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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">82643</article-id>
<article-id pub-id-type="doi">10.32604/cmes.2026.082643</article-id>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Article</subject>
</subj-group>
</article-categories>
<title-group>
<article-title>Computer Modelling of Thin, Soft Biological Tissues: A Decoupled Strategy for Standardizing Isotropic and Anisotropic Corneal Biomechanics</article-title>
<alt-title alt-title-type="left-running-head">Computer Modelling of Thin, Soft Biological Tissues: A Decoupled Strategy for Standardizing Isotropic and Anisotropic Corneal Biomechanics.</alt-title>
<alt-title alt-title-type="right-running-head">Computer Modelling of Thin, Soft Biological Tissues: A Decoupled Strategy for Standardizing Isotropic and Anisotropic Corneal Biomechanics.</alt-title>
</title-group>
<contrib-group>
<contrib id="author-1" contrib-type="author">
<name name-style="western"><surname>Gonz&#x00E1;lez-Cabrero</surname><given-names>Jos&#x00E9;</given-names></name><xref ref-type="aff" rid="aff-1">1</xref><xref ref-type="aff" rid="aff-2">2</xref></contrib>
<contrib id="author-2" contrib-type="author">
<name name-style="western"><surname>G&#x00F3;mez</surname><given-names>Carmelo</given-names></name><xref ref-type="aff" rid="aff-1">1</xref><xref ref-type="aff" rid="aff-2">2</xref></contrib>
<contrib id="author-3" contrib-type="author">
<name name-style="western"><surname>Paredes</surname><given-names>Manuel</given-names></name><xref ref-type="aff" rid="aff-3">3</xref></contrib>
<contrib id="author-4" contrib-type="author" corresp="yes">
<name name-style="western"><surname>Cavas</surname><given-names>Francisco</given-names></name><xref ref-type="aff" rid="aff-1">1</xref><xref ref-type="aff" rid="aff-2">2</xref><email>francisco.cavas@upct.es</email></contrib>
<aff id="aff-1"><label>1</label><institution>Departamento de Estructuras, Construcci&#x00F3;n y Expresi&#x00F3;n Gr&#x00E1;fica, Universidad Polit&#x00E9;cnica de Cartagena member of European University of Technology EUT&#x002B;, Campus Muralla del Mar, C/Doctor Fleming, s/n</institution>, <addr-line>Cartagena</addr-line>, <country>Espa&#x00F1;a</country></aff>
<aff id="aff-2"><label>2</label><institution>Grupo de Bioingenieria y Simulaci&#x00F3;n Computacional Aplicada, Universidad Polit&#x00E9;cnica de Cartagena member of European University of Technology EUT&#x002B;, Campus Muralla del Mar, C/Doctor Fleming, s/n</institution>, <addr-line>Cartagena</addr-line>, <country>Espa&#x00F1;a</country></aff>
<aff id="aff-3"><label>3</label><institution>ICA, Universit&#x00E9; de Toulouse, UPS, INSA, ISAE-SUPAERO, MINES-ALBI, CNRS, 3 rue Caroline Aigle</institution>, <addr-line>Toulouse</addr-line>, <country>France</country></aff>
</contrib-group>
<author-notes>
<corresp id="cor1"><label>&#x002A;</label>Corresponding Author: Francisco Cavas. Email: <email>francisco.cavas@upct.es</email></corresp>
</author-notes>
<pub-date date-type="collection" publication-format="electronic">
<year>2026</year>
</pub-date>
<pub-date date-type="pub" publication-format="electronic">
<day>27</day><month>07</month><year>2026</year>
</pub-date>
<volume>148</volume>
<issue>1</issue>
<elocation-id>13</elocation-id>
<history>
<date date-type="received">
<day>19</day>
<month>03</month>
<year>2026</year>
</date>
<date date-type="accepted">
<day>30</day>
<month>06</month>
<year>2026</year>
</date>
</history>
<permissions>
<copyright-statement>&#x00A9; 2026 The Authors. Published by Tech Science Press.</copyright-statement>
<copyright-year>2026</copyright-year>
<copyright-holder>The Authors</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_82643.pdf"></self-uri>
<abstract>
<p>The development of accurate digital twin models of the human cornea is a key factor for planning and monitoring eye treatments and clinical supervision. Corneal tissue can be simulated with the implementation of hyperelastic models based on strain energy density functions. However, the number of hyperelastic models and the parameters&#x2019; variation that define these models hinder comparison across different studies. Furthermore, parameter calculations based on a single test are an ill-posed problem. In this research, a novel sequential methodology based on collagen fibril crimping strain threshold has been implemented to calculate the corneal material&#x2019;s parameters. As an application case, this method has been applied to a hyperelastic Holzapfel&#x2013;Gasser&#x2013;Ogden (HGO) model to calculate the isotropic parameters associated with low stretch levels and the anisotropic parameters that consider the collagen fibres&#x2019; contribution at higher deformations. The sequential test combination applied to a standardized hyperelastic material model could contribute to ensuring physically meaningful and consistent material parameters, the comparison of different investigations, and the development of an accurate <italic>in silico</italic> patient-specific cornea model for clinical applications.</p>
</abstract>
<kwd-group kwd-group-type="author">
<kwd>Parameters calculation</kwd>
<kwd>optimization process</kwd>
<kwd>hyperelastic material</kwd>
<kwd>corneal biomechanics</kwd>
</kwd-group>
<funding-group>
<award-group id="awg1">
<funding-source>Fundaci&#x00F3;n S&#x00E9;neca&#x2013;Agencia de Ciencia y Tecnolog&#x00ED;a de la Regi&#x00F3;n de Murcia</funding-source>
<award-id>22665/PI/24</award-id>
</award-group>
</funding-group>
</article-meta>
</front>
<body>
<sec id="s1">
<label>1</label>
<title>Introduction</title>
<p>The human cornea is a thin tissue that adopts an aspherical shape as a result of a delicate balance among geometry, intraocular pressure, external loads, boundary conditions, and material mechanical properties, whose characterization is a key factor for the development of accurate patient-specific computational analysis [<xref ref-type="bibr" rid="ref-1">1</xref>] with the integration of material models.</p>
<p>Among available material models, the use of anisotropic hyperelastic models based on the integration of fiber is widely accepted. This assumption is supported by evidence from several studies [<xref ref-type="bibr" rid="ref-2">2</xref>] demonstrating that the collagen fibers contained in the lamellae of the corneal stroma are parallel within each lamella and vary across lamellae. These fibers show preferential nasal&#x2013;temporal and superior&#x2013;inferior orientations in the central cornea, which are maintained toward the limbal region, where collagen fibers adopt a preferential circumferential arrangement [<xref ref-type="bibr" rid="ref-3">3</xref>]. Loss of such preferential organization is associated with diseases such as keratoconus [<xref ref-type="bibr" rid="ref-4">4</xref>,<xref ref-type="bibr" rid="ref-5">5</xref>] in which the degradation of mechanical properties leads to corneal bulging and results in severe visual impairment [<xref ref-type="bibr" rid="ref-6">6</xref>].</p>
<p>The first anisotropic hyperelastic models for soft tissues evolved from the exponential formulation proposed by Fung [<xref ref-type="bibr" rid="ref-7">7</xref>], in which the strain-energy density function is expressed in terms of the components of the Green&#x2013;Lagrange strain tensor without explicitly introducing fiber orientation. This approach captures the global nonlinear response of the tissue from a purely phenomenological perspective, but the parameters lack physical meaning [<xref ref-type="bibr" rid="ref-8">8</xref>]. Additionally, the large number of parameters hinders their identification and may lead to non-polyconvex solutions that compromise model stability [<xref ref-type="bibr" rid="ref-9">9</xref>,<xref ref-type="bibr" rid="ref-10">10</xref>].</p>
<p>The development of invariant-based models represented a significant advancement in incorporating the contribution of fibrillar tissue components and remains the most widely used approach [<xref ref-type="bibr" rid="ref-9">9</xref>,<xref ref-type="bibr" rid="ref-10">10</xref>]. In such models, the free energy is decomposed into an isotropic part, corresponding to the extracellular matrix, and an anisotropic part, dependent on invariants associated with fiber directions. The inclusion of invariants in corneal analysis <inline-formula id="ieqn-1"><mml:math id="mml-ieqn-1"><mml:msub><mml:mi>I</mml:mi><mml:mrow><mml:mn>4</mml:mn></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">m</mml:mi><mml:mrow><mml:mrow><mml:mn mathvariant="bold">0</mml:mn></mml:mrow></mml:mrow></mml:msub><mml:mo>&#x22C5;</mml:mo><mml:mi mathvariant="bold-italic">C</mml:mi><mml:msub><mml:mi mathvariant="bold-italic">m</mml:mi><mml:mrow><mml:mrow><mml:mn mathvariant="bold">0</mml:mn></mml:mrow></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-2"><mml:math id="mml-ieqn-2"><mml:msub><mml:mi>I</mml:mi><mml:mrow><mml:mn>6</mml:mn></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">n</mml:mi><mml:mrow><mml:mrow><mml:mn mathvariant="bold">0</mml:mn></mml:mrow></mml:mrow></mml:msub><mml:mo>&#x22C5;</mml:mo><mml:mi mathvariant="bold-italic">C</mml:mi><mml:msub><mml:mi mathvariant="bold-italic">n</mml:mi><mml:mrow><mml:mrow><mml:mn mathvariant="bold">0</mml:mn></mml:mrow></mml:mrow></mml:msub></mml:math></inline-formula> enables capturing the strain along the preferential directions of two collagen fiber families, with these invariants representing the square of fiber stretch.</p>
<p>Formulations inspired by the Holzapfel&#x2013;Gasser&#x2013;Ogden (HGO) model [<xref ref-type="bibr" rid="ref-10">10</xref>] have been successfully adapted to corneal biomechanics, where two principal orthogonally oriented fiber families define stromal anisotropy [<xref ref-type="bibr" rid="ref-11">11</xref>]. These models offer an optimal balance between mathematical simplicity, numerical stability, and predictive capability, and they have therefore become the methodological standard for comparing experimental data and computational simulations in corneal biomechanics [<xref ref-type="bibr" rid="ref-1">1</xref>]. Their main limitations stem from the assumption of perfectly aligned fibers, which may overestimate stiffness in regions where angular dispersion is significant [<xref ref-type="bibr" rid="ref-10">10</xref>], the need to work in a limited range of deformation [<xref ref-type="bibr" rid="ref-12">12</xref>], and the need to be adapted in case of compression analysis [<xref ref-type="bibr" rid="ref-13">13</xref>]; however, their modular structure allows extensions to incorporate dispersion when structural data are available.</p>
<p>More recent models incorporate fiber dispersion through statistical distributions of collagen orientations [<xref ref-type="bibr" rid="ref-14">14</xref>], providing the most faithful representation of corneal microarchitecture. This approach can be formulated using angular integration (AI), where macroscopic response is obtained from an angular distribution function (e.g., von Mises, beta, or Gaussian), or through the generalized structure tensor (GST), which summarizes dispersion into an effective tensor [<xref ref-type="bibr" rid="ref-15">15</xref>,<xref ref-type="bibr" rid="ref-16">16</xref>]. In the cornea, these models allow reproducing regional variations in mechanical behavior and the influence of fibrillar architecture in conditions such as keratoconus [<xref ref-type="bibr" rid="ref-6">6</xref>]. Nevertheless, they require histological or small-angle X-ray scattering (SAXS) data to parameterize dispersion [<xref ref-type="bibr" rid="ref-17">17</xref>] and entail the development of new methodologies for assessing collagen fiber organization [<xref ref-type="bibr" rid="ref-18">18</xref>]. Furthermore, their numerical resolution can be computationally demanding when angular integration is explicitly implemented.</p>
