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<front>
<journal-meta>
<journal-id journal-id-type="pmc">FHMT</journal-id>
<journal-id journal-id-type="nlm-ta">FHMT</journal-id>
<journal-id journal-id-type="publisher-id">FHMT</journal-id>
<journal-title-group>
<journal-title>Frontiers in Heat and Mass Transfer</journal-title>
</journal-title-group>
<issn pub-type="epub">2151-8629</issn>
<publisher>
<publisher-name>Tech Science Press</publisher-name>
<publisher-loc>USA</publisher-loc>
</publisher>
</journal-meta>
<article-meta>
<article-id pub-id-type="publisher-id">69454</article-id>
<article-id pub-id-type="doi">10.32604/fhmt.2025.069454</article-id>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Article</subject>
</subj-group>
</article-categories>
<title-group>
<article-title>Comprehensive Study of the Effect of Ribs and Cavities on Thermal-Hydraulic Performance of Mini-Channel Heat Sinks</article-title>
<alt-title alt-title-type="left-running-head">Comprehensive Study of the Effect of Ribs and Cavities on Thermal-hydraulic Performance of Mini-channel Heat Sinks</alt-title>
<alt-title alt-title-type="right-running-head">Comprehensive Study of the Effect of Ribs and Cavities on Thermal-hydraulic Performance of Mini-channel Heat Sinks</alt-title>
</title-group>
<contrib-group>
<contrib id="author-1" contrib-type="author">
<name name-style="western"><surname>Lian</surname><given-names>Shuaimei</given-names></name></contrib>
<contrib id="author-2" contrib-type="author">
<name name-style="western"><surname>Liu</surname><given-names>Pingping</given-names></name></contrib>
<contrib id="author-3" contrib-type="author" corresp="yes">
<name name-style="western"><surname>Liao</surname><given-names>Wenling</given-names></name><email>lwlcdtu18@163.com</email></contrib>
<aff id="aff-1"><institution>School of Intelligent Manufacturing, Chengdu Technological University</institution>, <addr-line>Chengdu, 611730</addr-line>, <country>China</country></aff>
</contrib-group>
<author-notes>
<corresp id="cor1"><label>&#x002A;</label>Corresponding Author: Wenling Liao. Email: <email>lwlcdtu18@163.com</email></corresp>
</author-notes>
<pub-date date-type="collection" publication-format="electronic">
<year>2025</year>
</pub-date>
<pub-date date-type="pub" publication-format="electronic">
<day>31</day><month>10</month><year>2025</year>
</pub-date>
<volume>23</volume>
<issue>5</issue>
<fpage>1395</fpage>
<lpage>1415</lpage>
<history>
<date date-type="received">
<day>23</day>
<month>6</month>
<year>2025</year>
</date>
<date date-type="accepted">
<day>13</day>
<month>8</month>
<year>2025</year>
</date>
</history>
<permissions>
<copyright-statement>&#x00A9; 2025 The Authors.</copyright-statement>
<copyright-year>2025</copyright-year>
<copyright-holder>Published by Tech Science Press.</copyright-holder>
<license xlink:href="https://creativecommons.org/licenses/by/4.0/">
<license-p>This work is licensed under a <ext-link ext-link-type="uri" xlink:type="simple" xlink:href="https://creativecommons.org/licenses/by/4.0/">Creative Commons Attribution 4.0 International License</ext-link>, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.</license-p>
</license>
</permissions>
<self-uri content-type="pdf" xlink:href="TSP_FHMT_69454.pdf"></self-uri>
<abstract>
<p>In this work, numerical simulations are performed to investigate the influence of combining ribs and triangular cavities on the thermal-hydraulic performance (<italic>THP</italic>) of MCHS at fluid velocities ranging from 1 to 4 m/s (corresponding to Reynolds numbers (Re) of 129.75 to 519). Specifically, the ribs are positioned on the bottom wall, and the rib width is equal to the mini-channel width, while the triangular cavities are arranged on the two side walls of the MCHS. By analyzing and comparing key parameters such as velocity distribution, streamline patterns, pressure drop, skin friction coefficient (<italic>C</italic><sub><italic>f</italic></sub>), Nusselt number (<italic>Nu</italic>), friction factor (<italic>f</italic>), temperature fields, and performance evaluation criterion (<italic>PEC</italic>), the advantages of rib-cavity coupling configuration in enhancing <italic>THP</italic> are systematically discussed. Furthermore, the effects of cavity distribution (left, middle, and right), cavity depth (0.04, 0.06, and 0.08 mm), and rib height (0.02, 0.04, and 0.06 mm) on <italic>THP</italic> are analyzed to optimize the geometric parameters of the ribs and the cavities. The numerical simulation results indicate that, in comparison to the use of ribs or cavities alone, rib-cavity coupling can further improve the <italic>THP</italic> of MCHS without causing a significant increase in pressure drop. The downstream wall of the cavity is perpendicular to the flow direction which is more favorable for enhancing the heat transfer performance. Increasing the cavity depth improves the heat transfer performance of MCHS, the maximum <italic>Nu</italic> ratio increase by 35% at a rib height of 0.06 mm. However the increase in the rib height leads to a significant increase in the pressure drop, which in turn exerts a negative impact on <italic>THP</italic>, a maximum <italic>PEC</italic> of 1.198 is obtained at a rig height of 0.02 mm. The greatest improvement in <italic>THP</italic>, reaching 19.8%, is achieved when the cavity depth is 0.08 mm and the rib height is 0.02 mm.</p>
</abstract>
<kwd-group kwd-group-type="author">
<kwd>Mini-channel heat sinks</kwd>
<kwd>rib</kwd>
<kwd>cavity</kwd>
<kwd>synergistic effect</kwd>
<kwd>thermal-hydraulic performance</kwd>
</kwd-group>
<funding-group>
<award-group id="awg1">
<funding-source>Sichuan Natural Science Foundation</funding-source>
<award-id>2023NSFSC0870</award-id>
</award-group>
</funding-group>
</article-meta>
</front>
<body>
<sec id="s1">
<label>1</label>
<title>Introduction</title>
<p>Heat sink is a specially designed device or structure whose core function is to efficiently absorb and dissipate heat transferred from a heat source (such as electronic components, mechanical parts, or high-temperature equipment) by expanding heat dissipation area, optimizing heat transfer paths, or enhancing fluid flow, thereby maintaining the heat source within a safe operating temperature range. Owing to the advantages of lightweight, compact structure, and high heat transfer area ratio, mini-channel heat sinks (MCHS) have been widely used in fields such as electronic equipment cooling, aerospace and power systems, et al. [<xref ref-type="bibr" rid="ref-1">1</xref>,<xref ref-type="bibr" rid="ref-2">2</xref>]. In recent years, although the continuous advancement of technology has significantly improved the cooling performance of electronic devices, the simultaneous increase in their power consumption has imposed higher demands on heat dissipation capabilities [<xref ref-type="bibr" rid="ref-3">3</xref>]. To address this challenge, various approaches have been proposed to enhance the heat transfer performance of MCHS, including changing the cross-sectional shape [<xref ref-type="bibr" rid="ref-4">4</xref>&#x2013;<xref ref-type="bibr" rid="ref-9">9</xref>], introducing ribs or pins [<xref ref-type="bibr" rid="ref-10">10</xref>&#x2013;<xref ref-type="bibr" rid="ref-14">14</xref>], and replacing work fluid [<xref ref-type="bibr" rid="ref-15">15</xref>,<xref ref-type="bibr" rid="ref-16">16</xref>], wavy channel [<xref ref-type="bibr" rid="ref-17">17</xref>&#x2013;<xref ref-type="bibr" rid="ref-19">19</xref>], and multi-layer mini-channel [<xref ref-type="bibr" rid="ref-20">20</xref>,<xref ref-type="bibr" rid="ref-21">21</xref>].</p>
