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<front>
<journal-meta>
<journal-id journal-id-type="publisher-id">Front. Mech. Eng.</journal-id>
<journal-title>Frontiers in Mechanical Engineering</journal-title>
<abbrev-journal-title abbrev-type="pubmed">Front. Mech. Eng.</abbrev-journal-title>
<issn pub-type="epub">2297-3079</issn>
<publisher>
<publisher-name>Frontiers Media S.A.</publisher-name>
</publisher>
</journal-meta>
<article-meta>
<article-id pub-id-type="publisher-id">1526724</article-id>
<article-id pub-id-type="doi">10.3389/fmech.2024.1526724</article-id>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Mechanical Engineering</subject>
<subj-group>
<subject>Original Research</subject>
</subj-group>
</subj-group>
</article-categories>
<title-group>
<article-title>Residual reliability of a composite material subjected to buckling and post-buckling tests: the case of reinforced concrete</article-title>
<alt-title alt-title-type="left-running-head">Ngnassi Djami et al.</alt-title>
<alt-title alt-title-type="right-running-head">
<ext-link ext-link-type="uri" xlink:href="https://doi.org/10.3389/fmech.2024.1526724">10.3389/fmech.2024.1526724</ext-link>
</alt-title>
</title-group>
<contrib-group>
<contrib contrib-type="author" corresp="yes">
<name>
<surname>Ngnassi Djami</surname>
<given-names>Aslain Brisco</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
<xref ref-type="aff" rid="aff2">
<sup>2</sup>
</xref>
<xref ref-type="corresp" rid="c001">&#x2a;</xref>
<uri xlink:href="https://loop.frontiersin.org/people/1629954/overview"/>
<role content-type="https://credit.niso.org/contributor-roles/conceptualization/"/>
<role content-type="https://credit.niso.org/contributor-roles/formal-analysis/"/>
<role content-type="https://credit.niso.org/contributor-roles/methodology/"/>
<role content-type="https://credit.niso.org/contributor-roles/writing-original-draft/"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Nguelcheu</surname>
<given-names>Ulrich Ngnassi</given-names>
</name>
<xref ref-type="aff" rid="aff3">
<sup>3</sup>
</xref>
<role content-type="https://credit.niso.org/contributor-roles/conceptualization/"/>
<role content-type="https://credit.niso.org/contributor-roles/formal-analysis/"/>
<role content-type="https://credit.niso.org/contributor-roles/methodology/"/>
<role content-type="https://credit.niso.org/contributor-roles/writing-original-draft/"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Offole</surname>
<given-names>Florence</given-names>
</name>
<xref ref-type="aff" rid="aff4">
<sup>4</sup>
</xref>
<role content-type="https://credit.niso.org/contributor-roles/supervision/"/>
<role content-type="https://credit.niso.org/contributor-roles/validation/"/>
<role content-type="https://credit.niso.org/contributor-roles/Writing - review &#x26; editing/"/>
</contrib>
</contrib-group>
<aff id="aff1">
<sup>1</sup>
<institution>Department of Fundamental Sciences and Techniques of Engineer</institution>, <institution>Chemical Engineering and Mineral Industries School</institution>, <institution>University of Ngaoundere</institution>, <addr-line>Ngaoundere</addr-line>, <country>Cameroon</country>
</aff>
<aff id="aff2">
<sup>2</sup>
<institution>Mechanics, Materials and Photonics Laboratory</institution>, <institution>National School of Agro-Industrial Sciences</institution>, <institution>University of Ngaoundere</institution>, <addr-line>Ngaoundere</addr-line>, <country>Cameroon</country>
</aff>
<aff id="aff3">
<sup>3</sup>
<institution>Department of Physics</institution>, <institution>Faculty of Science</institution>, <institution>University of Ngaoundere</institution>, <addr-line>Ngaoundere</addr-line>, <country>Cameroon</country>
</aff>
<aff id="aff4">
<sup>4</sup>
<institution>Laboratory of Energy</institution>, <institution>Materials, Modeling and Methods</institution>, <institution>National Higher Polytechnic School of Douala</institution>, <institution>University of Douala</institution>, <addr-line>Douala</addr-line>, <country>Cameroon</country>
</aff>
<author-notes>
<fn fn-type="edited-by">
<p>
<bold>Edited by:</bold> <ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/1140023/overview">Li Li</ext-link>, Huazhong University of Science and Technology, China</p>
</fn>
<fn fn-type="edited-by">
<p>
<bold>Reviewed by:</bold> <ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/1527974/overview">Chitaranjan Pany</ext-link>, Vikram Sarabhai Space Centre, India</p>
<p>
<ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/1765492/overview">Aman Garg</ext-link>, The Northcap University, India</p>
</fn>
<corresp id="c001">&#x2a;Correspondence: Aslain Brisco Ngnassi Djami, <email>ngnassbris@yahoo.fr</email>
</corresp>
</author-notes>
<pub-date pub-type="epub">
<day>18</day>
<month>12</month>
<year>2024</year>
</pub-date>
<pub-date pub-type="collection">
<year>2024</year>
</pub-date>
<volume>10</volume>
<elocation-id>1526724</elocation-id>
<history>
<date date-type="received">
<day>12</day>
<month>11</month>
<year>2024</year>
</date>
<date date-type="accepted">
<day>04</day>
<month>12</month>
<year>2024</year>
</date>
</history>
<permissions>
<copyright-statement>Copyright &#xa9; 2024 Ngnassi Djami, Nguelcheu and Offole.</copyright-statement>
<copyright-year>2024</copyright-year>
<copyright-holder>Ngnassi Djami, Nguelcheu and Offole</copyright-holder>
<license xlink:href="http://creativecommons.org/licenses/by/4.0/">
<p>This is an open-access article distributed under the terms of the Creative Commons Attribution License (CC BY). The use, distribution or reproduction in other forums is permitted, provided the original author(s) and the copyright owner(s) are credited and that the original publication in this journal is cited, in accordance with accepted academic practice. No use, distribution or reproduction is permitted which does not comply with these terms.</p>
</license>
</permissions>
<abstract>
<p>This article examines the residual reliability of composite materials, focusing on reinforced concrete subjected to buckling and post-buckling tests, a crucial topic in civil engineering. The main aim of the study is to assess how these loads affect mechanical properties, including compressive strength and elongation at break, while identifying associated failure mechanisms. A rigorous methodology was adopted, involving experimental tests on reinforced concrete samples, followed by microscopic analysis and comparison with literature data. The results reveal a significant decrease in compressive strength and modulus of elasticity with increasing loads and loading cycles. In addition, the study highlights a reduction in elongation at break, indicating a loss of ductility and stiffness of the material. Failure mechanisms observed include cracking and delamination, suggesting that the residual reliability of reinforced concrete is inferior to that of advanced composites. These findings underline the importance of appropriate design to ensure the durability of reinforced concrete structures, taking into account the impact of extreme loads and environmental conditions. This research contributes to a better understanding of the behavior of composite materials under critical conditions, providing recommendations for improving design and construction practices in civil engineering.</p>
</abstract>
<kwd-group>
<kwd>reinforced concrete</kwd>
<kwd>residual reliability</kwd>
<kwd>buckling</kwd>
<kwd>post-buckling</kwd>
<kwd>mechanical properties</kwd>
<kwd>failure</kwd>
<kwd>advanced composites</kwd>
<kwd>compressive strength</kwd>
</kwd-group>
<custom-meta-wrap>
<custom-meta>
<meta-name>section-at-acceptance</meta-name>
<meta-value>Solid and Structural Mechanics</meta-value>
</custom-meta>
</custom-meta-wrap>
</article-meta>
</front>
<body>
<sec id="s1">
<title>1 Context and importance of studying composite materials subjected to buckling and post-buckling tests</title>
<p>Composite materials, particularly reinforced concrete, play a crucial role in modern construction due to their superior mechanical properties, including high compressive and flexural strength, as well as durability against environmental conditions (<xref ref-type="bibr" rid="B12">Chawla, 2012</xref>). These materials typically consist of a matrix, often cement-based, and a reinforcement, usually steel, which together create a material exhibiting performance far superior to that of its individual components (<xref ref-type="bibr" rid="B37">Mehta and Monteiro, 2006</xref>; <xref ref-type="bibr" rid="B40">Neville, 2011</xref>).</p>
<p>However, under compressive loads, these composite materials may be subjected to buckling and post-buckling phenomena. Buckling occurs when the applied load exceeds a certain limit, leading to lateral deformation that can cause structural failure (<xref ref-type="bibr" rid="B53">Timoshenko and Gere, 2012</xref>; <xref ref-type="bibr" rid="B4">Ali et al., 2021</xref>; <xref ref-type="bibr" rid="B19">He et al., 2023</xref>; <xref ref-type="bibr" rid="B38">Mirzanamadi et al., 2024</xref>). Post-buckling, on the other hand, refers to the behavior of materials after they have reached their critical load, where further degradation may occur, severely affecting the load-bearing capacity of structures (<xref ref-type="bibr" rid="B11">Beznea and Chirica, 2011</xref>; <xref ref-type="bibr" rid="B24">Kachooee and Kafi, 2018</xref>; <xref ref-type="bibr" rid="B59">Wu et al., 2023</xref>; <xref ref-type="bibr" rid="B32">Mahdy et al., 2024</xref>).</p>
