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<front>
<journal-meta>
<journal-id journal-id-type="pmc">CMC</journal-id>
<journal-id journal-id-type="nlm-ta">CMC</journal-id>
<journal-id journal-id-type="publisher-id">CMC</journal-id>
<journal-title-group>
<journal-title>Computers, Materials &#x0026; Continua</journal-title>
</journal-title-group>
<issn pub-type="epub">1546-2226</issn>
<issn pub-type="ppub">1546-2218</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">76418</article-id>
<article-id pub-id-type="doi">10.32604/cmc.2026.076418</article-id>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Article</subject>
</subj-group>
</article-categories>
<title-group>
<article-title>Physics-Informed Neural Networks for Bending Analysis of Graphene Origami-Enabled Auxetic Metamaterial Beams Based on Modified Coupled Stress Theory</article-title>
<alt-title alt-title-type="left-running-head">Physics-Informed Neural Networks for Bending Analysis of Graphene Origami-Enabled Auxetic Metamaterial Beams Based on Modified Coupled Stress Theory</alt-title>
<alt-title alt-title-type="right-running-head">Physics-Informed Neural Networks for Bending Analysis of Graphene Origami-Enabled Auxetic Metamaterial Beams Based on Modified Coupled Stress Theory</alt-title>
</title-group>
<contrib-group>
<contrib id="author-1" contrib-type="author" corresp="yes">
<name name-style="western"><surname>Zhu</surname><given-names>Zuoquan</given-names></name><xref rid="cor1" ref-type="corresp">&#x002A;</xref><email>zuoquanzhu@zznu.edu.cn</email></contrib>
<contrib id="author-2" contrib-type="author">
<name name-style="western"><surname>Wang</surname><given-names>Menghan</given-names></name></contrib>
<contrib id="author-3" contrib-type="author">
<name name-style="western"><surname>Li</surname><given-names>Xinyu</given-names></name></contrib>
<contrib id="author-4" contrib-type="author">
<name name-style="western"><surname>Zhao</surname><given-names>Mengxin</given-names></name></contrib>
<aff id="aff-1">
<institution>School of Mathematics and Statistics, Zhengzhou Normal University</institution>, <addr-line>Zhengzhou</addr-line>, <country>China</country></aff>
</contrib-group>
<author-notes>
<corresp id="cor1"><label>&#x002A;</label>Corresponding Author: Zuoquan Zhu. Email: <email>zuoquanzhu@zznu.edu.cn</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>9</day><month>4</month><year>2026</year>
</pub-date>
<volume>87</volume>
<issue>3</issue>
<elocation-id>25</elocation-id>
<history>
<date date-type="received">
<day>20</day>
<month>11</month>
<year>2025</year>
</date>
<date date-type="accepted">
<day>20</day>
<month>01</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_CMC_76418.pdf"></self-uri>
<abstract>
<p>Investigating the deformation behavior of graphene-reinforced composite structures holds significant engineering implications, while the rapid advancement of machine learning has introduced new technical approaches to structural bending analysis. In this study, we investigate the mechanical bending behavior of graphene origami (GOri)-enabled auxetic metamaterial beams using a physics-informed neural network (PINN). GOri-enabled auxetic metamaterials represent an innovative composite system characterized by a negative Poisson&#x2019;s ratio (NPR) and superior mechanical performance. Here, we propose a composite beam model incorporating the modified coupled stress theory (MCST) and employing the PINN method to solve higher-order bending governing equations. Compared to the analytical solution, the accuracy and effectiveness of the PINN framework as a meshless solver for higher-order partial differential equations are verified. The bending properties of metamaterial beams are studied by considering the mechanical properties and size effect of metamaterials. It was found that the length scale parameters, more graphene platelets, and a higher folding degree have the best reinforcement effect on composite beams. By systematically varying the GOri folding parameters and graphene content, we demonstrate the robustness of the PINN methodology in resolving microscale beam bending phenomena, particularly in capturing complex size-effect interactions.</p>
</abstract>
<kwd-group kwd-group-type="author">
<kwd>Physics-informed neural networks</kwd>
<kwd>graphene origami</kwd>
<kwd>mechanical metamaterial</kwd>
<kwd>folding degrees</kwd>
<kwd>bending analysis</kwd>
</kwd-group>
<funding-group>
<award-group id="awg1">
<funding-source>Natural Science Foundation of Henan</funding-source>
<award-id>252300420935</award-id>
</award-group>
<award-group id="awg2">
<funding-source>Young Backbone Teacher Training Program of Zhengzhou Normal University</funding-source>
<award-id>QNGG-232300</award-id>
</award-group>
<award-group id="awg3">
<funding-source>Zhengzhou Normal University Undergraduate Innovation and Entrepreneurship Training Program Project</funding-source>
<award-id>DCY2024011</award-id>
</award-group>
<award-group id="awg4">
<funding-source>Scientific Research Starting Foundation of Zhengzhou Normal University</funding-source>
<award-id>2021-702442</award-id>
</award-group>
</funding-group>
</article-meta>
</front>
<body>
<sec id="s1">
<label>1</label>
<title>Introduction</title>
<p>In recent years, there has been growing interest in nanotechnology. Nanomaterials and nanostructures are used to manufacture micro-electromechanical and nanoelectromechanical systems, which are widely used in the fields of machinery, aerospace, electronics, and biomedical engineering. Micro-nano scale systems, including biosensors, electrochemical actuators, supercapacitors, nanotubes, and nanoprobes, predominantly use nanorods, nanobeams, nanoplates, and nanoshells as fundamental structural units [<xref ref-type="bibr" rid="ref-1">1</xref>&#x2013;<xref ref-type="bibr" rid="ref-4">4</xref>]. Subsequently, advanced composites, such as functionally graded materials and graphene-based reinforced composites, have been developed, which have attracted scientists to establish mechanical models for their analysis. Among them, as a typical representative of the gradient structure, the mechanical behavior of mechanical metamaterial composite beams with a negative Poisson&#x2019;s ratio effect has attracted increasing attention from scholars.</p>
<p>Numerous experiments and theoretical studies have been conducted to effectively analyze and design metamaterial composite structures to characterize the mechanical behavior of the nanostructures. Zhao et al. unveiled the mechanism of a highly tunable negative Poisson&#x2019;s ratio and developed micromechanical models based on genetic programming for the accelerated prediction of mechanical properties in GOri-based metallic metamaterials [<xref ref-type="bibr" rid="ref-5">5</xref>,<xref ref-type="bibr" rid="ref-6">6</xref>]. They then developed a model for the first time to study the bending [<xref ref-type="bibr" rid="ref-7">7</xref>], buckling, and postbuckling properties [<xref ref-type="bibr" rid="ref-8">8</xref>]. Their findings indicated that graphene origami can significantly influence the buckling and postbuckling behavior of metamaterial composite beams. Karami and Ghayesh [<xref ref-type="bibr" rid="ref-9">9</xref>] investigated the dynamics of auxetic metamaterials using various shear deformation theories. Ezzati et al. [<xref ref-type="bibr" rid="ref-10">10</xref>] and Ebrahimi and Ahari [<xref ref-type="bibr" rid="ref-11">11</xref>] investigated the free vibration behavior and vibration control of a graphene origami auxetic beam. Ebrahimi and Parsi [<xref ref-type="bibr" rid="ref-12">12</xref>] revealed the elastic wave characteristics of functionally graded graphene origami-reinforced metamaterial beams. Recently, several papers have been published on the thermal-mechanical coupling behavior of functionally graded graphene origami-enabled metamaterials [<xref ref-type="bibr" rid="ref-13">13</xref>]. On the other hand, certain experimental studies have proven the significance of the material microstructure and long-range interaction force on the mechanical response of micro-and nanostructured components [<xref ref-type="bibr" rid="ref-14">14</xref>&#x2013;<xref ref-type="bibr" rid="ref-16">16</xref>]. Classical continuum theory cannot describe these small-scale effects well, but is widely used in macro-level structural modeling. Among the different modeling possibilities, one feasible method is to provide the so-called nonlocal continuum theory by directly modifying the classical theory. Over the years, researchers have proposed several non-local theories. The theories of stress gradient, strain gradient, and even integral type [<xref ref-type="bibr" rid="ref-17">17</xref>&#x2013;<xref ref-type="bibr" rid="ref-20">20</xref>] provide some classic examples in which the small-scale effect is considered by introducing one or more internal length scale parameters. When structural dimensions are at the micrometer/nanometer scale, microscopic effects become particularly significant, especially for the study of size effects in graphene origami-enhanced microstructures.</p>
