></corresp>
</author-notes>
<pub-date date-type="collection" publication-format="electronic">
<year>2024</year></pub-date>
<pub-date date-type="pub" publication-format="electronic">
<day>11</day>
<month>7</month>
<year>2024</year></pub-date>
<volume>22</volume>
<issue>3</issue>
<fpage>817</fpage>
<lpage>837</lpage>
<history>
<date date-type="received">
<day>19</day>
<month>2</month>
<year>2024</year>
</date>
<date date-type="accepted">
<day>25</day>
<month>4</month>
<year>2024</year>
</date>
</history>
<permissions>
<copyright-statement>&#x00A9; 2024 Fayz-Al-Asad et al.</copyright-statement>
<copyright-year>2024</copyright-year>
<copyright-holder>Fayz-Al-Asad et al.</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_FHMT_50814.pdf"></self-uri>
<abstract>
<p>The goal of this paper is to represent a numerical study of magnetohydrodynamic mixed convection heat transfer in a lid-driven vertical wavy enclosure with a fin attached to the bottom wall. We use a finite element method based on Galerkin weighted residual (GWR) techniques to set up the appropriate governing equations for the present flow model. We have conducted a parametric investigation to examine the impact of Hartmann and Richardson numbers on the flow pattern and heat transmission features inside a wavy cavity. We graphically represent the numerical results, such as isotherms, streamlines, velocity profiles, local and mean Nusselt numbers, and average surface temperature. Comparisons between the results of this work and previously published work in a literature review have been produced to examine the reliability and consistency of the data. The different sizes of the fin surface significantly impact flow creation and temperature fields. Additionally, the long fin size is necessary to enhance the heat transfer rate on the right surface at large Richardson numbers and low Hartmann numbers. Fin surfaces can significantly increase the mixing of fluid inside the enclosure, which can mean reductions in reaction times and operating costs, along with increases in heat transfer and efficiency.</p>
</abstract>
<kwd-group kwd-group-type="author">
<kwd>Fin surface</kwd>
<kwd>finite element method</kwd>
<kwd>combined convection</kwd>
<kwd>MHD</kwd>
<kwd>wavy enclosure</kwd>
</kwd-group>
</article-meta>
</front>
<body>
<sec id="s1">
<label>1</label>
<title>Introduction</title>
<p>Researchers have become interested in convection heat transition in the driven enclosure due to its diverse range of applications, including solar thermal collectors, float glass manufacture, microelectronic devices, and electrical devices. A vast number of researchers have recognized the focus on lid-driven, various-shaped cavities, both from engineering and theoretical viewpoints. The present model&#x2019;s specific engineering applications may include computer CPU heat sinks, radiators in cars, heat exchangers in power plants, heat transmission devices, and so on. Das et al. [<xref ref-type="bibr" rid="ref-1">1</xref>] examined free convection flow within the wavy frame enclosure. Their findings showed that a wavy surface&#x2019;s amplitude and undulation numbers affect the components that control heat in an enclosure. The natural convection within a vertically wavy wall enclosing an unstable case was statistically modeled by Rostami [<xref ref-type="bibr" rid="ref-2">2</xref>]. Azizul et al. [<xref ref-type="bibr" rid="ref-3">3</xref>] reported the impact of a heat line concept on mixed convection indoors with a wavy surface frame and nanofluids. Free convection via a skewed design wavy porous chamber was examined by Misirlioglu et al. [<xref ref-type="bibr" rid="ref-4">4</xref>]. The impact of wavy base cover on combined convection heat augmentation in a driven chamber was documented by Al-Amiri et al. [<xref ref-type="bibr" rid="ref-5">5</xref>]. They assessed the effect of flow creation and heat removal characteristics on the number of wavy surfaces, the Richardson number, and the appropriateness of a wavy surface. Mushate [<xref ref-type="bibr" rid="ref-6">6</xref>] examined a porous enclosure with undulations using CFD to predict natural convection. The outcomes showed that the heat change rate improves as the Rayleigh number rises and decreases as the amplitude rises. Mansour et al. [<xref ref-type="bibr" rid="ref-7">7</xref>] used a heated non equilibrium model to explore a free convective porous cavity with a wavy form and the effect of thermic radiation. The coupled convection throw nanofluid flow within a wavy form cage was studied by Nada et al. [<xref ref-type="bibr" rid="ref-8">8</xref>]. They discovered that, with regard to geometry, base surface ratios, and the Richardson number, the heat replacement rate increases with an increase in the nanoparticle volume fraction. Using a nanofluid and Buongiorno&#x2019;s mathematical description, Sheremet et al. [<xref ref-type="bibr" rid="ref-9">9</xref>] scrutinized free convection within a curved porous cavity with sinusoidal heat delivery on both level surfaces. Free convective movement in a non-uniformly heated curvy edge porous enclosure with nanofluid reporting the impacts of thermophoresis and Brownian dispersion was explored by Sheremet et al. [<xref ref-type="bibr" rid="ref-10">10</xref>]. Natural convection inside porous wavy structures, having sinusoidal warming and interior heat generation, was studied by Cheong et al. [<xref ref-type="bibr" rid="ref-11">11</xref>]. Alsabery et al. [<xref ref-type="bibr" rid="ref-12">12</xref>] examined the entropy-generating capabilities of a solid rotating cylinder with heat fluctuation in a warmed porous cavity underneath a curved framework. A recent heat conveyor study on convection inside a triangular wavy structure enclosure was made by Asad et al. [<xref ref-type="bibr" rid="ref-13">13</xref>].</p>
<p>Many engineering applications, including vacuum cleaners, washing machines, and blenders, all feature electric components that operate using magnetic principles. Ashorynejad et al. [<xref ref-type="bibr" rid="ref-14">14</xref>] explored combined nanofluid in a MHD convective wavy frame open enclosure. They followed the rule that the Nusselt number declines with an increase in a Hartmann number, but increases with a rise in Rayleigh number and nanoparticle size. Rahman et al. [<xref ref-type="bibr" rid="ref-15">15</xref>] studied the collective impacts of joule heating on magnetohydrodynamic convection within a driven frame enclosure. These authors and those of the references [<xref ref-type="bibr" rid="ref-16">16</xref>&#x2013;<xref ref-type="bibr" rid="ref-19">19</xref>] emphasized that the Hartmann number significantly influences the thermal fluctuations of the flow. Additionally, Joule heating factors influence flow design and isotherms. &#x00D6;ztop et al. [<xref ref-type="bibr" rid="ref-20">20</xref>] provided a summary of coupled magneto-convection in a lid-driven, differentially heated, wavy-walled structure occupied with nanofluid. They showed that the rate of heat removal declines as the Hartmann number increases. Additionally, depending on Hartmann (Ha) and Richardson values, the nanoparticles might cause the heat substitution rate to climb or fall. There are more recent studies on square, wavy, and triangle cavities under the effect of a hydromagnetic field in [<xref ref-type="bibr" rid="ref-21">21</xref>&#x2013;<xref ref-type="bibr" rid="ref-24">24</xref>].</p>