<p>Among these approaches, changing the cross-sectional shape and introducing ribs or pins, as there is no need for external energy consumption, has attracted great attention from researchers. Sui et al. [<xref ref-type="bibr" rid="ref-22">22</xref>&#x2013;<xref ref-type="bibr" rid="ref-24">24</xref>] employed numerical simulation and experimental methods to analyze the <italic>THP</italic> of rectangular wave mini-channels The results confirmed that the wave cross-sectional shape can remarkably enhance the heat transfer performance of MCHS, and the improvement in the heat transfer exceeding the pressure drop penalty. Yuan et al. [<xref ref-type="bibr" rid="ref-25">25</xref>] conducted numerical simulations to investigate the effect of non-uniform waviness on the heat transfer performance of MCHS. The results indicate that the mini-channel with divergent waviness exhibits superior heat transfer performance. Chai et al. [<xref ref-type="bibr" rid="ref-26">26</xref>] evaluated the impact of periodically expanding-contracting cross-section shapes on the heat transfer performance of MCHS, reporting that such configurations result in an average <italic>Nu</italic> that is 1.8 times higher than that of traditional MCHS. Kumar et al. [<xref ref-type="bibr" rid="ref-27">27</xref>] designed a novel circular wavy mini-channel and utilized numerical simulations to compare the effects of circular and sinusoidal waviness on the heat transfer performance of MCHS. The results reflect that the heat transfer performance of circular wavy MCHS is superior to that of sinusoidal wavy MCHS. Ahmed and Ahmed [<xref ref-type="bibr" rid="ref-28">28</xref>] performed numerical simulations to evaluate the impact of rectangular, triangular, and trapezoidal grooves on the heat transfer performance of MCHS. The results show that compared to rectangular and triangular grooves, trapezoidal grooves have the most significant improvement in the heat transfer performance. In addition, many numerical simulations and experiments have been conducted to analyze the impact of pins or fins on the heat transfer performance of MCHS. For instance, Xiao et al. [<xref ref-type="bibr" rid="ref-29">29</xref>] conducted numerical simulations to analyze the effects of V-shaped ribs on turbulent heat transfer in MCHS. The results indicate that V-shaped ribs can significantly enhance the turbulence effect and convective heat transfer performance of MCHS by inducing longitudinal swirls. Chai et al. [<xref ref-type="bibr" rid="ref-14">14</xref>,<xref ref-type="bibr" rid="ref-30">30</xref>] employed numerical simulations to analyze the influence of triangular and fan-shaped ribs on the heat transfer performance of MCHS. The numerical simulation results reveal that under low Reynolds number (<italic>Re</italic>) conditions, MCHS with triangular ribs achieve optimal <italic>THP</italic>, whereas fan-shaped ribs can significantly improve the <italic>THP</italic> of MCHS under high <italic>Re</italic> conditions. Hsieh et al. [<xref ref-type="bibr" rid="ref-31">31</xref>] conducted experiments to investigate the effect of pins with different shapes on the heat transfer performance of MCHS under low <italic>Re</italic> conditions. Their findings indicate that, compared with smooth microchannels, square pins yield the most significant improvement in heat transfer performance, followed by the elliptical, circular, hexagonal, and triangular pins, in that order. Hua et al. [<xref ref-type="bibr" rid="ref-32">32</xref>] conducted experiments to examine the effect of pins with different shapes on flow characteristics in MCHS, demonstrating that circular pins induce greater fluid flow resistance than elliptical pins. Chen et al. [<xref ref-type="bibr" rid="ref-33">33</xref>] analyzed the effects of the distribution direction, height, and offset value of the triangular prism on the flow characteristic and heat transfer performance of MCHS with a <italic>Re</italic> ranging from 211 to 884. They found that the optimal THP of MCHS is achieved when the prism height <italic>Hp</italic> &#x003D; 1 mm and the offset value <italic>S</italic> &#x003D; 0 mm.</p>
<p>Furthermore, to maximize the heat transfer performance of MCHS while controlling the pressure drop within a reasonable range, numerical simulations have also been employed to analyze the effects of combining ribs and cavities on the <italic>THP</italic> of MCHS. Zhu et al. [<xref ref-type="bibr" rid="ref-3">3</xref>] found that by integrating the advantages of rectangular cavities (which increase the flow area and reduce pressure drop) and fins (which enhance fluid disturbance and improve heat transfer), the cavity-fin combination can effectively boost the heat transfer performance of MCHS without increasing the pressure drop. Additionally, Zhu et al. [<xref ref-type="bibr" rid="ref-34">34</xref>] also analyzed the effects of rib type, distribution, and size on the heat transfer performance of MCHS. Datta et al. [<xref ref-type="bibr" rid="ref-35">35</xref>] conducted numerical simulations to assess the effect of the combination of trapezoidal cavities and ribs on the conjugate heat transfer performance of MCHS, revealing that this combination can effectively improve the conjugate heat transfer effect of MCHS and that rib type also exerts a significant impact on conjugate heat transfer. Li et al. [<xref ref-type="bibr" rid="ref-36">36</xref>&#x2013;<xref ref-type="bibr" rid="ref-39">39</xref>] further confirmed the superiority of the cavity-fin combination in improving the heat transfer performance of MCHS.</p>
<p>In summary, how to effectively improve the heat transfer performance of MCHS without causing a significant increase in fluid pressure drop remains a focus of current research. Although researchers have conducted numerical simulation studies on the combination of ribs and cavities to improve the <italic>THP</italic> of mini-channel heat sinks, rib dimensions is a critical factor affecting the heat transfer performance. At present, existing studies focused on the rib widths smaller than the mini-channel width, with a lack of research investigating scenarios where the rib width is equal to the mini-channel width. Therefore, this work performs numerical simulations to analyze the impact of the combining ribs and cavities on the <italic>THP</italic> of MCHS under the condition that the rib width equals the mini-channel width. Specially, the ribs and cavities are located on the bottom wall and the two side walls of the mini-channel, respectively. Based on the analysis of velocity distribution, streamline patterns, pressure drop, <italic>C</italic><sub><italic>f</italic></sub>, <italic>Nu</italic>, <italic>f</italic>, temperature fields, and <italic>PEC</italic>, the impact mechanism of the combination of ribs and cavities on the <italic>THP</italic> of MCHS is analyzed in detail.</p>
</sec>
<sec id="s2">
<label>2</label>
<title>Models</title>
<sec id="s2_1">
<label>2.1</label>
<title>Geometrical Model</title>
<p><xref ref-type="fig" rid="fig-1">Fig. 1</xref> shows the schematic diagram of the geometric structure of MCHS, the overall size of MCHS is 10 <inline-formula id="ieqn-1"><mml:math id="mml-ieqn-1"><mml:mo>&#x00D7;</mml:mo></mml:math></inline-formula> 3 <inline-formula id="ieqn-2"><mml:math id="mml-ieqn-2"><mml:mo>&#x00D7;</mml:mo></mml:math></inline-formula> 0.35 mm. Owing to the symmetry of the structure, only one minimum unit is selected for the simulation analysis. All the geometric parameters of the mini-channel are given in <xref ref-type="table" rid="table-1">Table 1</xref>. The boundary definitions for the solid and fluid domains in the numerical simulation are shown in <xref ref-type="fig" rid="fig-2">Fig. 2</xref>.</p>
<fig id="fig-1">
<label>Figure 1</label>
<caption>
<title>(<bold>a</bold>) Isometric view of mini-channels, and (<bold>b</bold>) cross-sectional view of a single mini-channel</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-1.tif"/>
</fig><table-wrap id="table-1">
<label>Table 1</label>
<caption>
<title>Geometry dimensions of mini-channel</title>
</caption>
<table>
<colgroup>
<col/>
<col/>
</colgroup>
<thead>
<tr>
<th>Dimension parameter</th>
<th>Value (mm)</th>
</tr>
</thead>
<tbody>
<tr>
<td>Mini-channel length (L)</td>
<td>10</td>
</tr>
<tr>
<td>Single mini-channel width (W)</td>
<td>0.3</td>
</tr>
<tr>
<td>Mini-channel height (H)</td>
<td>0.35</td>
</tr>
<tr>
<td>Lateral wall thickness (W<sub>w</sub>)</td>
<td>0.1</td>
</tr>
<tr>
<td>Channel width (W<sub>f</sub>)</td>
<td>0.1</td>
</tr>
<tr>
<td>Channel height (H<sub>f</sub>)</td>
<td>0.2</td>
</tr>
</tbody>
</table>
</table-wrap><fig id="fig-2">
<label>Figure 2</label>
<caption>
<title>(<bold>a</bold>) The fluid domain, and (<bold>b</bold>) boundary setting conditions</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-2.tif"/>
</fig>
