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<front>
<journal-meta>
<journal-id journal-id-type="publisher-id">Front. Physiol.</journal-id>
<journal-title>Frontiers in Physiology</journal-title>
<abbrev-journal-title abbrev-type="pubmed">Front. Physiol.</abbrev-journal-title>
<issn pub-type="epub">1664-042X</issn>
<publisher>
<publisher-name>Frontiers Media S.A.</publisher-name>
</publisher>
</journal-meta>
<article-meta>
<article-id pub-id-type="publisher-id">1518732</article-id>
<article-id pub-id-type="doi">10.3389/fphys.2025.1518732</article-id>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Physiology</subject>
<subj-group>
<subject>Original Research</subject>
</subj-group>
</subj-group>
</article-categories>
<title-group>
<article-title>Prediction of time averaged wall shear stress distribution in coronary arteries&#x2019; bifurcation varying in morphological features via deep learning</article-title>
<alt-title alt-title-type="left-running-head">Sarkhosh et al.</alt-title>
<alt-title alt-title-type="right-running-head">
<ext-link ext-link-type="uri" xlink:href="https://doi.org/10.3389/fphys.2025.1518732">10.3389/fphys.2025.1518732</ext-link>
</alt-title>
</title-group>
<contrib-group>
<contrib contrib-type="author">
<name>
<surname>Sarkhosh</surname>
<given-names>Mohammad Hossein</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
<xref ref-type="aff" rid="aff2">
<sup>2</sup>
</xref>
<role content-type="https://credit.niso.org/contributor-roles/writing-original-draft/"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Edrisnia</surname>
<given-names>Hadis</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
<role content-type="https://credit.niso.org/contributor-roles/writing-original-draft/"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Raveshi</surname>
<given-names>Mohammad Reza</given-names>
</name>
<xref ref-type="aff" rid="aff3">
<sup>3</sup>
</xref>
<role content-type="https://credit.niso.org/contributor-roles/funding-acquisition/"/>
<role content-type="https://credit.niso.org/contributor-roles/Writing - review &#x26; editing/"/>
</contrib>
<contrib contrib-type="author" corresp="yes">
<name>
<surname>Sharbatdar</surname>
<given-names>Mahkame</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
<xref ref-type="corresp" rid="c001">&#x2a;</xref>
<uri xlink:href="https://loop.frontiersin.org/people/2880923/overview"/>
<role content-type="https://credit.niso.org/contributor-roles/Writing - review &#x26; editing/"/>
</contrib>
</contrib-group>
<aff id="aff1">
<sup>1</sup>
<institution>Faculty of Mechanical Engineering</institution>, <institution>K. N. Toosi University of Technology</institution>, <addr-line>Tehran</addr-line>, <country>Iran</country>
</aff>
<aff id="aff2">
<sup>2</sup>
<institution>Faculty of Mechanical Engineering</institution>, <institution>Sharif University of Technology</institution>, <addr-line>Tehran</addr-line>, <country>Iran</country>
</aff>
<aff id="aff3">
<sup>3</sup>
<institution>Department of Mechanical and Aerospace Engineering</institution>, <addr-line>Monash University</addr-line>, <country>Australia</country>
</aff>
<author-notes>
<fn fn-type="edited-by">
<p>
<bold>Edited by:</bold> <ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/1205009/overview">Yonghui Qiao</ext-link>, Northwestern Polytechnical University, China</p>
</fn>
<fn fn-type="edited-by">
<p>
<bold>Reviewed by:</bold> <ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/1784354/overview">Wei Xuan Chan</ext-link>, Imperial College London, United Kingdom</p>
<p>
<ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/1946143/overview">Xuelan Zhang</ext-link>, University of Science and Technology Beijing, China</p>
</fn>
<corresp id="c001">&#x2a;Correspondence: Mahkame Sharbatdar, <email>m.sharbatdar@kntu.ac.ir</email>
</corresp>
</author-notes>
<pub-date pub-type="epub">
<day>04</day>
<month>03</month>
<year>2025</year>
</pub-date>
<pub-date pub-type="collection">
<year>2025</year>
</pub-date>
<volume>16</volume>
<elocation-id>1518732</elocation-id>
<history>
<date date-type="received">
<day>28</day>
<month>10</month>
<year>2024</year>
</date>
<date date-type="accepted">
<day>04</day>
<month>02</month>
<year>2025</year>
</date>
</history>
<permissions>
<copyright-statement>Copyright &#xa9; 2025 Sarkhosh, Edrisnia, Raveshi and Sharbatdar.</copyright-statement>
<copyright-year>2025</copyright-year>
<copyright-holder>Sarkhosh, Edrisnia, Raveshi and Sharbatdar</copyright-holder>
<license xlink:href="http://creativecommons.org/licenses/by/4.0/">
<p>This is an open-access article distributed under the terms of the Creative Commons Attribution License (CC BY). The use, distribution or reproduction in other forums is permitted, provided the original author(s) and the copyright owner(s) are credited and that the original publication in this journal is cited, in accordance with accepted academic practice. No use, distribution or reproduction is permitted which does not comply with these terms.</p>
</license>
</permissions>
<abstract>
<sec>
<title>Introduction</title>
<p>Understanding the hemodynamics of blood circulation is crucial to reveal the processes contributing to stenosis and atherosclerosis development.</p>
</sec>
<sec>
<title>Method</title>
<p>Computational fluid dynamics (CFD) facilitates this understanding by simulating blood flow patterns in coronary arteries. Nevertheless, applying CFD in fast-response scenarios presents challenge due to the high computational costs. To overcome this challenge, we integrate a deep learning (DL) method to improve efficiency and responsiveness. This study presents a DL approach for predicting Time-Averaged Wall Shear Stress (TAWSS) values in coronary arteries&#x2019; bifurcation.</p>
</sec>
<sec>
<title>Results</title>
<p>To prepare the dataset, 1800 idealized models with varying morphological parameters are created. Afterward, we design a CNN-based U-net architecture to predict TAWSS by the point cloud of the geometries. Moreover, this architecture is implemented using TensorFlow 2.3.0. Our results indicate that the proposed algorithms can generate results in less than one second, showcasing their suitability for applications in terms of computational efficiency.</p>
</sec>
<sec>
<title>Discussion</title>
<p>Furthermore, the DL-based predictions demonstrate strong agreement with results from CFD simulations, with a normalized mean absolute error of only 2.53% across various cases.</p>
</sec>
</abstract>
<kwd-group>
<kwd>hemodynamics</kwd>
<kwd>deep learning</kwd>
<kwd>coronary arteries</kwd>
<kwd>bifurcation</kwd>
<kwd>computational fluid dynamics (CFD)</kwd>
<kwd>time-averaged wall shear stress (TAWSS)</kwd>
</kwd-group>
<custom-meta-wrap>
<custom-meta>
<meta-name>section-at-acceptance</meta-name>
<meta-value>Computational Physiology and Medicine</meta-value>
</custom-meta>
</custom-meta-wrap>
</article-meta>
</front>
<body>
<sec id="s1">
<title>1 Introduction</title>
