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<front>
<journal-meta>
<journal-id journal-id-type="pmc">CMES</journal-id>
<journal-id journal-id-type="nlm-ta">CMES</journal-id>
<journal-id journal-id-type="publisher-id">CMES</journal-id>
<journal-title-group>
<journal-title>Computer Modeling in Engineering &#x0026; Sciences</journal-title>
</journal-title-group>
<issn pub-type="epub">1526-1506</issn>
<issn pub-type="ppub">1526-1492</issn>
<publisher>
<publisher-name>Tech Science Press</publisher-name>
<publisher-loc>USA</publisher-loc>
</publisher>
</journal-meta>
<article-meta>
<article-id pub-id-type="publisher-id">22716</article-id>
<article-id pub-id-type="doi">10.32604/cmes.2023.022716</article-id>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Article</subject>
</subj-group>
</article-categories>
<title-group>
<article-title>Turbulent Kinetic Energy of Flow during Inhale and Exhale to Characterize the Severity of Obstructive Sleep Apnea Patient</article-title>
<alt-title alt-title-type="left-running-head">Turbulent Kinetic Energy of Flow during Inhale and Exhale to Characterize the Severity of Obstructive Sleep Apnea Patient</alt-title>
<alt-title alt-title-type="right-running-head">Turbulent Kinetic Energy of Flow during Inhale and Exhale to Characterize the Severity of Obstructive Sleep Apnea Patient</alt-title>
</title-group>
<contrib-group content-type="authors">
<contrib id="author-1" contrib-type="author" corresp="yes">
<name name-style="western"><surname>Faizal</surname><given-names>W. M.</given-names>
</name><xref ref-type="aff" rid="aff-1">1</xref><email>wanmohd@unimap.edu.my</email></contrib>
<contrib id="author-2" contrib-type="author">
<name name-style="western"><surname>Khor</surname><given-names>C. Y.</given-names>
</name><xref ref-type="aff" rid="aff-1">1</xref></contrib>
<contrib id="author-3" contrib-type="author">
<name name-style="western"><surname>Yaakob</surname><given-names>Muhammad Nooramin Che</given-names>
</name><xref ref-type="aff" rid="aff-1">1</xref></contrib>
<contrib id="author-4" contrib-type="author">
<name name-style="western"><surname>Ghazali</surname><given-names>N. N. N.</given-names>
</name><xref ref-type="aff" rid="aff-2">2</xref></contrib>
<contrib id="author-5" contrib-type="author">
<name name-style="western"><surname>Zainon</surname><given-names>M. Z.</given-names>
</name><xref ref-type="aff" rid="aff-2">2</xref></contrib>
<contrib id="author-6" contrib-type="author">
<name name-style="western"><surname>Ibrahim</surname><given-names>Norliza Binti</given-names>
</name><xref ref-type="aff" rid="aff-3">3</xref></contrib>
<contrib id="author-7" contrib-type="author">
<name name-style="western"><surname>Razi</surname><given-names>Roziana Mohd</given-names>
</name><xref ref-type="aff" rid="aff-4">4</xref></contrib>
<aff id="aff-1"><label>1</label><institution>Faculty of Mechanical Engineering &#x0026; Technology, University Malaysia Perlis</institution>, <addr-line>Padang Besar, 02100</addr-line>, <country>Malaysia</country></aff>
<aff id="aff-2"><label>2</label><institution>Department of Mechanical Engineering, Faculty of Engineering, University of Malaya</institution>, <addr-line>Kuala Lumpur, 50603</addr-line>, <country>Malaysia</country></aff>
<aff id="aff-3"><label>3</label><institution>Department of Oral &#x0026; Maxillofacial Clinical Science, Faculty of Dentistry, University of Malaya</institution>, <addr-line>Kuala Lumpur, 50603</addr-line>, <country>Malaysia</country></aff>
<aff id="aff-4"><label>4</label><institution>Department of Paediatric Dentistry and Orthodontics, Faculty of Dentistry, University of Malaya</institution>, <addr-line>Kuala Lumpur, 50603</addr-line>, <country>Malaysia</country></aff>
</contrib-group>
<author-notes>
<corresp id="cor1"><label>&#x002A;</label>Corresponding Author: W. M. Faizal. Email: <email>wanmohd@unimap.edu.my</email></corresp>
</author-notes>
<pub-date publication-format="print" date-type="pub" iso-8601-date="2023-01-04">
<day>04</day>
<month>01</month>
<year>2023</year>
</pub-date>
<volume>136</volume>
<issue>1</issue>
<fpage>43</fpage>
<lpage>61</lpage>
<history>
<date date-type="received">
<day>23</day>
<month>3</month>
<year>2022</year>
</date>
<date date-type="accepted">
<day>15</day>
<month>9</month>
<year>2022</year>
</date>
</history>
<permissions>
<copyright-statement>&#x00A9; 2023 Faizal et al.</copyright-statement>
<copyright-year>2023</copyright-year>
<copyright-holder>Faizal et al.</copyright-holder>
<license xlink:href="https://creativecommons.org/licenses/by/4.0/">
<license-p>This work is licensed under a <ext-link ext-link-type="uri" xlink:type="simple" xlink:href="https://creativecommons.org/licenses/by/4.0/">Creative Commons Attribution 4.0 International License</ext-link>, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.</license-p>
</license>
</permissions>
<self-uri content-type="pdf" xlink:href="TSP_CMES_22716.pdf"></self-uri>
<abstract>
<p>This paper aims to investigate and present the numerical investigation of airflow characteristics using Turbulent Kinetic Energy (TKE) to characterize the upper airway with obstructive sleep apnea (OSA) under inhale and exhale breathing conditions. The importance of TKE under both breathing conditions is that it show an accurate method in expressing the severity of flow in sleep disorder. Computational fluid dynamics simulate the upper airway&#x2019;s airflow via steady-state Reynolds-averaged Navier-Stokes (RANS) with k&#x2013;&#x03C9; shear stress transport (SST) turbulence model. The three-dimensional (3D) airway model is created based on the CT scan images of an actual patient, meshed with 1.29 million elements using Materialise Interactive Medical Image Control System (MIMICS) and ANSYS software, respectively. High TKE were noticed around the region after the necking (smaller cross-sectional area) during the inhale and exhale breathing. The turbulent kinetic energy could be used as a valuable measure to identify the severity of OSA. This study is expected to provide a better understanding and clear visualization of the airflow characteristics during the inhale and exhale breathing in the upper airway of patients for medical practitioners in the OSA research field.</p>
</abstract>
<kwd-group kwd-group-type="author">
<kwd>Obstructive sleep apnea</kwd>
<kwd>breathing disorders</kwd>
<kwd>real patient</kwd>
<kwd>CFD</kwd>
<kwd>turbulent kinetic energy</kwd>
</kwd-group>
</article-meta>
</front>
<body>
<sec id="s1">
<label>1</label>
<title>Introduction</title>
<p>Obstructive sleep apnea (OSA) affects the quality of sleep for many patients. The OSA results in a temporary blockage of a patient&#x2019;s airway by several obstructions, such as collapse or laxity of airway tissues, which prevent normal airflow during breathing. The obstruction of the airway leads to hypopnea or apnea. Apnea is the complete blockage of air, while hypopnea is the partial blockage of air. Several situations differ the severity of blockage: relaxation of throat muscle, excessively bulky airway tissues, thick fatty tissue, and tongue falling back to the throat area. Apnea-Hypopnea Index (AHI) is practically used to determine the severity of OSA. Clinical data are collected to determine the severity of OSA via the average number of hypopnea or apnea events per hour of sleep.</p>
