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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">1595588</article-id>
<article-id pub-id-type="doi">10.3389/fphys.2025.1595588</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>Optimization of secondary flow path clearance in centrifugal blood pump: a combined numerical and experimental study</article-title>
<alt-title alt-title-type="left-running-head">Zhu 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.2025.1595588">10.3389/fphys.2025.1595588</ext-link>
</alt-title>
</title-group>
<contrib-group>
<contrib contrib-type="author">
<name>
<surname>Zhu</surname>
<given-names>Chenying</given-names>
</name>
<uri xlink:href="https://loop.frontiersin.org/people/2999720/overview"/>
<role content-type="https://credit.niso.org/contributor-roles/conceptualization/"/>
<role content-type="https://credit.niso.org/contributor-roles/formal-analysis/"/>
<role content-type="https://credit.niso.org/contributor-roles/methodology/"/>
<role content-type="https://credit.niso.org/contributor-roles/software/"/>
<role content-type="https://credit.niso.org/contributor-roles/validation/"/>
<role content-type="https://credit.niso.org/contributor-roles/writing-original-draft/"/>
<role content-type="https://credit.niso.org/contributor-roles/Writing - review &#x26; editing/"/>
</contrib>
<contrib contrib-type="author" corresp="yes">
<name>
<surname>Ye</surname>
<given-names>Ping</given-names>
</name>
<xref ref-type="corresp" rid="c001">&#x2a;</xref>
<uri xlink:href="https://loop.frontiersin.org/people/937382/overview"/>
<role content-type="https://credit.niso.org/contributor-roles/supervision/"/>
<role content-type="https://credit.niso.org/contributor-roles/Writing - review &#x26; editing/"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Chang</surname>
<given-names>Zhaohua</given-names>
</name>
<uri xlink:href="https://loop.frontiersin.org/people/1734023/overview"/>
<role content-type="https://credit.niso.org/contributor-roles/project-administration/"/>
<role content-type="https://credit.niso.org/contributor-roles/resources/"/>
<role content-type="https://credit.niso.org/contributor-roles/supervision/"/>
<role content-type="https://credit.niso.org/contributor-roles/Writing - review &#x26; editing/"/>
</contrib>
</contrib-group>
<aff>
<institution>School of Health Science and Engineering</institution>, <institution>University of Shanghai for Science and Technology</institution>, <addr-line>Shanghai</addr-line>, <country>China</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/848762/overview">Zengsheng Chen</ext-link>, Beihang 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/1448201/overview">Aniruddha Pandit</ext-link>, Institute of Chemical Technology, India</p>
<p>
<ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/1693892/overview">Peng Fang</ext-link>, Inner Mongolia University of Technology, China</p>
</fn>
<corresp id="c001">&#x2a;Correspondence: Ping Ye, <email>221300171@st.usst.edu.cn</email>
</corresp>
</author-notes>
<pub-date pub-type="epub">
<day>27</day>
<month>06</month>
<year>2025</year>
</pub-date>
<pub-date pub-type="collection">
<year>2025</year>
</pub-date>
<volume>16</volume>
<elocation-id>1595588</elocation-id>
<history>
<date date-type="received">
<day>18</day>
<month>03</month>
<year>2025</year>
</date>
<date date-type="accepted">
<day>16</day>
<month>06</month>
<year>2025</year>
</date>
</history>
<permissions>
<copyright-statement>Copyright &#xa9; 2025 Zhu, Ye and Chang.</copyright-statement>
<copyright-year>2025</copyright-year>
<copyright-holder>Zhu, Ye and Chang</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>Blood pumps as mechanical circulatory support (MCS) devices are widely used for patients with ventricular heart failure, and improving blood compatibility remains a key focus for researchers.</p>
</sec>
<sec>
<title>Methods</title>
<p>The effects of secondary flow path clearance on the performance and hemocompatibility of a centrifugal blood pump are investigated in this study. A blood pump of the specific design was developed for modeling and computer simulation, and 25 models were generated by varying its internal and outer clearance between 600 and 1,000 &#x3bc;m. This study systematically investigates the hydrodynamic and hemodynamic performance of designed blood pumps through integrated computational fluid dynamics simulations and <italic>in vitro</italic> hydraulic experiments.</p>
</sec>
<sec>
<title>Results</title>
<p>Key findings reveal a strong agreement between numerical predictions and experimental data, showing a maximum pressure deviation of 9% for the baseline pump configuration. Furthermore, the effect of the change in clearance on the head and efficiency is less than &#xb1;3%. The change in the secondary flow path significantly impacts hemolysis performance.</p>
</sec>
<sec>
<title>Discussion</title>
<p>An optimal clearance combination exists in the designed model, and for a specific flow field structure, asymmetric clearance may be an effective means to balance leakage control and turbulence suppression. Although the findings are specific to the pumps examined in this study, they provide valuable insights into the optimal design of blood pumps.</p>
</sec>
</abstract>
<kwd-group>
<kwd>centrifugal blood pump</kwd>
<kwd>fluid dynamics</kwd>
<kwd>shear stress</kwd>
<kwd>hemolysis</kwd>
<kwd>secondary flow clearance</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>Heart failure (HF) is a significant public health concern, impacting approximately 64 million individuals globally and imposing a considerable strain on healthcare systems due to its elevated mortality and morbidity rates (<xref ref-type="bibr" rid="B24">Shahim et al., 2023</xref>). Mechanical circulatory support (MCS) is commonly employed in patients with advanced HF to prolong life expectancy and improve functional capacity, often serving as a pathway to transplantation. Ventricular assist devices (VADs) are mechanical pumps that sustain blood circulation in a failing ventricle for short-term and long-term applications (<xref ref-type="bibr" rid="B13">Khera et al., 2015</xref>; <xref ref-type="bibr" rid="B2">Cai et al., 2017</xref>). In recent years, centrifugal blood pumps have gained widespread clinical adoption, largely due to the implementation of non-contact magnetic bearings, which minimize mechanical wear and reduce shear-induced blood damage. However, the high-speed rotation of the impeller inherently generates non-physiological shear stress (NPSS), exposing blood to mechanical forces that can damage cells (<xref ref-type="bibr" rid="B25">Thamsen et al., 2015</xref>). Excessive shear stress can rupture red blood cells (RBCs) or create membrane perforations once critical stress thresholds are exceeded (<xref ref-type="bibr" rid="B30">Yausda et al., 2000</xref>; <xref ref-type="bibr" rid="B15">Li et al., 2013</xref>; <xref ref-type="bibr" rid="B23">Shah et al., 2017</xref>; <xref ref-type="bibr" rid="B6">Faghih and Sharp, 2019</xref>). Research has identified specific shear stress thresholds related to various blood dysfunctions: 9 Pa for the degradation of von Willebrand factor, 50 Pa for platelet activation, and 150 Pa for the destruction of red blood cells. High levels of NPSS (&#x3e;100 Pa) can cause platelet activation even within a very short exposure time (&#x3c;1 s) (<xref ref-type="bibr" rid="B3">Chen et al., 2016</xref>). Hemolysis is known to follow a power-law relationship with both shear stress magnitude and exposure time. Therefore, precise control of shear stress distribution and blood residence time (RT) is essential in pump design to ensure blood compatibility.</p>
<p>Previous studies primarily focused on the design of the blade and volute of the blood pump, including aspects such as the number of blades, blade angles, and blade thickness, et al. (<xref ref-type="bibr" rid="B14">Li H. et al., 2023</xref>; <xref ref-type="bibr" rid="B1">Abbasnezhad and Bakir, 2025</xref>; <xref ref-type="bibr" rid="B16">Li Y. et al., 2023</xref>; <xref ref-type="bibr" rid="B28">Wu et al., 2021</xref>). However, attention has increasingly shifted toward secondary flow path clearances, including axial and radial gaps, which play a critical role in suppressing recirculation, reducing stagnation zones, and improving blood compatibility, especially in magnetically levitated (maglev) pumps where mechanical bearings are absent (<xref ref-type="bibr" rid="B27">Wu et al., 2020</xref>). A range of findings have been reported regarding clearance effects. <xref ref-type="bibr" rid="B18">Liu et al. (2019)</xref> reported that increasing radial clearance in axial flow pumps led to reductions in head pressure, efficiency, and scalar shear stress (SSS). <xref ref-type="bibr" rid="B21">Puentener et al. (2020)</xref> found that a larger radial clearance could significantly improve blood compatibility. <xref ref-type="bibr" rid="B26">Wu et al. (2010)</xref> quantitatively calculated pediatric blood pumps, and the results showed that there was an optimal tip clearance, through which hydraulic efficiency could be maximized and hemolysis minimized. While <xref ref-type="bibr" rid="B11">Gil et al. (2022)</xref> found that smaller blade tip gaps reduced hydraulic efficiency but increased hemolysis. <xref ref-type="bibr" rid="B12">Goodin et al. (2022)</xref> found that reducing secondary clearance had minimal impact on pump head. <xref ref-type="bibr" rid="B22">Rezaienia et al. (2018)</xref> demonstrated a unimodal relationship between axial/radial clearances and hemolysis index (HI), highlighting the role of vortices in hemocompatibility. <xref ref-type="bibr" rid="B19">Lv et al. (2024)</xref>; <xref ref-type="bibr" rid="B20">Lv et al. (2025)</xref> conducted numerical simulations to assess the effects of axial blade positions and radial clearance on pump performance and hemolysis. They found that shifting the axial position from the baseline (H &#x3d; 3.25 mm) to 2.5 and 4.0 mm increased the HI by 12.3% and 24.3%, respectively. Further analysis showed that increasing radial clearance reduced SSS but increased RT, particularly in the bottom clearance. At low flow rates, radial clearance had a greater impact on hemolysis than on thrombosis risk.</p>
