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<front>
<journal-meta>
<journal-id journal-id-type="publisher-id">Front. Phys.</journal-id>
<journal-title>Frontiers in Physics</journal-title>
<abbrev-journal-title abbrev-type="pubmed">Front. Phys.</abbrev-journal-title>
<issn pub-type="epub">2296-424X</issn>
<publisher>
<publisher-name>Frontiers Media S.A.</publisher-name>
</publisher>
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<article-meta>
<article-id pub-id-type="publisher-id">1079641</article-id>
<article-id pub-id-type="doi">10.3389/fphy.2022.1079641</article-id>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Physics</subject>
<subj-group>
<subject>Original Research</subject>
</subj-group>
</subj-group>
</article-categories>
<title-group>
<article-title>RETRACTED: Mixed convective heat transfer in a power-law fluid in a square enclosure: Higher order finite element solutions</article-title>
<alt-title alt-title-type="left-running-head">Bilal et al.</alt-title>
<alt-title alt-title-type="right-running-head">
<ext-link ext-link-type="uri" xlink:href="https://doi.org/10.3389/fphy.2022.1079641">10.3389/fphy.2022.1079641</ext-link>
</alt-title>
</title-group>
<contrib-group>
<contrib contrib-type="author">
<name>
<surname>Bilal</surname>
<given-names>S.</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
<uri xlink:href="https://loop.frontiersin.org/people/813663/overview"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Khan</surname>
<given-names>Noor Zeb</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Fatima</surname>
<given-names>Iqra</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
</contrib>
<contrib contrib-type="author" corresp="yes">
<name>
<surname>Riaz</surname>
<given-names>Arshad</given-names>
</name>
<xref ref-type="aff" rid="aff2">
<sup>2</sup>
</xref>
<xref ref-type="corresp" rid="c001">&#x2a;</xref>
<uri xlink:href="https://loop.frontiersin.org/people/813103/overview"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Ansari</surname>
<given-names>Ghulam Jillani</given-names>
</name>
<xref ref-type="aff" rid="aff3">
<sup>3</sup>
</xref>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Alhazmi</surname>
<given-names>Sharifah E.</given-names>
</name>
<xref ref-type="aff" rid="aff4">
<sup>4</sup>
</xref>
</contrib>
<contrib contrib-type="author">
<name>
<surname>El-Din</surname>
<given-names>ElSayed M. Tag</given-names>
</name>
<xref ref-type="aff" rid="aff5">
<sup>5</sup>
</xref>
</contrib>
</contrib-group>
<aff id="aff1">
<sup>1</sup>
<institution>Department of Mathematics</institution>, <institution>Air University</institution>, <addr-line>Islamabad</addr-line>, <country>Pakistan</country>
</aff>
<aff id="aff2">
<sup>2</sup>
<institution>Department of Mathematics</institution>, <institution>Division of Science and Technology</institution>, <institution>University of Education</institution>, <addr-line>Lahore</addr-line>, <country>Pakistan</country>
</aff>
<aff id="aff3">
<sup>3</sup>
<institution>Department of Information Sciences</institution>, <institution>Division of Science and Technology</institution>, <institution>University of Education</institution>, <addr-line>Lahore</addr-line>, <country>Pakistan</country>
</aff>
<aff id="aff4">
<sup>4</sup>
<institution>Mathematics Department</institution>, <institution>Al-Qunfudah University College</institution>, <institution>Umm Al-Qura University</institution>, <addr-line>Mecca</addr-line>, <country>Saudi Arabia</country>
</aff>
<aff id="aff5">
<sup>5</sup>
<institution>Center of Research</institution>, <institution>Faculty of Engineering</institution>, <institution>Future University in Egypt</institution>, <addr-line>New Cairo</addr-line>, <country>Egypt</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/165426/overview">Kh S. Mekheimer</ext-link>, Al-Azhar University, Egypt</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/1795434/overview">Nehad Ali Shah</ext-link>, Sejong University, South Korea</p>
<p>
<ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/295518/overview">M. Sankar</ext-link>, University of Technology and Applied Sciences (Oman), Oman</p>
</fn>
<corresp id="c001">&#x2a;Correspondence: Arshad Riaz, <email>arshad-riaz@ue.edu.pk</email>
</corresp>
<fn fn-type="other">
<p>This article was submitted to Statistical and Computational Physics, a section of the journal Frontiers in Physics</p>
</fn>
</author-notes>
<pub-date pub-type="epub">
<day>04</day>
<month>01</month>
<year>2023</year>
</pub-date>
<pub-date pub-type="collection">
<year>2022</year>
</pub-date>
<volume>10</volume>
<elocation-id>1079641</elocation-id>
<history>
<date date-type="received">
<day>25</day>
<month>10</month>
<year>2022</year>
</date>
<date date-type="accepted">
<day>05</day>
<month>12</month>
<year>2022</year>
</date>
</history>
<permissions>
<copyright-statement>Copyright &#xa9; 2023 Bilal, Khan, Fatima, Riaz, Ansari, Alhazmi and El-Din.</copyright-statement>
<copyright-year>2023</copyright-year>
<copyright-holder>Bilal, Khan, Fatima, Riaz, Ansari, Alhazmi and El-Din</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>Incorporation of momentum gradients produced due to inertial motion of the lid along with the presence of temperature differences in the configuration make the physical problem more significant. The joint variation of momentum and thermal diffusion in diversified natural liquids is recognized as mixed convection. Valuable attention has been received by such a phenomenon in different areas of science and technology such as in wind current&#x2013;based solar receivers, electronic instruments, control of emergency shutdown in reactors, thermal exchangers, oceanic currents, control of atmospheric pollution, and so on. So, the main focus is to contemplate hydrothermal characteristics of a power-law fluid contained in a square cavity with the movement of the upper lid and being thermally adiabatic. The other extremities are considered to be at rest, and the base wall is prescribed with uniform/non-uniform temperature distributions. The governing formulation of the problem is handled by executing a finite element approach. Hybrid meshing is performed for domain discretization, and weak variational formulation is utilized for formulation discretization. Second-degree polynomials are employed as the interpolation function, providing information about velocity and temperature distributions at boundary and intermediate nodes. The system of finalized non-linear equations is resolved by using the Paradiso software. The results for velocity and temperature distributions are attained comparatively for uniformly and non-uniformly heated profiles. The kinetic energy and average Nusselt number are also computed against flow concerning variables. From the attained graphical and tabular data, it is deduced that by increasing the Reynolds number, inertial forces dominate over buoyancy forces and the effect of lid movement is prominent on flow characteristics. It is also inferred that for the shear thickening case and for all values of the Reynolds number, the average Nusselt number shows a constant behavior.</p>
</abstract>
<kwd-group>
<kwd>mixed convection</kwd>
<kwd>square cavity</kwd>
<kwd>uniform/non-uniform heating</kwd>
<kwd>finite element method</kwd>
<kwd>heat transfer</kwd>
</kwd-group>
</article-meta>
</front>
<body>
<sec id="s1">
<title>1 Introduction</title>
<p>Buoyancy- and lid-driven flows inside confined geometries have appealed the promising intent of researchers. Representative fields of interest include flash drying, liquid fuels combustion, food processing plants, evaporation of cyclones, crystal growth, material separation processes, and so on. In recent years, modern technologies demand for combined (buoyancy- and lid-driven) diffusions in different procedures. Considerable work has been published on natural convection describing the role of buoyancy forces. Unfortunately, the combination of free and forced convection seldom arise in practice. Some already published work from where the motivation for the current effort has been taken is described here. Like, Lyican et al. [<xref ref-type="bibr" rid="B1">1</xref>] performed numerical computations to interpret hydrothermal characteristics of the natural convective flow in a trapezoidal enclosure by considering adiabatic extremities. Roy and Basak [<xref ref-type="bibr" rid="B2">2</xref>] made an outstanding effort to examine heat transfer generated by the thermally driven viscous liquid with a prescription of uniform heat distribution. By measuring the influence of oscillation of the flow and temperature propagation, the dual convective flow of a viscous liquid with wavy boundaries was manifested by Amiri et al. [<xref ref-type="bibr" rid="B3">3</xref>]. The impression of permeability on natural convection generated in trapezium along with the production