<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd">
<article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article">
 <front>
  <journal-meta>
   <journal-id journal-id-type="publisher-id">
    jamp
   </journal-id>
   <journal-title-group>
    <journal-title>
     Journal of Applied Mathematics and Physics
    </journal-title>
   </journal-title-group>
   <issn pub-type="epub">
    2327-4352
   </issn>
   <issn publication-format="print">
    2327-4379
   </issn>
   <publisher>
    <publisher-name>
     Scientific Research Publishing
    </publisher-name>
   </publisher>
  </journal-meta>
  <article-meta>
   <article-id pub-id-type="doi">
    10.4236/jamp.2025.138150
   </article-id>
   <article-id pub-id-type="publisher-id">
    jamp-144980
   </article-id>
   <article-categories>
    <subj-group subj-group-type="heading">
     <subject>
      Articles
     </subject>
    </subj-group>
    <subj-group subj-group-type="Discipline-v2">
     <subject>
      Physics 
     </subject>
     <subject>
       Mathematics
     </subject>
    </subj-group>
   </article-categories>
   <title-group>
    Natural Convective Nanofluid Flow over a Vertical Plate with Thermal Stratification
   </title-group>
   <contrib-group>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       Md Ziarul
      </surname>
      <given-names>
       Islam
      </given-names>
     </name>
    </contrib>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       Abdullah Ahmed
      </surname>
      <given-names>
       Foisal
      </given-names>
     </name>
    </contrib>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       Afsana
      </surname>
      <given-names>
       Shila
      </given-names>
     </name>
    </contrib>
   </contrib-group> 
   <aff id="affnull">
    <addr-line>
     aDepartment of Mathematics, University of Barishal, Barishal, Bangladesh
    </addr-line> 
   </aff> 
   <pub-date pub-type="epub">
    <day>
     08
    </day> 
    <month>
     08
    </month>
    <year>
     2025
    </year>
   </pub-date> 
   <volume>
    13
   </volume> 
   <issue>
    08
   </issue>
   <fpage>
    2645
   </fpage>
   <lpage>
    2657
   </lpage>
   <history>
    <date date-type="received">
     <day>
      10,
     </day>
     <month>
      July
     </month>
     <year>
      2025
     </year>
    </date>
    <date date-type="published">
     <day>
      18,
     </day>
     <month>
      July
     </month>
     <year>
      2025
     </year> 
    </date> 
    <date date-type="accepted">
     <day>
      18,
     </day>
     <month>
      August
     </month>
     <year>
      2025
     </year> 
    </date>
   </history>
   <permissions>
    <copyright-statement>
     © Copyright 2014 by authors and Scientific Research Publishing Inc. 
    </copyright-statement>
    <copyright-year>
     2014
    </copyright-year>
    <license>
     <license-p>
      This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/
     </license-p>
    </license>
   </permissions>
   <abstract>
    Natural convective flow of nanofluid over a vertical plate in a thermally stratified porous medium has been investigated. The governing equations have been transformed using similarity variables and solved numerically using the Finite Element Method. Key parameters such as Brownian motion, thermophoresis, Darcy number, buoyancy ratio and Prandtl number have been examined. Velocity, temperature, and nanoparticle concentration profiles have been analyzed. Heat transfer and shear stress have been evaluated using Nusselt number and wall shear. It has been observed that an increase in Brownian motion enhances heat transfer while reducing wall shear stress, whereas an increase in thermophoresis enhances both heat transfer and wall shear stress. Results have been presented graphically for clarity.
   </abstract>
   <kwd-group> 
    <kwd>
     Free Convection
    </kwd> 
    <kwd>
      Nanofluid
    </kwd> 
    <kwd>
      Thermal Stratification
    </kwd> 
    <kwd>
      Brownian Motion
    </kwd> 
    <kwd>
      Thermophoresis
    </kwd>
   </kwd-group>
  </article-meta>
 </front>
 <body>
  <sec id="s1">
   <title>1. Introduction</title>
   <p>Nanofluids have recently attracted significant attention in the field of thermal management and energy conversion due to their exceptional heat transfer properties. These fluids are created by dispersing a small amount of nanoparticles—such as metal oxides, metals, or carbon-based materials—into conventional base fluids like water, ethylene glycol, or oil. The inclusion of nanoparticles dramatically improves the thermal conductivity and convective heat transfer performance of the base fluid. This makes nanofluids highly suitable for various advanced engineering applications, including cooling of electronic devices, solar energy collectors, and chemical process industries, as supported by studies such as Ahmed et al. <xref ref-type="bibr" rid="scirp.144980-1">
     [1]
    </xref> and Anuradha and Yegammai <xref ref-type="bibr" rid="scirp.144980-2">
     [2]
    </xref>. Natural convection along vertical surfaces plays a vital role in many industrial and environmental applications. When such convection occurs within a porous medium, the interaction between buoyancy forces and the resistance offered by the porous structure creates complex flow and heat transfer phenomena. These interactions are well documented by Abdullah et al. <xref ref-type="bibr" rid="scirp.144980-3">
     [3]
    </xref> and Shokrgozar Abbasi <xref ref-type="bibr" rid="scirp.144980-4">
     [4]
    </xref>. Moreover, many real-world environments exhibit thermal stratification, where the ambient temperature varies with height. This vertical temperature gradient leads to density stratification, which significantly influences buoyancy-driven flow behavior and the development of the thermal boundary layer. The effects of thermal stratification on convection within porous media have been investigated by Farooq et al. <xref ref-type="bibr" rid="scirp.144980-5">
     [5]
    </xref> and Khan et al. <xref ref-type="bibr" rid="scirp.144980-6">
     [6]
    </xref>. In addition to these effects, nanofluid flows are influenced by nanoparticle dynamics such as Brownian motion and thermophoresis—the tendency of particles to move along temperature gradients—which further modify heat and mass transfer characteristics. These phenomena are studied extensively by Promvonge et al. <xref ref-type="bibr" rid="scirp.144980-7">
     [7]
    </xref> and Shukla et al. <xref ref-type="bibr" rid="scirp.144980-8">
     [8]
    </xref>. The governing partial differential equations for momentum, energy, and nanoparticle volume fraction were transformed using suitable non-similar variables, resulting in a system of coupled partial differential equations. This method assumes that flow properties vary similarly along the surface, allowing the spatial coordinate along the plate to be combined with the transverse coordinate. However, this approach can mask important spatial variations in boundary-layer thickness and heat transfer rates, particularly in complex situations like thermal stratification. To overcome these limitations, non-similar solution methods are employed, which retain the dependence on the streamwise coordinate and capture detailed spatial variations, as used by Chamkha and Gorla <xref ref-type="bibr" rid="scirp.144980-9">
     [9]
    </xref>, Semarakilmu <xref ref-type="bibr" rid="scirp.144980-10">
     [10]
    </xref>, Srinivasacharya and Surender <xref ref-type="bibr" rid="scirp.144980-11">
     [11]
    </xref> and Anwar Bég et al. <xref ref-type="bibr" rid="scirp.144980-12">
     [12]
    </xref>. In this study, the governing equations describing momentum, energy, and nanoparticle volume fraction are formulated into a coupled system of nonlinear differential equations that preserve non-similar characteristics. To solve these complex equations, the finite element method (FEM) is employed. FEM is a powerful numerical technique widely used for solving partial differential equations in engineering and physical sciences due to its flexibility and accuracy in handling complex geometries and boundary conditions. The numerical simulations cover a range of important dimensionless parameters, including the Brownian motion parameter, thermophoresis parameter, Darcy number representing porous medium permeability, buoyancy ratio parameter, and the Prandtl number, following the approaches of Ferdows and Alzahrani <xref ref-type="bibr" rid="scirp.144980-13">
     [13]
    </xref> and Duwairi and Naji <xref ref-type="bibr" rid="scirp.144980-14">
     [14]
    </xref>. From the numerical results, detailed profiles of velocity and temperature fields are obtained, allowing calculation of key physical quantities such as the local Nusselt number, which measures heat transfer efficiency, and wall shear stress, which relates to momentum transfer. These results align with previous studies by Jafarimoghaddam <xref ref-type="bibr" rid="scirp.144980-15">
     [15]
    </xref> and Nawaz and Khan <xref ref-type="bibr" rid="scirp.144980-16">
     [16]
    </xref>.</p>
   <p>By systematically studying the influence of these parameters, this work aims to enhance understanding of the combined heat and mass transfer processes in nanofluid flows under thermal stratification within porous media. The insights gained can support the design and optimization of thermal management systems and energy devices that utilize nanofluids, consistent with the findings of Ali and Al-Mubaddel <xref ref-type="bibr" rid="scirp.144980-17">
     [17]
    </xref>, Rashad et al. <xref ref-type="bibr" rid="scirp.144980-18">
     [18]
    </xref>, Chamkha et al. <xref ref-type="bibr" rid="scirp.144980-19">
     [19]
    </xref>, and Mahdy <xref ref-type="bibr" rid="scirp.144980-20">
     [20]
    </xref>.</p>
  </sec><sec id="s2">
   <title>2. Mathematical Formulation</title>
   <p>This study investigates steady, two-dimensional, laminar natural convection boundary layer flow of an incompressible nanofluid over a vertical plate embedded in a thermally stratified porous medium. The x-axis is taken along the plate (in the upward direction), and the y-axis is normal to it, with the origin at the leading edge.</p>
   <p>
    <xref ref-type="bibr" rid="scirp.144980-"></xref>The vertical plate is maintained at a constant surface temperature 
    <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
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    </math>, both higher than the corresponding ambient values. The surrounding porous medium is assumed to be isotropic, homogeneous, and saturated with the nanofluid. The ambient temperature is vertically stratified and varies linearly with 
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   <sec id="s2_1">
    <title>2.1. Governing Equations</title>
    <p>The nanofluid properties are constant except for the density, which varies with temperature in the buoyancy term according to the Boussinesq approximation. Applying standard boundary layer approximations, the governing equations for conservation of mass, momentum, energy, and nanoparticle volume fraction are derived. These equations account for Darcy resistance, Brownian motion, thermophoresis, and thermal stratification effects and are solved subject to appropriate boundary conditions at the plate surface and far from the wall.</p>
    <p>
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          <mn>
            2 
          </mn> 
         </msup> 
        </mrow> 
       </mfrac> 
      </mrow> 
     </math> (4)</p>
    <p>The Boundary Conditions are:</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         y 
       </mi> 
       <mo>
         → 
       </mo> 
       <mn>
         0 
       </mn> 
      </mrow> 
     </math>:</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         u 
       </mi> 
       <mo>
         = 
       </mo> 
       <mn>
         0 
       </mn> 
       <mo>
         , 
       </mo> 
       <mtext>
           