<p>A comparative study of CH-VAD and HeartMate III (<xref ref-type="bibr" rid="B29">Wu et al., 2024</xref>) showed that while narrow clearances reduce flow disturbances, they can concentrate blood damage near the blades; in contrast, wider clearances enhance secondary flows, increasing flow separation and efficiency loss. <xref ref-type="bibr" rid="B8">Fischer et al. (2025)</xref> evaluated 36 clearance configurations and found that even &#xb1;10% variations significantly influenced hemocompatibility, concluding that larger, more uniform clearances generally offer better blood compatibility. Despite these advances, existing studies often focus on axial or tip clearances, or only vary one radial clearance parameter at a time. The comprehensive influence of the internal and external radial clearances in the secondary flow path, especially their roles in balancing shear damage and RT, still requires further research.</p>
<p>This study evaluated the design of a centrifugal pump by investigating various parameters, including head, shear stress distribution, and HI. The hydraulic performance was validated through CFD simulations and hydraulic testing. The optimization of the blood pump&#x2019;s configuration aimed to reduce shear stress and RT, thereby significantly decreasing the incidence of hemolysis. This optimization specifically targeted the radial clearance size of the secondary flow path. The study employed Lagrangian particle tracking to evaluate various parameter models, enabling a comparison of RT and shear stress within the blood pump to predict hemolysis outcomes.</p>
</sec>
<sec sec-type="materials|methods" id="s2">
<title>2 Materials and methods</title>
<sec id="s2-1">
<title>2.1 Baseline blood pump model</title>
<p>
<xref ref-type="fig" rid="F1">Figure 1</xref> illustrates a three-dimensional representation of the centrifugal blood pump and its essential structural elements: the inlet, outlet, impeller, and volute. The baseline model was inspired by the general design characteristics of clinically approved centrifugal blood pumps, which are used for short- to medium-term mechanical circulatory support in patients with advanced HF. The inlet and outlet are oriented orthogonally at a 90&#xb0; angle. The impeller is characterized by a radial, open configuration comprising eight blades, of which four are classified as splitter blades. Prior studies have shown that the incorporation of splitter blades can help regulate the flow field and improve blood compatibility by mitigating flow-induced shear stress and pressure gradients (<xref ref-type="bibr" rid="B28">Wu et al., 2021</xref>; <xref ref-type="bibr" rid="B17">Li et al., 2022</xref>). A central column within the impeller enhances structural integrity and promotes uniform flow distribution. The impeller is completely supported by an advanced magnetic suspension system, eliminating mechanical contact and reducing wear. This system ensures axial stabilization of the rotor through passive suspension, while radial stability is maintained via a biased magnetic field, facilitating precise control over rotor dynamics. The main design parameters of the blood pump are shown in <xref ref-type="table" rid="T1">Table 1</xref>.</p>
<fig id="F1" position="float">
<label>FIGURE 1</label>
<caption>
<p>
<bold>(A)</bold> Schematic diagram of the centrifugal blood pump structure; <bold>(B)</bold> The axial section and radial section of 3D geometries of the maglev blood pump model.</p>
</caption>
<graphic xlink:href="fphys-16-1595588-g001.tif">
<alt-text content-type="machine-generated">Diagram showing a centrifugal pump. Part A illustrates the components, including the inlet, outlet, impeller, and volute. Part B shows cross-sectional views with dimensions labeled: D1, HT, HB, L1, L2, HV, D2, &#x3B2;1, &#x3B2;2, &#x3C6;, T, DB, and DV.</alt-text>
</graphic>
</fig>
<table-wrap id="T1" position="float">
<label>TABLE 1</label>
<caption>
<p>Main parameters of the blood pump.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Parameter</th>
<th align="center">Parameter description</th>
<th align="center">Value</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">n</td>
<td align="center">Rotational speed (rpm)</td>
<td align="center">3,000</td>
</tr>
<tr>
<td align="center">Q</td>
<td align="center">Flow rate (L/min)</td>
<td align="center">5</td>
</tr>
<tr>
<td align="center">H</td>
<td align="center">Design pressure head (mmHg)</td>
<td align="center">300</td>
</tr>
<tr>
<td align="center">D<sub>1</sub>
</td>
<td align="center">Inlet diameter (mm)</td>
<td align="center">9.5</td>
</tr>
<tr>
<td align="center">D<sub>2</sub>
</td>
<td align="center">Outlet diameter (mm)</td>
<td align="center">9.2</td>
</tr>
<tr>
<td align="center">D<sub>V</sub>
</td>
<td align="center">Volute diameter (mm)</td>
<td align="center">64</td>
</tr>
<tr>
<td align="center">H<sub>V</sub>
</td>
<td align="center">Volute height (mm)</td>
<td align="center">57.5</td>
</tr>
<tr>
<td align="center">D<sub>B</sub>
</td>
<td align="center">Blade diameter (mm)</td>
<td align="center">49</td>
</tr>
<tr>
<td align="center">&#x3c6;</td>
<td align="center">Volute tongue angle (&#xb0;)</td>
<td align="center">47.4</td>
</tr>
<tr>
<td align="center">N</td>
<td align="center">Number of blades (/)</td>
<td align="center">8</td>
</tr>
<tr>
<td align="center">T</td>
<td align="center">Blade thickness (mm)</td>
<td align="center">1.7</td>
</tr>
<tr>
<td align="center">&#x3b2;<sub>2</sub>
</td>
<td align="center">Blade outlet angle (&#xb0;)</td>
<td align="center">64</td>
</tr>
<tr>
<td align="center">&#x3b2;<sub>1</sub>
</td>
<td align="center">Blade inlet angle (&#xb0;)</td>
<td align="center">56.7</td>
</tr>
<tr>
<td align="center">&#x3b2;</td>
<td align="center">Wrap angle (&#xb0;)</td>
<td align="center">24.5</td>
</tr>
<tr>
<td align="center">H<sub>T</sub>
</td>
<td align="center">Top clearance (mm)</td>
<td align="center">2</td>
</tr>
<tr>
<td align="center">L<sub>1</sub>
</td>
<td align="center">Inner clearance (&#x3bc;m)</td>
<td align="center">700</td>
</tr>
<tr>
<td align="center">L<sub>2</sub>
</td>
<td align="center">Outer clearance (&#x3bc;m)</td>
<td align="center">600</td>
</tr>
<tr>
<td align="center">H<sub>B</sub>
</td>
<td align="center">Bottom clearance (mm)</td>
<td align="center">1</td>
</tr>
</tbody>
</table>
</table-wrap>
</sec>
<sec id="s2-2">
<title>2.2 Optimal experimental design</title>
<p>The selection of the secondary flow path clearance range (600&#x2013;1,000 &#x3bc;m) was based on two primary considerations. First, geometric constraints inherent to the overall pump head design necessitate compatibility with the magnetic levitation system. In fully maglev pumps, the impeller, housing, and magnetic suspension components must be tightly integrated, which places specific limits on feasible clearance dimensions. Second, the clearance range must support adequate hydraulic performance, including pressure head, efficiency, and flow stability. To identify an optimal configuration with favorable hydraulic and hemolytic performance, an orthogonal experimental design was employed to optimize geometric parameters. Two factors were selected for the secondary clearance design: the inner clearance (L<sub>1</sub>) and the outer clearance (L<sub>2</sub>), each defined at five levels. Using the orthogonal design principle, a total of 25 test combinations were generated, as summarized in <xref ref-type="table" rid="T2">Table 2</xref>.</p>
<table-wrap id="T2" position="float">
<label>TABLE 2</label>
<caption>
<p>Design parameters of clearance size.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th rowspan="2" align="center">Model</th>
<th colspan="2" align="center">Factor</th>
</tr>
<tr>
<th align="center">L<sub>1</sub> (&#x3bc;m)</th>
<th align="center">L<sub>2</sub> (&#x3bc;m)</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">1</td>
<td align="center">600</td>
<td align="center">600</td>
</tr>
<tr>
<td align="center">2</td>
<td align="center">600</td>
<td align="center">700</td>
</tr>
<tr>
<td align="center">3</td>
<td align="center">600</td>
<td align="center">800</td>
</tr>
<tr>
<td align="center">4</td>
<td align="center">600</td>
<td align="center">900</td>