<p>Despite significant advancements in medical therapy and the availability of both invasive and noninvasive diagnostic tests, cardiovascular disease continues to persist as the leading cause of mortality globally (<xref ref-type="bibr" rid="B33">Maurovich-Horvat et al., 2014</xref>; <xref ref-type="bibr" rid="B7">Benvidi and Firoozabadi, 2024</xref>). It is widely acknowledged that coronary artery hemodynamics and vessel geometry play a crucial role in the development and diagnosis of coronary artery disease (CAD) (<xref ref-type="bibr" rid="B35">Pinho et al., 2019</xref>; <xref ref-type="bibr" rid="B14">Eslami et al., 2020a</xref>). Due to the presence of turbulence in the flow, the frictional force exerted on the vessel wall, known as wall shear stress (WSS), can initiate plaque formation at regions of flow separation (<xref ref-type="bibr" rid="B10">Dong et al., 2015</xref>; <xref ref-type="bibr" rid="B46">Temov and Sun, 2016</xref>).</p>
<p>The left coronary artery and its bifurcations, specifically the left anterior descending (LAD) and left circumflex (LCX), are susceptible to the development of atherosclerosis (<xref ref-type="bibr" rid="B50">Zhang and Dou, 2015</xref>; <xref ref-type="bibr" rid="B11">Edrisnia et al., 2024</xref>). Additionally, bifurcations pose a heightened risk for restenosis and stent thrombosis (<xref ref-type="bibr" rid="B8">Chaichana et al., 2011</xref>; <xref ref-type="bibr" rid="B5">Beier et al., 2016</xref>; <xref ref-type="bibr" rid="B17">Freidoonimehr et al., 2021a</xref>; <xref ref-type="bibr" rid="B18">Freidoonimehr et al., 2021b</xref>). Hence, in clinical practice, it is imperative to assess these regions to identify high-risk patients who may have CAD at an early stage (<xref ref-type="bibr" rid="B21">Hoque et al., 2021</xref>). Parameters based on WSS, such as time-averaged wall shear stress (TAWSS) play a fundamental role in the progression of atherosclerosis, particularly in transient studies (<xref ref-type="bibr" rid="B4">Arzani et al., 2021</xref>). Studies have shown that a wider bifurcation angle is associated with lower wall shear stress and higher oscillatory shear index (OSI), which can contribute to the stimulation of atherosclerosis (<xref ref-type="bibr" rid="B44">Sun and Chaichana, 2016</xref>; <xref ref-type="bibr" rid="B45">Sun and Chaichana, 2017</xref>; <xref ref-type="bibr" rid="B30">Liu et al., 2019</xref>). Moreover, precise characterization of blood rheology, which involves the application of non-Newtonian models, is particularly crucial in these instances (<xref ref-type="bibr" rid="B36">Pinto and Campos, 2016</xref>; <xref ref-type="bibr" rid="B41">Sandeep and Shine, 2021</xref>).</p>
<p>Due to the shear thinning behavior of blood in small arteries, CFD is becoming increasingly essential in hemodynamics&#x2019; calculations. The accuracy of input data, such as vessel geometry information, appropriate boundary conditions, and material models, significantly influences the reliability and precision of CFD results (<xref ref-type="bibr" rid="B19">Gijsen et al., 2019</xref>; <xref ref-type="bibr" rid="B37">Rabbi et al., 2020</xref>; <xref ref-type="bibr" rid="B12">Edrisnia and Sharbatdar, 2024</xref>). However, the CFD technique is not well-suited for fast-response applications due to the inherent delay and relatively high computational costs involved. As a result, there is a need for an alternative approach to overcome this limitation.</p>
<p>Many state-of-the-art machine learning (ML) techniques, such as Convolutional Neural Networks (CNNs) and Multi-Layer Perceptrons (MLPs), are widely utilized for various applications, including 2D image segmentation and 3D point cloud segmentation (<xref ref-type="bibr" rid="B6">Bello et al., 2020</xref>; <xref ref-type="bibr" rid="B20">Hirzi et al., 2022</xref>; <xref ref-type="bibr" rid="B39">Sabet et al., 2022</xref>). Inspired by these algorithms, there is significant potential for employing them in hemodynamic parameter prediction. However, in scenarios with limited data availability, deep learning models, such as convolutional and recurrent neural networks, often lack robustness and fail to guarantee convergence. Therefore, ensuring access to sufficient and high-quality data is crucial for achieving reliable and accurate results. One promising approach to address data limitations is the use of idealized models in biomedical applications, which can simulate conditions with acceptable agreement to patient-specific cases. These enriched datasets improve algorithm training, enhancing their robustness and performance in real-world applications.</p>
<p>In fluid dynamics applications involving direct calculation of the flow field, ML, and deep learning (DL) approaches have been employed to address computational challenges. These techniques offer promising solutions for expediting computations and enabling fast-response simulations. For instance, Jordanski et al. (<xref ref-type="bibr" rid="B24">Jordanski et al., 2018</xref>) have utilized ML techniques to predict the WSS distribution in carotid bifurcation and abdominal aortic aneurysms. Liang et al. (<xref ref-type="bibr" rid="B27">Liang et al., 2017</xref>) have deployed a ML approach to establish the connections between shape features and the rupture risk of ascending aortic aneurysms as predicted by finite element analysis (FEA). Furthermore, Liang et al. (<xref ref-type="bibr" rid="B28">Liang et al., 2018</xref>; <xref ref-type="bibr" rid="B29">2020</xref>) have developed a DL model, including deep neural networks, to directly estimate the stress distributions in the aorta. <xref ref-type="bibr" rid="B32">Madani et al. (2018)</xref> have created data-efficient DL classifiers for cardiology prediction tasks, with a particular emphasis on relevant structures using pipeline-supervised models. Additionally, <xref ref-type="bibr" rid="B32">Madani et al. (2018)</xref> have investigated the connection between ML and finite element modeling for WSS prediction of arterial in the context of atherosclerosis. <xref ref-type="bibr" rid="B16">Farnoud et al. (2023)</xref> have employed random forest and gradient boosting models for ML analysis of drug delivery to nasal epithelium.</p>
<p>Similar studies are summarized in <xref ref-type="table" rid="T1">Table 1</xref>. The application of ML or DL to predict hemodynamic parameters, such as Fractional Flow Reserve, FFR, and forecast flow field patterns has remained limited (<xref ref-type="bibr" rid="B22">Itu et al. (2016)</xref>). However, there has been an implementation of a reduced-order model, which is highly specialized but has limited applicability. In other investigations, many researchers have employed the Point Net architecture to predict hemodynamic parameters in cardiovascular geometries. <xref ref-type="bibr" rid="B25">Li et al. (2021a)</xref> have developed a DL approach to predict the hemodynamics of different cerebral aneurysms before and after the insertion of a flow diverter (FD) stent. Moreover, <xref ref-type="bibr" rid="B26">Li et al. (2021b)</xref> have created cardiovascular hemodynamic point datasets and a dual sample channel DL network, capable of analyzing and reproducing the relationship between cardiovascular geometry and internal hemodynamics. The PointNet algorithm, originally proposed for hemodynamic prediction, is also tested in this study to compare its performance with the proposed model, as shown in <xref ref-type="table" rid="T1">Table 1</xref>.</p>