<p>In heat transfer, a rib is a protruding structure intentionally designed on a solid surface to enhance heat exchange between the surface and the surrounding fluid. It is typically integrally formed with the base surface or attached via welding, bonding, etc. A cavity refers to a closed or semi-closed space enclosed by solid boundaries, typically filled with gas, liquid, or vacuum, where the spatial scale is comparable to or larger than the characteristic scale of the heat transfer process. Given the small size of MCHS, triangular cross-section is adopted for the cavities on both sides of the mini-channel to facilitate the fabrication of cavities. The ribs, located on the bottom wall of the mini-channel, have the same cross-sectional shape as the cavities. <xref ref-type="fig" rid="fig-3">Fig. 3</xref> shows a schematic diagram of the geometry of the mini-channel incorporating ribs and cavities. Additionally, three different cavity distributions are designated as cavity left (C-L), cavity-middle (C-M), and cavity-right (C-R) to distinguish their positional differences. The specific dimensions of the ribs and cavities are shown in <xref ref-type="table" rid="table-2">Table 2</xref>. To distinguish the influence of rib height on <italic>THP</italic>, different rib heights are represented as R0.02, R0.04, and R0.06, respectively. Similarly, different cavity depths are represented as C0.04, C0.06, and C0.08, respectively.</p>
<fig id="fig-3">
<label>Figure 3</label>
<caption>
<title>The schematic diagram of the geometry of ribs and cavities: (<bold>a</bold>) axonometric view, (<bold>b</bold>) home view, and (<bold>c</bold>) side view</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-3.tif"/>
</fig><table-wrap id="table-2">
<label>Table 2</label>
<caption>
<title>The specific dimensions of ribs and cavities</title>
</caption>
<table>
<colgroup>
<col/>
<col/>
<col/>
<col/>
<col/>
</colgroup>
<thead>
<tr>
<th>Parameters</th>
<th>Pitch (S<sub>p</sub>)/mm</th>
<th>Cavity depth (H<sub>C</sub>)/mm</th>
<th>Cavity width (W<sub>c</sub>)/mm</th>
<th>Rib height (H<sub>r</sub>)/mm</th>
</tr>
</thead>
<tbody>
<tr>
<td>Values</td>
<td>0.8</td>
<td>0.04, 0.06, 0.08</td>
<td>0.2</td>
<td>0.02, 0.04, 0.06</td>
</tr>
</tbody>
</table>
</table-wrap>
</sec>
<sec id="s2_2">
<label>2.2</label>
<title>Numerical Model and Boundary Conditions</title>
<p>According to the research reported by Palm et al. [<xref ref-type="bibr" rid="ref-40">40</xref>], the single-phase flow in the mini-channel still obeys the N-S equation and continuity assumption when the hydraulic diameter is larger than 1 <inline-formula id="ieqn-3"><mml:math id="mml-ieqn-3"><mml:mo>&#x00D7;</mml:mo></mml:math></inline-formula> 10<sup>&#x2212;4</sup> m and the <italic>Re</italic> is less than 1200. Therefore, considering that the fluid is laminar and incompressible, as well as neglecting radiative heat transfer, the continuity equation, momentum equation, and energy equation can be described as follows.</p>
<p>Continuity equation:
<disp-formula id="eqn-1"><label>(1)</label><mml:math id="mml-eqn-1" display="block"><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mo>&#x22C5;</mml:mo><mml:mrow><mml:mover><mml:mi>U</mml:mi><mml:mo stretchy="false">&#x2192;</mml:mo></mml:mover></mml:mrow><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math></disp-formula></p>
<p>Momentum equation:
<disp-formula id="eqn-2"><label>(2)</label><mml:math id="mml-eqn-2" display="block"><mml:msub><mml:mi>&#x03C1;</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub><mml:mo stretchy="false">(</mml:mo><mml:mrow><mml:mover><mml:mi>U</mml:mi><mml:mo stretchy="false">&#x2192;</mml:mo></mml:mover></mml:mrow><mml:mo>&#x22C5;</mml:mo><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mrow><mml:mover><mml:mi>U</mml:mi><mml:mo stretchy="false">&#x2192;</mml:mo></mml:mover></mml:mrow><mml:mo stretchy="false">)</mml:mo><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mi>P</mml:mi><mml:mo>+</mml:mo><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mo stretchy="false">(</mml:mo><mml:msub><mml:mi>&#x03BC;</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mrow><mml:mover><mml:mi>U</mml:mi><mml:mo stretchy="false">&#x2192;</mml:mo></mml:mover></mml:mrow><mml:mo stretchy="false">)</mml:mo></mml:math></disp-formula></p>
<p>The energy equation for the fluid domain:
<disp-formula id="eqn-3"><label>(3)</label><mml:math id="mml-eqn-3" display="block"><mml:msub><mml:mi>&#x03C1;</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mi>p</mml:mi><mml:mo>,</mml:mo><mml:mi>f</mml:mi></mml:mrow></mml:msub><mml:mo stretchy="false">(</mml:mo><mml:mrow><mml:mover><mml:mi>U</mml:mi><mml:mo stretchy="false">&#x2192;</mml:mo></mml:mover></mml:mrow><mml:mo>&#x22C5;</mml:mo><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub><mml:mo stretchy="false">)</mml:mo><mml:mo>=</mml:mo><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mo stretchy="false">(</mml:mo><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub><mml:mo stretchy="false">)</mml:mo></mml:math></disp-formula></p>
<p>The energy equation for the solid domain:
<disp-formula id="eqn-4"><label>(4)</label><mml:math id="mml-eqn-4" display="block"><mml:msup><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math></disp-formula></p>
<p>In this work, the water is used as a working fluid to investigate the flow characteristics and heat transfer performance in mini-channels. The impact of temperature changes on the physical properties of water is neglected. In addition, the boundary conditions of the numerical simulation are written as follows:</p>
<p>(1) Inlet (<italic>x</italic> &#x003D; 0): The velocity-inlet boundary condition is applied to the mini-channel inlet.</p>
<p>The fluid with a temperature of 300 K. Refer to existing literature [<xref ref-type="bibr" rid="ref-3">3</xref>,<xref ref-type="bibr" rid="ref-41">41</xref>], the fluid velocity is set to 1, 1.5, 2, 2.5, 3, 3.5, and 4 m/s, and the corresponding <italic>Re</italic> are 129.75, 194.62, 259.5, 324.37, 389.25, 454.12, and 519, respectively.</p>
<p>(2) Outlet (x &#x003D; L): The pressure-outlet boundary condition is applied to the mini-channel outlet.</p>
<p>The pressure setting at the microchannel outlet is equal to atmospheric pressure.</p>
<p>(3) Contact surfaces of fluid and solid: The conjugate boundary condition is applied to the internal surface.
<disp-formula id="eqn-5"><label>(5)</label><mml:math id="mml-eqn-5" display="block"><mml:mrow><mml:mover><mml:mi>U</mml:mi><mml:mo stretchy="false">&#x2192;</mml:mo></mml:mover></mml:mrow><mml:mo>=</mml:mo><mml:mn>0</mml:mn><mml:mo>,</mml:mo><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow></mml:msub><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>n</mml:mi></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>n</mml:mi></mml:mrow></mml:mfrac></mml:math></disp-formula></p>
<p>(4) Bottom wall (z &#x003D; 0): The no-slip and uniform heat flux condition is applied to the bottom wall, the heat flux is <inline-formula id="ieqn-4"><mml:math id="mml-ieqn-4"><mml:msup><mml:mn>10</mml:mn><mml:mrow><mml:mn>6</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> w/m<sup>2</sup>.
<disp-formula id="eqn-6"><label>(6)</label><mml:math id="mml-eqn-6" display="block"><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow></mml:msub><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>z</mml:mi></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:msub><mml:mi>q</mml:mi><mml:mrow><mml:mi>w</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mrow><mml:mn>6</mml:mn></mml:mrow></mml:msup><mml:mtext>&#x00A0;</mml:mtext><mml:mi>w</mml:mi><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:msup><mml:mi>m</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:math></disp-formula></p>
<p>(5) Symmetry surface (<inline-formula id="ieqn-5"><mml:math id="mml-ieqn-5"><mml:mi>y</mml:mi><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math></inline-formula> and <inline-formula id="ieqn-6"><mml:math id="mml-ieqn-6"><mml:mi>y</mml:mi><mml:mo>=</mml:mo><mml:mi>W</mml:mi></mml:math></inline-formula>):
<disp-formula id="eqn-7"><label>(7)</label><mml:math id="mml-eqn-7" display="block"><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>y</mml:mi></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math></disp-formula></p>
<p>(6) Other surfaces: The no slip and no heat transfer conditions are applied to other surfaces.