of thermal convective potential with cold and heat parallel boundaries was explicated by Varol et al. [<xref ref-type="bibr" rid="B4">4</xref>, <xref ref-type="bibr" rid="B5">5</xref>]. Basak et al. [<xref ref-type="bibr" rid="B6">6</xref>] explained flow attributes of the fluid along with heat transfer in different zones of the enclosure by discussing the impact of the flow controlling convection Rayleigh number on momentum and temperature distributions <italic>via</italic> streamlines and isothermal contours, respectively. An innovative approach known as the heat line approach was introduced by Basak [<xref ref-type="bibr" rid="B7">7</xref>] to measure free convection in a trapezoidal enclosure. The heat transmission mechanism produced by uniform heat sources at boundaries by implementing the computational approach was addressed by Oztop et al. [<xref ref-type="bibr" rid="B8">8</xref>]. Impression of the transverse magnetic field on heat transport in a naturally convective flow of the viscous liquid was engrossed by Mahmoodi and Pour [<xref ref-type="bibr" rid="B9">9</xref>]. Convection in the isothermal flow of the viscous liquid saturated in the Darcy medium was accounted by Rehman et al. [<xref ref-type="bibr" rid="B10">10</xref>]. Jagadeesha et al. [<xref ref-type="bibr" rid="B11">11</xref>, <xref ref-type="bibr" rid="B12">12</xref>] explored the influence of tilt angle formed between sloping sides of the parallelogram cavity on convective transport by measuring flow patterns and thermal fields. They incorporated Darcy&#x2019;s law to depict the impact of permeability on flow and thermal characteristics. Sankar and his coresearchers [<xref ref-type="bibr" rid="B13">13</xref>&#x2013;<xref ref-type="bibr" rid="B16">16</xref>] adumbrated convection in the annular region by assuming different physical constraints and by employing a magnetic field and permeability aspects.</p>
<p>Polymeric natured fluids which exhibit both shear thinning and thickening attributes possess marvelous real-world applications. The characterization of such materials is identified by a variation in apparent viscosity against the magnitude of shearing rate. Intuitively, it is verified that coupling of momentum and thermal fields of such liquids in which viscosity changes point-wise has a more influential role in measuring heat transfer characteristics. Overwhelming fundamental significance of the described situations is found in reduction in heat loss from storage tanks, production of crude oil, reheating of food items, cooling of electronic components, melting and heating of polymeric pallets, and so forth. For a comprehensive mathematical disquisition of the mentioned materials, an outstanding mathematical model renowned as the power-law model is formulated. This model predicts the behavior of polymeric materials at zero and infinite stresses and describes the response of deformation rate. A number of studies pertaining to the power-law material in confined geometries with natural convection have been discussed. For instance, the impact of the Prandtl number and model parameter on thermal diffusion in the fluid along with a change in heat flux was presented by Hartnett [<xref ref-type="bibr" rid="B17">17</xref>]. Khezzar et al. [<xref ref-type="bibr" rid="B18">18</xref>] demonstrated characteristics of the power-law fluid with impersistent density by utilizing the Boussinesq approximation in a 2D cavity against the Rayleigh number. Sairamu and Chhabra [<xref ref-type="bibr" rid="B19">19</xref>] considered the quiescent power-law fluid embedded in a laminar flow enclosed in an inclined enclosure along with temperature-dependent density over a range of kinematic conditions. Mishra and Chhabra [<xref ref-type="bibr" rid="B20">20</xref>] executed analysis on a laminar convective flow of the power-law liquid with differentially heated horizontal cylinders aligned in the tandem direction. Some recent developments on non-Newtonian fluids with multiple physical aspects and in different flow generating domains are collected in Refs. [<xref ref-type="bibr" rid="B21">21</xref>&#x2013;<xref ref-type="bibr" rid="B25">25</xref>].</p>
<p>Based on thorough review about the related literature, it is explored that studies about the convectively driven flow in different configurations are abundantly available. But as far as the analysis of joint forced and free convection is concerned, especially in case of non-viscous fluid has not been done yet. So, to fill this gap, the present work is communicated and two additional thermal distributions are entertained in a comparative manner. So, to achieve this task, governing equations are structured in view of PDEs, and afterward, a finite element scheme is opted to simulate results and interpret the influence of the flow concerning on associated profiles. To the best of the authors&#x2019; knowledge, they have hoped that this work will fill the mentioned gap.</p>
</sec>
<sec id="s2">
<title>2 Mathematical modeling</title>
<p>The schematic representation of domain characterizing hydrothermal attributes of the power-law fluid enclosed in a square cavity is displayed in <xref ref-type="fig" rid="F1">Figure 1</xref>. Temperature-dependent density is assumed by incorporating the Boussinesq approximation. Shear thinning and thickening aspects of the power-law fluid against different magnitudes of the model parameter are investigated for uniformly and non-uniformly distributed thermal distribution.</p>
<fig id="F1" position="float">
<label>FIGURE 1</label>
<caption>
<p>Visualization of the enclosure with boundary constraints.</p>
</caption>
<graphic xlink:href="fphy-10-1079641-g001.tif"/>
</fig>
<p>The governing equations describing the tensorial representation of the power law are as follows. [<xref ref-type="bibr" rid="B6">6</xref>]:<disp-formula id="e1">
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<mml:mi>x</mml:mi>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:msub>
<mml:mi>u</mml:mi>
<mml:mi>y</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mn>2</mml:mn>
</mml:msup>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>n</mml:mi>
<mml:mo>&#x2212;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mn>2</mml:mn>
</mml:mfrac>
</mml:msup>
</mml:mrow>
</mml:math>
<label>(5)</label>
</disp-formula>
<disp-formula id="e6">
<mml:math id="m6">
<mml:mrow>
<mml:mi>&#x3c1;</mml:mi>
<mml:msub>
<mml:mi>C</mml:mi>
<mml:mi>p</mml:mi>
</mml:msub>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>u</mml:mi>
<mml:msub>
<mml:mi>T</mml:mi>
<mml:mi>x</mml:mi>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:mi>v</mml:mi>
<mml:msub>
<mml:mi>T</mml:mi>
<mml:mi>y</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msub>
<mml:mi>T</mml:mi>
<mml:mrow>
<mml:mi>x</mml:mi>
<mml:mi>x</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:msub>
<mml:mi>T</mml:mi>
<mml:mrow>
<mml:mi>y</mml:mi>
<mml:mi>y</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(6)</label>
</disp-formula>
</p>
<p>Associated boundary constraints are as follows:<disp-formula id="e7">
<mml:math id="m7">
<mml:mrow>
<mml:mi>u</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>x</mml:mi>
<mml:mo>,</mml:mo>
<mml:mi>L</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:math>
<label>(7)</label>
</disp-formula>at the top horizontal wall; <inline-formula id="inf1">
<mml:math id="m8">
<mml:mrow>
<mml:mi>u</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>x</mml:mi>
<mml:mo>,</mml:mo>
<mml:mn>0</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mi>u</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>0</mml:mn>
<mml:mo>,</mml:mo>
<mml:mi>y</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mi>u</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>L</mml:mi>
<mml:mo>,</mml:mo>
<mml:mi>y</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0</mml:mn>
<mml:mo>&#x3d;</mml:mo>
<mml:mi>v</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>x</mml:mi>
<mml:mo>,</mml:mo>
<mml:mn>0</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mi>v</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>x</mml:mi>
<mml:mo>,</mml:mo>
<mml:mi>L</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mi>v</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>0</mml:mn>
<mml:mo>,</mml:mo>
<mml:mi>Y</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mi>v</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>L</mml:mi>
<mml:mo>,</mml:mo>
<mml:mi>y</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
</inline-formula> at other walls; <inline-formula id="inf2">
<mml:math id="m9">
<mml:mrow>
<mml:mi>T</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>x</mml:mi>
<mml:mo>,</mml:mo>
<mml:mn>0</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula> or <inline-formula id="inf3">
<mml:math id="m10">
<mml:mrow>
<mml:mi>T</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>x</mml:mi>