<p>A fin like computer CPU heat sinks, a radiator in a car, heat exchangers in power plants, and heat shifting devices are only a few examples of engineering applications that also incorporate flow construction and heat substitution inside the enclosure. In addition, cutting-edge technologies like fennec canines and hydrogen fuel cells work by discharging heat. Nag et al. [<xref ref-type="bibr" rid="ref-25">25</xref>] reviewed free convective flow in a differential thermal enclosure amidst a horizontal block on a hot wall. Tasnim et al. [<xref ref-type="bibr" rid="ref-26">26</xref>] investigated how free convection heat changed when a baffle was joined to a heated wall. They discovered that fin length and Rayleigh number have a massive effect on the influence of fin position on the rate of heat removal. Sun et al. [<xref ref-type="bibr" rid="ref-27">27</xref>] reported of mix-convection applying triangular conductive fins in a driven chamber. A triangular fin was recommended as a useful parameter for flow design and heat transport speed. The effect of baffles and their length on free convection within transition enclosures was examined by Xu et al. [<xref ref-type="bibr" rid="ref-28">28</xref>]. They determined that at a critical (Ra) level sensitive to fin length, the stream pattern near the fin surface changes from a steady to intermittently unstable flow. By affixing a vertical fin to the lower wall of the standard cage by Asad et al. [<xref ref-type="bibr" rid="ref-29">29</xref>]. Laminar natural convection was generated by Elatar et al. [<xref ref-type="bibr" rid="ref-30">30</xref>] in a square chamber with a special horizontal fin enclosed at various positions and heights connected to a heated surface. They investigated how flow design and heat removal components were affected by the length and position of the fins. Siddiqui et al. [<xref ref-type="bibr" rid="ref-31">31</xref>] studied combined convection in a micro-polar liquid sliding wall cavity. In open enclosures, the effects of parallel insulated baffles were examined by Palaniappan et al. [<xref ref-type="bibr" rid="ref-32">32</xref>]. According to the literature, further activities related to this study are [<xref ref-type="bibr" rid="ref-33">33</xref>&#x2013;<xref ref-type="bibr" rid="ref-35">35</xref>]. Asad et al. [<xref ref-type="bibr" rid="ref-36">36</xref>] investigated the analytical modeling of the MHD boundary layer circulation of a chemically reacting upper convective Maxwell fluid via a vertical surface exposed to many stratifications with different characteristics. The performance of free convection and heat transfer in a curve-shaped enclosure was scrutinized by Asad et al. [<xref ref-type="bibr" rid="ref-37">37</xref>].</p>
<p>To the best of the researcher&#x2019;s knowledge, this indicates that no question about the enclosure with a vertical fin and a wavy form on both sides has been examined. This surviving study will numerically scrutinize the influence of fin size on magneto-combined convective heat transition in a moving-wall, wavy-shaped wall enclosure attached to a vertical fin.</p>
</sec>
<sec id="s2">
<label>2</label>
<title>Problem Specifications with Mathematical Model</title>
<p>For the current investigation, a physical wavy model with boundary conditions estimates a wavy frame enclosure, as shown in <xref ref-type="fig" rid="fig-1">Fig. 1</xref>. The thermo-physical characteristics of a fluid are maintained constant, with the exception of density variations in a buoyancy expression, which are controlled using the Boussinesq approximation. The dominance of viscous diffusion and radiation are also disregarded at the same time. The Newtonian, incompressible, steady, and laminar flow is generally assumed to represent the enclosing liquid.</p>
<fig id="fig-1">
<label>Figure 1</label>
<caption>
<title>Model with boundary conditions is schematically demonstrated</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_50814-fig-1.tif"/>
</fig>
<p>In accordance with the presumptions, the relevant governing equations (see reference [<xref ref-type="bibr" rid="ref-17">17</xref>]) are as follows:
<disp-formula id="eqn-1"><label>(1)</label><mml:math id="mml-eqn-1" display="block"><mml:mrow><mml:mtext>Continuity equation:</mml:mtext></mml:mrow><mml:mtext>&#x00A0;</mml:mtext><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03C8;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>X</mml:mi></mml:mrow></mml:mfrac><mml:mo>+</mml:mo><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03C6;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>Y</mml:mi></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mn>0</mml:mn><mml:mo>,</mml:mo></mml:math></disp-formula>
<disp-formula id="eqn-2"><label>(2)</label><mml:math id="mml-eqn-2" display="block"><mml:mrow><mml:mtext>Momentum equation in</mml:mtext></mml:mrow><mml:mspace width="thinmathspace" /><mml:mi>x</mml:mi><mml:mrow><mml:mtext>-direction:</mml:mtext></mml:mrow><mml:mtext>&#x00A0;</mml:mtext><mml:mi>&#x03C8;</mml:mi><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03C8;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>X</mml:mi></mml:mrow></mml:mfrac><mml:mo>+</mml:mo><mml:mi>&#x03C6;</mml:mi><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03C8;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>Y</mml:mi></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><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:mi>X</mml:mi></mml:mrow></mml:mfrac><mml:mo>+</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:mrow><mml:mi>R</mml:mi><mml:mi>e</mml:mi></mml:mrow></mml:mfrac><mml:msup><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mi>&#x03C8;</mml:mi><mml:mo>,</mml:mo></mml:math></disp-formula>
<disp-formula id="eqn-3"><label>(3)</label><mml:math id="mml-eqn-3" display="block"><mml:mrow><mml:mtext>Momentum equation in</mml:mtext></mml:mrow><mml:mspace width="thinmathspace" /><mml:mi>y</mml:mi><mml:mrow><mml:mtext>-direction:</mml:mtext></mml:mrow><mml:mtext>&#x00A0;</mml:mtext><mml:mi>&#x03C8;</mml:mi><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03C6;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>X</mml:mi></mml:mrow></mml:mfrac><mml:mo>+</mml:mo><mml:mi>&#x03C6;</mml:mi><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03C6;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>Y</mml:mi></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><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:mi>Y</mml:mi></mml:mrow></mml:mfrac><mml:mo>+</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:mrow><mml:mi>R</mml:mi><mml:mi>e</mml:mi></mml:mrow></mml:mfrac><mml:msup><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mi>&#x03C6;</mml:mi><mml:mo>+</mml:mo><mml:mfrac><mml:mrow><mml:mi>G</mml:mi><mml:mi>r</mml:mi></mml:mrow><mml:mrow><mml:mi>R</mml:mi><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mfrac><mml:mi>&#x03B8;</mml:mi><mml:mo>&#x2212;</mml:mo><mml:mfrac><mml:mrow><mml:mi>H</mml:mi><mml:msup><mml:mi>a</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mi>&#x03C6;</mml:mi></mml:mrow><mml:mrow><mml:mi>R</mml:mi><mml:mi>e</mml:mi></mml:mrow></mml:mfrac><mml:mo>,</mml:mo></mml:math></disp-formula>
<disp-formula id="eqn-4"><label>(4)</label><mml:math id="mml-eqn-4" display="block"><mml:mrow><mml:mtext>Energy equation:</mml:mtext></mml:mrow><mml:mtext>&#x00A0;</mml:mtext><mml:mi>&#x03C8;</mml:mi><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03B8;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>X</mml:mi></mml:mrow></mml:mfrac><mml:mo>+</mml:mo><mml:mi>&#x03C6;</mml:mi><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03B8;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>Y</mml:mi></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:mrow><mml:mi>P</mml:mi><mml:mi>r</mml:mi><mml:mi>R</mml:mi><mml:mi>e</mml:mi></mml:mrow></mml:mfrac><mml:msup><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mi>&#x03B8;</mml:mi><mml:mspace width="thinmathspace" /><mml:mo>.</mml:mo></mml:math></disp-formula></p>
<p>The topical variables of the <xref ref-type="disp-formula" rid="eqn-1">Eqs. (1)</xref>&#x2013;<xref ref-type="disp-formula" rid="eqn-4">(4)</xref> described above are, <italic>Pr</italic>, <italic>Ha</italic>, <italic>Gr</italic>, <italic>Re</italic>, and <italic>Ri</italic>, each of which is represented as