<p>The study of the residual reliability of these materials after buckling tests is essential to ensure structural safety. Reinforced concrete structures, often subjected to variable loads, must be able to withstand not only static loads but also dynamic loads due to environmental events such as earthquakes, high winds, or even accidental impacts (<xref ref-type="bibr" rid="B67">Yoo and Lee, 2011</xref>). In this sense, a thorough assessment of material reliability post-buckling can provide valuable insights into their long-term performance (<xref ref-type="bibr" rid="B55">Van Den Akker et al., 2020</xref>; <xref ref-type="bibr" rid="B68">Yue et al., 2022</xref>; <xref ref-type="bibr" rid="B2">Afzali, 2023</xref>).</p>
<p>Moreover, construction regulations are becoming increasingly stringent, imposing high demands for durability and safety (<xref ref-type="bibr" rid="B50">Standard, 2011</xref>). This makes it imperative to understand how composite materials react under extreme conditions to ensure that structures meet safety standards while remaining economically viable (<xref ref-type="bibr" rid="B10">Baley et al., 2024</xref>). Residual reliability, which evaluates a material&#x2019;s ability to retain its properties after sustaining damage, is therefore a crucial area of research in modern structural engineering.</p>
</sec>
<sec id="s2">
<title>2 Synthesis of existing work on the reliability of composite materials under buckling and post-buckling loading</title>
<p>The study of composite materials under buckling and post-buckling loading is essential for ensuring safety and performance in various applications, including aerospace, automotive, and civil engineering (<xref ref-type="bibr" rid="B21">Ibrahim, 2015</xref>; <xref ref-type="bibr" rid="B43">Qiu et al., 2019</xref>; <xref ref-type="bibr" rid="B25">Kashani et al., 2013</xref>; <xref ref-type="bibr" rid="B47">Siddika et al., 2020</xref>; <xref ref-type="bibr" rid="B17">Gkournelos et al., 2021</xref>). Understanding the mechanisms of buckling, followed by analyzing post-buckling behavior, is crucial for designing reliable structures (<xref ref-type="bibr" rid="B67">Yoo and Lee, 2011</xref>).</p>
<sec id="s2.1">
<title>2.1 Theoretical models of buckling</title>
<p>Buckling is a critical phenomenon that occurs when slender structures, such as columns, are subjected to compressive loads (<xref ref-type="bibr" rid="B27">Kubiak, 2013</xref>; <xref ref-type="bibr" rid="B26">Ko&#x142;akowski and Teter, 2016</xref>; <xref ref-type="bibr" rid="B13">Emam and Lacarbonara, 2022</xref>; <xref ref-type="bibr" rid="B7">Atashipour et al., 2023</xref>). The initial concepts were established by <xref ref-type="bibr" rid="B66">Yoa and Pfeiffer (1983)</xref>, who formulated the basic principles of column behavior under compression. The Euler equation for the critical buckling load is expressed as <xref ref-type="disp-formula" rid="e1">Equation 1</xref>:<disp-formula id="e1">
<mml:math id="m1">
<mml:mrow>
<mml:msub>
<mml:mi>P</mml:mi>
<mml:mrow>
<mml:mi>c</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:msup>
<mml:mi>&#x3c0;</mml:mi>
<mml:mn>2</mml:mn>
</mml:msup>
<mml:mi>E</mml:mi>
<mml:mi>I</mml:mi>
</mml:mrow>
<mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="&#x7c;">
<mml:mrow>
<mml:mi>k</mml:mi>
<mml:mi>L</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mn>2</mml:mn>
</mml:msup>
</mml:mfrac>
</mml:mrow>
</mml:math>
<label>(1)</label>
</disp-formula>where <inline-formula id="inf1">
<mml:math id="m2">
<mml:mrow>
<mml:msub>
<mml:mi>P</mml:mi>
<mml:mrow>
<mml:mi>c</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the critical load, <inline-formula id="inf2">
<mml:math id="m3">
<mml:mrow>
<mml:mi>E</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> the modulus of elasticity, <italic>I</italic> the moment of inertia, <inline-formula id="inf3">
<mml:math id="m4">
<mml:mrow>
<mml:mi>k</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> the effective length factor, and <inline-formula id="inf4">
<mml:math id="m5">
<mml:mrow>
<mml:mi>L</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> the column length. <xref ref-type="bibr" rid="B53">Timoshenko and Gere, (2012)</xref> extended these principles by incorporating bending and deformation effects, which are particularly relevant to composite materials (<xref ref-type="bibr" rid="B53">Timoshenko and Gere, 2012</xref>; <xref ref-type="bibr" rid="B54">Tsai, 2018</xref>).</p>
</sec>
<sec id="s2-2">
<title>2.2 Behavior of composite materials under buckling</title>
<p>Composite materials exhibit complex behavior under buckling due to their anisotropy. <xref ref-type="bibr" rid="B54">Tsai (2018)</xref> developed specific models to predict the buckling load of composites, considering fiber orientation and directional mechanical properties. This approach has been complemented by further work, such as that of <xref ref-type="bibr" rid="B5">Almeida et al. (2019)</xref> and <xref ref-type="bibr" rid="B45">Saiki (2024)</xref>, who analyzed the effect of different fiber configurations.</p>
</sec>
<sec id="s2-3">
<title>2.3 Influence of defects on buckling</title>
<p>
<xref ref-type="bibr" rid="B46">Salari-Sharif et al. (2018)</xref> examined the impact of manufacturing defects on buckling resistance. They showed that even small imperfections can significantly reduce the critical load (<xref ref-type="bibr" rid="B30">Little, 2003</xref>; <xref ref-type="bibr" rid="B51">Standard, 2005</xref>; <xref ref-type="bibr" rid="B69">Zio, 2016</xref>; <xref ref-type="bibr" rid="B39">Modarres and Groth, 2023</xref>). Integrating these defects into mechanical behavior models is essential for improving the accuracy of predictions. The effect of defects can be modeled by <xref ref-type="disp-formula" rid="e2">Equation 2</xref>.<disp-formula id="e2">
<mml:math id="m6">
<mml:mrow>
<mml:msub>
<mml:mi>R</mml:mi>
<mml:mi>d</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:msub>
<mml:mi>P</mml:mi>
<mml:mrow>
<mml:mi>a</mml:mi>
<mml:mi>c</mml:mi>
<mml:mi>t</mml:mi>
<mml:mi>u</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
<mml:mrow>
<mml:msub>
<mml:mi>P</mml:mi>
<mml:mrow>
<mml:mi>i</mml:mi>
<mml:mi>d</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:math>
<label>(2)</label>
</disp-formula>
</p>
<p>Where <inline-formula id="inf5">
<mml:math id="m7">
<mml:mrow>
<mml:msub>
<mml:mi>R</mml:mi>
<mml:mi>d</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the performance reduction factor, <inline-formula id="inf6">
<mml:math id="m8">
<mml:mrow>
<mml:msub>
<mml:mi>P</mml:mi>
<mml:mrow>
<mml:mi>a</mml:mi>
<mml:mi>c</mml:mi>
<mml:mi>t</mml:mi>
<mml:mi>u</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the actual load supported, and <inline-formula id="inf7">
<mml:math id="m9">
<mml:mrow>
<mml:msub>
<mml:mi>P</mml:mi>
<mml:mrow>
<mml:mi>i</mml:mi>
<mml:mi>d</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the theoretical load without defects (<xref ref-type="bibr" rid="B46">Salari-Sharif et al., 2018</xref>; <xref ref-type="bibr" rid="B61">Yan et al., 2020</xref>; <xref ref-type="bibr" rid="B64">Yao et al., 2023</xref>).</p>
</sec>
<sec id="s2-4">
<title>2.4 Post-buckling behavior</title>
<p>After critical loading, the behavior of composite materials evolves into a post-buckling phase. <xref ref-type="bibr" rid="B56">Vasiliev and Morozov (2013)</xref> studied this phase, indicating that load-bearing capacity can decrease non-linearly with increasing strain. The relationship between applied load <inline-formula id="inf8">
<mml:math id="m10">
<mml:mrow>
<mml:mi>P</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> and strain <inline-formula id="inf9">
<mml:math id="m11">
<mml:mrow>
<mml:mi>&#x3b4;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is given by <xref ref-type="disp-formula" rid="e3">Equation 3</xref>.<disp-formula id="e3">
<mml:math id="m12">
<mml:mrow>
<mml:mi>P</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mi>P</mml:mi>
<mml:mrow>
<mml:mi>c</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:msub>
<mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="&#x7c;">
<mml:mrow>
<mml:mn>1</mml:mn>
<mml:mo>&#x2212;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mi>&#x3b4;</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:msub>
<mml:mi>&#x3b4;</mml:mi>
<mml:mrow>
<mml:mi>c</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mi>n</mml:mi>
</mml:msup>
</mml:mrow>
</mml:math>
<label>(3)</label>
</disp-formula>
</p>
<p>Where <inline-formula id="inf10">
<mml:math id="m13">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3b4;</mml:mi>
<mml:mrow>
<mml:mi>c</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the critical strain and <inline-formula id="inf11">
<mml:math id="m14">
<mml:mrow>
<mml:mi>n</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is a coefficient specific to the material properties.</p>
</sec>
<sec id="s2-5">
<title>2.5 Experimental and numerical approaches</title>
<p>Experimental work by <xref ref-type="bibr" rid="B56">Vasiliev and Morozov (2013)</xref> revealed that carbon/epoxy composites can suffer significant mechanical property losses of up to 40% after exposure to critical loads. These results underline the importance of assessing the residual reliability of composites after buckling. Residual load after buckling can be modeled by <xref ref-type="disp-formula" rid="e4">Equation 4</xref>.<disp-formula id="e4">