<mml:mo>,</mml:mo>
<mml:mn>0</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mi mathvariant="italic">sin</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mi>&#x3c0;</mml:mi>
<mml:mi>x</mml:mi>
</mml:mrow>
<mml:mi>L</mml:mi>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
</inline-formula> at the bottom horizontal wall;<disp-formula id="e8">
<mml:math id="m11">
<mml:mrow>
<mml:mi>T</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>0</mml:mn>
<mml:mo>,</mml:mo>
<mml:mi>y</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0</mml:mn>
<mml:mo>&#x3d;</mml:mo>
<mml:mi>T</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>L</mml:mi>
<mml:mo>,</mml:mo>
<mml:mi>y</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(8)</label>
</disp-formula>at the side vertical walls; and <inline-formula id="inf4">
<mml:math id="m12">
<mml:mrow>
<mml:msub>
<mml:mi>T</mml:mi>
<mml:mi>y</mml:mi>
</mml:msub>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>x</mml:mi>
<mml:mo>,</mml:mo>
<mml:mi>L</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula> at the top horizontal wall.</p>
<p>The defined equations in Eqs. <xref ref-type="disp-formula" rid="e2">2</xref>&#x2013;<xref ref-type="disp-formula" rid="e4">4</xref> are dimensionalized by the mentioned transformation<disp-formula id="e9">
<mml:math id="m13">
<mml:mrow>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mi>x</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>L</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mo>,</mml:mo>
<mml:mtext>&#x2009;</mml:mtext>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mi>y</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>L</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mo>,</mml:mo>
<mml:mtext>&#x2009;</mml:mtext>
<mml:msup>
<mml:mi>u</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mi>u</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>U</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mo>,</mml:mo>
<mml:mtext>&#x2009;</mml:mtext>
<mml:msup>
<mml:mi>v</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mi>v</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>U</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mo>,</mml:mo>
<mml:mtext>&#x2009;</mml:mtext>
<mml:msup>
<mml:mi>&#x3b8;</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mi>T</mml:mi>
<mml:mo>&#x2212;</mml:mo>
<mml:msub>
<mml:mi>T</mml:mi>
<mml:mi>C</mml:mi>
</mml:msub>
</mml:mrow>
<mml:mrow>
<mml:msub>
<mml:mi>T</mml:mi>
<mml:mi>h</mml:mi>
</mml:msub>
<mml:mo>&#x2212;</mml:mo>
<mml:msub>
<mml:mi>T</mml:mi>
<mml:mi>c</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfrac>
<mml:mo>,</mml:mo>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mi mathvariant="normal">a</mml:mi>
<mml:mi mathvariant="normal">n</mml:mi>
<mml:mi mathvariant="normal">d</mml:mi>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mtext>&#x2009;</mml:mtext>
<mml:msup>
<mml:mi>P</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mi>P</mml:mi>
<mml:mrow>
<mml:mi>&#x3c1;</mml:mi>
<mml:msup>
<mml:mi>U</mml:mi>
<mml:mn>2</mml:mn>
</mml:msup>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:math>
<label>(9)</label>
</disp-formula>
<disp-formula id="equ1">
<mml:math id="m14">
<mml:mrow>
<mml:mi>&#x3bc;</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mi>U</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>L</mml:mi>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mrow>
<mml:mi>n</mml:mi>
<mml:mo>&#x2212;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:msup>
<mml:msup>
<mml:mi>&#x3bc;</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>.</mml:mo>
</mml:mrow>
</mml:math>
</disp-formula>
</p>
<p>Eqs. <xref ref-type="disp-formula" rid="e1">1</xref>&#x2013;<xref ref-type="disp-formula" rid="e10">10</xref> are reduced to non-dimensionalized representation<disp-formula id="e10">
<mml:math id="m15">
<mml:mrow>
<mml:msubsup>
<mml:mi>u</mml:mi>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x2a;</mml:mo>
</mml:msubsup>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mo>&#x2b;</mml:mo>
<mml:msubsup>
<mml:mi>v</mml:mi>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x2a;</mml:mo>
</mml:msubsup>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0</mml:mn>
</mml:mrow>
</mml:math>
<label>(10)</label>
</disp-formula>
<disp-formula id="e11">
<mml:math id="m16">
<mml:mrow>
<mml:msup>
<mml:mi>u</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:msubsup>
<mml:mi>u</mml:mi>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x2a;</mml:mo>
</mml:msubsup>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mo>&#x2b;</mml:mo>
<mml:msup>
<mml:mi>v</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:msubsup>
<mml:mi>u</mml:mi>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x2a;</mml:mo>
</mml:msubsup>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mo>&#x3d;</mml:mo>
<mml:mo>&#x2212;</mml:mo>
<mml:msubsup>
<mml:mi>P</mml:mi>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x2a;</mml:mo>
</mml:msubsup>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mo>&#x2b;</mml:mo>
<mml:mfrac>
<mml:mn>1</mml:mn>
<mml:mrow>
<mml:mi mathvariant="normal">R</mml:mi>
<mml:mi mathvariant="normal">e</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mrow>
<mml:mfenced open="[" close="]" separators="|">
<mml:mrow>
<mml:mn>2</mml:mn>
<mml:mfrac>
<mml:mo>&#x2202;</mml:mo>
<mml:mrow>
<mml:mo>&#x2202;</mml:mo>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
</mml:mrow>
</mml:mfrac>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:msup>
<mml:mi>&#x3bc;</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
</mml:mrow>
<mml:mrow>
<mml:mi>m</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:msubsup>
<mml:mi>u</mml:mi>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x2a;</mml:mo>
</mml:msubsup>
<mml:mtext>&#x2009;</mml:mtext>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x2b;</mml:mo>
<mml:mfrac>
<mml:mo>&#x2202;</mml:mo>
<mml:mrow>
<mml:mo>&#x2202;</mml:mo>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
</mml:mrow>
</mml:mfrac>
<mml:mrow>
<mml:mfenced open="{" close="}" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:msup>
<mml:mi>&#x3bc;</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
</mml:mrow>
<mml:mrow>
<mml:mi>m</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msubsup>
<mml:mi>u</mml:mi>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x2a;</mml:mo>
</mml:msubsup>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mo>&#x2b;</mml:mo>
<mml:msubsup>
<mml:mi>v</mml:mi>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x2a;</mml:mo>
</mml:msubsup>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mtext>&#x2009;</mml:mtext>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(11)</label>
</disp-formula>
<disp-formula id="e12">
<mml:math id="m17">
<mml:mrow>
<mml:msup>
<mml:mi>u</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:msubsup>
<mml:mi>v</mml:mi>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x2a;</mml:mo>
</mml:msubsup>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mo>&#x2b;</mml:mo>
<mml:msup>
<mml:mi>v</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:msubsup>
<mml:mi>v</mml:mi>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x2a;</mml:mo>
</mml:msubsup>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mo>&#x3d;</mml:mo>
<mml:mo>&#x2212;</mml:mo>
<mml:msubsup>
<mml:mi>P</mml:mi>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x2a;</mml:mo>
</mml:msubsup>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mo>&#x2b;</mml:mo>
<mml:mfrac>
<mml:mn>1</mml:mn>
<mml:mrow>
<mml:mi mathvariant="normal">R</mml:mi>
<mml:mi mathvariant="normal">e</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mrow>
<mml:mfenced open="[" close="]" separators="|">
<mml:mrow>
<mml:mn>2</mml:mn>
<mml:mfrac>
<mml:mo>&#x2202;</mml:mo>
<mml:mrow>
<mml:mo>&#x2202;</mml:mo>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
</mml:mrow>
</mml:mfrac>
<mml:mrow>
<mml:mfenced open="{" close="}" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:msup>
<mml:mi>&#x3bc;</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
</mml:mrow>
<mml:mrow>
<mml:mi>m</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msubsup>
<mml:mi>v</mml:mi>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x2a;</mml:mo>
</mml:msubsup>
<mml:mtext>&#x2009;</mml:mtext>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x2b;</mml:mo>
<mml:mfrac>
<mml:mo>&#x2202;</mml:mo>
<mml:mrow>
<mml:mo>&#x2202;</mml:mo>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
</mml:mrow>
</mml:mfrac>
<mml:mrow>
<mml:mfenced open="{" close="}" separators="|">
<mml:mrow>
<mml:msup>
<mml:mi>&#x3bc;</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msubsup>
<mml:mi>u</mml:mi>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x2a;</mml:mo>