<p>In addition, advanced computational methods have significantly expanded the analytical capabilities of metamaterial composite systems. Neural networks, particularly deep-learning frameworks, have emerged as powerful tools in engineering disciplines such as materials science [<xref ref-type="bibr" rid="ref-21">21</xref>], solid mechanics [<xref ref-type="bibr" rid="ref-22">22</xref>], and fluid mechanics [<xref ref-type="bibr" rid="ref-23">23</xref>]. In the above research, the data-driven method was mainly used to minimize the error norm between network prediction and real data (training data) to train the model parameters [<xref ref-type="bibr" rid="ref-24">24</xref>]. However, their reliance on empirical correlations often limits their physical interpretability, and large-scale datasets are required for reliable predictions. To address these limitations, PINNs have gained traction by integrating governing differential equations into the learning process [<xref ref-type="bibr" rid="ref-25">25</xref>]. This framework introduces loss functions that enforce boundary conditions and conservation laws, thereby enabling the extraction of physics-compliant solutions without exhaustive data requirements. PINNs have been successfully applied to solve complex partial differential equations in fluid dynamics (e.g., Navier-Stokes equation [<xref ref-type="bibr" rid="ref-26">26</xref>]), phase transition phenomena (Cahn-Hilliard and Allen-Cahn equation [<xref ref-type="bibr" rid="ref-27">27</xref>]), and heat transfer processes [<xref ref-type="bibr" rid="ref-28">28</xref>]. In the field of solid mechanics, PINNs have demonstrated potential for modeling mechanical behaviors. For instance, Xue et al. [<xref ref-type="bibr" rid="ref-29">29</xref>] incorporated two loss functions, mass transfer and stress field, and used them to numerically obtain the solution of diffusion stress in an elastic sphere. Fallah and Aghdam [<xref ref-type="bibr" rid="ref-30">30</xref>] applied PINNs to study the bending and free vibration characteristics of three-dimensional functionally graded porous beams. Kianian et al. [<xref ref-type="bibr" rid="ref-31">31</xref>] extended the PINN approach to model the static bending response of micro/nanoelectromechanical systems. Moreover, Bazmara et al. [<xref ref-type="bibr" rid="ref-32">32</xref>] proposed an NN framework based on physical information to predict the nonlinear buckling behavior of 3D functionally graded (FG) porous beams on elastic foundations. These studies highlight PINN&#x2019;s ability to handle higher-order differential equations and achieve close agreement with the numerical solutions. However, PINN is rarely used to solve the mechanical behavior of graphene origami composite beams, considering the size effect.</p>
<p>The key contributions of this work are as follows: On the one hand, a large body of scholarly work has employed PINN to investigate the bending behavior of functionally graded material (FGM) nanobeams and nanoplates. These studies typically rely on small-scale theories, such as the strain gradient theory and nonlocal elasticity theory, yet their research focus remains confined to traditional functionally graded materials rather than mechanical metamaterials. However, some scholars have applied PINN to analyze the bending or buckling responses [<xref ref-type="bibr" rid="ref-33">33</xref>] of origami metamaterial composite beams/plates; the critical factor of the size effect has been overlooked in their investigations. Against this backdrop, this study addresses the bending problem of beams subjected to the combined influence of the size effect and metamaterial characteristics. Since the differential equations incorporate physical information, only the loss associated with boundary conditions needs to be considered during model training, eliminating the need for mesh partitioning and effectively improving computational efficiency. By employing both numerical methods and mesh-free PINN methods for parallel solution, this study aims to contribute to the advancement of research in this field.</p>
<p>In this study, a physics-informed neural network was used to analyze the bending behavior of graphene origami-reinforced metamaterial beams. The governing equation, a fourth-order differential equation with variable coefficients, was combined with the boundary conditions formulated using Hamilton&#x2019;s principle. A deep feedforward neural network is constructed to approximate the beam bending deflection. Its parameters are optimized by minimizing a composite loss function that forces both the governing equations and boundary constraints. To validate the proposed approach, PINN predictions were compared against available analytical solutions. The convergence and accuracy of the PINN in predicting deflections under different boundary conditions were studied. Then, the influence of the graphene origami content, distribution, and size parameter on the deflection of graphene origami-reinforced metamaterial beams is investigated.</p>
</sec>
<sec id="s2">
<label>2</label>
<title>Mathematical Formulations</title>
<sec id="s2_1">
<label>2.1</label>
<title>Effective Material Properties</title>
<p>Consider a functionally graded graphene origami/Sn (GOri/Sn) composite microbeam with a rectangular cross-section. The microbeam had a length <inline-formula id="ieqn-1"><mml:math id="mml-ieqn-1"><mml:mi>L</mml:mi></mml:math></inline-formula>, height <inline-formula id="ieqn-2"><mml:math id="mml-ieqn-2"><mml:mi>h</mml:mi></mml:math></inline-formula>, and width <inline-formula id="ieqn-3"><mml:math id="mml-ieqn-3"><mml:mi>b</mml:mi></mml:math></inline-formula>, as schematically depicted in <xref ref-type="fig" rid="fig-1">Fig. 1</xref>. The rectangular Cartesian coordinate axes used to study infinitesimal bending deformations are also shown in the figure. Here, the neutral surface of the beam lies in the x-y plane, and the positive <italic>z</italic>-axis points upward along the thickness direction. The beam material was assumed isotropic and linearly elastic. Moreover, this study extends the application of the machine-learning-based method to the bending analysis of microbeams using PINN.</p>
<fig id="fig-1">
<label>Figure 1</label>
<caption>
<title>(<bold>a</bold>) The geometry and cross-section of the GOri/Sn composite beam. (<bold>b</bold>) Schematic of PINN framework for beam bending analysis.</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_76418-fig-1.tif"/>
</fig>
<p>The elastic modulus (<inline-formula id="ieqn-4"><mml:math id="mml-ieqn-4"><mml:msub><mml:mi>E</mml:mi><mml:mrow><mml:mi>e</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>), Poisson&#x2019;s ratio (<inline-formula id="ieqn-5"><mml:math id="mml-ieqn-5"><mml:msub><mml:mi>&#x03BD;</mml:mi><mml:mrow><mml:mi>e</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>), and density (<inline-formula id="ieqn-6"><mml:math id="mml-ieqn-6"><mml:msub><mml:mi>&#x03C1;</mml:mi><mml:mrow><mml:mi>e</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>) of the materials were determined using a micromechanical model assisted by genetic programming (GP), as proposed by Zhao et al. [<xref ref-type="bibr" rid="ref-5">5</xref>,<xref ref-type="bibr" rid="ref-6">6</xref>]
<disp-formula id="eqn-1"><label>(1)</label><mml:math id="mml-eqn-1" display="block"><mml:mtable columnalign="left" rowspacing="4pt" columnspacing="1em"><mml:mtr><mml:mtd><mml:msub><mml:mi>E</mml:mi><mml:mrow><mml:mi>e</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mrow><mml:mn>1</mml:mn><mml:mo>+</mml:mo><mml:mi>&#x03BE;</mml:mi><mml:mi>&#x03B7;</mml:mi><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mn>1</mml:mn><mml:mo>&#x2212;</mml:mo><mml:mi>&#x03B7;</mml:mi><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mfrac></mml:mstyle><mml:msub><mml:mi>E</mml:mi><mml:mrow><mml:mi>S</mml:mi><mml:mi>n</mml:mi></mml:mrow></mml:msub><mml:mo>&#x00D7;</mml:mo><mml:msub><mml:mi>f</mml:mi><mml:mrow><mml:mi>E</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>T</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:msub><mml:mi>v</mml:mi><mml:mrow><mml:mi>e</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>v</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>v</mml:mi><mml:mrow><mml:mi>S</mml:mi><mml:mi>n</mml:mi></mml:mrow></mml:msub><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>S</mml:mi><mml:mi>n</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mo>&#x00D7;</mml:mo><mml:msub><mml:mi>f</mml:mi><mml:mrow><mml:mi>v</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>T</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:msub><mml:mi>&#x03C1;</mml:mi><mml:mrow><mml:mi>e</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>&#x03C1;</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>&#x03C1;</mml:mi><mml:mrow><mml:mi>S</mml:mi><mml:mi>n</mml:mi></mml:mrow></mml:msub><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>S</mml:mi><mml:mi>n</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mo>&#x00D7;</mml:mo><mml:msub><mml:mi>f</mml:mi><mml:mrow><mml:mi>&#x03C1;</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>T</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula></p>
<p>The coefficients for material (<inline-formula id="ieqn-7"><mml:math id="mml-ieqn-7"><mml:mi>&#x03B7;</mml:mi></mml:math></inline-formula>) and size (<inline-formula id="ieqn-8"><mml:math id="mml-ieqn-8"><mml:mi>&#x03BE;</mml:mi></mml:math></inline-formula>) are outlined below:
<disp-formula id="eqn-2"><label>(2)</label><mml:math id="mml-eqn-2" display="block"><mml:mi>&#x03B7;</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>E</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:msub><mml:mi>E</mml:mi><mml:mrow><mml:mi>S</mml:mi><mml:mi>n</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mn>1</mml:mn></mml:mrow><mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>E</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:msub><mml:mi>E</mml:mi><mml:mrow><mml:mi>S</mml:mi><mml:mi>n</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mi>&#x03BE;</mml:mi></mml:mrow></mml:mfrac><mml:mo>,</mml:mo><mml:mi>&#x03BE;</mml:mi><mml:mo>=</mml:mo><mml:mn>2</mml:mn><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>l</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:math></disp-formula>where <inline-formula id="ieqn-9"><mml:math id="mml-ieqn-9"><mml:msub><mml:mi>l</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-10"><mml:math id="mml-ieqn-10"><mml:msub><mml:mi>t</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> denote the length and thickness of the graphene, respectively. The transformation functions, <inline-formula id="ieqn-11"><mml:math id="mml-ieqn-11"><mml:msub><mml:mi>f</mml:mi><mml:mrow><mml:mi>E</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>T</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>,</mml:mo></mml:math></inline-formula><inline-formula id="ieqn-12"><mml:math id="mml-ieqn-12"><mml:msub><mml:mi>f</mml:mi><mml:mrow><mml:mi>v</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>T</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and <inline-formula id="ieqn-13"><mml:math id="mml-ieqn-13"><mml:msub><mml:mi>f</mml:mi><mml:mrow><mml:mi>&#x03C1;</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>T</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>were derived using the GP algorithm developed by Zhao et al. [<xref ref-type="bibr" rid="ref-5">5</xref>,<xref ref-type="bibr" rid="ref-6">6</xref>]</p>