</tr>
<tr>
<td align="center">5</td>
<td align="center">600</td>
<td align="center">1,000</td>
</tr>
<tr>
<td align="center">6 (baseline pump)</td>
<td align="center">700</td>
<td align="center">600</td>
</tr>
<tr>
<td align="center">7</td>
<td align="center">700</td>
<td align="center">700</td>
</tr>
<tr>
<td align="center">8</td>
<td align="center">700</td>
<td align="center">800</td>
</tr>
<tr>
<td align="center">9</td>
<td align="center">700</td>
<td align="center">900</td>
</tr>
<tr>
<td align="center">10</td>
<td align="center">700</td>
<td align="center">1,000</td>
</tr>
<tr>
<td align="center">11</td>
<td align="center">800</td>
<td align="center">600</td>
</tr>
<tr>
<td align="center">12</td>
<td align="center">800</td>
<td align="center">700</td>
</tr>
<tr>
<td align="center">13</td>
<td align="center">800</td>
<td align="center">800</td>
</tr>
<tr>
<td align="center">14</td>
<td align="center">800</td>
<td align="center">900</td>
</tr>
<tr>
<td align="center">15</td>
<td align="center">800</td>
<td align="center">1,000</td>
</tr>
<tr>
<td align="center">16</td>
<td align="center">900</td>
<td align="center">600</td>
</tr>
<tr>
<td align="center">17</td>
<td align="center">900</td>
<td align="center">700</td>
</tr>
<tr>
<td align="center">18</td>
<td align="center">900</td>
<td align="center">800</td>
</tr>
<tr>
<td align="center">19</td>
<td align="center">900</td>
<td align="center">900</td>
</tr>
<tr>
<td align="center">20</td>
<td align="center">900</td>
<td align="center">1,000</td>
</tr>
<tr>
<td align="center">21</td>
<td align="center">1,000</td>
<td align="center">600</td>
</tr>
<tr>
<td align="center">22</td>
<td align="center">1,000</td>
<td align="center">700</td>
</tr>
<tr>
<td align="center">23</td>
<td align="center">1,000</td>
<td align="center">800</td>
</tr>
<tr>
<td align="center">24</td>
<td align="center">1,000</td>
<td align="center">900</td>
</tr>
<tr>
<td align="center">25</td>
<td align="center">1,000</td>
<td align="center">1,000</td>
</tr>
</tbody>
</table>
</table-wrap>
</sec>
<sec id="s2-3">
<title>2.3 CFD analysis</title>
<sec id="s2-3-1">
<title>2.3.1 Mesh details and independence analysis</title>
<p>Geometry was initially developed in Solidworks 2023 (Solidworks v2023, Waltham, MA, United States), and imported into Design Modeler (ANSYS, Inc., Canonsburg, PA, United States) for fluid domain extraction. The fluid domain was segmented into three parts: the inlet, the impeller rotation region, and the volute (outlet). Interfaces were created between these sections to ensure seamless data transfer. To enhance the reliability of the simulation, the blood pump&#x2019;s inlet and outlet were extended. This strategy was employed to minimize the influence of boundary conditions on the simulation results, thereby ensuring that the flow entering the computational domain was fully developed. Unstructured tetrahedral meshes were used for all fluid domains. A more refined meshing strategy was implemented in regions prone to complex flow dynamics or high shear stress, such as near the impeller blades, secondary flow paths, and the volute casing. Specifically, five-layer elements were applied along the walls in these critical areas, enhancing the mesh&#x2019;s ability to capture boundary layer effects and providing greater accuracy in predicting shear stress distributions. A mesh sensitivity analysis was conducted for the baseline pump, utilizing four grids with sizes of 1.45 million, 2.48 million, 3.95 million, and 5.16 million, respectively.</p>
</sec>
<sec id="s2-3-2">
<title>2.3.2 CFD methods</title>
<p>The software FLUENT 2023R2 (ANSYS, Inc., Canonsburg, PA, United States), was used for numerical simulations. In this model, considering the relatively high shear rates (&#x3e;100 s<sup>&#x2212;1</sup>) typically present in rotary blood pumps, the non-Newtonian properties of blood (such as shear thinning behavior, etc.) can be reasonably neglected. Therefore, modeling blood as an incompressible Newtonian fluid is an appropriate simplification, as supported by previous experimental studies (<xref ref-type="bibr" rid="B17">Li et al., 2022</xref>; <xref ref-type="bibr" rid="B29">Wu et al., 2024</xref>). A constant viscosity of 0.0035 Pa&#xb7;s and a density of 1,050 kg/m<sup>3</sup> were adopted in the simulations (<xref ref-type="bibr" rid="B22">Rezaienia et al., 2018</xref>). The shear stress transport (SST) k-&#x3c9; turbulence model was chosen for its high accuracy and robustness in capturing near-wall effects. The impeller&#x2019;s rotational motion was modeled using the steady &#x201c;frame motion&#x201d; approach, and all walls were defined as no-slip boundaries. The semi-implicit pressure-linked equations (SIMPLE) method was utilized to solve the governing fluid equations. A mass flow inlet, corresponding to 0.0875 kg/s (equivalent to a flow rate of 5 L/min), was set for the inlet, while a zero-pressure condition was applied at the outlet. A parametric study was conducted using the workbench to evaluate the hydraulic performance of the centrifugal blood pump, and the inlet and outlet pressure drop and outlet flow were obtained by changing the input parameters (speed and flow). Convergence was deemed achieved when all residuals fell below 10<sup>&#x2013;3</sup> and both outlet pressure and flow rate reached a state of stabilization. The governing equations utilized in this analysis are the Navier-Stokes equations, as shown in <xref ref-type="disp-formula" rid="e1">Equation 1</xref>.<disp-formula id="e1">
<mml:math id="m1">
<mml:mrow>
<mml:mi mathvariant="bold-italic">&#x3c1;</mml:mi>
<mml:mrow>
<mml:mfenced open="[" close="]" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mi mathvariant="bold-italic">&#x2202;</mml:mi>
<mml:mi mathvariant="bold-italic">u</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi mathvariant="bold-italic">&#x2202;</mml:mi>
<mml:mi mathvariant="bold-italic">t</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mo>&#x2b;</mml:mo>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi mathvariant="bold-italic">u</mml:mi>
<mml:mo>&#xb7;</mml:mo>
<mml:mo>&#x2207;</mml:mo>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mi mathvariant="bold-italic">u</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mi mathvariant="bold-italic">&#x3bc;</mml:mi>
<mml:msup>
<mml:mo>&#x2207;</mml:mo>
<mml:mn mathvariant="bold">2</mml:mn>
</mml:msup>
<mml:mi mathvariant="bold-italic">u</mml:mi>
<mml:mo>&#x2212;</mml:mo>
<mml:mo>&#x2207;</mml:mo>
<mml:mi mathvariant="bold-italic">p</mml:mi>
<mml:mo>&#x2b;</mml:mo>
<mml:mi mathvariant="bold-italic">&#x3c1;</mml:mi>
<mml:mi mathvariant="bold-italic">g</mml:mi>
</mml:mrow>
</mml:math>
<label>(1)</label>
</disp-formula>where <inline-formula id="inf1">
<mml:math id="m2">
<mml:mrow>
<mml:mi>u</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is the velocity field of the fluid, t is the time, <inline-formula id="inf2">
<mml:math id="m3">
<mml:mrow>
<mml:mi>&#x3bc;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is the dynamic viscosity, <inline-formula id="inf3">
<mml:math id="m4">
<mml:mrow>
<mml:mi>&#x3c1;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is the density of the fluid, <inline-formula id="inf4">
<mml:math id="m5">
<mml:mrow>
<mml:mi>p</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is the pressure, and <inline-formula id="inf5">
<mml:math id="m6">
<mml:mrow>
<mml:mi>g</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is external body force.</p>
</sec>
<sec id="s2-3-3">
<title>2.3.3 Indicators</title>
<p>Hemolysis is primarily attributed to non-physiological shear stress and prolonged exposure. An increase in shear stress can result in damage to red blood cells. The shear stress tensor is calculated based on the velocity field obtained from a three-dimensional numerical simulation. <xref ref-type="disp-formula" rid="e2">Equations 2</xref>, <xref ref-type="disp-formula" rid="e3">3</xref> are the corrected formula for calculating the SSS (<xref ref-type="bibr" rid="B5">Faghih and Keith Sharp, 2016</xref>):<disp-formula id="e2">
<mml:math id="m7">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="bold-italic">&#x3c4;</mml:mi>
<mml:mrow>
<mml:mi mathvariant="bold-italic">s</mml:mi>
<mml:mi mathvariant="bold-italic">c</mml:mi>
<mml:mi mathvariant="bold-italic">a</mml:mi>
<mml:mi mathvariant="bold-italic">l</mml:mi>
<mml:mi mathvariant="bold-italic">a</mml:mi>
<mml:mi mathvariant="bold-italic">r</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mrow>
<mml:mfenced open="[" close="]" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mn mathvariant="bold">1</mml:mn>
</mml:mrow>
<mml:mrow>
<mml:mn mathvariant="bold">12</mml:mn>
</mml:mrow>
</mml:mfrac>
<mml:mo>&#x2211;</mml:mo>
<mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="bold-italic">&#x3c4;</mml:mi>
<mml:mrow>
<mml:mi mathvariant="bold-italic">i</mml:mi>
<mml:mi mathvariant="bold-italic">i</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x2212;</mml:mo>
<mml:msub>
<mml:mi mathvariant="bold-italic">&#x3c4;</mml:mi>
<mml:mrow>
<mml:mi mathvariant="bold-italic">j</mml:mi>
<mml:mi mathvariant="bold-italic">j</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mn mathvariant="bold">2</mml:mn>