<disp-formula id="eqn-5"><label>(5)</label><mml:math id="mml-eqn-5" display="block"><mml:mi>P</mml:mi><mml:mi>r</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mi>&#x03BD;</mml:mi><mml:mi>&#x03B1;</mml:mi></mml:mfrac><mml:mo>,</mml:mo><mml:mi>R</mml:mi><mml:mi>e</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:msub><mml:mi>&#x03C8;</mml:mi><mml:mrow><mml:mi>l</mml:mi><mml:mi>i</mml:mi><mml:mi>d</mml:mi></mml:mrow></mml:msub><mml:mi>W</mml:mi></mml:mrow><mml:mi>&#x03BD;</mml:mi></mml:mfrac><mml:mo>,</mml:mo><mml:mspace width="thinmathspace" /><mml:mspace width="thinmathspace" /><mml:mi>G</mml:mi><mml:mi>r</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mi>g</mml:mi><mml:mi>&#x03B2;</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mi>h</mml:mi></mml:mrow></mml:msub><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mi>c</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:msup><mml:mi>W</mml:mi><mml:mrow><mml:mn>3</mml:mn></mml:mrow></mml:msup></mml:mrow><mml:msup><mml:mi>&#x03BD;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mfrac><mml:mo>,</mml:mo><mml:mi>R</mml:mi><mml:mi>i</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mi>G</mml:mi><mml:mi>r</mml:mi></mml:mrow><mml:mrow><mml:mi>R</mml:mi><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mfrac><mml:mo>,</mml:mo><mml:mspace width="thinmathspace" /><mml:mi>H</mml:mi><mml:mi>a</mml:mi><mml:mo>=</mml:mo><mml:msub><mml:mi>B</mml:mi><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msub><mml:mi>W</mml:mi><mml:msqrt><mml:mfrac><mml:mi>&#x03C3;</mml:mi><mml:mi>&#x03BC;</mml:mi></mml:mfrac></mml:msqrt><mml:mspace width="thinmathspace" /><mml:mspace width="thinmathspace" /><mml:mrow><mml:mtext>and&#xA0;</mml:mtext></mml:mrow><mml:mi>&#x03B8;</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mi>h</mml:mi></mml:mrow></mml:msub><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mi>c</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x0394;</mml:mi></mml:mrow><mml:mi>T</mml:mi></mml:mrow></mml:mfrac></mml:math></disp-formula></p>
<sec id="s2_1">
<label>2.1</label>
<title>Boundary Conditions</title>
<p><disp-formula id="eqn-6a"><label>(6a)</label><mml:math id="mml-eqn-6a" display="block"><mml:mrow><mml:mtext mathvariant="bold">For</mml:mtext></mml:mrow><mml:mspace width="thinmathspace" /><mml:mrow><mml:mtext mathvariant="bold">fin</mml:mtext></mml:mrow><mml:mspace width="thinmathspace" /><mml:mrow><mml:mtext mathvariant="bold">surface:</mml:mtext></mml:mrow><mml:mtext>&#x00A0;</mml:mtext><mml:mn>0</mml:mn><mml:mo>&#x2264;</mml:mo><mml:mi>Y</mml:mi><mml:mo>&#x2264;</mml:mo><mml:mi>L</mml:mi><mml:mo>,</mml:mo><mml:mi>&#x03C8;</mml:mi><mml:mo>=</mml:mo><mml:mi>&#x03C6;</mml:mi><mml:mo>=</mml:mo><mml:mn>0</mml:mn><mml:mo>;</mml:mo><mml:mspace width="thinmathspace" /><mml:mi>X</mml:mi><mml:mo>=</mml:mo><mml:mi>H</mml:mi><mml:mo>+</mml:mo><mml:mfrac><mml:mi>B</mml:mi><mml:mn>2</mml:mn></mml:mfrac><mml:mrow><mml:mtext>&#xA0;and&#xA0;</mml:mtext></mml:mrow><mml:mi>X</mml:mi><mml:mo>=</mml:mo><mml:mi>H</mml:mi><mml:mo>&#x2212;</mml:mo><mml:mfrac><mml:mi>B</mml:mi><mml:mn>2</mml:mn></mml:mfrac><mml:mspace width="thinmathspace" /><mml:mo stretchy="false">(</mml:mo><mml:mrow><mml:mtext>see references</mml:mtext></mml:mrow><mml:mspace width="thinmathspace" /><mml:mo stretchy="false">[</mml:mo><mml:mrow><mml:mn>26</mml:mn></mml:mrow><mml:mo stretchy="false">]</mml:mo><mml:mspace width="thinmathspace" /><mml:mrow><mml:mtext>and</mml:mtext></mml:mrow><mml:mspace width="thinmathspace" /><mml:mo stretchy="false">[</mml:mo><mml:mrow><mml:mn>30</mml:mn></mml:mrow><mml:mo stretchy="false">]</mml:mo><mml:mo stretchy="false">)</mml:mo></mml:math></disp-formula></p>
<p><disp-formula id="eqn-6b"><label>(6b)</label><mml:math id="mml-eqn-6b" display="block"><mml:mrow><mml:mtext>For</mml:mtext></mml:mrow><mml:mspace width="thinmathspace" /><mml:mrow><mml:mtext>the</mml:mtext></mml:mrow><mml:mspace width="thinmathspace" /><mml:mrow><mml:mtext>top</mml:mtext></mml:mrow><mml:mspace width="thinmathspace" /><mml:mrow><mml:mtext>&#xA0;wall</mml:mtext></mml:mrow><mml:mo>:</mml:mo><mml:mspace width="thinmathspace" /><mml:msub><mml:mi>&#x03C8;</mml:mi><mml:mrow><mml:mi>l</mml:mi><mml:mi>i</mml:mi><mml:mi>d</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mn>1</mml:mn><mml:mo>,</mml:mo><mml:mi>&#x03C6;</mml:mi><mml:mo>=</mml:mo><mml:mn>0</mml:mn><mml:mo>,</mml:mo><mml:mi>&#x03B8;</mml:mi><mml:mo>=</mml:mo><mml:mn>1</mml:mn></mml:math></disp-formula></p>
<p><disp-formula id="eqn-6c"><label>(6c)</label><mml:math id="mml-eqn-6c" display="block"><mml:mrow><mml:mtext>For</mml:mtext></mml:mrow><mml:mspace width="thinmathspace" /><mml:mrow><mml:mtext>the</mml:mtext></mml:mrow><mml:mspace width="thinmathspace" /><mml:mrow><mml:mtext>bottom</mml:mtext></mml:mrow><mml:mspace width="thinmathspace" /><mml:mrow><mml:mtext>wall</mml:mtext></mml:mrow><mml:mo>:</mml:mo><mml:mspace width="thinmathspace" /><mml:mi>&#x03C8;</mml:mi><mml:mo>=</mml:mo><mml:mi>&#x03C6;</mml:mi><mml:mo>=</mml:mo><mml:mn>0</mml:mn><mml:mo>,</mml:mo><mml:mi>&#x03B8;</mml:mi><mml:mo>=</mml:mo><mml:mn>1</mml:mn></mml:math></disp-formula></p>
<p><disp-formula id="eqn-6d"><label>(6d)</label><mml:math id="mml-eqn-6d" display="block"><mml:mrow><mml:mtext>For</mml:mtext></mml:mrow><mml:mspace width="thinmathspace" /><mml:mrow><mml:mtext>left</mml:mtext></mml:mrow><mml:mspace width="thinmathspace" /><mml:mrow><mml:mtext>surface</mml:mtext></mml:mrow><mml:mo>:</mml:mo><mml:mspace width="thinmathspace" /><mml:mi>&#x03C8;</mml:mi><mml:mo>=</mml:mo><mml:mi>&#x03C6;</mml:mi><mml:mo>=</mml:mo><mml:mn>0</mml:mn><mml:mo>,</mml:mo><mml:mi>&#x03B8;</mml:mi><mml:mo>=</mml:mo><mml:mn>0</mml:mn><mml:mo>;</mml:mo><mml:mi>A</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mn>1</mml:mn><mml:mo>&#x2212;</mml:mo><mml:mi>cos</mml:mi><mml:mo>&#x2061;</mml:mo><mml:mrow><mml:mo>(</mml:mo><mml:mn>2</mml:mn><mml:mi>&#x03C0;</mml:mi><mml:mi>&#x03BB;</mml:mi><mml:mi>X</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>)</mml:mo></mml:mrow></mml:math></disp-formula></p>
<p><disp-formula id="eqn-6e"><label>(6e)</label><mml:math id="mml-eqn-6e" display="block"><mml:mrow><mml:mtext>For</mml:mtext></mml:mrow><mml:mspace width="thinmathspace" /><mml:mrow><mml:mtext>right</mml:mtext></mml:mrow><mml:mspace width="thinmathspace" /><mml:mrow><mml:mtext>surface</mml:mtext></mml:mrow><mml:mo>:</mml:mo><mml:mspace width="thinmathspace" /><mml:mi>&#x03C8;</mml:mi><mml:mo>=</mml:mo><mml:mi>&#x03C6;</mml:mi><mml:mo>=</mml:mo><mml:mn>0</mml:mn><mml:mo>,</mml:mo><mml:mi>&#x03B8;</mml:mi><mml:mo>=</mml:mo><mml:mn>0</mml:mn><mml:mo>;</mml:mo><mml:mn>1</mml:mn><mml:mo>&#x2212;</mml:mo><mml:mi>A</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mn>1</mml:mn><mml:mo>&#x2212;</mml:mo><mml:mi>cos</mml:mi><mml:mo>&#x2061;</mml:mo><mml:mrow><mml:mo>(</mml:mo><mml:mn>2</mml:mn><mml:mi>&#x03C0;</mml:mi><mml:mi>&#x03BB;</mml:mi><mml:mi>X</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>)</mml:mo></mml:mrow></mml:math></disp-formula></p>
<p>where <italic>H</italic> &#x003D; (<italic>h/W</italic>) is a dimensionless fin location, <italic>L</italic> &#x003D; (<italic>l/W</italic>) is a dimensionless fin size and <italic>B</italic> &#x003D; (<italic>b/W</italic>) is a dimensionless fin thickness.</p>
</sec>
<sec id="s2_2">
<label>2.2</label>
<title>Calculation of Nusselt Number</title>
<p>The Nusselt number and global Nusselt number are induced as follows by incorporating the dimensionless parameters in <xref ref-type="disp-formula" rid="eqn-5">Eq. (5)</xref>:
<disp-formula id="eqn-7"><label>(7)</label><mml:math id="mml-eqn-7" display="block"><mml:mi>N</mml:mi><mml:msub><mml:mi>u</mml:mi><mml:mrow><mml:mi>L</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mrow><mml:mo fence="true" stretchy="true" symmetric="true"></mml:mo><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03B8;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>N</mml:mi></mml:mrow></mml:mfrac><mml:mo>|</mml:mo></mml:mrow><mml:mrow><mml:mi>S</mml:mi></mml:mrow></mml:msub><mml:mspace width="thinmathspace" /><mml:mrow><mml:mtext>and</mml:mtext></mml:mrow><mml:mspace width="thinmathspace" /><mml:mspace width="thinmathspace" /><mml:mi>N</mml:mi><mml:msub><mml:mi>u</mml:mi><mml:mrow><mml:mi>a</mml:mi><mml:mi>v</mml:mi><mml:mi>g</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msubsup><mml:mo>&#x222B;</mml:mo><mml:mrow><mml:mn>0</mml:mn></mml:mrow><mml:mrow><mml:mi>W</mml:mi></mml:mrow></mml:msubsup><mml:msub><mml:mrow><mml:mo fence="true" stretchy="true" symmetric="true"></mml:mo><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03B8;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>N</mml:mi></mml:mrow></mml:mfrac><mml:mo>|</mml:mo></mml:mrow><mml:mrow><mml:mi>S</mml:mi></mml:mrow></mml:msub><mml:mi>d</mml:mi><mml:mi>s</mml:mi></mml:math></disp-formula></p>
</sec>
</sec>
<sec id="s3">
<label>3</label>