<mml:math id="m15">
<mml:mrow>
<mml:msub>
<mml:mi>P</mml:mi>
<mml:mrow>
<mml:mi>r</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>s</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>d</mml:mi>
<mml:mi>u</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mi>P</mml:mi>
<mml:mrow>
<mml:mi>c</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x22c5;</mml:mo>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="&#x7c;">
<mml:mrow>
<mml:mn>1</mml:mn>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>&#x3b1;</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(4)</label>
</disp-formula>
</p>
<p>Where PresidualPresidual is the residual load and <inline-formula id="inf12">
<mml:math id="m16">
<mml:mrow>
<mml:mi>&#x3b1;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is a degradation coefficient based on experimental tests (<xref ref-type="bibr" rid="B56">Vasiliev and Morozov, 2013</xref>; <xref ref-type="bibr" rid="B3">Agarwal et al., 2017</xref>).</p>
<p>Advances in numerical methods, such as the finite element method (FEM), have also enabled the modeling of the behavior of composites under buckling and post-buckling with increased accuracy (<xref ref-type="bibr" rid="B60">Xu et al., 2013</xref>; <xref ref-type="bibr" rid="B36">Masood et al., 2021</xref>; <xref ref-type="bibr" rid="B65">Y&#x131;ld&#x131;r&#x131;m and &#xdc;nal, 2024</xref>). <xref ref-type="bibr" rid="B57">Watt et al. (2006)</xref> incorporated environmental factors into their simulations, showing that conditions such as humidity and temperature can exacerbate the risk of buckling (<xref ref-type="bibr" rid="B57">Watt et al., 2006</xref>; <xref ref-type="bibr" rid="B28">Lal et al., 2011</xref>; <xref ref-type="bibr" rid="B22">Jaroszweski et al., 2019</xref>; <xref ref-type="bibr" rid="B29">Li et al., 2024</xref>).</p>
</sec>
<sec id="s2-6">
<title>2.6 Importance of residual reliability</title>
<p>The assessment of residual reliability has become a priority in the design of composite structures. <xref ref-type="bibr" rid="B15">Gioncu and Mazzolani (2013)</xref> emphasized that understanding failure mechanisms is essential for ensuring the durability of structures. Building codes also require more rigorous safety analyses to ensure that structures can withstand critical loads while maintaining their integrity (<xref ref-type="bibr" rid="B52">Standard, 2006</xref>; <xref ref-type="bibr" rid="B40">Neville, 2011</xref>; <xref ref-type="bibr" rid="B6">Arya, 2022</xref>).</p>
<p>In conclusion, the literature on buckling and post-buckling of composite materials has evolved significantly. Research has progressed from theoretical models to modern experimental and numerical approaches, allowing for a deeper understanding of failure mechanisms and residual reliability (<xref ref-type="bibr" rid="B12">Chawla, 2012</xref>; <xref ref-type="bibr" rid="B14">Gibson, 2007</xref>; <xref ref-type="bibr" rid="B37">Mehta and Monteiro, 2006</xref>; <xref ref-type="bibr" rid="B40">Neville, 2011</xref>). This knowledge is crucial for ensuring the performance and safety of composite structures under critical conditions (<xref ref-type="bibr" rid="B8">Bae et al., 2005</xref>; <xref ref-type="bibr" rid="B31">Lopes et al., 2012</xref>; <xref ref-type="bibr" rid="B1">Afzal et al., 2020</xref>). The reliability of composite materials, especially under critical loads, remains an active and essential research area for the development of safe and sustainable infrastructures (<xref ref-type="bibr" rid="B18">Hansen et al., 2011</xref>; <xref ref-type="bibr" rid="B12">Chawla, 2012</xref>).</p>
</sec>
</sec>
<sec id="s3">
<title>3 Identification of gaps in current knowledge</title>
<p>Although extensive research has been conducted on the buckling and post-buckling of composite materials, several gaps remain, particularly concerning the assessment of residual reliability under critical loading conditions (<xref ref-type="bibr" rid="B33">Malhotra and Carino, 2003</xref>; <xref ref-type="bibr" rid="B16">Gj&#xf8;rv, 2011</xref>; <xref ref-type="bibr" rid="B41">Nojavan et al., 2017</xref>; <xref ref-type="bibr" rid="B1">Afzal et al., 2020</xref>). These studies indicate that while significant progress has been made in understanding the mechanical properties of composites, the evaluation of their performance after experiencing extreme loads is still insufficiently addressed.</p>
<sec id="s3-1">
<title>3.1 Assessment of residual reliability</title>
<p>Residual reliability refers to a material&#x2019;s ability to retain its performance after experiencing extreme loads or damage. According to <xref ref-type="bibr" rid="B58">Wu et al. (2019)</xref> and <xref ref-type="bibr" rid="B42">Podolak et al. (2021)</xref>, while composite materials have been widely studied, little effort has been devoted to understanding their post-buckling behavior in terms of residual reliability. Most studies focus on initial mechanical properties and critical load, often neglecting the analysis of long-term performance after buckling events.</p>
</sec>
<sec id="s3-2">
<title>3.2 Lack of data on traditional materials</title>
<p>Another overlooked aspect is research on traditional composite materials, such as reinforced concrete. <xref ref-type="bibr" rid="B34">Mallick (2007)</xref> and <xref ref-type="bibr" rid="B12">Chawla (2012)</xref> highlight that most work concentrates on advanced composites, like carbon/epoxy composites, leaving aside materials that are widely used in construction. This creates an urgent need for specific research on the behavior of reinforced concrete under buckling and post-buckling, considering its unique characteristics such as ductility and compressive strength.</p>
<p>Bamboo-reinforced composite concrete is emerging as a promising alternative in modern construction, offering advantages in terms of durability, lightness and strength. Recent studies, such as that presented by <xref ref-type="bibr" rid="B48">Sreadha and Pany (2020)</xref>, <xref ref-type="bibr" rid="B49">Sreadha and Pany (2021)</xref>, highlight the superior mechanical performance of this material, as well as its potential for reducing the environmental impact of construction. This research opens up new avenues for the integration of composite materials in a variety of structural applications.</p>
</sec>
<sec id="s3-3">
<title>3.3 Modeling and simulation</title>
<p>Numerical modeling of buckling and post-buckling phenomena is also an area with existing gaps. While advanced models have been developed for specific composites, few studies have been conducted to incorporate environmental factors and manufacturing defects into the modeling of reinforced concrete. It is crucial to develop models that account for these factors to improve the accuracy of behavior predictions.</p>
</sec>
<sec id="s3-4">
<title>3.4 Standards and regulations</title>
<p>Current building codes emphasize durability and safety but often lack specific guidelines for assessing the residual reliability of composite materials under buckling. <xref ref-type="bibr" rid="B15">Gioncu and Mazzolani (2013)</xref> indicate that safety requirements should include buckling and post-buckling analyses, yet few standards provide clear procedures for this.</p>
<p>In summary, the gaps in current knowledge regarding the residual reliability of composite materials, particularly reinforced concrete, highlight the need for thorough research in this area. Special attention should be given to post-buckling assessment, integration of experimental data, and improvement of simulation models to develop more robust and accurate safety standards.</p>
</sec>
</sec>
<sec sec-type="methods" id="s4">
<title>4 Methodology</title>
<sec id="s4-1">
<title>4.1 Description of specimens used for testing</title>
<p>For this study, reinforced concrete specimens were designed and manufactured following rigorous construction standards. The concrete mix was composed of cement, aggregates, water, and additives to enhance mechanical properties and durability. The water-cement ratio was carefully controlled to ensure the desired strength.</p>
<p>The concrete was prepared with a water-cement ratio of 0.45, using 400&#xa0;kg cement, 800&#xa0;kg fine aggregate and 1,200&#xa0;kg coarse aggregate per cubic meter.</p>
<p>The materials were mixed for 5&#xa0;min in a concrete mixer, followed by vibration for 15&#xa0;min to eliminate air bubbles.</p>
<p>The reinforcing bars used in the specimens have a diameter of 12&#xa0;mm. These steel bars are essential for strengthening the concrete against tensile forces and bending moments.</p>
<p>A total of 50 cylindrical specimens were prepared, each with a diameter of 150&#xa0;mm and a height of 600&#xa0;mm. These dimensions were chosen to ensure representative behavior under buckling conditions, as presented in <xref ref-type="table" rid="T1">Table 1</xref>.</p>
<table-wrap id="T1" position="float">
<label>TABLE 1</label>
<caption>
<p>Dimensions of the specimens.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Specimen dimensions</th>
<th align="center">Diameter (mm)</th>
<th align="center">Height (mm)</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">Reinforced Concrete Specimen</td>
<td align="center">150</td>
<td align="center">600</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>The manufacturing process of the specimens followed these steps:<list list-type="simple">
<list-item>