<table-wrap id="T1" position="float">
<label>TABLE 1</label>
<caption>
<p>Comparison of ML- and DL-based methods on hemodynamic prediction.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Methodology</th>
<th align="center">Output</th>
<th align="center">Model</th>
<th align="center">Input</th>
<th align="center">Data set</th>
<th align="center">Performance</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">Proposed model</td>
<td align="center">TAWSS</td>
<td align="center">Coronary artery bifurcation</td>
<td align="center">Fixed number of point cloud</td>
<td align="center">1800</td>
<td align="center">MRE &#x3c;11.3%<break/>NAME &#x3c;2.5%</td>
</tr>
<tr>
<td align="center">Point Net</td>
<td align="center">TAWSS</td>
<td align="center">Coronary artery bifurcation</td>
<td align="center">Fixed number of point cloud</td>
<td align="center">1800</td>
<td align="center">MRE &#x3c;24%<break/>NAME &#x3c; &#x2212;</td>
</tr>
<tr>
<td align="center">Neural network approach<break/>Itu et al. (<xref ref-type="bibr" rid="B22">Itu et al., 2016</xref>)</td>
<td align="center">FFR<break/>value</td>
<td align="center">Coronary artery</td>
<td align="center">Geometric parameter</td>
<td align="center">12,000</td>
<td align="center">Error &#x3d; 0.03%</td>
</tr>
<tr>
<td align="center">U-net architecture<break/>
<xref ref-type="bibr" rid="B43">Su et al. (2020)</xref>
</td>
<td align="center">WSS</td>
<td align="center">Coronary artery</td>
<td align="center">Fixed number of vessel&#x2019;s centerline coordination</td>
<td align="center">2000</td>
<td align="center">MAE &#x3c;11.7<break/>NAME &#x3c;2.5%</td>
</tr>
<tr>
<td align="center">Point net<break/>
<xref ref-type="bibr" rid="B25">Li et al. (2021a)</xref>
</td>
<td align="center">Pressure, velocity</td>
<td align="center">idealized cerebral aneurysm</td>
<td align="center">Flexible point cloud</td>
<td align="center">500</td>
<td align="center">MRE &#x3c;13%<break/>NAME &#x3c;6.5%</td>
</tr>
<tr>
<td align="center">Point net<break/>
<xref ref-type="bibr" rid="B47">Wang et al. (2023a)</xref>
</td>
<td align="center">Pressure, velocity</td>
<td align="center">Clinical geometry with carotid artery stenosis</td>
<td align="center">High resolution point cloud</td>
<td align="center">1,000</td>
<td align="center">MRE &#x3c;12.5%<break/>NAME &#x3c;7.5%</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>Studies on PointNet consistently highlight its strength in capturing global geometric variations but reveal its limitations in addressing local variations. To overcome this, researchers often train separate PointNet models for pre-treatment and post-treatment simulations. In contrast, <xref ref-type="bibr" rid="B43">Su et al. (2020)</xref> proposed an alternative approach using idealized geometries with varying stenosis diameters and locations, employing multivariable linear regression (MLR), multi-layer perceptrons (MLPs), and convolutional neural networks (CNNs) as substitutes for computational fluid dynamics (CFD) to compute wall shear stress (WSS) during medical examinations. Although previous study (<xref ref-type="bibr" rid="B43">Su et al., 2020</xref>) described their input in <xref ref-type="table" rid="T1">Table 1</xref> as a &#x201c;fixed number of vessel&#x2019;s centerline coordinates,&#x201d; they effectively utilized point cloud data in a different coordinate system. Specifically, their input features included the centerline coordinates in the XY plane, along with the distance and angle relative to the centerline. Their study focused on a single coronary artery, varying morphological parameters such as vessel diameter, stenosis, and curvature.</p>
<p>To the best of our knowledge, researchers have proposed DL algorithm for predicting the TAWSS of bifurcations. However, no research has investigated DL-driven prediction on the cases varying in diameters and angulations using U-net structure. For this purpose, point cloud datasets are developed based on CFD simulations of ideal coronary bifurcations, including its hemodynamic parameters. Additionally, a CNN-based U-net is developed to generate the point cloud input for predicting TAWSS at each point. Finally, the effectiveness of the DL approach is assessed by evaluating the prediction errors in TAWSS.</p>
</sec>
<sec sec-type="materials|methods" id="s2">
<title>2 Material and method</title>
<sec id="s2-1">
<title>2.1 Dataset generation: creation of models and CFD simulation</title>
<p>To generate the dataset, various healthy coronary artery bifurcation geometries across a broad demographic with transient boundary conditions are simulated using the finite volume method. A 3D parametric model is first established to efficiently create diverse artery geometries as shown in <xref ref-type="fig" rid="F1">Figure 1A</xref>. Furthermore, five morphological parameters, namely, the diameters of the left main coronary artery (<inline-formula id="inf1">
<mml:math id="m1">
<mml:mrow>
<mml:msub>
<mml:mi>D</mml:mi>
<mml:mrow>
<mml:mi>L</mml:mi>
<mml:mi>M</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>), left circumflex artery (<inline-formula id="inf2">
<mml:math id="m2">
<mml:mrow>
<mml:msub>
<mml:mi>D</mml:mi>
<mml:mrow>
<mml:mi>L</mml:mi>
<mml:mi>C</mml:mi>
<mml:mi>x</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>), and left anterior descending (<inline-formula id="inf3">
<mml:math id="m3">
<mml:mrow>
<mml:msub>
<mml:mi>D</mml:mi>
<mml:mrow>
<mml:mi>L</mml:mi>
<mml:mi>A</mml:mi>
<mml:mi>D</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>), along with the angles between LM and LAD (&#x263;) and between LAD and LCx (&#x3b1;), are selected. A total of 1800 bifurcation models were generated with scripting option in ANSYS workbench using values selected from a reasonable range, with detailed parameter values shown in <xref ref-type="table" rid="T2">Table 2</xref> and corresponding references provided in <xref ref-type="sec" rid="s13">Supplementary Tables S3, 4</xref>. Additionally, <xref ref-type="sec" rid="s13">Supplementary Figure S2</xref> presents a visualization of a number of generated idealized geometries with varying morphological features.</p>
<fig id="F1" position="float">
<label>FIGURE 1</label>
<caption>
<p>
<bold>(A)</bold> An example of an idealized geometry depicting a 3D bifurcation, <bold>(B)</bold> pressure wave for LAD and LCx outlets, <bold>(C)</bold> flow velocity for LM inlet, and <bold>(D)</bold> verification of the results. Comparison between peak inlet pressure at LM in the proposed model and Jahromi et al. study (<xref ref-type="bibr" rid="B23">Jahromi et al., 2019</xref>).</p>