<p>Previously, Faizal&#x00A0;et&#x00A0;al.&#x00A0;[<xref ref-type="bibr" rid="ref-1">1</xref>] showed the importance of TKE in visualizing the accurate method in expressing flow concentration during light and heavy breathing for OSA patients. The high intensity of TKE shown in flow concentration during light and heavy breathing might induce high vibration to the soft tissue around the upper airways. Due to this, many previous researchers discovered that the vibration of soft tissue and snoring phenomena during a night of sleep might cause damage to the soft tissues, vessels, and nerves, thus resulting in sleep apnea for the patient [<xref ref-type="bibr" rid="ref-2">2</xref>]. However, the metrics of vibration and snoring are rarely correlated with the airflow effects. According to the principles of fluid mechanics, a turbulent airflow in a passage could cause vibration, leading to structural damage. This phenomenon has already been established in other engineering disciplines, such as in nuclear plants [<xref ref-type="bibr" rid="ref-3">3</xref>], aircraft design [<xref ref-type="bibr" rid="ref-4">4</xref>], and structural design [<xref ref-type="bibr" rid="ref-5">5</xref>]. Thus, it could be argued that a turbulent flow would cause vibration that could damage soft tissues, vessels, and nerves.</p>
<p>Computational fluid dynamics (CFD) has emerged as one of the powerful tools for attaining a deep insight into many medical disorders, including that of OSA [<xref ref-type="bibr" rid="ref-6">6</xref>]. Recently, many researchers focused on fluid mechanics in understanding the flow mechanism inside the upper airway [<xref ref-type="bibr" rid="ref-7">7</xref>&#x2013;<xref ref-type="bibr" rid="ref-9">9</xref>]. It has been applied to study the upper airway anatomy and airflow and discover the virtual reality surgery in sleep-disordered breathing (SDB) [<xref ref-type="bibr" rid="ref-10">10</xref>]. Recently, Faizal&#x00A0;et&#x00A0;al.&#x00A0;[<xref ref-type="bibr" rid="ref-11">11</xref>] reviewed the importance of computational simulation for understanding the human upper airway (HUA) in sleep apnea assessment. Powell&#x00A0;et&#x00A0;al.&#x00A0;[<xref ref-type="bibr" rid="ref-12">12</xref>] constructed a complete CFD model that includes the details of the pharyngeal to investigate the human upper airway that has been used for surgery. Zhao&#x00A0;et&#x00A0;al.&#x00A0;[<xref ref-type="bibr" rid="ref-13">13</xref>] utilized CFD to establish the pharyngeal airway model before and after surgery. The generalized airflow and pressure profile were used to determine the possible relationship with the treatment outcome. The research mentioned above considered seven OSA patients in investigations of the upper airway. It was found that two OSA patients still experienced OSA even after treatment. The flow pattern in the human upper airway [<xref ref-type="bibr" rid="ref-14">14</xref>,<xref ref-type="bibr" rid="ref-15">15</xref>] has been studied using experimental means or via CFD, where the results are focused on the velocity, pressure, and wall shear stress. Similarly, Mylavarapu&#x00A0;et&#x00A0;al.&#x00A0;[<xref ref-type="bibr" rid="ref-16">16</xref>] used the CFD model to simultaneously model the airflow velocity, pressure, and wall shear stress in the human upper airway. With the knowledge of turbulent flow in the human upper airway, it is possible to avoid OSA. Besides, the simulation technique is also applicable in the study of human cough jet development and expiratory droplet dispersion [<xref ref-type="bibr" rid="ref-17">17</xref>]. The large eddy simulation (LES) model has been incorporated with the weakly compressible smoothed particle hydrodynamics method in simulating the cough jet from the human mouth. The cough turbulent flow correlated with the virus droplet dispersion was crucially affected by the two-way coupling of the droplets and ambient air.</p>
<p>Understanding the upper airway flow pattern can help with sleep apnea and respiratory disease treatment. The flow pattern visualization in the actual airways is complex and challenging. Thus, the flow pattern during the inhalation and exhalation breathing can be visualized in CFD simulation and particle image velocimetry experiments [<xref ref-type="bibr" rid="ref-18">18</xref>]. The &#x201C;glottal jet&#x201D; phenomenon is less noticeable at higher flow rates, and the separation zone is smaller during inhalation. However, the maximum velocity was significantly lower than during inhalation. The flow fields in the trachea region were unaffected by the exhalation breathing modes [<xref ref-type="bibr" rid="ref-7">7</xref>]. The simulation of inhale/exhale breathing also facilitates the visualization and understanding of the particle motion in the human airway. The steady flow replaced the asymmetric cycle simulation for nonstationary flow. The volumetric flow rates were used as the combinations of maximum and average flow rates during inhalation [<xref ref-type="bibr" rid="ref-19">19</xref>]. The CFD simulation during inhalation and exhalation with prescribed wall motion by magnetic resonance imaging provides new insight into the realistic flow behaviors of breathing. The active motion of the airway could produce physiologically realistic results in the CFD simulation [<xref ref-type="bibr" rid="ref-20">20</xref>]. Thus, the CFD simulation is significant in studying the flow pattern visualization of the upper airways.</p>
<p>Therefore, the current study is the continuity research from our previous finding [<xref ref-type="bibr" rid="ref-1">1</xref>], and it is motivated to investigate the turbulent airflow in the pharyngeal airway for a patient diagnosed with OSA, mainly focusing on the inhale and exhale flow condition. The CFD simulation was applied for the task undertaken. The novelty is explained by visualizing the turbulent kinetic energy (TKE) to relate the severity of OSA patients with eddies of the airflow in the pharyngeal airway during inhale and exhale breathing. The CFD result indicates a more reliable but relatively simplified upper airway model to understand OSA. As far as the authors are aware, the literature lacks a study on the effect of TKE on the breathing pattern of OSA patients. Thus, this field has a significant research gap, particularly in simulation modelling analysis. The present study focuses primarily on body characteristics to comprehend the OSA phenomenon, but it does not adequately demonstrate the airflow details that contribute to our understanding of OSA. This study proposes and describes the impact of inhalation and exhalation on OSA patients&#x2019; airways. The findings contribute to the visualization of TKE of the airflow, which is related to the severity of OSA patients with pharyngeal airway eddies. In addition, the examination of the flow pattern breathing contributes to the understanding of TKE airflow characteristics.</p>
</sec>
<sec id="s2">
<label>2</label>
<title>Method to Study the Human Upper Airway</title>
<p>The method used in this work includes CFD modelling and segmentation of computed tomography scan (CT scan) acquisition, which has been described and explained in previous research [<xref ref-type="bibr" rid="ref-1">1</xref>]. Therefore, <xref ref-type="fig" rid="fig-1">Fig. 1</xref> portrays the CFD modelling in which the model was a segmentation of the pharyngeal in the human upper airway. The volume of the model was created based on real patient computed tomography (CT) images. The focus was on both flow simulations. Thus, the marked locations of P6 and P1 are defined as the inlet and outlet boundary conditions for inhaling, but for exhaling, P6 is defined as outlet and P1 as an inlet. The TKE in the upper airway was obtained in the simulation by considering all essential parameters and boundary conditions adopted in previous research.</p>
<fig id="fig-1">
<label>Figure 1</label>
<caption>
<title>Breathing condition for inhaling and exhaling for OSA patient</title>
</caption>
<graphic mimetype="image" mime-subtype="png" xlink:href="CMES_22716-fig-1.png"/>
</fig>
<sec id="s2_1">
<label>2.1</label>
<title>Method to Study the Human Upper Airway</title>