</mml:msubsup>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mo>&#x2b;</mml:mo>
<mml:msubsup>
<mml:mi>v</mml:mi>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x2a;</mml:mo>
</mml:msubsup>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mtext>&#x2009;</mml:mtext>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x2b;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
<mml:msup>
<mml:mrow>
<mml:mi mathvariant="normal">R</mml:mi>
<mml:mi mathvariant="normal">e</mml:mi>
</mml:mrow>
<mml:mn>2</mml:mn>
</mml:msup>
</mml:mfrac>
<mml:msup>
<mml:mi>&#x3b8;</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
</mml:mrow>
</mml:math>
<label>(12)</label>
</disp-formula>
<disp-formula id="e13">
<mml:math id="m18">
<mml:mrow>
<mml:msup>
<mml:mi>u</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:msubsup>
<mml:mi>&#x3b8;</mml:mi>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x2a;</mml:mo>
</mml:msubsup>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mo>&#x2b;</mml:mo>
<mml:msup>
<mml:mi>v</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:msubsup>
<mml:mi>&#x3b8;</mml:mi>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x2a;</mml:mo>
</mml:msubsup>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mn>1</mml:mn>
<mml:mrow>
<mml:mi mathvariant="normal">P</mml:mi>
<mml:mi mathvariant="normal">r</mml:mi>
<mml:mi mathvariant="normal">R</mml:mi>
<mml:mi mathvariant="normal">e</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msubsup>
<mml:mi>&#x3b8;</mml:mi>
<mml:mrow>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
</mml:mrow>
<mml:mo>&#x2a;</mml:mo>
</mml:msubsup>
<mml:mo>&#x2b;</mml:mo>
<mml:msubsup>
<mml:mi>&#x3b8;</mml:mi>
<mml:mrow>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
</mml:mrow>
<mml:mo>&#x2a;</mml:mo>
</mml:msubsup>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mtext>&#x2009;</mml:mtext>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>.</mml:mo>
</mml:mrow>
</mml:math>
<label>(13)</label>
</disp-formula>
</p>
<p>Boundary constraints in a dimensionless form are given as follows:</p>
<p>
<inline-formula id="inf5">
<mml:math id="m19">
<mml:mrow>
<mml:msup>
<mml:mi>u</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>,</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula> at the top horizontal wall;<disp-formula id="e14">
<mml:math id="m20">
<mml:mrow>
<mml:msup>
<mml:mi>u</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>,</mml:mo>
<mml:mn>0</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mi>u</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>0</mml:mn>
<mml:mo>,</mml:mo>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mi>u</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>1</mml:mn>
<mml:mo>,</mml:mo>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0</mml:mn>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mi>v</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>,</mml:mo>
<mml:mn>0</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mi>v</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>,</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mi>v</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>0</mml:mn>
<mml:mo>,</mml:mo>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mi>v</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>1</mml:mn>
<mml:mo>,</mml:mo>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(14)</label>
</disp-formula>at all the solid walls; <inline-formula id="inf6">
<mml:math id="m21">
<mml:mrow>
<mml:msup>
<mml:mi>&#x3b8;</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>,</mml:mo>
<mml:mn>0</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula> or <inline-formula id="inf7">
<mml:math id="m22">
<mml:mrow>
<mml:msup>
<mml:mi>&#x3b8;</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>,</mml:mo>
<mml:mn>0</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mi>sin</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>&#x3c0;</mml:mi>
<mml:msup>
<mml:mi>X</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
</inline-formula> at the bottom horizontal wall;<disp-formula id="e15">
<mml:math id="m23">
<mml:mrow>
<mml:msup>
<mml:mi>&#x3b8;</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>0</mml:mn>
<mml:mo>,</mml:mo>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0</mml:mn>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mi>&#x3b8;</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>1</mml:mn>
<mml:mo>,</mml:mo>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(15)</label>
</disp-formula>at the side vertical walls; And <inline-formula id="inf8">
<mml:math id="m24">
<mml:mrow>
<mml:msubsup>
<mml:mi>&#x3b8;</mml:mi>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x2a;</mml:mo>
</mml:msubsup>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msup>
<mml:mi>Y</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>,</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula> at the top horizontal wall.</p>
<p>The involved physical variables in the analysis are represented as follows:<disp-formula id="e16">
<mml:math id="m25">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:msub>
<mml:mi>U</mml:mi>
<mml:mrow>
<mml:mi>L</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>d</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mtext>&#xa0;</mml:mtext>
<mml:mi>L</mml:mi>
</mml:mrow>
<mml:mi>&#x3bd;</mml:mi>
</mml:mfrac>
<mml:mo>,</mml:mo>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mi>g</mml:mi>
<mml:mi>&#x3b2;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msub>
<mml:mi>T</mml:mi>
<mml:mi>h</mml:mi>
</mml:msub>
<mml:mo>&#x2212;</mml:mo>
<mml:msub>
<mml:mi>T</mml:mi>
<mml:mi>c</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:msup>
<mml:mi>L</mml:mi>
<mml:mn>3</mml:mn>
</mml:msup>
</mml:mrow>
<mml:msup>
<mml:mi>&#x3bd;</mml:mi>
<mml:mn>2</mml:mn>
</mml:msup>
</mml:mfrac>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mi mathvariant="normal">a</mml:mi>
<mml:mi mathvariant="normal">n</mml:mi>
<mml:mi mathvariant="normal">d</mml:mi>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mi>Pr</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mi>&#x3bd;</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>&#x3b1;</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mo>.</mml:mo>
</mml:mrow>
</mml:math>
<label>(16)</label>
</disp-formula>
</p>
<p>Global quantity of interest named as the Nusselt number is also computed as follows:<disp-formula id="e17">
<mml:math id="m26">
<mml:mrow>
<mml:mi>N</mml:mi>
<mml:mi>u</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mrow>
<mml:mfenced open="" close="|" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2202;</mml:mo>
<mml:mi>&#x3b8;</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mo>&#x2202;</mml:mo>
<mml:mi>n</mml:mi>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mrow>
<mml:mi>w</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>l</mml:mi>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mi mathvariant="normal">a</mml:mi>
<mml:mi mathvariant="normal">n</mml:mi>
<mml:mi mathvariant="normal">d</mml:mi>
<mml:mtext>&#x2009;</mml:mtext>
<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>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mn>1</mml:mn>
</mml:mrow>
<mml:mrow>
<mml:mi>L</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mrow>
<mml:munderover>
<mml:mstyle displaystyle="true">
<mml:mo>&#x222b;</mml:mo>
</mml:mstyle>
<mml:mn>0</mml:mn>
<mml:mi>L</mml:mi>
</mml:munderover>
<mml:mrow>
<mml:mi>N</mml:mi>
<mml:mi>u</mml:mi>
<mml:mi>d</mml:mi>
<mml:mi>S</mml:mi>
<mml:mo>.</mml:mo>
</mml:mrow>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(17)</label>
</disp-formula>
</p>
</sec>
<sec id="s3">
<title>3 Computational procedure</title>
<p>Analytical methods are unable to solve the resultant model differential equations attained for complex engineering problems, especially in view of the mixed convection problem discussed in the current study that contains non-linear complexity in both momentum and temperature equations. In addition, singularity is also generated at the boundary of the domain. So, execution of computational approaches such as finite volume, finite element, and finite difference are considered to be the fittest to attain the approximate solution [<xref ref-type="bibr" rid="B26">26</xref>&#x2013;<xref ref-type="bibr" rid="B29">29</xref>]. Among this, the most flexible and rapid technique is the finite element scheme. To resolve the complexly structured problem first, discretization of the domain is performed by executing hp-refinement. Since the current problem is in 2D, the completed domain is distributed in the form triangular and rectangular elements as shown in <xref ref-type="fig" rid="F2">Figure 2</xref> and <xref ref-type="table" rid="T1">Table 1</xref>. Afterward, by using the Lagrange interpolation formula shape function, defining the behavior of field variables at each node is obliged. Here, the quadratic shape function consisting of piece-wise continuous second-degree polynomial for velocity and temperature is opted, whereas pressure is approximated by linear polynomial. After the selection of suitable shape functions, discretization of the governing differential system by employing a weak formulation variational procedure is capitalized and element level equations are formed. With the help of the decided shape function, the construction of basic functions is controlled. Afterward, the associated boundary conditions are loaded in the governing equations and the system of non-linear equations is developed. After that, Newton&#x2019;s approach is used to linearize non-linearized expressions, and the resulting linear system of equations is solved directly using an elimination-based method with a unique rearrangement of unknowns. The calculations scheme is shown in <xref ref-type="fig" rid="F3">Figure 3</xref>.</p>