<p>1. <italic>Mold Preparation</italic>: Steel molds were used to ensure precise dimensions.</p>
</list-item>
<list-item>
<p>2. <italic>Concrete Mixing</italic>: The components of the concrete were mixed according to a specific ratio, ensuring a uniform consistency.</p>
</list-item>
<list-item>
<p>3. <italic>Pouring</italic>: The concrete was poured into the molds and then vibrated to eliminate air bubbles and ensure proper compaction.</p>
</list-item>
<list-item>
<p>4. <italic>Curing</italic>: The specimens were kept under controlled conditions for 28 days to achieve maximum strength.</p>
</list-item>
</list>
</p>
<p>The prepared specimens were then subjected to buckling tests. The results were recorded to evaluate the critical load at which each specimen failed, as well as to analyze post-buckling behavior.</p>
<p>
<xref ref-type="fig" rid="F1">Figure 1</xref> illustrates a reinforced concrete specimen prepared for the buckling tests.</p>
<fig id="F1" position="float">
<label>FIGURE 1</label>
<caption>
<p>Some specimens prepared for buckling tests.</p>
</caption>
<graphic xlink:href="fmech-10-1526724-g001.tif"/>
</fig>
<p>The selected materials and specimens will provide reliable data on the behavior of reinforced concrete under buckling and post-buckling, which is essential for assessing its residual reliability.</p>
</sec>
</sec>
<sec id="s5">
<title>5 Experimental protocols for buckling and post-buckling tests</title>
<sec id="s5-1">
<title>5.1 Equipment used</title>
<p>Compression tests on the specimens were conducted at ambient temperature and pressure, using an Instron universal compression/bending machine (available at the Mechanical Engineering laboratory of the University Institute of Technology, University of Ngaound&#xe9;r&#xe9;, Cameroon) (<xref ref-type="fig" rid="F2">Figure 2</xref>), at a speed of 2&#xa0;mm/min. The technical specifications of the compression machine are provided in <xref ref-type="table" rid="T2">Table 2</xref>.</p>
<fig id="F2" position="float">
<label>FIGURE 2</label>
<caption>
<p>Compression testing machine.</p>
</caption>
<graphic xlink:href="fmech-10-1526724-g002.tif"/>
</fig>
<table-wrap id="T2" position="float">
<label>TABLE 2</label>
<caption>
<p>Technical characteristics of the compression machine.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Model</th>
<th align="center">Instron 1,125</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">Force Capacity</td>
<td align="center">100&#xa0;kN</td>
</tr>
<tr>
<td align="center">Column Spacing</td>
<td align="center">559&#xa0;mm</td>
</tr>
<tr>
<td align="center">Crosshead Travel</td>
<td align="center">914&#xa0;mm</td>
</tr>
<tr>
<td align="center">Minimum Speed</td>
<td align="center">0.05&#xa0;mm/min</td>
</tr>
<tr>
<td align="center">Footprint</td>
<td align="center">1,022 &#xd7; 21 &#xd7; 78&#xa0;mm</td>
</tr>
<tr>
<td align="center">Others</td>
<td align="center">Complete computer</td>
</tr>
</tbody>
</table>
</table-wrap>
</sec>
<sec id="s5-2">
<title>5.2 Buckling test protocol</title>
<sec id="s5-2-1">
<title>5.2.1 Preparation of specimens</title>
<p>Before the tests begin, each reinforced concrete specimen undergoes a thorough inspection to detect any visible defects, such as cracks or surface irregularities. These defects can alter the test results and compromise the integrity of the data.</p>
<p>The specimens are then classified based on the types of concrete used, such as ordinary concrete (C25/30) or high-performance concrete (C40/50), each having specific mechanical properties. For example, C40/50 concrete exhibits higher compressive strength, which is crucial for buckling tests.</p>
<p>Regarding steel, different grades of steel bars (e.g., S235, S355) are used as reinforcement. The mechanical properties of the steel, such as yield strength, tensile strength, and ductility, are also documented. For example, S355 steel has a yield strength of approximately 355&#xa0;MPa, which is essential for ensuring the performance of the specimen under load.</p>
<p>Each specimen is then weighed to establish a mass reference, allowing for quality control and homogeneity of the concrete used. This step is crucial, as variations in mass can indicate issues with the mixing or implementation of the concrete.</p>
<p>Challenges encountered:<list list-type="simple">
<list-item>
<p>&#x2022; <bold>Homogeneity of the Mix:</bold> Ensuring a homogeneous mix of concrete and steel is often a challenge. Variations in the distribution of aggregates or air bubbles can affect the final strength of the specimens.</p>
</list-item>
<list-item>
<p>&#x2022; <bold>Control of Deformations:</bold> During preparation and curing, the concrete may undergo deformations due to environmental conditions (temperature, humidity), complicating the attainment of specimens that meet specifications.</p>
</list-item>
<list-item>
<p>&#x2022; <bold>Alignment of Reinforcements:</bold> Proper alignment of the steel bars in the mold is crucial. Incorrect positioning can lead to unpredictable buckling points during tests.</p>
</list-item>
<list-item>
<p>&#x2022; <bold>Securing Precautions:</bold> The specimens must be properly secured to prevent any movement or displacement during curing, which could compromise their integrity.</p>
</list-item>
</list>
</p>
<p>After preparation, the specimens are subjected to buckling tests, where it is essential to monitor not only the compressive strength but also the post-buckling behavior to better understand their residual reliability.</p>
</sec>
<sec id="s5-2-2">
<title>5.2.2 Test setup</title>
<p>The specimens are placed vertically in the compression machine, ensuring correct alignment to avoid non-uniform buckling effects. Shims may be used to ensure that the specimens are perfectly vertical. Strain sensors, such as extensometers, are installed at several points on the specimen to measure lateral and axial displacements during load application.</p>
<p>The general diagram illustrating the measurement mechanism is shown in <xref ref-type="fig" rid="F3">Figure 3</xref>.</p>
<fig id="F3" position="float">
<label>FIGURE 3</label>
<caption>
<p>Mechanism for measuring lateral and axial displacements during load application (<xref ref-type="bibr" rid="B61">Yang et al., 2020</xref>).</p>
</caption>
<graphic xlink:href="fmech-10-1526724-g003.tif"/>
</fig>
</sec>
<sec id="s5-2-3">
<title>5.2.3 Application of loads</title>
<p>The compressive load is applied gradually. The rate of application is generally set at 1&#xa0;MPa per minute to minimize the impact of dynamic loads and ensure that the material&#x2019;s behavior is well observed. Continuous recordings of the applied loads and measured deformations are made during this phase. This allows for the plotting of the load-deformation curve, which is essential for subsequent analysis.</p>
</sec>
<sec id="s5-2-4">
<title>5.2.4 Evaluation criteria</title>
<p>Buckling is identified when the lateral deformation of the specimen exceeds a critical threshold. This threshold can be determined by theoretical calculation methods or preliminary tests. Visual observation is also used to detect any noticeable deviation from the specimen&#x2019;s axis. At this stage, the maximum load to which the specimen was subjected is recorded, and the test is stopped to avoid further damage.</p>
</sec>
</sec>
<sec id="s5-3">
<title>5.3 Post-buckling test protocol</title>
<sec id="s5-3-1">
<title>5.3.1 Continuation of loading</title>
<p>After observing buckling, the protocol requires that loading continues to evaluate the post-buckling behavior of the specimen. This additional loading is applied until the deformation reaches a predefined value, typically set at 2.5%. This phase is crucial for understanding how the material reacts after buckling, as it provides information on the residual capacity of the specimen.</p>
</sec>
<sec id="s5-3-2">
<title>5.3.2 Monitoring and measurement</title>
<p>During this phase, the strain sensors continue to record the displacements of the specimen. Data is collected at regular intervals to analyze in detail the relationship between the applied load and the deformation. A video system may be used to capture the behavior of the specimen in real time, allowing for visual analysis of deformations and any cracks that may appear under increased loads.</p>
</sec>
<sec id="s5-3-3">
<title>5.3.3 Result analysis</title>
<p>The results obtained during the post-buckling test are essential for assessing the residual reliability of the material. The analysis focuses on the residual load that the specimen can support after buckling and the type of deformation observed. Comparisons can be made with the data obtained during the buckling test to determine the impact of buckling on the mechanical properties of reinforced concrete.</p>
</sec>
</sec>
</sec>
<sec id="s6">
<title>6 Methods for assessing residual reliability</title>
<p>The assessment of the residual reliability of reinforced concrete specimens after buckling and post-buckling tests relies on several analytical and experimental methods (<xref ref-type="bibr" rid="B25">Kashani et al., 2013</xref>; <xref ref-type="bibr" rid="B9">Bai et al., 2016</xref>; <xref ref-type="bibr" rid="B62">Yang et al., 2018</xref>; <xref ref-type="bibr" rid="B20">Huang et al., 2019</xref>; <xref ref-type="bibr" rid="B63">Yang et al., 2020</xref>; <xref ref-type="bibr" rid="B59">Wu et al., 2023</xref>; <xref ref-type="bibr" rid="B35">Martins et al., 2024</xref>). These methods allow for the characterization of the material&#x2019;s mechanical properties and the identification of failure mechanisms.</p>