<p>All procedures in this study were conducted in accordance with the Universiti Malaysia Perlis Research Ethics Committee, Perlis, Malaysia-UniMAP/PTNC(P&#x0026;I)/JKETIKA (10/11/2021) approved protocols. Written informed consents were received from all the patients, and the study was conducted according to the tenets of the Declaration of Helsinki for research involving human subjects. The upper airway geometry is extracted from CT scan images of 24-year-old female nonsmoking OSA patient volunteers. The BMI of the patient is 70.3 kg/m<sup>2</sup>, and the AHI is 99.5. The summarized characteristics of the OSA subject that were selected for the conduction of the upper airway CT scan. According to previous works, the focus of the subject of interest was decided to be from the nostril until the pharyngeal [<xref ref-type="bibr" rid="ref-13">13</xref>]. A total of 431 frames with 0.3 mm of slice thickness covering the upper airway CT scan of the subject were performed using an i-CAT Cone Beam 3D Dental Imaging System (version 3.1.62 supplied by Imaging Science International, Hatfield, USA), as shown in <xref ref-type="fig" rid="fig-2">Fig. 2</xref>.</p>
<fig id="fig-2">
<label>Figure 2</label>
<caption>
<title>The airways of OSA patient: (a) coronal view; (b) axial view; (c) sagittal view; and (d) 3D volume pharyngeal airway</title>
</caption>
<graphic mimetype="image" mime-subtype="png" xlink:href="CMES_22716-fig-2.png"/>
</fig>
<p>The airway boundary is identified from the CT scan images via a threshold based on the intensity of the grey image. The thresholding method divides images into sub-images and then determines the threshold value for each portion in order to find different threshold values for various parts of the images. The results of the thresholding are then combined for each component of the image. This technique splits an image into vertical and horizontal parts containing a section of the object&#x2019;s background. Finally, interpolation is required to achieve the desired outcomes [<xref ref-type="bibr" rid="ref-21">21</xref>]. The images were captured while the patient was awake and lying down with their face upward, as explained in the works of Chan&#x00A0;et&#x00A0;al.&#x00A0;[<xref ref-type="bibr" rid="ref-22">22</xref>]. Each CT scan has 534 pixels &#x00D7; 534 pixels, and the pixel spacing is 0.3 mm &#x00D7; 0.3 mm. A series of CT scan images were stored in a Digital Imaging and Communications in Medicine (DICOM) format. Then, the DICOM images were imported into a three-dimensional (3D) medical image processing MIMICS software (version 15.0; Materialise, Leuven, Belgium). The image segmentation of the upper airway was carried out to identify the 3D airway region based on the pixel value (Hounsfield unit) from the DICOM image series. The airway surface model was generated using segment airway in pulmonary function test, as shown in <xref ref-type="fig" rid="fig-2">Fig. 2</xref>. Then, the 3D volume of the pharyngeal airway was created and exported for the 3D model mesh generation.</p>
</sec>
<sec id="s2_2">
<label>2.2</label>
<title>Mesh Generation</title>
<p>The model generated by the MIMICS software was transferred to 3-Matic (version 15.0; Leuven, Belgium) to create the volume mesh. The preprocessor, ICEM (ANSYS, USA), generated unstructured tetrahedral meshes for airway volume. The mesh quality was controlled to ensure the highest level of result accuracy. The surfaces of the pharyngeal airway have meshed with 2.0 mm of Maximum face size. The maximum and minimum size of the mesh is 2 mm and 0.002 mm, respectively. An inflation of the pharyngeal airway mesh was considered around the wall boundary to increase the accuracy of the simulation. This consideration also ensures an excellent fine mesh is created next to the wall, thus providing an adequately small mesh close to the size of the wall mesh. The y&#x002B; (dimensionless distance) approach was used to accurately estimate the initial boundary layer thickness [<xref ref-type="bibr" rid="ref-12">12</xref>] that corresponds to the near-wall cell size (0.272). The quality of the meshed airway model was examined in ANSYS, where the quality of the mesh is measured by the average skewness value and standard deviation. The skewness value is 0.2142, which indicates an excellent cell quality (0&#x2013;0.25), as recommended by ANSYS. Then, the mesh sensitivity grid study was performed on the 3D airway model with different grid scales. The 5-grid size was performed to establish acceptable accuracy, as shown by the previous research approach.</p>
</sec>
<sec id="s2_3">
<label>2.3</label>
<title>Numerical Modelling of the Upper Airway</title>
<p>Inhalation and exhalation breathing involve the airflow passing through the pharyngeal airway. The airflow characteristics may vary due to the uniqueness of the pharyngeal airway. Thus, in the simulation analysis, the flow field in the pharyngeal airway for OSA patients is computed by using a steady-state Reynolds-averaged Navier-Stokes (RANS) formulation, with the k&#x2013;&#x03C9; shear stress transport (SST) turbulence model with low Reynolds number correction [<xref ref-type="bibr" rid="ref-23">23</xref>]. The popular k&#x2013;&#x03C9; SST turbulence model was considered in this work instead of the k&#x2013;&#x03F5; model due to the greater accuracy of the former in viscous near-wall region treatment while considering the effects of adverse pressure gradient [<xref ref-type="bibr" rid="ref-24">24</xref>]. The solver used in the simulation had been validated in our previous studies [<xref ref-type="bibr" rid="ref-1">1</xref>]. The comparison of the simulation and previous experimental results showed a good agreement on the wall static pressure induced by the airflow 1.</p>
<sec id="s2_3_1">
<label>2.3.1</label>
<title>RANS</title>
<p>The fluid governing equations were solved in ANSYS Fluent 16.2 (ANSYS, USA). Considering the UA airflow (0.05) low Mach number during inhalation, the flow was modelled as incompressible and Newtonian. The standard shear stress transport (SST) <inline-formula id="ieqn-1"><mml:math id="mml-ieqn-1"><mml:mrow><mml:mi mathvariant="normal">k</mml:mi></mml:mrow><mml:mrow><mml:mo>&#x2212;</mml:mo></mml:mrow><mml:mi>&#x03C9;</mml:mi></mml:math></inline-formula> model was selected to model the flow turbulence. By comparing with the physical experimental result, our preliminary sensitivity study of applying different turbulence models proved the SST model&#x2019;s appropriateness of the SST &#x006B;&#x2212;&#x03C9; model in solving the complex UA flow has been validated in previous research [<xref ref-type="bibr" rid="ref-1">1</xref>]. It is in agreement with other studies that indicate that the SST <inline-formula id="ieqn-2"><mml:math id="mml-ieqn-2"><mml:mrow><mml:mi mathvariant="normal">k</mml:mi></mml:mrow><mml:mrow><mml:mo>&#x2212;</mml:mo></mml:mrow><mml:mi>&#x03C9;</mml:mi></mml:math></inline-formula> model has advantages in solving complex transional flow [<xref ref-type="bibr" rid="ref-23">23</xref>] including the UA transitional flow [<xref ref-type="bibr" rid="ref-9">9</xref>]. The governing equations for the time-averaged airflow were the listed continuity (<xref ref-type="disp-formula" rid="eqn-1">Eq. (1)</xref>), and the Reynold averaged Navier Stokes (RANS) (<xref ref-type="disp-formula" rid="eqn-2">Eq. (2)</xref>). In this study, the RANS model is utilized to estimate the flow velocity and structure that is both reasonable and accurate. On the other hand, LES or DES models concentrate primarily on intricate geometry. They require a more extended amount of time to run when compared with other models of the same type.</p>
<p><disp-formula id="eqn-1"><label>(1)</label><mml:math id="mml-eqn-1" display="block"><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mover><mml:mi>u</mml:mi><mml:mo stretchy="false">&#x2192;</mml:mo></mml:mover></mml:mrow><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math></disp-formula></p>