</mml:msup>
<mml:mo>&#x2b;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mn mathvariant="bold">1</mml:mn>
</mml:mrow>
<mml:mrow>
<mml:mn mathvariant="bold">2</mml:mn>
</mml:mrow>
</mml:mfrac>
<mml:mo>&#x2211;</mml:mo>
<mml:msup>
<mml:msub>
<mml:mi mathvariant="bold-italic">&#x3c4;</mml:mi>
<mml:mrow>
<mml:mi mathvariant="bold-italic">i</mml:mi>
<mml:mi mathvariant="bold-italic">j</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mn mathvariant="bold">2</mml:mn>
</mml:msup>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mn mathvariant="bold">1</mml:mn>
</mml:mrow>
<mml:mrow>
<mml:mn mathvariant="bold">2</mml:mn>
</mml:mrow>
</mml:mfrac>
</mml:msup>
</mml:mrow>
</mml:math>
<label>(2)</label>
</disp-formula>
<disp-formula id="e3">
<mml:math id="m8">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="bold-italic">&#x3c4;</mml:mi>
<mml:mrow>
<mml:mi mathvariant="bold-italic">i</mml:mi>
<mml:mi mathvariant="bold-italic">j</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mi mathvariant="bold-italic">&#x3bc;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mi mathvariant="bold-italic">&#x2202;</mml:mi>
<mml:msub>
<mml:mi mathvariant="bold-italic">U</mml:mi>
<mml:mi mathvariant="bold-italic">i</mml:mi>
</mml:msub>
</mml:mrow>
<mml:mrow>
<mml:mi mathvariant="bold-italic">&#x2202;</mml:mi>
<mml:msub>
<mml:mi mathvariant="bold-italic">x</mml:mi>
<mml:mi mathvariant="bold-italic">j</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfrac>
<mml:mo>&#x2b;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mi mathvariant="bold-italic">&#x2202;</mml:mi>
<mml:msub>
<mml:mi mathvariant="bold-italic">U</mml:mi>
<mml:mi mathvariant="bold-italic">j</mml:mi>
</mml:msub>
</mml:mrow>
<mml:mrow>
<mml:mi mathvariant="bold-italic">&#x2202;</mml:mi>
<mml:msub>
<mml:mi mathvariant="bold-italic">x</mml:mi>
<mml:mi mathvariant="bold-italic">i</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(3)</label>
</disp-formula>where <inline-formula id="inf6">
<mml:math id="m9">
<mml:mrow>
<mml:msub>
<mml:mi>U</mml:mi>
<mml:mi>i</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is blood velocity and <inline-formula id="inf7">
<mml:math id="m10">
<mml:mrow>
<mml:mi>&#x3bc;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is blood viscosity.</p>
<p>The Lagrange method was applied to track particle trajectories between the inlet and outlet of the device. The HI values were integrated along each particle trajectory and averaged to determine the total HI value of the blood flowing through the device (<xref ref-type="bibr" rid="B10">Garon and Farinas, 2004</xref>). <xref ref-type="disp-formula" rid="e4">Equation 4</xref> is the specific calculation formula. The HI along all pathlines were considered representative of the overall HI for the pump.<disp-formula id="e4">
<mml:math id="m11">
<mml:mrow>
<mml:mi mathvariant="bold-italic">H</mml:mi>
<mml:mi mathvariant="bold-italic">I</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mn mathvariant="bold">1</mml:mn>
</mml:mrow>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="bold-italic">N</mml:mi>
<mml:mi mathvariant="bold-italic">P</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfrac>
<mml:mstyle displaystyle="true">
<mml:munderover>
<mml:mo>&#x2211;</mml:mo>
<mml:mrow>
<mml:mi mathvariant="bold-italic">P</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn mathvariant="bold">1</mml:mn>
</mml:mrow>
<mml:msub>
<mml:mi mathvariant="bold-italic">N</mml:mi>
<mml:mi mathvariant="bold-italic">P</mml:mi>
</mml:msub>
</mml:munderover>
</mml:mstyle>
<mml:mi mathvariant="bold-italic">C</mml:mi>
<mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mstyle displaystyle="true">
<mml:munderover>
<mml:mo>&#x2211;</mml:mo>
<mml:mrow>
<mml:mi mathvariant="bold-italic">i</mml:mi>
<mml:mi mathvariant="bold-italic">n</mml:mi>
<mml:mi mathvariant="bold-italic">l</mml:mi>
<mml:mi mathvariant="bold-italic">e</mml:mi>
<mml:mi mathvariant="bold-italic">t</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi mathvariant="bold-italic">o</mml:mi>
<mml:mi mathvariant="bold-italic">u</mml:mi>
<mml:mi mathvariant="bold-italic">t</mml:mi>
<mml:mi mathvariant="bold-italic">l</mml:mi>
<mml:mi mathvariant="bold-italic">e</mml:mi>
<mml:mi mathvariant="bold-italic">t</mml:mi>
</mml:mrow>
</mml:munderover>
</mml:mstyle>
<mml:mo>&#x2206;</mml:mo>
<mml:mi mathvariant="bold-italic">t</mml:mi>
<mml:msup>
<mml:mi mathvariant="bold-italic">&#x3c4;</mml:mi>
<mml:mrow>
<mml:mi mathvariant="bold-italic">&#x3b1;</mml:mi>
<mml:mo>/</mml:mo>
<mml:mi mathvariant="bold-italic">&#x3b2;</mml:mi>
</mml:mrow>
</mml:msup>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mi mathvariant="bold-italic">&#x3b2;</mml:mi>
</mml:msup>
</mml:mrow>
</mml:math>
<label>(4)</label>
</disp-formula>where <inline-formula id="inf8">
<mml:math id="m12">
<mml:mrow>
<mml:mi>C</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1.228</mml:mn>
<mml:mo>&#xd7;</mml:mo>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mn>5</mml:mn>
</mml:mrow>
</mml:msup>
<mml:mo>;</mml:mo>
<mml:mi>&#x3b1;</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1.9918</mml:mn>
<mml:mo>;</mml:mo>
<mml:mi>&#x3b2;</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.6606</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula> for ovine blood (<xref ref-type="bibr" rid="B4">Ding et al., 2015</xref>). <inline-formula id="inf9">
<mml:math id="m13">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is the SSS, <inline-formula id="inf10">
<mml:math id="m14">
<mml:mrow>
<mml:mo>&#x2206;</mml:mo>
<mml:mi>t</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is the RT. <inline-formula id="inf11">
<mml:math id="m15">
<mml:mrow>
<mml:msub>
<mml:mi>N</mml:mi>
<mml:mi>P</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the number of track particles.</p>
</sec>
</sec>
<sec id="s2-4">
<title>2.4 Validation</title>
<p>Experimental tests were carried out to evaluate the hydraulic performance of the baseline pump. The experimental setup is depicted in <xref ref-type="fig" rid="F2">Figure 2</xref>. The pump head was fabricated from transparent polycarbonate (PC) material, with both internal and external surfaces polished to minimize flow resistance. A water&#x2013;glycerol mixture (viscosity of 0.0035 Pa&#xb7;s at 24&#xb0;C) was used to match blood viscosity. Although this Newtonian fluid does not capture the shear-thinning behavior of real blood, prior studies suggest that in high-shear regions (&#x3e;100 s<sup>&#x2212;1</sup>), the approximation remains valid for hydraulic performance validation. The inlet and outlet pressures were measured using digital pressure sensors (model GP-M001, Keyence), while an ultrasonic flow meter (model FD-XS20, Keyence) was used to capture the volumetric flow rates. To assess the pump&#x2019;s performance under different operating conditions, various experimental scenarios were established by adjusting the pump&#x2019;s rotational speed and the proportional valve on the outflow tubing. These adjustments allowed for a comprehensive evaluation of the pump&#x2019;s hydraulic characteristics. It was assumed that maintaining the rotational stability of the motor shaft would not significantly affect the fluid dynamics. The pump was tested across a range of rotational speeds, from 2,500 to 3,500 rpm, with 24 operational tests conducted to record pressure head and flow rate data.</p>
<fig id="F2" position="float">
<label>FIGURE 2</label>
<caption>
<p>Schematic and photograph of the flow loop used to simulate hydraulic properties.</p>
</caption>
<graphic xlink:href="fphys-16-1595588-g002.tif">
<alt-text content-type="machine-generated">Diagram and photograph of a laboratory setup. The diagram labels components as follows: 1 is a blood pump at the inlet, 2 are pressure sensors, 3 is a flow meter, 4 is a proportional valve, and 5 is a reservoir. The photograph shows the physical components on a lab bench, arranged similarly to the diagram, with each component labeled corresponding to the diagram's numbers.</alt-text>
</graphic>
</fig>
<p>As illustrated in <xref ref-type="fig" rid="F3">Figure 3</xref>, a range of particle trace numbers was selected to assess their predictive accuracy for hemolysis. It was observed that when the particle trace number reached 1,600, the hemolysis value remained relatively stable, even with further increases in the number of traces. In order to minimize the calculation error as much as possible, the subsequent HI prediction experiments utilized 2,000 particle traces for calculations.</p>
<fig id="F3" position="float">
<label>FIGURE 3</label>
<caption>
<p>Pathline independence: Sensitivity analysis of particle size number with SSS(Pa), RT(s) and HI.</p>
</caption>
<graphic xlink:href="fphys-16-1595588-g003.tif">
<alt-text content-type="machine-generated">Line graph displaying the relationship between pathline number and three parameters: SSS (Pa) in black, RT (s) in red, and HI in blue. The x-axis represents pathline number from 0 to 2000, while the left y-axis represents SSS (4.4 to 4.8) and RT (0.30 to 0.50). The right y-axis indicates HI (0.000120 to 0.000150). Each parameter exhibits distinct patterns, with SSS generally highest, followed by HI, and then RT.</alt-text>
</graphic>