<p>In our previous study [<xref ref-type="bibr" rid="ref-19">19</xref>] a stepwise identification process was proposed to reduce coupling between isotropic and anisotropic components showing that multiple parameter combinations can reproduce the same experimental tests, leading to non-unique but physically plausible solutions showing that direct material&#x2019;s parameter sets calculation based on single tests is an ill-posed problem [<xref ref-type="bibr" rid="ref-20">20</xref>] and isotropic and anisotropic effects may compensate each other during optimization due to the nonlinear material behavior [<xref ref-type="bibr" rid="ref-21">21</xref>] being necessary the implementation of parametric analysis [<xref ref-type="bibr" rid="ref-22">22</xref>]. Furthermore, the combination of different IOP with parameter sets can reproduce similar results [<xref ref-type="bibr" rid="ref-23">23</xref>].</p>
<p>This lack of uniqueness hinders comparison between studies and limits the comparison between biomechanical models, necessitating the establishment of a standardized protocol to compare the results from different investigations adapted to the physiological stress state of the cornea that works as membranes submitted to a biaxial state due to the intraocular pressure effect.</p>
<p>This study proposes a unified comparative framework for the calculation of material parameters by employing the Holzapfel&#x2013;Gasser&#x2013;Ogden (HGO) model due to mathematical simplicity and predictive capacity, and a novel protocol based on a strain threshold for sequential parameter identification. The establishment of a strain threshold can be useful to consider the influence of matrix and fibers contribution allowing at low strain level, where fibers contribution is negligible, the use of uniaxial and equi-biaxial tests results for isotropic parameters calculation considering test coupons cut in any direction whereas uniaxial and equi-biaxial tests results considering superior-inferior and nasal-temporal directions can be used to calculate the anisotropic parameter with strain values exceeding the threshold. The calculation is improved with the implementation of an optimization process based on weighted functions to increase the accuracy in the physiological intraocular pressure range [<xref ref-type="bibr" rid="ref-21">21</xref>], considering data tests based on strain rates close to physiological states [<xref ref-type="bibr" rid="ref-24">24</xref>].</p>
<p>The development of this novel methodology may contribute to the establishment of a robust and efficient common framework for the comparison and validation of experimental data that can be adapted to incorporate dispersion when structural data are available and the definition of different material types for <italic>in silico</italic>, patient-specific biomechanical cornea models.</p>
</sec>
<sec id="s2">
<label>2</label>
<title>Materials and Methodology</title>
<p>In this research, a structural methodology is proposed to optimise the material parameters of corneal tissue through a multi-stage approach applied to the average equi-biaxial test curve obtained from the investigation of Hatami-Marbini and Emu [<xref ref-type="bibr" rid="ref-24">24</xref>] at a strain rate of 2 mm/min. The mentioned investigation was carried out with porcine corneas, and the results are extrapolable considering the similar behaviour to the human cornea in short cycles [<xref ref-type="bibr" rid="ref-25">25</xref>,<xref ref-type="bibr" rid="ref-26">26</xref>] and considering the difficulty in obtaining human corneas.</p>
<p>The optimization process employed to determine the material parameters of a Holzapfel-Gasser-Ogden (HGO) model is based on the introduction of a strain threshold to delineate the region in which the influence of collagen fibres may be considered negligible. Collagen fibres are the main load-bearing elements of the cornea, and when they are stretched, the cornea exhibits a stiffening process known as collagen fibre recruitment [<xref ref-type="bibr" rid="ref-27">27</xref>], where the fibres gradually begin to work, increasing the stiffness of the tissue. This process is related to fibers&#x2019; tortuosity [<xref ref-type="bibr" rid="ref-28">28</xref>,<xref ref-type="bibr" rid="ref-29">29</xref>]. The collagen fibers&#x2019; tortuosity is reduced with age, and this factor could explain the stiffness increment obtained in the inflation test of groups of human corneas with different ages [<xref ref-type="bibr" rid="ref-30">30</xref>]. Considering the results of the inflation test, Jan and Sigal [<xref ref-type="bibr" rid="ref-31">31</xref>] proposed a limit of 10 mmHg. Under this value, the effect of collagen fibrils can be neglected. This value is close to the value obtained by Foong et al. [<xref ref-type="bibr" rid="ref-27">27</xref>] considering a global eye model. Under the framework of a simplified shell theory [<xref ref-type="bibr" rid="ref-32">32</xref>], the cornea is idealized as a membrane with pinned boundary conditions. In this way, true strain (<inline-formula id="ieqn-3"><mml:math id="mml-ieqn-3"><mml:mrow><mml:mi mathvariant="normal">&#x03B5;</mml:mi></mml:mrow><mml:mo stretchy="false">)</mml:mo></mml:math></inline-formula> can be estimated according to the following equation:<disp-formula id="eqn-1"><label>(1)</label><mml:math id="mml-eqn-1" display="block"><mml:mrow><mml:mi mathvariant="normal">&#x03B5;</mml:mi></mml:mrow><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mrow><mml:mtext>IOP</mml:mtext></mml:mrow><mml:mo>&#x22C5;</mml:mo><mml:mrow><mml:mtext>R</mml:mtext></mml:mrow></mml:mrow><mml:mrow><mml:mn>2</mml:mn><mml:mo>&#x22C5;</mml:mo><mml:mrow><mml:mtext>t</mml:mtext></mml:mrow><mml:mo>&#x22C5;</mml:mo><mml:mrow><mml:mtext>E</mml:mtext></mml:mrow></mml:mrow></mml:mfrac></mml:math></disp-formula>where IOP is the intraocular pressure, R the average corneal radius, t the average corneal thickness, and E the elastic modulus. A sensitivity analysis was conducted to assess the influence of key biomechanical and geometrical parameters, including intraocular pressure (IOP), mean corneal radius (R), average corneal thickness (t), and Young&#x2019;s modulus (E). The corresponding parameter ranges are presented in the following <xref ref-type="table" rid="table-1">Table 1</xref>.</p>
<table-wrap id="table-1">
<label>Table 1</label>
<caption>
<title>Average and standard deviation of corneal parameters.</title>
</caption>
<table>
<colgroup>
<col align="center"/>
<col align="center"/>
<col align="center"/>
<col align="center"/>
</colgroup>
<thead>
<tr>
<th></th>
<th>Average (&#x03BC;)</th>
<th>Standard Deviation (&#x03C3;)</th>
<th>Reference</th>
</tr>
</thead>
<tbody>
<tr>
<td>IOP (mmHg)</td>
<td>14.24</td>
<td>2.8</td>
<td>[<xref ref-type="bibr" rid="ref-33">33</xref>]</td>
</tr>
<tr>
<td>Average thickness (&#x03BC;m)</td>
<td>570</td>
<td>34</td>
<td>[<xref ref-type="bibr" rid="ref-34">34</xref>&#x2013;<xref ref-type="bibr" rid="ref-36">36</xref>]</td>
</tr>
<tr>
<td>Average radius (mm)</td>
<td>7.1</td>
<td>0.3</td>
<td>[<xref ref-type="bibr" rid="ref-37">37</xref>]</td>
</tr>
<tr>
<td>E (MPa)</td>
<td>0.25</td>
<td>0.1</td>
<td>[<xref ref-type="bibr" rid="ref-38">38</xref>]</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>Estimated physiological strain has been calculated for each parameter range. The results obtained can be observed in <xref ref-type="fig" rid="fig-1">Fig. 1</xref>.</p>
<fig id="fig-1">
<label>Figure 1</label>
<caption>
<title>Estimation of the physiological strain based on extended range parameters.</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMES_82643-fig-1.tif"/>
</fig>
<p>According to previous research work [<xref ref-type="bibr" rid="ref-39">39</xref>], collagen fibrillar recruitment in the cornea does not occur immediately upon loading but is preceded by a regime dominated by molecular-level deformation until approximately 2.8% strain, according to experimental observations. At values lower than this strain, most of the deformation is accommodated by molecular straightening associated with the helical arrangement of tropocollagen, whereas mechanisms such as fibrillar elongation and reorientation become more evident beyond this level. In this research work, a strain level of 2% (<xref ref-type="fig" rid="fig-1">Fig. 1</xref>) has been considered for a significant pre-recruitment regime with the hypothesis that it lies within the range where the response remains predominantly governed by molecular mechanisms [<xref ref-type="bibr" rid="ref-39">39</xref>] while remaining below the transition region and the minimum estimated physiological strain level calculated of 2.45%.</p>

<p>Below the 2% strain threshold (<italic>&#x03BB;</italic> &#x003D; 1.02), the corneal response can be considered isotropic, and both strip tensile and biaxial tests can be used with test coupons cut in any direction, making either valid to estimate the isotropic parameters <inline-formula id="ieqn-4"><mml:math id="mml-ieqn-4"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-5"><mml:math id="mml-ieqn-5"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula>. In this strain range, the cornea can be modelled with a simpler material model considering only the isotropic contribution of the Mooney-Rivlin material model. However, in simulations at higher strain levels, the collagen fiber recruitment cannot be neglected, and the contribution of the anisotropic component must be incorporated. The anisotropic material components <inline-formula id="ieqn-6"><mml:math id="mml-ieqn-6"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-7"><mml:math id="mml-ieqn-7"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> that dominate the mechanical response of the corneal tissue at higher strain levels can be obtained from uniaxial and equi-biaxial tests carried out considering nasal-temporal and superior-inferior directions where there is a preferential fiber orientation.</p>
<p>In this research, as an application case, experimental curves acquired at a strain rate of 2% per minute are used throughout the calibration process. This strain rate is compatible with the daily variation of the intraocular pressure (IOP) and the associated strain fluctuations 0%&#x2013;3% that affect the corneal shape. Parameter optimization was carried out with <italic>ad-hoc</italic> software developed with Python version 3.11.9 (Python Software Foundation). The parameters calculated have been applied, as an application case, to a virtual inflation test of an <italic>in silico</italic> patient-specific cornea model carried out with a finite element model developed with ANSYS 2023 R1 software (Swanson Analysis System Inc., Houston, PA, USA). The entire process is schematized in <xref ref-type="fig" rid="fig-2">Figs. 2</xref> and <xref ref-type="fig" rid="fig-3">3</xref>.</p>
<fig id="fig-2">
<label>Figure 2</label>
<caption>
<title>Steps that conform to the material parameters estimation analysis.</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMES_82643-fig-2.tif"/>
</fig><fig id="fig-3">
<label>Figure 3</label>
<caption>
<title>Steps that conform to the material parameters estimation analysis (continuation).</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMES_82643-fig-3a.tif"/>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMES_82643-fig-3b.tif"/>
</fig>
<p><bold><italic>Mathematical Modelling</italic></bold></p>