<p><disp-formula id="eqn-2"><label>(2)</label><mml:math id="mml-eqn-2" display="block"><mml:mi>&#x03C1;</mml:mi><mml:msub><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>u</mml:mi><mml:mrow><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>x</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>P</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>x</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mfrac><mml:mo>+</mml:mo><mml:mfrac><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>x</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mfrac><mml:mrow><mml:mo>[</mml:mo><mml:mi>&#x03BC;</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>x</mml:mi><mml:mrow><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mfrac><mml:mo>+</mml:mo><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>u</mml:mi><mml:mrow><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>x</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mfrac><mml:mo>)</mml:mo></mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mi>&#x03C1;</mml:mi><mml:mover><mml:mrow><mml:msubsup><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2032;</mml:mi></mml:mrow></mml:msubsup><mml:msubsup><mml:mi>u</mml:mi><mml:mrow><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2032;</mml:mi></mml:mrow></mml:msubsup></mml:mrow><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mo>]</mml:mo></mml:mrow></mml:math></disp-formula>where <inline-formula id="ieqn-3"><mml:math id="mml-ieqn-3"><mml:mi>u</mml:mi></mml:math></inline-formula> is the velocity, <inline-formula id="ieqn-4"><mml:math id="mml-ieqn-4"><mml:mi>i</mml:mi></mml:math></inline-formula> and <inline-formula id="ieqn-5"><mml:math id="mml-ieqn-5"><mml:mi>j</mml:mi></mml:math></inline-formula> represent the Cartesian coordinates. For the advection scheme, a second-order upwind discretization scheme was chosen. The results were considered as converged when the residual level dropped to the defined residual target of <inline-formula id="ieqn-6"><mml:math id="mml-ieqn-6"><mml:mn>1</mml:mn><mml:mo>&#x00D7;</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mn>6</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>.</p>
</sec>
<sec id="s2_3_2">
<label>2.3.2</label>
<title>Turbulent Kinetic Energy (TKE) Equation</title>
<p>The TKE equation is developed from the mass and momentum conservation equations to describe how the mean flow feeds kinetic energy into turbulence, given its essential role in developing the turbulent model in CFD modelling. The Reynolds decomposition method was used to decompose the velocity signal, <inline-formula id="ieqn-7"><mml:math id="mml-ieqn-7"><mml:msub><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>, into mean <inline-formula id="ieqn-8"><mml:math id="mml-ieqn-8"><mml:mover><mml:mi>u</mml:mi><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover></mml:math></inline-formula> and fluctuation component, <inline-formula id="ieqn-9"><mml:math id="mml-ieqn-9"><mml:msup><mml:mi>u</mml:mi><mml:mrow><mml:mi mathvariant="normal">&#x2032;</mml:mi></mml:mrow></mml:msup></mml:math></inline-formula>. Therefore, the amount of turbulent fluctuation is described by the root-mean-square of the difference of instantaneous velocity and mean velocity [<xref ref-type="bibr" rid="ref-25">25</xref>], as represented in <xref ref-type="disp-formula" rid="eqn-3">Eq. (3)</xref>.</p>
<p><disp-formula id="eqn-3"><label>(3)</label><mml:math id="mml-eqn-3" display="block"><mml:msup><mml:mi>u</mml:mi><mml:mi mathvariant="normal">&#x2032;</mml:mi></mml:msup><mml:mo>=</mml:mo><mml:msqrt><mml:mfrac><mml:mn>1</mml:mn><mml:msub><mml:mi>N</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub></mml:mfrac><mml:munderover><mml:mo>&#x2211;</mml:mo><mml:mrow><mml:mi>i</mml:mi><mml:mo>=</mml:mo><mml:mn>1</mml:mn></mml:mrow><mml:mrow><mml:mi>N</mml:mi></mml:mrow></mml:munderover><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub><mml:mo>&#x2212;</mml:mo><mml:mover><mml:mi>u</mml:mi><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:msqrt></mml:math></disp-formula>where <inline-formula id="ieqn-10"><mml:math id="mml-ieqn-10"><mml:mi>N</mml:mi></mml:math></inline-formula> is the number of samples in the signal included in the ANSYS simulation. The equation of fluctuation component is also applicable for the velocity signal, <inline-formula id="ieqn-11"><mml:math id="mml-ieqn-11"><mml:mi>v</mml:mi></mml:math></inline-formula> and <inline-formula id="ieqn-12"><mml:math id="mml-ieqn-12"><mml:mi>w</mml:mi></mml:math></inline-formula>. For compressible flow, it is convenient to use Favre averaging. From the continuity and momentum equation, it is possible to deduced a transport equation for turbulent kinetic energy per unit mass, <inline-formula id="ieqn-13"><mml:math id="mml-ieqn-13"><mml:mi>k</mml:mi><mml:mo>=</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mn>1</mml:mn><mml:mn>2</mml:mn></mml:mfrac></mml:mstyle><mml:mrow><mml:mover><mml:mrow><mml:msubsup><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2032;</mml:mi></mml:mrow></mml:msubsup><mml:msubsup><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2032;</mml:mi></mml:mrow></mml:msubsup></mml:mrow><mml:mo>&#x007E;</mml:mo></mml:mover></mml:mrow><mml:mo>,</mml:mo></mml:math></inline-formula></p>
<p><disp-formula id="eqn-4"><label>(4)</label><mml:math id="mml-eqn-4" display="block"><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mover><mml:mi>&#x03C1;</mml:mi><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mi>k</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>t</mml:mi></mml:mrow></mml:mfrac><mml:mo>+</mml:mo><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mover><mml:mi>&#x03C1;</mml:mi><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mspace width="thinmathspace" /><mml:mover><mml:msub><mml:mi>u</mml:mi><mml:mrow><mml:mi>j</mml:mi></mml:mrow></mml:msub><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>x</mml:mi><mml:mrow><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mover><mml:mi>&#x03C1;</mml:mi><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mrow><mml:mover><mml:mrow><mml:msubsup><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2032;</mml:mi></mml:mrow></mml:msubsup><mml:msubsup><mml:mi>u</mml:mi><mml:mrow><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2032;</mml:mi></mml:mrow></mml:msubsup></mml:mrow><mml:mo>&#x007E;</mml:mo></mml:mover></mml:mrow><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mover><mml:msub><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>x</mml:mi><mml:mrow><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mfrac><mml:mo>&#x2212;</mml:mo><mml:mover><mml:mrow><mml:msub><mml:mi>&#x03C4;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msubsup><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2032;</mml:mi></mml:mrow></mml:msubsup></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>x</mml:mi><mml:mrow><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mfrac></mml:mrow><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mo>+</mml:mo><mml:mover><mml:mrow><mml:msup><mml:mi>P</mml:mi><mml:mi