       </mtext> 
       <mtext>
           
       </mtext> 
       <mi>
         v 
       </mi> 
       <mo>
         = 
       </mo> 
       <mn>
         0 
       </mn> 
       <mo>
         , 
       </mo> 
       <mtext>
           
       </mtext> 
       <mtext>
           
       </mtext> 
       <mi>
         T 
       </mi> 
       <mo>
         = 
       </mo> 
       <msub> 
        <mi>
          T 
        </mi> 
        <mi>
          w 
        </mi> 
       </msub> 
       <mo>
         , 
       </mo> 
       <mtext>
           
       </mtext> 
       <mtext>
           
       </mtext> 
       <mi>
         ϕ 
       </mi> 
       <mo>
         = 
       </mo> 
       <msub> 
        <mi>
          ϕ 
        </mi> 
        <mi>
          w 
        </mi> 
       </msub> 
      </mrow> 
     </math> (5a)</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         y 
       </mi> 
       <mo>
         → 
       </mo> 
       <mi>
         ∞ 
       </mi> 
      </mrow> 
     </math>:</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         u 
       </mi> 
       <mo>
         → 
       </mo> 
       <mn>
         0 
       </mn> 
       <mo>
         , 
       </mo> 
       <mtext>
           
       </mtext> 
       <mtext>
           
       </mtext> 
       <mi>
         T 
       </mi> 
       <mo>
         → 
       </mo> 
       <msub> 
        <mi>
          T 
        </mi> 
        <mi>
          ∞ 
        </mi> 
       </msub> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mi>
          x 
        </mi> 
        <mo>
          ) 
        </mo> 
       </mrow> 
       <mo>
         , 
       </mo> 
       <mtext>
           
       </mtext> 
       <mtext>
           
       </mtext> 
       <mi>
         ϕ 
       </mi> 
       <mo>
         → 
       </mo> 
       <msub> 
        <mi>
          ϕ 
        </mi> 
        <mi>
          ∞ 
        </mi> 
       </msub> 
      </mrow> 
     </math> (5b)</p>
   </sec>
   <sec id="s2_2">
    <title>2.2. Similarity Transformations</title>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         η 
       </mi> 
       <mo>
         = 
       </mo> 
       <mi>
         G 
       </mi> 
       <msup> 
        <mi>
          r 
        </mi> 
        <mrow> 
         <mrow> 
          <mn>
            1 
          </mn> 
          <mo>
            / 
          </mo> 
          <mn>
            4 
          </mn> 
         </mrow> 
        </mrow> 
       </msup> 
       <msup> 
        <mi>
          ξ 
        </mi> 
        <mrow> 
         <mo>
           − 
         </mo> 
         <mrow> 
          <mn>
            1 
          </mn> 
          <mo>
            / 
          </mo> 
          <mn>
            4 
          </mn> 
         </mrow> 
        </mrow> 
       </msup> 
       <mfrac> 
        <mi>
          y 
        </mi> 
        <mi>
          L 
        </mi> 
       </mfrac> 
       <mo>
         , 
       </mo> 
       <mtext>
           
       </mtext> 
       <mtext>
           
       </mtext> 
       <mi>
         ξ 
       </mi> 
       <mo>
         = 
       </mo> 
       <mfrac> 
        <mi>
          x 
        </mi> 
        <mi>
          L 
        </mi> 
       </mfrac> 
      </mrow> 
     </math></p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         ψ 
       </mi> 
       <mo>
         = 
       </mo> 
       <mfrac> 
        <mi>
          μ 
        </mi> 
        <mi>
          ρ 
        </mi> 
       </mfrac> 
       <mi>
         G 
       </mi> 
       <msup> 
        <mi>
          r 
        </mi> 
        <mrow> 
         <mrow> 
          <mn>
            1 
          </mn> 
          <mo>
            / 
          </mo> 
          <mn>
            4 
          </mn> 
         </mrow> 
        </mrow> 
       </msup> 
       <msup> 
        <mi>
          ξ 
        </mi> 
        <mrow> 
         <mrow> 
          <mn>
            3 
          </mn> 
          <mo>
            / 
          </mo> 
          <mn>
            4 
          </mn> 
         </mrow> 
        </mrow> 
       </msup> 
       <mi>
         f 
       </mi> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <mi>
           ξ 
         </mi> 
         <mo>
           , 
         </mo> 
         <mi>
           η 
         </mi> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
      </mrow> 
     </math></p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         T 
       </mi> 
       <mo>
         − 
       </mo> 
       <msub> 
        <mi>
          T 
        </mi> 
        <mi>
          ∞ 
        </mi> 
       </msub> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mi>
          x 
        </mi> 
        <mo>
          ) 
        </mo> 
       </mrow> 
       <mo>
         = 
       </mo> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <msub> 
          <mi>
            T 
          </mi> 
          <mi>
            w 
          </mi> 
         </msub> 
         <mo>
           − 
         </mo> 
         <msub> 
          <mi>
            T 
          </mi> 
          <mrow> 
           <mi>
             ∞ 
           </mi> 
           <mo>
             , 
           </mo> 
           <mn>
             0 
           </mn> 
          </mrow> 
         </msub> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
       <mi>
         θ 
       </mi> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <mi>
           ξ 
         </mi> 
         <mo>
           , 
         </mo> 
         <mi>
           η 
         </mi> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
      </mrow> 
     </math></p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         ϕ 
       </mi> 
       <mo>
         − 
       </mo> 
       <msub> 
        <mi>
          ϕ 
        </mi> 
        <mi>
          ∞ 
        </mi> 
       </msub> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mi>
          x 
        </mi> 
        <mo>
          ) 
        </mo> 
       </mrow> 
       <mo>
         = 
       </mo> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <msub> 
          <mi>
            ϕ 
          </mi> 
          <mi>
            w 
          </mi> 
         </msub> 
         <mo>
           − 
         </mo> 
         <msub> 
          <mi>
            ϕ 
          </mi> 
          <mi>
            ∞ 
          </mi> 
         </msub> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
       <mi>
         g 
       </mi> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <mi>
           ξ 
         </mi> 
         <mo>
           , 
         </mo> 
         <mi>
           η 
         </mi> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
      </mrow> 
     </math></p>
    <p>Here, ψ is the stream function such that: 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         u 
       </mi> 
       <mo>
         = 
       </mo> 
       <mfrac> 
        <mrow> 
         <mo>
           ∂ 
         </mo> 
         <mi>
           ψ 
         </mi> 
        </mrow> 
        <mrow> 
         <mo>
           ∂ 
         </mo> 
         <mi>
           y 
         </mi> 
        </mrow> 
       </mfrac> 
       <mo>
         , 
       </mo> 
       <mtext>
           