<p><disp-formula id="eqn-3a"><label>(3a)</label><mml:math id="mml-eqn-3a" 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:msub><mml:mi>f</mml:mi><mml:mi>E</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mrow><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mo>,</mml:mo><mml:mrow><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mo>,</mml:mo><mml:mi>T</mml:mi></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:mn>1.11</mml:mn><mml:mo>&#x2212;</mml:mo><mml:mn>1.22</mml:mn><mml:mrow><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mn>0.134</mml:mn><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mfrac><mml:mi>T</mml:mi><mml:mrow><mml:mrow><mml:msub><mml:mi>T</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mn>0.559</mml:mn><mml:mrow><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mfrac><mml:mi>T</mml:mi><mml:mrow><mml:mrow><mml:msub><mml:mi>T</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow><mml:mo>)</mml:mo></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mrow><mml:mtext>&#xA0;</mml:mtext></mml:mrow></mml:mtd><mml:mtd><mml:mi></mml:mi><mml:mspace width="1em" /><mml:mspace width="1em" /><mml:mspace width="1em" /><mml:mspace width="1em" /><mml:mspace width="1em" /><mml:mspace width="1em" /><mml:mspace width="1em" /><mml:mo>&#x2212;</mml:mo><mml:mn>5.5</mml:mn><mml:mrow><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mo>+</mml:mo><mml:mn>38</mml:mn><mml:mrow><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:msubsup><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow><mml:mn>2</mml:mn></mml:msubsup><mml:mo>&#x2212;</mml:mo><mml:mn>20.6</mml:mn><mml:msubsup><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow><mml:mn>2</mml:mn></mml:msubsup><mml:msubsup><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow><mml:mn>2</mml:mn></mml:msubsup></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<disp-formula id="eqn-3b"><label>(3b)</label><mml:math id="mml-eqn-3b" 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:msub><mml:mi>f</mml:mi><mml:mi>v</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mrow><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mo>,</mml:mo><mml:mrow><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mo>,</mml:mo><mml:mi>T</mml:mi></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:mn>1.01</mml:mn><mml:mo>&#x2212;</mml:mo><mml:mn>1.43</mml:mn><mml:mrow><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mo>+</mml:mo><mml:mn>0.165</mml:mn><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mfrac><mml:mi>T</mml:mi><mml:mrow><mml:mrow><mml:msub><mml:mi>T</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mn>16.8</mml:mn><mml:mrow><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mn>1.1</mml:mn><mml:mrow><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mfrac><mml:mi>T</mml:mi><mml:mrow><mml:mrow><mml:msub><mml:mi>T</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mn>16</mml:mn><mml:msubsup><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow><mml:mn>2</mml:mn></mml:msubsup><mml:msubsup><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow><mml:mn>2</mml:mn></mml:msubsup></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<disp-formula id="eqn-3c"><label>(3c)</label><mml:math id="mml-eqn-3c" 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:msub><mml:mi>f</mml:mi><mml:mi>&#x03C1;</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mrow><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mo>,</mml:mo><mml:mi>T</mml:mi></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:mn>1.01</mml:mn><mml:mo>&#x2212;</mml:mo><mml:mn>2.01</mml:mn><mml:msubsup><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow><mml:mn>2</mml:mn></mml:msubsup><mml:mo>&#x2212;</mml:mo><mml:mn>0.0131</mml:mn><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mfrac><mml:mi>T</mml:mi><mml:mrow><mml:mrow><mml:msub><mml:mi>T</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow><mml:mo>)</mml:mo></mml:mrow></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula></p>
<p>With the temperature <inline-formula id="ieqn-14"><mml:math id="mml-ieqn-14"><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> set at 300 K, the current ambient temperature can be confidently represented as <inline-formula id="ieqn-15"><mml:math id="mml-ieqn-15"><mml:mi>T</mml:mi></mml:math></inline-formula>. Because the influence of temperature was not considered in this study, we assumed that the temperature remained <inline-formula id="ieqn-16"><mml:math id="mml-ieqn-16"><mml:mi>T</mml:mi><mml:mo>=</mml:mo><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula>. The volume fractions <inline-formula id="ieqn-17"><mml:math id="mml-ieqn-17"><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:mi>k</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> of the <italic>k</italic>th layer for two graphene content distribution are considered. On one hand, the surface layers are GOri rich while the middle layer is poor in the <inline-formula id="ieqn-18"><mml:math id="mml-ieqn-18"><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> beam, <inline-formula id="ieqn-19"><mml:math id="mml-ieqn-19"><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:mi>k</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:mn>2</mml:mn><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>|</mml:mo><mml:mn>2</mml:mn><mml:mi>k</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>N</mml:mi><mml:mrow><mml:mi>L</mml:mi></mml:mrow></mml:msub><mml:mo>&#x2212;</mml:mo><mml:mn>1</mml:mn><mml:mo>|</mml:mo></mml:mrow><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:msub><mml:mi>N</mml:mi><mml:mrow><mml:mi>L</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> in which <inline-formula id="ieqn-20"><mml:math id="mml-ieqn-20"><mml:mi>k</mml:mi><mml:mo>=</mml:mo><mml:mn>1</mml:mn><mml:mo>,</mml:mo><mml:mn>2</mml:mn><mml:mo>,</mml:mo><mml:mo>&#x22C5;</mml:mo><mml:mo>&#x22C5;</mml:mo><mml:mo>&#x22C5;</mml:mo><mml:mo>,</mml:mo><mml:msub><mml:mi>N</mml:mi><mml:mrow><mml:mi>L</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> (<inline-formula id="ieqn-21"><mml:math id="mml-ieqn-21"><mml:msub><mml:mi>N</mml:mi><mml:mrow><mml:mi>L</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>: total layer number) [<xref ref-type="bibr" rid="ref-34">34</xref>&#x2013;<xref ref-type="bibr" rid="ref-36">36</xref>]. On the other hand, the GOri content is the same in each layer in a <inline-formula id="ieqn-22"><mml:math id="mml-ieqn-22"><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> beam, <inline-formula id="ieqn-23"><mml:math id="mml-ieqn-23"><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:mi>k</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:msub><mml:mi>V</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>.</p>
<p>At the same time, the H coverage <inline-formula id="ieqn-24"><mml:math id="mml-ieqn-24"><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:mi>z</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> with uniform distribution <inline-formula id="ieqn-25"><mml:math id="mml-ieqn-25"><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> and non-uniform distribution <inline-formula id="ieqn-26"><mml:math id="mml-ieqn-26"><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> along the thickness direction is governed by
<disp-formula id="ueqn-24"><label>( 4a)</label><mml:math id="mml-ueqn-24" 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:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>:</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:mi>z</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mtd><mml:mtd><mml:mi></mml:mi><mml:mo>=</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<disp-formula id="eqn-4b"><label>(4b)</label><mml:math id="mml-eqn-4b" 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:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>:</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:mi>z</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mtd><mml:mtd><mml:mi></mml:mi><mml:mo>=</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mi>cos</mml:mi><mml:mo>&#x2061;</mml:mo><mml:mrow><mml:mo>(</mml:mo><mml:mi>z</mml:mi><mml:mi>&#x03C0;</mml:mi><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mi>h</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula></p>
<p>Taking the four distribution scenarios as an example, the effective Poisson&#x2019;s ratio <inline-formula id="ieqn-27"><mml:math id="mml-ieqn-27"><mml:msub><mml:mi>&#x03BD;</mml:mi><mml:mrow><mml:mi>e</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> of the GOri/Sn composite beam, as a function of the GOri parameter model, is graphically presented in <xref ref-type="fig" rid="fig-2">Fig. 2</xref>. <xref ref-type="fig" rid="fig-2">Fig. 2</xref> depicts the effective Poisson&#x2019;s ratio distribution of the graphene origami-reinforced composite beams along the thickness direction. With an increase in the GOri content and folding degree, the GOri/Sn composite beam shows an auxetic effect (i.e., the Poisson&#x2019;s ratio is less than zero). In the subsequent discussion, we explore the bending behavior of composite beams with auxetic effects caused by the graphene origami content and folding degree. In addition, a similar phenomenon of graphene origami composite structure patterns with different layers and non-uniform distribution can be found in [<xref ref-type="bibr" rid="ref-34">34</xref>,<xref ref-type="bibr" rid="ref-35">35</xref>].</p>
<fig id="fig-2">
<label>Figure 2</label>
<caption>
<title>The variation of Poisson&#x2019;s ratio for GOri/Sn composite beam for different composite patterns: (<bold>a</bold>) <inline-formula id="ieqn-28"><mml:math id="mml-ieqn-28"><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>; (<bold>b</bold>) <inline-formula id="ieqn-29"><mml:math id="mml-ieqn-29"><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>; (<bold>c</bold>) <inline-formula id="ieqn-30"><mml:math id="mml-ieqn-30"><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>; (<bold>d</bold>) <inline-formula id="ieqn-31"><mml:math id="mml-ieqn-31"><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>.</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_76418-fig-2a.tif"/>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_76418-fig-2b.tif"/>
</fig>
</sec>