mathvariant="normal">&#x2032;</mml:mi></mml:msup><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msubsup><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2032;</mml:mi></mml:mrow></mml:msubsup></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>x</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mfrac></mml:mrow><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mo>+</mml:mo><mml:mover><mml:msubsup><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2032;</mml:mi></mml:mrow></mml:msubsup><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mover><mml:mi>p</mml:mi><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>x</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mfrac><mml:mo>+</mml:mo><mml:mfrac><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>x</mml:mi><mml:mrow><mml:mi>k</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mfrac><mml:mrow><mml:mo>[</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:mn>2</mml:mn></mml:mfrac><mml:mover><mml:mrow><mml:mi>&#x03C1;</mml:mi><mml:msubsup><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2032;</mml:mi></mml:mrow></mml:msubsup><mml:msubsup><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2032;</mml:mi></mml:mrow></mml:msubsup><mml:msubsup><mml:mi>u</mml:mi><mml:mrow><mml:mi>k</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2032;</mml:mi></mml:mrow></mml:msubsup></mml:mrow><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mo>+</mml:mo><mml:mover><mml:mrow><mml:msubsup><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2032;</mml:mi></mml:mrow></mml:msubsup><mml:msub><mml:mi>&#x03C4;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>k</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mo>&#x2212;</mml:mo><mml:mover><mml:mrow><mml:msup><mml:mi>p</mml:mi><mml:mrow><mml:mi mathvariant="normal">&#x2032;</mml:mi></mml:mrow></mml:msup><mml:msubsup><mml:mi>u</mml:mi><mml:mrow><mml:mi>k</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2032;</mml:mi></mml:mrow></mml:msubsup></mml:mrow><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mo>]</mml:mo></mml:mrow></mml:math></disp-formula></p>
<p>Using this equation, the velocity fluctuation used in calculating the TKE around the upper airway may be useful in identifying the severity of blockage to breathing in the upper airway.</p>
</sec>
<sec id="s2_3_3">
<label>2.3.3</label>
<title>Reynolds Number</title>
<p>Previous researcher explained the flow mechanism in the upper airways, and two Reynolds numbers were used in this study. In terms of definitions, there is a significant difference between Turbulent Reynolds number, Re<sub>y</sub> and Reynolds number, Re. The Turbulent Reynolds number is the ratio between the kinetic energy and work of friction. However, the Reynolds number is the ratio between the inertia force and viscosity force.</p>
<p>The definition of Turbulent Reynolds Number, <inline-formula id="ieqn-14"><mml:math id="mml-ieqn-14"><mml:mi>R</mml:mi><mml:msub><mml:mi>e</mml:mi><mml:mrow><mml:mi>y</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> [<xref ref-type="bibr" rid="ref-25">25</xref>] is shown in <xref ref-type="disp-formula" rid="eqn-5">Eq. (5)</xref>:</p>
<p><disp-formula id="eqn-5"><label>(5)</label><mml:math id="mml-eqn-5" display="block"><mml:mi>R</mml:mi><mml:msub><mml:mi>e</mml:mi><mml:mrow><mml:mi>y</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mrow><mml:mrow><mml:mi mathvariant="italic">K</mml:mi><mml:mi mathvariant="italic">i</mml:mi><mml:mi mathvariant="italic">n</mml:mi><mml:mi mathvariant="italic">e</mml:mi><mml:mi mathvariant="italic">c</mml:mi><mml:mi mathvariant="italic">t</mml:mi><mml:mi mathvariant="italic">i</mml:mi><mml:mi mathvariant="italic">c</mml:mi></mml:mrow><mml:mrow><mml:mi>&#x00A0;</mml:mi><mml:mi mathvariant="italic">E</mml:mi><mml:mi mathvariant="italic">n</mml:mi><mml:mi mathvariant="italic">e</mml:mi><mml:mi mathvariant="italic">r</mml:mi><mml:mi mathvariant="italic">g</mml:mi><mml:mi mathvariant="italic">y</mml:mi></mml:mrow></mml:mrow><mml:mrow><mml:mi>W</mml:mi><mml:mi>o</mml:mi><mml:mi>r</mml:mi><mml:mi>k</mml:mi><mml:mi>&#x00A0;</mml:mi><mml:mi>o</mml:mi><mml:mi>f</mml:mi><mml:mi>&#x00A0;</mml:mi><mml:mrow><mml:mi mathvariant="italic">f</mml:mi><mml:mi mathvariant="italic">r</mml:mi><mml:mi mathvariant="italic">i</mml:mi><mml:mi mathvariant="italic">c</mml:mi><mml:mi mathvariant="italic">t</mml:mi><mml:mi mathvariant="italic">i</mml:mi><mml:mi mathvariant="italic">o</mml:mi><mml:mi mathvariant="italic">n</mml:mi></mml:mrow></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mi>K</mml:mi><mml:mi>E</mml:mi></mml:mrow><mml:mi>W</mml:mi></mml:mfrac></mml:math></disp-formula></p>
<p>The definition of Reynolds Number, <inline-formula id="ieqn-15"><mml:math id="mml-ieqn-15"><mml:mi>R</mml:mi><mml:mi>e</mml:mi></mml:math></inline-formula> is as shown in <xref ref-type="disp-formula" rid="eqn-6">Eq. (6)</xref>:</p>
<p><disp-formula id="eqn-6"><label>(6)</label><mml:math id="mml-eqn-6" display="block"><mml:mi>R</mml:mi><mml:mi>e</mml:mi><mml:mo>=</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mrow><mml:mrow><mml:mi mathvariant="italic">I</mml:mi><mml:mi mathvariant="italic">n</mml:mi><mml:mi mathvariant="italic">e</mml:mi><mml:mi mathvariant="italic">r</mml:mi><mml:mi mathvariant="italic">t</mml:mi><mml:mi mathvariant="italic">i</mml:mi><mml:mi mathvariant="italic">a</mml:mi><mml:mi>&#x00A0;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="italic">F</mml:mi><mml:mi mathvariant="italic">o</mml:mi><mml:mi mathvariant="italic">r</mml:mi><mml:mi mathvariant="italic">c</mml:mi><mml:mi mathvariant="italic">e</mml:mi></mml:mrow></mml:mrow><mml:mrow><mml:mrow><mml:mi mathvariant="italic">V</mml:mi><mml:mi mathvariant="italic">i</mml:mi><mml:mi mathvariant="italic">s</mml:mi><mml:mi mathvariant="italic">c</mml:mi><mml:mi mathvariant="italic">o</mml:mi><mml:mi>&#x00A0;</mml:mi><mml:mi mathvariant="italic">s</mml:mi><mml:mi mathvariant="italic">i</mml:mi><mml:mi mathvariant="italic">t</mml:mi><mml:mi mathvariant="italic">y</mml:mi><mml:mi>&#x00A0;</mml:mi></mml:mrow><mml:mi>o</mml:mi><mml:mi>f</mml:mi><mml:mrow><mml:mi mathvariant="italic">f</mml:mi><mml:mi mathvariant="italic">r</mml:mi><mml:mi mathvariant="italic">i</mml:mi><mml:mi mathvariant="italic">c</mml:mi><mml:mi mathvariant="italic">t</mml:mi><mml:mi mathvariant="italic">i</mml:mi><mml:mi mathvariant="italic">o</mml:mi><mml:mi mathvariant="italic">n</mml:mi></mml:mrow></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mi>&#x03C1;</mml:mi><mml:mi>D</mml:mi><mml:mover><mml:mi>u</mml:mi><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover></mml:mrow><mml:mi>&#x03BC;</mml:mi></mml:mfrac></mml:math></disp-formula>where <inline-formula id="ieqn-16"><mml:math id="mml-ieqn-16"><mml:mi>&#x03C1;</mml:mi></mml:math></inline-formula> is the density of air, <inline-formula id="ieqn-17"><mml:math id="mml-ieqn-17"><mml:mi>D</mml:mi></mml:math></inline-formula> is the diameter of the cross-sectional, <inline-formula id="ieqn-18"><mml:math id="mml-ieqn-18"><mml:mover><mml:mi>u</mml:mi><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover></mml:math></inline-formula> is the mean velocity and <inline-formula id="ieqn-19"><mml:math id="mml-ieqn-19"><mml:mi>&#x03BC;</mml:mi></mml:math></inline-formula> is the dynamic viscosity.</p>
</sec>
<sec id="s2_3_4">
<label>2.3.4</label>
<title>Boundary Conditions</title>
<p>The boundary conditions of the 3D model were defined via the surface of the model, as mentioned in <xref ref-type="fig" rid="fig-1">Fig. 1</xref>. The inlet and outlet boundary conditions in the simulation were referred from the works of Mihaesu&#x00A0;et&#x00A0;al.&#x00A0;[<xref ref-type="bibr" rid="ref-9">9</xref>]. The steady-state turbulent airway flow is computed by ANSYS Fluent, which solves finite volume using fitted grids. During breathing, the velocity profile was assumed to be uniform, and the axial component of the velocity was perpendicular to the flow inlet, the nasopharynx [<xref ref-type="bibr" rid="ref-12">12</xref>]. Light breathing was considered at the inlet for both breathing conditions, where a volume flow rate of 7.5&#x00A0;L/min was considered in the simulation [<xref ref-type="bibr" rid="ref-26">26</xref>]. A turbulent intensity of 10% was considered to mimic the real condition, where the outlet was defined by an average gauge pressure of 0 Pa [<xref ref-type="bibr" rid="ref-27">27</xref>].</p>
</sec>
<sec id="s2_3_5">
<label>2.3.5</label>
<title>Limitation of the Study</title>