       </mtext> 
       <mi>
         v 
       </mi> 
       <mo>
         = 
       </mo> 
       <mo>
         − 
       </mo> 
       <mfrac> 
        <mrow> 
         <mo>
           ∂ 
         </mo> 
         <mi>
           ψ 
         </mi> 
        </mrow> 
        <mrow> 
         <mo>
           ∂ 
         </mo> 
         <mi>
           x 
         </mi> 
        </mrow> 
       </mfrac> 
      </mrow> 
     </math></p>
    <p>Using Equations (1)-(4) and after some algebraic manipulation the momentum, energy and volume fraction equations are obtained as follows</p>
    <p>Final Non-Dimensional Governing Equations</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msup> 
        <mi>
          f 
        </mi> 
        <mo>
          ‴ 
        </mo> 
       </msup> 
       <mo>
         + 
       </mo> 
       <mfrac> 
        <mn>
          3 
        </mn> 
        <mn>
          4 
        </mn> 
       </mfrac> 
       <mi>
         f 
       </mi> 
       <msup> 
        <mi>
          f 
        </mi> 
        <mo>
          ″ 
        </mo> 
       </msup> 
       <mo>
         − 
       </mo> 
       <mfrac> 
        <mn>
          1 
        </mn> 
        <mn>
          2 
        </mn> 
       </mfrac> 
       <msup> 
        <mrow> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <msup> 
           <mi>
             f 
           </mi> 
           <mo>
             ′ 
           </mo> 
          </msup> 
          <mo>
            ) 
          </mo> 
         </mrow> 
        </mrow> 
        <mn>
          2 
        </mn> 
       </msup> 
       <mo>
         + 
       </mo> 
       <mi>
         θ 
       </mi> 
       <mo>
         − 
       </mo> 
       <msub> 
        <mi>
          N 
        </mi> 
        <mi>
          r 
        </mi> 
       </msub> 
       <mi>
         g 
       </mi> 
       <mo>
         − 
       </mo> 
       <mfrac> 
        <mrow> 
         <msup> 
          <mi>
            ξ 
          </mi> 
          <mrow> 
           <mrow> 
            <mn>
              1 
            </mn> 
            <mo>
              / 
            </mo> 
            <mn>
              2 
            </mn> 
           </mrow> 
          </mrow> 
         </msup> 
        </mrow> 
        <mrow> 
         <mi>
           D 
         </mi> 
         <mi>
           a 
         </mi> 
         <mo>
           ⋅ 
         </mo> 
         <mi>
           G 
         </mi> 
         <msup> 
          <mi>
            r 
          </mi> 
          <mrow> 
           <mrow> 
            <mn>
              1 
            </mn> 
            <mo>
              / 
            </mo> 
            <mn>
              2 
            </mn> 
           </mrow> 
          </mrow> 
         </msup> 
        </mrow> 
       </mfrac> 
       <msup> 
        <mi>
          f 
        </mi> 
        <mo>
          ′ 
        </mo> 
       </msup> 
       <mo>
         = 
       </mo> 
       <mi>
         ξ 
       </mi> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <msup> 
          <mi>
            f 
          </mi> 
          <mo>
            ′ 
          </mo> 
         </msup> 
         <mfrac> 
          <mrow> 
           <mo>
             ∂ 
           </mo> 
           <msup> 
            <mi>
              f 
            </mi> 
            <mo>
              ′ 
            </mo> 
           </msup> 
          </mrow> 
          <mrow> 
           <mo>
             ∂ 
           </mo> 
           <mi>
             ξ 
           </mi> 
          </mrow> 
         </mfrac> 
         <mo>
           − 
         </mo> 
         <msup> 
          <mi>
            f 
          </mi> 
          <mo>
            ″ 
          </mo> 
         </msup> 
         <mfrac> 
          <mrow> 
           <mo>
             ∂ 
           </mo> 
           <mi>
             f 
           </mi> 
          </mrow> 
          <mrow> 
           <mo>
             ∂ 
           </mo> 
           <mi>
             ξ 
           </mi> 
          </mrow> 
         </mfrac> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
      </mrow> 
     </math> (6)</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mfrac> 
        <mn>
          1 
        </mn> 
        <mrow> 
         <mi>
           P 
         </mi> 
         <mi>
           r 
         </mi> 
        </mrow> 
       </mfrac> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <msup> 
          <mi>
            θ 
          </mi> 
          <mo>
            ″ 
          </mo> 
         </msup> 
         <mo>
           + 
         </mo> 
         <mi>
           N 
         </mi> 
         <mi>
           b 
         </mi> 
         <mo>
           ⋅ 
         </mo> 
         <msup> 
          <mi>
            g 
          </mi> 
          <mo>
            ′ 
          </mo> 
         </msup> 
         <msup> 
          <mi>
            θ 
          </mi> 
          <mo>
            ′ 
          </mo> 
         </msup> 
         <mo>
           + 
         </mo> 
         <mi>
           N 
         </mi> 
         <mi>
           t 
         </mi> 
         <mo>
           ⋅ 
         </mo> 
         <msup> 
          <mrow> 
           <mrow> 
            <mo>
              ( 
            </mo> 
            <msup> 
             <mi>
               θ 
             </mi> 
             <mo>
               ′ 
             </mo> 
            </msup> 
            <mo>
              ) 
            </mo> 
           </mrow> 
          </mrow> 
          <mn>
            2 
          </mn> 
         </msup> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
       <mo>
         − 
       </mo> 
       <msub> 
        <mi>
          ϵ 
        </mi> 
        <mn>
          1 
        </mn> 
       </msub> 
       <mi>
         ξ 
       </mi> 
       <msup> 
        <mi>
          f 
        </mi> 
        <mo>
          ′ 
        </mo> 
       </msup> 
       <mo>
         + 
       </mo> 
       <mfrac> 
        <mn>
          3 
        </mn> 
        <mn>
          4 
        </mn> 
       </mfrac> 
       <mi>
         f 
       </mi> 
       <msup> 
        <mi>
          θ 
        </mi> 
        <mo>
          ′ 
        </mo> 
       </msup> 
       <mo>
         = 
       </mo> 
       <mi>
         ξ 
       </mi> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <msup> 
          <mi>
            f 
          </mi> 
          <mo>
            ′ 
          </mo> 
         </msup> 
         <mfrac> 
          <mrow> 
           <mo>
             ∂ 
           </mo> 
           <mi>
             θ 
           </mi> 
          </mrow> 
          <mrow> 
           <mo>
             ∂ 
           </mo> 
           <mi>
             ξ 
           </mi> 
          </mrow> 
         </mfrac> 
         <mo>
           − 
         </mo> 
         <msup> 
          <mi>
            θ 
          </mi> 
          <mo>
            ′ 
          </mo> 
         </msup> 
         <mfrac> 
          <mrow> 
           <mo>
             ∂ 
           </mo> 
           <mi>
             f 
           </mi> 
          </mrow> 
          <mrow> 
           <mo>
             ∂ 
           </mo> 
           <mi>
             ξ 
           </mi> 
          </mrow> 
         </mfrac> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
      </mrow> 
     </math> (7)</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mfrac> 
        <mn>
          1 
        </mn> 
        <mrow> 
         <mi>
           S 
         </mi> 
         <msub> 
          <mi>
            c 
          </mi> 
          <mi>
            n 
          </mi> 
         </msub> 
        </mrow> 
       </mfrac> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <msup> 
          <mi>
            g 
          </mi> 
          <mo>
            ″ 
          </mo> 
         </msup> 
         <mo>
           + 
         </mo> 
         <mfrac> 
          <mrow> 
           <mi>
             N 
           </mi> 
           <mi>
             t 
           </mi> 
          </mrow> 
          <mrow> 
           <mi>
             N 
           </mi> 
           <mi>
             b 
           </mi> 
          </mrow> 
         </mfrac> 
         <msup> 
          <mi>
            θ 
          </mi> 
          <mo>
            ″ 
          </mo> 
         </msup> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
       <mo>
         + 
       </mo> 
       <mfrac> 
        <mn>
          3 
        </mn> 
        <mn>
          4 
        </mn> 
       </mfrac> 
       <mi>
         f 
       </mi> 
       <msup> 
        <mi>
          g 
        </mi> 
        <mo>
          ′ 
        </mo> 
       </msup> 
       <mo>
         = 
       </mo> 
       <mi>
         ξ 
       </mi> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <msup> 
          <mi>
            f 
          </mi> 
          <mo>
            ′ 
          </mo> 
         </msup> 
         <mfrac> 
          <mrow> 
           <mo>
             ∂ 
           </mo> 
           <mi>
             g 
           </mi> 
          </mrow> 
          <mrow> 
           <mo>