<title>Numerical Technique with Validation</title>
<p>The pertinent governing <xref ref-type="disp-formula" rid="eqn-1">Eqs. (1)</xref>&#x2013;<xref ref-type="disp-formula" rid="eqn-4">(4)</xref> jointly amidst <xref ref-type="disp-formula" rid="eqn-6a">Eqs. (6a)</xref>&#x2013;<xref ref-type="disp-formula" rid="eqn-6e">(6e)</xref> are constructed computationally using a Galerkin finite element approach. First, using the &#x03B3; (penalty variable) and the incompressibility review of <xref ref-type="disp-formula" rid="eqn-1">Eq. (1)</xref> as follows:
<disp-formula id="eqn-8"><label>(8)</label><mml:math id="mml-eqn-8" display="block"><mml:mi>P</mml:mi><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mi>&#x03B3;</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03C8;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>X</mml:mi></mml:mrow></mml:mfrac><mml:mo>+</mml:mo><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03C6;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>Y</mml:mi></mml:mrow></mml:mfrac><mml:mo>)</mml:mo></mml:mrow></mml:math></disp-formula></p>
<p>The following conservations of momentum <xref ref-type="disp-formula" rid="eqn-2">Eqs. (2)</xref>, <xref ref-type="disp-formula" rid="eqn-3">(3)</xref> using <xref ref-type="disp-formula" rid="eqn-8">Eq. (8)</xref>, we get
<disp-formula id="eqn-9"><label>(9)</label><mml:math id="mml-eqn-9" display="block"><mml:mi>&#x03C8;</mml:mi><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03C8;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>X</mml:mi></mml:mrow></mml:mfrac><mml:mo>+</mml:mo><mml:mi>&#x03C6;</mml:mi><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03C8;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>Y</mml:mi></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mi>&#x03B3;</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03C8;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>X</mml:mi></mml:mrow></mml:mfrac><mml:mo>+</mml:mo><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03C6;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>Y</mml:mi></mml:mrow></mml:mfrac><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:mrow><mml:mi>R</mml:mi><mml:mi>e</mml:mi></mml:mrow></mml:mfrac><mml:msup><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mi>&#x03C8;</mml:mi></mml:math></disp-formula>
<disp-formula id="eqn-10"><label>(10)</label><mml:math id="mml-eqn-10" display="block"><mml:mi>&#x03C8;</mml:mi><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03C6;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>X</mml:mi></mml:mrow></mml:mfrac><mml:mo>+</mml:mo><mml:mi>&#x03C6;</mml:mi><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03C6;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>Y</mml:mi></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mi>&#x03B3;</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03C8;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>X</mml:mi></mml:mrow></mml:mfrac><mml:mo>+</mml:mo><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03C6;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>Y</mml:mi></mml:mrow></mml:mfrac><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:mrow><mml:mi>R</mml:mi><mml:mi>e</mml:mi></mml:mrow></mml:mfrac><mml:msup><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mi>&#x03C6;</mml:mi><mml:mo>+</mml:mo><mml:mi>R</mml:mi><mml:mi>i</mml:mi><mml:mspace width="thinmathspace" /><mml:mi>&#x03B8;</mml:mi><mml:mo>&#x2212;</mml:mo><mml:mfrac><mml:mrow><mml:mi>H</mml:mi><mml:msup><mml:mi>a</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mi>&#x03C6;</mml:mi></mml:mrow><mml:mrow><mml:mi>R</mml:mi><mml:mi>e</mml:mi></mml:mrow></mml:mfrac></mml:math></disp-formula></p>
<p>Secondly, the progression of momentum and energy in <xref ref-type="disp-formula" rid="eqn-9">Eqs. (9)</xref>, <xref ref-type="disp-formula" rid="eqn-10">(10)</xref> and <xref ref-type="disp-formula" rid="eqn-4">(4)</xref> sequentially utilizing <xref ref-type="disp-formula" rid="eqn-6a">Eqs. (6a)</xref>&#x2013;<xref ref-type="disp-formula" rid="eqn-6e">(6e)</xref> are organized by selecting the Galerkin finite element policy [<xref ref-type="bibr" rid="ref-38">38</xref>&#x2013;<xref ref-type="bibr" rid="ref-40">40</xref>].</p>
<p>The engagement function estimates flow (&#x03C8;, &#x03C6;), and heat qualities (&#x03B8;) using a main set: <inline-formula id="ieqn-2"><mml:math id="mml-ieqn-2"><mml:msubsup><mml:mrow><mml:mo>{</mml:mo><mml:msub><mml:mi>&#x03D5;</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub><mml:mo>}</mml:mo></mml:mrow><mml:mrow><mml:mi>i</mml:mi><mml:mo>=</mml:mo><mml:mn>1</mml:mn></mml:mrow><mml:mrow><mml:mi>k</mml:mi></mml:mrow></mml:msubsup></mml:math></inline-formula> as
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<p>A Galerkin weighted residual approach and finite element techniques are employed within the inner node domain (&#x03A9;), integrating them across the computational domain to derive the nonlinear <xref ref-type="disp-formula" rid="eqn-9">Eqs. (9)</xref>, <xref ref-type="disp-formula" rid="eqn-10">(10)</xref>, and <xref ref-type="disp-formula" rid="eqn-4">(4)</xref>, which are then discretized using small free triangular meshes as illustrated in <xref ref-type="fig" rid="fig-2">Fig. 2</xref>.</p>
<fig id="fig-2">
<label>Figure 2</label>
<caption>
<title>Distribution of the grid size of (a) 1702 and (b) 13273 elements</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_50814-fig-2.tif"/>
</fig>
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mathvariant="normal">&#x2202;</mml:mi><mml:mi>X</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>&#x03D5;</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>X</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>+</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>&#x03D5;</mml:mi><mml:mrow><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>Y</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>&#x03D5;</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>Y</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>]</mml:mo></mml:mrow><mml:mi>d</mml:mi><mml:mi>X</mml:mi><mml:mi>d</mml:mi><mml:mi>Y</mml:mi></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>where the iteration, residual, and node numbers <italic>k</italic>, <italic>j</italic>, and <italic>i</italic> are listed consecutively. The procedures that came after <xref ref-type="disp-formula" rid="eqn-12">Eqs. (12)</xref>&#x2013;<xref ref-type="disp-formula" rid="eqn-14">(14)</xref> were carried out using the Gaussian quadrature technique.</p>
<p>Lastly, Newton Raphson&#x2019;s iteration scheme was engaged to find out residual equations iteratively. The elaborate clarification may be exposed in a literature review [<xref ref-type="bibr" rid="ref-13">13</xref>,<xref ref-type="bibr" rid="ref-37">37</xref>]. After a convergence inquiry, the computational approach&#x2019;s convergence policies are realized and regarded as
<disp-formula id="eqn-15"><label>(15)</label><mml:math id="mml-eqn-15" display="block"><mml:mrow><mml:mo>|</mml:mo><mml:mfrac><mml:mrow><mml:msup><mml:mrow><mml:mi mathvariant="normal">&#x03A0;</mml:mi></mml:mrow><mml:mrow><mml:mi>n</mml:mi><mml:mo>+</mml:mo><mml:mn>1</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:msup><mml:mrow><mml:mi mathvariant="normal">&#x03A0;</mml:mi></mml:mrow><mml:mrow><mml:mi>n</mml:mi></mml:mrow></mml:msup></mml:mrow><mml:msup><mml:mrow><mml:mi mathvariant="normal">&#x03A0;</mml:mi></mml:mrow><mml:mrow><mml:mi>n</mml:mi><mml:mo>+</mml:mo><mml:mn>1</mml:mn></mml:mrow></mml:msup></mml:mfrac><mml:mo>|</mml:mo></mml:mrow><mml:mo>&#x2264;</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mn>5</mml:mn></mml:mrow></mml:msup></mml:math></disp-formula>where <italic>n</italic> is an N-R iteration loop and <inline-formula id="ieqn-3"><mml:math id="mml-ieqn-3"><mml:mrow><mml:mi mathvariant="normal">&#x03A0;</mml:mi></mml:mrow></mml:math></inline-formula> is a function of velocity and temperature.</p>