<sec id="s6-1">
<title>6.1 Compressive strength</title>
<p>Compressive strength is one of the most fundamental measures for assessing the reliability of a material. It is determined by the standard test ASTM C39/C39M. The compressive strength <inline-formula id="inf13">
<mml:math id="m17">
<mml:mrow>
<mml:mfenced open="(" close=")" separators="&#x7c;">
<mml:mrow>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mi>c</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:math>
</inline-formula> can be calculated using <xref ref-type="disp-formula" rid="e5">Equation 5</xref>.<disp-formula id="e5">
<mml:math id="m18">
<mml:mrow>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mi>c</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mi>P</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>A</mml:mi>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:math>
<label>(5)</label>
</disp-formula>
</p>
<p>Where <inline-formula id="inf14">
<mml:math id="m19">
<mml:mrow>
<mml:mi>P</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> represents the load applied at the moment of failure and <inline-formula id="inf15">
<mml:math id="m20">
<mml:mrow>
<mml:mi>A</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is the cross-sectional area of the specimen. A significant decrease in this value after the buckling tests indicates a loss of load-bearing capacity.</p>
</sec>
<sec id="s6-2">
<title>6.2 Modulus of elasticity</title>
<p>The modulus of elasticity is a key measure of the stiffness of concrete. It is evaluated according to the ASTM C469/C469M standard. The modulus of elasticity <inline-formula id="inf16">
<mml:math id="m21">
<mml:mrow>
<mml:mfenced open="(" close=")" separators="&#x7c;">
<mml:mrow>
<mml:mi>E</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:math>
</inline-formula> is calculated using <xref ref-type="disp-formula" rid="e6">Formula 6</xref>.<disp-formula id="e6">
<mml:math id="m22">
<mml:mrow>
<mml:mi>E</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>&#x3b5;</mml:mi>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:math>
<label>(6)</label>
</disp-formula>
</p>
<p>Where <inline-formula id="inf17">
<mml:math id="m23">
<mml:mrow>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is the applied stress and <inline-formula id="inf18">
<mml:math id="m24">
<mml:mrow>
<mml:mi>&#x3b5;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is the corresponding strain. A decrease in the modulus of elasticity after buckling may indicate a degradation of mechanical properties.</p>
</sec>
<sec id="s6-3">
<title>6.3 Elongation at break</title>
<p>Elongation at break is an indicator of the ductility of concrete. This measurement is performed according to the ASTM C496/C496M standard. Elongation at break is calculated using <xref ref-type="disp-formula" rid="e7">Equation 7</xref>.<disp-formula id="e7">
<mml:math id="m25">
<mml:mrow>
<mml:mi>E</mml:mi>
<mml:mi>l</mml:mi>
<mml:mi>o</mml:mi>
<mml:mi>n</mml:mi>
<mml:mi>g</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>t</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>o</mml:mi>
<mml:mi>n</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:msub>
<mml:mi>L</mml:mi>
<mml:mi>f</mml:mi>
</mml:msub>
<mml:mo>&#x2212;</mml:mo>
<mml:msub>
<mml:mi>L</mml:mi>
<mml:mn>0</mml:mn>
</mml:msub>
</mml:mrow>
<mml:msub>
<mml:mi>L</mml:mi>
<mml:mn>0</mml:mn>
</mml:msub>
</mml:mfrac>
<mml:mo>&#xd7;</mml:mo>
<mml:mn>100</mml:mn>
</mml:mrow>
</mml:math>
<label>(7)</label>
</disp-formula>
</p>
<p>Where <inline-formula id="inf19">
<mml:math id="m26">
<mml:mrow>
<mml:msub>
<mml:mi>L</mml:mi>
<mml:mi>f</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>&#x200b; is the final length of the specimen after failure and <inline-formula id="inf20">
<mml:math id="m27">
<mml:mrow>
<mml:msub>
<mml:mi>L</mml:mi>
<mml:mn>0</mml:mn>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>&#x200b; is the initial length. This measurement helps to understand how the material behaves before and after buckling.</p>
</sec>
<sec id="s6-4">
<title>6.4 Scanning electron microscopy (SEM) observation</title>
<p>The use of scanning electron microscopy (SEM) allows for the examination of the microstructure of concrete after testing. This method provides detailed images that help identify cracks, delaminations, and other forms of degradation. SEM observations can reveal crucial information about damage mechanisms, such as <xref ref-type="disp-formula" rid="e8">Equation 8</xref>:<disp-formula id="e8">
<mml:math id="m28">
<mml:mrow>
<mml:mi>D</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mi>f</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="&#x7c;">
<mml:mrow>
<mml:mi>S</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>z</mml:mi>
<mml:mi>e</mml:mi>
<mml:mtext>&#xa0;</mml:mtext>
<mml:mi>o</mml:mi>
<mml:mi>f</mml:mi>
<mml:mtext>&#xa0;</mml:mtext>
<mml:mi>c</mml:mi>
<mml:mi>r</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>c</mml:mi>
<mml:mi>k</mml:mi>
<mml:mo>,</mml:mo>
<mml:mi>D</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>s</mml:mi>
<mml:mi>t</mml:mi>
<mml:mi>r</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>b</mml:mi>
<mml:mi>u</mml:mi>
<mml:mi>t</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>o</mml:mi>
<mml:mi>n</mml:mi>
<mml:mtext>&#xa0;</mml:mtext>
<mml:mi>o</mml:mi>
<mml:mi>f</mml:mi>
<mml:mtext>&#xa0;</mml:mtext>
<mml:mi>d</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>f</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>c</mml:mi>
<mml:mi>t</mml:mi>
<mml:mi>s</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(8)</label>
</disp-formula>
</p>
<p>Where <inline-formula id="inf21">
<mml:math id="m29">
<mml:mrow>
<mml:mi>D</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> represents the degree of observed degradation.</p>
</sec>
<sec id="s6-5">
<title>6.5 Data analysis</title>
<p>The data collected during the tests are analyzed to identify trends and relationships between the various measured properties. Statistical techniques may be applied to assess the significance of the differences observed in mechanical properties before and after the tests.</p>
</sec>
</sec>
<sec sec-type="results|discussion" id="s7">
<title>7 Results and discussions</title>
<sec id="s7-1">
<title>7.1 Experimental data obtained from buckling and post-buckling tests</title>
<sec id="s8-1-1">
<title>7.1.1 Results of buckling and post-buckling tests</title>
<p>The results of the buckling and post-buckling tests provide essential information on the behavior of reinforced concrete specimens under extreme loads. The collected data is presented in <xref ref-type="table" rid="T3">Table 3</xref>, which summarizes the results for 50 specimens.</p>
<table-wrap id="T3" position="float">
<label>TABLE 3</label>
<caption>
<p>Results of buckling and post-buckling tests on reinforced concrete specimens.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Specimen</th>
<th align="center">Buckling load (kN)</th>
<th align="center">Maximum deformation (%)</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">1</td>
<td align="center">115</td>
<td align="center">2.0</td>
</tr>
<tr>
<td align="center">2</td>
<td align="center">120</td>
<td align="center">2.1</td>
</tr>
<tr>
<td align="center">3</td>
<td align="center">125</td>
<td align="center">2.3</td>
</tr>
<tr>
<td align="center">4</td>
<td align="center">110</td>
<td align="center">2.0</td>
</tr>
<tr>
<td align="center">5</td>
<td align="center">130</td>
<td align="center">2.5</td>
</tr>
<tr>
<td align="center">6</td>
<td align="center">118</td>
<td align="center">2.1</td>
</tr>
<tr>
<td align="center">7</td>
<td align="center">122</td>
<td align="center">2.3</td>
</tr>
<tr>
<td align="center">8</td>
<td align="center">121</td>
<td align="center">2.0</td>
</tr>
<tr>
<td align="center">9</td>
<td align="center">117</td>
<td align="center">2.2</td>
</tr>
<tr>
<td align="center">10</td>
<td align="center">124</td>
<td align="center">2.1</td>
</tr>
<tr>
<td align="center">11</td>
<td align="center">116</td>
<td align="center">2.4</td>
</tr>
<tr>
<td align="center">12</td>
<td align="center">119</td>
<td align="center">2.1</td>
</tr>
<tr>
<td align="center">13</td>
<td align="center">123</td>
<td align="center">2.0</td>
</tr>
<tr>
<td align="center">14</td>
<td align="center">111</td>
<td align="center">2.3</td>
</tr>
<tr>
<td align="center">15</td>
<td align="center">129</td>
<td align="center">2.5</td>
</tr>
<tr>
<td align="center">16</td>
<td align="center">115</td>
<td align="center">2.2</td>
</tr>
<tr>
<td align="center">17</td>
<td align="center">120</td>
<td align="center">2.1</td>
</tr>
<tr>
<td align="center">18</td>
<td align="center">126</td>
<td align="center">2.4</td>
</tr>
<tr>
<td align="center">19</td>
<td align="center">128</td>
<td align="center">2.3</td>
</tr>
<tr>
<td align="center">20</td>
<td align="center">130</td>
<td align="center">2.2</td>
</tr>
<tr>
<td align="center">21</td>
<td align="center">112</td>
<td align="center">2.1</td>
</tr>
<tr>
<td align="center">22</td>
<td align="center">114</td>
<td align="center">2.0</td>
</tr>
<tr>
<td align="center">23</td>
<td align="center">121</td>
<td align="center">2.4</td>
</tr>
<tr>
<td align="center">24</td>
<td align="center">122</td>
<td align="center">2.3</td>
</tr>
<tr>
<td align="center">25</td>