             ∂ 
           </mo> 
           <mi>
             ξ 
           </mi> 
          </mrow> 
         </mfrac> 
         <mo>
           − 
         </mo> 
         <msup> 
          <mi>
            g 
          </mi> 
          <mo>
            ′ 
          </mo> 
         </msup> 
         <mfrac> 
          <mrow> 
           <mo>
             ∂ 
           </mo> 
           <mi>
             f 
           </mi> 
          </mrow> 
          <mrow> 
           <mo>
             ∂ 
           </mo> 
           <mi>
             ξ 
           </mi> 
          </mrow> 
         </mfrac> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
      </mrow> 
     </math> (8)</p>
    <p>Boundary condition</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         η 
       </mi> 
       <mo>
         → 
       </mo> 
       <mn>
         0 
       </mn> 
      </mrow> 
     </math> 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mn>
         3 
       </mn> 
       <mi>
         f 
       </mi> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <mi>
           ξ 
         </mi> 
         <mo>
           , 
         </mo> 
         <mn>
           0 
         </mn> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
       <mo>
         + 
       </mo> 
       <mn>
         4 
       </mn> 
       <mi>
         ξ 
       </mi> 
       <msub> 
        <mrow> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mrow> 
           <mfrac> 
            <mrow> 
             <mo>
               ∂ 
             </mo> 
             <mi>
               f 
             </mi> 
            </mrow> 
            <mrow> 
             <mo>
               ∂ 
             </mo> 
             <mi>
               ξ 
             </mi> 
            </mrow> 
           </mfrac> 
          </mrow> 
          <mo>
            ) 
          </mo> 
         </mrow> 
        </mrow> 
        <mrow> 
         <mi>
           η 
         </mi> 
         <mo>
           = 
         </mo> 
         <mn>
           0 
         </mn> 
        </mrow> 
       </msub> 
       <mo>
         = 
       </mo> 
       <mn>
         0 
       </mn> 
      </mrow> 
     </math>, 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msup> 
        <mi>
          f 
        </mi> 
        <mo>
          ′ 
        </mo> 
       </msup> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <mi>
           ξ 
         </mi> 
         <mo>
           , 
         </mo> 
         <mn>
           0 
         </mn> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
       <mo>
         = 
       </mo> 
       <mn>
         0 
       </mn> 
      </mrow> 
     </math>, 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         θ 
       </mi> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <mi>
           ξ 
         </mi> 
         <mo>
           , 
         </mo> 
         <mn>
           0 
         </mn> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
       <mo>
         = 
       </mo> 
       <mn>
         1 
       </mn> 
       <mo>
         − 
       </mo> 
       <msub> 
        <mi>
          ϵ 
        </mi> 
        <mn>
          1 
        </mn> 
       </msub> 
       <mi>
         ξ 
       </mi> 
      </mrow> 
     </math>, 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         g 
       </mi> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <mi>
           ξ 
         </mi> 
         <mo>
           , 
         </mo> 
         <mn>
           0 
         </mn> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
       <mo>
         = 
       </mo> 
       <mn>
         1 
       </mn> 
      </mrow> 
     </math> (9a)</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         η 
       </mi> 
       <mo>
         → 
       </mo> 
       <mi>
         ∞ 
       </mi> 
      </mrow> 
     </math> 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msup> 
        <mi>
          f 
        </mi> 
        <mo>
          ′ 
        </mo> 
       </msup> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <mi>
           ξ 
         </mi> 
         <mo>
           , 
         </mo> 
         <mi>
           ∞ 
         </mi> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
       <mo>
         = 
       </mo> 
       <mn>
         0 
       </mn> 
      </mrow> 
     </math>, 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         θ 
       </mi> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <mi>
           ξ 
         </mi> 
         <mo>
           , 
         </mo> 
         <mi>
           ∞ 
         </mi> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
       <mo>
         = 
       </mo> 
       <mn>
         0 
       </mn> 
      </mrow> 
     </math>, 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         g 
       </mi> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <mi>
           ξ 
         </mi> 
         <mo>
           , 
         </mo> 
         <mi>
           ∞ 
         </mi> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
       <mo>
         = 
       </mo> 
       <mn>
         0 
       </mn> 
      </mrow> 
     </math> (9b)</p>
    <p>Non-Dimensional Parameters:</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         G 
       </mi> 
       <mi>
         r 
       </mi> 
       <mo>
         = 
       </mo> 
       <mfrac> 
        <mrow> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mrow> 
           <mn>
             1 
           </mn> 
           <mo>
             − 
           </mo> 
           <msub> 
            <mi>
              ϕ 
            </mi> 
            <mi>
              ∞ 
            </mi> 
           </msub> 
          </mrow> 
          <mo>
            ) 
          </mo> 
         </mrow> 
         <msub> 
          <mi>
            ρ 
          </mi> 
          <mrow> 
           <mi>
             f 
           </mi> 
           <mi>
             ∞ 
           </mi> 
          </mrow> 
         </msub> 
         <msup> 
          <mi>
            g 
          </mi> 
          <mo>
            * 
          </mo> 
         </msup> 
         <msub> 
          <mi>
            β 
          </mi> 
          <mi>
            T 
          </mi> 
         </msub> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mrow> 
           <msub> 
            <mi>
              T 
            </mi> 
            <mi>
              w 
            </mi> 
           </msub> 
           <mo>
             − 
           </mo> 
           <msub> 
            <mi>
              T 
            </mi> 
            <mrow> 
             <mi>
               ∞ 
             </mi> 
             <mo>
               , 
             </mo> 
             <mn>
               0 
             </mn> 
            </mrow> 
           </msub> 
          </mrow> 
          <mo>
            ) 
          </mo> 
         </mrow> 
         <msup> 
          <mi>
            L 
          </mi> 
          <mn>
            3 
          </mn> 
         </msup> 
        </mrow> 
        <mrow> 
         <mi>
           μ 
         </mi> 
         <mi>
           ϑ 
         </mi> 
        </mrow> 
       </mfrac> 
      </mrow> 
     </math> (Grashof number),</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         D 
       </mi> 
       <mi>
         a 
       </mi> 
       <mo>
         = 
       </mo> 
       <mfrac> 
        <mrow> 
         <msub> 
          <mi>
            K 
          </mi> 
          <mi>
            p 
          </mi> 
         </msub> 
        </mrow> 
        <mrow> 
         <msup> 
          <mi>
            L 
          </mi> 
          <mn>
            2 
          </mn> 
         </msup> 
        </mrow> 
       </mfrac> 
      </mrow> 
     </math> (Darcy number),</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         P 
       </mi> 
       <mi>
         r 
       </mi> 
       <mo>
         = 
       </mo> 
       <mfrac> 
        <mi>
          μ 
        </mi> 
        <mrow> 
         <mi>
           ρ 
         </mi> 
         <mi>
           α 
         </mi> 
        </mrow> 
       </mfrac> 
      </mrow> 
     </math> (Prandtl number),</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          N 
        </mi> 
        <mi>
          r 
        </mi> 
       </msub> 
       <mo>
         = 
       </mo> 
       <mfrac> 
        <mrow> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mrow> 
           <msub> 
            <mi>
              ρ 
            </mi> 
            <mi>
              p 
            </mi> 
           </msub> 
           <mo>
             − 
           </mo> 
           <msub> 
            <mi>
              ρ 
            </mi> 
            <mrow> 
             <mi>
               f 
             </mi> 
             <mi>
               ∞ 
             </mi> 
            </mrow> 
           </msub> 
          </mrow> 
          <mo>
            ) 
          </mo> 
         </mrow> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mrow> 
           <msub> 
            <mi>
              ϕ 
            </mi> 
            <mi>