<p>Considering the current investigation at <italic>Pr</italic> &#x003D; 0.71, <italic>L</italic> &#x003D; 0.45, <italic>Ri</italic> &#x003D; 1, &#x03BB; &#x003D; 2, and <italic>H</italic> &#x003D; 0.50, identify the appropriate grid size. <xref ref-type="table" rid="table-1">Table 1</xref> displays the average Nusselt number of a fin, while <xref ref-type="fig" rid="fig-3">Fig. 3</xref> illustrates it. We examined a grid sensitivity assessment with various types of meshes and found an appropriate answer for the current research. <xref ref-type="table" rid="table-1">Table 1</xref> and <xref ref-type="fig" rid="fig-3">Fig. 3</xref> show that the grid size of 6844 nodes and 13,273 elements provided a satisfactory solution for the present numerical investigation.</p>
<table-wrap id="table-1">
<label>Table 1</label>
<caption>
<title>Grid refinement is required at <italic>L</italic> &#x003D; 0.45, <italic>Ri</italic> &#x003D; 1, <italic>Pr</italic> &#x003D; 0.71, and <italic>H</italic> &#x003D; 0.50</title>
</caption>
<table frame="hsides">
<colgroup>
<col align="left"/>
<col align="left"/>
<col align="left"/>
<col align="left"/>
<col align="left"/>
<col align="left"/>
<col align="left"/>
</colgroup>
<thead>
<tr>
<th>Grid size</th>
<th>Grid name</th>
<th>Nodes</th>
<th>Elements</th>
<th><inline-formula id="ieqn-4"><mml:math id="mml-ieqn-4"><mml:mrow><mml:mi>N</mml:mi></mml:mrow><mml:msub><mml:mrow><mml:mi>u</mml:mi></mml:mrow><mml:mrow><mml:mrow><mml:mi>a</mml:mi><mml:mi>v</mml:mi><mml:mi>g</mml:mi></mml:mrow></mml:mrow></mml:msub></mml:math></inline-formula></th>
<th>Time (s)</th>
<th>Residual error (%)</th>
</tr>
</thead>
<tbody>
<tr>
<td>Grid-1</td>
<td>Normal</td>
<td>931</td>
<td>1702</td>
<td>5.1290</td>
<td>7</td>
<td></td>
</tr>
<tr>
<td>Grid-2</td>
<td>Fine</td>
<td>1213</td>
<td>2245</td>
<td>5.2303</td>
<td>10</td>
<td>1.936791</td>
</tr>
<tr>
<td>Grid-3</td>
<td>Finer</td>
<td>1823</td>
<td>3421</td>
<td>5.3952</td>
<td>13</td>
<td>3.056420</td>
</tr>
<tr>
<td>Grid-4</td>
<td>Extra fine</td>
<td>6844</td>
<td>13,273</td>
<td>5.6491</td>
<td>21</td>
<td>4.494521</td>
</tr>
<tr>
<td>Grid-5</td>
<td>Extremely fine</td>
<td>25,133</td>
<td>49,464</td>
<td>5.6617</td>
<td>48</td>
<td>0.222548</td>
</tr>
</tbody>
</table>
</table-wrap><fig id="fig-3">
<label>Figure 3</label>
<caption>
<title>Grid survey for several elements</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_50814-fig-3.tif"/>
</fig>
<p>The mean Nusselt number on the right surface was compared between Elatar et al. [<xref ref-type="bibr" rid="ref-30">30</xref>] and Nag et al. [<xref ref-type="bibr" rid="ref-25">25</xref>] values at <italic>Ra</italic> &#x003D; 10<sup>6</sup> and <italic>L</italic> &#x003D; 0.20 to confirm the accuracy of the current model&#x2019;s analytical results. With the largest derivation of less than 3.0%, the mean Nusselt number examined in <xref ref-type="table" rid="table-2">Table 2</xref> demonstrates the outstanding acceptance of those queries. Besides, a matching of local Nusselt numbers adjusted for the instant results with Elatar et al. [<xref ref-type="bibr" rid="ref-30">30</xref>] variant <italic>Ra</italic> (10<sup>3</sup>, 10<sup>4</sup>, 10<sup>5</sup>, and 10<sup>6</sup>) and <italic>H</italic> (0.25, 0.50, and 0.75) at <italic>L</italic> &#x003D; 0.5 and <italic>B</italic> &#x003D; 0.01 as exhibited in <xref ref-type="fig" rid="fig-4">Fig. 4</xref>. The local Nusselt number can highlight the significant adjustment of instant results by Elatar et al. [<xref ref-type="bibr" rid="ref-30">30</xref>], as viewed in <xref ref-type="fig" rid="fig-4">Fig. 4</xref>.</p>
<table-wrap id="table-2">
<label>Table 2</label>
<caption>
<title>Code validation of <italic>Nu</italic><sub><italic>avg</italic></sub> for <italic>L</italic> &#x003D; 0.20 and <italic>Ra</italic> &#x003D; 10<sup>6</sup></title>
</caption>
<table frame="hsides">
<colgroup>
<col align="left"/>
<col align="left"/>
<col align="left"/>
<col align="left"/>
</colgroup>
<thead>
<tr>
<th><italic>B</italic></th>
<th>Nag et al. [<xref ref-type="bibr" rid="ref-25">25</xref>]</th>
<th>Elatar et al. [<xref ref-type="bibr" rid="ref-30">30</xref>]</th>
<th>Present result</th>
</tr>
</thead>
<tbody>
<tr>
<td>0.1</td>
<td>9.033</td>
<td>8.947</td>
<td>8.985</td>
</tr>
<tr>
<td>0.02</td>
<td>8.861</td>
<td>8.672</td>
<td>8.783</td>
</tr>
<tr>
<td>0.04</td>
<td>8.888</td>
<td>8.710</td>
<td>8.838</td>
</tr>
</tbody>
</table>
</table-wrap><fig id="fig-4">
<label>Figure 4</label>
<caption>
<title>Comparison of <italic>Nu</italic><sub><italic>L</italic></sub> variant <italic>H</italic> and <italic>Ra</italic> at <italic>L</italic> &#x003D; 0.5 and <italic>B</italic> &#x003D; 0.01</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_50814-fig-4.tif"/>
</fig>
<p>In this research, our laptop configuration was Intel (R), Core (TM) i5-8350U, CPU @ (1.70&#x2013;1.90) GHz, 8.00 GB (RAM), 64-bit operating system, x64-based processor.</p>
</sec>
<sec id="s4">
<label>4</label>
<title>Result on Discussions</title>
<p>The present numerical outcomes have been executed by employing the weighted residual tactics finite element scheme for exploring combined magneto-convection temperature substitution and flow field into a two-sided wavy surface enclosure to dominate the uniform magnetic field. The numerical findings of variant parameters like Richardson number (<italic>Ri</italic>), fin size (L), and Hartmann number are performed to determine the properties of flow patterns and temperature transport using streamlines, isotherms, and the average Nusselt number. The mean fluid temperature removal effectiveness inside the enclosure for three variant fin sizes of thermal cases is presented in graphical and tabulator form.</p>
<sec id="s4_1">
<label>4.1</label>
<title>Impact of Hartmann Number</title>
<p>The results are visualized as streamlines in <xref ref-type="fig" rid="fig-5">Fig. 5</xref>; isotherms in <xref ref-type="fig" rid="fig-6">Fig. 6</xref>; and velocity outlines in <xref ref-type="fig" rid="fig-7">Fig. 7</xref> are scrutinized, acquiring the following ranges: are Hartmann number (<italic>Ha</italic> &#x003D; 0, 20, 40, 60), fin size (<italic>L</italic> &#x003D; 0.25, 0.35, 0.45), fin location (<italic>H</italic> &#x003D; 0.50) with number of amplitude (<italic>A</italic> &#x003D; 0.10), oscillations (&#x03BB; &#x003D; 2.0), and thickness of fin (<italic>B</italic> &#x003D; 0.04) at <italic>Ri</italic> &#x003D; 1.0. The buoyancy force within the cavity is stronger when <italic>Ha</italic> &#x003D; 0, as can be seen in <xref ref-type="fig" rid="fig-5">Fig. 5</xref>. Two vortices also develop inside the cavity, one of which is a main vortex caused by moving the top wall, and the other is a minor vortex generated by the right half of an enclosure. Again, the buoyancy force inside the cavity is strong for <italic>Ha</italic> &#x003D; 20 and 40, and two vortices can be seen there. Another vortex occurred inside the hollow created by the movement of the moving wall at <italic>Ha</italic> &#x003D; 60. Additionally, raising the fin surfaces also raises the flow patterns. The underlying physical reality is that, when the Hartmann number rises, the flow circulation diminishes. This is since using a magnetic field tends to slow down internal fluid dynamics. This indicates that a magnetic field impact has a massive impact on the flow field.</p>
<fig id="fig-5">
<label>Figure 5</label>
<caption>
<title>Streamlines for several <italic>Ha</italic> and <italic>L</italic> at <italic>A</italic> &#x003D; 0.10, &#x03BB; &#x003D; 2.0 and <italic>Ri</italic> &#x003D; 1.0</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_50814-fig-5.tif"/>
</fig><fig id="fig-6">
<label>Figure 6</label>
<caption>
<title>Isotherms for several <italic>Ha</italic> and <italic>L</italic> at <italic>A</italic> &#x003D; 0.10, &#x03BB; &#x003D; 2.0 and <italic>Ri</italic> &#x003D; 1</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_50814-fig-6.tif"/>
</fig><fig id="fig-7">
<label>Figure 7</label>
<caption>
<title>Velocity sketches for different <italic>L</italic> and <italic>Ha</italic> at <italic>A</italic> &#x003D; 0.10, &#x03BB; &#x003D; 2.0 and <italic>Ri</italic> &#x003D; 1.0</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_50814-fig-7.tif"/>
</fig>