<p>Some of the limitations of this study include the limited extent of the airway understudy, the fact that the velocity of breathing is considered uniform, patients were awake and in an upright posture during the scans, the absence of a sleep study, the lack of sleepiness scales or questionnaires, the unknown stage of respiration, and the lack of tongue control. In addition, the airway is not a rigid structure, and the effects of the soft tissue placidness could not be taken into consideration. Besides, the biomechanical model&#x0027;s design and analysis are excluded in the current study.</p>
</sec>
</sec>
</sec>
<sec id="s3">
<label>3</label>
<title>Results and Discussion</title>
<p>The CFD simulation result of the airway analysis is significant and valuable to a medical practitioner because it provides a clear airflow visualization. The current airway analysis assessment focuses on various aspects, such as the cross-sectional area, airflow patterns, velocity, pressure, wall shear stress, turbulent kinetic energy, and turbulent Reynolds number. <xref ref-type="fig" rid="fig-3">Fig. 3</xref> shows the variation of airway cross-sectional area in thirty-four-plane images, with the location of the cross-sectional plane in the z-direction (i.e., flow direction). This indicates that the patient has a minimum cross-sectional area of 7.68 mm<sup>2</sup> at 28 mm from the inlet.</p>
<fig id="fig-3">
<label>Figure 3</label>
<caption>
<title>Cross-sectional area along the flow direction of the airway model generated through CT Scan data that refers to a region with obstructions</title>
</caption>
<graphic mimetype="image" mime-subtype="png" xlink:href="CMES_22716-fig-3.png"/>
</fig>
<sec id="s3_1">
<label>3.1</label>
<title>Cross-Sectional Area</title>
<p>The minimum area is crucial for patients with sleep apnea. Contraction of the cross-sectional area influences the smoothness of the airflow when passing through the upper airway. This situation is also defined as the obstruction of airflow during inhalation. The narrow airway area in a patient with OSA might have been caused by the collapse or laxity of airway tissue. Most researchers, such as Lantz&#x00A0;et&#x00A0;al.&#x00A0;[<xref ref-type="bibr" rid="ref-28">28</xref>], Chouly&#x00A0;et&#x00A0;al.&#x00A0;[<xref ref-type="bibr" rid="ref-29">29</xref>], and Djukic&#x00A0;et&#x00A0;al.&#x00A0;[<xref ref-type="bibr" rid="ref-30">30</xref>], have discussed and employed the flow values (i.e., velocity, pressure, and wall shear stress) to describe the characteristics of the upper airway. In this work, the additional flow parameter, TKE, is considered to describe the characteristics of the upper airway. Other flow parameters were also considered to visualize the phenomena and flow patterns in the upper airway.</p>
</sec>
<sec id="s3_2">
<label>3.2</label>
<title>Flow Pattern in Pharyngeal Airway</title>
<p><xref ref-type="fig" rid="fig-4">Fig. 4a</xref> depicts the axial velocity contour (m/s) and streamlines along the upper airway&#x0027;s midsagittal plane in the nasopharynx, oropharynx, and hypopharynx. The results show that the highest velocity began after the airflow at the oropharynx. As the airflow approached the minimum cross-sectional area of the airway (retropalatal pharynx), the velocity increased, and the airflow seemed to have developed a turbulent flow pattern that also generated the flow recirculation regions (negative axial velocity), as shown in <xref ref-type="fig" rid="fig-4">Fig. 4b</xref>. The dilation of the cross-sectional area after the narrow area had affected the airflow in the OSA patient&#x0027;s airway. Thus, the flow recirculation is concentrated around this region, typically formed downstream with obstructions (narrow area). The existence of negative axial velocity may lead to the vibration of airway tissue due to continuous breathing. Hence, it is highly likely that this region will generate vibration, causing the snoring. Snoring is known to reduce the strength of the tissue in patients with sleep apnea [<xref ref-type="bibr" rid="ref-31">31</xref>].</p>
<fig id="fig-4">
<label>Figure 4</label>
<caption>
<title>Velocity magnitude in the pharyngeal airway: (a) velocity contour at centre plane; and (b) streamline velocity along the centre plane</title>
</caption>
<graphic mimetype="image" mime-subtype="png" xlink:href="CMES_22716-fig-4.png"/>
</fig>
<p><xref ref-type="fig" rid="fig-4">Fig. 4b</xref> exhibits the recirculation region phenomenon caused by a narrow breathing area. Narrowed breathing area gives the exact definition of hypopnea in calculating the degree of blockage of breathing airway during sleep. By understanding the recirculation region, a new tool may be introduced in calculating the degree of blockage from the simulation of the upper airway without requiring the patient to sleep all night. <xref ref-type="fig" rid="fig-5">Fig. 5</xref> shows the maximum velocity and area distribution around the upper airway&#x2019;s maximum narrowing. The maximum velocity in maximum narrowing is also known as &#x201C;pharyngeal jet&#x201D;, whereby it creates a compact region and induces recirculation flow. The average velocity also indicates the maximum velocity around the narrow region. In this situation, the high-velocity airflow had induced a high fluctuation that contributes to the vortices in a turbulent flow. Thus, the TKE, as explained in <xref ref-type="disp-formula" rid="eqn-4">Eq. (4)</xref>, is used to describe the mean kinetic energy per unit mass of vortices after the maximum narrowing in the upper airway is reached.</p>
<fig id="fig-5">
<label>Figure 5</label>
<caption>
<title>Maximum velocity and area distribution in pharyngeal airway</title>
</caption>
<graphic mimetype="image" mime-subtype="png" xlink:href="CMES_22716-fig-5.png"/>
</fig>
<p>The correlation between velocity and the area of the upper airway was investigated in this study. The region of interest (ROI) was focused on positions ranging from 0.01 to 0.028 m and 0.03 to 0.04 m. The airflow velocity passing from 0.01 to 0.028 experienced the convergence of the cross-sectional area of the upper airway. In contrast, after position 0.028 m, the cross-sectional area of the upper airway is increased; this can be observed in <xref ref-type="fig" rid="fig-5">Fig. 5</xref>. <xref ref-type="fig" rid="fig-6">Fig. 6</xref> shows the correlation between airflow velocity and area. The simulation results revealed that the airflow velocity decreased with the increasing area under the fitting of the power function at positions from 0.01 to 0.028 m. The coefficient of determination (R<sup>2</sup>) is 0.9981 and indicates the excellent data fit in the regression model. However, the correlation between velocity and area is in the polynomial behavior after the airflow passes through the narrow area. The R<sup>2</sup> is 0.9854, demonstrating the excellent data fitting of the polynomial function to describe the relationship between velocity and area (positions 0.03 to 0.04 m). The change in the correlation between velocity and airflow was attributed to the airflow characteristic after passing through the narrow area, as aforementioned in <xref ref-type="fig" rid="fig-4">Figs. 4</xref> and <xref ref-type="fig" rid="fig-5">5</xref>.</p>
<fig id="fig-6">
<label>Figure 6</label>
<caption>
<title>Statistical analysis between velocity and area for the range of position 0.01 to 0.028 and 0.03 to 0.04</title>
</caption>
<graphic mimetype="image" mime-subtype="png" xlink:href="CMES_22716-fig-6.png"/>
</fig>
</sec>
<sec id="s3_3">
<label>3.3</label>
<title>Pressure Distribution Profile</title>
<p>The airway wall or tissue experiences the variation of pressure when airflow passes through the airway. Pressure variation may lead to the vibration of airway tissue. <xref ref-type="fig" rid="fig-7">Figs. 7a</xref> and <xref ref-type="fig" rid="fig-7">7b</xref> illustrate the pressure on the airway wall (unit: Pa) during the inspiration and expiration breathing phase, respectively. It is observed that the inhale and exhale breathing have the low-pressure region around the narrow area. This observation corresponded to the large velocity around the narrow area. Higher velocity gives the higher pressure drop.</p>