              w 
            </mi> 
           </msub> 
           <mo>
             − 
           </mo> 
           <msub> 
            <mi>
              ϕ 
            </mi> 
            <mi>
              ∞ 
            </mi> 
           </msub> 
          </mrow> 
          <mo>
            ) 
          </mo> 
         </mrow> 
        </mrow> 
        <mrow> 
         <msub> 
          <mi>
            ρ 
          </mi> 
          <mrow> 
           <mi>
             f 
           </mi> 
           <mi>
             ∞ 
           </mi> 
          </mrow> 
         </msub> 
         <msub> 
          <mi>
            β 
          </mi> 
          <mi>
            T 
          </mi> 
         </msub> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mrow> 
           <msub> 
            <mi>
              T 
            </mi> 
            <mi>
              w 
            </mi> 
           </msub> 
           <mo>
             − 
           </mo> 
           <msub> 
            <mi>
              T 
            </mi> 
            <mrow> 
             <mi>
               ∞ 
             </mi> 
             <mo>
               , 
             </mo> 
             <mn>
               0 
             </mn> 
            </mrow> 
           </msub> 
          </mrow> 
          <mo>
            ) 
          </mo> 
         </mrow> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mrow> 
           <mn>
             1 
           </mn> 
           <mo>
             − 
           </mo> 
           <msub> 
            <mi>
              ϕ 
            </mi> 
            <mi>
              ∞ 
            </mi> 
           </msub> 
          </mrow> 
          <mo>
            ) 
          </mo> 
         </mrow> 
        </mrow> 
       </mfrac> 
      </mrow> 
     </math> (Buoyancy ratio),</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         N 
       </mi> 
       <mi>
         b 
       </mi> 
       <mo>
         = 
       </mo> 
       <mfrac> 
        <mrow> 
         <mi>
           τ 
         </mi> 
         <msub> 
          <mi>
            D 
          </mi> 
          <mi>
            B 
          </mi> 
         </msub> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mrow> 
           <msub> 
            <mi>
              ϕ 
            </mi> 
            <mi>
              w 
            </mi> 
           </msub> 
           <mo>
             − 
           </mo> 
           <msub> 
            <mi>
              ϕ 
            </mi> 
            <mi>
              ∞ 
            </mi> 
           </msub> 
          </mrow> 
          <mo>
            ) 
          </mo> 
         </mrow> 
        </mrow> 
        <mi>
          α 
        </mi> 
       </mfrac> 
      </mrow> 
     </math> (Brownian motion),</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         N 
       </mi> 
       <mi>
         t 
       </mi> 
       <mo>
         = 
       </mo> 
       <mfrac> 
        <mrow> 
         <mi>
           τ 
         </mi> 
         <msub> 
          <mi>
            D 
          </mi> 
          <mi>
            T 
          </mi> 
         </msub> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mrow> 
           <msub> 
            <mi>
              T 
            </mi> 
            <mi>
              w 
            </mi> 
           </msub> 
           <mo>
             − 
           </mo> 
           <msub> 
            <mi>
              T 
            </mi> 
            <mrow> 
             <mi>
               ∞ 
             </mi> 
             <mo>
               , 
             </mo> 
             <mn>
               0 
             </mn> 
            </mrow> 
           </msub> 
          </mrow> 
          <mo>
            ) 
          </mo> 
         </mrow> 
        </mrow> 
        <mrow> 
         <mi>
           α 
         </mi> 
         <msub> 
          <mi>
            T 
          </mi> 
          <mi>
            ∞ 
          </mi> 
         </msub> 
        </mrow> 
       </mfrac> 
      </mrow> 
     </math> (Thermophoresis),</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         S 
       </mi> 
       <msub> 
        <mi>
          c 
        </mi> 
        <mi>
          n 
        </mi> 
       </msub> 
       <mo>
         = 
       </mo> 
       <mfrac> 
        <mi>
          ν 
        </mi> 
        <mrow> 
         <msub> 
          <mi>
            D 
          </mi> 
          <mi>
            B 
          </mi> 
         </msub> 
        </mrow> 
       </mfrac> 
      </mrow> 
     </math> (Nanoparticle Schmidt number).</p>
    <p>Local Nusselt number 
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         N 
       </mi> 
       <msub> 
        <mi>
          u 
        </mi> 
        <mi>
          ξ 
        </mi> 
       </msub> 
      </mrow> 
     </math></p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         N 
       </mi> 
       <msub> 
        <mi>
          u 
        </mi> 
        <mi>
          ξ 
        </mi> 
       </msub> 
       <mo>
         = 
       </mo> 
       <mo>
         − 
       </mo> 
       <mi>
         G 
       </mi> 
       <msup> 
        <mi>
          r 
        </mi> 
        <mrow> 
         <mrow> 
          <mn>
            1 
          </mn> 
          <mo>
            / 
          </mo> 
          <mn>
            4 
          </mn> 
         </mrow> 
        </mrow> 
       </msup> 
       <msup> 
        <mi>
          ξ 
        </mi> 
        <mrow> 
         <mrow> 
          <mn>
            3 
          </mn> 
          <mo>
            / 
          </mo> 
          <mn>
            4 
          </mn> 
         </mrow> 
        </mrow> 
       </msup> 
       <msub> 
        <mrow> 
         <mrow> 
          <mrow> 
           <mfrac> 
            <mrow> 
             <mo>
               ∂ 
             </mo> 
             <mi>
               θ 
             </mi> 
            </mrow> 
            <mrow> 
             <mo>
               ∂ 
             </mo> 
             <mi>
               η 
             </mi> 
            </mrow> 
           </mfrac> 
          </mrow> 
          <mo>
            | 
          </mo> 
         </mrow> 
        </mrow> 
        <mrow> 
         <mi>
           η 
         </mi> 
         <mo>
           = 
         </mo> 
         <mn>
           0 
         </mn> 
        </mrow> 
       </msub> 
      </mrow> 
     </math></p>
    <p>Shear Stress</p>
    <p>
     <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mover accent="true"> 
         <mi>
           τ 
         </mi> 
         <mo>
           ˜ 
         </mo> 
        </mover> 
        <mi>
          w 
        </mi> 
       </msub> 
       <mo>
         = 
       </mo> 
       <msup> 
        <mi>
          ξ 
        </mi> 
        <mrow> 
         <mrow> 
          <mn>
            1 
          </mn> 
          <mo>
            / 
          </mo> 
          <mn>
            4 
          </mn> 
         </mrow> 
        </mrow> 
       </msup> 
       <msup> 
        <mi>
          f 
        </mi> 
        <mo>
          ″ 
        </mo> 
       </msup> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <mi>
           ξ 
         </mi> 
         <mo>
           , 
         </mo> 
         <mn>
           0 
         </mn> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
      </mrow> 
     </math></p>
   </sec>
   <sec id="s2_3">
    <title>2.3. Numerical Method and Validation</title>
    <p>The coupled non-similar boundary-layer equations were solved using the Finite Element Method (FEM) with quadratic elements. A uniform mesh of 100 elements was used along the η-direction for each ξ-slice, resulting in approximately 608 nodes per slice.</p>
    <p>A grid independence test was performed by refining the mesh from 50 to 125 elements. As shown in <xref ref-type="table" rid="table1">
      Table 1
     </xref>, the computed wall heat transfer rate 
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <mo>
           − 
         </mo> 
         <msup> 
          <mi>
            θ 
          </mi> 
          <mo>
            ′ 
          </mo> 
         </msup> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mn>
            0 
          </mn> 
          <mo>
            ) 
          </mo> 
         </mrow> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
      </mrow> 
     </math> and wall shear stress 
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <msup> 
          <mi>
            f 
          </mi> 
          <mo>
            ″ 
          </mo> 
         </msup> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mn>
            0 
          </mn> 
          <mo>
            ) 
          </mo> 
         </mrow> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
      </mrow> 
     </math> converge within 1.5% variation, confirming mesh independence.</p>
    <table-wrap id="table1">
     <label>
      <xref ref-type="table" rid="table1">
       Table 1
      </xref></label>
     <caption>
      <title>
       <xref ref-type="bibr" rid="scirp.144980-"></xref>Table 1. Effect of 