<p>It is widely accepted that corneal tissue can be modelled as a hyperelastic material where the local deformation is represented by the deformation gradient <inline-formula id="ieqn-8"><mml:math id="mml-ieqn-8"><mml:mrow><mml:mrow><mml:mi mathvariant="bold">F</mml:mi></mml:mrow></mml:mrow><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mrow><mml:mi mathvariant="bold">x</mml:mi></mml:mrow></mml:mrow></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mrow><mml:mi mathvariant="bold">X</mml:mi></mml:mrow></mml:mrow></mml:mrow></mml:mfrac></mml:math></inline-formula>, which relates the position of a material point in the deformed configuration <inline-formula id="ieqn-9"><mml:math id="mml-ieqn-9"><mml:mrow><mml:mi mathvariant="bold">x</mml:mi></mml:mrow></mml:math></inline-formula> to its initial position <inline-formula id="ieqn-10"><mml:math id="mml-ieqn-10"><mml:mrow><mml:mi mathvariant="bold">X</mml:mi></mml:mrow></mml:math></inline-formula>. The determinant of this deformation gradient, <inline-formula id="ieqn-11"><mml:math id="mml-ieqn-11"><mml:mi>J</mml:mi><mml:mo>=</mml:mo><mml:mo movablelimits="true" form="prefix">det</mml:mo><mml:mo stretchy="false">(</mml:mo><mml:mrow><mml:mrow><mml:mi mathvariant="bold">F</mml:mi></mml:mrow></mml:mrow><mml:mo stretchy="false">)</mml:mo></mml:math></inline-formula>, represents the volumetric change of a differential volume and takes a value of 1 for incompressible materials. In isothermal processes, it is common to use a strain energy density function <inline-formula id="ieqn-12"><mml:math id="mml-ieqn-12"><mml:mi>&#x03C8;</mml:mi></mml:math></inline-formula> from which the Cauchy stress tensor <inline-formula id="ieqn-13"><mml:math id="mml-ieqn-13"><mml:mi mathvariant="bold-italic">&#x03C3;</mml:mi></mml:math></inline-formula> can be derived. For a quasi-incompressible material, this relationship is given by the following expression, where the Lagrange multiplier and the isochoric component of the strain energy density <inline-formula id="ieqn-14"><mml:math id="mml-ieqn-14"><mml:mover><mml:mrow><mml:mi mathvariant="normal">&#x03C8;</mml:mi></mml:mrow><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover></mml:math></inline-formula> is considered:<disp-formula id="eqn-2"><label>(2)</label><mml:math id="mml-eqn-2" display="block"><mml:mrow><mml:mi mathvariant="bold-italic">&#x03C3;</mml:mi></mml:mrow><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mi>p</mml:mi><mml:mrow><mml:mrow><mml:mi mathvariant="bold">I</mml:mi></mml:mrow></mml:mrow><mml:mo>+</mml:mo><mml:mfrac><mml:mn>2</mml:mn><mml:mi>J</mml:mi></mml:mfrac><mml:mrow><mml:mrow><mml:mi mathvariant="bold">F</mml:mi></mml:mrow></mml:mrow><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mover><mml:mi mathvariant="normal">&#x03A8;</mml:mi><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mi mathvariant="bold-italic">C</mml:mi></mml:mrow></mml:mrow></mml:mfrac></mml:mstyle><mml:mrow><mml:msup><mml:mi mathvariant="bold-italic">F</mml:mi><mml:mrow><mml:mi mathvariant="bold-italic">T</mml:mi></mml:mrow></mml:msup></mml:mrow></mml:math></disp-formula></p>
<p>The Lagrange multiplier <inline-formula id="ieqn-15"><mml:math id="mml-ieqn-15"><mml:mi>p</mml:mi></mml:math></inline-formula> is determined by imposing an incompressibility constraint. The second component considers the deviatoric component, where <inline-formula id="ieqn-16"><mml:math id="mml-ieqn-16"><mml:msup><mml:mrow><mml:mrow><mml:mi mathvariant="bold">C</mml:mi></mml:mrow><mml:mo>=</mml:mo><mml:mrow><mml:mi mathvariant="bold">F</mml:mi></mml:mrow></mml:mrow><mml:mrow><mml:mi>T</mml:mi></mml:mrow></mml:msup><mml:mrow><mml:mrow><mml:mi mathvariant="bold">F</mml:mi></mml:mrow></mml:mrow></mml:math></inline-formula> is the right Cauchy-Green deformation tensor. The deviatoric component, which is expressed as a function of invariants, can be observed in the following equation. In this research, an HGO-Mooney-Rivlin constitutive model is considered.
<disp-formula id="eqn-3"><label>(3)</label><mml:math id="mml-eqn-3" display="block"><mml:msub><mml:mi>&#x03C8;</mml:mi><mml:mrow><mml:mi>d</mml:mi><mml:mi>e</mml:mi><mml:mi>v</mml:mi><mml:mi>i</mml:mi><mml:mi>a</mml:mi><mml:mi>t</mml:mi><mml:mi>o</mml:mi><mml:mi>r</mml:mi><mml:mi>i</mml:mi><mml:mi>c</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mover><mml:mi>I</mml:mi><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mo>&#x2212;</mml:mo><mml:mn>3</mml:mn><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mover><mml:mi>I</mml:mi><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub><mml:mo>&#x2212;</mml:mo><mml:mn>3</mml:mn><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mrow><mml:mn>2</mml:mn><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:mrow></mml:mfrac></mml:mstyle><mml:munder><mml:mo>&#x2211;</mml:mo><mml:mrow><mml:mi>i</mml:mi><mml:mo>=</mml:mo><mml:mn>4</mml:mn><mml:mo>,</mml:mo><mml:mn>6</mml:mn></mml:mrow></mml:munder><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mtext>ex</mml:mtext></mml:mrow><mml:mrow><mml:mtext>p</mml:mtext></mml:mrow><mml:mrow><mml:mo>[</mml:mo><mml:mrow><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:mrow><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mover><mml:mi>I</mml:mi><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub><mml:mo>&#x2212;</mml:mo><mml:mn>3</mml:mn><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>]</mml:mo></mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mn>1</mml:mn><mml:mo>)</mml:mo></mml:mrow></mml:math></disp-formula>where the parameters <inline-formula id="ieqn-17"><mml:math id="mml-ieqn-17"><mml:msub><mml:mrow><mml:mtext>c</mml:mtext></mml:mrow><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-18"><mml:math id="mml-ieqn-18"><mml:msub><mml:mrow><mml:mtext>c</mml:mtext></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> represent the isotropic behaviour of the material, and the parameters <inline-formula id="ieqn-19"><mml:math id="mml-ieqn-19"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-20"><mml:math id="mml-ieqn-20"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> define the anisotropic behaviour of the material.</p>
<p>The parameter <inline-formula id="ieqn-21"><mml:math id="mml-ieqn-21"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> defines the stiffness influence of the fibers in the preferred direction analysed and will vary depending on the fibers&#x2019; concentration, while <inline-formula id="ieqn-22"><mml:math id="mml-ieqn-22"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> is a dimensionless parameter that accounts for the nonlinear behaviour of the fibers at large strains.</p>
<p>The isotropic expression is defined using a Neo-Hookean model, where the invariant <inline-formula id="ieqn-23"><mml:math id="mml-ieqn-23"><mml:mover><mml:msub><mml:mi>I</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mo>=</mml:mo><mml:mi>t</mml:mi><mml:mi>r</mml:mi><mml:mover><mml:mrow><mml:mi mathvariant="bold">C</mml:mi></mml:mrow><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover></mml:math></inline-formula> represents the trace of the right Cauchy-Green deformation tensor where <inline-formula id="ieqn-24"><mml:math id="mml-ieqn-24"><mml:mover><mml:mrow><mml:mi mathvariant="bold">C</mml:mi></mml:mrow><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mo>=</mml:mo><mml:msup><mml:mover><mml:mrow><mml:mi mathvariant="bold">F</mml:mi></mml:mrow><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mrow><mml:mrow><mml:mtext>T</mml:mtext></mml:mrow></mml:mrow></mml:msup><mml:mover><mml:mrow><mml:mi mathvariant="bold">F</mml:mi></mml:mrow><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover></mml:math></inline-formula> with <inline-formula id="ieqn-25"><mml:math id="mml-ieqn-25"><mml:mover><mml:mrow><mml:mi mathvariant="bold">F</mml:mi></mml:mrow><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mo>=</mml:mo><mml:msup><mml:mi>J</mml:mi><mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mn>1</mml:mn><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mn>3</mml:mn></mml:mrow></mml:msup><mml:mrow><mml:mi mathvariant="bold">F</mml:mi></mml:mrow></mml:math></inline-formula>, the invariant <inline-formula id="ieqn-26"><mml:math id="mml-ieqn-26"><mml:mover><mml:msub><mml:mi>I</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover></mml:math></inline-formula> is defined as <inline-formula id="ieqn-27"><mml:math id="mml-ieqn-27"><mml:mover><mml:msub><mml:mi>I</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mo>=</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:mn>2</mml:mn></mml:mfrac><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:mi>t</mml:mi><mml:mi>r</mml:mi><mml:mo stretchy="false">(</mml:mo><mml:mover><mml:mrow><mml:mi mathvariant="bold">C</mml:mi></mml:mrow><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mo stretchy="false">)</mml:mo><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:mi>t</mml:mi><mml:mi>r</mml:mi><mml:mo stretchy="false">(</mml:mo><mml:msup><mml:mover><mml:mrow><mml:mi mathvariant="bold">C</mml:mi></mml:mrow><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo stretchy="false">)</mml:mo><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>, while the invariants <inline-formula id="ieqn-28"><mml:math id="mml-ieqn-28"><mml:mover><mml:msub><mml:mi>I</mml:mi><mml:mrow><mml:mn>4</mml:mn></mml:mrow></mml:msub><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mo>=</mml:mo><mml:msub><mml:mrow><mml:mi mathvariant="bold">m</mml:mi></mml:mrow><mml:mrow><mml:mrow><mml:mn mathvariant="bold">0</mml:mn></mml:mrow></mml:mrow></mml:msub><mml:mover><mml:mrow><mml:mi mathvariant="bold">C</mml:mi></mml:mrow><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:msub><mml:mrow><mml:mrow><mml:mi mathvariant="bold">m</mml:mi></mml:mrow></mml:mrow><mml:mrow><mml:mrow><mml:mn mathvariant="bold">0</mml:mn></mml:mrow></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-29"><mml:math id="mml-ieqn-29"><mml:mover><mml:msub><mml:mi>I</mml:mi><mml:mrow><mml:mn>6</mml:mn></mml:mrow></mml:msub><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mo>=</mml:mo><mml:msub><mml:mrow><mml:mi mathvariant="bold">n</mml:mi></mml:mrow><mml:mrow><mml:mrow><mml:mn mathvariant="bold">0</mml:mn></mml:mrow></mml:mrow></mml:msub><mml:mover><mml:mrow><mml:mi mathvariant="bold">C</mml:mi></mml:mrow><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:msub><mml:mrow><mml:mrow><mml:mi mathvariant="bold">n</mml:mi></mml:mrow></mml:mrow><mml:mrow><mml:mrow><mml:mn mathvariant="bold">0</mml:mn></mml:mrow></mml:mrow></mml:msub></mml:math></inline-formula> are pseudo-invariants that represent the squared fiber stretches in the initial state. Defining the preferred fiber directions as <inline-formula id="ieqn-30"><mml:math id="mml-ieqn-30"><mml:msub><mml:mrow><mml:mrow><mml:mi mathvariant="bold">m</mml:mi></mml:mrow></mml:mrow><mml:mrow><mml:mrow><mml:mn mathvariant="bold">0</mml:mn></mml:mrow></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mrow><mml:mo>[</mml:mo><mml:mrow><mml:mn mathvariant="bold">1</mml:mn><mml:mo mathvariant="bold">,</mml:mo><mml:mn mathvariant="bold">0</mml:mn></mml:mrow><mml:mo>,</mml:mo><mml:mrow><mml:mrow><mml:mn mathvariant="bold">0</mml:mn></mml:mrow></mml:mrow><mml:mo>]</mml:mo></mml:mrow></mml:math></inline-formula> and <inline-formula id="ieqn-31"><mml:math id="mml-ieqn-31"><mml:msub><mml:mrow><mml:mrow><mml:mi mathvariant="bold">n</mml:mi></mml:mrow></mml:mrow><mml:mrow><mml:mrow><mml:mn mathvariant="bold">0</mml:mn></mml:mrow></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mrow><mml:mo>[</mml:mo><mml:mrow><mml:mn mathvariant="bold">0</mml:mn><mml:mo mathvariant="bold">,</mml:mo><mml:mn mathvariant="bold">1</mml:mn></mml:mrow><mml:mo>,</mml:mo><mml:mrow><mml:mrow><mml:mn mathvariant="bold">0</mml:mn></mml:mrow></mml:mrow><mml:mo>]</mml:mo></mml:mrow></mml:math></inline-formula>.</p>
<p>Considering the proposed model, the stress of a uniaxial and biaxial tensile test depending on the stretch can be observed in <xref ref-type="disp-formula" rid="eqn-4">Eqs. (4)</xref>&#x2013;<xref ref-type="disp-formula" rid="eqn-7">(7)</xref>, respectively:<list list-type="bullet">
<list-item>
<p>Uniaxial tensile test</p></list-item>
</list>