</caption>
<graphic xlink:href="fphys-16-1518732-g001.tif"/>
</fig>
<table-wrap id="T2" position="float">
<label>TABLE 2</label>
<caption>
<p>The range of morphological parameters.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Parameter</th>
<th align="center">
<inline-formula id="inf4">
<mml:math id="m4">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">D</mml:mi>
<mml:mrow>
<mml:mi mathvariant="italic">L</mml:mi>
<mml:mi mathvariant="italic">M</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> (mm)</th>
<th align="center">
<inline-formula id="inf5">
<mml:math id="m5">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">D</mml:mi>
<mml:mrow>
<mml:mi mathvariant="italic">L</mml:mi>
<mml:mi mathvariant="italic">C</mml:mi>
<mml:mi mathvariant="italic">x</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> (mm)</th>
<th align="center">
<inline-formula id="inf6">
<mml:math id="m6">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="italic">D</mml:mi>
<mml:mrow>
<mml:mi mathvariant="italic">L</mml:mi>
<mml:mi mathvariant="italic">A</mml:mi>
<mml:mi mathvariant="italic">D</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> (mm)</th>
<th align="center">&#x263; (degree)</th>
<th align="center">&#x3b1; (degree)</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">Range</td>
<td align="center">2.18&#x2013;4.18</td>
<td align="center">1.5&#x2013;3.5</td>
<td align="center">1.5&#x2013;3.5</td>
<td align="center">112.75&#x2013;172.75</td>
<td align="center">15&#x2013;130</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>To create the computational fluid domain, ANSYS meshing software is utilized and a mesh is applied with tetrahedral control volumes in the geometry. Seven prismatic layers with a growth rate of 1.2 are deployed to minimize computational errors near the wall. Moreover, grid independence is studied using the geometry with the largest diameters by evaluating TAWSS values at 6 points on the wall shown in <xref ref-type="sec" rid="s13">Supplementary Figure S1</xref>, across three different mesh resolutions with precise TAWSS values comparison provided in <xref ref-type="sec" rid="s13">Supplementary Table S2</xref>. Therefore, applying this process in a geometry with largest diameters is more effective way than including a larger subset of the 1800 geometries because fine mesh in this case would be extra fine for smaller bifurcation models.</p>
<p>The results of this comparison are presented in <xref ref-type="table" rid="T3">Table 3</xref>. As depicted, using the medium mesh can provide us with accurate simulations and hence is chosen for its balance between accuracy and computational cost. The difference error with fine mesh, 0.8%, is almost negligible.</p>
<table-wrap id="T3" position="float">
<label>TABLE 3</label>
<caption>
<p>Numerical sensitivity study.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Mesh type</th>
<th align="center">Cells number</th>
<th align="center">Node number</th>
<th align="center">Prismatic layer</th>
<th colspan="2" align="center">Error (%)</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">Coarse</td>
<td align="center">1,554,000</td>
<td align="center">531,000</td>
<td align="center">7</td>
<td rowspan="2" align="center">3.58</td>
<td align="left"/>
</tr>
<tr>
<td align="center">Medium</td>
<td align="center">2,392,000</td>
<td align="center">794,000</td>
<td align="center">7</td>
<td rowspan="2" align="center">0.8</td>
</tr>
<tr>
<td align="center">Fine</td>
<td align="center">3,342,000</td>
<td align="center">1,085,000</td>
<td align="center">7</td>
<td align="left"/>
</tr>
</tbody>
</table>
</table-wrap>
<p>The boundary conditions are representative of a general healthy population obtained from 20 healthy subjects in the Davies et al. study (<xref ref-type="bibr" rid="B9">Davies et al., 2006</xref>). They showed that inlet and outlet BCs consist of predominant waves that follow a similar pattern across all subjects during each cardiac cycle. Although the intensity and timing of individual waves varied between the subjects, the wave remained consistently similar in the left coronary arteries. Consequently, this consistency justifies the selection of following conditions for the 1800 geometries studied. For the outlets in the LCx and LAD coronaries are pressure waves throughout a cardiac cycle provided in <xref ref-type="fig" rid="F1">Figure 1B</xref>, while for the inlet in the LM is fully-developed time-varying flow velocity wave shown in <xref ref-type="fig" rid="F1">Figure 1C</xref>. Consequently, considering the mass flow rate, the BCs do not depend on the morphological parameters and mass flow rate can adjust itself in different geometries. To verify CFD models, two diagrams are compared in <xref ref-type="fig" rid="F1">Figure 1D</xref> from the current simulation and data obtained from Jahromi et al. study (<xref ref-type="bibr" rid="B23">Jahromi et al., 2019</xref>). The comparison contains the maximum pressure at the inlet in LM.</p>
<p>Each numerical model is extended at inlet to seven times their diameters for fully developed profile and numerical stability, then a flat velocity boundary condition is applied at the inlet (<xref ref-type="bibr" rid="B34">Numata et al., 2017</xref>; <xref ref-type="bibr" rid="B43">Su et al., 2020</xref>). Furthermore, based on the time step dependency analysis shown in <xref ref-type="sec" rid="s13">Supplementary Table S1</xref>, a time step size of 0.0025 [s] is selected for the simulations. Additionally, the simulations are run over three cardiac cycles to ensure repetitive steady state, as the difference in TAWSS values at the points shown in <xref ref-type="sec" rid="s13">Supplementary Figure S2</xref> between the third and fourth cycles is only 0.61%, confirming the convergence and periodic consistency of the results. The continuity and Navier-Stokes equations (<xref ref-type="disp-formula" rid="e1">Equations 1</xref>, <xref ref-type="disp-formula" rid="e2">2</xref>), respectively) governing the blood flow are solved using the CFD software ANSYS-CFX 20.1 (ANSYS Inc., PA, USA):<disp-formula id="e1">
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</disp-formula>where <inline-formula id="inf7">
<mml:math id="m9">
<mml:mrow>
<mml:mover accent="true">
<mml:mi>u</mml:mi>
<mml:mo>&#x2192;</mml:mo>
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<mml:mo>,</mml:mo>
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<mml:mo>,</mml:mo>
<mml:mi>p</mml:mi>
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<mml:math id="m10">
<mml:mrow>
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</inline-formula> represent fluid velocity vector, density, pressure, and dynamic viscosity, respectively.</p>
<p>In the CFD simulation, a high-resolution advection scheme is employed alongside the second-order backward Euler method for time-stepping, achieving a balance between precision and computational efficiency in transient simulations. Convergence is meticulously managed with up to 500 coefficient loops per time step and an RMS residual target of 1E-5 to ensure both accuracy and reliability of the results.</p>