       <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
  
         <msub> 
   
          <mi>
           
    ϵ
   
          </mi> 
   
          <mn>
           
    1
   
          </mn> 
  
         </msub> 
 
        </mrow>

       </math> on heat transfer rate and shear stress.</title>
     </caption>
     <table class="MsoTableGrid custom-table" border="0" cellspacing="0" cellpadding="0"> 
      <tr> 
       <td class="custom-bottom-td acenter" width="6.60%"><p style="text-align:center"> 
         <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
           <msub> 
            <mi>
              ϵ 
            </mi> 
            <mn>
              1 
            </mn> 
           </msub> 
          </mrow> 
         </math></p></td> 
       <td class="custom-bottom-td acenter" width="19.34%"><p style="text-align:center"> 
         <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
           <mo>
             − 
           </mo> 
           <msup> 
            <mi>
              θ 
            </mi> 
            <mo>
              ′ 
            </mo> 
           </msup> 
           <mrow> 
            <mo>
              ( 
            </mo> 
            <mn>
              0 
            </mn> 
            <mo>
              ) 
            </mo> 
           </mrow> 
          </mrow> 
         </math></p></td> 
       <td class="custom-bottom-td acenter" width="26.21%"><p style="text-align:center"></p></td> 
       <td class="custom-bottom-td acenter" width="19.34%"><p style="text-align:center"> 
         <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
           <msup> 
            <mi>
              f 
            </mi> 
            <mo>
              ″ 
            </mo> 
           </msup> 
           <mrow> 
            <mo>
              ( 
            </mo> 
            <mn>
              0 
            </mn> 
            <mo>
              ) 
            </mo> 
           </mrow> 
          </mrow> 
         </math></p></td> 
       <td class="custom-bottom-td acenter" width="26.21%"><p style="text-align:center"></p></td> 
      </tr> 
      <tr> 
       <td class="custom-bottom-td custom-top-td acenter" width="6.60%"><p style="text-align:center"></p></td> 
       <td class="custom-bottom-td custom-top-td acenter" width="19.34%"><p style="text-align:center">Current Study</p></td> 
       <td class="custom-bottom-td custom-top-td acenter" width="26.21%"><p style="text-align:center">Srinivasacharya <xref ref-type="bibr" rid="scirp.144980-11">
          [11]
         </xref></p></td> 
       <td class="custom-bottom-td custom-top-td acenter" width="19.34%"><p style="text-align:center">Current Study</p></td> 
       <td class="custom-bottom-td custom-top-td acenter" width="26.21%"><p style="text-align:center">Srinivasacharya <xref ref-type="bibr" rid="scirp.144980-11">
          [11]
         </xref></p></td> 
      </tr> 
      <tr> 
       <td class="custom-top-td acenter" width="6.60%"><p style="text-align:center">0.0</p></td> 
       <td class="custom-top-td acenter" width="19.34%"><p style="text-align:center">0.210</p></td> 
       <td class="custom-top-td acenter" width="26.21%"><p style="text-align:center">0.287</p></td> 
       <td class="custom-top-td acenter" width="19.34%"><p style="text-align:center">0.754</p></td> 
       <td class="custom-top-td acenter" width="26.21%"><p style="text-align:center">0.914</p></td> 
      </tr> 
      <tr> 
       <td class="acenter" width="6.60%"><p style="text-align:center">0.2</p></td> 
       <td class="acenter" width="19.34%"><p style="text-align:center">0.212</p></td> 
       <td class="acenter" width="26.21%"><p style="text-align:center">0.290</p></td> 
       <td class="acenter" width="19.34%"><p style="text-align:center">0.734</p></td> 
       <td class="acenter" width="26.21%"><p style="text-align:center">0.895</p></td> 
      </tr> 
      <tr> 
       <td class="acenter" width="6.60%"><p style="text-align:center">0.4</p></td> 
       <td class="acenter" width="19.34%"><p style="text-align:center">0.214</p></td> 
       <td class="acenter" width="26.21%"><p style="text-align:center">0.292</p></td> 
       <td class="acenter" width="19.34%"><p style="text-align:center">0.714</p></td> 
       <td class="acenter" width="26.21%"><p style="text-align:center">0.876</p></td> 
      </tr> 
      <tr> 
       <td class="acenter" width="6.60%"><p style="text-align:center">0.6</p></td> 
       <td class="acenter" width="19.34%"><p style="text-align:center">0.216</p></td> 
       <td class="acenter" width="26.21%"><p style="text-align:center">0.294</p></td> 
       <td class="acenter" width="19.34%"><p style="text-align:center">0.694</p></td> 
       <td class="acenter" width="26.21%"><p style="text-align:center">0.858</p></td> 
      </tr> 
      <tr> 
       <td class="acenter" width="6.60%"><p style="text-align:center">0.8</p></td> 
       <td class="acenter" width="19.34%"><p style="text-align:center">0.217</p></td> 
       <td class="acenter" width="26.21%"><p style="text-align:center">0.296</p></td> 
       <td class="acenter" width="19.34%"><p style="text-align:center">0.675</p></td> 
       <td class="acenter" width="26.21%"><p style="text-align:center">0.839</p></td> 
      </tr> 
     </table>
    </table-wrap>
    <p>The global FEM system was solved using the Chebyshev Method with a convergence tolerance of 10<sup>−</sup><sup>6</sup>. The maximum residual in the governing equations was verified to be below 10<sup>−</sup><sup>5</sup>, ensuring solution accuracy.</p>
   </sec>
  </sec><sec id="s3">
   <title>3. Result and Discussion</title>
   <p>
    <xref ref-type="table" rid="table1">
     Table 1
    </xref> compares the dimensionless wall heat transfer rate 
    <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mo>
        − 
      </mo> 
      <msup> 
       <mi>
         θ 
       </mi> 
       <mo>
         ′ 
       </mo> 
      </msup> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mn>
         0 
       </mn> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> and shear stress 
    <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msup> 
       <mi>
         f 
       </mi> 
       <mo>
         ″ 
       </mo> 
      </msup> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mn>
         0 
       </mn> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> between the present study and Srinivasacharya for varying thermal stratification parameter 
    <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         ϵ 
       </mi> 
       <mn>
         1 
       </mn> 
      </msub> 
     </mrow> 
    </math>. As 
    <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         ϵ 
       </mi> 
       <mn>
         1 
       </mn> 
      </msub> 
     </mrow> 
    </math> increases, 
    <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mo>
        − 
      </mo> 
      <msup> 
       <mi>
         θ 
       </mi> 
       <mo>
         ′ 
       </mo> 
      </msup> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mn>
         0 
       </mn> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> slightly rises, indicating enhanced heat transfer due to stratification. The present study shows a ~3.33% increase at 
    <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         ϵ 
       </mi> 
       <mn>
         1 
       </mn> 
      </msub> 
      <mo>
        = 
      </mo> 
      <mn>
        0.8 
      </mn> 
     </mrow> 
    </math>, closely matching the ~3.14% increase reported in .</p>
   <p>Conversely, 
    <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msup> 
       <mi>
         f 
       </mi> 
       <mo>
         ″ 
       </mo> 
      </msup> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mn>
         0 
       </mn> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> decreases with increasing 
    <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         ϵ 
       </mi> 
       <mn>
         1 
       </mn> 
      </msub> 
     </mrow> 
    </math>, suggesting reduced momentum transfer. A ~10.52% drop is observed in the current results, consistent with the ~8.19% reduction in <xref ref-type="bibr" rid="scirp.144980-11">
     [11]
    </xref>. This close agreement validates the accuracy of the present numerical approach and demonstrates the impact of thermal stratification on boundary layer behavior.</p>
   <p>
    <xref ref-type="table" rid="table2">
     Table 2
    </xref> compares the dimensionless heat transfer rate 
    <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mo>
        − 
      </mo> 
      <msup> 
       <mi>
         θ 
       </mi> 
       <mo>
         ′ 
       </mo> 
      </msup> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mn>
         0 
       </mn> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> and shear stress 
    <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msup> 
       <mi>
         f 
       </mi> 
       <mo>
         ″ 
       </mo> 
      </msup> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mn>
         0 
       </mn> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> from the present study with those of Srinivasacharya for varying Pr, Nb, Nt, and Gr. Results show that 
    <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mo>
        − 
      </mo> 
      <msup> 
       <mi>
         θ 
       </mi> 
       <mo>
         ′ 
       </mo> 
      </msup> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mn>
         0 
       </mn> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> increases with Nb and Nt, indicating improved heat transfer. Similarly, 
    <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msup> 
       <mi>
         f 
       </mi> 
       <mo>
         ″ 
       </mo> 
      </msup> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mn>
         0 
       </mn> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> rises with Pr, reflecting stronger momentum transfer. The close agreement with confirms the accuracy of the present numerical method and highlights the influence of these parameters on thermal and flow behavior in nanofluid boundary layers.</p>
   <table-wrap id="table2">
    <label>
     <xref ref-type="table" rid="table2">
      Table 2
     </xref></label>
    <caption>
     <title>
      <xref ref-type="bibr" rid="scirp.144980-"></xref>Table 2. Effects of Pr, Nb, Nt and Gr on heat transfer 

      <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
  
        <mrow>
   
         <mo>
          
    (
   
         </mo> 
   
         <mrow> 
    
          <mo>
           
     −
    
          </mo>
    
          <msup> 
     
           <mi>
             θ 
           </mi> 
     
           <mo>
             ′ 
           </mo> 
    
          </msup> 
    
          <mrow>
     
           <mo>
             ( 
           </mo> 
     
           <mn>
             0 
           </mn> 
     
           <mo>
             ) 
           </mo>
    
          </mrow>
   
         </mrow> 
   
         <mo>
          
    )
   
         </mo>
  
        </mrow>
 
       </mrow>

      </math> and shear stress 

      <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
  
        <mrow>
   
         <mo>
          
    (
   
         </mo> 
   
         <mrow> 
    
          <msup> 
     
           <mi>
             f 
           </mi> 
     
           <mo>
             ″ 
           </mo> 
    
          </msup> 
    
          <mrow>
     
           <mo>
             ( 
           </mo> 
     
           <mn>
             0 
           </mn> 
     
           <mo>
             ) 
           </mo>
    
          </mrow>
   
         </mrow> 
   
         <mo>
          
    )
   