<disp-formula id="eqn-4"><label>(4)</label><mml:math id="mml-eqn-4" display="block"><mml:mtable columnalign="right left right left right left right left right left right left" rowspacing="3pt" columnspacing="0em 2em 0em 2em 0em 2em 0em 2em 0em 2em 0em" displaystyle="true"><mml:mtr><mml:mtd /><mml:mtd><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>x</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>2</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>4</mml:mn></mml:mrow></mml:msup></mml:mfrac><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mn>2</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>4</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mn>1</mml:mn><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mfrac></mml:mstyle><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mn>2</mml:mn><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:mn>1</mml:mn><mml:mo>)</mml:mo></mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mrow><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:mn>1</mml:mn><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mrow></mml:msup></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<disp-formula id="eqn-5"><label>(5)</label><mml:math id="mml-eqn-5" display="block"><mml:mtable columnalign="right left right left right left right left right left right left" rowspacing="3pt" columnspacing="0em 2em 0em 2em 0em 2em 0em 2em 0em 2em 0em" displaystyle="true"><mml:mtr><mml:mtd /><mml:mtd><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>y</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>z</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<list list-type="bullet">
<list-item>
<p>Biaxial tensile test</p></list-item>
</list>
<disp-formula id="eqn-6"><label>(6)</label><mml:math id="mml-eqn-6" display="block"><mml:mtable columnalign="right left right left right left right left right left right left" rowspacing="3pt" columnspacing="0em 2em 0em 2em 0em 2em 0em 2em 0em 2em 0em" displaystyle="true"><mml:mtr><mml:mtd /><mml:mtd><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>x</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>y</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>2</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>4</mml:mn></mml:mrow></mml:msup></mml:mfrac><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mn>2</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>4</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mn>1</mml:mn><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mfrac></mml:mstyle><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mn>2</mml:mn><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:mn>1</mml:mn><mml:mo>)</mml:mo></mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mrow><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:mn>1</mml:mn><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mrow></mml:msup></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<disp-formula id="eqn-7"><label>(7)</label><mml:math id="mml-eqn-7" display="block"><mml:mtable columnalign="right left right left right left right left right left right left" rowspacing="3pt" columnspacing="0em 2em 0em 2em 0em 2em 0em 2em 0em 2em 0em" displaystyle="true"><mml:mtr><mml:mtd /><mml:mtd><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>z</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula></p>
<p>As can be observed, the stress value depends on the stretch (<italic>&#x03BB;</italic>) value reached and the material properties (<italic>c</italic><sub>1</sub>, <italic>c</italic><sub>2</sub>, <italic>k</italic><sub>1,</sub> and <italic>k</italic><sub>2</sub>) that can be calculated based on test results. In this research work, the following multistage process is proposed according to <xref ref-type="fig" rid="fig-4">Fig. 4</xref>:</p>
<fig id="fig-4">
<label>Figure 4</label>
<caption>
<title>Flow chart of the parameters&#x2019; calculation process.</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMES_82643-fig-4.tif"/>
</fig>
<p>In step 1, experimental data from uniaxial and/or equi-biaxial tests are considered to calculate the isotropic parameters <inline-formula id="ieqn-32"><mml:math id="mml-ieqn-32"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-33"><mml:math id="mml-ieqn-33"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> in the low strain regime, under the strain threshold (<italic>&#x03BB;</italic> &#x003D; 1.02) and considering an iterative parameter optimization process based on the definition of a differential evolution algorithm. The mathematical formulation of the Cauchy stress tensor differs depending on the loading condition. In the uniaxial case, assuming deformation in the <italic>x</italic>-direction and zero lateral stresses (<inline-formula id="ieqn-34"><mml:math id="mml-ieqn-34"><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>y</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>z</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math></inline-formula>), the Cauchy stress is given by:<disp-formula id="eqn-8"><label>(8)</label><mml:math id="mml-eqn-8" display="block"><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>x</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>2</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mn>1</mml:mn><mml:mi>&#x03BB;</mml:mi></mml:mfrac></mml:mstyle><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mn>2</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:mi>&#x03BB;</mml:mi><mml:mo>&#x2212;</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mn>1</mml:mn><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mfrac></mml:mstyle><mml:mo>)</mml:mo></mml:mrow></mml:math></disp-formula></p>
<p>Whereas in the equi-biaxial case, assuming deformation in the <italic>x</italic>-direction and <italic>y</italic>-direction and zero stress in the <italic>z</italic>-direction, the Cauchy stress is given by:<disp-formula id="eqn-9"><label>(9)</label><mml:math id="mml-eqn-9" display="block"><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>x</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>y</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>2</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mn>1</mml:mn><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>4</mml:mn></mml:mrow></mml:msup></mml:mfrac></mml:mstyle><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mn>2</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>4</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mn>1</mml:mn><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mfrac></mml:mstyle><mml:mo>)</mml:mo></mml:mrow></mml:math></disp-formula></p>
<p>In this step, the material parameters <inline-formula id="ieqn-35"><mml:math id="mml-ieqn-35"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-36"><mml:math id="mml-ieqn-36"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> must ensure that the stress response exhibits a monotonically increasing behavior under both uniaxial and biaxial tensile loading conditions, being <inline-formula id="ieqn-37"><mml:math id="mml-ieqn-37"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> &#x003E; 0. In both cases, a penalty factor of 10<sup>20</sup> has been included to enforce the solution.</p>
<p>In step 2, <inline-formula id="ieqn-38"><mml:math id="mml-ieqn-38"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-39"><mml:math id="mml-ieqn-39"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> parameters are calculated considering uniaxial and/or equi-biaxial experiment data with <inline-formula id="ieqn-40"><mml:math id="mml-ieqn-40"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-41"><mml:math id="mml-ieqn-41"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> values obtained from step 1 and adding the anisotropic term in a strain range above the defined threshold (<italic>&#x03BB;</italic> &#x003D; 1.02). The mathematical formulation of the Cauchy stress tensor differs depending on the loading condition. In the uniaxial case, assuming deformation in the <italic>x</italic>-direction and zero lateral stresses (<inline-formula id="ieqn-42"><mml:math id="mml-ieqn-42"><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>y</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>z</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math></inline-formula>), the Cauchy stress is given by:<disp-formula id="eqn-10"><label>(10)</label><mml:math id="mml-eqn-10" display="block"><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>x</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>2</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mn>1</mml:mn><mml:mi>&#x03BB;</mml:mi></mml:mfrac></mml:mstyle><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mn>2</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:mi>&#x03BB;</mml:mi><mml:mo>&#x2212;</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mn>1</mml:mn><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mfrac></mml:mstyle><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mn>2</mml:mn><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:mn>1</mml:mn><mml:mo>)</mml:mo></mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mrow><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:mn>1</mml:mn><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mrow></mml:msup></mml:math></disp-formula>whereas in the equi-biaxial case, assuming deformation in the <italic>x</italic>-direction and <italic>y</italic>-direction and zero stress in the <italic>z</italic>-direction, the Cauchy stress is given by:<disp-formula id="eqn-11"><label>(11)</label><mml:math id="mml-eqn-11" display="block"><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>x</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>y</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>2</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mn>1</mml:mn><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>4</mml:mn></mml:mrow></mml:msup></mml:mfrac></mml:mstyle><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mn>2</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>4</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mn>1</mml:mn><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mfrac></mml:mstyle><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mn>4</mml:mn><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:mn>1</mml:mn><mml:mo>)</mml:mo></mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mrow><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:mn>1</mml:mn><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mrow></mml:msup><mml:mo>.</mml:mo></mml:math></disp-formula></p>
<p>The anisotropic term incorporates the effects due to collagen fiber recruitment, which becomes significant at higher stretch levels, incorporating the characteristic nonlinear stiffening observed in experimental data. In this step, a mathematical condition of <inline-formula id="ieqn-43"><mml:math id="mml-ieqn-43"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> &#x003E; 0 and <inline-formula id="ieqn-44"><mml:math id="mml-ieqn-44"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> &#x003E; 0 is imposed with a penalty factor of 10<sup>20</sup> to enforce a monotonically increasing behavior under both uniaxial and biaxial tensile loading conditions.</p>