<fig id="F2" position="float">
<label>FIGURE 2</label>
<caption>
<p>Domain discretization at the coarser level.</p>
</caption>
<graphic xlink:href="fphy-10-1079641-g002.tif"/>
</fig>
<table-wrap id="T1" position="float">
<label>TABLE 1</label>
<caption>
<p>Mesh statistics at different refinement levels.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Refinement level</th>
<th align="center">&#x23;E</th>
<th align="center">DOF</th>
<th align="center">Triangle</th>
<th align="center">Quad</th>
<th align="center">Edge element</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">Extremely coarse</td>
<td align="center">192</td>
<td align="center">580</td>
<td align="center">128</td>
<td align="center">64</td>
<td align="center">32</td>
</tr>
<tr>
<td align="center">Extra coarse</td>
<td align="center">342</td>
<td align="center">976</td>
<td align="center">246</td>
<td align="center">96</td>
<td align="center">48</td>
</tr>
<tr>
<td align="center">Coarser</td>
<td align="center">538</td>
<td align="center">1440</td>
<td align="center">418</td>
<td align="center">120</td>
<td align="center">60</td>
</tr>
<tr>
<td align="center">Coarse</td>
<td align="center">1002</td>
<td align="center">2560</td>
<td align="center">818</td>
<td align="center">184</td>
<td align="center">92</td>
</tr>
<tr>
<td align="center">Normal</td>
<td align="center">1492</td>
<td align="center">3684</td>
<td align="center">1260</td>
<td align="center">232</td>
<td align="center">116</td>
</tr>
<tr>
<td align="center">Fine</td>
<td align="center">2516</td>
<td align="center">5900</td>
<td align="center">2228</td>
<td align="center">288</td>
<td align="center">144</td>
</tr>
<tr>
<td align="center">Finer</td>
<td align="center">6636</td>
<td align="center">15124</td>
<td align="center">6020</td>
<td align="center">616</td>
<td align="center">308</td>
</tr>
<tr>
<td align="center">Extra fine</td>
<td align="center">16952</td>
<td align="center">37508</td>
<td align="center">15752</td>
<td align="center">1200</td>
<td align="center">600</td>
</tr>
<tr>
<td align="center">Extremely fine</td>
<td align="center">26212</td>
<td align="center">56028</td>
<td align="center">25012</td>
<td align="center">1200</td>
<td align="center">600</td>
</tr>
</tbody>
</table>
</table-wrap>
<fig id="F3" position="float">
<label>FIGURE 3</label>
<caption>
<p>Representation of steps in the computational scheme.</p>
</caption>
<graphic xlink:href="fphy-10-1079641-g003.tif"/>
</fig>
</sec>
<sec id="s4">
<title>4 Results and interpretation</title>
<p>The effect of flow controlling parameters on velocity and temperature distributions in view of the streamline and isotherm representation is discussed in this portion. Since, in the present problem, a mixed convection is assumed, which is produced by the motion of the upper wall and uniformly/non-uniformly heated base wall, it is analyzed against the Reynolds number (Ra) and Grashof number. In addition, different cases of the power-law index (n) are taken into account which represents shear thinning and thickening properties of the fluid.</p>
<sec id="s4-1">
<title>4.1 Program validation and comparison test</title>
<p>To assure the accuracy and credibility of the implemented computation scheme, it is validated with results published by Basak et al. [<xref ref-type="bibr" rid="B6">6</xref>] by restricting the present problem to a Newtonian case for <italic>n</italic> &#x3d; 1 as shown in <xref ref-type="fig" rid="F4">Figure 4</xref>. Here, streamlines and isotherms are generated by fixing <inline-formula id="inf9">
<mml:math id="m27">
<mml:mrow>
<mml:mi mathvariant="italic">Pr</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.7</mml:mn>
<mml:mo>,</mml:mo>
<mml:mtext>&#xa0;</mml:mtext>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1.0</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>, and <inline-formula id="inf10">
<mml:math id="m28">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>3</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>. From the displayed sketches, a complete match of results is seen, which develops the trust of readers to consider the present study as a reference.</p>
<fig id="F4" position="float">
<label>FIGURE 4</label>
<caption>
<p>Comparison of results with the outcome published by Basak et al. [<xref ref-type="bibr" rid="B6">6</xref>].</p>
</caption>
<graphic xlink:href="fphy-10-1079641-g004.tif"/>
</fig>
<p>The effectiveness of the Grashof number <inline-formula id="inf11">
<mml:math id="m29">
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:math>
</inline-formula> on momentum distribution is given by considering vast range varying from 10<sup>3</sup> to 10<sup>5</sup> and providing other parameters with fixed values such as <inline-formula id="inf12">
<mml:math id="m30">
<mml:mrow>
<mml:mi mathvariant="italic">Pr</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.015</mml:mn>
<mml:mo>,</mml:mo>
<mml:mtext>&#xa0;</mml:mtext>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1.0</mml:mn>
<mml:mo>,</mml:mo>
</mml:mrow>
</mml:math>
</inline-formula> and <inline-formula id="inf13">
<mml:math id="m31">
<mml:mrow>
<mml:mi>n</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.8</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>. From the illustrated sketch (in <xref ref-type="fig" rid="F5">Figures 5A&#x2013;C</xref>), it is noticed that due to the increase in <italic>Gr</italic>, velocity change in the domain is dependent on buoyancy forces. In addition, <italic>Re</italic> is assumed to be 1 which shows no influence of inertial forces. It is also observed that at <italic>Gr</italic> &#x3d; 10<sup>3</sup> and 10<sup>4</sup>, two primary vortices are formed in which fluids are moving in clockwise and anti-clock wise directions. However, at <italic>Gr</italic> &#x3d; 10<sup>5</sup>, the secondary vortex disappears and the fluid starts moving in a single circular vortex. The reason behind this impact is that by increasing <italic>Gr</italic>, viscosity of the fluid decreases due to which the movement of particles raises, which is evident from the mathematical relation, that is, <inline-formula id="inf14">
<mml:math id="m32">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mi>g</mml:mi>
<mml:mi>&#x3b2;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msub>
<mml:mi>T</mml:mi>
<mml:mi>h</mml:mi>
</mml:msub>
<mml:mo>&#x2212;</mml:mo>
<mml:msub>
<mml:mi>T</mml:mi>
<mml:mi>c</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:msup>
<mml:mi>L</mml:mi>
<mml:mn>3</mml:mn>
</mml:msup>
</mml:mrow>
<mml:msup>
<mml:mi>&#x3bd;</mml:mi>
<mml:mn>2</mml:mn>
</mml:msup>
</mml:mfrac>
<mml:mo>.</mml:mo>
</mml:mrow>
</mml:math>
</inline-formula>
</p>
<fig id="F5" position="float">
<label>FIGURE 5</label>
<caption>
<p>Influence of <inline-formula id="inf15">
<mml:math id="m33">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> on streamlines for the uniform heated case: <bold>(A)</bold> <inline-formula id="inf16">
<mml:math id="m34">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>3</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>, <bold>(B)</bold> <inline-formula id="inf17">
<mml:math id="m35">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>4</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>, and <bold>(C)</bold> <inline-formula id="inf18">
<mml:math id="m36">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>5</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>.</p>
</caption>
<graphic xlink:href="fphy-10-1079641-g005.tif"/>
</fig>
<p>Change in the temperature profile versus the Grashof number <inline-formula id="inf19">
<mml:math id="m37">
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:math>
</inline-formula> in view of isothermal patterns is addressed in <xref ref-type="fig" rid="F6">Figures 6A&#x2013;C</xref>. During the simulations, <italic>Gr</italic> is varied between <inline-formula id="inf20">