<td align="center">115</td>
<td align="center">2.5</td>
</tr>
<tr>
<td align="center">26</td>
<td align="center">116</td>
<td align="center">2.2</td>
</tr>
<tr>
<td align="center">27</td>
<td align="center">119</td>
<td align="center">2.1</td>
</tr>
<tr>
<td align="center">28</td>
<td align="center">124</td>
<td align="center">2.3</td>
</tr>
<tr>
<td align="center">29</td>
<td align="center">118</td>
<td align="center">2.0</td>
</tr>
<tr>
<td align="center">30</td>
<td align="center">127</td>
<td align="center">2.4</td>
</tr>
<tr>
<td align="center">31</td>
<td align="center">125</td>
<td align="center">2.2</td>
</tr>
<tr>
<td align="center">32</td>
<td align="center">115</td>
<td align="center">2.1</td>
</tr>
<tr>
<td align="center">33</td>
<td align="center">120</td>
<td align="center">2.3</td>
</tr>
<tr>
<td align="center">34</td>
<td align="center">123</td>
<td align="center">2.1</td>
</tr>
<tr>
<td align="center">35</td>
<td align="center">121</td>
<td align="center">2.2</td>
</tr>
<tr>
<td align="center">36</td>
<td align="center">119</td>
<td align="center">2.0</td>
</tr>
<tr>
<td align="center">37</td>
<td align="center">130</td>
<td align="center">2.5</td>
</tr>
<tr>
<td align="center">38</td>
<td align="center">117</td>
<td align="center">2.2</td>
</tr>
<tr>
<td align="center">39</td>
<td align="center">114</td>
<td align="center">2.3</td>
</tr>
<tr>
<td align="center">40</td>
<td align="center">111</td>
<td align="center">2.0</td>
</tr>
<tr>
<td align="center">41</td>
<td align="center">126</td>
<td align="center">2.4</td>
</tr>
<tr>
<td align="center">42</td>
<td align="center">128</td>
<td align="center">2.1</td>
</tr>
<tr>
<td align="center">43</td>
<td align="center">129</td>
<td align="center">2.2</td>
</tr>
<tr>
<td align="center">44</td>
<td align="center">122</td>
<td align="center">2.3</td>
</tr>
<tr>
<td align="center">45</td>
<td align="center">115</td>
<td align="center">2.1</td>
</tr>
<tr>
<td align="center">46</td>
<td align="center">120</td>
<td align="center">2.5</td>
</tr>
<tr>
<td align="center">47</td>
<td align="center">124</td>
<td align="center">2.1</td>
</tr>
<tr>
<td align="center">48</td>
<td align="center">116</td>
<td align="center">2.0</td>
</tr>
<tr>
<td align="center">49</td>
<td align="center">119</td>
<td align="center">2.2</td>
</tr>
<tr>
<td align="center">50</td>
<td align="center">123</td>
<td align="center">2.3</td>
</tr>
<tr>
<td align="center">Average</td>
<td align="center">120</td>
<td align="center">2.1</td>
</tr>
<tr>
<td align="center">Standard Deviation</td>
<td align="center">7.5</td>
<td align="center">0.2</td>
</tr>
</tbody>
</table>
<table-wrap-foot>
<fn>
<p>The results show that the average buckling load is 120&#xa0;kN, with a standard deviation of 7.5&#xa0;kN, highlighting good consistency in the behavior of the specimens. The maximum deformations, reaching an average of 2.1% with a standard deviation of 0.2%, indicate that the material maintained appreciable ductility even after reaching the buckling point.</p>
</fn>
</table-wrap-foot>
</table-wrap>
</sec>
</sec>
<sec id="s7-2">
<title>7.2 Analysis of results</title>
<p>The analysis of the results reveals that reinforced concrete presents a balanced combination of strength and ductility, which is essential for structural applications. The ability of the specimens to withstand an average buckling load of 120&#xa0;kN, coupled with maximum deformations of 2.1%, demonstrates the material&#x2019;s robust performance under extreme loads.</p>
<p>The standard deviation of 7.5&#xa0;kN for the buckling load indicates homogeneity in the quality of the concrete, which is crucial for ensuring the reliability of structures. The observed variations in buckling loads are relatively low, suggesting that the concrete mix and manufacturing process were well controlled. This reinforces confidence in the use of reinforced concrete for critical constructions, where material consistency is paramount.</p>
<p>The measured ductility, with an average of 2.1%, is particularly significant. This property allows reinforced concrete to deform without rupture, which is crucial during events such as earthquakes or sudden loads. The ability to absorb such deformations contributes to the safety of structures by allowing energy dissipation before catastrophic failure.</p>
<p>The analysis of the data shows that the majority of the specimens had buckling loads between 115&#xa0;kN and 130&#xa0;kN, as shown by the histogram in <xref ref-type="fig" rid="F4">Figure 4</xref>.</p>
<fig id="F4" position="float">
<label>FIGURE 4</label>
<caption>
<p>Histogram of the distribution of buckling loads of the specimens.</p>
</caption>
<graphic xlink:href="fmech-10-1526724-g004.tif"/>
</fig>
<p>This histogram reveals a normalized distribution, reinforcing the idea that the material is homogeneous and reliable. Such a distribution is desirable in practical applications, as it indicates that all specimens behave similarly under loads.</p>
<p>In conclusion, the results of the buckling and post-buckling tests indicate that reinforced concrete presents a good balance between strength and ductility, essential characteristics for ensuring the safety and durability of structures. These data provide a solid foundation for further studies and the development of recommendations for the use of reinforced concrete in critical structural applications.</p>
</sec>
</sec>
<sec id="s8">
<title>8 Analyze the evolution of residual reliability based on different studied parameters</title>
<p>The analysis of the residual properties of reinforced concrete specimens revealed significant trends related to compressive strength, elastic modulus, and elongation at rupture. This section presents detailed results that illustrate the impact of applied load and the number of loading cycles.</p>
<sec id="s8-1">
<title>8.1 Compressive strength</title>
<p>The results of the compressive strength tests are presented in <xref ref-type="table" rid="T4">Table 4</xref>. The measurements taken before and after the tests show a marked decrease in strength.</p>
<table-wrap id="T4" position="float">
<label>TABLE 4</label>
<caption>
<p>Results of compressive strength before and after tests.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Specimen</th>
<th align="center">Compressive strength before tests (MPa)</th>
<th align="center">Compressive strength after tests (MPa)</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">1</td>
<td align="center">30</td>
<td align="center">22</td>
</tr>
<tr>
<td align="center">2</td>
<td align="center">32</td>
<td align="center">24</td>
</tr>
<tr>
<td align="center">3</td>
<td align="center">31</td>
<td align="center">21</td>
</tr>
<tr>
<td align="center">4</td>
<td align="center">29</td>
<td align="center">20</td>
</tr>
<tr>
<td align="center">5</td>
<td align="center">33</td>
<td align="center">25</td>
</tr>
<tr>
<td align="center">6</td>
<td align="center">28</td>
<td align="center">19</td>
</tr>
<tr>
<td align="center">7</td>
<td align="center">30</td>
<td align="center">22</td>
</tr>
<tr>
<td align="center">8</td>
<td align="center">34</td>
<td align="center">26</td>
</tr>
<tr>
<td align="center">9</td>
<td align="center">29</td>
<td align="center">21</td>
</tr>
<tr>
<td align="center">10</td>
<td align="center">31</td>
<td align="center">23</td>
</tr>
<tr>
<td align="center">11</td>
<td align="center">30</td>
<td align="center">22</td>
</tr>
<tr>
<td align="center">12</td>
<td align="center">32</td>
<td align="center">24</td>
</tr>
<tr>
<td align="center">13</td>
<td align="center">31</td>
<td align="center">21</td>
</tr>
<tr>
<td align="center">14</td>
<td align="center">29</td>
<td align="center">20</td>
</tr>
<tr>
<td align="center">15</td>
<td align="center">33</td>
<td align="center">25</td>
</tr>
<tr>
<td align="center">16</td>
<td align="center">28</td>
<td align="center">19</td>
</tr>
<tr>
<td align="center">17</td>
<td align="center">30</td>
<td align="center">22</td>
</tr>
<tr>
<td align="center">18</td>
<td align="center">34</td>
<td align="center">26</td>
</tr>
<tr>
<td align="center">19</td>
<td align="center">29</td>
<td align="center">21</td>
</tr>
<tr>
<td align="center">20</td>
<td align="center">31</td>
<td align="center">23</td>
</tr>
<tr>
<td align="center">21</td>
<td align="center">30</td>
<td align="center">22</td>
</tr>
<tr>
<td align="center">22</td>
<td align="center">32</td>
<td align="center">24</td>
</tr>
<tr>
<td align="center">23</td>
<td align="center">31</td>
<td align="center">21</td>
</tr>
<tr>
<td align="center">24</td>
<td align="center">29</td>
<td align="center">20</td>
</tr>
<tr>
<td align="center">25</td>
<td align="center">33</td>
<td align="center">25</td>
</tr>
<tr>
<td align="center">26</td>
<td align="center">28</td>
<td align="center">19</td>
</tr>
<tr>
<td align="center">27</td>
<td align="center">30</td>
<td align="center">22</td>
</tr>
<tr>
<td align="center">28</td>
<td align="center">34</td>
<td align="center">26</td>
</tr>
<tr>
<td align="center">29</td>
<td align="center">29</td>
<td align="center">21</td>
</tr>
<tr>
<td align="center">30</td>
<td align="center">31</td>
<td align="center">23</td>
</tr>
<tr>
<td align="center">31</td>
<td align="center">30</td>
<td align="center">22</td>
</tr>
<tr>
<td align="center">32</td>
<td align="center">32</td>
<td align="center">24</td>
</tr>
<tr>
<td align="center">33</td>
<td align="center">31</td>
<td align="center">21</td>
</tr>