<p>In step 3, an optimization process has been applied to improve the results considering the complete curve. This procedure has been applied considering previously calculated values of <inline-formula id="ieqn-45"><mml:math id="mml-ieqn-45"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula>, <inline-formula id="ieqn-46"><mml:math id="mml-ieqn-46"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula>, <inline-formula id="ieqn-47"><mml:math id="mml-ieqn-47"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-48"><mml:math id="mml-ieqn-48"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> as initial values of the iterative process. In case of <inline-formula id="ieqn-49"><mml:math id="mml-ieqn-49"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula>, <inline-formula id="ieqn-50"><mml:math id="mml-ieqn-50"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula>, <inline-formula id="ieqn-51"><mml:math id="mml-ieqn-51"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula>, the refined optimization is substantiated due to the mathematical influence of the parameters at low stretch ratio of the uniaxial and equi-biaxial curve that can be calculated considering the derivative of the uniaxial and equi-biaxial Cauchy stress expression given respectively in <xref ref-type="disp-formula" rid="eqn-12">Eqs. (12)</xref> and <xref ref-type="disp-formula" rid="eqn-13">(13)</xref> with respect to the stretch ratio <inline-formula id="ieqn-52"><mml:math id="mml-ieqn-52"><mml:mi>&#x03BB;</mml:mi></mml:math></inline-formula>. The derivative value at <inline-formula id="ieqn-53"><mml:math id="mml-ieqn-53"><mml:mi>&#x03BB;</mml:mi></mml:math></inline-formula> &#x003D; 1, which considers the initial slope of the stress&#x2013;stretch curve, depends not only on the isotropic parameters <inline-formula id="ieqn-54"><mml:math id="mml-ieqn-54"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-55"><mml:math id="mml-ieqn-55"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> but also on the anisotropic parameter <inline-formula id="ieqn-56"><mml:math id="mml-ieqn-56"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> as can be observed in the following equation:<disp-formula id="eqn-12"><label>(12)</label><mml:math id="mml-eqn-12" display="block"><mml:mtable columnalign="right left right left right left right left right left right left" rowspacing="3pt" columnspacing="0em 2em 0em 2em 0em 2em 0em 2em 0em 2em 0em" displaystyle="true"><mml:mtr><mml:mtd /><mml:mtd><mml:msub><mml:mrow><mml:mo fence="true" stretchy="true" symmetric="true"></mml:mo><mml:mfrac><mml:mrow><mml:mi>d</mml:mi><mml:mi>&#x03C3;</mml:mi></mml:mrow><mml:mrow><mml:mi>d</mml:mi><mml:mi>&#x03BB;</mml:mi></mml:mrow></mml:mfrac><mml:mo>|</mml:mo></mml:mrow><mml:mrow><mml:mi>&#x03BB;</mml:mi><mml:mo>=</mml:mo><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>6</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:mn>6</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:mn>4</mml:mn><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<disp-formula id="eqn-13"><label>(13)</label><mml:math id="mml-eqn-13" display="block"><mml:mtable columnalign="right left right left right left right left right left right left" rowspacing="3pt" columnspacing="0em 2em 0em 2em 0em 2em 0em 2em 0em 2em 0em" displaystyle="true"><mml:mtr><mml:mtd /><mml:mtd><mml:msub><mml:mrow><mml:mo fence="true" stretchy="true" symmetric="true"></mml:mo><mml:mfrac><mml:mrow><mml:mi>d</mml:mi><mml:mi>&#x03C3;</mml:mi></mml:mrow><mml:mrow><mml:mi>d</mml:mi><mml:mi>&#x03BB;</mml:mi></mml:mrow></mml:mfrac><mml:mo>|</mml:mo></mml:mrow><mml:mrow><mml:mi>&#x03BB;</mml:mi><mml:mo>=</mml:mo><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>12</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:mn>12</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:mn>8</mml:mn><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula></p>
<p>The exponential term associated with <inline-formula id="ieqn-57"><mml:math id="mml-ieqn-57"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> vanishes when <inline-formula id="ieqn-58"><mml:math id="mml-ieqn-58"><mml:mi>&#x03BB;</mml:mi></mml:math></inline-formula> &#x003D; 1 because its derivative is proportional to (<inline-formula id="ieqn-59"><mml:math id="mml-ieqn-59"><mml:msup><mml:mi>&#x03BB;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> &#x2212; 1), which is zero at that point. Consequently, <inline-formula id="ieqn-60"><mml:math id="mml-ieqn-60"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> has no influence at low stretch ratio, confirming that it only affects the stress behavior at higher deformations. This highlights a critical insight: From a mathematical point of view, <inline-formula id="ieqn-61"><mml:math id="mml-ieqn-61"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> cannot be neglected in the early stretch domain, even though it is typically associated with fiber recruitment at larger deformations. This result emphasizes the mathematical importance of incorporating the anisotropic parameter <inline-formula id="ieqn-62"><mml:math id="mml-ieqn-62"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> in the early stages of stress-stretch behavior, especially when interpreting or calibrating experimental data within the physiological range, and the need to incorporate a refined optimization process when decoupled material properties are calculated. Although in the mathematical model <inline-formula id="ieqn-63"><mml:math id="mml-ieqn-63"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> has a constant value, this value considers the stiffness influence of fibers depending on the fibers&#x2019; recruitment and preferential orientation. In this research work, the hypothesis that in the proximity of <italic>&#x03BB;</italic> &#x003D; 1 the contribution to the derivative of the anisotropic component cannot be greater than the contribution of the isotropic component has been considered with the inclusion of a penalty factor of 10<sup>20</sup> in case that this value exceeds the value of the isotropic component according to <xref ref-type="disp-formula" rid="eqn-14">Eqs. (14)</xref> and <xref ref-type="disp-formula" rid="eqn-15">(15)</xref>, considering uniaxial and biaxial tensile tests, respectively.</p>
<p>Penalty factor in case that
<disp-formula id="eqn-14"><label>(14)</label><mml:math id="mml-eqn-14" display="block"><mml:mn>4</mml:mn><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mo>&#x2265;</mml:mo><mml:mn>12</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:mn>12</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></disp-formula></p>
<p>(Uniaxial test)</p>
<p>Penalty factor in case that
<disp-formula id="eqn-15"><label>(15)</label><mml:math id="mml-eqn-15" display="block"><mml:mn>8</mml:mn><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mo>&#x2265;</mml:mo><mml:mn>12</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:mn>12</mml:mn><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></disp-formula></p>
<p>(Biaxial test)</p>
<p>The simultaneous optimization of all parameters, even when initialized from reasonable starting values, may lead to significant variations due to their intrinsic mathematical interdependence. Therefore, in this study, constraints are imposed such that the optimized values of <inline-formula id="ieqn-64"><mml:math id="mml-ieqn-64"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-65"><mml:math id="mml-ieqn-65"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> must yield at least 95% of the coefficient of determination obtained in Step 1, with a penalty factor of 10<sup>20</sup> in case this value is lower according to <xref ref-type="disp-formula" rid="eqn-16">Eq. (16)</xref>, while also penalizing large individual variations of these parameters through a penalty factor applied to the sum of the squares of their variations according to <xref ref-type="disp-formula" rid="eqn-17">Eq. (17)</xref>:</p>
<p>Penalty factor in case that
<disp-formula id="eqn-16"><label>(16)</label><mml:math id="mml-eqn-16" display="block"><mml:mtable columnalign="right left right left right left right left right left right left" rowspacing="3pt" columnspacing="0em 2em 0em 2em 0em 2em 0em 2em 0em 2em 0em" displaystyle="true"><mml:mtr><mml:mtd /><mml:mtd><mml:msubsup><mml:mi>R</mml:mi><mml:mrow><mml:mi>S</mml:mi><mml:mi>T</mml:mi><mml:mi>E</mml:mi><mml:mi>P</mml:mi><mml:mspace width="thinmathspace" /><mml:mn>3</mml:mn></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msubsup><mml:mo>&#x2265;</mml:mo><mml:mn>0.95</mml:mn><mml:mo>&#x22C5;</mml:mo><mml:msubsup><mml:mi>R</mml:mi><mml:mrow><mml:mi>S</mml:mi><mml:mi>T</mml:mi><mml:mi>E</mml:mi><mml:mi>P</mml:mi><mml:mspace width="thinmathspace" /><mml:mn>1</mml:mn></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msubsup></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<disp-formula id="eqn-17"><label>(17)</label><mml:math id="mml-eqn-17" display="block"><mml:mtable columnalign="right left right left right left right left right left right left" rowspacing="3pt" columnspacing="0em 2em 0em 2em 0em 2em 0em 2em 0em 2em 0em" displaystyle="true"><mml:mtr><mml:mtd /><mml:mtd><mml:mrow><mml:mtext>Penalty factor</mml:mtext></mml:mrow><mml:mo>=</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mrow><mml:mn>10</mml:mn></mml:mrow></mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mrow><mml:msub><mml:mi>C</mml:mi><mml:mrow><mml:mn>1</mml:mn><mml:mspace width="thinmathspace" /><mml:mi>S</mml:mi><mml:mi>T</mml:mi><mml:mi>E</mml:mi><mml:mi>P</mml:mi><mml:mspace width="thinmathspace" /><mml:mn>3</mml:mn></mml:mrow></mml:msub><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>C</mml:mi><mml:mrow><mml:mn>1</mml:mn><mml:mspace width="thinmathspace" /><mml:mi>S</mml:mi><mml:mi>T</mml:mi><mml:mi>E</mml:mi><mml:mi>P</mml:mi><mml:mspace width="thinmathspace" /><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:mrow><mml:msub><mml:mi>C</mml:mi><mml:mrow><mml:mn>1</mml:mn><mml:mspace width="thinmathspace" /><mml:mi>S</mml:mi><mml:mi>T</mml:mi><mml:mi>E</mml:mi><mml:mi>P</mml:mi><mml:mspace width="thinmathspace" /><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:mfrac></mml:mstyle><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:mfrac><mml:mrow><mml:msub><mml:mi>C</mml:mi><mml:mrow><mml:mn>2</mml:mn><mml:mspace width="thinmathspace" /><mml:mi>S</mml:mi><mml:mi>T</mml:mi><mml:mi>E</mml:mi><mml:mi>P</mml:mi><mml:mspace width="thinmathspace" /><mml:mn>3</mml:mn></mml:mrow></mml:msub><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>C</mml:mi><mml:mrow><mml:mn>2</mml:mn><mml:mspace width="thinmathspace" /><mml:mi>S</mml:mi><mml:mi>T</mml:mi><mml:mi>E</mml:mi><mml:mi>P</mml:mi><mml:mspace width="thinmathspace" /><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:mrow><mml:msub><mml:mi>C</mml:mi><mml:mrow><mml:mn>2</mml:mn><mml:mspace width="thinmathspace" /><mml:mi>S</mml:mi><mml:mi>T</mml:mi><mml:mi>E</mml:mi><mml:mi>P</mml:mi><mml:mspace width="thinmathspace" /><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:mfrac><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>)</mml:mo></mml:mrow></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula></p>
<p>This strategy ensures consistency in the isotropic parameters identified in Step 1 for <italic>&#x03BB;</italic> &#x2264; 1.02, improving at the same time the fitting of the global test curve where the <inline-formula id="ieqn-66"><mml:math id="mml-ieqn-66"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> value has greater importance at high stretch level, adapting the curvature through the exponential term.</p>
<p>In Step 4, the final proposed material parameters are evaluated by computing the determination coefficient (<italic>R</italic><sup>2</sup>), the residual sum of squares (SS<sub>Res</sub>), and the total variance in experimental data (SS<sub>Tot</sub>).</p>
<p>The optimization of the constitutive parameters was performed using a global evolutionary algorithm based on the differential evolution (DE) method, as implemented in the SciPy optimization library. The DE algorithm employed a population-based stochastic search with the default &#x201C;best1bin&#x201D; mutation strategy and binomial crossover scheme. A maximum number of 10,000 iterations was specified, together with a convergence tolerance on the objective function of <inline-formula id="ieqn-67"><mml:math id="mml-ieqn-67"><mml:msup><mml:mn>10</mml:mn><mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mn>9</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>. A fixed random seed (seed &#x003D; 1) was used to ensure reproducibility, and a final local refinement step (&#x201C;polish&#x201D;) was applied to enhance solution accuracy. The cost function was defined as a weighted least-squares error between experimental and model-predicted stresses, incorporating additional physically motivated constraints such as parameter positivity, monotonicity of the stress&#x2013;strain response, and controlled variation between optimization steps. This procedure ensures a stable and physically consistent identification of the model parameters across different deformation regimes.</p>
</sec>
<sec id="s3">
<label>3</label>
<title>Results</title>
<sec id="s3_1">
<label>3.1</label>
<title>Parameters&#x2019; Optimization</title>