<mml:math id="m38">
<mml:mrow>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>3</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula> and <inline-formula id="inf21">
<mml:math id="m39">
<mml:mrow>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>5</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula> and other concerning parameters are fixed at <inline-formula id="inf22">
<mml:math id="m40">
<mml:mrow>
<mml:mi mathvariant="italic">Pr</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.015</mml:mn>
<mml:mo>,</mml:mo>
<mml:mtext>&#xa0;</mml:mtext>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1.000</mml:mn>
<mml:mo>,</mml:mo>
</mml:mrow>
</mml:math>
</inline-formula> and <inline-formula id="inf23">
<mml:math id="m41">
<mml:mrow>
<mml:mi>n</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.8</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>. An important direction to observe is that in the case of uniform heating, thermal singularity is generated at the left and right most corners of the cavity due to the provision of a uniform heat source. Symmetric aptitude of the isotherm is adhered to in the case of <italic>Gr</italic> &#x3d; <inline-formula id="inf24">
<mml:math id="m42">
<mml:mrow>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>3</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula> and <inline-formula id="inf25">
<mml:math id="m43">
<mml:mrow>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>4</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>, whereas the deviation in the pattern is attained at <italic>Gr</italic> &#x3d; <inline-formula id="inf26">
<mml:math id="m44">
<mml:mrow>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>5</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula> in the middle line. The reason behind this behavior is that at <italic>Gr</italic> &#x3d; <inline-formula id="inf27">
<mml:math id="m45">
<mml:mrow>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>5</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>, the production of the temperature gradient exemplifies due to which the transmission of heat from the hotter zone to the colder one increases and the symmetricity is disturbed.</p>
<fig id="F6" position="float">
<label>FIGURE 6</label>
<caption>
<p>Influence of <italic>Gr</italic> on temperature distribution for the uniform heating case: <bold>(A)</bold> <inline-formula id="inf28">
<mml:math id="m46">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>3</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>, <bold>(B)</bold> <inline-formula id="inf29">
<mml:math id="m47">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>4</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>, and <bold>(C)</bold> <inline-formula id="inf30">
<mml:math id="m48">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>5</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>.</p>
</caption>
<graphic xlink:href="fphy-10-1079641-g006.tif"/>
</fig>
<p>The dominating role of the Reynolds number (<italic>Re</italic>) in controlling lid-driven forces and in managing the phenomenon of mixed convection is explicated in <xref ref-type="fig" rid="F7">Figures 7A&#x2013;C</xref>. In this sketch, streamlines are represented against variation in (<italic>Re</italic>) from 1 to 100 and with fixation of <inline-formula id="inf31">
<mml:math id="m49">
<mml:mrow>
<mml:mi mathvariant="italic">Pr</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.015</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula> and <inline-formula id="inf32">
<mml:math id="m50">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>3</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>. It is seen that at <italic>Re</italic> &#x3d; 1, the impact of natural convection dominates over forced convection due to which circulations are generated in the flow domain. But by increasing the magnitude of <italic>Re</italic> from 10 to 100, the effectiveness of inertial forces is dominated due to which the movement of the fluid near the upper lid is generated. Maximum velocity of the fluid is attained near the upper wall due to the movement of the wall and only primary vortex are generated. In the case of <italic>Re</italic> &#x3d; 100, the role of inertial forces dominates over buoyancy forces due to which again a similar trend is observed as in the case of <italic>Re</italic> &#x3d; 10.</p>
<fig id="F7" position="float">
<label>FIGURE 7</label>
<caption>
<p>Influence of <italic>Re</italic> on streamlines for the uniform heating case: <bold>(A)</bold> <inline-formula id="inf33">
<mml:math id="m51">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1.000</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>, <bold>(B)</bold> <inline-formula id="inf34">
<mml:math id="m52">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>10.00</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>, and <bold>(C)</bold> <inline-formula id="inf35">
<mml:math id="m53">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>100.0</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>.</p>
</caption>
<graphic xlink:href="fphy-10-1079641-g007.tif"/>
</fig>
<p>The description of the thermal distribution against the Reynolds number (Re) with <inline-formula id="inf36">
<mml:math id="m54">
<mml:mrow>
<mml:mi mathvariant="italic">Pr</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.015</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula> and <inline-formula id="inf37">
<mml:math id="m55">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>3</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula> is evaluated in <xref ref-type="fig" rid="F8">Figure 8</xref> for uniform heating. No obvious change in isotherms is depicted at each magnitude of <italic>Re</italic>. This justifies the fact that for the production of convection in the domain, the role of the Prandtl number cannot be neglected.</p>
<fig id="F8" position="float">
<label>FIGURE 8</label>
<caption>
<p>Influence of <italic>Re</italic> on the temperature profile for the uniform heating case: <bold>(A)</bold> <inline-formula id="inf38">
<mml:math id="m56">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1.000</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>, <bold>(B)</bold> <inline-formula id="inf39">
<mml:math id="m57">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>10.00</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>, and <bold>(C)</bold> <inline-formula id="inf40">
<mml:math id="m58">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>100.0</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>.</p>
</caption>
<graphic xlink:href="fphy-10-1079641-g008.tif"/>
</fig>
<p>The effect of incrementing magnitude of the Prandtl number (Pr) on velocity distribution is seen in <xref ref-type="fig" rid="F9">Figures 9A&#x2013;C</xref>. Here, <inline-formula id="inf41">
<mml:math id="m59">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>3</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>, <inline-formula id="inf42">
<mml:math id="m60">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>, and <italic>n</italic> &#x3d; 0.8 are managed and the situation of uniform heating is accounted. Since the Prandtl number (Pr) shows the significant ratio of momentum to thermal diffusivities and plays a vital role in diffusion control, this figure is displayed. From the exhibited graphs, it is observed that vortices squeeze at <italic>Pr</italic> &#x3d; 10 due to the huge production of momentum diffusivity.</p>
<fig id="F9" position="float">
<label>FIGURE 9</label>
<caption>
<p>Influence of <italic>Pr</italic> on streamlines for the uniform heating case: <bold>(A)</bold> <inline-formula id="inf43">
<mml:math id="m61">
<mml:mrow>
<mml:mi mathvariant="italic">Pr</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.015</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>, <bold>(B)</bold> <inline-formula id="inf44">
<mml:math id="m62">
<mml:mrow>
<mml:mi mathvariant="italic">Pr</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.7</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>, and <bold>(C)</bold> <inline-formula id="inf45">
<mml:math id="m63">
<mml:mrow>
<mml:mi mathvariant="italic">Pr</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>10</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>.</p>
</caption>
<graphic xlink:href="fphy-10-1079641-g009.tif"/>
</fig>
<p>Discussion about the impact of Pr on the thermal profile for uniform heat distribution through isothermal plots is addressed in <xref ref-type="fig" rid="F10">Figures 10A&#x2013;C</xref>. It is revealed that symmetricity of lines is immensely disturbed when the Prandtl number increases from 0.015 to 10. At lower magnitude of Pr, that is, at 0.015, the thermal diffusion is maximum and heat generated from the bottom wall due to uniform heat supply. In addition, it is seen that the magnitude of heat transferred in the case of <italic>Pr</italic> &#x3d; 10 is more due to uplift in momentum diffusivity, due to which the kinetic energy of particles increases. Attachment of isotherms with boundaries is seen at a larger magnitude of <italic>Pr</italic>.</p>