         </mo>
  
        </mrow>
 
       </mrow>

      </math>.</title>
    </caption>
    <table class="MsoTableGrid custom-table" border="0" cellspacing="0" cellpadding="0"> 
     <tr> 
      <td rowspan="2" class="acenter" width="6.61%"><p style="text-align:center">Pr</p></td> 
      <td rowspan="2" class="acenter" width="5.73%"><p style="text-align:center">Nb</p></td> 
      <td rowspan="2" class="acenter" width="5.50%"><p style="text-align:center">Nt</p></td> 
      <td rowspan="2" class="acenter" width="6.61%"><p style="text-align:center">Gr</p></td> 
      <td class="custom-bottom-td acenter" width="16.04%"><p style="text-align:center"> 
        <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
          <mo>
            − 
          </mo> 
          <msup> 
           <mi>
             θ 
           </mi> 
           <mo>
             ′ 
           </mo> 
          </msup> 
          <mrow> 
           <mo>
             ( 
           </mo> 
           <mn>
             0 
           </mn> 
           <mo>
             ) 
           </mo> 
          </mrow> 
         </mrow> 
        </math></p></td> 
      <td class="custom-bottom-td acenter" width="21.73%"><p style="text-align:center"></p></td> 
      <td class="custom-bottom-td acenter" width="16.04%"><p style="text-align:center"> 
        <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
          <msup> 
           <mi>
             f 
           </mi> 
           <mo>
             ″ 
           </mo> 
          </msup> 
          <mrow> 
           <mo>
             ( 
           </mo> 
           <mn>
             0 
           </mn> 
           <mo>
             ) 
           </mo> 
          </mrow> 
         </mrow> 
        </math></p></td> 
      <td class="custom-bottom-td acenter" width="21.73%"><p style="text-align:center"></p></td> 
     </tr> 
     <tr> 
      <td class="custom-bottom-td custom-top-td acenter" width="16.04%"><p style="text-align:center">Current Study</p></td> 
      <td class="custom-bottom-td custom-top-td acenter" width="21.73%"><p style="text-align:center">Srinivasacharya <xref ref-type="bibr" rid="scirp.144980-11">
         [11]
        </xref></p></td> 
      <td class="custom-bottom-td custom-top-td acenter" width="16.04%"><p style="text-align:center">Current Study</p></td> 
      <td class="custom-bottom-td custom-top-td acenter" width="21.73%"><p style="text-align:center">Srinivasacharya <xref ref-type="bibr" rid="scirp.144980-11">
         [11]
        </xref></p></td> 
     </tr> 
     <tr> 
      <td class="custom-top-td acenter" width="6.61%"><p style="text-align:center">0.71</p></td> 
      <td class="custom-top-td acenter" width="5.73%"><p style="text-align:center">0.1</p></td> 
      <td class="custom-top-td acenter" width="5.50%"><p style="text-align:center">0.1</p></td> 
      <td class="custom-top-td acenter" width="6.61%"><p style="text-align:center">1.0</p></td> 
      <td class="custom-top-td acenter" width="16.04%"><p style="text-align:center">0.201</p></td> 
      <td class="custom-top-td acenter" width="21.73%"><p style="text-align:center">0.274</p></td> 
      <td class="custom-top-td acenter" width="16.04%"><p style="text-align:center">0.732</p></td> 
      <td class="custom-top-td acenter" width="21.73%"><p style="text-align:center">0.887</p></td> 
     </tr> 
     <tr> 
      <td class="acenter" width="6.61%"><p style="text-align:center">0.71</p></td> 
      <td class="acenter" width="5.73%"><p style="text-align:center">0.5</p></td> 
      <td class="acenter" width="5.50%"><p style="text-align:center">0.3</p></td> 
      <td class="acenter" width="6.61%"><p style="text-align:center">1.0</p></td> 
      <td class="acenter" width="16.04%"><p style="text-align:center">0.210</p></td> 
      <td class="acenter" width="21.73%"><p style="text-align:center">0.287</p></td> 
      <td class="acenter" width="16.04%"><p style="text-align:center">0.754</p></td> 
      <td class="acenter" width="21.73%"><p style="text-align:center">0.914</p></td> 
     </tr> 
     <tr> 
      <td class="acenter" width="6.61%"><p style="text-align:center">0.71</p></td> 
      <td class="acenter" width="5.73%"><p style="text-align:center">0.9</p></td> 
      <td class="acenter" width="5.50%"><p style="text-align:center">0.7</p></td> 
      <td class="acenter" width="6.61%"><p style="text-align:center">1.0</p></td> 
      <td class="acenter" width="16.04%"><p style="text-align:center">0.228</p></td> 
      <td class="acenter" width="21.73%"><p style="text-align:center">0.311</p></td> 
      <td class="acenter" width="16.04%"><p style="text-align:center">0.698</p></td> 
      <td class="acenter" width="21.73%"><p style="text-align:center">0.846</p></td> 
     </tr> 
     <tr> 
      <td class="acenter" width="6.61%"><p style="text-align:center">1.5</p></td> 
      <td class="acenter" width="5.73%"><p style="text-align:center">0.1</p></td> 
      <td class="acenter" width="5.50%"><p style="text-align:center">0.3</p></td> 
      <td class="acenter" width="6.61%"><p style="text-align:center">5.0</p></td> 
      <td class="acenter" width="16.04%"><p style="text-align:center">0.193</p></td> 
      <td class="acenter" width="21.73%"><p style="text-align:center">0.263</p></td> 
      <td class="acenter" width="16.04%"><p style="text-align:center">0.925</p></td> 
      <td class="acenter" width="21.73%"><p style="text-align:center">1.121</p></td> 
     </tr> 
     <tr> 
      <td class="acenter" width="6.61%"><p style="text-align:center">1.5</p></td> 
      <td class="acenter" width="5.73%"><p style="text-align:center">0.5</p></td> 
      <td class="acenter" width="5.50%"><p style="text-align:center">0.3</p></td> 
      <td class="acenter" width="6.61%"><p style="text-align:center">5.0</p></td> 
      <td class="acenter" width="16.04%"><p style="text-align:center">0.205</p></td> 
      <td class="acenter" width="21.73%"><p style="text-align:center">0.279</p></td> 
      <td class="acenter" width="16.04%"><p style="text-align:center">0.963</p></td> 
      <td class="acenter" width="21.73%"><p style="text-align:center">1.166</p></td> 
     </tr> 
     <tr> 
      <td class="acenter" width="6.61%"><p style="text-align:center">1.5</p></td> 
      <td class="acenter" width="5.73%"><p style="text-align:center">0.9</p></td> 
      <td class="acenter" width="5.50%"><p style="text-align:center">0.3</p></td> 
      <td class="acenter" width="6.61%"><p style="text-align:center">5.0</p></td> 
      <td class="acenter" width="16.04%"><p style="text-align:center">0.217</p></td> 
      <td class="acenter" width="21.73%"><p style="text-align:center">0.296</p></td> 
      <td class="acenter" width="16.04%"><p style="text-align:center">0.902</p></td> 
      <td class="acenter" width="21.73%"><p style="text-align:center">1.093</p></td> 
     </tr> 
     <tr> 
      <td class="acenter" width="6.61%"><p style="text-align:center">3.0</p></td> 
      <td class="acenter" width="5.73%"><p style="text-align:center">0.1</p></td> 
      <td class="acenter" width="5.50%"><p style="text-align:center">0.7</p></td> 
      <td class="acenter" width="6.61%"><p style="text-align:center">10.0</p></td> 
      <td class="acenter" width="16.04%"><p style="text-align:center">0.175</p></td> 
      <td class="acenter" width="21.73%"><p style="text-align:center">0.239</p></td> 
      <td class="acenter" width="16.04%"><p style="text-align:center">1.142</p></td> 
      <td class="acenter" width="21.73%"><p style="text-align:center">1.384</p></td> 
     </tr> 
     <tr> 
      <td class="acenter" width="6.61%"><p style="text-align:center">3.0</p></td> 
      <td class="acenter" width="5.73%"><p style="text-align:center">0.5</p></td> 
      <td class="acenter" width="5.50%"><p style="text-align:center">0.7</p></td> 
      <td class="acenter" width="6.61%"><p style="text-align:center">10.0</p></td> 
      <td class="acenter" width="16.04%"><p style="text-align:center">0.212</p></td> 
      <td class="acenter" width="21.73%"><p style="text-align:center">0.289</p></td> 
      <td class="acenter" width="16.04%"><p style="text-align:center">1.078</p></td> 
      <td class="acenter" width="21.73%"><p style="text-align:center">1.306</p></td> 
     </tr> 
     <tr> 
      <td class="acenter" width="6.61%"><p style="text-align:center">3.0</p></td> 
      <td class="acenter" width="5.73%"><p style="text-align:center">0.9</p></td> 
      <td class="acenter" width="5.50%"><p style="text-align:center">0.7</p></td> 
      <td class="acenter" width="6.61%"><p style="text-align:center">10.0</p></td> 
      <td class="acenter" width="16.04%"><p style="text-align:center">0.224</p></td> 
      <td class="acenter" width="21.73%"><p style="text-align:center">0.305</p></td> 
      <td class="acenter" width="16.04%"><p style="text-align:center">1.015</p></td> 
      <td class="acenter" width="21.73%"><p style="text-align:center">1.230</p></td> 
     </tr> 
     <tr> 
      <td class="acenter" width="6.61%"><p style="text-align:center">0.71</p></td> 
      <td class="acenter" width="5.73%"><p style="text-align:center">0.5</p></td> 
      <td class="acenter" width="5.50%"><p style="text-align:center">0.3</p></td> 
      <td class="acenter" width="6.61%"><p style="text-align:center">10.0</p></td> 
      <td class="acenter" width="16.04%"><p style="text-align:center">0.178</p></td> 
      <td class="acenter" width="21.73%"><p style="text-align:center">0.243</p></td> 
      <td class="acenter" width="16.04%"><p style="text-align:center">1.243</p></td> 
      <td class="acenter" width="21.73%"><p style="text-align:center">1.506</p></td> 
     </tr> 
    </table>
   </table-wrap>
   <p>
    <xref ref-type="fig" rid="fig1">
     Figure 1
    </xref> shows that increasing thermal stratification ( 
    <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         ϵ 
       </mi> 
       <mn>
         1 
       </mn> 
      </msub> 
     </mrow> 
    </math>) reduces velocity (~18%), temperature (~25%), and nanoparticle concentration (~15%) near the wall due to weakened buoyancy effects.</p>
   <fig id="fig1" position="float">
    <label>Figure 1</label>
    <caption>
     <title>(a) Velocity Profile (b) Temperature Profile (c) Nanoparticle ProfileFigure 1. Velocity, Temperature and Nanoparticle Profiles for different values of 