<disp-formula id="eqn-8"><label>(8)</label><mml:math id="mml-eqn-8" display="block"><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>n</mml:mi></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mn>0</mml:mn><mml:mo>,</mml:mo><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>n</mml:mi></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math></disp-formula></p>
</sec>
<sec id="s2_3">
<label>2.3</label>
<title>Data Acquisition and Performance Evaluation</title>
<p>To effectively compare and evaluate the simulation results, the following parameters are explained.</p>
<p>Reynolds number (<italic>Re</italic>): After determining the geometric parameters of the mini-channel and the working fluid, <italic>Re</italic> can be calculated from the fluid velocity at the inlet.
<disp-formula id="eqn-9"><label>(9)</label><mml:math id="mml-eqn-9" display="block"><mml:mtable columnalign="right left right left right left right left right left right left" rowspacing="3pt" columnspacing="0em 2em 0em 2em 0em 2em 0em 2em 0em 2em 0em" displaystyle="true"><mml:mtr><mml:mtd /><mml:mtd><mml:mi>R</mml:mi><mml:mi>e</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:msub><mml:mi>&#x03C1;</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub><mml:msub><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>n</mml:mi></mml:mrow></mml:msub><mml:msub><mml:mi>D</mml:mi><mml:mrow><mml:mi>h</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:msub><mml:mi>&#x03BC;</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub></mml:mfrac></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<disp-formula id="eqn-10"><label>(10)</label><mml:math id="mml-eqn-10" display="block"><mml:mtable columnalign="right left right left right left right left right left right left" rowspacing="3pt" columnspacing="0em 2em 0em 2em 0em 2em 0em 2em 0em 2em 0em" displaystyle="true"><mml:mtr><mml:mtd /><mml:mtd><mml:msub><mml:mi>D</mml:mi><mml:mrow><mml:mi>h</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mn>2</mml:mn><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mfrac></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula></p>
<p>(Skin friction coefficient) <inline-formula id="ieqn-7"><mml:math id="mml-ieqn-7"><mml:msub><mml:mi>C</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>: <inline-formula id="ieqn-8"><mml:math id="mml-ieqn-8"><mml:msub><mml:mi>C</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is used to reflect the thickness of the fluid boundary layer in the mini-channel
<disp-formula id="eqn-11"><label>(11)</label><mml:math id="mml-eqn-11" display="block"><mml:msub><mml:mi>C</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mfrac><mml:msub><mml:mi>&#x03C4;</mml:mi><mml:mrow><mml:mi>w</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mn>0.5</mml:mn><mml:msub><mml:mi>&#x03C1;</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub><mml:msubsup><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>n</mml:mi></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msubsup></mml:mrow></mml:mfrac></mml:math></disp-formula></p>
<p>(Nusselt number) <italic>Nu</italic>: The heat transfer performance of mini-channels is evaluated by <italic>Nu</italic>.
<disp-formula id="eqn-12"><label>(12)</label><mml:math id="mml-eqn-12" display="block"><mml:mtable columnalign="right left right left right left right left right left right left" rowspacing="3pt" columnspacing="0em 2em 0em 2em 0em 2em 0em 2em 0em 2em 0em" displaystyle="true"><mml:mtr><mml:mtd /><mml:mtd><mml:mi>N</mml:mi><mml:mi>u</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mi>h</mml:mi><mml:msub><mml:mi>D</mml:mi><mml:mrow><mml:mi>h</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub></mml:mfrac></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<disp-formula id="eqn-13"><label>(13)</label><mml:math id="mml-eqn-13" display="block"><mml:mtable columnalign="right left right left right left right left right left right left" rowspacing="3pt" columnspacing="0em 2em 0em 2em 0em 2em 0em 2em 0em 2em 0em" displaystyle="true"><mml:mtr><mml:mtd /><mml:mtd><mml:mi>h</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:msub><mml:mi>q</mml:mi><mml:mrow><mml:mi>w</mml:mi></mml:mrow></mml:msub><mml:msub><mml:mi>A</mml:mi><mml:mrow><mml:mi>w</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>A</mml:mi><mml:mrow><mml:mi>c</mml:mi><mml:mi>o</mml:mi><mml:mi>n</mml:mi></mml:mrow></mml:msub><mml:mo stretchy="false">(</mml:mo><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mi>w</mml:mi></mml:mrow></mml:msub><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub><mml:mo stretchy="false">)</mml:mo></mml:mrow></mml:mfrac></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula></p>
<p>(Friction factor) <italic>f</italic>: The <italic>f</italic> is used to quantitatively describe the flow characteristics of the fluid, which can be described as:
<disp-formula id="eqn-14"><label>(14)</label><mml:math id="mml-eqn-14" display="block"><mml:mi>f</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mn>2</mml:mn><mml:msub><mml:mi>D</mml:mi><mml:mrow><mml:mi>h</mml:mi></mml:mrow></mml:msub><mml:mi mathvariant="normal">&#x0394;</mml:mi><mml:mi>p</mml:mi></mml:mrow><mml:mrow><mml:msub><mml:mi>&#x03C1;</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub><mml:msubsup><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>n</mml:mi></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msubsup><mml:mi>L</mml:mi></mml:mrow></mml:mfrac></mml:math></disp-formula></p>
<p>(Performance evaluation criterion) <italic>PEC</italic>: <italic>PEC</italic> is used to quantitatively describe the <italic>THP</italic> of microchannels, which can be given by Ref. [<xref ref-type="bibr" rid="ref-42">42</xref>]:
<disp-formula id="eqn-15"><label>(15)</label><mml:math id="mml-eqn-15" display="block"><mml:mi>P</mml:mi><mml:mi>E</mml:mi><mml:mi>C</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mi>N</mml:mi><mml:mi>u</mml:mi><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mi>N</mml:mi><mml:msub><mml:mi>u</mml:mi><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msub></mml:mrow><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:mi>f</mml:mi><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:msub><mml:mi>f</mml:mi><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mn>1</mml:mn><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mn>3</mml:mn><mml:mo>)</mml:mo></mml:mrow></mml:mrow></mml:msup></mml:mfrac></mml:math></disp-formula></p>
<p>In <xref ref-type="disp-formula" rid="eqn-9">Eqs. (9)</xref>&#x2013;<xref ref-type="disp-formula" rid="eqn-15">(15)</xref>, <inline-formula id="ieqn-9"><mml:math id="mml-ieqn-9"><mml:msub><mml:mi>&#x03C1;</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the fluid density, <inline-formula id="ieqn-10"><mml:math id="mml-ieqn-10"><mml:msub><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>n</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the inlet fluid velocity, <inline-formula id="ieqn-11"><mml:math id="mml-ieqn-11"><mml:msub><mml:mi>D</mml:mi><mml:mrow><mml:mi>h</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the equivalent hydraulic diameter of the mini-channel, <inline-formula id="ieqn-12"><mml:math id="mml-ieqn-12"><mml:msub><mml:mi>&#x03BC;</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the fluid dynamic viscosity, <inline-formula id="ieqn-13"><mml:math id="mml-ieqn-13"><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the fluid channel height, <inline-formula id="ieqn-14"><mml:math id="mml-ieqn-14"><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the fluid channel weight, <inline-formula id="ieqn-15"><mml:math id="mml-ieqn-15"><mml:msub><mml:mi>&#x03C4;</mml:mi><mml:mrow><mml:mi>w</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the wall shear stress, <inline-formula id="ieqn-16"><mml:math id="mml-ieqn-16"><mml:mi>h</mml:mi></mml:math></inline-formula> is the heat transfer coefficient, <inline-formula id="ieqn-17"><mml:math id="mml-ieqn-17"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the thermal conductivity of the fluid, <inline-formula id="ieqn-18"><mml:math id="mml-ieqn-18"><mml:msub><mml:mi>q</mml:mi><mml:mrow><mml:mi>w</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the heat flux, <inline-formula id="ieqn-19"><mml:math id="mml-ieqn-19"><mml:msub><mml:mi>A</mml:mi><mml:mrow><mml:mi>w</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the area of heating surface, <inline-formula id="ieqn-20"><mml:math id="mml-ieqn-20"><mml:msub><mml:mi>A</mml:mi><mml:mrow><mml:mi>c</mml:mi><mml:mi>o</mml:mi><mml:mi>n</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the area of fluid-solid contact surface, <inline-formula id="ieqn-21"><mml:math id="mml-ieqn-21"><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mi>w</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the area-weighted average temperature of heating surface, <inline-formula id="ieqn-22"><mml:math id="mml-ieqn-22"><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the volume-weighted average fluid temperature, <inline-formula id="ieqn-23"><mml:math id="mml-ieqn-23"><mml:mi mathvariant="normal">&#x0394;</mml:mi><mml:mi>p</mml:mi></mml:math></inline-formula> is the pressure drop between the inlet and outlet, <inline-formula id="ieqn-24"><mml:math id="mml-ieqn-24"><mml:mi>L</mml:mi></mml:math></inline-formula> is the mini-channel length, <inline-formula id="ieqn-25"><mml:math id="mml-ieqn-25"><mml:mi>N</mml:mi><mml:msub><mml:mi>u</mml:mi><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-26"><mml:math id="mml-ieqn-26"><mml:msub><mml:mi>f</mml:mi><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> are the <italic>Nu</italic> and <italic>f</italic> of the traditional channel, respectively.</p>