<fig id="fig-7">
<label>Figure 7</label>
<caption>
<title>Contour of upper airway total pressure on the airway wall during (a) inhale and (b) exhale</title>
</caption>
<graphic mimetype="image" mime-subtype="png" xlink:href="CMES_22716-fig-7.png"/>
</fig>
<p>The TKE value will be high if the velocity fluctuation is in a randomized direction, with high magnitude impacting the blockage in the breathing area, as visualized in <xref ref-type="fig" rid="fig-4">Fig. 4</xref>; there is low pressure at the narrow cross-sectional breathing area the exhale. The high wall shear stress is mainly observed in the obstructed regions, contributing to high turbulent energy near the wall [<xref ref-type="bibr" rid="ref-24">24</xref>]. In a recent study, Gupta&#x00A0;et&#x00A0;al.&#x00A0;[<xref ref-type="bibr" rid="ref-32">32</xref>] found that shear stress generates fluctuating velocity and produces TKE in this region. The fluctuating velocity and turbulent flow near the wall will induce vibration and simultaneously generate snoring. As such, the severity of snoring directly corresponds to the TKE. The occurrence of snoring in the long term would cause reduced tissue strength for the pharyngeal, which will lead to the laxity or collapse of tissue due to gravitational effects when the patient sleeps in a lying down position. Consequently, this makes it a contributing factor to sleep apnea. Besides, the velocity gradient affects the wall shear stress. The changes in velocity around the obstructed regions indicated the higher wall shear stress in those regions. The upper airway walls&#x2019; exposure to high wall shear stress may play a significant role in the respiratory disease&#x0027;s inflammatory process [<xref ref-type="bibr" rid="ref-33">33</xref>,<xref ref-type="bibr" rid="ref-34">34</xref>].</p>
</sec>
<sec id="s3_4">
<label>3.4</label>
<title>Turbulent Reynolds Number</title>
<p>The turbulent Reynolds number and Reynolds number were considered in this work to describe the airflow characteristics of the airway of an OSA patient. The severe vibration of airway tissue leads to snoring, where long-term snoring weakens the airway tissue, thus leading to the blockage of airflow (i.e., sleep hypopnea and apnea). Previous researchers often employ the Reynolds number to express the flow condition in the study of the airway. The subject mainly breathed in a turbulent region expressed in the Reynolds number shown in <xref ref-type="fig" rid="fig-8">Fig. 8</xref>. The flow develops a turbulent region at 0.014 m from the inlet with the Reynolds number 4096. The flow reaches a peak at 0.04 m from the inlet with the value of the Reynolds Number 7534, but for the healthy person in normal breathing, the Reynolds number is estimated around 2084. High turbulent Reynolds number was identified around a region after the narrow area. Both Reynolds (Re) and turbulent Reynolds (Re<sub>y</sub>) were concentrated in a similar region. The results indicate that Re corresponded to the Re<sub>y</sub>. This situation can be observed at the first peak of the plot (at the position &#x007E;0.04 m) for Re and Re<sub>y</sub> in <xref ref-type="fig" rid="fig-8">Fig. 8</xref>, respectively. The Re<sub>y</sub> is helpful for the identification of the turbulence level of airflow in an airway.</p>
<fig id="fig-8"><label>Figure 8</label><caption><title>Turbulent Reynolds number, Re<sub>y</sub>, and Reynolds number along the upper airway during inhaling under light breathing conditions</title></caption><graphic mimetype="image" mime-subtype="png" xlink:href="CMES_22716-fig-8.png"/></fig>
<p>Turbulent Reynolds number was considered to explain the intensity of turbulence or energy of the Reynolds number, as expressed in <xref ref-type="disp-formula" rid="eqn-6">Eq. (6)</xref>. The turbulent Reynolds number reflects the level of turbulence in each area (cross-sectional area of the airway). The high-velocity intensity in the upper airway indicates high turbulence generated from friction work, as expressed in <xref ref-type="disp-formula" rid="eqn-6">Eq. (6)</xref>. High-velocity intensity is generated from the critical cross-sectional area, while the recirculation region (<xref ref-type="fig" rid="fig-4">Fig. 4</xref>) is attributable to the mechanism of hypopnea in clinical areas. High turbulent Reynold number contour is observed around inhale and exhale breathing outlets after the narrow-area (<xref ref-type="fig" rid="fig-9">Fig. 9</xref>). The high turbulent Reynolds number is higher during exhale breathing (<xref ref-type="fig" rid="fig-9">Fig. 9</xref>) than inhale breathing around that narrow area. This situation may lead to the high tendency of sound-producing in exhaling breathing. The explanation of the turbulent Reynolds number will provide a new tool in establishing the severity of the OSA through the consideration of AHI as the evaluation method.</p>
<fig id="fig-9"><label>Figure 9</label><caption><title>Contour of turbulent Reynolds number, Re<sub>y</sub>, in the upper airway at the center plane for (a) inhale and (b) exhale breathing</title></caption><graphic mimetype="image" mime-subtype="png" xlink:href="CMES_22716-fig-9.png"/></fig>
</sec>
<sec id="s3_5">
<label>3.5</label>
<title>Turbulent Kinetic Energy (TKE) Distribution along the Pharyngeal Airway</title>
<p>The turbulent kinetic energy is associated with the kinetic energy of vortices (velocity fluctuation) generated in the turbulent flow, which quantifies the turbulence level in the airway. In the clinical study, the index to measure the severity of OSA is the apnea-hypopnea index called AHI, a diagnosis of the periodic breathing of a patient during sleep. Hypopnea is when the patient undergoes shallow breathing due to a constricted airway. The constricted airway will induce the intensity of the flow, causing high turbulent flow that creates velocity fluctuation, as shown in <xref ref-type="fig" rid="fig-10">Fig. 10</xref>. The fluctuation of velocity (<xref ref-type="disp-formula" rid="eqn-3">Eq. (3)</xref>) and TKE (<xref ref-type="disp-formula" rid="eqn-4">Eq. (4)</xref>) are related to hypopnea, which causes shallow breathing during sleep in measure of the AHI and TKE in CFD simulation.</p>
<fig id="fig-10">
<label>Figure 10</label>
<caption>
<title>Contour of turbulent kinetic energy (TKE) in the upper airway at the centre plane (a) inhale and (b) exhale breathing condition</title>
</caption>
<graphic mimetype="image" mime-subtype="png" xlink:href="CMES_22716-fig-10.png"/>
</fig>
<p>The CFD analysis computes TKE, and turbulent Reynolds number Re<sub>y</sub>. <xref ref-type="fig" rid="fig-8">Figs. 8</xref> and <xref ref-type="fig" rid="fig-10">10</xref> show the distribution of TKE obtained from the velocity fluctuation, as shown in <xref ref-type="disp-formula" rid="eqn-4">Eq. (4)</xref>; whereas the turbulent Reynolds number was computed from <xref ref-type="disp-formula" rid="eqn-6">Eq. (6)</xref>, following the works by Calmet&#x00A0;et&#x00A0;al.&#x00A0;[<xref ref-type="bibr" rid="ref-7">7</xref>]. The airflow motion in the airway is predominantly by the energy in turbulent flow; therefore, the application of TKE is deemed suitable to describe the vortex and quantify the turbulence level. The results show high turbulent kinetic energy concentrated after the narrow region. In addition, the formation of a jet stream was observed in the pharynx of the airway. The jet stream formed had hit the wall in the inhalation area, which may have caused velocity remodeling near the airway wall. <xref ref-type="fig" rid="fig-10">Fig. 10</xref> portrays the occurrence of TKE at high-velocity fluctuation induced by the recirculation phenomenon. TKE value helps provide new information on airflow characteristics. TKE can be used as a new parameter to characterize, as well as in the detection of the patient with OSA. Turbulent flow is generated when the airflow passes through the critical sectional area (<xref ref-type="fig" rid="fig-3">Fig. 3</xref>) in the patient&#x0027;s upper airway. The severity of the turbulence can be explained more impressively and accurately by visualizing the TKE parameter (maximum TKE 77.19, in <xref ref-type="fig" rid="fig-10">Fig. 10</xref>), which is similar to the clinical parameter, AHI of the patient (99.5). The TKE and AHI parameters are related to the OSA phenomenon, which will be helpful in the measurement of the severity of OSA.</p>