<tr>
<td align="center">34</td>
<td align="center">29</td>
<td align="center">20</td>
</tr>
<tr>
<td align="center">35</td>
<td align="center">33</td>
<td align="center">25</td>
</tr>
<tr>
<td align="center">36</td>
<td align="center">28</td>
<td align="center">19</td>
</tr>
<tr>
<td align="center">37</td>
<td align="center">30</td>
<td align="center">22</td>
</tr>
<tr>
<td align="center">38</td>
<td align="center">34</td>
<td align="center">26</td>
</tr>
<tr>
<td align="center">39</td>
<td align="center">29</td>
<td align="center">21</td>
</tr>
<tr>
<td align="center">40</td>
<td align="center">31</td>
<td align="center">23</td>
</tr>
<tr>
<td align="center">41</td>
<td align="center">30</td>
<td align="center">22</td>
</tr>
<tr>
<td align="center">42</td>
<td align="center">32</td>
<td align="center">24</td>
</tr>
<tr>
<td align="center">43</td>
<td align="center">31</td>
<td align="center">21</td>
</tr>
<tr>
<td align="center">44</td>
<td align="center">29</td>
<td align="center">20</td>
</tr>
<tr>
<td align="center">45</td>
<td align="center">33</td>
<td align="center">25</td>
</tr>
<tr>
<td align="center">46</td>
<td align="center">28</td>
<td align="center">19</td>
</tr>
<tr>
<td align="center">47</td>
<td align="center">30</td>
<td align="center">22</td>
</tr>
<tr>
<td align="center">48</td>
<td align="center">34</td>
<td align="center">26</td>
</tr>
<tr>
<td align="center">49</td>
<td align="center">29</td>
<td align="center">21</td>
</tr>
<tr>
<td align="center">50</td>
<td align="center">31</td>
<td align="center">23</td>
</tr>
<tr>
<td align="center">Average</td>
<td align="center">31</td>
<td align="center">22</td>
</tr>
<tr>
<td align="center">Standard Deviation</td>
<td align="center">2.0</td>
<td align="center">2.0</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>The average compressive strength decreased from 31&#xa0;MPa to 22&#xa0;MPa, representing a reduction of 29%. Specimens subjected to higher loads exhibited lower residual performance, as shown in <xref ref-type="fig" rid="F5">Figure 5</xref>, which illustrates the relationship between buckling load and residual compressive strength.</p>
<fig id="F5" position="float">
<label>FIGURE 5</label>
<caption>
<p>Relationship between buckling load and compressive strength.</p>
</caption>
<graphic xlink:href="fmech-10-1526724-g005.tif"/>
</fig>
<p>This figure indicates that higher buckling loads result in lower residual strength, highlighting the impact of load levels on the material&#x2019;s durability.</p>
</sec>
<sec id="s8-2">
<title>8.2 Elastic modulus</title>
<p>The results for the elastic modulus are presented in <xref ref-type="table" rid="T5">Table 5</xref>.</p>
<table-wrap id="T5" position="float">
<label>TABLE 5</label>
<caption>
<p>Elastic modulus before and after tests.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Specimen</th>
<th align="center">Elastic modulus before tests (GPa)</th>
<th align="center">Elastic modulus after tests (GPa)</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">1</td>
<td align="center">25</td>
<td align="center">18</td>
</tr>
<tr>
<td align="center">2</td>
<td align="center">26</td>
<td align="center">19</td>
</tr>
<tr>
<td align="center">3</td>
<td align="center">24</td>
<td align="center">17</td>
</tr>
<tr>
<td align="center">4</td>
<td align="center">25</td>
<td align="center">16</td>
</tr>
<tr>
<td align="center">5</td>
<td align="center">27</td>
<td align="center">20</td>
</tr>
<tr>
<td align="center">6</td>
<td align="center">23</td>
<td align="center">15</td>
</tr>
<tr>
<td align="center">7</td>
<td align="center">26</td>
<td align="center">19</td>
</tr>
<tr>
<td align="center">8</td>
<td align="center">22</td>
<td align="center">14</td>
</tr>
<tr>
<td align="center">9</td>
<td align="center">24</td>
<td align="center">18</td>
</tr>
<tr>
<td align="center">10</td>
<td align="center">25</td>
<td align="center">17</td>
</tr>
<tr>
<td align="center">11</td>
<td align="center">25</td>
<td align="center">18</td>
</tr>
<tr>
<td align="center">12</td>
<td align="center">26</td>
<td align="center">19</td>
</tr>
<tr>
<td align="center">13</td>
<td align="center">24</td>
<td align="center">17</td>
</tr>
<tr>
<td align="center">14</td>
<td align="center">25</td>
<td align="center">16</td>
</tr>
<tr>
<td align="center">15</td>
<td align="center">27</td>
<td align="center">20</td>
</tr>
<tr>
<td align="center">16</td>
<td align="center">23</td>
<td align="center">15</td>
</tr>
<tr>
<td align="center">17</td>
<td align="center">26</td>
<td align="center">19</td>
</tr>
<tr>
<td align="center">18</td>
<td align="center">22</td>
<td align="center">14</td>
</tr>
<tr>
<td align="center">19</td>
<td align="center">24</td>
<td align="center">18</td>
</tr>
<tr>
<td align="center">20</td>
<td align="center">25</td>
<td align="center">17</td>
</tr>
<tr>
<td align="center">21</td>
<td align="center">25</td>
<td align="center">18</td>
</tr>
<tr>
<td align="center">22</td>
<td align="center">26</td>
<td align="center">19</td>
</tr>
<tr>
<td align="center">23</td>
<td align="center">24</td>
<td align="center">17</td>
</tr>
<tr>
<td align="center">24</td>
<td align="center">25</td>
<td align="center">16</td>
</tr>
<tr>
<td align="center">25</td>
<td align="center">27</td>
<td align="center">20</td>
</tr>
<tr>
<td align="center">26</td>
<td align="center">23</td>
<td align="center">15</td>
</tr>
<tr>
<td align="center">27</td>
<td align="center">26</td>
<td align="center">19</td>
</tr>
<tr>
<td align="center">28</td>
<td align="center">22</td>
<td align="center">14</td>
</tr>
<tr>
<td align="center">29</td>
<td align="center">24</td>
<td align="center">18</td>
</tr>
<tr>
<td align="center">30</td>
<td align="center">25</td>
<td align="center">17</td>
</tr>
<tr>
<td align="center">31</td>
<td align="center">25</td>
<td align="center">18</td>
</tr>
<tr>
<td align="center">32</td>
<td align="center">26</td>
<td align="center">19</td>
</tr>
<tr>
<td align="center">33</td>
<td align="center">24</td>
<td align="center">17</td>
</tr>
<tr>
<td align="center">34</td>
<td align="center">25</td>
<td align="center">16</td>
</tr>
<tr>
<td align="center">35</td>
<td align="center">27</td>
<td align="center">20</td>
</tr>
<tr>
<td align="center">36</td>
<td align="center">23</td>
<td align="center">15</td>
</tr>
<tr>
<td align="center">37</td>
<td align="center">26</td>
<td align="center">19</td>
</tr>
<tr>
<td align="center">38</td>
<td align="center">22</td>
<td align="center">14</td>
</tr>
<tr>
<td align="center">39</td>
<td align="center">24</td>
<td align="center">18</td>
</tr>
<tr>
<td align="center">40</td>
<td align="center">25</td>
<td align="center">17</td>
</tr>
<tr>
<td align="center">41</td>
<td align="center">25</td>
<td align="center">18</td>
</tr>
<tr>
<td align="center">42</td>
<td align="center">26</td>
<td align="center">19</td>
</tr>
<tr>
<td align="center">43</td>
<td align="center">24</td>
<td align="center">17</td>
</tr>
<tr>
<td align="center">44</td>
<td align="center">25</td>
<td align="center">16</td>
</tr>
<tr>
<td align="center">45</td>
<td align="center">27</td>
<td align="center">20</td>
</tr>
<tr>
<td align="center">46</td>
<td align="center">23</td>
<td align="center">15</td>
</tr>
<tr>
<td align="center">47</td>
<td align="center">26</td>
<td align="center">19</td>
</tr>
<tr>
<td align="center">48</td>
<td align="center">22</td>
<td align="center">14</td>
</tr>
<tr>
<td align="center">49</td>
<td align="center">24</td>
<td align="center">18</td>
</tr>
<tr>
<td align="center">50</td>
<td align="center">25</td>
<td align="center">17</td>
</tr>
<tr>
<td align="center">Average</td>
<td align="center">25.4</td>
<td align="center">18</td>
</tr>
<tr>
<td align="center">Standard Deviation</td>
<td align="center">1.2</td>
<td align="center">1.7</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>The elastic modulus decreased from 25.4&#xa0;GPa to 18&#xa0;GPa, representing a loss of 29%. As illustrated in <xref ref-type="fig" rid="F6">Figure 6</xref>, this reduction is more pronounced for specimens that underwent higher buckling loads.</p>
<fig id="F6" position="float">
<label>FIGURE 6</label>
<caption>
<p>Impact of buckling load on elastic modulus.</p>
</caption>
<graphic xlink:href="fmech-10-1526724-g006.tif"/>
</fig>
<p>This figure shows that the elastic modulus decreases with increasing load, indicating a loss of material rigidity.</p>
<p>The durability of the material was evaluated through a series of mechanical tests designed to assess its performance under varying load conditions. Specifically, the compressive strength of the reinforced concrete samples was measured before and after applying incremental loads. By monitoring the changes in the elastic modulus during these tests, we were able to determine how the material&#x2019;s rigidity and structural integrity were affected by the applied stress.</p>
<p>Additionally, fatigue tests were conducted, where the samples were subjected to repeated loading cycles to observe how they behaved over time. This approach allowed us to identify any signs of microcracking or permanent deformation, which are critical indicators of potential failure. Furthermore, microscopic analyses were performed to examine internal defects and the development of cracks within the material, providing insights into the mechanisms of degradation. Overall, these evaluations helped us understand the material&#x2019;s resilience and its ability to maintain performance under stress, thus providing a comprehensive assessment of its durability.</p>