<p>On the other hand, due to the larger values of Hartmann number, conduction-dominant heat transmission is seen from isotherms that are nearly identical and evenly dispersed in <xref ref-type="fig" rid="fig-6">Fig. 6</xref>, which is consistent with the influence of the magnetic field. <xref ref-type="fig" rid="fig-7">Fig. 7</xref> shows the impact of the vertical component of the velocity contours at the enclosure variant&#x2019;s horizontal midline at <italic>Ha</italic>, <italic>L</italic>, and <italic>Ri</italic> &#x003D; 1. It is evident that the varying rate of velocity is distinct for each fin surface but comparable for each Hartmann number. Furthermore, as the Hartmann number decreases, the absolute value of the supreme and infimum velocities improves, raising the buoyancy force.</p>
</sec>
<sec id="s4_2">
<label>4.2</label>
<title>Impact of Richardson Number</title>
<p>The results are displayed as streamlines in <xref ref-type="fig" rid="fig-8">Fig. 8</xref>; isotherms in <xref ref-type="fig" rid="fig-9">Fig. 9</xref>; and velocity sketches in <xref ref-type="fig" rid="fig-10">Fig. 10</xref>. The subsequent range, as Richardson number, fin size (<italic>L</italic> &#x003D; 0.25, 0.35, 0.45), fin location (<italic>H</italic> &#x003D; 0.50), number of amplitude (<italic>A</italic> &#x003D; 0.1) with oscillations number (&#x03BB; &#x003D; 2.0), and fin thickness (<italic>B</italic> &#x003D; 0.04) at <italic>Ha</italic> &#x003D; 20 were taken into consideration for flow inside a vertical, wavy frame cavity, and then visually graphically. <xref ref-type="fig" rid="fig-8">Fig. 8</xref> shows that one vortex occurs within the lid wall-created enclosure when <italic>Ri</italic> &#x003D; 0.1 and for all sizes of fins.</p>
<fig id="fig-8">
<label>Figure 8</label>
<caption>
<title>Streamlines for several <italic>L</italic> and <italic>Ri</italic> at <italic>A</italic> &#x003D; 0.10, &#x03BB; &#x003D; 2.0 and <italic>Ha</italic> &#x003D; 20</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_50814-fig-8.tif"/>
</fig><fig id="fig-9">
<label>Figure 9</label>
<caption>
<title>Isotherms for several <italic>L</italic> and <italic>R</italic>i at <italic>A</italic> &#x003D; 0.10, &#x03BB; &#x003D; 2.0 and <italic>Ha</italic> &#x003D; 20</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_50814-fig-9a.tif"/>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_50814-fig-9b.tif"/>
</fig><fig id="fig-10">
<label>Figure 10</label>
<caption>
<title>Velocity outlines for variant <italic>L</italic> and <italic>Ri</italic> at <italic>A</italic> &#x003D; 0.10, &#x03BB; &#x003D; 2.0 and <italic>Ha</italic> &#x003D; 20</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_50814-fig-10.tif"/>
</fig>
<p>This buoyancy force strength is high within a wavy cavity. Again, the flow configuration is comparable to <italic>Ri</italic> &#x003D; 0.1 when <italic>Ri</italic> &#x003D; 1.0 and for all sizes of fin, but two vortices emerge on the on the interior side of the wavy structure enclosure: a minor vortex and a major vortex. Furthermore, for all fin surfaces with extended Richardson numbers (<italic>Ri</italic> &#x003D; 5 and 10), the buoyancy force has a stronger influence, and two vortices appear to be moving along the left and right of a wave-shaped hollow. The physical basis for this is that the buoyancy force&#x2019;s impact on the flow area is more strongly influenced by the Richardson numbers and fin length. <xref ref-type="fig" rid="fig-9">Fig. 9</xref> shows that exposed isotherms show heat amplification caused mostly by conduction. It is clear that if heated and fin surfaces are present, a thick thermic frame layer is present, and that layer becomes thinner as Ri increases until it reaches 10 for all fin surfaces. Rising Ri and L enhance the curvature of isotherms, and heat lines are squeezed to the fin surface and vertical sides of wavy walls, which results in expanded heat replacement by convection. <xref ref-type="fig" rid="fig-10">Fig. 10</xref> illustrates the effects of velocity sketches on the horizontal center line for various fin sizes and Richardson&#x2019;s number in relation to fin placement (<italic>H</italic> &#x003D; 0.50), <italic>Ha</italic> &#x003D; 20, and <italic>Pr</italic> &#x003D; 0.71 of the cavity. Lower <italic>Ri and</italic> more subtle fluctuations in the velocity contours are the telltale signs of it. But the most dramatic difference is in the drawings with greater <italic>RI</italic> velocities. Furthermore, when <italic>Ri</italic> increases for all baffles, the absolute value of infima and dominance of a velocity increase.</p>
</sec>
<sec id="s4_3">
<label>4.3</label>
<title>Heat Transfer</title>
<p><xref ref-type="fig" rid="fig-11">Fig. 11</xref> presents the mean fluid temperature (<italic>&#x03B8;</italic><sub><italic>avg</italic></sub>) for several <italic>L</italic>, <italic>Ri</italic>, and <italic>Ha</italic>, whereas the value of the other parameter is kept constant. <xref ref-type="fig" rid="fig-11">Fig. 11</xref> shows that the mean liquid temperature rises steadily with an increase in the value of <italic>Ri</italic> when <italic>Ha</italic> is fixed. Additionally, it should be highlighted that when <italic>Ha</italic> reduces, the mean fluid temperature rises. <xref ref-type="table" rid="table-3">Table 3</xref> analyzes the statistical value of the mean fluid temperature inside the enclosure. Moreover, from <xref ref-type="table" rid="table-3">Table 3</xref>, the highest mean fluid temperature inside the enclosure is 0.53403, found at <italic>L</italic> &#x003D; 0.45, <italic>B</italic> &#x003D; 0.50, <italic>Ha</italic> &#x003D; 0, and <italic>Ri</italic> &#x003D; 10.</p>
<fig id="fig-11">
<label>Figure 11</label>
<caption>
<title>&#x03B8;<sub><italic>avg</italic></sub> for different <italic>Ha</italic>, <italic>L</italic> and <italic>Ri</italic> at <italic>A</italic> &#x003D; 0.10, &#x03BB; &#x003D; 2.0</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_50814-fig-11.tif"/>
</fig><table-wrap id="table-3">
<label>Table 3</label>
<caption>
<title><italic>&#x03B8;</italic><sub><italic>avg</italic></sub> for numerous <italic>Ha</italic>, <italic>L</italic> and <italic>Ri</italic> at <italic>Pr</italic> &#x003D; 0.71, <italic>A</italic> &#x003D; 0.10 and &#x03BB; &#x003D; 2.0</title>
</caption>
<table frame="hsides">
<colgroup>
<col align="left"/>
<col align="left"/>
<col align="left"/>
<col align="left"/>
<col align="left"/>
<col align="left"/>
</colgroup>
<thead>
<tr>
<th></th>
<th></th>
<th align="center" colspan="4">Mean fluid temperature (<italic>&#x03B8;</italic><sub><italic>avg</italic></sub>)</th>
</tr>
<tr>
<th><italic>L</italic></th>
<th><italic>Ri</italic></th>
<th><italic>Ha</italic> &#x003D; 0</th>
<th><italic>Ha</italic> &#x003D; 20</th>
<th><italic>Ha</italic> &#x003D; 40</th>
<th><italic>Ha</italic> &#x003D; 60</th>
</tr>
</thead>
<tbody>
<tr>
<td rowspan="4">L &#x003D; 0.25</td>
<td>0.1</td>
<td>0.44621</td>
<td>0.44362</td>
<td>0.44253</td>
<td>0.44227</td>
</tr>
<tr>
<td>1</td>
<td>0.45074</td>
<td>0.44907</td>
<td>0.44849</td>
<td>0.44837</td>
</tr>
<tr>
<td>5</td>
<td>0.47049</td>
<td>0.46671</td>
<td>0.46457</td>
<td>0.46388</td>
</tr>
<tr>
<td>10</td>
<td>0.47290</td>
<td>0.46795</td>
<td>0.46513</td>
<td>0.46423</td>
</tr>
<tr>
<td rowspan="4">L &#x003D; 0.35</td>
<td>0.1</td>
<td>0.47661</td>
<td>0.47465</td>
<td>0.47373</td>
<td>0.47348</td>
</tr>
<tr>
<td>1</td>
<td>0.48250</td>
<td>0.48091</td>
<td>0.48014</td>
<td>0.47993</td>
</tr>
<tr>
<td>5</td>
<td>0.50282</td>
<td>0.49889</td>
<td>0.49654</td>
<td>0.49577</td>
</tr>
<tr>
<td>10</td>
<td>0.50690</td>
<td>0.50181</td>
<td>0.49879</td>
<td>0.49780</td>
</tr>
<tr>
<td rowspan="4">L &#x003D; 0.45</td>
<td>0.1</td>
<td>0.50535</td>
<td>0.50380</td>
<td>0.50300</td>
<td>0.50276</td>
</tr>
<tr>
<td>1</td>
<td>0.51077</td>
<td>0.50924</td>
<td>0.50839</td>
<td>0.50813</td>
</tr>
<tr>
<td>5</td>
<td>0.52929</td>
<td>0.52568</td>
<td>0.52345</td>
<td>0.52270</td>
</tr>
<tr>
<td>10</td>
<td>0.53403</td>
<td>0.52920</td>
<td>0.52627</td>