</sec>
<sec id="s2_4">
<label>2.4</label>
<title>Grid Independence and Model Validation</title>
<p>In this work, the mesh division is performed by using Fluent Meshing. <xref ref-type="fig" rid="fig-4">Fig. 4</xref> shows the schematic diagram of grid. As shown in <xref ref-type="fig" rid="fig-4">Fig. 4</xref>, the near-wall mesh is encrypted to capture the flow characteristics of the near-wall fluid as much as possible. The effect of five different grid numbers on computational accuracy as shown in <xref ref-type="fig" rid="fig-5">Fig. 5</xref>. It can be seen that as the number of grids reaches 600,000, the increase in the grid number has very little impact on the error of calculation result. When the grid number is between 720,000 and 840,000, the error percentage of <italic>Nu</italic> and <italic>f</italic> is less than 0.43% and 0.44%, respectively. Therefore, to ensure computational accuracy and save computational cost, the mesh parameters of 720,000 are adopted for the mesh division of the geometric model, The specific grid parameters are shown in <xref ref-type="table" rid="table-3">Table 3</xref>.</p>
<fig id="fig-4">
<label>Figure 4</label>
<caption>
<title>Schematic diagram of grid: (<bold>a</bold>) axonometric view, (<bold>b</bold>) home view, and (<bold>c</bold>) side view</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-4.tif"/>
</fig><fig id="fig-5">
<label>Figure 5</label>
<caption>
<title>Effect of grid number on calculation error at <italic>Re</italic> &#x003D; 454</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-5.tif"/>
</fig><table-wrap id="table-3">
<label>Table 3</label>
<caption>
<title>Corresponding grid parameters with 720,000 grids</title>
</caption>
<table>
<colgroup>
<col align="center"/>
<col align="center"/>
<col align="center"/>
<col align="center"/>
<col align="center"/>
<col align="center"/>
</colgroup>
<thead>
<tr>
<th align="center">Parameters</th>
<th align="center">Maximum size/(mm)</th>
<th align="center">Minimum size/(mm)</th>
<th align="center">Number of boundary layers</th>
<th align="center">First layer height/(mm)</th>
<th align="center">Growth rate</th>
</tr>
</thead>
<tbody>
<tr>
<td>Value</td>
<td>0.015</td>
<td>0.0015</td>
<td>10</td>
<td>0.0005</td>
<td>1.2</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>The accuracy of the simulation method is verified before conducting numerical simulation. <xref ref-type="fig" rid="fig-6">Fig. 6</xref> shows the comparison of <italic>Nu</italic> and <italic>fRe</italic> between the simulation results and the experimental results reported by Chai et al. [<xref ref-type="bibr" rid="ref-43">43</xref>]. It is evident that a good agreement between the simulation results and experimental results has been observed within the <italic>Re</italic> range of 150 to 650. The maximum deviations of <italic>Nu</italic> and <italic>fRe</italic> for simulation results and experimental date are 2.2% and 2.6%, respectively, which confirms the feasibility of using simulation methods for the analysis of <italic>THP</italic> of MCHS.</p>
<fig id="fig-6">
<label>Figure 6</label>
<caption>
<title>Comparison of numerical results and experimental data</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-6.tif"/>
</fig>
</sec>
</sec>
<sec id="s3">
<label>3</label>
<title>Results and Discussion</title>
<sec id="s3_1">
<label>3.1</label>
<title>Flow Characteristics</title>
<p>To comprehensively evaluate the advantages of rib-cavity coupling in enhancing the <italic>THP</italic> of MCHS, the influence of ribs alone, cavities alone, and rib-cavity synergy on flow characteristics and heat transfer performance of MCHS has been analyzed. <xref ref-type="fig" rid="fig-7">Fig. 7</xref> displays the velocity distribution in mini-channels with ribs, cavities, and rib-cavity combinations at <italic>Re</italic> &#x003D; 519. Under the constraint of constant flow rate, the introduction of ribs or cavities alters the cross-sectional area of the mini-channel, leading to periodic fluctuations in fluid velocity along the flow direction. However, the differential effects of ribs and cavities on the cross-sectional area also result in distinct patterns of velocity fluctuation. For the R0.02 configuration (rib height &#x003D; 0.02 mm), the maximum velocity occurs at the mini-channel cross-section near the ribs, as the ribs narrow the fluid flow region, while the minimum velocity is observed in the upstream and downstream regions of the ribs. For the C0.08 configuration (cavity depth &#x003D; 0.08 mm), owing to the expansion of the flow cross-sectional area caused by the cavities, the minimum velocity is located near the cavity cross-section of the mini-channel. For the R0.02-C0.08 combined configuration, the mini-channel cross-sectional area remains enlarged after rib-cavity coupling, resulting in a slight reduction in velocity within the channel. Furthermore, compared with the R0.02 and C0.08 configurations, the R0.02-C0.08 configuration exhibits a more irregular velocity distribution perpendicular to the fluid flow direction.</p>
<fig id="fig-7">
<label>Figure 7</label>
<caption>
<title>Velocity contours on the <italic>y</italic> &#x003D; 0 and <italic>x</italic> &#x003D; 5 planes for R0.02, C0.08, and R0.02-C0.08. Configurations at <italic>Re</italic> &#x003D; 519: (<bold>a</bold>) R0.02, (<bold>b</bold>) C0.08, and (<bold>c</bold>) R0.02-C0.08</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-7.tif"/>
</fig>
<p><xref ref-type="fig" rid="fig-8">Fig. 8</xref> depicts the two-dimensional streamline distributions on the <italic>x</italic> &#x003D; 5 mm plane for R0.02, C0.08, and R0.02-C0.08 configurations at <italic>Re</italic> &#x003D; 519. Evidently, for the R0.02 configuration, fluid fluctuations induced by the ribs enhance fluid mixing between the near-bottom wall region and the central region of the mini-channel. For the C0.08 configuration, the cavities promote fluid mixing between the near-side wall region and the central region but exert negligible influence on fluid mixing near the bottom wall. In contrast, for the R0.02-C0.08 configuration, the coupling of ribs and cavities resulting in fluid mixing within the mini-channel that integrates the effects of ribs and cavities on fluid flow. Specially, fluid near both the bottom and side wall exhibits enhanced mixing effect with the fluid in the central region, which is more conducive to improving the heat transfer efficiency of MCHS.</p>
<fig id="fig-8">
<label>Figure 8</label>
<caption>
<title>Two-dimensional streamline distributions on the <italic>x</italic> &#x003D; 5 planes for R0.02, C0.08, and R0.02-C0.08 configurations at <italic>Re</italic> &#x003D; 519: (<bold>a</bold>) R0.02, (<bold>b</bold>) C0.08, and (<bold>c</bold>) R0.02-C0.08</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-8.tif"/>
</fig>
<p><xref ref-type="fig" rid="fig-9">Fig. 9</xref> compares the pressure variation along the flow direction in three types of mini-channels. Under the same outlet pressure condition, notable differences are observed in the inlet pressure of the three types of mini-channels. The inlet pressure of the R0.02-C0.08 configuration is the highest, followed by that of R0.02 and C0.08, respectively. This phenomenon is primarily attributed to the significant flow obstruction induced by ribs. When coupled with cavities, the intensified fluid disturbance further enhances this obstruction effect. Moreover, compared to cavities, ribs generate greater flow resistance in the mini-channel. Therefore, special attention should be paid to the impact of ribs on fluid flow during the design process.</p>