<sec id="s2_2">
<label>2.2</label>
<title>Modified Couple Stress Theory</title>
<p>Based on the modified coupled stress theory [<xref ref-type="bibr" rid="ref-37">37</xref>], the strain energy <inline-formula id="ieqn-32"><mml:math id="mml-ieqn-32"><mml:mi>U</mml:mi></mml:math></inline-formula> of an isotropic elastic material in the domain <inline-formula id="ieqn-33"><mml:math id="mml-ieqn-33"><mml:mrow><mml:mi mathvariant="normal">&#x03A9;</mml:mi></mml:mrow></mml:math></inline-formula> can be formulated as follows
<disp-formula id="eqn-5"><label>(5)</label><mml:math id="mml-eqn-5" display="block"><mml:mi>U</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:mn>2</mml:mn></mml:mfrac><mml:msub><mml:mo>&#x222B;</mml:mo><mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x03A9;</mml:mi></mml:mrow></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:mi mathvariant="bold-italic">&#x03C3;</mml:mi><mml:mo>&#x003A;</mml:mo><mml:mi mathvariant="bold-italic">&#x03B5;</mml:mi><mml:mo>+</mml:mo><mml:mrow><mml:mtext mathvariant="bold">m</mml:mtext></mml:mrow><mml:mo>&#x003A;</mml:mo><mml:mi mathvariant="bold-italic">&#x03C7;</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mtext>d</mml:mtext></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x03A9;</mml:mi></mml:mrow></mml:math></disp-formula>where <inline-formula id="ieqn-34"><mml:math id="mml-ieqn-34"><mml:mi mathvariant="bold-italic">&#x03C3;</mml:mi></mml:math></inline-formula>, <inline-formula id="ieqn-35"><mml:math id="mml-ieqn-35"><mml:mi mathvariant="bold-italic">&#x03B5;</mml:mi></mml:math></inline-formula>, <inline-formula id="ieqn-36"><mml:math id="mml-ieqn-36"><mml:mrow><mml:mtext mathvariant="bold">m</mml:mtext></mml:mrow></mml:math></inline-formula>, and <inline-formula id="ieqn-37"><mml:math id="mml-ieqn-37"><mml:mi mathvariant="bold-italic">&#x03C7;</mml:mi></mml:math></inline-formula> represent the Cauchy stress tensor, strain tensor, deviatoric part of the couple stress tensor, and symmetric curvature tensor, respectively. The tensors are defined as follows:
<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:mrow><mml:mi mathvariant="bold-italic">&#x03C3;</mml:mi></mml:mrow></mml:mtd><mml:mtd><mml:mi></mml:mi><mml:mo>=</mml:mo><mml:mi>&#x03BB;</mml:mi><mml:mi>t</mml:mi><mml:mi>r</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi mathvariant="bold-italic">&#x03B5;</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mtext mathvariant="bold">I</mml:mtext></mml:mrow><mml:mo>+</mml:mo><mml:mn>2</mml:mn><mml:mi>&#x03BC;</mml:mi><mml:mi mathvariant="bold-italic">&#x03B5;</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="bold-italic">&#x03B5;</mml:mi><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:mi mathvariant="normal">&#x2207;</mml:mi><mml:mrow><mml:mtext mathvariant="bold">u</mml:mtext></mml:mrow><mml:mo>+</mml:mo><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mrow><mml:mtext mathvariant="bold">u</mml:mtext></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mi>T</mml:mi></mml:mrow></mml:msup><mml:mo>]</mml:mo></mml:mrow></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:mrow><mml:mtext mathvariant="bold">m</mml:mtext></mml:mrow></mml:mtd><mml:mtd><mml:mi></mml:mi><mml:mo>=</mml:mo><mml:mn>2</mml:mn><mml:mi>&#x03BC;</mml:mi><mml:msup><mml:mrow><mml:mi>&#x2113;</mml:mi></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mi>&#x03C7;</mml:mi><mml:mo>,</mml:mo><mml:mi>&#x03C7;</mml:mi><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:mi mathvariant="normal">&#x2207;</mml:mi><mml:mi>&#x03B8;</mml:mi><mml:mo>+</mml:mo><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mi>&#x03B8;</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mi>T</mml:mi></mml:mrow></mml:msup><mml:mo>]</mml:mo></mml:mrow></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>where <inline-formula id="ieqn-38"><mml:math id="mml-ieqn-38"><mml:mrow><mml:mtext mathvariant="bold">u</mml:mtext></mml:mrow></mml:math></inline-formula> denotes the displacement vector, <inline-formula id="ieqn-39"><mml:math id="mml-ieqn-39"><mml:mi>&#x03B8;</mml:mi><mml:mo>=</mml:mo><mml:mrow><mml:mtext>curl</mml:mtext></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mtext mathvariant="bold">u</mml:mtext></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mspace width="negativethinmathspace" /><mml:mrow><mml:mrow><mml:mo>/</mml:mo></mml:mrow></mml:mrow><mml:mn>2</mml:mn></mml:math></inline-formula> represents the rotation vector, <inline-formula id="ieqn-40"><mml:math id="mml-ieqn-40"><mml:mrow><mml:mi>&#x2113;</mml:mi></mml:mrow></mml:math></inline-formula> is the material length scale parameter introduced to account for the size effect, and <inline-formula id="ieqn-41"><mml:math id="mml-ieqn-41"><mml:mi>&#x03BB;</mml:mi></mml:math></inline-formula> and <inline-formula id="ieqn-42"><mml:math id="mml-ieqn-42"><mml:mi>&#x03BC;</mml:mi></mml:math></inline-formula> are Lam&#x00E9; constants in classical continuum mechanics. Note that <inline-formula id="ieqn-43"><mml:math id="mml-ieqn-43"><mml:mi>&#x03BC;</mml:mi></mml:math></inline-formula> is also known as shear modulus. They can be written as
<disp-formula id="eqn-8"><label>(8)</label><mml:math id="mml-eqn-8" 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:mi>&#x03BB;</mml:mi></mml:mtd><mml:mtd><mml:mi></mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:msub><mml:mi>E</mml:mi><mml:mrow><mml:mi>e</mml:mi></mml:mrow></mml:msub><mml:msub><mml:mi>&#x03BD;</mml:mi><mml:mrow><mml:mi>e</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mn>1</mml:mn><mml:mo>+</mml:mo><mml:msub><mml:mi>&#x03BD;</mml:mi><mml:mrow><mml:mi>e</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mn>1</mml:mn><mml:mo>&#x2212;</mml:mo><mml:mn>2</mml:mn><mml:msub><mml:mi>&#x03BD;</mml:mi><mml:mrow><mml:mi>e</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:mrow></mml:mfrac></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<disp-formula id="eqn-9"><label>(9)</label><mml:math id="mml-eqn-9" display="block"><mml:mtable columnalign="right left right left right left right left right left right left" rowspacing="3pt" columnspacing="0em 2em 0em 2em 0em 2em 0em 2em 0em 2em 0em" displaystyle="true"><mml:mtr><mml:mtd><mml:mi>&#x03BC;</mml:mi></mml:mtd><mml:mtd><mml:mi></mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:msub><mml:mi>E</mml:mi><mml:mrow><mml:mi>e</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mn>2</mml:mn><mml:mrow><mml:mo>(</mml:mo><mml:mn>1</mml:mn><mml:mo>+</mml:mo><mml:msub><mml:mi>&#x03BD;</mml:mi><mml:mrow><mml:mi>e</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:mrow></mml:mfrac></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula></p>
</sec>
<sec id="s2_3">
<label>2.3</label>
<title>Governing Equations</title>
<p>In this study, the Euler-Bernoulli beam theory was utilized to model the beam. Consequently, the displacement field can be expressed as
<disp-formula id="eqn-10"><label>(10)</label><mml:math id="mml-eqn-10" display="block"><mml:mtable columnalign="right left right left right left right left right left right left" rowspacing="3pt" columnspacing="0em 2em 0em 2em 0em 2em 0em 2em 0em 2em 0em" displaystyle="true"><mml:mtr><mml:mtd><mml:msub><mml:mi>u</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>,</mml:mo><mml:mi>z</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mtd><mml:mtd><mml:mi></mml:mi><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mi>z</mml:mi><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>w</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>x</mml:mi></mml:mrow></mml:mfrac></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<disp-formula id="eqn-11"><label>(11)</label><mml:math id="mml-eqn-11" 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:msub><mml:mi>u</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>,</mml:mo><mml:mi>z</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mtd><mml:mtd><mml:mi></mml:mi><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<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:msub><mml:mi>u</mml:mi><mml:mrow><mml:mn>3</mml:mn></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>,</mml:mo><mml:mi>z</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mtd><mml:mtd><mml:mi></mml:mi><mml:mo>=</mml:mo><mml:mi>w</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>where <inline-formula id="ieqn-44"><mml:math id="mml-ieqn-44"><mml:mi>w</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> represents the transverse displacements on the midplane of the FG nanobeam.</p>
<p>The tensors associated with <xref ref-type="disp-formula" rid="eqn-6">Eqs. (6)</xref> and <xref ref-type="disp-formula" rid="eqn-7">(7)</xref> can be written as
<disp-formula id="eqn-13"><label>(13)</label><mml:math id="mml-eqn-13" display="block"><mml:msub><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>x</mml:mi><mml:mi>x</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mi>z</mml:mi><mml:mfrac><mml:mrow><mml:msup><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mi>w</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msup><mml:mi>x</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mfrac><mml:mo>,</mml:mo><mml:msub><mml:mi>&#x03B8;</mml:mi><mml:mrow><mml:mi>y</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mrow><mml:mo>(</mml:mo><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>w</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>x</mml:mi></mml:mrow></mml:mfrac><mml:mo>)</mml:mo></mml:mrow><mml:mo>,</mml:mo><mml:msub><mml:mi>&#x03C7;</mml:mi><mml:mrow><mml:mi>x</mml:mi><mml:mi>y</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:mn>2</mml:mn></mml:mfrac><mml:mrow><mml:mo>(</mml:mo><mml:mfrac><mml:mrow><mml:msup><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mi>w</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msup><mml:mi>x</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mfrac><mml:mo>)</mml:mo></mml:mrow></mml:math></disp-formula></p>
<p>Substituting <xref ref-type="disp-formula" rid="eqn-13">Eq. (13)</xref> into <xref ref-type="disp-formula" rid="eqn-6">Eq. (6)</xref>, the strain energy <inline-formula id="ieqn-45"><mml:math id="mml-ieqn-45"><mml:mi>U</mml:mi></mml:math></inline-formula> can be written as:
<disp-formula id="eqn-14"><label>(14)</label><mml:math id="mml-eqn-14" display="block"><mml:mi>U</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:mn>2</mml:mn></mml:mfrac><mml:msub><mml:mo>&#x222C;</mml:mo><mml:mrow><mml:mi>V</mml:mi></mml:mrow></mml:msub><mml:mo>&#x222B;</mml:mo><mml:mrow><mml:mo>[</mml:mo><mml:msub><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>x</mml:mi><mml:mi>x</mml:mi></mml:mrow></mml:msub><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>x</mml:mi><mml:mi>x</mml:mi></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:mn>2</mml:mn><mml:msub><mml:mi>m</mml:mi><mml:mrow><mml:mi>x</mml:mi><mml:mi>y</mml:mi></mml:mrow></mml:msub><mml:msub><mml:mi>&#x03C7;</mml:mi><mml:mrow><mml:mi>x</mml:mi><mml:mi>y</mml:mi></mml:mrow></mml:msub><mml:mo>]</mml:mo></mml:mrow><mml:mi>d</mml:mi><mml:mi>v</mml:mi><mml:mo>+</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:mn>2</mml:mn></mml:mfrac><mml:msub><mml:mo>&#x222D;</mml:mo><mml:mrow><mml:mi>V</mml:mi></mml:mrow></mml:msub><mml:mo>&#x222B;</mml:mo><mml:mrow><mml:mo>[</mml:mo><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>x</mml:mi><mml:mi>x</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mi>z</mml:mi><mml:mfrac><mml:mrow><mml:msup><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mi>w</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msup><mml:mi>x</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mfrac><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mn>4</mml:mn><mml:msup><mml:mrow><mml:mi>&#x2113;</mml:mi></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mi>&#x03BC;</mml:mi><mml:msubsup><mml:mi>&#x03C7;</mml:mi><mml:mrow><mml:mi>x</mml:mi><mml:mi>y</mml:mi></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msubsup><mml:mo>]</mml:mo></mml:mrow><mml:mi>d</mml:mi><mml:mi>v</mml:mi></mml:math></disp-formula></p>
<p>By employing the stress tensor from <xref ref-type="disp-formula" rid="eqn-6">Eq. (6)</xref> and taking the variation in the strain energy, we obtain
<disp-formula id="eqn-15"><label>(15)</label><mml:math id="mml-eqn-15" display="block"><mml:mtable columnalign="left" rowspacing="4pt" columnspacing="1em"><mml:mtr><mml:mtd><mml:mi>&#x03B4;</mml:mi><mml:mi>U</mml:mi><mml:mo>=</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mn>1</mml:mn><mml:mn>2</mml:mn></mml:mfrac></mml:mstyle><mml:msub><mml:mo>&#x222C;</mml:mo><mml:mrow><mml:mi>V</mml:mi></mml:mrow></mml:msub><mml:mo>&#x222B;</mml:mo><mml:mi>&#x03B4;</mml:mi><mml:mrow><mml:mo>[</mml:mo><mml:mrow><mml:mo>(</mml:mo><mml:mi>&#x03BB;</mml:mi><mml:mo>+</mml:mo><mml:mn>2</mml:mn><mml:mi>&#x03BC;</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mi>z</mml:mi><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mrow><mml:msup><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mi>w</mml:mi></mml:mrow><mml:mrow><mml:mi 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mathvariant="normal">&#x2202;</mml:mi><mml:msup><mml:mi>x</mml:mi><mml:mrow><mml:mn>4</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mfrac></mml:mstyle><mml:mi>&#x03B4;</mml:mi><mml:mi>w</mml:mi><mml:mo>+</mml:mo><mml:msup><mml:mrow><mml:mi>&#x2113;</mml:mi></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:msub><mml:mi>B</mml:mi><mml:mrow><mml:mn>11</mml:mn></mml:mrow></mml:msub><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mrow><mml:msup><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mn>4</mml:mn></mml:mrow></mml:msup><mml:mi>w</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msup><mml:mi>x</mml:mi><mml:mrow><mml:mn>4</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mfrac></mml:mstyle><mml:mi>&#x03B4;</mml:mi><mml:mi>w</mml:mi><mml:mo>]</mml:mo></mml:mrow><mml:mi>d</mml:mi><mml:mi>x</mml:mi></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>in which <inline-formula id="ieqn-46"><mml:math id="mml-ieqn-46"><mml:msub><mml:mi>A</mml:mi><mml:mrow><mml:mn>11</mml:mn></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mo>&#x222B;</mml:mo><mml:mrow><mml:mi>A</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:mi>&#x03BB;</mml:mi><mml:mo>+</mml:mo><mml:mn>2</mml:mn><mml:mi>&#x03BC;</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:msup><mml:mi>z</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mi>d</mml:mi><mml:mi>A</mml:mi><mml:mrow><mml:mtext>&#xA0;and&#xA0;</mml:mtext></mml:mrow><mml:msub><mml:mi>B</mml:mi><mml:mrow><mml:mn>11</mml:mn></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mo>&#x222B;</mml:mo><mml:mrow><mml:mi>A</mml:mi></mml:mrow></mml:msub><mml:mi>&#x03BC;</mml:mi><mml:mi>d</mml:mi><mml:mi>A</mml:mi></mml:math></inline-formula>.</p>
<p>By disregarding the body force and body couple, the work <inline-formula id="ieqn-47"><mml:math id="mml-ieqn-47"><mml:mi>W</mml:mi></mml:math></inline-formula> performed by external forces in the form of transverse loading <inline-formula id="ieqn-48"><mml:math id="mml-ieqn-48"><mml:mi>q</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> can be written as
<disp-formula id="eqn-16"><label>(16)</label><mml:math id="mml-eqn-16" display="block"><mml:mi>W</mml:mi><mml:mo>=</mml:mo><mml:msubsup><mml:mo>&#x222B;</mml:mo><mml:mrow><mml:mi>x</mml:mi><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:mrow><mml:mrow><mml:mi>L</mml:mi></mml:mrow></mml:msubsup><mml:mi>q</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mi>w</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mtext>d</mml:mtext></mml:mrow><mml:mi>x</mml:mi></mml:math></disp-formula></p>
<p>Substitute <xref ref-type="disp-formula" rid="eqn-13">Eqs. (13)</xref> and <xref ref-type="disp-formula" rid="eqn-15">(15)</xref> into Hamilton&#x2019;s principle and setting the resulting expression to zero, that is,
<disp-formula id="eqn-17"><label>(17)</label><mml:math id="mml-eqn-17" display="block"><mml:mi>&#x03B4;</mml:mi><mml:mrow><mml:mi mathvariant="normal">&#x03A0;</mml:mi></mml:mrow><mml:mo>=</mml:mo><mml:msubsup><mml:mo>&#x222B;</mml:mo><mml:mrow><mml:mn>0</mml:mn></mml:mrow><mml:mrow><mml:mi>L</mml:mi></mml:mrow></mml:msubsup><mml:mrow><mml:mo>(</mml:mo><mml:mi>&#x03B4;</mml:mi><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:mi>&#x03B4;</mml:mi><mml:mi>W</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mtext>d</mml:mtext></mml:mrow><mml:mi>x</mml:mi><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math></disp-formula></p>
<p>The governing equations of motion can be derived as [<xref ref-type="bibr" rid="ref-38">38</xref>]
<disp-formula id="eqn-18"><label>(18)</label><mml:math id="mml-eqn-18" display="block"><mml:msub><mml:mi>A</mml:mi><mml:mrow><mml:mn>11</mml:mn></mml:mrow></mml:msub><mml:mfrac><mml:mrow><mml:msup><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mn>4</mml:mn></mml:mrow></mml:msup><mml:mi>w</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msup><mml:mi>x</mml:mi><mml:mrow><mml:mn>4</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mfrac><mml:mo>+</mml:mo><mml:msup><mml:mrow><mml:mi>&#x2113;</mml:mi></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:msub><mml:mi>B</mml:mi><mml:mrow><mml:mn>11</mml:mn></mml:mrow></mml:msub><mml:mfrac><mml:mrow><mml:msup><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mn>4</mml:mn></mml:mrow></mml:msup><mml:mi>w</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msup><mml:mi>x</mml:mi><mml:mrow><mml:mn>4</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mi>q</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></disp-formula></p>
<p>In addition, we can define the equivalent stiffness as <inline-formula id="ieqn-49"><mml:math id="mml-ieqn-49"><mml:msub><mml:mi>D</mml:mi><mml:mrow><mml:mi>e</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mi>D</mml:mi><mml:mo>+</mml:mo><mml:msup><mml:mi>D</mml:mi><mml:mrow><mml:mrow><mml:mi>&#x2113;</mml:mi></mml:mrow></mml:mrow></mml:msup><mml:mo>=</mml:mo><mml:msub><mml:mi>A</mml:mi><mml:mrow><mml:mn>11</mml:mn></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msup><mml:mrow><mml:mi>&#x2113;</mml:mi></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:msub><mml:mi>B</mml:mi><mml:mrow><mml:mn>11</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula>. It can be observed that for <inline-formula id="ieqn-50"><mml:math id="mml-ieqn-50"><mml:msup><mml:mi>D</mml:mi><mml:mrow><mml:mrow><mml:mi>&#x2113;</mml:mi></mml:mrow></mml:mrow></mml:msup><mml:mo>=</mml:mo><mml:mrow><mml:mi>&#x2113;</mml:mi></mml:mrow><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math></inline-formula>, <xref ref-type="disp-formula" rid="eqn-18">Eq. (18)</xref> yields the governing equation of classical beam theory. Based on our knowledge of material mechanics, it is easy to obtain analytical expressions for the deflection of a microbeam under different boundary conditions with finite element method.</p>
</sec>
</sec>
<sec id="s3">
<label>3</label>
<title>Physics-Informed Neural Networks Framework</title>