</fig>
</sec>
</sec>
<sec sec-type="results" id="s3">
<title>3 Results</title>
<sec id="s3-1">
<title>3.1 Mesh independence analysis</title>
<p>A mesh independence analysis was conducted to validate the adequacy of mesh quality for precise computational results (see <xref ref-type="table" rid="T3">Table 3</xref>). Four different mesh resolutions, ranging from coarse to fine, were created, and corresponding fluid dynamic simulations were performed to assess the impact of mesh density on the pump head. The predicted pressure head stabilized beyond 2.5 million elements, with Case 3 (3.95 million elements) yielding an error of less than 0.4% compared to the finest mesh. Considering both computational efficiency and accuracy, the third mesh configuration was selected for all subsequent analyses. The grid elements for different pump models were kept at around four million.</p>
<table-wrap id="T3" position="float">
<label>TABLE 3</label>
<caption>
<p>Results of Mesh independence analysis.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Case</th>
<th align="center">Mesh number (<inline-formula id="inf12">
<mml:math id="m16">
<mml:mrow>
<mml:mo>&#xd7;</mml:mo>
<mml:msup>
<mml:mn mathvariant="bold">10</mml:mn>
<mml:mn mathvariant="bold">6</mml:mn>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>)</th>
<th align="center">Average Y&#x2b; of all faces</th>
<th align="center">Head (mmHg)</th>
<th align="center">Error of head (%)</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">1</td>
<td align="center">1.45</td>
<td align="center">9.07</td>
<td align="center">320.75</td>
<td align="center">4.56</td>
</tr>
<tr>
<td align="center">2</td>
<td align="center">2.48</td>
<td align="center">0.361</td>
<td align="center">318.09</td>
<td align="center">3.70</td>
</tr>
<tr>
<td align="center">3</td>
<td align="center">3.95</td>
<td align="center">0.353</td>
<td align="center">305.61</td>
<td align="center">0.37</td>
</tr>
<tr>
<td align="center">4</td>
<td align="center">5.16</td>
<td align="center">0.327</td>
<td align="center">306.75</td>
<td align="center">-</td>
</tr>
</tbody>
</table>
<table-wrap-foot>
<fn>
<p>Error of head (%), defined as &#x7c;head&#x2a; &#x2212; head<sub>4</sub>&#x7c;/head<sub>4</sub> &#x2a; 100, where head<sub>4</sub> is the head predicted for case 4; head&#x2a; represents the head of each case.</p>
</fn>
</table-wrap-foot>
</table-wrap>
</sec>
<sec id="s3-2">
<title>3.2 Experiment validation of hydraulic performance</title>
<p>The relationship between the inlet-outlet pressure difference and flow rate (H-Q curves) at a given rotational speed is a key parameter for assessing the hydraulic performance of a blood pump. The simulated results at various rotational speeds were validated against experimental data as shown in <xref ref-type="fig" rid="F4">Figure 4A</xref>. The overall trend of the H-Q curve exhibits a relatively smooth profile, consistent with the characteristics of a centrifugal pump. The maximum error of approximately 9% observed at 3,500 rpm and 0.1 L/min represents the difference between CFD simulation results and experimental measurements.</p>
<fig id="F4" position="float">
<label>FIGURE 4</label>
<caption>
<p>
<bold>(A)</bold> H-Q curve (the simulated head and measured head at different rotational speeds) of the baseline blood pump; <bold>(B)</bold> Pressure distribution within the baseline pump at 3,000 rpm and 5 L/min; <bold>(C)</bold> Velocity vector field showing flow direction and magnitude.</p>
</caption>
<graphic xlink:href="fphys-16-1595588-g004.tif">
<alt-text content-type="machine-generated">Graph A shows pressure head (H) versus flow rate (Q) for different RPMs, with distinct computational and experimental data. Image B is a pressure distribution diagram in a circular structure, ranging from -350 to 0 mm Hg. Image C displays a velocity field in a streamline pattern, with velocities from 0.00 to 8.00 m/s.</alt-text>
</graphic>
</fig>
<p>To further validate the flow characteristics within the pump, the pressure and velocity vector fields of the baseline model were extracted at a flow rate of 5 L/min and a rotation speed of 3,000 rpm. These measurements were taken from the cross-section, as illustrated in <xref ref-type="fig" rid="F4">Figures 4B, C</xref>. Localized low-pressure regions are observed near the leading edge of the blades and the center column. Pressure increases radially from the center toward the periphery, corresponding to the acceleration of fluid outward, which results in a pressure rise. The volute exhibits a uniform distribution, with a pronounced pressure increase observed near the outlet.</p>
</sec>
<sec id="s3-3">
<title>3.3 Influence of clearance on hydraulic performance</title>
<p>The influence of secondary flow path clearances on hydraulic performance was systematically assessed across 25 orthogonal design combinations (<xref ref-type="table" rid="T4">Table 4</xref>). The changes in clearance affected the pump volume minimally (&#x3c;3%), and the variations in pressure head and efficiency remained within &#xb1;3% and &#xb1;5%, respectively, suggesting a limited influence of secondary flow path clearance adjustments on pump hydraulic performance. Compared with the baseline pump, several configurations significantly improved the hydraulic head and efficiency. Model 16 achieved the highest efficiency (&#x2b;5.16%), while Model 21 attained the maximum pressure head (&#x2b;3.10%). However, certain designs, such as Model 13, led to performance deterioration (efficiency &#x2212;4.53%), indicating sensitivity to structural changes. An increase in clearance results in a higher leakage flow within the secondary flow path.</p>
<table-wrap id="T4" position="float">
<label>TABLE 4</label>
<caption>
<p>Comparison of hydraulic properties of different clearance sizes.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Model</th>
<th align="center">Volume (V) (mL)</th>
<th align="center">V<sub>error</sub> (%)</th>
<th align="center">Head (H) (mmHg)</th>
<th align="center">H<sub>error</sub> (%)</th>
<th align="center">Efficiency (&#x3b7;) (%)</th>
<th align="center">&#x3b7;<sub>error</sub> (%)</th>
<th align="center">Leakage flow (kg/s)</th>
<th align="center">Leakage portion (%)</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">1</td>
<td align="center">32.91</td>
<td align="center">&#x2212;0.21</td>
<td align="center">310.87</td>
<td align="center">1.72</td>
<td align="center">42.75</td>
<td align="center">1.83</td>
<td align="center">0.00143</td>
<td align="center">1.63</td>
</tr>
<tr>
<td align="center">2</td>
<td align="center">33.10</td>
<td align="center">0.37</td>
<td align="center">307.23</td>
<td align="center">0.53</td>
<td align="center">41.50</td>
<td align="center">&#x2212;1.14</td>
<td align="center">0.00059</td>
<td align="center">0.67</td>
</tr>
<tr>
<td align="center">3</td>
<td align="center">33.30</td>
<td align="center">0.96</td>
<td align="center">303.33</td>
<td align="center">&#x2212;0.75</td>
<td align="center">41.11</td>
<td align="center">&#x2212;2.07</td>
<td align="center">0.00060</td>
<td align="center">0.68</td>
</tr>
<tr>
<td align="center">4</td>
<td align="center">33.50</td>
<td align="center">1.60</td>
<td align="center">305.31</td>
<td align="center">&#x2212;0.10</td>
<td align="center">41.52</td>
<td align="center">&#x2212;1.10</td>
<td align="center">0.00116</td>
<td align="center">1.32</td>
</tr>
<tr>
<td align="center">5</td>
<td align="center">33.71</td>
<td align="center">2.22</td>
<td align="center">307.96</td>
<td align="center">0.77</td>
<td align="center">41.70</td>
<td align="center">&#x2212;0.67</td>
<td align="center">0.00048</td>
<td align="center">0.55</td>
</tr>
<tr>
<td align="center">6 (baseline pump)</td>
<td align="center">32.98</td>
<td align="center">&#x2014;</td>
<td align="center">305.61</td>
<td align="center">&#x2014;</td>
<td align="center">41.98</td>
<td align="center">&#x2014;</td>
<td align="center">0.00052</td>
<td align="center">0.59</td>
</tr>
<tr>
<td align="center">7</td>
<td align="center">33.17</td>
<td align="center">0.59</td>
<td align="center">305.52</td>
<td align="center">&#x2212;0.03</td>
<td align="center">41.67</td>
<td align="center">&#x2212;0.74</td>
<td align="center">0.00081</td>
<td align="center">0.93</td>
</tr>
<tr>
<td align="center">8</td>
<td align="center">33.38</td>
<td align="center">1.21</td>
<td align="center">301.63</td>
<td align="center">&#x2212;1.30</td>
<td align="center">41.02</td>
<td align="center">&#x2212;2.29</td>
<td align="center">0.00065</td>
<td align="center">0.74</td>
</tr>
<tr>
<td align="center">9</td>
<td align="center">33.58</td>
<td align="center">1.82</td>
<td align="center">310.93</td>
<td align="center">1.74</td>
<td align="center">42.20</td>
<td align="center">0.52</td>
<td align="center">0.00119</td>
<td align="center">1.36</td>
</tr>
<tr>
<td align="center">10</td>
<td align="center">33.78</td>
<td align="center">2.44</td>
<td align="center">313.30</td>
<td align="center">2.52</td>
<td align="center">43.47</td>
<td align="center">3.54</td>
<td align="center">0.00049</td>
<td align="center">0.56</td>
</tr>
<tr>
<td align="center">11</td>
<td align="center">33.05</td>
<td align="center">0.21</td>
<td align="center">301.04</td>