<td>0.52530</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>A plot of the mean Nusselt number for several fin sizes (<italic>L</italic>), Hartmann numbers (<italic>Ha</italic>), and Richardson numbers (Ri) shows that, at the same time, the values of the other parameters are maintained at their default values, as observed in <xref ref-type="fig" rid="fig-12">Fig. 12</xref> and numerical values in <xref ref-type="table" rid="table-4">Table 4</xref>. As exposed in <xref ref-type="fig" rid="fig-12">Fig. 12</xref>, the mean Nusselt number rises firmly when the Hartmann number reduces for a unique fin length. Moreover, raising the Richardson number improved the mean Nusselt number on the right surface. <italic>Ri</italic> rises at a constant fin size; the buoyancy force expands and gains a heat replacement rate. <xref ref-type="table" rid="table-4">Table 4</xref> explores the statistical value of the mean Nusselt number through the right wall surface for several <italic>Ri, Ha</italic>, and <italic>L</italic>. As reported in <xref ref-type="table" rid="table-4">Table 4</xref>, it proves that the value of heat removal performance rate is improved by inflating <italic>Ri</italic> and reducing <italic>Ha</italic> and <italic>L</italic>. Moreover, from <xref ref-type="table" rid="table-4">Table 4</xref>, the supreme <italic>Nu</italic><sub><italic>avg</italic></sub> is 7.6491 along the right cool surface exposed at <italic>L</italic> &#x003D; 0.45, <italic>B</italic> &#x003D; 0.50, and <italic>Ri</italic> &#x003D; 10.</p>
<fig id="fig-12">
<label>Figure 12</label>
<caption>
<title><italic>Nu</italic><sub><italic>avg</italic></sub> for various <italic>L</italic>, <italic>Ri</italic> and <italic>Ha</italic> at <italic>A</italic> &#x003D; 0.10 and &#x03BB; &#x003D; 2.0</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_50814-fig-12.tif"/>
</fig><table-wrap id="table-4">
<label>Table 4</label>
<caption>
<title><italic>Nu</italic><sub><italic>avg</italic></sub> for various <italic>L</italic>, <italic>Ri</italic> and <italic>Ha</italic> at <italic>Pr</italic> &#x003D; 0.71, <italic>A</italic> &#x003D; 0.10 and &#x03BB; &#x003D; 2.0</title>
</caption>
<table frame="hsides">
<colgroup>
<col align="left"/>
<col align="left"/>
<col align="left"/>
<col align="left"/>
<col align="left"/>
<col align="left"/>
</colgroup>
<thead>
<tr>
<th></th>
<th></th>
<th align="center" colspan="4">Mean nusselt number (<italic>Nu</italic><sub><italic>avg</italic></sub>)</th>
</tr>
<tr>
<th><italic>L</italic></th>
<th><italic>Ha</italic></th>
<th><italic>Ri</italic> &#x003D; 0.1</th>
<th><italic>Ri</italic> &#x003D; 1</th>
<th><italic>Ri</italic> &#x003D; 5</th>
<th><italic>Ri</italic> &#x003D; 10</th>
</tr>
</thead>
<tbody>
<tr>
<td rowspan="4">L &#x003D; 0.25</td>
<td>0</td>
<td>6.3764</td>
<td>6.4095</td>
<td>6.6872</td>
<td>6.9981</td>
</tr>
<tr>
<td>20</td>
<td>6.3541</td>
<td>6.3794</td>
<td>6.6539</td>
<td>6.9670</td>
</tr>
<tr>
<td>40</td>
<td>6.3417</td>
<td>6.3637</td>
<td>6.6471</td>
<td>6.9684</td>
</tr>
<tr>
<td>60</td>
<td>6.3312</td>
<td>6.3561</td>
<td>6.6327</td>
<td>6.9602</td>
</tr>
<tr>
<td rowspan="4">L &#x003D; 0.35</td>
<td>0</td>
<td>6.5975</td>
<td>6.6529</td>
<td>6.9985</td>
<td>7.3648</td>
</tr>
<tr>
<td>20</td>
<td>6.5761</td>
<td>6.6137</td>
<td>6.9367</td>
<td>7.3077</td>
</tr>
<tr>
<td>40</td>
<td>6.5713</td>
<td>6.6105</td>
<td>6.9271</td>
<td>7.2946</td>
</tr>
<tr>
<td>60</td>
<td>6.5625</td>
<td>6.6027</td>
<td>6.9129</td>
<td>7.2841</td>
</tr>
<tr>
<td rowspan="4">L &#x003D; 0.45</td>
<td>0</td>
<td>6.8217</td>
<td>6.8786</td>
<td>7.2917</td>
<td>7.6491</td>
</tr>
<tr>
<td>20</td>
<td>6.7948</td>
<td>6.8405</td>
<td>7.2264</td>
<td>7.5774</td>
</tr>
<tr>
<td>40</td>
<td>6.7801</td>
<td>6.8277</td>
<td>7.2179</td>
<td>7.5638</td>
</tr>
<tr>
<td>60</td>
<td>6.7693</td>
<td>6.8163</td>
<td>7.2056</td>
<td>7.5490</td>
</tr>
</tbody>
</table>
</table-wrap>
</sec>
<sec id="s4_4">
<label>4.4</label>
<title>Calculation of Fin Surface Effectiveness</title>
<p>Fin surface effectiveness is a variation that assesses an improvement in heat conversion within the cavity with fin surfaces compared to a case without fin surfaces, as pursued by Elatar et al. [<xref ref-type="bibr" rid="ref-30">30</xref>] as follows:
<disp-formula id="eqn-16"><label>(16)</label><mml:math id="mml-eqn-16" display="block"><mml:msub><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mfrac><mml:msub><mml:mi>Q</mml:mi><mml:mrow><mml:mi>f</mml:mi><mml:mi>i</mml:mi><mml:mi>n</mml:mi></mml:mrow></mml:msub><mml:msub><mml:mi>Q</mml:mi><mml:mrow><mml:mi>w</mml:mi><mml:mi>i</mml:mi><mml:mi>t</mml:mi><mml:mi>h</mml:mi><mml:mi>o</mml:mi><mml:mi>u</mml:mi><mml:mi>t</mml:mi><mml:mi>f</mml:mi><mml:mi>i</mml:mi><mml:mi>n</mml:mi></mml:mrow></mml:msub></mml:mfrac></mml:math></disp-formula></p>
<p><xref ref-type="fig" rid="fig-13">Fig. 13</xref> exhibits fin effectiveness regarding distinct fin lengths <inline-formula id="ieqn-5"><mml:math id="mml-ieqn-5"><mml:mrow><mml:mo>(</mml:mo><mml:mn>0.25</mml:mn><mml:mo>&#x2264;</mml:mo><mml:mi>L</mml:mi><mml:mo>&#x2264;</mml:mo><mml:mn>0.45</mml:mn><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>, Hartmann number (<italic>Ha</italic> &#x003D; 0, 20, 40, 60), and Richardson number <inline-formula id="ieqn-6"><mml:math id="mml-ieqn-6"><mml:mrow><mml:mo>(</mml:mo><mml:mn>0.1</mml:mn><mml:mo>&#x2264;</mml:mo><mml:mi>R</mml:mi><mml:mi>i</mml:mi><mml:mo>&#x2264;</mml:mo><mml:mn>10</mml:mn><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> at <italic>Pr</italic> &#x003D; 0.71, <italic>A</italic> &#x003D; 0.10, <italic>&#x03BB;</italic> &#x003D; 2.0. <xref ref-type="fig" rid="fig-13">Fig. 13</xref> shows that fin efficiency steadily increases with increasing <italic>Ri</italic> for a different fin size, while the magnetic domain declines for all fin sizes. Moreover, a key component of controlling the heat replacement rate is fin blockage, which is produced when convective heat fluctuation and an extended fin length start to convert the dominating supporting conduction.</p>
<fig id="fig-13">
<label>Figure 13</label>
<caption>
<title>&#x03B5;<sub><italic>f</italic></sub> for various <italic>L</italic>, <italic>Ri</italic> and <italic>Ha</italic> at <italic>A</italic> &#x003D; 0.10 and &#x03BB; &#x003D; 2.0</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_50814-fig-13a.tif"/>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_50814-fig-13b.tif"/></fig>
<p>As a result, to increase the rate of heat release for individually fin length, a relatively high Richardson number is required. <xref ref-type="table" rid="table-5">Table 5</xref> shows the statistical value of fin effectiveness noted that the &#x03B5;<sub><italic>f</italic></sub> &#x003E; 1 for all <italic>L</italic>. This means, based on the numerical data, the fin placement affects their efficacy for all fin surfaces. Moreover, from <xref ref-type="table" rid="table-5">Table 5</xref>, the best fin effectiveness is 1.211730 audited at <italic>L</italic> &#x003D; 0.45, <italic>H</italic> &#x003D; 0.50, <italic>Ha</italic> &#x003D; 0 and <italic>Ri</italic> &#x003D; 10.</p>
<table-wrap id="table-5">
<label>Table 5</label>
<caption>
<title>&#x03B5;<sub><italic>f</italic></sub> for different <italic>L</italic>, <italic>Ri</italic> and <italic>Ha</italic> at <italic>A</italic> &#x003D; 0.10 and &#x03BB; &#x003D; 2.0</title>
</caption>
<table frame="hsides">
<colgroup>
<col align="left"/>
<col align="left"/>
<col align="left"/>
<col align="left"/>
<col align="left"/>
<col align="left"/>
</colgroup>
<thead>
<tr>
<th><italic>L</italic></th>
<th><italic>Ri</italic></th>
<th align="center" colspan="4">Fin surface effectiveness (&#x03B5;<sub><italic>f</italic></sub>)</th>
</tr>
<tr>
<th></th>
<th></th>
<th><italic>Ha</italic> &#x003D; 0</th>
<th><italic>Ha</italic> &#x003D; 20</th>
<th><italic>Ha</italic> &#x003D; 40</th>
<th><italic>Ha</italic> &#x003D; 60</th>
</tr>
</thead>
<tbody>
<tr>
<td rowspan="4"><italic>L</italic> &#x003D; 0.25</td>
<td>0.1</td>
<td>1.081425</td>
<td>1.080930</td>
<td>1.079222</td>
<td>1.075849</td>
</tr>
<tr>
<td>1</td>
<td>1.087349</td>
<td>1.087252</td>
<td>1.086481</td>
<td>1.084033</td>
</tr>
<tr>
<td>5</td>
<td>1.103860</td>
<td>1.103765</td>
<td>1.103278</td>
<td>1.101785</td>
</tr>
<tr>
<td>10</td>
<td>1.118086</td>
<td>1.117703</td>
<td>1.116529</td>
<td>1.114484</td>
</tr>
<tr>
<td rowspan="4"><italic>L</italic> &#x003D; 0.35</td>
<td>0.1</td>
<td>1.132538</td>
<td>1.132198</td>
<td>1.130892</td>
<td>1.126286</td>
</tr>