<fig id="F10" position="float">
<label>FIGURE 10</label>
<caption>
<p>Influence of <italic>Pr</italic> on temperature distribution for the uniform heating case: <bold>(A)</bold> <inline-formula id="inf46">
<mml:math id="m64">
<mml:mrow>
<mml:mi mathvariant="italic">Pr</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.015</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>, <bold>(B)</bold> <inline-formula id="inf47">
<mml:math id="m65">
<mml:mrow>
<mml:mi mathvariant="italic">Pr</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.700</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>, and <bold>(C)</bold> <inline-formula id="inf48">
<mml:math id="m66">
<mml:mrow>
<mml:mi mathvariant="italic">Pr</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>10.00</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>.</p>
</caption>
<graphic xlink:href="fphy-10-1079641-g010.tif"/>
</fig>
<p>The velocity distribution in assistance with the streamline pattern against the Grashof number (Gr) is probed in <xref ref-type="fig" rid="F11">Figures 11A&#x2013;C</xref>. A wide range of <italic>Gr</italic> is selected from <inline-formula id="inf49">
<mml:math id="m67">
<mml:mrow>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>3</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula> to <inline-formula id="inf50">
<mml:math id="m68">
<mml:mrow>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>5</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>, <italic>Re</italic> is fixed at 1, and the power-law index (n) is kept constant at 0.5. Unlike the variation in the velocity profile against <italic>Gr</italic> in the case of uniform heating, here, the behavior is quite different. Here, it is revealed that primary and secondary vortices remain intact and move toward the upper wall. It shows that even at <italic>Re</italic> &#x3d; 1, the role of inertial forces is also present, which seems to be neglected in the case of uniform heating. It adheres that buoyancy forces are still dominant over inertial forces with an increase in <italic>Gr</italic>. This fact is proved by the reason that an increment in <italic>Gr</italic> causes the viscosity to reduce and less resistance will be offered to the molecules.</p>
<fig id="F11" position="float">
<label>FIGURE 11</label>
<caption>
<p>Influence of <italic>Gr</italic> on streamlines for the non-uniform heating case: <bold>(A)</bold> <inline-formula id="inf51">
<mml:math id="m69">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>3</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>, <bold>(B)</bold> <inline-formula id="inf52">
<mml:math id="m70">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>4</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>, and <bold>(C)</bold> <inline-formula id="inf53">
<mml:math id="m71">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>5</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>.</p>
</caption>
<graphic xlink:href="fphy-10-1079641-g011.tif"/>
</fig>
<p>The temperature distribution against <italic>Gr</italic> by employing a non-uniform heating situation is evaluated in <xref ref-type="fig" rid="F12">Figures 12A&#x2013;C</xref> for <italic>Re</italic> &#x3d; 1, <italic>n</italic> &#x3d; 0.8, and <italic>Pr</italic> &#x3d; 0.015. It is found that isotherm intensity is indicated at <italic>Gr</italic> &#x3d; 10<sup>5</sup>, due to the production of thermal convective potential in different zones of the enclosure, which is justified by the deviation in isotherms displayed in the figure. It is also manifested that thermal singularity is removed in the case of non-uniform heating, which is produced in the situation of uniform heating. The perfect parabolic behavior of isotherms is attained at <inline-formula id="inf54">
<mml:math id="m72">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>3</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula> and <inline-formula id="inf55">
<mml:math id="m73">
<mml:mrow>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>4</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>, which discloses that heat propagated in a parabolic form from the base wall to the upper boundary.</p>
<fig id="F12" position="float">
<label>FIGURE 12</label>
<caption>
<p>Influence of <italic>Gr</italic> on temperature with non-uniform heating: <bold>(A)</bold> <inline-formula id="inf56">
<mml:math id="m74">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>3</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>, <bold>(B)</bold> <inline-formula id="inf57">
<mml:math id="m75">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>4</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>, and <bold>(C)</bold> <inline-formula id="inf58">
<mml:math id="m76">
<mml:mrow>
<mml:mi>G</mml:mi>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mn>5</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>.</p>
</caption>
<graphic xlink:href="fphy-10-1079641-g012.tif"/>
</fig>
<p>The deviation in velocity distribution against the Reynolds number (Re) is manipulated in <xref ref-type="fig" rid="F13">Figures 13A&#x2013;C</xref>. During the evaluation of this sketch, three different magnitudes of <italic>Re</italic> are taken, which shows the dominance of different regimes. At <italic>Re</italic> &#x3d; 1, the forced and free convection balances each other&#x2019;s effects and no one dominates the other, whereas at <italic>Re</italic> &#x3d; 10, the impact of natural convection dominates over forced convection, but in the case of <italic>Re</italic> &#x3d; 100, forced convection effects on flow characteristics are more than the free convection regime. From the plots, it is seen that maximum velocity in the flow is attained near the moved wall and zero velocity is found where no slip conditions are applied.</p>
<fig id="F13" position="float">
<label>FIGURE 13</label>
<caption>
<p>Influence of <italic>Re</italic> on streamlines for the non-uniform heating case: <bold>(A)</bold> <inline-formula id="inf59">
<mml:math id="m77">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>, <bold>(B)</bold> <inline-formula id="inf60">
<mml:math id="m78">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>10</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>, and <bold>(C)</bold> <inline-formula id="inf61">
<mml:math id="m79">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>100</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>.</p>
</caption>
<graphic xlink:href="fphy-10-1079641-g013.tif"/>
</fig>
<p>No significant change in the temperature distribution evidenced against the Reynolds number (Re) in spite of providing non-uniform heating at the base wall is illustrated in <xref ref-type="fig" rid="F14">Figures 14A&#x2013;C</xref>. This behavior is similar to the case of uniform heating. This figure shows that consideration of high <italic>Pr</italic> in the case of temperature diffusion is more valuable. Since <italic>Pr</italic> is taken as 0.015 which is much lower in magnitude, no change is observed.</p>
<fig id="F14" position="float">
<label>FIGURE 14</label>
<caption>
<p>Influence of <italic>Re</italic> on the temperature profile for the non-uniform heating case. <bold>(A)</bold> <inline-formula id="inf62">
<mml:math id="m80">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>, <bold>(B)</bold> <inline-formula id="inf63">
<mml:math id="m81">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>10</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>, <bold>(C)</bold> <inline-formula id="inf64">
<mml:math id="m82">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>100</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>.</p>
</caption>
<graphic xlink:href="fphy-10-1079641-g014.tif"/>
</fig>
<p>Streamline patterns showing change in the momentum profile against <italic>Pr</italic> is elaborated in <xref ref-type="fig" rid="F15">Figures 15A&#x2013;C</xref>. It is seen that at <italic>Pr</italic> &#x3d; 0.015 and 7, two vortices are formed, whereas at <italic>Pr</italic> &#x3d; 10, the left primary vortex squeezes and merges into the other. It is seen that maximum velocity is attained at a lower magnitude of <italic>Pr</italic> because by increasing <italic>Pr</italic>, viscosity of the fluid increases, due to which viscous force causes the fluid particles to move with less velocity.</p>
<fig id="F15" position="float">
<label>FIGURE 15</label>
<caption>
<p>Influence of <italic>Pr</italic> on streamlines for the non-uniform heating case: <bold>(A)</bold> <inline-formula id="inf65">