<td align="center">&#x2212;1.50</td>
<td align="center">40.98</td>
<td align="center">&#x2212;2.38</td>
<td align="center">0.00059</td>
<td align="center">0.68</td>
</tr>
<tr>
<td align="center">12</td>
<td align="center">33.24</td>
<td align="center">0.80</td>
<td align="center">301.42</td>
<td align="center">&#x2212;1.37</td>
<td align="center">40.52</td>
<td align="center">&#x2212;3.48</td>
<td align="center">0.00047</td>
<td align="center">0.53</td>
</tr>
<tr>
<td align="center">13</td>
<td align="center">33.45</td>
<td align="center">1.42</td>
<td align="center">301.87</td>
<td align="center">&#x2212;1.22</td>
<td align="center">40.08</td>
<td align="center">&#x2212;4.53</td>
<td align="center">0.00084</td>
<td align="center">0.96</td>
</tr>
<tr>
<td align="center">14</td>
<td align="center">33.65</td>
<td align="center">2.03</td>
<td align="center">305.06</td>
<td align="center">&#x2212;0.18</td>
<td align="center">41.21</td>
<td align="center">&#x2212;1.82</td>
<td align="center">0.00091</td>
<td align="center">1.04</td>
</tr>
<tr>
<td align="center">15</td>
<td align="center">33.85</td>
<td align="center">2.65</td>
<td align="center">305.89</td>
<td align="center">0.09</td>
<td align="center">41.96</td>
<td align="center">&#x2212;0.05</td>
<td align="center">0.00047</td>
<td align="center">0.53</td>
</tr>
<tr>
<td align="center">16</td>
<td align="center">33.19</td>
<td align="center">0.64</td>
<td align="center">304.23</td>
<td align="center">&#x2212;0.45</td>
<td align="center">44.15</td>
<td align="center">5.16</td>
<td align="center">0.00113</td>
<td align="center">1.29</td>
</tr>
<tr>
<td align="center">17</td>
<td align="center">33.31</td>
<td align="center">1.02</td>
<td align="center">301.88</td>
<td align="center">&#x2212;1.22</td>
<td align="center">40.81</td>
<td align="center">&#x2212;2.79</td>
<td align="center">0.00054</td>
<td align="center">0.62</td>
</tr>
<tr>
<td align="center">18</td>
<td align="center">33.52</td>
<td align="center">1.63</td>
<td align="center">310.10</td>
<td align="center">1.47</td>
<td align="center">40.81</td>
<td align="center">&#x2212;2.79</td>
<td align="center">0.00108</td>
<td align="center">1.24</td>
</tr>
<tr>
<td align="center">19</td>
<td align="center">33.72</td>
<td align="center">2.25</td>
<td align="center">307.63</td>
<td align="center">0.66</td>
<td align="center">42.93</td>
<td align="center">2.27</td>
<td align="center">0.00090</td>
<td align="center">1.02</td>
</tr>
<tr>
<td align="center">20</td>
<td align="center">33.92</td>
<td align="center">2.87</td>
<td align="center">304.03</td>
<td align="center">&#x2212;0.52</td>
<td align="center">40.81</td>
<td align="center">&#x2212;2.78</td>
<td align="center">0.00085</td>
<td align="center">0.98</td>
</tr>
<tr>
<td align="center">21</td>
<td align="center">33.19</td>
<td align="center">0.64</td>
<td align="center">315.10</td>
<td align="center">3.10</td>
<td align="center">42.16</td>
<td align="center">0.42</td>
<td align="center">0.00055</td>
<td align="center">0.62</td>
</tr>
<tr>
<td align="center">22</td>
<td align="center">33.38</td>
<td align="center">1.23</td>
<td align="center">301.15</td>
<td align="center">&#x2212;1.46</td>
<td align="center">40.80</td>
<td align="center">&#x2212;2.81</td>
<td align="center">0.00066</td>
<td align="center">0.75</td>
</tr>
<tr>
<td align="center">23</td>
<td align="center">33.59</td>
<td align="center">1.84</td>
<td align="center">307.34</td>
<td align="center">0.57</td>
<td align="center">43.18</td>
<td align="center">2.85</td>
<td align="center">0.00070</td>
<td align="center">0.80</td>
</tr>
<tr>
<td align="center">24</td>
<td align="center">33.79</td>
<td align="center">2.46</td>
<td align="center">299.81</td>
<td align="center">&#x2212;1.90</td>
<td align="center">41.05</td>
<td align="center">&#x2212;2.22</td>
<td align="center">0.00072</td>
<td align="center">0.83</td>
</tr>
<tr>
<td align="center">25</td>
<td align="center">33.99</td>
<td align="center">3.08</td>
<td align="center">304.13</td>
<td align="center">&#x2212;0.48</td>
<td align="center">40.26</td>
<td align="center">&#x2212;4.10</td>
<td align="center">0.00115</td>
<td align="center">1.31</td>
</tr>
</tbody>
</table>
<table-wrap-foot>
<fn>
<p>V<sub>error</sub>, defined as (V&#x2a; &#x2212; V<sub>baseline</sub>)&#x2215;V<sub>baseline</sub>&#x2a;100; V&#x2a; represents the volume of each model; H<sub>error</sub>, defined as (H&#x2a; &#x2212; H<sub>baseline</sub>)&#x2215;H<sub>baseline</sub>&#x2a;100; H&#x2a; represents the pressure head of each model; <bold>&#x3b7;</bold>
<sub>error</sub>, defined as (<bold>&#x3b7;</bold>&#x2a; &#x2212; <bold>&#x3b7;</bold>
<sub>baseline</sub>)&#x2215;<bold>&#x3b7;</bold>
<sub>baseline</sub>&#x2a;100; <bold>&#x3b7;</bold>&#x2a; represents the efficiency of each model. Ratio of Leakage flow (%), defined as Q<sub>leakage flow</sub>/Q<sub>inlet</sub>. The leakage flow is defined as the flow rate at the cross-section of the inlet of the secondary flow path.</p>
</fn>
</table-wrap-foot>
</table-wrap>
</sec>
<sec id="s3-4">
<title>3.4 Influence of clearance on SSS</title>
<p>High SSS areas increase the risk of thrombosis, and identifying high SSS areas in the blood pump is important for predicting the probability of thrombosis. It was classified into three levels: (1) above 9 Pa: induced von Willebrand factor cleavage; (2) above 50 Pa can induce platelet activation; (3) above 150 Pa, associated with hemolysis risk (<xref ref-type="bibr" rid="B9">Fraser et al., 2012</xref>). <xref ref-type="fig" rid="F5">Figure 5</xref> illustrates the volume ratios of SSS exceeding 50 and 150 Pa across the 25 models. The volume fraction corresponding to high shear stress (&#x3e;50 Pa) ranges from approximately 0.46%&#x2013;0.51%, indicating that although high shear regions occupy a relatively small portion of the total volume, they still pose a potential risk of hemolysis. For regions with extremely high shear stress (&#x3e;150 Pa), the volume fraction is even smaller, consistently below 0.0073%. Among all models, Model 2 exhibits the highest proportion of regions with SSS greater than 50 Pa, reaching 0.51%, whereas Model 25 shows the lowest proportion at 0.46%. Regarding the extremely high shear stress (&#x3e;150 Pa), the baseline pump displays the highest volume ratio of 0.0073%, while Model 25 has the lowest at 0.0057%.</p>
<fig id="F5" position="float">
<label>FIGURE 5</label>
<caption>
<p>Statistical comparison of the volume proportions exceeding shear stress thresholds of 50 and 150 Pa across all 25 pump configurations.</p>
</caption>
<graphic xlink:href="fphys-16-1595588-g005.tif">
<alt-text content-type="machine-generated">Two bar charts compare the performance of 25 models against a baseline pump. The top chart shows data for pressure greater than fifty pascals, with values ranging from 0.46 to 0.51 percent. The bottom chart displays pressure greater than one hundred fifty pascals, with values from 0.0051 to 0.0073 percent. Models consistently meet or exceed the baseline in both charts.</alt-text>
</graphic>
</fig>
<p>To further illustrate the spatial characteristics of shear stress distribution, the baseline pump model (Model 6) was selected for detailed visualization of SSS, as shown in <xref ref-type="fig" rid="F6">Figure 6</xref>. This configuration exhibits extensive regions exceeding the hemolysis threshold of 150 Pa, with localized high-shear zones observed near the leading edges of the impeller blades, the volute tongue, and the secondary flow path area.</p>
<fig id="F6" position="float">
<label>FIGURE 6</label>
<caption>
<p>Three-dimensional distribution of SSS(Pa) for the baseline pump.</p>
</caption>
<graphic xlink:href="fphys-16-1595588-g006.tif">
<alt-text content-type="machine-generated">Simulation graphic showing stress distribution in a circular component with internal flow paths. The color scale on the left indicates stress from zero to one hundred pascals, with red representing the highest stress. Enlarged sections emphasize stress concentration points along a secondary flow path.</alt-text>
</graphic>
</fig>
</sec>
<sec id="s3-5">
<title>3.5 Orthogonal analysis and optimal design</title>