<tr>
<td>1</td>
<td>1.138264</td>
<td>1.138125</td>
<td>1.138077</td>
<td>1.135724</td>
</tr>
<tr>
<td>5</td>
<td>1.153317</td>
<td>1.153249</td>
<td>1.153224</td>
<td>1.152160</td>
</tr>
<tr>
<td>10</td>
<td>1.169180</td>
<td>1.168798</td>
<td>1.167629</td>
<td>1.165381</td>
</tr>
<tr>
<td rowspan="4"><italic>L</italic> &#x003D; 0.45</td>
<td>0.1</td>
<td>1.183970</td>
<td>1.183324</td>
<td>1.180897</td>
<td>1.175560</td>
</tr>
<tr>
<td>1</td>
<td>1.187686</td>
<td>1.187577</td>
<td>1.187263</td>
<td>1.184662</td>
</tr>
<tr>
<td>5</td>
<td>1.197163</td>
<td>1.197054</td>
<td>1.196953</td>
<td>1.195186</td>
</tr>
<tr>
<td>10</td>
<td>1.211730</td>
<td>1.211083</td>
<td>1.209867</td>
<td>1.207140</td>
</tr>
</tbody>
</table>
</table-wrap>
</sec>
</sec>
<sec id="s5">
<label>5</label>
<title>Conclusion</title>
<p>The overall destination of this inquiry is to determine the impact of fin size with Richardson number and Hartmann number variance on hydromagnetic mixed convective flow with heat removal performance within a two-side wavy surface enclosure. The numerical method was verified by contrasting the mean Nusselt number and local Nusselt number obtained by the code with previously published data for existing inquiries. Based on the results, the following will be stated:
<list list-type="bullet">
<list-item>
<p>These outcomes confirmed that the fin length difference greatly influences the flow features and temperature field within the cavity.</p></list-item>
<list-item>
<p>A higher Richardson number and a lower Hartman number can be achieved by keeping the fin size constant and improving the heat transfer performance rate. As the fin size is extended, the average fluid temperature as well as the heat production speed increase.</p></list-item>
<list-item>
<p>The highest mean fluid temperature inside the cavity is 0.53403, or 11.45% (approx.), found at <italic>L</italic> &#x003D; 0.45, <italic>B</italic> &#x003D; 0.50, <italic>Ha</italic> &#x003D; 0, and <italic>Ri</italic> &#x003D; 10.</p></list-item>
<list-item>
<p>When the Richardson number progresses to a uniform fin size, the buoyancy force increases, and the heat transfer rate improves. For a specific fin size, as the value of <italic>Ri</italic>rises and <italic>Ha</italic> decreases, the mean Nusselt number rises. The supreme <italic>Nu</italic><sub><italic>avg</italic></sub> is 7.6491, or 6.48% (approx.) along the right cool surface exposed at <italic>L</italic> &#x003D; 0.45, <italic>B</italic> &#x003D; 0.50, and <italic>Ri</italic> &#x003D; 10.</p></list-item>
<list-item>
<p>The baffle&#x2019;s effectiveness is improved by raising <italic>Ri</italic> and reducing <italic>Ha</italic> for all changes in fin sizes while the fin is in a particular position. The maximum fin effectiveness is 1.211730, or 7.728% (approx.) audited at <italic>L</italic> &#x003D; 0.45, <italic>H</italic> &#x003D; 0.50, <italic>Ha</italic> &#x003D; 0, and <italic>Ri</italic> &#x003D; 10.</p></list-item>
</list></p>
</sec>
</body>
<back>
<glossary content-type="abbreviations" id="glossary-1">
<title>Nomenclature</title>
<def-list>
<def-item>
<term><italic>A</italic></term>
<def>
<p>Amplitude</p>
</def>
</def-item>
<def-item>
<term><italic>B</italic><sub>0</sub></term>
<def>
<p>Magnetic field strength</p>
</def>
</def-item>
<def-item>
<term><italic>B</italic></term>
<def>
<p>Nondimensional fin thickness,</p>
</def>
</def-item>
<def-item>
<term><italic>H</italic></term>
<def>
<p>Nondimensional fin position</p>
</def>
</def-item>
<def-item>
<term><italic>g</italic></term>
<def>
<p>Gravitational force, <italic>m/s</italic><sup>2</sup></p>
</def>
</def-item>
<def-item>
<term><italic>Gr</italic></term>
<def>
<p>Grashof number, <italic>W</italic><sup>3</sup><italic>g&#x03B2;(T</italic><sub>h</sub> &#x2212; <italic>T</italic><sub>c</sub><italic>)/v</italic><sup>2</sup></p>
</def>
</def-item>
<def-item>
<term><italic>Ha</italic></term>
<def>
<p>Hartmann number, <inline-formula id="ieqn-1"><mml:math id="mml-ieqn-1"><mml:msub><mml:mi>B</mml:mi><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msub><mml:mi>W</mml:mi><mml:msqrt><mml:mi>&#x03B1;</mml:mi><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mi>&#x03C1;</mml:mi></mml:msqrt></mml:math></inline-formula></p>
</def>
</def-item>
<def-item>
<term><italic>L</italic></term>
<def>
<p>Nondimensional fin length</p>
</def>
</def-item>
<def-item>
<term><italic>N</italic></term>
<def>
<p>Nondimensional distance normal to surface coordinates</p>
</def>
</def-item>
<def-item>
<term><italic>Nu</italic><sub><italic>avg</italic></sub></term>
<def>
<p>Average Nusselt number</p>
</def>
</def-item>
<def-item>
<term><italic>Nu</italic><sub><italic>L</italic></sub></term>
<def>
<p>Local Nusselt number</p>
</def>
</def-item>
<def-item>
<term><italic>Pr</italic></term>
<def>
<p>Prandlt number, <italic>v/&#x03B1;</italic></p>
</def>
</def-item>
<def-item>
<term><italic>Re</italic></term>
<def>
<p>Reynold number, <italic>&#x03C8;W</italic>/<italic>v</italic></p>
</def>
</def-item>
<def-item>
<term><italic>Ri</italic></term>
<def>
<p>Richardson number, <italic>Gr/Re</italic><sup>2</sup></p>
</def>
</def-item>
<def-item>
<term><italic>S</italic></term>
<def>
<p>Nondimensional special coordinate along wavy surface</p>
</def>
</def-item>
<def-item>
<term><italic>W</italic></term>
<def>
<p>Enclosure height and width, <italic>m</italic></p>
</def>
</def-item>
<def-item>
<term><italic>&#x03C8;, &#x03C6;</italic></term>
<def>
<p>Nondimensional velocity in X and Y axis, respectively, (<italic>&#x03C8; &#x003D; uW/&#x03B1;, &#x03C6; &#x003D; vW/&#x03B1;</italic>)</p>
</def>
</def-item>
</def-list>
<def-list>
<title>Greek Symbols</title>
<def-item>
<term><italic>&#x03B1;</italic></term>
<def>
<p>Thermal diffusivity, <italic>m</italic><sup>2</sup><italic>/s</italic></p>
</def>
</def-item>
<def-item>
<term><italic>&#x03B2;</italic></term>
<def>
<p>A coefficient of thermal expansion, 1/<italic>K</italic></p>
</def>
</def-item>
<def-item>
<term><italic>&#x03C1;</italic></term>
<def>
<p>Local density, <italic>kg/m</italic><sup>3</sup></p>
</def>
</def-item>
<def-item>
<term><italic>&#x03BC;</italic></term>
<def>
<p>Dynamic viscosity, <italic>Ns/m</italic><sup>2</sup></p>
</def>
</def-item>
<def-item>
<term><italic>&#x03B8;</italic></term>
<def>
<p>Nondimensional temperature (<italic>T &#x2212; T</italic><sub>c</sub>)/(<italic>T</italic><sub>h &#x2212;</sub> <italic>T</italic><sub>c</sub>)</p>
</def>
</def-item>
<def-item>
<term><italic>&#x03C5;</italic></term>
<def>
<p>Kinematic viscosity, <italic>m</italic><sup>2</sup><italic>/s</italic></p>
</def>
</def-item>
<def-item>
<term><italic>&#x03BB;</italic></term>
<def>
<p>Number of oscillations</p>
</def>
</def-item>
<def-item>
<term><italic>&#x03B5;</italic></term>
<def>
<p>Effectiveness</p>
</def>
</def-item>
</def-list>
<def-list>
<title>Subscripts
</title>
<def-item>
<term><italic>avg</italic></term>
<def>
<p>Average</p>
</def>
</def-item>
<def-item>
<term><italic>c</italic></term>
<def>
<p>Cool</p>
</def>
</def-item>
<def-item>
<term><italic>h</italic></term>
<def>
<p>Hot</p>
</def>
</def-item>
<def-item>
<term><italic>f</italic></term>
<def>
<p>Fin</p>
</def>
</def-item>
</def-list>
</glossary>
<ack><p>The authors express their gratitude to their affiliated universities and thank the Deanship of Scientific Research at Umm Al-Qura University for supporting this work through Grant Code: 22UQU4240002DSR19.</p>
</ack>
<sec><title>Funding Statement</title>
<p>The authors received no specific funding for this study.</p>
</sec>
<sec><title>Author Contributions</title>
<p>The authors confirm contribution to the paper as follows: study conception and design, data collection, analysis and interpretation of results, draft manuscript preparation: Md. Fayz-Al-Asad, F. Mebarek-Oudina, H. Vaidya, Md. Shamim Hasan, and Md. Manirul Alam Sarker, A. I. Ismail. 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>Data are available on request.</p>
</sec>
<sec sec-type="COI-statement"><title>Conflicts of Interest</title>
<p>The authors certify that there are no conflicts of interest about the publication of this research.</p>
</sec>
<ref-list content-type="authoryear">
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