<fig id="fig-9">
<label>Figure 9</label>
<caption>
<title>Variations of pressure vs <italic>x</italic> for R0.02, C0.08, and R0.02-C0.08 configurations at <italic>Re</italic> &#x003D; 519</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-9.tif"/>
</fig>
</sec>
<sec id="s3_2">
<label>3.2</label>
<title>Heat Transfer Performance</title>
<p><xref ref-type="fig" rid="fig-10">Fig. 10</xref> compares the skin friction coefficient (<italic>C</italic><sub><italic>f</italic></sub>) of the R0.02, C0.08, and R0.02-C0.08 configurations at <italic>Re</italic> &#x003D; 519. It is observed that <italic>C</italic><sub><italic>f</italic></sub> exhibits periodic fluctuations, which can be attributed to the periodic distribution of ribs and cavities. However, the <italic>C</italic><sub><italic>f</italic></sub> relationship between the two sides and bottom walls of the three types of mini-channels is not consistent. For the bottom wall (<xref ref-type="fig" rid="fig-10">Fig. 10a</xref>), the R0.02 configuration yields the highest average <italic>C</italic><sub><italic>f</italic></sub>, followed by R0.02-C0.08 and C0.08, respectively. Furthermore, in both the R0.02 and R0.02-C0.08 configurations, the maximum C<sub><italic>f</italic></sub> occurs on the upstream side of the rib, which is attributed to the impact effect of the fluid on this region. As shown in <xref ref-type="fig" rid="fig-10">Fig. 10b</xref>, the R0.02-C0.08 configuration exhibits the highest average <italic>C</italic><sub><italic>f</italic></sub> on the side wall, followed by C0.08 and R0.02. The maximum <italic>C</italic><sub><italic>f</italic></sub> of R0.02-C0.08 and C0.08 is located on the downstream side of the cavity, which is attributed to the flow attachment of the fluid in the region. Conversely, the minimum <italic>C</italic><sub><italic>f</italic></sub> in R0.02-C0.08 and C0.08 is observed at the central region of the cavity. This phenomenon is due to the low fluid velocity in the cavity area, resulting in the thickest fluid boundary layer.</p>
<fig id="fig-10">
<label>Figure 10</label>
<caption>
<title>Normalized <italic>C</italic><sub><italic>f</italic></sub> contours and profiles on the wall for R0.02, C0.08, and R0.02-C0.08 configurations at <italic>Re</italic> &#x003D; 519: (<bold>a</bold>) interface bottom wall, (<bold>b</bold>) interface side wall</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-10.tif"/>
</fig>
<p><xref ref-type="fig" rid="fig-11">Fig. 11</xref> shows the <italic>Nu</italic> contours of R0.02, C0.08, and R0.02-C0.08 configurations at <italic>Re</italic> &#x003D; 519. Consistent with the <italic>C</italic><sub><italic>f</italic></sub> comparison results of the three types of mini-channels discussed above, the regions of maximum <italic>Nu</italic> within the mini-channel correspond one-to-one with those of maximum <italic>C</italic><sub><italic>f</italic></sub>. Besides, the average <italic>Nu</italic> values follow the order: <italic>Nu</italic> (R0.02-C0.08) &#x003E; <italic>Nu</italic> (C0.08) &#x003E; <italic>Nu</italic> (R0.02). The phenomenon indicates that the synergistic heat transfer enhancement achieved by the combination of ribs and cavities is superior to that of ribs or cavities acting alone.</p>
<fig id="fig-11">
<label>Figure 11</label>
<caption>
<title>Normalized <italic>Nu</italic> contours on the wall for R0.02, C0.08, and R0.02-C0.08 configurations at <italic>Re</italic> &#x003D; 519: (<bold>a</bold>) R0.02, (<bold>b</bold>) C0.08, and (<bold>c</bold>) R0.02-C0.08</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-11.tif"/>
</fig>
<p><xref ref-type="fig" rid="fig-12">Fig. 12</xref> displays the temperature contours of the R0.02, C0.08, and R0.02-C0.08 configurations at <italic>Re</italic> &#x003D; 519. The average fluid temperature in R0.02-C0.08 configuration is the highest, followed by that in C0.08 and then R0.02. Consequently, MCHS with coupled ribs and cavities has the best heat transfer enhancement, indicating that the coupling of ribs and cavities can integrate the advantages of ribs and cavities in enhancing the heat transfer, further improving the heat transfer effect of MCHS without significantly increasing the pressure drop.</p>
<fig id="fig-12">
<label>Figure 12</label>
<caption>
<title>Temperature contours on the <italic>y</italic> &#x003D; 0 and outlet planes for R0.02, C0.08, and R0.02-C0.08 configurations at <italic>Re</italic> &#x003D; 519: (<bold>a</bold>) R0.02, (<bold>b</bold>) C0.08, and (<bold>c</bold>) R0.02-C0.08</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-12.tif"/>
</fig>
<p>The combination of rib and cavity has different effects on the heat transfer performance and pressure drop, and the pressure drop is not necessarily optimal when the heat transfer performance is optimal, so it is necessary to select the appropriate rib and cavity structure according to the specific situation [<xref ref-type="bibr" rid="ref-44">44</xref>]. To further optimize the geometric parameters of ribs and cavities for enhanced heat transfer, the effects of the cavity distribution, cavity depth, and rib height are systematically discussed in the subsequent sections.</p>
</sec>
<sec id="s3_3">
<label>3.3</label>
<title>Effect of Cavity Distribution</title>
<p><xref ref-type="fig" rid="fig-13">Fig. 13</xref> shows the influence of cavity distribution on velocity distribution in mini-channels. As shown in <xref ref-type="fig" rid="fig-13">Fig. 13</xref>, various in cavity distribution lead to differences in fluid velocity within the central region of the mini-channels. Specially, the fluid velocity in the central region of C0.08-L is the highest, followed by C0.08-M and C0.08-R, respectively. This is mainly attributed to the varying degrees of fluid backflow induced in the cavity area by different cavity distributions. For the C0.08-R configuration, the downstream wall of the cavity is completely perpendicular to the flow direction, resulting in the strongest fluid impingement on the cavity wall. This intense impingement reduces the fluid velocity near the wall, resulting in a significant increase in fluid velocity in the central region under constant flow rate conditions. However, for the C0.08-M and C0.08-L, since the downstream wall of the cavity is not perpendicular to the flow direction, the impact of the fluid on the cavity wall is also reduced compared to C0.08-R. Therefore, the smaller the angle between the downstream wall of the cavity and the flow direction, the less the influence of fluid impact on the fluid velocity near the wall, and the smaller the fluid velocity in the central region under constant flow rate conditions.</p>
<fig id="fig-13">
<label>Figure 13</label>
<caption>
<title>Velocity contours on the <italic>z</italic> &#x003D; 0.25 plane for C0.08-L, C0.08-M, and C0.08-R configurations at <italic>Re</italic> &#x003D; 519</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-13.tif"/>
</fig>
<p><xref ref-type="fig" rid="fig-14">Fig. 14</xref> presents the comparison of <italic>C</italic><sub><italic>f</italic></sub> contours and profiles for C0.08-L, C0.08-M, and C0.08-R configurations at <italic>Re</italic> &#x003D; 519. It is observed that, the maximum <italic>C</italic><sub><italic>f</italic></sub> is located on the downstream wall region of the cavity for the mini-channel with different cavity distributions. This phenomenon arises from fluid impingement on the downstream cavity wall. Specifically, in the C0.08-R configuration, the fluid impingement on the downstream wall of the cavity is the strongest, resulting in the largest <italic>C</italic><sub><italic>f</italic></sub>. Consequently, the average <italic>C</italic><sub><italic>f</italic></sub> of C0.08-R is the highest, followed by C0.08-M and C0.08-L, respectively.</p>
<fig id="fig-14">
<label>Figure 14</label>
<caption>
<title>Normalized <italic>C</italic><sub><italic>f</italic></sub> contours and profiles vs <italic>x</italic> on the wall for C0.08-R, C0.08-M, and C0.08-L configurations at <italic>Re</italic> &#x003D; 519</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-14.tif"/>
</fig>