<p>The blood is considered to be an incompressible, laminar fluid with a density of 1,060&#xa0;kg <inline-formula id="inf9">
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<table-wrap id="T4" position="float">
<label>TABLE 4</label>
<caption>
<p>Parameters of Carreau-Yasuda blood viscosity model.</p>
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<table>
<thead valign="top">
<tr>
<th align="center">
<inline-formula id="inf13">
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<p>TAWSS over a cardiac cycle, is calculated to reach a meaningful conclusion and is extracted from each model to be utilized in the DL algorithm. The formula for computing TAWSS is given by <xref ref-type="disp-formula" rid="e4">Equation 4</xref> as:<disp-formula id="e4">
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</mml:math>
<label>(4)</label>
</disp-formula>
</p>
<p>Previous studies show different instant WSS values but similar TAWSS values in rigid and fluid-structure interaction (FSI) models (<xref ref-type="bibr" rid="B49">Zeng et al., 2003</xref>; <xref ref-type="bibr" rid="B15">Eslami et al., 2020b</xref>). Therefore, the coronary artery is assumed to be rigid during the simulations due to computational efficiency.</p>
</sec>
<sec id="s2-2">
<title>2.2 DL model</title>
<sec id="s2-2-1">
<title>2.2.1 Supervised learning</title>
<p>Supervised learning is a ML approach where a model is trained on labeled input-output pairs to learn patterns and predict outcomes on new, unseen data. The process involves minimizing the error between predicted outputs and ground truth labels using various algorithms such as linear regression, support vector machines, and deep neural networks (<xref ref-type="bibr" rid="B38">Rashidi et al., 2019</xref>). As TAWSS is continuous, regression algorithms are utilized to predict TAWSS in bifurcation models. In this section, we introduce the input and output of the DL algorithm, followed by the introduction of U-net architecture, tailored for predicting TAWSS in diverse bifurcation models. For this purpose, out of the 1800 models, 60 models are randomly selected in each batch of 300 models, resulting in a total of 360 models used for testing. Additionally, 10% of the remaining 1440 models are chosen for validation from the training set.</p>
</sec>
<sec id="s2-2-2">
<title>2.2.2 Input and output variables</title>
<p>ML algorithms often struggle with unstructured data. To address this, an interpolation step is applied during post-processing to map the TAWSS values onto a structured surface mesh (4,096 &#xd7; 3), ensuring that each simulation result is in a structured format. The input of the DL is a point cloud data (mesh nodes coordinates) extracted from CFD-based results with a uniform distribution, representing the geometry of the bifurcation model and the output is the TAWSS at each point. <xref ref-type="fig" rid="F2">Figure 2</xref> illustrates the structure of the input and output components, designed to replace the function of CFD simulation in fast-response applications. As discussed previously, all geometries have 4,096 nodes, the input includes 3 components of each node (<inline-formula id="inf23">
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</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>), and dimensions of the input and the output are 4,096 &#xd7; 3 and 4,096 &#xd7; 1, respectively. The proposed architecture consists of two main parts: encoder and decoder as it is depicted in <xref ref-type="fig" rid="F2">Figure 2</xref>. In the encoder part main features of point clouds are extracted. After which, these features are transformed to the TAWSS values using decoder section.</p>
<fig id="F2" position="float">
<label>FIGURE 2</label>
<caption>
<p>Concept of proposed model.</p>
</caption>
<graphic xlink:href="fphys-16-1518732-g002.tif"/>
</fig>
</sec>
<sec id="s2-2-3">
<title>2.2.3 DL model</title>
<p>U-Net is a CNN structure developed for segmenting biomedical images, specifically for tasks requiring detailed segmentation, it comprises a contracting and expanding path formed a U-shape (<xref ref-type="bibr" rid="B3">Arvind et al., 2023</xref>). The contracting path uses convolutional and pooling layers to reduce image dimensions and enhance feature extraction. Meanwhile, the expanding path employs upsampling and concatenation to recover spatial resolution and refine segmentation. Notably, U-Net incorporates skip connections to preserve spatial information, aiding accurate segmentation. Widely adopted, U-Net&#x2019;s simplicity and adaptability have made it popular in various computer vision applications, including satellite imagery (<xref ref-type="bibr" rid="B2">Alsabhan and Alotaiby, 2022</xref>) and road segmentation (<xref ref-type="bibr" rid="B47">Wang R. et al., 2023</xref>).</p>
<p>The architecture used to derive TAWSS from the point clouds of geometry is a modified U-net structure, as shown in <xref ref-type="fig" rid="F3">Figure 3</xref>. Initially, the resolution of the input geometry increases from 4,096 &#xd7; 3 to 4,096 &#xd7; 8 after two neural network layers. Then it is reshaped to a dimension of 64 &#xd7; 64 &#xd7; 8, followed by the application of a convolutional layer with same depth to 64 &#xd7; 64 &#xd7; 8. Another convolutional layer is then applied, maintaining the same dimensions. In the encoder section, four max-pooling operations progressively halve the spatial dimensions. For instance, the first max-pooling layer reduces the dimensions from 64 &#xd7; 64 &#xd7; 8 to 32 &#xd7; 32 &#xd7; 8. After each max-pooling step, two convolutional layers are applied while keeping the same dimensions. Once the final max-pooling is completed, the encoded data passes through four additional convolutional layers.</p>
<fig id="F3" position="float">
<label>FIGURE 3</label>
<caption>
<p>The proposed model features a CNN layer structured in a U-Net architecture, where each encoded and decoded layer is color-coded for clarity. The skip connections transfer encoded data to their corresponding decoded layers for concatenation.</p>
</caption>
<graphic xlink:href="fphys-16-1518732-g003.tif"/>
</fig>
<p>In the decoder section, four transposed convolution layers are used to progressively restore the spatial dimensions. For example, the first transposed layer expands the dimensions from 4 &#xd7; 4 &#xd7; 8 to 8 &#xd7; 8 &#xd7; 8, followed by a skip connection that merges the corresponding feature maps from the encoder path. As shown in <xref ref-type="fig" rid="F3">Figure 3</xref>, two additional convolutional layers with dimensions of 8 &#xd7; 8 &#xd7; 8 are applied. This process is repeated for the subsequent transposed layers. To mitigate overfitting during training, an initial learning rate of 0.001 is used, with exponential decay applied every 2000 steps. Additionally, batch normalization is implemented after each convolutional layer and before the ReLU activation, except for the output layer, where it is deemed unnecessary for regression operations. Moreover, all convolutional layers utilize a 3 &#xd7; 3 kernel size.</p>