<p>In <xref ref-type="fig" rid="F7">Figure 7</xref>, the impact of the radial clearance size in the secondary path on the average SSS, average RT, and HI value of particle paths is compared. The RT heat map indicates that the overall RT values range from 0.32 to 0.42 s. With the increase of L<sub>2</sub>, especially when L<sub>1</sub> is small (such as 600 &#x3bc;m), RT tends to increase initially and then decrease. In contrast, when L<sub>1</sub> and L<sub>2</sub> is larger (such as 900&#x2013;1,000 &#x3bc;m), the distribution of RT becomes more uniform. The maximum RT occurred at L<sub>1</sub> &#x3d; 800 &#x3bc;m and L<sub>2</sub> &#x3d; 1,000 &#x3bc;m (0.419 s), while the minimum value occurred at L<sub>1</sub> &#x3d; 900 &#x3bc;m and L<sub>2</sub> &#x3d; 600 &#x3bc;m (0.321 s). The SSS heat map shows relatively small variation across the parameter space, with most values falling between 4.5 and 5.0 Pa. The SSS value reaches the maximum (5.018 Pa) at L<sub>1</sub> &#x3d; 800 &#x3bc;m and L<sub>2</sub> &#x3d; 800 &#x3bc;m, whereas the minimum (4.518 Pa) at L<sub>1</sub> &#x3d; 600 &#x3bc;m and L<sub>2</sub> &#x3d; 800 &#x3bc;m. When L<sub>1</sub> or L<sub>2</sub> is fixed, SSS does not exhibit a clear monotonic trend but instead shows nonlinear fluctuations, indicating that L<sub>1</sub> and L<sub>2</sub> have a complex coupling effect on shear stress. When L<sub>1</sub> &#x3d; 600 &#x3bc;m and L<sub>2</sub> &#x3d; 800 &#x3bc;m, the HI is the lowest at 0.00012%. While the highest HI (0.00016%) appears at L<sub>1</sub> &#x3d; 800 &#x3bc;m and L<sub>2</sub> &#x3d; 700 &#x3bc;m. Compared with the baseline pump, the HI shows a minimum reduction of 8.76% and a maximum increase of 23.86%. Overall, HI tends to increase slightly with higher SSS; however, the correlation is not strictly consistent. To quantitatively assess the relative contributions of RT and SSS to hemolysis, a linear regression analysis was performed between the predicted HI and each of the two parameters across 25 simulation cases (<xref ref-type="fig" rid="F8">Figure 8</xref>). The results show that HI exhibited a stronger correlation with SSS (<italic>R</italic>
<sup>2</sup> &#x3d; 0.758) than with RT (<italic>R</italic>
<sup>2</sup> &#x3d; 0.667), indicating that shear-induced damage is more predictive of hemolysis than particle RT.</p>
<fig id="F7" position="float">
<label>FIGURE 7</label>
<caption>
<p>Heatmaps showing the distribution of RT(s), SSS(Pa), and HI across 25 pump configurations with varying secondary clearance combinations.</p>
</caption>
<graphic xlink:href="fphys-16-1595588-g007.tif">
<alt-text content-type="machine-generated">Three heatmaps display data for different metrics across L1 and L2 measurements in micrometers. The first heatmap, in blue, shows RT values ranging from 0.340 to 0.557. The second, in green, displays SSS values from 4.534 to 5.348. The third, in red, presents HI values between 1.25E-4 and 2.10E-4. Each heatmap has a grid with specific numerical data corresponding to varying L1 and L2 values.</alt-text>
</graphic>
</fig>
<fig id="F8" position="float">
<label>FIGURE 8</label>
<caption>
<p>Linear regression analysis of HI with two key hemodynamic parameters: RT(s) and SSS(Pa).</p>
</caption>
<graphic xlink:href="fphys-16-1595588-g008.tif">
<alt-text content-type="machine-generated">The image shows two scatter plots with trend lines. The left plot depicts the relationship between HI and SSS (Pa), with an R-squared value of 0.758. The right plot shows the relationship between HI and RT (s), with an R-squared value of 0.667. Both graphs have a positive linear trend.</alt-text>
</graphic>
</fig>
<p>Turbulent viscosity serves as a key indicator for characterizing the intensity of turbulence within the pump. <xref ref-type="fig" rid="F9">Figure 9</xref> present the streamlines of three representative pump models, with color maps indicating turbulent viscosity and velocity, respectively. Model 23 exhibits substantially higher turbulent viscosity throughout the pump compared to Models 3 and 5, with Model 5 showing moderately higher values than Model 3. These results indicate that compared with the optimal model, increasing either the inner (L<sub>1</sub>) or outer (L<sub>2</sub>) secondary clearance leads to a notable increase in turbulence intensity, particularly within the secondary flow path regions.</p>
<fig id="F9" position="float">
<label>FIGURE 9</label>
<caption>
<p>The streamlines of the three selected models are colored using <bold>(A)</bold> turbulence intensity and <bold>(B)</bold> velocity.</p>
</caption>
<graphic xlink:href="fphys-16-1595588-g009.tif">
<alt-text content-type="machine-generated">Flow visualization images depict eddy viscosity and velocity in different models. Section A shows eddy viscosity with a scale from blue to red indicating viscosity levels in pascals per second. Section B illustrates velocity with colors from blue to red representing velocity magnitude in meters per second. Model parameters include L&#x2081; and L&#x2082; with specified micrometer measurements for Models 5, 3, and 23.</alt-text>
</graphic>
</fig>
<p>Calculate the RT, SSS, and HI of the blood pump by 25 groups of orthogonal designs. <xref ref-type="table" rid="T5">Table 5</xref> presents the mean values of the three indicators calculated using <xref ref-type="disp-formula" rid="e5">Equation 5</xref> at each level of each factor.<disp-formula id="e5">
<mml:math id="m17">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="bold-italic">k</mml:mi>
<mml:mi mathvariant="bold-italic">i</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mn mathvariant="bold">1</mml:mn>
</mml:mrow>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="bold-italic">N</mml:mi>
<mml:mi mathvariant="bold-italic">i</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfrac>
<mml:msub>
<mml:mi mathvariant="bold-italic">K</mml:mi>
<mml:mi mathvariant="bold-italic">i</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mn mathvariant="bold">1</mml:mn>
</mml:mrow>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="bold-italic">N</mml:mi>
<mml:mi mathvariant="bold-italic">i</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfrac>
<mml:mstyle displaystyle="true">
<mml:munderover>
<mml:mo>&#x2211;</mml:mo>
<mml:mrow>
<mml:mi mathvariant="bold-italic">j</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn mathvariant="bold">1</mml:mn>
</mml:mrow>
<mml:msub>
<mml:mi mathvariant="bold-italic">N</mml:mi>
<mml:mi mathvariant="bold-italic">i</mml:mi>
</mml:msub>
</mml:munderover>
</mml:mstyle>
<mml:msub>
<mml:mi mathvariant="bold-italic">y</mml:mi>
<mml:mi mathvariant="bold-italic">i</mml:mi>
</mml:msub>
<mml:mo>,</mml:mo>
<mml:mi mathvariant="bold-italic">j</mml:mi>
</mml:mrow>
</mml:math>
<label>(5)</label>
</disp-formula>
</p>
<table-wrap id="T5" position="float">
<label>TABLE 5</label>
<caption>
<p>The sum and mean of each level of every factor.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th rowspan="2" align="center">Factor</th>
<th rowspan="2" align="center">Level</th>
<th colspan="3" align="center">Results</th>
</tr>
<tr>
<th align="center">Average RT(s)</th>
<th align="center">Average SSS(Pa)</th>
<th align="center">Average HI</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td rowspan="5" align="center">L<sub>1</sub>
</td>
<td align="center">600</td>
<td align="center">0.366</td>
<td align="center">4.773</td>
<td align="center">0.000142</td>
</tr>
<tr>
<td align="center">700</td>
<td align="center">0.347</td>
<td align="center">4.721</td>
<td align="center">0.000134</td>
</tr>
<tr>
<td align="center">800</td>
<td align="center">0.390</td>
<td align="center">4.832</td>
<td align="center">0.000152</td>
</tr>
<tr>
<td align="center">900</td>
<td align="center">0.352</td>
<td align="center">4.811</td>
<td align="center">0.000141</td>
</tr>
<tr>
<td align="center">1,000</td>
<td align="center">0.361</td>
<td align="center">4.795</td>
<td align="center">0.000142</td>
</tr>
<tr>
<td colspan="2" align="center">R</td>
<td align="center">0.043</td>
<td align="center">0.111</td>
<td align="center">0.000018</td>
</tr>
<tr>
<td colspan="2" align="center">Optimal level</td>
<td align="center">700</td>
<td align="center">700</td>
<td align="center">700</td>
</tr>
<tr>
<td rowspan="5" align="center">L<sub>2</sub>
</td>
<td align="center">600</td>
<td align="center">0.363</td>
<td align="center">4.786</td>
<td align="center">0.000142</td>
</tr>
<tr>
<td align="center">700</td>
<td align="center">0.367</td>
<td align="center">4.775</td>
<td align="center">0.000143</td>
</tr>
<tr>
<td align="center">800</td>
<td align="center">0.351</td>
<td align="center">4.790</td>
<td align="center">0.000140</td>
</tr>
<tr>
<td align="center">900</td>
<td align="center">0.360</td>
<td align="center">4.775</td>
<td align="center">0.000141</td>
</tr>
<tr>
<td align="center">1,000</td>
<td align="center">0.375</td>
<td align="center">4.806</td>
<td align="center">0.000146</td>
</tr>
<tr>
<td colspan="2" align="center">R</td>
<td align="center">0.024</td>
<td align="center">0.031</td>
<td align="center">0.000007</td>
</tr>
<tr>
<td colspan="2" align="center">Optimal level</td>
<td align="center">800</td>
<td align="center">700/900</td>
<td align="center">800</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>The range R in <xref ref-type="disp-formula" rid="e6">Equation 6</xref> is the difference between the maximum and minimum values of a single prediction result.<disp-formula id="e6">
<mml:math id="m18">
<mml:mrow>
<mml:mi mathvariant="bold-italic">R</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mi mathvariant="bold-italic">max</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="bold-italic">k</mml:mi>
<mml:mn mathvariant="bold">1</mml:mn>
</mml:msub>
<mml:mo>,</mml:mo>
<mml:msub>
<mml:mi mathvariant="bold-italic">k</mml:mi>
<mml:mn mathvariant="bold">2</mml:mn>
</mml:msub>
<mml:mo>,</mml:mo>
<mml:msub>
<mml:mrow>
<mml:mo>&#x2026;</mml:mo>
<mml:mo>,</mml:mo>
<mml:mi mathvariant="bold-italic">k</mml:mi>
</mml:mrow>
<mml:mi mathvariant="bold-italic">i</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi mathvariant="bold-italic">min</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="bold-italic">k</mml:mi>
<mml:mn mathvariant="bold">1</mml:mn>