<p>This section employs a general PINN model to solve the bending <xref ref-type="disp-formula" rid="eqn-18">Eq. (18)</xref>. PINNs, a specialized class of artificial neural networks, are used to obtain an approximate solution of the governing differential equations. To solve <xref ref-type="disp-formula" rid="eqn-18">Eq. (18)</xref>, a neural network is constructed with the spatial variable <italic>x</italic> as its input to approximate the solution. Within the PINN framework, a feedforward neural network (FNN) [<xref ref-type="bibr" rid="ref-39">39</xref>] is commonly adopted as the neural network architecture [<xref ref-type="bibr" rid="ref-40">40</xref>,<xref ref-type="bibr" rid="ref-41">41</xref>] due to its strong function approximation capability and structural simplicity. An illustration of the FNN is shown in <xref ref-type="fig" rid="fig-1">Fig. 1</xref>. Thus, the approximate solution can be written as <disp-formula id="eqn-19"><label>(19)</label><mml:math id="mml-eqn-19" display="block"><mml:mrow><mml:mover><mml:mi>w</mml:mi><mml:mo stretchy="false">&#x005E;</mml:mo></mml:mover></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:mi>F</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:msup><mml:mrow><mml:mtext>N&#xA0;</mml:mtext></mml:mrow><mml:mrow><mml:mi>L</mml:mi></mml:mrow></mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>;</mml:mo><mml:mi>W</mml:mi><mml:mo>,</mml:mo><mml:mi>b</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></disp-formula>where <inline-formula id="ieqn-51"><mml:math id="mml-ieqn-51"><mml:mrow><mml:mover><mml:mi>w</mml:mi><mml:mo stretchy="false">&#x005E;</mml:mo></mml:mover></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> is the approximate solution, <inline-formula id="ieqn-52"><mml:math id="mml-ieqn-52"><mml:mi>F</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>x</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> denotes the FNN. The FNN is structured as an <italic>L</italic>-layer deep neural network. It accepts an input vector <inline-formula id="ieqn-53"><mml:math id="mml-ieqn-53"><mml:mi>x</mml:mi></mml:math></inline-formula>, produces an output vector <inline-formula id="ieqn-54"><mml:math id="mml-ieqn-54"><mml:mrow><mml:mover><mml:mi>w</mml:mi><mml:mo stretchy="false">&#x005E;</mml:mo></mml:mover></mml:mrow></mml:math></inline-formula>, and is parameterized by a weight matrix <inline-formula id="ieqn-55"><mml:math id="mml-ieqn-55"><mml:mi>W</mml:mi></mml:math></inline-formula> and a bias vector <inline-formula id="ieqn-56"><mml:math id="mml-ieqn-56"><mml:mi>b</mml:mi></mml:math></inline-formula>. The network was trained using a backpropagation algorithm [<xref ref-type="bibr" rid="ref-42">42</xref>], which iteratively reduces a composite loss function. This loss function quantifies the discrepancy between the network&#x2019;s predictions and the target solution [<xref ref-type="bibr" rid="ref-43">43</xref>]. In the context of PINNs, the loss function incorporates differential equations and boundary conditions <disp-formula id="eqn-20"><label>(20)</label><mml:math id="mml-eqn-20" display="block"><mml:mi>L</mml:mi><mml:mi>o</mml:mi><mml:mi>s</mml:mi><mml:mi>s</mml:mi><mml:mo>=</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mrow><mml:mi>P</mml:mi><mml:mi>D</mml:mi><mml:mi>E</mml:mi></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mrow><mml:mi>B</mml:mi><mml:mi>C</mml:mi></mml:mrow></mml:msub></mml:math></disp-formula>where <inline-formula id="ieqn-57"><mml:math id="mml-ieqn-57"><mml:msub><mml:mi>L</mml:mi><mml:mrow><mml:mi>P</mml:mi><mml:mi>D</mml:mi><mml:mi>E</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-58"><mml:math id="mml-ieqn-58"><mml:msub><mml:mi>L</mml:mi><mml:mrow><mml:mi>B</mml:mi><mml:mi>C</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> represent the losses associated with partial differential equations and boundary conditions, respectively. It is noteworthy that the partial differential term within the loss function can be analytically derived using automatic differentiation [<xref ref-type="bibr" rid="ref-44">44</xref>].</p>
<p>The loss function endowed with physical constraints is a crucial element in PINNs. It facilitates the training of neural networks in accordance with the physical laws. Within the current PINN-based computational mechanics framework, two main types of loss functions are commonly employed: the allocation loss function and the energy-based loss function. In the allocation loss function, the residuals of the equilibrium equation and boundary conditions were compelled to be zero at each sample point. In this study, an allocation loss function was adopted to formulate the loss function. In this approach, the mean-square error is used to define the loss function: <disp-formula id="eqn-21"><label>(21)</label><mml:math id="mml-eqn-21" display="block"><mml:mtable columnalign="left" rowspacing="4pt" columnspacing="1em"><mml:mtr><mml:mtd><mml:mi>L</mml:mi><mml:mi>o</mml:mi><mml:mi>s</mml:mi><mml:mi>s</mml:mi><mml:mo>=</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mn>1</mml:mn><mml:mi>n</mml:mi></mml:mfrac></mml:mstyle><mml:munderover><mml:mo>&#x2211;</mml:mo><mml:mrow><mml:mi>i</mml:mi><mml:mo>=</mml:mo><mml:mn>1</mml:mn></mml:mrow><mml:mrow><mml:mi>n</mml:mi></mml:mrow></mml:munderover><mml:msubsup><mml:mi>R</mml:mi><mml:mrow><mml:mi>P</mml:mi><mml:mi>D</mml:mi><mml:mi>E</mml:mi></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msubsup><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>x</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mn>1</mml:mn><mml:mi>m</mml:mi></mml:mfrac></mml:mstyle><mml:munderover><mml:mo>&#x2211;</mml:mo><mml:mrow><mml:mi>i</mml:mi><mml:mo>=</mml:mo><mml:mn>1</mml:mn></mml:mrow><mml:mrow><mml:mi>m</mml:mi></mml:mrow></mml:munderover><mml:msubsup><mml:mi>R</mml:mi><mml:mrow><mml:mi>B</mml:mi><mml:mi>C</mml:mi></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msubsup><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>x</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mn>1</mml:mn><mml:mi>n</mml:mi></mml:mfrac></mml:mstyle><mml:munderover><mml:mo>&#x2211;</mml:mo><mml:mrow><mml:mi>i</mml:mi><mml:mo>=</mml:mo><mml:mn>1</mml:mn></mml:mrow><mml:mrow><mml:mi>n</mml:mi></mml:mrow></mml:munderover><mml:msup><mml:mrow><mml:mo>[</mml:mo><mml:msub><mml:mi>D</mml:mi><mml:mrow><mml:mi>e</mml:mi></mml:mrow></mml:msub><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mover><mml:mi>w</mml:mi><mml:mo stretchy="false">&#x005E;</mml:mo></mml:mover></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>x</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msup><mml:mi>x</mml:mi><mml:mrow><mml:mn>4</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>&#x2212;</mml:mo><mml:mi>q</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>x</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mo>]</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mspace width="2em" /><mml:mo>+</mml:mo><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mover><mml:mi>w</mml:mi><mml:mo stretchy="false">&#x005E;</mml:mo></mml:mover></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mn>0</mml:mn><mml:mo>)</mml:mo></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>+</mml:mo><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mover><mml:mi>w</mml:mi><mml:mo stretchy="false">&#x005E;</mml:mo></mml:mover></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mi>L</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>+</mml:mo><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mrow><mml:msup><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mrow><mml:mover><mml:mi>w</mml:mi><mml:mo stretchy="false">&#x005E;</mml:mo></mml:mover></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mn>0</mml:mn><mml:mo>)</mml:mo></mml:mrow></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msup><mml:mi>x</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>+</mml:mo><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mrow><mml:msup><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mrow><mml:mover><mml:mi>w</mml:mi><mml:mo stretchy="false">&#x005E;</mml:mo></mml:mover></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mi>L</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msup><mml:mi>x</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>where <inline-formula id="ieqn-59"><mml:math id="mml-ieqn-59"><mml:msub><mml:mi>R</mml:mi><mml:mrow><mml:mi>P</mml:mi><mml:mi>D</mml:mi><mml:mi>E</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> and <inline-formula id="ieqn-60"><mml:math id="mml-ieqn-60"><mml:msub><mml:mi>R</mml:mi><mml:mrow><mml:mi>B</mml:mi><mml:mi>C</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> are the residuals of the equilibrium equation and the boundary conditions, respectively. Here, <italic>n</italic> represents the total number of sample points and <italic>m</italic> is the number of sample points on the boundary. Subsequently, the training algorithm is implemented to search for the neural network mapping that satisfies the governing equations at sample points. A schematic of the PINN algorithm applied to the bending equation is illustrated in <xref ref-type="fig" rid="fig-1">Fig. 1b</xref>.</p>
</sec>
<sec id="s4">
<label>4</label>
<title>Results and Discussion</title>
<p>The developed physics-informed neural network was used for numerical calculations. In addition, to verify the reliability of the PINN approximate solution, the numerical results obtained based on finite element and analytical expressions are also presented and used as reference numerical solutions, in which the focus of the analysis is on the bending behavior of GOri/Sn metamaterial microbeams. In this study, all tasks were trained using an NVIDIA Titan RTX GPU. As depicted in Fig. S1 (Supporting Information), we trained three different neural network architectures with varying numbers of hidden layers. Based on the training speed, convergence curve volatility, and forecasting performance of each neural network, we selected a three-layer network with 40 nodes as the architecture for this study. As shown by the error curve in Fig. S2 (Supporting Information), compared to other adaptive stochastic gradient descent methods such as stochastic gradient descent (SGD) and root mean square propagation (RMSPro), the Adam algorithm demonstrates superior performance in model optimization. It enables faster computation and convergence, making it an ideal optimization algorithm for neural network training. Additionally, the Adam optimization scheme [<xref ref-type="bibr" rid="ref-45">45</xref>] is prominent, extensively applied, and highly adaptable within the PINN methodology. In this study, an Adam optimizer with an initial learning rate of 10<sup>&#x2212;4</sup> is used to train the deep neural network (DNN). Fig. S3 (Supporting Information) shows the variation in loss function values during model training under different activation functions. When using rectified linear unit (ReLU) as the activation function, the loss decreases more slowly, ultimately leading to underfitting in the final training results. When training models with tanh and Sigmoid as activation functions, the loss function converges more rapidly. Furthermore, upon convergence, the loss value of the tanh model is lower than that of the Sigmoid model. Thus, the hyperbolic tangent (tanh) function was used as the activation function within the FNNs [<xref ref-type="bibr" rid="ref-46">46</xref>]. In the workflow described in this paper, 200 sample points within the domain and 100 boundary sample points were generated using the Latin hypercube sampling (LHS) method. The maximum training iterations were set to 50,000, and parameters were initialized using the Glorot normal distribution initializer. Geometric parameters of pristine graphene: <inline-formula id="ieqn-61"><mml:math id="mml-ieqn-61"><mml:msub><mml:mi>l</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>r</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>83.76</mml:mn><mml:mover><mml:mrow><mml:mtext>A</mml:mtext></mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mover></mml:math></inline-formula> and <inline-formula id="ieqn-62"><mml:math id="mml-ieqn-62"><mml:msub><mml:mi>t</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>r</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>3.4</mml:mn><mml:mspace width="thinmathspace" /><mml:mover><mml:mrow><mml:mtext>A</mml:mtext></mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mover></mml:math></inline-formula> [<xref ref-type="bibr" rid="ref-5">5</xref>]. The material parameters at room temperature are presented in <xref ref-type="table" rid="table-1">Table 1</xref>.</p>