<p><xref ref-type="fig" rid="fig-5">Fig. 5</xref> shows the stress&#x2013;stretch response obtained at each stage of the proposed steps parameter calibration methodology, with the respective correlation coefficients (<italic>R</italic><sup>2</sup>) between the theoretical and experimental curves considering data values of an equi-biaxial curve as defined in point 2. In Step 1, the isotropic parameters <inline-formula id="ieqn-68"><mml:math id="mml-ieqn-68"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-69"><mml:math id="mml-ieqn-69"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> were fitted using only the low-deformation region (<inline-formula id="ieqn-70"><mml:math id="mml-ieqn-70"><mml:mi>&#x03BB;</mml:mi></mml:math></inline-formula> &#x2264; 1.02), assuming negligible fiber contribution. In Step 2, <inline-formula id="ieqn-71"><mml:math id="mml-ieqn-71"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-72"><mml:math id="mml-ieqn-72"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> were fixed, and the anisotropic parameters <inline-formula id="ieqn-73"><mml:math id="mml-ieqn-73"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-74"><mml:math id="mml-ieqn-74"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> were optimized over the curve at stretch values greater than the stretch threshold value. In Step 3, a global re-optimization of parameters c<sub>1</sub>, c<sub>2</sub>, k<sub>1,</sub> and k<sub>2,</sub> considering initial values from Step 2 and the global test curve, has been carried out. In all cases, the optimization process is based on the comparison of the test values with the theoretical values calculated.</p>
<fig id="fig-5">
<label>Figure 5</label>
<caption>
<title>Stress-stretch curves correlation to optimize <inline-formula id="ieqn-75"><mml:math id="mml-ieqn-75"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula>, <inline-formula id="ieqn-76"><mml:math id="mml-ieqn-76"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula>, <inline-formula id="ieqn-77"><mml:math id="mml-ieqn-77"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-78"><mml:math id="mml-ieqn-78"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula>.</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMES_82643-fig-5.tif"/>
</fig>
<p>The evolution of the fitted parameters across steps is summarized in <xref ref-type="table" rid="table-2">Table 2</xref>, highlighting the trade-off between isotropic and anisotropic contributions.</p>
<table-wrap id="table-2">
<label>Table 2</label>
<caption>
<title>Estimated HGO material-parameters.</title>
</caption>
<table>
<colgroup>
<col align="center"/>
<col align="center"/>
<col align="center"/>
<col align="center"/>
<col align="center"/>
</colgroup>
<thead>
<tr>
<th>Biaxial Curve (Step)</th>
<th><inline-formula id="ieqn-79"><mml:math id="mml-ieqn-79"><mml:msub><mml:mi mathvariant="bold-italic">c</mml:mi><mml:mrow><mml:mrow><mml:mn mathvariant="bold">1</mml:mn></mml:mrow></mml:mrow></mml:msub></mml:math></inline-formula> (MPa)</th>
<th><inline-formula id="ieqn-80"><mml:math id="mml-ieqn-80"><mml:msub><mml:mi mathvariant="bold-italic">c</mml:mi><mml:mrow><mml:mrow><mml:mn mathvariant="bold">2</mml:mn></mml:mrow></mml:mrow></mml:msub></mml:math></inline-formula> (MPa)</th>
<th><inline-formula id="ieqn-81"><mml:math id="mml-ieqn-81"><mml:msub><mml:mi mathvariant="bold-italic">k</mml:mi><mml:mrow><mml:mrow><mml:mn mathvariant="bold">1</mml:mn></mml:mrow></mml:mrow></mml:msub></mml:math></inline-formula> (MPa)</th>
<th><inline-formula id="ieqn-82"><mml:math id="mml-ieqn-82"><mml:msub><mml:mi mathvariant="bold-italic">k</mml:mi><mml:mrow><mml:mrow><mml:mn mathvariant="bold">2</mml:mn></mml:mrow></mml:mrow></mml:msub></mml:math></inline-formula> (&#x2212;)</th>
</tr>
</thead>
<tbody>
<tr>
<td>Step 1</td>
<td>0.1163</td>
<td>&#x2212;0.0292</td>
<td>&#x2212;</td>
<td>&#x2212;</td>
</tr>
<tr>
<td>Step 2</td>
<td>0.1163</td>
<td>&#x2212;0.0292</td>
<td>0.0845</td>
<td>37.2</td>
</tr>
<tr>
<td>Step 3</td>
<td>0.1069</td>
<td>&#x2212;0.0268</td>
<td>0.0894</td>
<td>36.3</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>Polyconvexity has been checked by comparing the value of sigma in the biaxial state, considering the values of <italic>c</italic><sub>1</sub> and <italic>c</italic><sub>2</sub> calculated in step 1 and step 3 for the isotropic contribution until a value of <italic>&#x03BB;</italic> &#x003D; 1.5 far away from the typical rupture stretch ratio [<xref ref-type="bibr" rid="ref-40">40</xref>] and taking into account that the contribution of the anisotropic component is always positive and increases monotonically. As can be observed in <xref ref-type="fig" rid="fig-6">Fig. 6</xref>.</p>
<fig id="fig-6">
<label>Figure 6</label>
<caption>
<title>Polyconvexity check in the isotropic component.</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMES_82643-fig-6.tif"/>
</fig>
<p>To further assess the quality of the parameter identification and evaluate the fitting performance beyond global indicators, a residual analysis was carried out for each calibration step. <xref ref-type="fig" rid="fig-7">Fig. 7</xref> presents the distribution of residuals along with complementary error metrics, including the coefficient of determination (<inline-formula id="ieqn-83"><mml:math id="mml-ieqn-83"><mml:msup><mml:mi>R</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>), root-mean-square error (RMSE), mean absolute error (MAE), and mean relative error. This combined representation allows a detailed evaluation of both the global agreement and the local discrepancies between experimental data and model predictions across the different deformation regimes.</p>
<fig id="fig-7">
<label>Figure 7</label>
<caption>
<title>Residual distribution and fitting error metrics (<italic>R</italic><sup>2</sup>, RMSE, MAE) for the three-step parameter identification.</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMES_82643-fig-7.tif"/>
</fig>
</sec>
<sec id="s3_2">
<label>3.2</label>
<title>Influence of Curve Origin on Parameter Estimation</title>
<p>In biomechanical testing of soft tissues, it is common for the initial portion of the experimental stress&#x2013;stretch curve to exhibit negligible stress values, even as stretch increases. This apparent lack of initial stress may result from experimental effects such as viscoelastic settling, slack compensation, or imperfect clamping between the sample and grips that can introduce slight movements or deformations without a corresponding internal stress. This means that the stretch ratio begins to increase while the tissue has not yet fully engaged mechanically, making it difficult to precisely identify the true origin of the mechanical response.</p>
<p>To account for this uncertainty, the coordinate system can be shifted to redefine the effective origin, selecting the point at which stress begins to rise consistently above zero. This adjustment allows the removal of non-physical flat regions and improves the accuracy of model fitting.</p>
<p>A representative example of this procedure is shown in <xref ref-type="fig" rid="fig-8">Fig. 8</xref>. A shift in the assumed origin leads to a redistribution of the identified material parameters while preserving an equivalent fitting quality, as evidenced by the identical coefficient of determination obtained in both cases. In particular, the translated configuration results in a reduction of the isotropic contribution, with <inline-formula id="ieqn-84"><mml:math id="mml-ieqn-84"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> decreasing from 0.1069 to 0.0797 MPa and <inline-formula id="ieqn-85"><mml:math id="mml-ieqn-85"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> approaching zero, while the anisotropic parameters increase, with <inline-formula id="ieqn-86"><mml:math id="mml-ieqn-86"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> rising from 0.0894 to 0.1032 MPa and <inline-formula id="ieqn-87"><mml:math id="mml-ieqn-87"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> from 36.3 to 38.5.</p>
<fig id="fig-8">
<label>Figure 8</label>
<caption>
<title>Effect of shifting the curve origin on parameter estimation for biaxial stress&#x2013;stretch data.</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMES_82643-fig-8.tif"/>
</fig>
<p>To assess the physical consistency of these parameter variations, the initial experimental data were analyzed. In the low-strain regime (<inline-formula id="ieqn-88"><mml:math id="mml-ieqn-88"><mml:mn>1.003</mml:mn><mml:mo>&#x2264;</mml:mo><mml:mi>&#x03BB;</mml:mi><mml:mo>&#x2264;</mml:mo><mml:mn>1.021</mml:mn></mml:math></inline-formula>), the stress increases from approximately 0.005 to 0.022 MPa, yielding an estimated initial slope <inline-formula id="ieqn-89"><mml:math id="mml-ieqn-89"><mml:mfrac><mml:mrow><mml:mi>d</mml:mi><mml:mi>&#x03C3;</mml:mi></mml:mrow><mml:mrow><mml:mi>d</mml:mi><mml:mi>&#x03BB;</mml:mi></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mn>0.94</mml:mn></mml:math></inline-formula> MPa under biaxial conditions. Considering that, for a Mooney&#x2013;Rivlin-type response, the biaxial stiffness is approximately twice the uniaxial one, this corresponds to an effective tensile modulus on the order of <inline-formula id="ieqn-90"><mml:math id="mml-ieqn-90"><mml:mi>E</mml:mi><mml:mo>=</mml:mo><mml:mn>0.47</mml:mn></mml:math></inline-formula> MPa.</p>
<p>This value is higher than the typical range reported in the literature for pig corneal tissue [<xref ref-type="bibr" rid="ref-25">25</xref>], suggesting that the experimental curve may already include partial fiber recruitment or residual prestress effects. However, it is important to note that when the anisotropic contribution is neglected, the isotropic stiffness given by <inline-formula id="ieqn-91"><mml:math id="mml-ieqn-91"><mml:mn>6</mml:mn><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mo>&#x2248;</mml:mo><mml:mn>0.48</mml:mn></mml:math></inline-formula> MPa remains close to the expected experimental range, indicating a reasonable agreement with the initial mechanical response. When the term <inline-formula id="ieqn-92"><mml:math id="mml-ieqn-92"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> is included, the effective modulus increases significantly, as reflected in the expression <inline-formula id="ieqn-93"><mml:math id="mml-ieqn-93"><mml:mi>E</mml:mi><mml:mo>=</mml:mo><mml:mn>6</mml:mn><mml:mo stretchy="false">(</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub><mml:mo stretchy="false">)</mml:mo><mml:mo>+</mml:mo><mml:mn>4</mml:mn><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula>. This increase is not necessarily indicative of an actual stiffening of the tissue at very low strains, but rather a consequence of the mathematical formulation, in which the anisotropic term contributes to the tangent stiffness from <inline-formula id="ieqn-94"><mml:math id="mml-ieqn-94"><mml:mi>&#x03BB;</mml:mi><mml:mo>=</mml:mo><mml:mn>1</mml:mn></mml:math></inline-formula>. Physically, collagen fibers are not expected to contribute significantly at the onset of deformation, and therefore this effect may lead to an overestimation of the initial modulus. This limitation could be mitigated by introducing a formulation in which the parameter <inline-formula id="ieqn-95"><mml:math id="mml-ieqn-95"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> evolves with the degree of fiber recruitment, allowing the anisotropic contribution to activate progressively rather than instantaneously. Consequently, while the redistribution between isotropic and anisotropic parameters remains sensitive to the choice of origin, the underlying mechanical response can be interpreted consistently when considering the role of fiber recruitment in the model formulation.</p>
</sec>
<sec id="s3_3">
<label>3.3</label>
<title>Finite Element Analysis Application Case</title>
<p>As an application case, the calculated Holzapfel-Gasser-Ogden (HGO) parameters have been implemented in a patient-specific cornea model submitted to an inflation test considering pivotal boundary conditions [<xref ref-type="bibr" rid="ref-41">41</xref>]. The finite element model has been developed with ANSYS 2023 R1 software (Swanson Analysis System Inc., Houston, PA, USA). The corneal mesh, shown in <xref ref-type="fig" rid="fig-9">Fig. 9</xref>, is based on 20,160 SOLID185 elements distributed radially and circumferentially, with 4 elements across the corneal thickness [<xref ref-type="bibr" rid="ref-41">41</xref>]. A robust fully integrated scheme combined with a (u-p) mixed displacement-pressure formulation has been implemented to ensure robust performance when quasi-incompressible material properties are applied. The application of both techniques enhances numerical stability, improving the solution accuracy, suppressing non-physical deformation modes, and mitigating the volumetric locking.</p>