<mml:math id="m83">
<mml:mrow>
<mml:mi mathvariant="italic">Pr</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.015</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>, <bold>(B)</bold> <inline-formula id="inf66">
<mml:math id="m84">
<mml:mrow>
<mml:mi mathvariant="italic">Pr</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.7</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>, and <bold>(C)</bold> <inline-formula id="inf67">
<mml:math id="m85">
<mml:mrow>
<mml:mi mathvariant="italic">Pr</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>10</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>.</p>
</caption>
<graphic xlink:href="fphy-10-1079641-g015.tif"/>
</fig>
<p>Transmission of heat in an enclosure by providing non-uniform heating at the base wall was divulged against <italic>Pr</italic> in <xref ref-type="fig" rid="F16">Figures 16A&#x2013;C</xref>. An increment in <italic>Pr</italic> tends to produce more heat flux in the domain as an outcome of temperature profile upsurge. In addition, it is because of the reason that by increasing <italic>Pr</italic>, momentum diffusivity rises due to which the average kinetic energy mounts and causes a positive effect on temperature. It is worthwhile to mention that in the case of non-uniform heating, thermal discontinuity is removed.</p>
<fig id="F16" position="float">
<label>FIGURE 16</label>
<caption>
<p>Influence of <italic>Pr</italic> on temperature distribution for the non-uniform heating case: <bold>(A)</bold> <inline-formula id="inf68">
<mml:math id="m86">
<mml:mrow>
<mml:mi mathvariant="italic">Pr</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.015</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>, <bold>(B)</bold> <inline-formula id="inf69">
<mml:math id="m87">
<mml:mrow>
<mml:mi mathvariant="italic">Pr</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.700</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>, and <bold>(C)</bold> <inline-formula id="inf70">
<mml:math id="m88">
<mml:mrow>
<mml:mi mathvariant="italic">Pr</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>10.00</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>.</p>
</caption>
<graphic xlink:href="fphy-10-1079641-g016.tif"/>
</fig>
<p>The measurement of the heat flux coefficient against the Reynolds number (<italic>Re</italic>) for n &#x3d; 0.8, 1, and 1.2 and Pr &#x3d; 0.015 and 10 is discussed in <xref ref-type="fig" rid="F17">Figure 17</xref>. It is seen that for all magnitudes of <italic>Re</italic> and for <italic>n</italic> &#x3d; 1.2, no significant change in heat flux is attained, whereas at <italic>Re</italic> &#x3e; 10 and for <italic>n</italic> &#x3d; 1, elevation in heat flux is found. The reason behind this behavior is that by increasing <italic>Re</italic>, viscosity of the fluid decreases due to which the kinetic energy of molecules lifts and the associated heat energy also elevates.</p>
<fig id="F17" position="float">
<label>FIGURE 17</label>
<caption>
<p>Variation in the local Nusselt number <inline-formula id="inf71">
<mml:math id="m89">
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>N</mml:mi>
<mml:msub>
<mml:mi>u</mml:mi>
<mml:mrow>
<mml:mi>L</mml:mi>
<mml:mi>o</mml:mi>
<mml:mi>c</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:math>
</inline-formula> against the Reynolds number <inline-formula id="inf72">
<mml:math id="m90">
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:math>
</inline-formula>.</p>
</caption>
<graphic xlink:href="fphy-10-1079641-g017.tif"/>
</fig>
<p>Plotting of the average Nusselt number against <italic>Re</italic> for <italic>n</italic> &#x3c; 1 and <italic>n</italic> &#x3e; 1 along with fixation of <italic>Pr</italic> &#x3d; 0.015 and 10 is displayed in <xref ref-type="fig" rid="F18">Figure 18</xref>. It is observed that the heat flux coefficient in the case of <italic>n</italic> &#x3d; 1 is more than that for shear thickening situation (<italic>n</italic> &#x3e; 1). In addition, it is seen that for all values of <italic>n</italic>, the average Nusselt number intensifies against <italic>Re</italic>.</p>
<fig id="F18" position="float">
<label>FIGURE 18</label>
<caption>
<p>Variation in the average Nusselt number <inline-formula id="inf80">
<mml:math id="m98">
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<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:mrow>
</mml:mfenced>
</mml:mrow>
</mml:math>
</inline-formula> against the Reynolds number <inline-formula id="inf81">
<mml:math id="m99">
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:math>
</inline-formula>.</p>
</caption>
<graphic xlink:href="fphy-10-1079641-g018.tif"/>
</fig>
<p>Variation in the kinetic energy along the vertical cutline against <inline-formula id="inf73">
<mml:math id="m91">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is shown in <xref ref-type="fig" rid="F19">Figure 19</xref> for each case of <inline-formula id="inf74">
<mml:math id="m92">
<mml:mrow>
<mml:mi>n</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula>. When we increase the value of <inline-formula id="inf75">
<mml:math id="m93">
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:math>
</inline-formula> from 1 to 100, we can observe that <inline-formula id="inf76">
<mml:math id="m94">
<mml:mrow>
<mml:mi>K</mml:mi>
<mml:mo>.</mml:mo>
<mml:mi>E</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> increases abruptly. It is due to the fact that an increment in the Reynolds number <inline-formula id="inf77">
<mml:math id="m95">
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:math>
</inline-formula> causes the viscosity to reduce, and as a result, the energy due to the motion of fluid increases gradually.</p>
<fig id="F19" position="float">
<label>FIGURE 19</label>
<caption>
<p>Variation in the kinetic energy <inline-formula id="inf78">
<mml:math id="m96">
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>K</mml:mi>
<mml:mo>.</mml:mo>
<mml:mi>E</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:math>
</inline-formula> against the Reynolds number <inline-formula id="inf79">
<mml:math id="m97">
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>R</mml:mi>
<mml:mi>e</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:math>
</inline-formula>.</p>
</caption>
<graphic xlink:href="fphy-10-1079641-g019.tif"/>
</fig>
</sec>
</sec>
<sec sec-type="conclusion" id="s5">
<title>5 Conclusion</title>
<p>In this article, the authors have dedicated their efforts to investigate hydrothermal attributes of the power-law liquid in a square enclosure by incorporating the aspects of inertial and buoyancy forces. The formulation of the problem conceding the aspects of mixed convection in the non-Newtonian model is attained in the form of complex PDEs. Finite element computations are performed to resolve the coupled system of equations. The results are drawn in a graphical manner to disclose the impact of flow concerning parameters. Some key findings are itemized as follows:<list list-type="simple">
<list-item>
<p>1) Thermal singularity is removed in the case of non-uniform heating and retained in uniform heating.</p>
</list-item>
<list-item>
<p>2) At <italic>Re</italic> &#x3d; 1, the inertial forces and buoyancy forces balance each other, whereas in the case of <italic>Re</italic> &#x3d; 100, forced convection dominates over natural convection.</p>
</list-item>
<list-item>
<p>3) The local and global heat flux coefficient increases against uplift in <italic>Re</italic>.</p>
</list-item>
<list-item>
<p>4) The kinetic energy of the fluid depreciated against <italic>Re</italic>.</p>
</list-item>
<list-item>
<p>5) At a low magnitude of <italic>Pr</italic>, no significant effect of <italic>Re</italic> on the temperature distribution is seen in both cases.</p>
</list-item>
<list-item>
<p>6) In the case of a high Prandtl number (<italic>Pr</italic>), the movement of the fluid squeezes due to the uplift in the viscous diffusion.</p>
</list-item>
</list>
</p>
</sec>
</body>
<back>
<sec sec-type="data-availability" id="s6">
<title>Data availability statement</title>
<p>The original contributions presented in the study are included in the article/supplementary material, Further inquiries can be directed to the corresponding author.</p>
</sec>
<sec id="s7">
<title>Author contributions</title>
<p>All authors listed have made a substantial, direct, and intellectual contribution to the work and approved it for publication.</p>
</sec>
<ack>
<p>The authors would like to thank the Deanship of Scientific Research at Umm Al-Qura University for supporting this work by Grant Code: (22UQU4282396DSR30) (<email>sehazmi@uqu.edu.sa</email>).</p>
</ack>
<sec sec-type="COI-statement" id="s8">
<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="s9">
<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>
</sec>
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