      <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
  
        <msub> 
   
         <mi>
          
    ϵ
   
         </mi> 
   
         <mn>
          
    1
   
         </mn> 
  
        </msub> 
 
       </mrow>

      </math>.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1724265-rId147.jpeg?20250821033100" />
   </fig>
   <p>
    <xref ref-type="fig" rid="fig2">
     Figure 2
    </xref> reveals that higher buoyancy ratio ( 
    <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         N 
       </mi> 
       <mi>
         r 
       </mi> 
      </msub> 
     </mrow> 
    </math>) enhances velocity (~22%) and temperature (~12%) while shifting the peak nanoparticle concentration ~10% away from the wall, indicating stronger particle-driven buoyancy.</p>
   <p>
    <xref ref-type="fig" rid="fig3">
     Figure 3
    </xref> illustrates the effect of thermophoresis parameter (Nt) on flow characteristics. As Nt increases to 0.5, velocity decreases slightly (~8%), while near-wall temperature rises (~15%) due to reduced cooling. Nanoparticle concentration at the wall increases significantly (~20%), indicating enhanced thermophoretic transport toward the surface.</p>
   <fig id="fig2" position="float">
    <label>Figure 2</label>
    <caption>
     <title>(a) Velocity Profile (b) Temperature Profile (c) Nanoparticle ProfileFigure 2. Velocity, Temperature and Nanoparticle Profiles for different values of Nr.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1724265-rId152.jpeg?20250821033101" />
   </fig>
   <fig id="fig3" position="float">
    <label>Figure 3</label>
    <caption>
     <title>(a) Velocity Profile (b) Temperature Profile (c) Nanoparticle ProfileFigure 3. Velocity, Temperature and Nanoparticle Profiles for different values of Nt.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1724265-rId153.jpeg?20250821033100" />
   </fig>
   <p>
    <xref ref-type="fig" rid="fig4">
     Figure 4
    </xref> shows that higher Grashof number (Gr) significantly boosts velocity (3× at Gr = 5), thins the thermal boundary layer (~20%), and increases near-wall nanoparticle accumulation (~18%) due to stronger buoyancy-driven convection.</p>
   <p>
    <xref ref-type="fig" rid="fig5">
     Figure 5
    </xref> demonstrates that increasing Darcy number (Da) improves permeability, nearly doubling velocity, increasing thermal penetration (~35%), and extending nanoparticle dispersion (~40%).</p>
   <p>
    <xref ref-type="fig" rid="fig6">
     Figure 6
    </xref> It is observed that increasing the Brownian motion parameter (Nb) leads to a decrease in wall temperature while increasing nanoparticle concentration near the surface. This is due to enhanced thermal diffusion caused by Brownian motion. As Nb increases, more thermal energy is consumed in the random movement of nanoparticles, resulting in a temperature drop near the wall.</p>
   <p>
    <xref ref-type="fig" rid="fig7">
     Figure 7
    </xref> shows the variation in Nusselt number and shear stress with respect to thermal stratification ( 
    <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         ϵ 
       </mi> 
       <mn>
         1 
       </mn> 
      </msub> 
     </mrow> 
    </math>). As 
    <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         ϵ 
       </mi> 
       <mn>
         1 
       </mn> 
      </msub> 
     </mrow> 
    </math>increases to 1.0, the Nusselt number drops by nearly 30%, indicating a substantial decline in convective heat transfer efficiency, due to reduced thermal gradients. The corresponding shear stress also decreases by around 22%, reflecting diminished velocity gradients and weaker wall shear forces. This suggests that increasing stratification not only suppresses heat transfer but also slows down the boundary layer flow.</p>
   <fig id="fig4" position="float">
    <label>Figure 4</label>
    <caption>
     <title>(a) Velocity Profile (b) Temperature Profile (c) Nanoparticle ProfileFigure 4. Velocity, Temperature and Nanoparticle Profiles for different values of Gr.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1724265-rId158.jpeg?20250821033100" />
   </fig>
   <fig id="fig5" position="float">
    <label>Figure 5</label>
    <caption>
     <title>(a) Velocity Profile (b) Temperature Profile (c) Nanoparticle ProfileFigure 5. Velocity, Temperature and Nanoparticle Profiles for different values of Da.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1724265-rId159.jpeg?20250821033100" />
   </fig>
   <fig id="fig6" position="float">
    <label>Figure 6</label>
    <caption>
     <title>(a) Velocity Profile (b) Temperature Profile (c) Nanoparticle ProfileFigure 6. Velocity, Temperature and Nanoparticle Profiles for different values of Nb.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1724265-rId160.jpeg?20250821033101" />
   </fig>
   <fig id="fig7" position="float">
    <label>Figure 7</label>
    <caption>
     <title>(a) Nusselt Number (b) Shear StressFigure 7. Nusselt Number and Shear Stress for different values of 

      <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
  
        <msub> 
   
         <mi>
          
    ϵ
   
         </mi> 
   
         <mn>
          
    1
   
         </mn> 
  
        </msub> 
 
       </mrow>

      </math>.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1724265-rId161.jpeg?20250821033100" />
   </fig>
   <p>
    <xref ref-type="fig" rid="fig8">
     Figure 8
    </xref> shows the influence of thermophoresis (Nt) on Nusselt number and shear stress. An increase in Nt to 0.7 enhances the Nusselt number by roughly 18%, as thermophoretic forces promote the movement of nanoparticles from hot to cooler regions, intensifying local heat transport. The shear stress also increases by nearly 12%, suggesting greater flow resistance near the wall due to accumulated nanoparticles, which exert additional drag on the fluid.</p>
   <fig id="fig8" position="float">
    <label>Figure 8</label>
    <caption>
     <title>(a) Nusselt Number (b) Shear StressFigure 8. Nusselt Number and Shear Stress for different values of Nt.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1724265-rId164.jpeg?20250821033100" />
   </fig>
   <p>
    <xref ref-type="fig" rid="fig9">
     Figure 9
    </xref> illustrates the effect of the Prandtl number (Pr) on the Nusselt number and shear stress. At higher values of Pr (Pr = 7.0), the Nusselt number peaks, showing about a 50% increase over low-Pr fluids like air (Pr = 0.71). This enhancement is attributed to a reduction in thermal diffusivity, which intensifies the temperature gradient and boosts heat transfer. Additionally, the shear stress also reaches its maximum at Pr = 7.0, as viscous effects dominate and create steeper velocity gradients near the wall.</p>
   <fig id="fig9" position="float">
    <label>Figure 9</label>
    <caption>
     <title>(a) Nusselt Number (b) Shear StressFigure 9. Nusselt Number and Shear Stress for different values of Pr.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1724265-rId165.jpeg?20250821033100" />
   </fig>
   <p>Physical Interpretation of Nt and Nb Effects</p>
   <p>The thermophoresis parameter (Nt) causes nanoparticles to drift from hot to cold regions. As Nt increases, more particles accumulate near the wall, enhancing heat transfer and increasing the Nusselt number. Meanwhile, Brownian motion (Nb) contributes to thermal mixing and redistributes particles randomly. These two mechanisms interact to influence heat and momentum transport. A higher Nt strengthens thermal boundary layer thickness, while Nb significantly influences the nanoparticle volume fraction distribution.</p>
  </sec><sec id="s4">
   <title>4. Conclusions</title>
   <p>This study investigated natural convection of nanofluid over a vertical plate in a thermally stratified porous medium using a non-similar formulation solved via the Finite Element Method. Results show that increasing the thermal stratification parameter 
    <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         ϵ 
       </mi> 
       <mn>
         1 
       </mn> 
      </msub> 
     </mrow> 
    </math> reduces velocity, temperature, and nanoparticle concentration due to weakened buoyancy.</p>
   <p>Key observations include:</p>
   <p>1) Higher Nt enhances temperature and wall shear stress.</p>
   <p>2) Higher Nb increases nanoparticle concentration but slightly lowers temperature.</p>
   <p>3) Nusselt number rises with Nt, but decreases with Nb.</p>
   <p>4) Wall shear stress decreases with 
    <math xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         ϵ 
       </mi> 
       <mn>
         1 
       </mn> 
      </msub> 
     </mrow> 
    </math> but increases with Nt and Nb.</p>
   <p>Limitations and Future Work:</p>
   <p>This study assumes a single-phase nanofluid model with constant thermophysical properties. It also neglects thermal dispersion, slip effects, and magnetohydrodynamic influences. Future extensions may include two-phase models, non-Newtonian base fluids, or magnetically influenced flows for broader applicability.</p>
  </sec><sec id="s5">
   <title>5. Practical Engineering Applications</title>
   <p>The study of nanofluid flow over a vertical surface embedded in a porous medium under double stratification has significant practical relevance in modern engineering systems. One of the key areas where such flow dynamics play a critical role is in the design and optimization of porous heat exchangers. In these systems, the enhanced thermal conductivity provided by nanoparticles, combined with the permeability characteristics of the porous matrix, can substantially improve heat transfer rates. This results in more compact, efficient, and energy-saving heat exchangers suitable for industrial thermal management, electronics cooling, and renewable energy systems.</p>
   <p>Another important application lies in geothermal energy extraction and coating technologies, where stratified nanofluid flow influences the thermal performance of geothermal wells or heat pipes. The presence of double stratification—both thermal and solutal—affects how efficiently heat can be transported through the subsurface environment. By understanding and optimizing such flows, engineers can develop more effective thermal insulation coatings and energy-efficient systems for use in underground thermal reservoirs or building-integrated geothermal systems.</p>
   <p>Moreover, the combined effect of buoyancy-driven flow and nanoparticle transport in stratified porous environments also finds application in thermal barrier coatings, solar collectors, chemical reactors, and biomedical devices, where precise thermal regulation is essential. Therefore, the findings of this study not only contribute to theoretical understanding but also serve as a foundation for engineering innovations in energy, environment, and materials technology.</p>
  </sec><sec id="s6">
   <title>NOTES</title>
   <p>*Corresponding author.</p>
  </sec>
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