<p><xref ref-type="fig" rid="fig-15">Fig. 15</xref> shows the influence of cavity distribution on the wall and fluid temperature at the mini-channel outlet. The C0.08-R configuration exhibits the lowest outlet wall temperature and the highest fluid temperature, which is attributed to the heat transfer from the wall to the fluid under equal heat flux conditions. Compared to C0.08-R, the outlet fluid temperature of C0.08-M is slightly lower, while that of C0.08-L is the smallest. Therefore, the C0.08-R configuration is more conducive to heat dissipation.</p>
<fig id="fig-15">
<label>Figure 15</label>
<caption>
<title>Temperature contours on the <italic>x</italic> &#x003D; 10 plane and profiles vs <italic>z</italic> for C0.08-R, C0.08-M, and C0.08-L configurations at <italic>Re</italic> &#x003D; 519</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-15.tif"/>
</fig>
<p><xref ref-type="fig" rid="fig-16">Fig. 16</xref> shows a comparison of the <italic>Nu</italic> ratio, <italic>f</italic> ratio, and <italic>PEC</italic> for C0.08-L, C0.08-M, and C0.08-R configurations. Across all <italic>Re</italic> conditions, the <italic>Nu</italic> ratio of C0.08-R is consistently the highest, followed by C0.08-M and C0.08-L. This indicates that C0.08-R exhibits the best heat transfer performance, which is consistent with the analysis results presented in <xref ref-type="fig" rid="fig-14">Figs. 14</xref> and <xref ref-type="fig" rid="fig-15">15</xref>. Similarly, cavity distribution exerts a certain impact on <italic>f</italic> ratio, and the <italic>f</italic> ratio of C0.08-R is the highest, followed by C0.08-L and C0.08-M. However, the percentage difference in the <italic>f</italic> ratio caused by different cavity distributions is very small. Therefore, under all <italic>Re</italic> conditions, the <italic>PEC</italic> values of C0.08-R and C0.08-M are the same and higher than that of C0.08-L. To further investigate the effects of cavity depth and rib height on <italic>THP</italic>, a cavity distribution similar to that of C0.08-M is selected.</p>
<fig id="fig-16">
<label>Figure 16</label>
<caption>
<title>Comparison of <italic>Nu</italic> ratio, <italic>f</italic> ratio, and <italic>PEC</italic> for C0.08-R, C0.08-M, and C0.08-L configurations: (<bold>a</bold>) <italic>Nu/Nu</italic><sub><italic>0</italic></sub>, (<bold>b</bold>) <italic>f/f</italic><sub><italic>0</italic></sub>, (<bold>c</bold>) <italic>PEC</italic></title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-16.tif"/>
</fig>
</sec>
<sec id="s3_4">
<label>3.4</label>
<title>Effect of Rib Height</title>
<p><xref ref-type="fig" rid="fig-17">Fig. 17</xref> shows the effect of rib height on velocity fluctuations along the flow direction in the mini-channel. Under constant flow rate conditions, ribs with different heights induce periodic velocity fluctuation in the mini-channel. While the rib height does not affect the frequency of velocity fluctuations, it significantly alters their amplitude. Notably, the amplitude of velocity fluctuations in the mini-channel increases with rib height increases. Moreover, compared to rib heights of 0.02 mm and 0.04 mm, the amplitude of velocity fluctuation increases more significantly when the rib height is 0.06 mm. This phenomenon is mainly due to the sharp increase in the blocking effect of ribs on fluid as the rib height increases when the mini-channel height is only 0.02 mm. The larger the amplitude of velocity fluctuations in the mini-channel, the more favorable it is for enhancing fluid mixing between the near wall and central regions.</p>
<fig id="fig-17">
<label>Figure 17</label>
<caption>
<title>Velocity contours on the <italic>y</italic> &#x003D; 0 and <italic>x</italic> &#x003D; 5 planes and profiles vs <italic>x</italic> for R0.02-C0.06, R0.04-C0.06, and R0.06-C0.06 configurations at <italic>Re</italic> &#x003D; 519</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-17.tif"/>
</fig>
<p><xref ref-type="fig" rid="fig-18">Fig. 18</xref> displays the comparison of pressure contours along the flow direction in mini-channels with ribs of different heights. An increase in the rib height leads to a sharp increase in the flow-blocking effect, which in turn results in an increase in fluid pressure drop within the mini-channel. As shown in <xref ref-type="fig" rid="fig-18">Fig. 18</xref>, under the same fluid pressure at the mini-channel outlet, the inlet fluid pressure of R0.06-C0.06 is the highest, followed by R0.04-C0.06 and R0.02-C0.06. Therefore, an increase in the rib height not only amplifies the amplitude of velocity fluctuations but also increases flow resistance, thereby increasing power demand at the inlet of mini-channels.</p>
<fig id="fig-18">
<label>Figure 18</label>
<caption>
<title>Pressure contours on the <italic>y</italic> &#x003D; 0 plane for R0.02-C0.06, R0.04-C0.06 and R0.06-C0.06 configurations at <italic>Re</italic> &#x003D; 519</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-18.tif"/>
</fig>
<p><xref ref-type="fig" rid="fig-19">Fig. 19</xref> shows the effect of rib height on <italic>C</italic><sub><italic>f</italic></sub> and <italic>Nu</italic> contours at <italic>Re</italic> &#x003D; 519. Due to the fluid impingement and flow attachment effects on the wall, significant increases in <italic>C</italic><sub><italic>f</italic></sub> are observed on the upstream side of the ribs and the downstream side of the cavities in the mini-channel with different rib heights. At the same time, it can be observed that as the rib height increases, both the maximum and average <italic>C</italic><sub><italic>f</italic></sub> values of the mini-channel is gradually increase. Similarly, the region of the maximum <italic>Nu</italic> coincide with those of the maximum <italic>C</italic><sub><italic>f</italic></sub>. As the increase of the rib height, the average <italic>Nu</italic> gradually increases, indicating that the heat transfer performance of the mini-channel is gradually enhanced.</p>
<fig id="fig-19">
<label>Figure 19</label>
<caption>
<title>Normalized <italic>C</italic><sub><italic>f</italic></sub> and <italic>Nu</italic> contours on the wall for R0.02-C0.06, R0.04-C0.06, and R0.06-C0.06 configurations at <italic>Re</italic> &#x003D; 519</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-19.tif"/>
</fig>
<p><xref ref-type="fig" rid="fig-20">Fig. 20</xref> shows a comparison of the <italic>Nu</italic> ratio, <italic>f</italic> ratio, and <italic>PEC</italic> for R0.02-C0.06, R0.04-C0.06, and R0.06-C0.06 configurations. For the <italic>Nu</italic> ratio, all three configurations exhibit a gradual increasing trend with rising <italic>Re</italic>, indicates that increasing the <italic>Re</italic> is beneficial to enhancing the heat transfer effect of the mini-channel. Besides, the higher rib height corresponds to a higher the <italic>Nu</italic> ratio and the better the heat transfer performance, which confirming the analysis results presented in <xref ref-type="fig" rid="fig-19">Fig. 19</xref>. The maximum <italic>Nu</italic> ratio of 1.35 can be obtained for R0.06-C0.06 at <italic>Re</italic> is 519. Similarly, the <italic>f</italic> ratio of the mini-channel with different rib heights gradually increases as the rib height and <italic>Re</italic> increase, further confirming the influence of ribs on fluid flow in the mini-channel. In addition, compared to the increase in <italic>f</italic> ratio caused by increasing the rib height from 0.02 mm to 0.04 mm, the increase in <italic>f</italic> ratio is more significant when the rib height increases from 0.04 mm to 0.06 mm, which is consistent with the analysis of velocity fluctuations in <xref ref-type="fig" rid="fig-17">Fig. 17</xref>. For the <italic>PEC</italic>, although increasing the rib height can improve the heat transfer performance of the mini-channel, it also significantly increases fluid flow resistance. Consequently, the R0.02-C0.06 configuration achieving the best <italic>PEC</italic> performance, followed by R0.04-C0.06 and R0.06-C0.06, respectively. A maximum <italic>PEC</italic> of 1.198 is obtained for the R0.02-C0.06 configuration at a rig height of 0.02 mm and <italic>Re</italic> &#x003D; 519.</p>
<fig id="fig-20">
<label>Figure 20</label>
<caption>
<title>Comparison of <italic>Nu</italic> ratio, <italic>f</italic> ratio, and <italic>PEC</italic> for R0.02-C0.06, R0.04-C0.06, and R0.06-C0.06 configurations: (<bold>a</bold>) <italic>Nu/Nu</italic><sub><italic>0</italic></sub>, (<bold>b</bold>) <italic>f/f</italic><sub><italic>0</italic></sub>, (<bold>c</bold>) <italic>PEC</italic></title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-20.tif"/>
</fig>