<p>To quantitatively assess the discrepancy between the outcomes predicted by the DL and CFD simulations, we referenced previous studies (<xref ref-type="bibr" rid="B25">Li et al. (2021a)</xref>, <xref ref-type="bibr" rid="B26">Li et al. (2021b)</xref>, <xref ref-type="bibr" rid="B47">Wang et al. (2023a)</xref>) and employed the mean radial error (MRE) and normalized mean absolute error (NAME). These metrics were used to evaluate the error magnitude at individual mesh points (<xref ref-type="bibr" rid="B25">Li et al., 2021a</xref>; <xref ref-type="bibr" rid="B48">Wang S. et al., 2023</xref>). MRE quantifies the difference between the predicted DL values and the corresponding actual values across all points within the model. In contrast, NAME measures the deviation of the DL-derived results from the actual values across the entire flow field represented by CFD results. The precise formulations of MRE and NAME are provided in <xref ref-type="disp-formula" rid="e5">Equations 5</xref>, <xref ref-type="disp-formula" rid="e6">6</xref>.<disp-formula id="e5">
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<mml:mn>100</mml:mn>
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<label>(6)</label>
</disp-formula>where <inline-formula id="inf24">
<mml:math id="m30">
<mml:mrow>
<mml:msub>
<mml:mi>y</mml:mi>
<mml:mi>i</mml:mi>
</mml:msub>
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</inline-formula> and <inline-formula id="inf25">
<mml:math id="m31">
<mml:mrow>
<mml:msub>
<mml:mover accent="true">
<mml:mi>y</mml:mi>
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</mml:mover>
<mml:mi>i</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> denote the <italic>i</italic>th values of TAWSS obtained by DL-predicted and CFD-simulated results, respectively. <inline-formula id="inf26">
<mml:math id="m32">
<mml:mrow>
<mml:mi>i</mml:mi>
</mml:mrow>
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<mml:math id="m33">
<mml:mrow>
<mml:mi>N</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is the total number of nodes, &#x7c;&#x7c; denotes the absolute value. NAME measures the absolute error for each individual data point after normalizing it by the peak value, and then calculates the average. It is essential to emphasize that max{y} represents the highest value obtained from these 1800 models.</p>
<p>To optimize the DL model, an additional study of the network layers is provided in the <xref ref-type="sec" rid="s13">Supplementary Material</xref>. <xref ref-type="sec" rid="s13">Supplementary Table S5</xref> investigates the effect of encoding/decoding sessions, revealing that increasing the number of sessions enhances prediction performance. <xref ref-type="sec" rid="s13">Supplementary Table S6</xref> demonstrates that utilizing four convolutional layers in the final encoding section yields the best prediction accuracy. Additionally, <xref ref-type="sec" rid="s13">Supplementary Table S7</xref> highlights the significant impact of skip connections, showing that they can reduce the MRE by half, further improving prediction performance.</p>
<p>This investigation is carried out on a Windows 10 workstation featuring a 3.4&#xa0;GHz CPU and 128&#xa0;GB of RAM. CFD simulations are performed using ANSYS-CFX 20.1 (ANSYS Inc., PA, USA). The computational time varies, usually below the 50&#xa0;minutes for most cases, with an average duration of approximately 45&#xa0;min. We implement the DL models using TensorFlow 2.0 and expedited the training process with a 12G TITAN Xp GPU. The training phase for the proposed model, with 27,339 parameters, lasted approximately 2&#xa0;hours. The dataset preparation, which involves simulating 1800 idealized models, required about 1350&#xa0;h. Nevertheless, all neural networks demonstrated the ability to generate a TAWSS map in less than 1&#xa0;s during testing.</p>
</sec>
</sec>
</sec>
<sec sec-type="results" id="s3">
<title>3 Results</title>
<p>Ordering point clouds is crucial, particularly in CNN architectures, as it helps extract local features. Principal Component Analysis (PCA) ordering is used which is one of the simplest methods for imposing order. This approach aligns the point cloud with its principal axes by computing eigenvectors of the covariance matrix. The points are then sorted based on their projections along the principal eigenvector, which corresponds to the direction of maximum variance. To assess its functionality, this ordering technique is compared with x, y, and z ordering points. As it is concluded from the <xref ref-type="table" rid="T5">Table 5</xref>, the MRE and NAME for ordering in canonical order is much better, 11.3 and 2.5, respectively.</p>
<table-wrap id="T5" position="float">
<label>TABLE 5</label>
<caption>
<p>Result of training the proposed U-net with ordering points in x, y, z-directions, and PCA ordering.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Order</th>
<th align="center">MRE</th>
<th align="center">NAME</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">x-ordering</td>
<td align="center">34 &#xb1; 8.3</td>
<td align="center">3 &#xb1; 1.2</td>
</tr>
<tr>
<td align="center">y-ordering</td>
<td align="center">29.1 &#xb1; 7.5</td>
<td align="center">3.6 &#xb1; 1.1</td>
</tr>
<tr>
<td align="center">z-ordering</td>
<td align="center">27.6 &#xb1; 3</td>
<td align="center">3.7 &#xb1; 1.8</td>
</tr>
<tr>
<td align="center">Principle axes ordering</td>
<td align="center">11.3 &#xb1; 5.5</td>
<td align="center">2.5 &#xb1; 0.6</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>As shown in <xref ref-type="fig" rid="F3">Figure 3</xref>, one of the steps in the process involves reshaping 4,096 points into a 64 &#xd7; 64 format. Specifically, the points are grouped into 64 clusters, each containing 64 points. After applying ordering to the point clouds, the grouping is schematically illustrated in <xref ref-type="sec" rid="s13">Supplementary Figure S3</xref>.</p>
<p>In this study, our primary focus is on examining the hemodynamic parameter known as TAWSS, a metric previously investigated in studies related to coronary arteries (<xref ref-type="bibr" rid="B13">Eshtehardi et al., 2012</xref>; <xref ref-type="bibr" rid="B43">Su et al., 2020</xref>). <xref ref-type="fig" rid="F4">Figure 4</xref> compares the TAWSS values obtained from the CFD and DL models across two perspectives. Due to the curved geometry of the LAD and LCx in the idealized model, the TAWSS distribution is asymmetrical between the front and back views. Notably, the TAWSS values in the front view, as shown in <xref ref-type="fig" rid="F4">Figures 4A, C</xref>, are almost 25% higher than those in the back views depicted in <xref ref-type="fig" rid="F4">Figures 4B, D</xref>. In <xref ref-type="fig" rid="F4">Figure 4A</xref>, left and right branches correspond to the LAD and LCx arteries, respectively. Although the values demonstrate good predictive capabilities in the LM and LAD vessels, the exact TAWSS values distribution from the CFD simulation (<xref ref-type="fig" rid="F4">Figures 4A, B</xref>) has higher values in the bifurcation and LCx artery in this case.</p>