<p>The advent of high-resolution three-dimensional TKE able to be constructed from a synthesis of standard two-dimensional cross-sectional images, and of &#x201C;Volume Render Mode,&#x201D; a technique to analyze information inside a three-dimensional volume by digitally enhancing individual flow, promises to revolutionize the diagnosis of obstructive sleep apnea in patients, and the level severity of AHI. Using the different post-processing display parameters, the volume-rendered image provides better visualization performance when there are no significant differences in the signal levels of the conventional approach, as shown in <xref ref-type="fig" rid="fig-11">Fig. 11</xref>. In <xref ref-type="fig" rid="fig-11">Fig. 11</xref>, the TKE occurs after the critical area for both breathing conditions, either inspiration or expiration.</p>
<fig id="fig-11">
<label>Figure 11</label>
<caption>
<title>Volume Rendering of turbulent kinetic energy (TKE) for (a) inhale and (b) exhale breathing conditions</title>
</caption>
<graphic mimetype="image" mime-subtype="png" xlink:href="CMES_22716-fig-11.png"/>
</fig>
</sec>
<sec id="s3_6">
<label>3.6</label>
<title>Body Force Acting on the Upper Airways</title>
<p>The biomechanical aspect during the inhale and exhale breathing is focused on the body forces exerted on the upper airway. During breathing, the deterioration of the airflow pattern creates pressure variation, velocity, and TKE in the upper airway. as shown in <xref ref-type="fig" rid="fig-4">Figs. 4</xref>, <xref ref-type="fig" rid="fig-7">7</xref>, <xref ref-type="fig" rid="fig-9">9</xref>, and <xref ref-type="fig" rid="fig-11">11</xref>. The pressure variation leads to the variation of body forces acting on the upper airway. The forces acting on the upper airways during inhale and exhale breathing are depicted in <xref ref-type="fig" rid="fig-12">Fig. 12</xref>. The simulation results (<xref ref-type="fig" rid="fig-12">Fig. 12</xref>) demonstrated that the forces exerted on the upper airway during inhaling are greater than exhaling. The forces are concentrated on the upper airway after the narrow region. This phenomenon also corresponded to the high turbulent kinetic energy (TKE) found in <xref ref-type="fig" rid="fig-10">Fig. 10</xref> (in <xref ref-type="sec" rid="s3_5">Section 3.5</xref>), indicating that the high TKE could increase body forces. The pressure variation, velocity, and TKE corresponded with the biomechanical aspect of the upper airway. The phenomenon is synchronous with the findings in the previous work [<xref ref-type="bibr" rid="ref-35">35</xref>]. The width of the pharyngeal airway [<xref ref-type="bibr" rid="ref-35">35</xref>] crucially influenced the vortex formation, aerodynamic pressure, and pharyngeal wall force.</p>
<fig id="fig-12">
<label>Figure 12</label>
<caption>
<title>Body forces acting on the upper airways during inhale (left) and exhale (right) breathing condition</title>
</caption>
<graphic mimetype="image" mime-subtype="png" xlink:href="CMES_22716-fig-12.png"/>
</fig>
</sec>
</sec>
<sec id="s4">
<label>4</label>
<title>Conclusion</title>
<p>In this study, the computational analysis in analyzing the airflow characteristics in the upper airway has been investigated. Based on the results of this investigation, the following conclusions can be made:
<list list-type="bullet">
<list-item>
<p>By comprehending the recirculation region and turbulent kinetic energy (TKE), a new tool could be developed to calculate the severity of obstruction in the simulation of the upper airway without requiring the patient to sleep all night in order to measure the obstruction in their breathing airway.</p></list-item>
<list-item>
<p>The presence of turbulent flow may result in the vibration of the airway tissue, thereby reducing the tissue&#x0027;s strength over time; this causes laxity or collapse of tissue, which obstructs airflow.</p></list-item>
<list-item>
<p>The current simulation results are expected to visualize the airflow characteristics during inhale and exhale breathing, thereby improving the understanding for medical practitioners in the OSA research field.</p></list-item>
</list></p>
<p>This work can be expanded for future recommendations by considering other aspects of the research scope, such as the growing number of case studies, fluid-structure interaction, expiratory breathing, and airway tissue vibration.</p>
</sec>
</body>
<back>
<glossary content-type="abbreviations" id="glossary-1">
<label>Nomenclature</label>
<title>List of symbols</title>
<def-list>
<def-item>
<term><italic>D</italic></term>
<def>
<p>Diameter of the cross-sectional </p>
</def>
<def>
<p>m</p>
</def>
</def-item>
<def-item>
<term><italic>KE</italic></term>
<def>
<p>Kinetic energy</p></def>
<def><p>-</p>
</def>
</def-item>
<def-item>
<term><italic>N</italic></term>
<def>
<p>Number of samples in the signal</p></def>
<def><p>-</p>
</def>
</def-item>
<def-item>
<term><italic>p</italic></term>
<def>
<p>Pressure</p></def>
<def><p>Pa</p>
</def>
</def-item>
<def-item>
<term><italic>Re</italic></term>
<def>
<p>Reynolds Number</p></def> <def><p>-</p>
</def>
</def-item>
<def-item>
<term><italic>Re</italic><sub><italic>y</italic></sub></term>
<def>
<p>Turbulent Reynolds Number</p></def>
<def><p>-</p>
</def>
</def-item>
<def-item>
<term><italic>W</italic></term>
<def>
<p>Work of friction</p></def>
<def><p>-</p>
</def>
</def-item>
<def-item>
<term><italic>t</italic></term>
<def>
<p>Time</p></def> <def><p>s</p>
</def>
</def-item>
<def-item>
<term><inline-formula id="ieqn-20"><mml:math id="mml-ieqn-20"><mml:mover><mml:mi>u</mml:mi><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover></mml:math></inline-formula></term>
<def>
<p>mean velocity</p></def> <def><p>m/s</p>
</def>
</def-item>
<def-item>
<term><italic>u</italic></term>
<def>
<p>Fluid velocity component in x-direction</p></def> <def><p>m/s</p>
</def>
</def-item>
<def-item>
<term><italic>v</italic></term>
<def>
<p>Fluid velocity component in y-direction</p></def> <def><p>m/s</p>
</def>
</def-item>
<def-item>
<term><italic>w</italic></term>
<def>
<p>Fluid velocity component in z-direction</p></def> <def><p>m/s</p>
</def>
</def-item>
<def-item>
<term><italic>x, y, z</italic></term>
<def>
<p>Cartesian coordinates</p></def> <def><p>-</p>
</def>
</def-item>
<def-item>
<term><italic>i, j, k</italic></term>
<def>
<p>Unit vector of the coordinates system</p></def> <def><p>-</p>
</def>
</def-item>
<def-item>
<term>Greek letters</term></def-item>
<def-item>
<term><italic>&#x03C1;</italic></term>
<def>
<p>Density</p></def> <def><p>kg/m<sup>3</sup></p>
</def>
</def-item>
<def-item>
<term><italic>&#x03BC;</italic></term>
<def>
<p>Dynamic viscosity</p></def> <def><p>kg/ms</p>
</def>
</def-item>
</def-list>
</glossary>
<fn-group>
<fn fn-type="other"><p><bold>Funding Statement:</bold> This work is supported by the Fundamental Research Grant Scheme provided by the Ministry of Higher Education (Ref. No. FRGS/1/2020/TK0/UNIMAP/03/26).</p>
</fn>
<fn fn-type="conflict"><p><bold>Conflicts of Interest:</bold> The authors declare that they have no conflicts of interest to report regarding the present study.</p>
</fn>
</fn-group>
<ref-list content-type="authoryear">
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