<table-wrap id="table-1">
<label>Table 1</label>
<caption>
<title>Mechanical properties of graphene and Sn.</title>
</caption>
<table>
<colgroup>
<col align="center"/>
<col align="center"/>
<col align="center"/>
</colgroup>
<thead>
<tr>
<th></th>
<th>Sn matrix [<xref ref-type="bibr" rid="ref-47">47</xref>]</th>
<th>Graphene [<xref ref-type="bibr" rid="ref-5">5</xref>]</th>
</tr>
</thead>
<tbody>
<tr>
<td>Young&#x2019;s modulus (GPa)</td>
<td>51</td>
<td>929.57</td>
</tr>
<tr>
<td>Mass density (kg/m<sup>3</sup>)</td>
<td>8800</td>
<td>1800</td>
</tr>
<tr>
<td>Poisson&#x2019;s ratio</td>
<td>0.34</td>
<td>0.22</td>
</tr>
</tbody>
</table>
</table-wrap>
<sec id="s4_1">
<label>4.1</label>
<title>Validation</title>
<p>To check the accuracy of the numerical calculation results of the analytical method, considering the thickness of the homogeneous microbeam <inline-formula id="ieqn-63"><mml:math id="mml-ieqn-63"><mml:mi>h</mml:mi><mml:mo>=</mml:mo><mml:mn>1</mml:mn><mml:mspace width="thinmathspace" /><mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x0B5;</mml:mi></mml:mrow></mml:mrow><mml:mrow><mml:mtext>m</mml:mtext></mml:mrow></mml:math></inline-formula> and ignoring the influence of origami graphene, the approximate solution of PINN in this study was compared with the analytical solution of deflection under three boundary conditions, as shown in <xref ref-type="fig" rid="fig-3">Fig. 3</xref>. We adopted the finite element method to obtain its analytical solution, the details of which are as follows: (1) Mesh size and type: The computational domain was discretized using 4-node quadrilateral elements with a mesh density of 0.1 nm element size to balance accuracy and computational efficiency. Mesh convergence tests were performed to confirm that further refinement did not alter the results significantly. (2) Solver specifications: The finite element method (FEM) simulations were conducted using COMSOL Multiphysics 6.3, with a direct solver for these cases and a convergence tolerance of 1 &#x00D7; 10<sup>&#x2212;6</sup> for displacement residuals and 1 &#x00D7; 10<sup>&#x2212;6</sup> for force residuals (Fig. S4, Supporting Information). (3) Boundary conditions: The same boundary conditions as those applied in the PINN model were enforced in the FEM, including uniform load <inline-formula id="ieqn-64"><mml:math id="mml-ieqn-64"><mml:mi>q</mml:mi></mml:math></inline-formula> on the surface of the beam and the displacement boundary condition. To facilitate the comparison and discussion of the calculation results, the dimensionless deflection is defined as <inline-formula id="ieqn-65"><mml:math id="mml-ieqn-65"><mml:mover><mml:mi>w</mml:mi><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mo>=</mml:mo><mml:mi>w</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mfrac><mml:mrow><mml:mi>E</mml:mi><mml:mi>I</mml:mi></mml:mrow><mml:mrow><mml:mi>q</mml:mi><mml:msup><mml:mi>L</mml:mi><mml:mrow><mml:mn>4</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mfrac><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>.</p>
<fig id="fig-3">
<label>Figure 3</label>
<caption>
<title>Non-dimensional deflection of micro-beam and loss function value of (<bold>a</bold>) C-C, (<bold>b</bold>) S-S and (<bold>c</bold>) C-F beams under uniform distributed load (<inline-formula id="ieqn-66"><mml:math id="mml-ieqn-66"><mml:mi>L</mml:mi><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mi>h</mml:mi><mml:mo>=</mml:mo><mml:mn>10</mml:mn><mml:mo>,</mml:mo><mml:mi>q</mml:mi><mml:mo>=</mml:mo><mml:mn>1</mml:mn><mml:mi>N</mml:mi><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mi>m</mml:mi><mml:mo>,</mml:mo><mml:mrow><mml:mi>&#x2113;</mml:mi></mml:mrow><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mi>h</mml:mi><mml:mo>=</mml:mo><mml:mn>0</mml:mn><mml:mo>,</mml:mo><mml:mn>0.2</mml:mn><mml:mo>,</mml:mo><mml:mn>0.4</mml:mn><mml:mo>,</mml:mo><mml:mn>0.6</mml:mn></mml:math></inline-formula>).</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_76418-fig-3.tif"/>
</fig>
<p><xref ref-type="fig" rid="fig-3">Fig. 3</xref> shows the nondimensional deflection of a homogeneous microbeam with three boundary conditions: simply supported at both ends, fixed at both ends, and a cantilever beam, along with the values of the loss function. The PINN prediction under the three boundary conditions is consistent with the exact solution. In addition, after 10,000 iterations, the loss function values in all three cases quickly decreased to less than 10<sup>&#x2013;4</sup>. This indicates that the network converged to the final solution with a high degree of accuracy.</p>

<p>To investigate the validity of the developed PINN approach, the present results are compared with those obtained by Park and Gao [<xref ref-type="bibr" rid="ref-48">48</xref>] based on the couple stress theory shown in <xref ref-type="fig" rid="fig-4">Fig. 4</xref>. The figure clearly demonstrates excellent agreement between the results derived from the PINN approach and those reported in the literature.</p>
<fig id="fig-4">
<label>Figure 4</label>
<caption>
<title>Comparing the present results with the work of Park and Gao [<xref ref-type="bibr" rid="ref-48">48</xref>] in variation of dimensionless deflection of beam under C&#x2013;F boundary conditions with changes in beam thickness.</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_76418-fig-4.tif"/>
</fig>
</sec>
<sec id="s4_2">
<label>4.2</label>
<title>Parametric Analysis</title>
<p>A comprehensive parameter analysis was carried out through parameter research based on the PINN approach. The bending characteristics of composite beams with different porosities, slenderness ratios, and boundary conditions were studied.</p>
<p>To provide further insight into the outputs of the PINN approach, <xref ref-type="fig" rid="fig-5">Fig. 5</xref> describes how the maximum deflection of the graphene origami composite beam is affected by the scale parameters, graphene origami content, and folding degree (at this time, the folding degree of graphene is 50%) under a uniformly distributed load and fixed boundary at both ends. It can be observed that the dimensionless maximum deflection decreased with increasing graphene content. This is because when the graphene content increased, the equivalent stiffness of the GOri/Sn composites increased, and they exhibited better bending performance. However, with an increase in the folding degree of graphene (the mass fraction of graphene is 2.5 wt%), the equivalent elastic modulus of the composite beam decreases and exhibits the characteristics of metamaterials [<xref ref-type="bibr" rid="ref-49">49</xref>,<xref ref-type="bibr" rid="ref-50">50</xref>], and it is observed that the maximum deflection increases slightly. Considering the size effect, the increase in graphene content reduced the maximum deflection by 61.5% (<inline-formula id="ieqn-67"><mml:math id="mml-ieqn-67"><mml:mrow><mml:mi>&#x2113;</mml:mi></mml:mrow><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mi>h</mml:mi><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math></inline-formula>), and the maximum deflection increased by 16.7% (<inline-formula id="ieqn-68"><mml:math id="mml-ieqn-68"><mml:mrow><mml:mi>&#x2113;</mml:mi></mml:mrow><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mi>h</mml:mi><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math></inline-formula>). This is due to the fact that the stiffness-hardening effect in micro-scale by the MCST. Due to the competing mechanisms between the stiffness hardening effect of the size effect and the stiffness weakening caused by graphene folding, the deflection trend gradually flattens as the folding degree increases.</p>
<fig id="fig-5">
<label>Figure 5</label>
<caption>
<title>Dimensionless maximum deflection with C-C boundary conditions vs. GOri content and folding degree for different composite patterns (<bold>a</bold>) <inline-formula id="ieqn-69"><mml:math id="mml-ieqn-69"><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>; (<bold>b</bold>) <inline-formula id="ieqn-70"><mml:math id="mml-ieqn-70"><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>; (<bold>c</bold>) <inline-formula id="ieqn-71"><mml:math id="mml-ieqn-71"><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>;(<bold>d</bold>) <inline-formula id="ieqn-72"><mml:math id="mml-ieqn-72"><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>.</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_76418-fig-5a.tif"/>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_76418-fig-5b.tif"/>
</fig>
<p><xref ref-type="fig" rid="fig-6">Fig. 6</xref> shows the influence of the scale parameters, graphene origami content, and folding degree on the maximum deflection of the graphene origami composite beam under a uniformly distributed load and simply supported boundary conditions at both ends (at this time, the folding degree of graphene is 50%), and a conclusion similar to that in <xref ref-type="fig" rid="fig-5">Fig. 5</xref> can be obtained. Increasing the graphene origami content enhances the effective stiffness, while increasing the folding degree reduces the effective stiffness of the composite beam. In addition, considering the size effect, an increase in graphene content will lead to a maximum deflection reduction of 64.3% (<inline-formula id="ieqn-73"><mml:math id="mml-ieqn-73"><mml:mrow><mml:mi>&#x2113;</mml:mi></mml:mrow><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mi>h</mml:mi><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math></inline-formula>), and the maximum deflection of graphene folding will increase by 27.5% (<inline-formula id="ieqn-74"><mml:math id="mml-ieqn-74"><mml:mrow><mml:mi>&#x2113;</mml:mi></mml:mrow><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mi>h</mml:mi><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math></inline-formula>). The primary cause of this change stems from the stiffness hardening effect from the size effect.</p>