<fig id="fig-9">
<label>Figure 9</label>
<caption>
<title>Corneal mesh model. Top and side views.</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMES_82643-fig-9.tif"/>
</fig>
<p>The geometrical model is based on the physiological geometry of a healthy cornea (G0) measured with a Sirius corneal topographer [<xref ref-type="bibr" rid="ref-42">42</xref>] (CSO-Costruzione Strumenti Oftalmici, Florence, Italy) and is affected by the influence of the measured intraocular pressure (16 mmHg).</p>
<p>Corneal data, as can be observed in <xref ref-type="table" rid="table-3">Table 3</xref>, were acquired by a single experienced optometrist using the Sirius<sup>&#x00AE;</sup> system (CSO, Florence, Italy). Only scans exhibiting optimal acquisition quality were included in the analysis. The patient was examined at the Vissum Ophthalmological Hospital of Alicante (Spain), and written informed consent was obtained prior to this analysis. The research work adhered to the Declaration of Helsinki (7th revision, Fortaleza, 2013) and received approval from the Ethics Committee of the Polytechnic University of Cartagena (CEI21_001).</p>
<table-wrap id="table-3">
<label>Table 3</label>
<caption>
<title>Summary of the clinical characteristics of the cornea analyzed. Abbreviations: A-K, Amsler-Krumeich criteria; IOP, intraocular pressure (mmHg); 3 km A-K, Mean keratometry in the 3-mm central zone; Eye (OD Right eye, OS Left eye); Axial Length (mm), Sphere (diopters); Cylinder (diopters); SE, spherical equivalent (diopters); CDVA, corrected visual acuity.</title>
</caption>
<table>
<colgroup>
<col align="center"/>
<col align="center"/>
<col align="center"/>
<col align="center"/>
<col align="center"/>
<col align="center"/>
<col align="center"/>
<col align="center"/>
<col align="center"/> </colgroup>
<thead>
<tr>
<th>A-K</th>
<th>IOP</th>
<th>3 km A-K</th>
<th>Eye</th>
<th>Axial Length</th>
<th>Sphere</th>
<th>Cylinder</th>
<th>SE</th>
<th>CDVA</th>
</tr>
</thead>
<tbody>
<tr>
<td>0</td>
<td>16</td>
<td>44.86</td>
<td>OD</td>
<td>23.93</td>
<td>0</td>
<td>0</td>
<td>0</td>
<td>1</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>To consider the influence of intraocular pressure in the real stress field of the cornea, the stress-free geometry must be calculated. In this research, an iterative displacement method [<xref ref-type="bibr" rid="ref-43">43</xref>] is considered. This process ensures that finite-element simulations start from a physically unloaded state and that the predicted deformations and stress fields correspond to realistic physiological conditions. Results are illustrated in <xref ref-type="fig" rid="fig-10">Fig. 10</xref>, where the maximum physiological displacement obtained is 0.244 mm, which agrees with experimentally reported values for healthy corneas at similar pressure levels [<xref ref-type="bibr" rid="ref-10">10</xref>].</p>
<fig id="fig-10">
<label>Figure 10</label>
<caption>
<title>FEA material validation. Stress-free geometry generation and simulated displacement results under IOP &#x003D; 16 mmHg.</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMES_82643-fig-10.tif"/>
</fig>
<p>The model has been submitted to incremental intraocular pressure, as can be observed in <xref ref-type="fig" rid="fig-11">Fig. 11</xref>. The evolution showed a typical non-linear behavior associated with the anisotropic hyperelastic model introduced. Compared with a typical inflation test, the influence of the anisotropic component affects from the beginning of the load application, reducing the non-linear behavior at low intraocular pressure levels. The values reached are in line with the results obtained in other investigations [<xref ref-type="bibr" rid="ref-44">44</xref>].</p>
<fig id="fig-11">
<label>Figure 11</label>
<caption>
<title>Apical rise (mm) evolution depending on the intraocular pressure applied in the posterior zone (mmHg).</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMES_82643-fig-11.tif"/>
</fig>
<p><xref ref-type="fig" rid="fig-12">Fig. 12</xref> shows the distribution map of the stress intensity on the anterior and posterior surfaces of the cornea, respectively. In the posterior surface, a clear directional pattern is observed, where the superior&#x2013;inferior and nasal&#x2013;temporal regions transmit more load toward the limbus. This behaviour is reflected in the cross-shaped green pattern, indicating regions with higher localized stiffness aligned with the predominant collagen fiber directions. The localized high-stress area in the superior cornea is mainly due to the irregularity of limbus associated and constraints influence [<xref ref-type="bibr" rid="ref-45">45</xref>]. In the posterior zone, the maximum stress value is reached at the center with a value close to 20,600 MPa in line with results of other investigations [<xref ref-type="bibr" rid="ref-46">46</xref>].</p>
<fig id="fig-12">
<label>Figure 12</label>
<caption>
<title>Stress intensity (MPa) in anterior (left) and posterior (right) corneal surfaces under IOP &#x003D; 16 mmHg.</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMES_82643-fig-12.tif"/>
</fig>
<p>An estimation of the secant elastic modulus has been obtained by comparing the stress and strain intensity when an intraocular pressure of 16 mmHg is applied, as can be observed in <xref ref-type="fig" rid="fig-13">Fig. 13</xref>. Results showed an average value of 0.42 MPa in the central zone in line with typical values at low stretch ratio.</p>
<fig id="fig-13">
<label>Figure 13</label>
<caption>
<title>Stress intensity/strain intensity distributions (Pa) in anterior (left) and posterior (right) corneal surfaces under IOP &#x003D; 16 mmHg.</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMES_82643-fig-13.tif"/>
</fig>
</sec>
</sec>
<sec id="s4">
<label>4</label>
<title>Discussion</title>
<p>The generation of patient-specific computational models enabling the biomechanical simulation of corneal tissue for clinical and/or surgical purposes can be addressed through finite element formulations that achieve an adequate balance between accuracy and computational cost [<xref ref-type="bibr" rid="ref-45">45</xref>]. This requires constitutive models that account for the anisotropic hyperelastic behavior of the corneal stroma, typically characterized by a large number of parameters whose identification, when relying on a single type of mechanical test, constitutes an ill-posed problem [<xref ref-type="bibr" rid="ref-20">20</xref>], as multiple parameter sets may yield similar responses [<xref ref-type="bibr" rid="ref-19">19</xref>]. Additionally, the wide variety of available constitutive models [<xref ref-type="bibr" rid="ref-47">47</xref>] complicates cross-study comparisons [<xref ref-type="bibr" rid="ref-10">10</xref>,<xref ref-type="bibr" rid="ref-48">48</xref>], making it necessary to establish a common framework that allows the stiffness of the selected material model to be compared while distinguishing the isotropic and anisotropic contributions. This limitation is directly evidenced in the present work, where different parameter sets were found to produce nearly identical stress&#x2013;strain responses, highlighting the intrinsic non-uniqueness of the inverse identification problem even when using a structured multi-step optimization strategy.</p>
<p>Although anisotropic hyperelastic models based on fiber dispersion generally provide superior accuracy [<xref ref-type="bibr" rid="ref-41">41</xref>], their formulation relies on integrating complex functions derived from generalized distributions or from more rigorous patient-specific measurements [<xref ref-type="bibr" rid="ref-2">2</xref>,<xref ref-type="bibr" rid="ref-16">16</xref>], both of which increase the number of variables and the overall complexity of parameter estimation, hindering comparability. This limitation becomes particularly relevant in the present study, where the use of a simplified invariant-based formulation allows a controlled analysis of parameter contributions while still capturing the main nonlinear response.</p>
<p>Xu et al. [<xref ref-type="bibr" rid="ref-49">49</xref>] showed that the dispersion parameter influence can be neglected in the total apical displacement, whereas it is important for corneal aberrations at physiological states. This observation is consistent with the present results, where the anisotropic contribution was found to influence the mechanical response from the very early stages of deformation, despite being traditionally associated with higher stretch levels.</p>
<p>In this context and considering the limited strain range experienced by the cornea under physiological conditions [<xref ref-type="bibr" rid="ref-21">21</xref>], behaving as a membrane subjected to a biaxial loading state, together with its quasi-incompressible nature and the preferential collagen fiber orientation in the central region along the nasal&#x2013;temporal and superior&#x2013;inferior directions [<xref ref-type="bibr" rid="ref-50">50</xref>], supports the use of invariant-based formulations that enable inter-study comparison using simpler and more standardized mechanical tests [<xref ref-type="bibr" rid="ref-24">24</xref>] like uniaxial and equi-biaxial tests. This approach was used in a previous investigation by our research group [<xref ref-type="bibr" rid="ref-19">19</xref>] considering the Holzapfel&#x2013;Gasser&#x2013;Ogden (HGO) model [<xref ref-type="bibr" rid="ref-15">15</xref>]; however, previous studies did not explicitly analyze the individual contribution of each parameter, nor the potential coupling between isotropic and anisotropic components under physiological strain levels, which is addressed in the present work [<xref ref-type="bibr" rid="ref-21">21</xref>].</p>
<p>The analysis of parameter contributions represents a critical aspect in understanding the mechanical response of the cornea. While isotropic and anisotropic components both contribute to the overall stress field, the present results show that the parameter <italic>k</italic><sub>1</sub> influences the response from the early stages of deformation, whereas <italic>k</italic><sub>2</sub> becomes relevant at higher stretch levels, governing the exponential stiffening behavior [<xref ref-type="bibr" rid="ref-49">49</xref>]. However, the residual analysis reveals systematic deviations across the stretch range, indicating that the current HGO formulation does not fully capture the transition between matrix-dominated and fiber-dominated regimes. This suggests that, despite accurate global fitting metrics, the model exhibits limitations in representing the detailed curvature of the experimental response, particularly in intermediate deformation ranges</p>
<p>Pandolfi and Manganiello [<xref ref-type="bibr" rid="ref-10">10</xref>] show different parameter sets based on the application of a Holzapfel Gasser Ogden model to the results of different tests. However, there is a lack of information on the strain rates used in these tests that affect the results obtained [<xref ref-type="bibr" rid="ref-51">51</xref>]. In the present work, the use of consistent experimental datasets [<xref ref-type="bibr" rid="ref-24">24</xref>] and a controlled strain rate [<xref ref-type="bibr" rid="ref-21">21</xref>] allows a more reliable comparison of material parameters, reducing one of the main sources of variability reported in the literature.</p>