<p>Therefore, when only heat transfer performance is considered and the influence of rib height on pressure drop is neglected, superior heat transfer performance can be achieved by selecting ribs with greater height. However, when both heat transfer performance and pressure drop are considered, a lower rib height yields the optimal overall performance, which is consistent with the research results of Lan et al. [<xref ref-type="bibr" rid="ref-45">45</xref>].</p>
</sec>
<sec id="s3_5">
<label>3.5</label>
<title>Effect of Cavity Depth</title>
<p><xref ref-type="fig" rid="fig-21">Fig. 21</xref> presents the influence of cavity depth on velocity fluctuations in mini-channels. As shown in <xref ref-type="fig" rid="fig-21">Fig. 21</xref>, the velocity exhibits periodic fluctuations along the flow direction, but the impact of changes in cavity depth on velocity fluctuation amplitude is very small. This is mainly because, although the increase in the cavity depth causes an expansion of the cross-sectional area of the mini-channel, the fluid velocity within the cavity remains very low, ultimately failing to significantly affect the velocity distribution of the fluid in the central region.</p>
<fig id="fig-21">
<label>Figure 21</label>
<caption>
<title>Velocity contours on the <italic>y</italic> &#x003D; 0 plane vs <italic>x</italic> for R0.02-C0.04, R0.02-C0.06, and R0.02-C0.08 configurations at <italic>Re</italic> &#x003D; 519</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-21.tif"/>
</fig>
<p><xref ref-type="fig" rid="fig-22">Fig. 22</xref> shows the normalized <italic>C</italic><sub><italic>f</italic></sub> contours and profiles of R0.02-C0.04, R0.02-C0.06, and R0.02-C0.08 configurations at <italic>Re</italic> &#x003D; 519. It can be seen from the contours and profiles that the increase in the cavity depth mainly results in a larger maximum <italic>C</italic><sub><italic>f</italic></sub> improvement of the mini-channel, which in turn leads to an increase in the average <italic>C</italic><sub><italic>f</italic></sub> as the cavity depth increases. This phenomenon is attributed to the enhanced flow adhesion effect of the fluid on the downstream side of the cavity as cavity depth increases, which is consistent with the results presented in <xref ref-type="fig" rid="fig-10">Figs. 10</xref>, <xref ref-type="fig" rid="fig-11">11</xref> and <xref ref-type="fig" rid="fig-19">19</xref>. Therefore, as the cavity depth increases, the heat transfer performance of the mini-channel gradually improves due to the thinning of the fluid boundary layer.</p>
<fig id="fig-22">
<label>Figure 22</label>
<caption>
<title>Normalized <italic>C</italic><sub><italic>f</italic></sub> contours and profiles on the wall for R0.02-C0.04, R0.02-C0.06, and R0.02-C0.08 configurations at <italic>Re</italic> &#x003D; 519</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-22.tif"/>
</fig>
<p><xref ref-type="fig" rid="fig-23">Fig. 23</xref> presents the effect of cavity depth on temperature contours and profiles. Corresponding to the effect of cavity depth on average <italic>C</italic><sub><italic>f</italic></sub> depicted in <xref ref-type="fig" rid="fig-22">Fig. 22</xref>, an increase in the cavity depth leads to a rise in the average fluid temperature at the mini-channel outlet.</p>
<fig id="fig-23">
<label>Figure 23</label>
<caption>
<title>(<bold>a</bold>) Temperature contours on the <italic>x</italic> &#x003D; 0, 10, and 20 planes and (<bold>b</bold>) profiles versus <italic>x</italic> for R0.02-C0.04, R0.02-C0.06 and R0.02-C0.08 configurations at <italic>Re</italic> &#x003D; 519.</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-23.tif"/>
</fig>
<p><xref ref-type="fig" rid="fig-24">Fig. 24</xref> depicts the comparison of the <italic>Nu</italic> ratio, <italic>f</italic> ratio, and <italic>PEC</italic> under different cavity depths. Notably, the <italic>Nu</italic> ratio shows a gradually increasing trend with both increasing <italic>Re</italic> and cavity depth. Specially, the maximum <italic>Nu</italic> ratio of 1.23 can be obtained at a cavity depth of 0.08 mm and <italic>Re</italic> &#x003D; 519. Similarly, an increase in the cavity depth causes an increase in flow resistance in the mini-channel, thus the <italic>f</italic> ratio increases with the increase of <italic>Re</italic> and cavity depth, but the increase is limited to within 5%. The comprehensive impact of cavity depth on the <italic>Nu</italic> ratio and the <italic>f</italic> ratio reveals that increasing cavity depth exerts a more pronounced influence on <italic>Nu</italic> amplification than on <italic>f</italic> amplification. A maximum <italic>PEC</italic> of 1.198 can be obtained at a cavity depth of 0.08 mm and 0.06 mm as well as <italic>Re</italic> &#x003D; 519.</p>
<fig id="fig-24">
<label>Figure 24</label>
<caption>
<title>Comparison of <italic>Nu</italic> ratio, <italic>f</italic> ratio, and <italic>PEC</italic> for R0.02-C0.04, R0.02-C0.06 and R0.02-C0.08 configurations: (<bold>a</bold>) <italic>Nu/Nu</italic><sub><italic>0</italic></sub>, (<bold>b</bold>) <italic>f/f</italic><sub><italic>0</italic></sub>, (<bold>c</bold>) <italic>PEC</italic></title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="FHMT_69454-fig-24.tif"/>
</fig>
</sec>
</sec>
<sec id="s4">
<label>4</label>
<title>Conclusions</title>
<p>In this work, the advantages of rib-cavity coupling in enhancing the <italic>THP</italic> of MCHS are systematically investigated, in comparison to the use of ribs or cavities alone. In addition, under rib-cavity coupling conditions, the effects of cavity distributions, cavity depths, and rib heights on the <italic>THP</italic> are analyzed to optimize appropriate parameters. The key findings are summarized as follows:
<list list-type="simple">
<list-item><label>(1)</label><p>Without significantly increasing the fluid pressure drop in the mini-channel, rib-cavity coupling can effectively enhance the convective heat transfer effect between the fluid and the bottom as well as sides wall of MCHS, and improve the <italic>THP</italic> of MCHS compared to ribs or cavities alone.</p></list-item>
<list-item><label>(2)</label><p>Variations in cavity distribution alter the intensity of fluid impingement on the wall, which in turn has different effects on the <italic>THP</italic> of MCHS. The cavity distribution in C0.08-M configuration yields optimal <italic>THP</italic> of MCHS.</p></list-item>
<list-item><label>(3)</label><p>Increasing the rib height effectively enhances the heat transfer performance of MCHS, but it also leads to a significant increase in pressure drop. Compared to traditional mini-channels, when the rib height is 0.06 mm, the <italic>Nu</italic> ratio and <italic>f</italic> ratio increase by 35% and 19%, respectively. However, MCHS can obtain optimal <italic>THP</italic> when the rib height is the minimum value of 0.02 mm. Therefore, the selection of rib height needs to be determined in conjunction with the requirements for the heat transfer and the pressure drop.</p></list-item>
<list-item><label>(4)</label><p>Increasing the cavity depth can improve the heat transfer performance and the pressure drop of MCHS, while also enhancing the <italic>THP</italic>. The highest <italic>PEC</italic> of 1.198 is achieved when the cavity depth is 0.08 mm and 0.06 mm, which increases by 19.8% compared to traditional mini-channels.</p></list-item>
</list></p>
</sec>
</body>
<back>
<ack>
<p>This work was supported by the Sichuan Natural Science Foundation.</p>
</ack>
<sec>
<title>Funding Statement</title>
<p>The research was funded by the Sichuan Natural Science Foundation, grant number 2023NSFSC0870.</p>
</sec>
<sec>
<title>Author Contributions</title>
<p>The authors confirm contribution to the paper as follows: study conception and design: Wenling Liao; data collection: Shuaimei Lian; analysis and interpretation of results: Shuaimei Lian, Pingping Liu, Wenling Liao; draft manuscript preparation: Shuaimei Lian, Pingping Liu. All authors reviewed the results and approved the final version of the manuscript.</p>
</sec>
<sec sec-type="data-availability">
<title>Availability of Data and Materials</title>
<p>The data that support the findings of this study are available from the corresponding author, Wenling Liao, upon reasonable request.</p>
</sec>
<sec>
<title>Ethics Approval</title>
<p>Not applicable.</p>
</sec>
<sec sec-type="COI-statement">
<title>Conflicts of Interest</title>
<p>The authors declare no conflicts of interest to report regarding the present study.</p>
</sec>
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