<fig id="fig-6">
<label>Figure 6</label>
<caption>
<title>Dimensionless maximum deflection with S-S boundary conditions vs. GOri content and folding degree for different composite patterns (<bold>a</bold>) <inline-formula id="ieqn-75"><mml:math id="mml-ieqn-75"><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>; (<bold>b</bold>) <inline-formula id="ieqn-76"><mml:math id="mml-ieqn-76"><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>; (<bold>c</bold>) <inline-formula id="ieqn-77"><mml:math id="mml-ieqn-77"><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>; (<bold>d</bold>) <inline-formula id="ieqn-78"><mml:math id="mml-ieqn-78"><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>.</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_76418-fig-6a.tif"/>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_76418-fig-6b.tif"/>
</fig>
<p><xref ref-type="fig" rid="fig-7">Fig. 7</xref> describes the influence of scale parameters, graphene origami content, and folding degree on the maximum deflection of the graphene origami composite beam under the condition of C-F boundary conditions. We observe that an increase in graphene content leads to an increase in effective stiffness, thereby reducing the maximum bending deflection. Simultaneously, the degree of graphene folding weakens the bending performance. Based on the MCST, the maximum deflection decreases by 60% (<inline-formula id="ieqn-79"><mml:math id="mml-ieqn-79"><mml:mrow><mml:mi>&#x2113;</mml:mi></mml:mrow><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mi>h</mml:mi><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math></inline-formula>) with increased graphene content. In contrast, it increases by 8.2% (<inline-formula id="ieqn-80"><mml:math id="mml-ieqn-80"><mml:mrow><mml:mi>&#x2113;</mml:mi></mml:mrow><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mi>h</mml:mi><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math></inline-formula>) due to the folding degree of graphene origami.</p>
<fig id="fig-7">
<label>Figure 7</label>
<caption>
<title>Dimensionless maximum deflection with C-F boundary conditions vs. GOri content and folding degree for different composite patterns (<bold>a</bold>) <inline-formula id="ieqn-81"><mml:math id="mml-ieqn-81"><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>; (<bold>b</bold>) <inline-formula id="ieqn-82"><mml:math id="mml-ieqn-82"><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>; (<bold>c</bold>) <inline-formula id="ieqn-83"><mml:math id="mml-ieqn-83"><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>; (<bold>d</bold>) <inline-formula id="ieqn-84"><mml:math id="mml-ieqn-84"><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>.</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_76418-fig-7a.tif"/>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_76418-fig-7b.tif"/>
</fig>
<p>From <xref ref-type="fig" rid="fig-5">Figs. 5</xref>&#x2013;<xref ref-type="fig" rid="fig-7">7</xref>, we can obtain the following results regarding the pattern distribution under three boundary conditions. In the H coverage with an X-type distribution, increasing the GOri content reduces the dimensionless deflection. In contrast, for H coverage with a U-type distribution, increasing the GOri content causes the dimensionless deflection to first increase and then decrease. Additionally, as shown in the <xref ref-type="fig" rid="fig-5">Figs. 5</xref> and <xref ref-type="fig" rid="fig-7">7</xref>, with an increase in the graphene folding degree, the dimensionless maximum bending deflection occurs, which is attributed to the reduction in Young&#x2019;s modulus and the emergence of a negative Poisson&#x2019;s ratio. Furthermore, the results indicate that among the tested configurations, the <inline-formula id="ieqn-85"><mml:math id="mml-ieqn-85"><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> beam demonstrates the smallest dimensionless maximum bending deflection, followed in sequence by the <inline-formula id="ieqn-86"><mml:math id="mml-ieqn-86"><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> beam, <inline-formula id="ieqn-87"><mml:math id="mml-ieqn-87"><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>X</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> beam, and <inline-formula id="ieqn-88"><mml:math id="mml-ieqn-88"><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mi>U</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>R</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> beams. These findings suggest that dispersing a higher GOri content near the beam surfaces can enhance the structural performance of the metamaterial.</p>
<p>Finally, to further reveal the mechanism of graphene origami, we determined the influence of the slenderness ratio on the static bending behavior of graphene origami metamaterial and homogeneous beams, as shown in <xref ref-type="fig" rid="fig-8">Fig. 8</xref>. In this case, we do not consider the size effect. As expected, increasing the slenderness ratio led to greater bending deformation. When the composite beam is made of metamaterials, compared to the pure Sn beam, a smaller deflection can be obtained; that is, the stability of the metamaterial beam is better.</p>
<fig id="fig-8">
<label>Figure 8</label>
<caption>
<title>Effect of slenderness ratio on the dimensionless maximum deflection of the metamaterial beams and homogeneous beam with three boundaries (<inline-formula id="ieqn-89"><mml:math id="mml-ieqn-89"><mml:msub><mml:mi>W</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>r</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>2.5</mml:mn><mml:mspace width="thinmathspace" /><mml:mrow><mml:mtext>wt%</mml:mtext></mml:mrow><mml:mo>,</mml:mo><mml:msub><mml:mi>H</mml:mi><mml:mrow><mml:mi>G</mml:mi><mml:mi>r</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>50</mml:mn><mml:mi mathvariant="normal">&#x0025;</mml:mi></mml:math></inline-formula>).</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_76418-fig-8.tif"/>
</fig>
<p>It is worth noting that the PINN approximation method adopted in this study is suitable for beams with various boundary and load conditions, although it is not described in detail here for brevity. Among the three boundary conditions (C-C, C-F, S-S), the deflection of the C-F beam was the largest and that of the C-C beam was the smallest. Because the clamped constraint is much stiffer than the S-S and C-F constraints. The addition of graphene origami affected the mechanical behavior of the composite beams. Our results demonstrate that the proposed GOri/Sn metamaterial beam exhibits enhanced bending performance in comparison with a pure metal beam.</p>
</sec>
</sec>
<sec id="s5">
<label>5</label>
<title>Conclusions</title>
<p>Inspired by deep learning technology, we propose a physically constrained deep learning method to solve the bending problem of graphene origami-reinforced composite microbeams. Bending control equations and boundary conditions are embedded into the loss function of the network as physical information constraints, which can reflect the complex mechanical behavior and ensure the physical rationality of the identification results.</p>
<p>Through an example of composite microbeam bending under a uniformly distributed load, the accuracy of PINNs and traditional analytical solution methods in the calculation results is compared. In addition, a numerical example of the influence of the graphene origami content and the folding degree of the composite beam on the bending behavior under the size effect verifies the possibility of using a small amount of training data to accurately predict the mechanical behavior in different calculation domains in PINNs. It is worth noting that PINNs are still a promising research field in calculation methods and are excellent candidates for solving inverse and other mechanical problems. For the inverse problem, the traditional forward finite element method is difficult to deal with and usually requires additional optimization algorithms, such as the genetic algorithm and the gradient descent method. In the future, we plan to conduct related research on inverse problems.</p>
</sec>
<sec sec-type="supplementary-material" id="s6">
<title>Supplementary Materials</title>
<supplementary-material id="SD1">
<media xlink:href="CMC_76418-s001.docx"/>
</supplementary-material>
</sec>
</body>
<back>
<ack>
<p>Not applicable.</p>
</ack>
<sec>
<title>Funding Statement</title>
<p>This work was supported by the Natural Science Foundation of Henan (252300420935), Young Backbone Teacher Training Program of Zhengzhou Normal University (QNGG-232300), Zhengzhou Normal University Undergraduate Innovation and Entrepreneurship Training Program Project (DCY2024011), and Scientific Research Starting Foundation of Zhengzhou Normal University (2021-702442).</p>
</sec>
<sec>
<title>Author Contributions</title>
<p>Zuoquan Zhu: writing&#x2014;review and editing, Writing&#x2014;original draft, visualization, project administration, funding acquisition. Menghan Wang: formal analysis and data curation. Xinyu Li: validation, formal analysis and data curation. Mengxin Zhao: validation, formal analysis. 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>Data will be made available on request.</p>
</sec>
<sec>
<title>Ethics Approval</title>
<p>Not applicable.</p>
</sec>
<sec sec-type="COI-statement">
<title>Conflicts of Interest</title>
<p>The authors declare no conflicts of interest.</p>
</sec>
<sec>
<title>Supplementary Materials</title>
<p>The supplementary material is available online at <ext-link ext-link-type="uri" xlink:href="https://www.techscience.com/doi/10.32604/cmc.2026.076418/s1">https://www.techscience.com/doi/10.32604/cmc.2026.076418/s1</ext-link>.</p>
</sec>
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