<p>Considering the results obtained in this research work, the isotropic contribution, characterized by the shear modulus <inline-formula id="ieqn-97"><mml:math id="mml-ieqn-97"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> &#x002B; <inline-formula id="ieqn-98"><mml:math id="mml-ieqn-98"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> &#x003D; 0.08 MPa for the reference configuration and <inline-formula id="ieqn-99"><mml:math id="mml-ieqn-99"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>0.0797</mml:mn></mml:math></inline-formula> MPa for the translated solution, falls within the range of values reported in recent studies [<xref ref-type="bibr" rid="ref-41">41</xref>] and remains consistent with experimentally measured shear properties of corneal tissue [<xref ref-type="bibr" rid="ref-52">52</xref>]. However, it should be noted that the parameter <inline-formula id="ieqn-100"><mml:math id="mml-ieqn-100"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> takes negative values in the original configuration (<inline-formula id="ieqn-101"><mml:math id="mml-ieqn-101"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mn>0.0268</mml:mn></mml:math></inline-formula> MPa), which may raise concerns regarding material stability. In the present work, this issue has been explicitly addressed by enforcing monotonicity conditions on the isotropic contribution, ensuring that the resulting stress&#x2013;strain response remains physically admissible and strictly increasing over the considered stretch range. The introduction of negative <inline-formula id="ieqn-102"><mml:math id="mml-ieqn-102"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> values is therefore justified as a modelling strategy to improve the fitting accuracy in the low-strain regime, where the experimental response is particularly sensitive to the initial curvature of the stress&#x2013;strain curve.</p>
<p>Nonlinear parameters show differences when compared with other investigations [<xref ref-type="bibr" rid="ref-10">10</xref>,<xref ref-type="bibr" rid="ref-41">41</xref>] that can be attributed to the strain rate implemented in biomechanical tests and the optimization process. Particularly, the nonlinear parameter <inline-formula id="ieqn-103"><mml:math id="mml-ieqn-103"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> &#x003D; 36.3 is notably lower than values reached in other investigations considering inflation tests (200 [<xref ref-type="bibr" rid="ref-41">41</xref>]&#x2013;750 [<xref ref-type="bibr" rid="ref-13">13</xref>]) but remains consistent with values derived from uniaxial or biaxial tests [<xref ref-type="bibr" rid="ref-10">10</xref>]; this result reflects the moderate level of exponential stiffening observed within the physiological strain range, where fiber recruitment is still limited. Additionally, the parameter identification process reveals a strong sensitivity to the reference configuration, as demonstrated by the translated solution, which produces a similar fitting quality (<inline-formula id="ieqn-104"><mml:math id="mml-ieqn-104"><mml:msup><mml:mi>R</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>=</mml:mo><mml:mn>0.991</mml:mn></mml:math></inline-formula>) with a different parameter set. This behaviour confirms the inherent non-uniqueness of the inverse problem, as multiple combinations of <italic>c</italic><sub>1</sub>, <italic>c</italic><sub>2</sub>, <italic>k</italic><sub>1</sub> and <italic>k</italic><sub>2</sub> are able to reproduce the experimental response with comparable accuracy. Furthermore, the reliance on <inline-formula id="ieqn-105"><mml:math id="mml-ieqn-105"><mml:msup><mml:mi>R</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> alone may lead to misleading conclusions regarding model performance, as evidenced by the residual analysis, which reveals systematic deviations across the stretch range despite the high goodness-of-fit values. These findings confirm that additional metrics and qualitative assessments are required to properly evaluate nonlinear constitutive models. The physiological relevance of the identified parameters is supported by previous work from Jan and Sigal [<xref ref-type="bibr" rid="ref-31">31</xref>], who demonstrated that collagen fiber recruitment becomes significant only above intraocular pressure thresholds of approximately 10&#x2013;15 mmHg, corresponding to stretch levels of <inline-formula id="ieqn-106"><mml:math id="mml-ieqn-106"><mml:mi>&#x03BB;</mml:mi><mml:mo>=</mml:mo><mml:mn>1.02</mml:mn></mml:math></inline-formula>, in agreement with thin-shell mechanical models of the cornea subjected to biaxial loading conditions [<xref ref-type="bibr" rid="ref-32">32</xref>].</p>
<p>As an application case, the identified material parameters were implemented in a patient-specific corneal finite element model of a healthy subject. The simulation results produced apical displacement values within the expected physiological range under an intraocular pressure of 16 mmHg, reaching a maximum value of 0.244 mm, in agreement with previous experimental observations in healthy human corneas [<xref ref-type="bibr" rid="ref-13">13</xref>]. The mechanical response is governed by an isotropic contribution characterized by an effective shear modulus <inline-formula id="ieqn-107"><mml:math id="mml-ieqn-107"><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>0.080</mml:mn></mml:math></inline-formula> MPa, which is consistent with reported values for corneal tissue stiffness, ensuring a realistic representation of the initial deformation regime. In terms of stress distribution, the model predicts peak values of approximately 20 kPa in the central region under physiological loading conditions, with a spatial pattern exhibiting clear anatomical alignment with collagen fiber orientations, where preferential load transmission occurs along the nasal&#x2013;temporal and superior&#x2013;inferior directions, in agreement with previous investigations. Additionally, the nonlinear response governed by the anisotropic parameters (<inline-formula id="ieqn-108"><mml:math id="mml-ieqn-108"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-109"><mml:math id="mml-ieqn-109"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula>) leads to a progressive stiffening of the tissue at higher strain levels, although the relatively low values of <inline-formula id="ieqn-110"><mml:math id="mml-ieqn-110"><mml:msub><mml:mi>k</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> reflect a moderate exponential behavior consistent with the physiological deformation range considered. Despite these consistent global results, it should be noted that the parameter identification is not unique, as different parameter sets provide similar displacement and stress fields, highlighting the need for complementary validation metrics and reinforcing the importance of cautious interpretation of model predictions.</p>
<p>Overall, this research proposes a structured and physiologically grounded methodology for corneal parameter identification, combining experimental fitting and computational application within a finite element framework. However, the results also reveal inherent limitations related to parameter non-uniqueness and constitutive model sensitivity, which are not always fully addressed in existing literature. These findings emphasize the necessity of incorporating additional validation tools, such as residual analysis and sensitivity studies, to improve the robustness of biomechanical models. As a natural extension of the present work, future research will focus on the experimental validation of the proposed framework through direct comparison with patient-specific inflation tests and <italic>in vivo</italic> measurements, enabling a more rigorous assessment of the predictive capability of the identified parameters. In addition, further developments will consider the incorporation of advanced constitutive formulations accounting for progressive collagen recruitment and viscoelastic effects, as well as uncertainty quantification strategies to evaluate the robustness of the parameter identification process. These improvements are expected to strengthen the physiological relevance of the model and enhance its applicability in clinically oriented, patient-specific corneal biomechanics simulations.</p>
</sec>
<sec id="s5">
<label>5</label>
<title>Conclusion</title>
<p>This study presents a structured and computationally efficient framework for corneal material parameter identification based on the HGO hyperelastic formulation, enabling the consistent integration of uniaxial and biaxial experimental data through a multi-step calibration strategy. The introduction of a strain threshold allows the separation of matrix- and fiber-dominated mechanical regimes, providing a stable and accurate representation of the corneal response within the physiological deformation range, including the early contribution of anisotropic components and the progressive nonlinear stiffening associated with collagen fiber recruitment. The identified material parameters yield shear moduli and stress&#x2013;strain responses consistent with reported corneal biomechanics, and their implementation in a patient-specific finite element model produces physiologically realistic displacement and stress distributions aligned with collagen fiber architecture. These results demonstrate the capability of the proposed methodology to support reliable <italic>in silico</italic> simulations and enhance inter-study comparability. Moreover, the framework offers a solid basis for future advancements, including the incorporation of microstructure-informed formulations, refined constitutive models accounting for fiber recruitment and dispersion, and uncertainty quantification strategies, thereby strengthening its applicability for both physiological analysis and patient-specific clinical applications in corneal biomechanics.</p>
</sec>
</body>
<back>
<ack>
<p>Not applicable.</p>
</ack>
<sec>
<title>Funding Statement</title>
<p>This work was supported by the Fundaci&#x00F3;n S&#x00E9;neca&#x2013;Agencia de Ciencia y Tecnolog&#x00ED;a de la Regi&#x00F3;n de Murcia (Spain) through research project 22665/PI/24. The study was also conducted in collaboration with the Association for the Integration of Disabled People in the Comarca del Mar Menor (AIDEMAR) under the UPCT&#x2013;AIDEMAR collaboration agreement.</p>
</sec>
<sec>
<title>Author Contributions</title>
<p>Conceptualization: Jos&#x00E9; Gonz&#x00E1;lez-Cabrero, Carmelo G&#x00F3;mez and Francisco Cavas; methodology: Jos&#x00E9; Gonz&#x00E1;lez-Cabrero, Carmelo G&#x00F3;mez and Francisco Cavas; software: Jos&#x00E9; Gonz&#x00E1;lez-Cabrero and Carmelo G&#x00F3;mez; validation: Carmelo G&#x00F3;mez and Manuel Paredes; formal analysis: Jos&#x00E9; Gonz&#x00E1;lez-Cabrero, Carmelo G&#x00F3;mez and Manuel Paredes; investigation: Jos&#x00E9; Gonz&#x00E1;lez-Cabrero, Carmelo G&#x00F3;mez and Francisco Cavas; resources: Manuel Paredes; data curation: Jos&#x00E9; Gonz&#x00E1;lez-Cabrero, Manuel Paredes and Carmelo G&#x00F3;mez; writing&#x2014;original draft preparation: Jos&#x00E9; Gonz&#x00E1;lez-Cabrero, Carmelo G&#x00F3;mez, Manuel Paredes, and Francisco Cavas; writing&#x2014;review and editing: Carmelo G&#x00F3;mez, Manuel Paredes and Francisco Cavas; visualization: Manuel Paredes and Francisco Cavas; supervision: Manuel Paredes and Francisco Cavas; project administration: Jos&#x00E9; Gonz&#x00E1;lez-Cabrero, Carmelo G&#x00F3;mez and Francisco Cavas; funding acquisition: Carmelo G&#x00F3;mez and Francisco Cavas. All authors reviewed and approved the final version of the manuscript.</p>
</sec>
<sec sec-type="data-availability">
<title>Availability of Data and Materials</title>
<p>The data that support the findings of this study are available from the corresponding author, Francisco Cavas, upon reasonable request.</p>
</sec>
<sec>
<title>Ethics Approval</title>
<p>The study was conducted in accordance with the principles of the Declaration of Helsinki and was approved by the Ethics Committee of the Polytechnic University of Cartagena, Spain (approval code: CEI21_001).</p>
</sec>
<sec sec-type="COI-statement">
<title>Conflicts of Interest</title>
<p>The authors declare no conflicts of interest.</p>
</sec>
<ref-list content-type="authoryear">
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