</mml:msub>
<mml:mo>,</mml:mo>
<mml:mi mathvariant="bold-italic">k</mml:mi>
<mml:mo>,</mml:mo>
<mml:msub>
<mml:mrow>
<mml:mo>&#x2026;</mml:mo>
<mml:mo>,</mml:mo>
<mml:mi mathvariant="bold-italic">k</mml:mi>
</mml:mrow>
<mml:mi mathvariant="bold-italic">i</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(6)</label>
</disp-formula>
</p>
<p>The R value reflects the impact of each factor on the optimization; a larger R value indicates a greater influence. As shown in <xref ref-type="table" rid="T5">Table 5</xref>, the influence of L<sub>1</sub> on average SSS, average RT, and average HI is consistently greater than that of L<sub>2</sub>. The minimum average SSS values for factors L<sub>1</sub> and L<sub>2</sub> occur at 700 and 800 &#x3bc;m, respectively. For average RT, the minimum values correspond to 700 &#x3bc;m for L<sub>1</sub> and 700 &#x3bc;m or 900 &#x3bc;m for L<sub>2</sub>. When HI is taken as the final optimization objective, the optimal design parameter combination is L<sub>1</sub> &#x3d; 700 &#x3bc;m and L<sub>2</sub> &#x3d; 800 &#x3bc;m.</p>
</sec>
</sec>
<sec sec-type="discussion" id="s4">
<title>4 Discussion</title>
<p>This study presents a pump head suitable for a fully maglev non-contact centrifugal pump designed for use in VADs. The pump head&#x2019;s hydraulic and hemodynamic performance was assessed through a combination of CFD simulations and experimental validation. The use of an unstructured tetrahedral mesh model in conjunction with the k-&#x3c9; shear stress transport turbulence model provided a detailed understanding of the flow dynamics within the pump. The grid independence analysis method was used to evaluate the variation in pump head pressure with different grid numbers. Finally, about four million grid cells were selected for CFD calculation and analysis. After conducting the hydraulic test, the pressure-flow curve of the centrifugal pump was created. The results indicated that the simulated head pressure was consistent with the measured head pressure. The pressure of the centrifugal pump changed gently with the flow rate during the whole working process, and there was no pressure distortion, indicating that the flow field design of the pump was reasonable.</p>
<p>Our results demonstrate that variations in secondary clearance (L<sub>1</sub> and L<sub>2</sub>) have a limited influence on overall hydraulic performance, with pressure head and efficiency fluctuating within &#xb1;5%. This aligns with the findings by <xref ref-type="bibr" rid="B8">Fischer et al. (2025)</xref>, who reported that axial and radial clearance size variations (0.5&#x2013;3 mm) had a relatively small effect (&#xb1;10%) on key performance indicators. However, these clearance modifications significantly affect blood compatibility indicators, particularly HI, shear stress distribution, RT, and turbulence intensity. Among all tested configurations, the combination of L<sub>1</sub> &#x3d; 600 &#xb5;m and L<sub>2</sub> &#x3d; 800 &#xb5;m yielded the lowest HI, demonstrating an 8.76% improvement over the baseline.</p>
<p>Analysis of shear stress and flow patterns revealed that hemolysis is primarily driven by localized high shear stress zones and prolonged blood residence in recirculatory regions. The average RT of the particles varies with the increase of the clearance in the secondary flow path. A common trend observed is that if L<sub>1</sub> or L<sub>2</sub> is fixed and another clearance size is increased, the average RT first shows a decrease, and then continues to increase as the clearance further increases. Compared to the model with the lowest HI (L<sub>1</sub> &#x3d; 600 &#x3bc;m, L<sub>2</sub> &#x3d; 800 &#x3bc;m), increasing the outer clearance L<sub>2</sub> to 1,000 &#x3bc;m while keeping L<sub>1</sub> fixed led to a rise in RT from 0.333 to 0.399 s, whereas the SSS showed only a slight change (from 4.518 to 4.669 Pa). As shown in <xref ref-type="fig" rid="F9">Figure 9</xref>, this increase in RT is primarily attributed to elevated turbulence intensity within the secondary flow path. In particular, intensified turbulence in the bottom gap region prolongs blood retention, ultimately contributing to a significant increase in the HI. Regression analysis confirmed a stronger correlation between HI and SSS (<italic>R</italic>
<sup>2</sup> &#x3d; 0.758) than RT (<italic>R</italic>
<sup>2</sup> &#x3d; 0.667), reinforcing the dominance of shear-induced hemolysis mechanisms.</p>
<p>Our findings align with previous studies by <xref ref-type="bibr" rid="B22">Rezaienia et al., 2018</xref>) and Fischer et al. (2024), who observed that axial and radial clearances affect hemolysis through their impact on secondary flows and vortices. However, our study extends these insights by employing a denser parametric matrix (25 combinations) and integrating Lagrangian particle tracking to predict HI more accurately. By designing radial clearances of different sizes and predicting their impact on hemolysis, it was found that there is an optimal range for the radial clearance size. Hemolysis is strongly influenced by high shear stress and flow recirculation, and proper clearance selection can mitigate these effects without significantly compromising hydraulic performance.</p>
<p>Studies have shown that hemolysis is closely related to high shear stress and flow recirculation within the pump, and the design of the secondary flow path clearance can significantly influence these factors. Although experiments have partially verified the simulation and numerical predictions presented in this study, there are still some parts that need to be continued. While this work examined the effects of selected discrete combinations of inner (L<sub>1</sub>) and outer (L<sub>2</sub>) clearance sizes on hemodynamic and hemolytic performance, a comprehensive sensitivity analysis across a continuous range of gap sizes was not feasible due to computational constraints. Future studies will aim to conduct higher-resolution parametric analyses and incorporate uncertainty quantification to more thoroughly assess the influence of clearance variations on pump performance and blood compatibility. Moreover, the current numerical model employed a steady-state CFD approach. However, transient simulations are necessary to capture time-dependent shear stress fluctuations and hemolysis dynamics, which are important for evaluating the pump&#x2019;s washing efficiency and long-term blood compatibility (<xref ref-type="bibr" rid="B7">Fang et al., 2023</xref>). Incorporating unsteady flow analysis in future work will enable a more accurate and holistic understanding of pump performance under physiological conditions. This study also adopted a Newtonian fluid model to simplify blood rheology. Nonetheless, it is well recognized that blood exhibits non-Newtonian shear-thinning behavior, particularly in low shear regions where viscosity can vary significantly. Future simulations will adopt a Carreau&#x2013;Yasuda model to more accurately represent the shear-dependent viscosity and improve the predictive accuracy of hemolysis risk. Finally, further <italic>in vitro</italic> validation, especially direct quantification of hemolysis, is essential to confirm the numerical findings and assess the clinical viability of the pump design. In particular, prolonged RT in low-shear regions not only exacerbates hemolysis but also elevates thrombogenic risk due to platelet activation and aggregation. Therefore, future research should also include thrombogenicity evaluation to provide a comprehensive assessment of the pump&#x2019;s blood compatibility.</p>
</sec>
</body>
<back>
<sec sec-type="data-availability" id="s5">
<title>Data availability statement</title>
<p>The raw data supporting the conclusion of this article will be made available by the authors, without undue reservation.</p>
</sec>
<sec sec-type="author-contributions" id="s6">
<title>Author contributions</title>
<p>CZ: Conceptualization, Formal Analysis, Methodology, Software, Validation, Writing &#x2013; original draft, Writing &#x2013; review and editing. PY: Supervision, Writing &#x2013; review and editing. ZC: Project administration, Resources, Supervision, Writing &#x2013; review and editing.</p>
</sec>
<sec sec-type="funding-information" id="s7">
<title>Funding</title>
<p>The author(s) declare that no financial support was received for the research and/or publication of this article.</p>
</sec>
<sec sec-type="COI-statement" id="s8">
<title>Conflict of interest</title>
<p>The authors declare that the research was conducted in the absence of any commercial or financial relationships that could be construed as a potential conflict of interest.</p>
</sec>
<sec sec-type="ai-statement" id="s9">
<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="s10">
<title>Publisher&#x2019;s note</title>
<p>All claims expressed in this article are solely those of the authors and do not necessarily represent those of their affiliated organizations, or those of the publisher, the editors and the reviewers. Any product that may be evaluated in this article, or claim that may be made by its manufacturer, is not guaranteed or endorsed by the publisher.</p>
</sec>
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