<fig id="F4" position="float">
<label>FIGURE 4</label>
<caption>
<p>TAWSS distribution. Comparison between CFD results <bold>(A, B)</bold> and proposed DL model results <bold>(C, D)</bold> in one case in two different views, <bold>(A, C)</bold> TAWSS contours in front view, <bold>(B, D)</bold> TAWSS contours in back view.</p>
</caption>
<graphic xlink:href="fphys-16-1518732-g004.tif"/>
</fig>
<p>
<xref ref-type="fig" rid="F5">Figure 5</xref> depicts the comparison of TAWSS distribution between CFD and DL models along three lines on the wall within a bifurcation, representing specific paths of interest on the walls of LM, LAD, and LCx arteries. Each line consists of ten points, evenly spaced in the same direction as indicated by the arrow, to report the TAWSS value. This analysis evaluates the DL model&#x2019;s ability to approximate the TAWSS distribution compared to the CFD approach from simulation. Generally, trends agree quite well in the models, however, in some points the absolute error is higher compared to other regions. For instance, in <xref ref-type="fig" rid="F5">Figure 5C</xref>, it can be observed that in TAWSS graph along the LAD, in one point the difference reaches 20%.</p>
<fig id="F5" position="float">
<label>FIGURE 5</label>
<caption>
<p>TAWSS distribution comparison between CFD and proposed DL models along three paths in a bifurcation, <bold>(A)</bold> schematic of selected paths along the vessels in the bifurcation geometry, <bold>(B&#x2013;D)</bold> comparison between TAWSS values in DL and CFD results along the selected paths.</p>
</caption>
<graphic xlink:href="fphys-16-1518732-g005.tif"/>
</fig>
<p>Notably, the TAWSS value line graph for the LM artery in <xref ref-type="fig" rid="F5">Figure 5B</xref> reduces from more than 15 [Pa] to 5 [Pa] at the outlet, with the DL model accurately predicting this trend. Moreover, TAWSS values along the LAD artery in <xref ref-type="fig" rid="F5">Figure 5C</xref> remain relatively constant, fluctuating between 10 [Pa] and less than 12 [Pa] from the CFD and DL models, respectively. Additionally, there was a slight increase in TAWSS values along the line on the wall of LCx artery in the CFD model shown in <xref ref-type="fig" rid="F5">Figure 5D</xref>, from 8 to 10 [Pa], with a less than 0.5 [Pa] difference in the DL model.</p>
<p>
<xref ref-type="fig" rid="F6">Figure 6</xref> presents the results of TAWSS distribution obtained from CFD simulations (depicted in <xref ref-type="fig" rid="F6">Figures 6A&#x2013;C</xref> and the DL predictions (illustrated in <xref ref-type="fig" rid="F6">Figures 6D&#x2013;F</xref>, showing three different models with varying morphological parameters and associated errors. In all models, the left and right branches correspond to the LCx and LAD arteries, respectively. In branch region, the DL model tends to underestimate TAWSS values in LCx in <xref ref-type="fig" rid="F6">Figure 6F</xref>). Nevertheless, it is evident that it is capable of capturing the overall pattern and values of TAWSS distribution.</p>
<fig id="F6" position="float">
<label>FIGURE 6</label>
<caption>
<p>TAWSS distribution. Comparison between TAWSS values from CFD results <bold>(A&#x2013;C)</bold> and proposed DL model results <bold>(D&#x2013;F)</bold> in three cases with varying morphological parameters.</p>
</caption>
<graphic xlink:href="fphys-16-1518732-g006.tif"/>
</fig>
<p>
<xref ref-type="fig" rid="F7">Figure 7</xref> presents a line graph comparing the TAWSS distribution in a region of interest on the LCx for varying &#x3b1; angles in two models. The TAWSS values are averaged across the region&#x2019;s points, and the comparison is made between CFD and DL model outputs. The results show that the DL model accurately captures the overall increasing trend of TAWSS as the angle widens. Beyond 110&#xb0;, TAWSS values plateau, although the DL model introduces minor variations. At smaller angles (below 70&#xb0;), the differences between the models are minimal, remaining under 1.6&#xa0;Pa, with the DL model closely matching the rising trend. However, at 75 and 105&#xb0;, the model shows larger deviations, with discrepancies of 1.5&#xa0;Pa and 1.1&#xa0;Pa, respectively. While the DL model generally performs well in predicting TAWSS, fluctuating patterns in DL model suggest that further refinement is needed to improve its accuracy.</p>
<fig id="F7" position="float">
<label>FIGURE 7</label>
<caption>
<p>TAWSS prediction in the region of interest varying in the <inline-formula id="inf28">
<mml:math id="m34">
<mml:mrow>
<mml:mi>&#x3b1;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> angle between LCx and LAD arteries.</p>
</caption>
<graphic xlink:href="fphys-16-1518732-g007.tif"/>
</fig>
</sec>
<sec sec-type="discussion" id="s4">
<title>4 Discussion</title>
<p>
<xref ref-type="bibr" rid="B43">Su et al. (2020)</xref> achieved real-time 2D WSS prediction by creating numerous idealized blood vessel models derived from a limited clinical dataset and utilizing a CNN. It is shown in this study that CNN works better than MLP and MLR. However, their study does not include more complex geometries like bifurcations. Moreover, in their input they utilized 2D information of geometry which is much more straightforward than using a point cloud as an input. The Point Net structure, on the other hand, provides a significant advantage for geometries before and after treatment. <xref ref-type="bibr" rid="B25">Li et al. (2021a)</xref> and <xref ref-type="bibr" rid="B48">Wang et al. (2023b)</xref> applied the same structure for idealized geometry with cerebral aneurysm and patient-specific carotid artery geometries with stenosis, respectively. Despite its benefit that is robust to the number of input models, Point Net faces a prominent challenge in terms of variation in geometry features. As in the previous investigation, the Point Net model was trained separately for carotid arteries with and without stenosis (<xref ref-type="bibr" rid="B48">Wang S. et al., 2023</xref>).</p>
<p>However, in the proposed model not only the model is trained to predict data varying in the most crucial parameters like diameters and angels of bifurcation, but also it utilizes a point cloud as the input. The error function results for TAWSS at each mesh point, evaluated across the testing set models using the MRE <xref ref-type="disp-formula" rid="e5">Equation 5</xref> and NAME <xref ref-type="disp-formula" rid="e6">Equation 6</xref>, were 11.39 &#xb1; 5.5 and 2.5 &#xb1; 0.56, respectively. It is important to note that the model was not previously trained on the testing set, which comprised 360 bifurcation models.</p>
<p>Due to the high dimensions of input data, CNN is a great tool for encoding the point cloud since it reduces trainable parameters rather than using MLP. In CNNs, each neuron in a layer is linked to a small region of the previous layer, known as the receptive field. This sparse connectivity minimizes redundancy, allowing the network to focus on local patterns. In the case study of Gharleghi et al. (<xref ref-type="bibr" rid="B40">Samarasinghe, 2020</xref>), they used CNN structure to predict the TAWSS in bifurcations, however, they used unfolding techniques to make 3D point clouds to 2D data. In case of bifurcation there is a complex relation between points in the center of geometry. Unfolding point clouds leads not to consider the relation between points where CNNs solely rely on local data. As a result, this structure cannot predict wide ranges of characteristics.</p>
<p>The proposed DL model for predicting TAWSS in coronary artery bifurcations offers substantial advantages for medical applications, particularly in real-time diagnostics and treatment planning. Traditional CFD simulations, though accurate, are computationally intensive and impractical for fast-response scenarios in clinical settings. Our DL-based approach, which predicts TAWSS with a normalized mean absolute error of 2.53% in under one second, overcomes this challenge by drastically enhancing computational efficiency without compromising accuracy. This advancement facilitates rapid, patient-specific assessments of hemodynamic factors linked to atherosclerosis and stenosis, enabling timely decision-making for both surgical and non-invasive interventions. Additionally, the model&#x2019;s versatility across various coronary geometries further increases its clinical applicability, presenting a promising tool for personalized cardiovascular care.</p>
</sec>
<sec id="s5">
<title>5 Limitations and future remarks</title>
<p>A limitation we faced was the lack of patient-specific bifurcation models. To address this, we generated artificial bifurcation datasets for DL model, incorporating morphological parameters as substitutes for real-world data. Consequently, the optimal network parameters derived from the training samples deviated from actual clinical scenarios. Furthermore, during the CFD simulation process, we applied generic boundary conditions instead of tailored, patient-specific ones. Nevertheless, this approach is consistent with previous simulation studies (<xref ref-type="bibr" rid="B9">Davies et al., 2006</xref>; <xref ref-type="bibr" rid="B23">Jahromi et al., 2019</xref>). Another limitation was the use of a fixed number of point cloud as a input of the model, which could vary depending on the complexity of DL networks. Additionally, since our DL model&#x2019;s input consisted of a uniform and fixed number of point cloud points across the geometries, some transitions in TAWSS values may have been overlooked in certain regions. Despite these constraints, we present a DL method that takes into account various restrictions, including dynamic flow boundary conditions. The DL model achieved an MRE value of 11.39 on the test dataset, successfully capturing the overall trend. However, a point-by-point analysis along the three vessels in <xref ref-type="fig" rid="F5">Figure 5</xref> reveals that the absolute relative error at one point reaches 20%. This result shows a limitation of the DL model, which could be addressed in future studies. Other parameters, such as velocity and pressure, are vector quantities, requiring predictions in three directions at each point. Additionally, velocity and pressure are defined for the fluid domain, making their complexity different from TAWSS, which is only defined on the wall. These aspects can be explored in future studies.</p>
<p>As a proof of concept, this study demonstrates the feasibility of using a DL-based approach for fast and accurate TAWSS prediction. The model achieved a NAME of only 2.5% and generate predictions in less than one second, underscoring its potential for rapid clinical applications. The efficiency gains, along with the strong correlation to CFD results, represent valuable contributions to the field.</p>
</sec>
<sec sec-type="conclusion" id="s6">
<title>6 Conclusion</title>
<p>In this study, we introduced a simulation-based framework for the first time to achieve Unet-based prediction of TAWSS in coronary arteries bifurcation with varied diameters and angels. Through the generation of high-quality point cloud datasets and the utilization of U-net, we demonstrated that the DL-based approach yields highly accurate predictions closely aligning with CFD simulations. Importantly, this achievement is accompanied by a notable reduction in computational costs. This emphasizes the potential and viability of the DL-based strategy for rapid and precise forecasting of TAWSS in coronary arteries bifurcation.</p>
</sec>
</body>
<back>
<sec sec-type="data-availability" id="s7">
<title>Data availability statement</title>
<p>The original contributions presented in the study are included in the article/<xref ref-type="sec" rid="s13">Supplementary Material</xref>, further inquiries can be directed to the corresponding author.</p>
</sec>
<sec sec-type="author-contributions" id="s8">
<title>Author contributions</title>
<p>MoS: Writing&#x2013;original draft. HE: Writing&#x2013;original draft. MR: Funding acquisition, Writing&#x2013;review and editing. MaS: Writing&#x2013;review and editing.</p>
</sec>
<sec sec-type="funding-information" id="s9">
<title>Funding</title>
<p>The author(s) declare that no financial support was received for the research, authorship, and/or publication of this article.</p>
</sec>
<sec sec-type="COI-statement" id="s10">
<title>Conflict of interest</title>
<p>The authors declare that the research was conducted in the absence of any commercial or financial relationships that could be construed as a potential conflict of interest.</p>
</sec>
<sec sec-type="ai-statement" id="s11">
<title>Generative AI statement</title>
<p>The author(s) declare that no Generative AI was used in the creation of this manuscript.</p>
</sec>
<sec sec-type="disclaimer" id="s12">
<title>Publisher&#x2019;s note</title>
<p>All claims expressed in this article are solely those of the authors and do not necessarily represent those of their affiliated organizations, or those of the publisher, the editors and the reviewers. Any product that may be evaluated in this article, or claim that may be made by its manufacturer, is not guaranteed or endorsed by the publisher.</p>
</sec>
<sec id="s13">
<title>Supplementary material</title>
<p>The Supplementary Material for this article can be found online at: <ext-link ext-link-type="uri" xlink:href="https://www.frontiersin.org/articles/10.3389/fphys.2025.1518732/full#supplementary-material">https://www.frontiersin.org/articles/10.3389/fphys.2025.1518732/full&#x23;supplementary-material</ext-link>
</p>
<supplementary-material xlink:href="Table1.docx" id="SM1" mimetype="application/docx" xmlns:xlink="http://www.w3.org/1999/xlink"/>
</sec>
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