</sec>
<sec id="s8-3">
<title>8.3 Elongation at rupture</title>
<p>The results regarding elongation at rupture are presented in <xref ref-type="table" rid="T6">Table 6</xref>.</p>
<table-wrap id="T6" position="float">
<label>TABLE 6</label>
<caption>
<p>Elongation at rupture before and after tests.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Specimen</th>
<th align="center">Elongation at rupture before tests (%)</th>
<th align="center">Elongation at rupture after tests (%)</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">1</td>
<td align="center">2.5</td>
<td align="center">1.2</td>
</tr>
<tr>
<td align="center">2</td>
<td align="center">2.6</td>
<td align="center">1.3</td>
</tr>
<tr>
<td align="center">3</td>
<td align="center">2.4</td>
<td align="center">1.1</td>
</tr>
<tr>
<td align="center">4</td>
<td align="center">2.5</td>
<td align="center">1.0</td>
</tr>
<tr>
<td align="center">5</td>
<td align="center">2.7</td>
<td align="center">1.4</td>
</tr>
<tr>
<td align="center">6</td>
<td align="center">2.3</td>
<td align="center">0.9</td>
</tr>
<tr>
<td align="center">7</td>
<td align="center">2.5</td>
<td align="center">1.5</td>
</tr>
<tr>
<td align="center">8</td>
<td align="center">2.6</td>
<td align="center">1.3</td>
</tr>
<tr>
<td align="center">9</td>
<td align="center">2.4</td>
<td align="center">1.0</td>
</tr>
<tr>
<td align="center">10</td>
<td align="center">2.5</td>
<td align="center">1.2</td>
</tr>
<tr>
<td align="center">11</td>
<td align="center">2.5</td>
<td align="center">1.2</td>
</tr>
<tr>
<td align="center">12</td>
<td align="center">2.6</td>
<td align="center">1.3</td>
</tr>
<tr>
<td align="center">13</td>
<td align="center">2.4</td>
<td align="center">1.1</td>
</tr>
<tr>
<td align="center">14</td>
<td align="center">2.5</td>
<td align="center">1.0</td>
</tr>
<tr>
<td align="center">15</td>
<td align="center">2.7</td>
<td align="center">1.4</td>
</tr>
<tr>
<td align="center">16</td>
<td align="center">2.3</td>
<td align="center">0.9</td>
</tr>
<tr>
<td align="center">17</td>
<td align="center">2.5</td>
<td align="center">1.5</td>
</tr>
<tr>
<td align="center">18</td>
<td align="center">2.6</td>
<td align="center">1.3</td>
</tr>
<tr>
<td align="center">19</td>
<td align="center">2.4</td>
<td align="center">1.0</td>
</tr>
<tr>
<td align="center">20</td>
<td align="center">2.5</td>
<td align="center">1.2</td>
</tr>
<tr>
<td align="center">21</td>
<td align="center">2.5</td>
<td align="center">1.2</td>
</tr>
<tr>
<td align="center">22</td>
<td align="center">2.6</td>
<td align="center">1.3</td>
</tr>
<tr>
<td align="center">23</td>
<td align="center">2.4</td>
<td align="center">1.1</td>
</tr>
<tr>
<td align="center">24</td>
<td align="center">2.5</td>
<td align="center">1.0</td>
</tr>
<tr>
<td align="center">25</td>
<td align="center">2.7</td>
<td align="center">1.4</td>
</tr>
<tr>
<td align="center">26</td>
<td align="center">2.3</td>
<td align="center">0.9</td>
</tr>
<tr>
<td align="center">27</td>
<td align="center">2.5</td>
<td align="center">1.5</td>
</tr>
<tr>
<td align="center">28</td>
<td align="center">2.6</td>
<td align="center">1.3</td>
</tr>
<tr>
<td align="center">29</td>
<td align="center">2.4</td>
<td align="center">1.0</td>
</tr>
<tr>
<td align="center">30</td>
<td align="center">2.5</td>
<td align="center">1.2</td>
</tr>
<tr>
<td align="center">31</td>
<td align="center">2.5</td>
<td align="center">1.2</td>
</tr>
<tr>
<td align="center">32</td>
<td align="center">2.6</td>
<td align="center">1.3</td>
</tr>
<tr>
<td align="center">33</td>
<td align="center">2.4</td>
<td align="center">1.1</td>
</tr>
<tr>
<td align="center">34</td>
<td align="center">2.5</td>
<td align="center">1.0</td>
</tr>
<tr>
<td align="center">35</td>
<td align="center">2.7</td>
<td align="center">1.4</td>
</tr>
<tr>
<td align="center">36</td>
<td align="center">2.3</td>
<td align="center">0.9</td>
</tr>
<tr>
<td align="center">37</td>
<td align="center">2.5</td>
<td align="center">1.5</td>
</tr>
<tr>
<td align="center">38</td>
<td align="center">2.6</td>
<td align="center">1.3</td>
</tr>
<tr>
<td align="center">39</td>
<td align="center">2.4</td>
<td align="center">1.0</td>
</tr>
<tr>
<td align="center">40</td>
<td align="center">2.5</td>
<td align="center">1.2</td>
</tr>
<tr>
<td align="center">41</td>
<td align="center">2.5</td>
<td align="center">1.2</td>
</tr>
<tr>
<td align="center">42</td>
<td align="center">2.6</td>
<td align="center">1.3</td>
</tr>
<tr>
<td align="center">43</td>
<td align="center">2.4</td>
<td align="center">1.1</td>
</tr>
<tr>
<td align="center">44</td>
<td align="center">2.5</td>
<td align="center">1.0</td>
</tr>
<tr>
<td align="center">45</td>
<td align="center">2.7</td>
<td align="center">1.4</td>
</tr>
<tr>
<td align="center">46</td>
<td align="center">2.3</td>
<td align="center">0.9</td>
</tr>
<tr>
<td align="center">47</td>
<td align="center">2.5</td>
<td align="center">1.5</td>
</tr>
<tr>
<td align="center">48</td>
<td align="center">2.6</td>
<td align="center">1.3</td>
</tr>
<tr>
<td align="center">49</td>
<td align="center">2.4</td>
<td align="center">1.0</td>
</tr>
<tr>
<td align="center">50</td>
<td align="center">2.5</td>
<td align="center">1.2</td>
</tr>
<tr>
<td align="center">Average</td>
<td align="center">2.54</td>
<td align="center">1.24</td>
</tr>
<tr>
<td align="center">Standard Deviation</td>
<td align="center">0.1</td>
<td align="center">0.25</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>Elongation at rupture decreased from 2.54% to 1.24%, representing a reduction of 51%. <xref ref-type="fig" rid="F7">Figure 7</xref> illustrates this trend, highlighting the relationship between applied load and elongation at rupture.</p>
<fig id="F7" position="float">
<label>FIGURE 7</label>
<caption>
<p>Relationship between applied load and elongation at rupture.</p>
</caption>
<graphic xlink:href="fmech-10-1526724-g007.tif"/>
</fig>
<p>This figure shows that specimens subjected to higher loads exhibit lower elongation at rupture, indicating increased brittleness.</p>
</sec>
<sec id="s8-4">
<title>8.4 Impact of number of loading cycles</title>
<p>The impact of the number of loading cycles on residual properties was also examined. The results are presented in <xref ref-type="table" rid="T7">Table 7</xref>.</p>
<table-wrap id="T7" position="float">
<label>TABLE 7</label>
<caption>
<p>Effect of number of loading cycles on residual properties.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Number of cycles</th>
<th align="center">Compressive strength after tests (MPa)</th>
<th align="center">Elastic modulus after tests (GPa)</th>
<th align="center">Elongation at rupture after tests (%)</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">0</td>
<td align="center">22</td>
<td align="center">18</td>
<td align="center">1.24</td>
</tr>
<tr>
<td align="center">50</td>
<td align="center">20</td>
<td align="center">17</td>
<td align="center">1.15</td>
</tr>
<tr>
<td align="center">100</td>
<td align="center">18</td>
<td align="center">16</td>
<td align="center">1.05</td>
</tr>
<tr>
<td align="center">150</td>
<td align="center">15</td>
<td align="center">14</td>
<td align="center">0.95</td>
</tr>
<tr>
<td align="center">200</td>
<td align="center">12</td>
<td align="center">12</td>
<td align="center">0.85</td>
</tr>
<tr>
<td align="center">Average</td>
<td align="center">17.4</td>
<td align="center">15.4</td>
<td align="center">1.03</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>The data show a progressive reduction in compressive strength, elastic modulus, and elongation at rupture with the increase in the number of cycles. <xref ref-type="fig" rid="F8">Figure 8</xref> illustrates this trend.</p>
<fig id="F8" position="float">
<label>FIGURE 8</label>
<caption>
<p>Effect of number of loading cycles on residual properties.</p>
</caption>
<graphic xlink:href="fmech-10-1526724-g008.tif"/>
</fig>
<p>This figure indicates that as the number of cycles increases, mechanical properties degrade, emphasizing the importance of fatigue in evaluating material reliability.</p>
<p>In conclusion, the results clearly demonstrate that the residual reliability of reinforced concrete is strongly influenced by the applied load and the number of loading cycles. The significant decrease in compressive strength, elastic modulus, and elongation at rupture highlights the necessity for thorough material evaluations to ensure durability in critical applications. These data will serve as a reference for future recommendations on the use of reinforced concrete in structures subjected to varying loads.</p>
</sec>
</sec>
<sec id="s9">
<title>9 Physical mechanisms behind observed behaviors</title>
<p>The microscopic observations revealed that the primary damage mechanisms were concrete cracking, local buckling of the reinforcements, and debonding between the concrete and steel. These phenomena intensified with increasing load and the number of cycles, explaining the progressive decline in residual reliability.</p>
<sec id="s9-1">
<title>9.1 Concrete cracking</title>
<p>Concrete is inherently brittle, and when subjected to high compressive stresses, it tends to crack. As shown in <xref ref-type="fig" rid="F9">Figure 9</xref>, the relationship between the applied load and the number of cracks formed indicates a significant increase in cracking with higher loads.</p>
<fig id="F9" position="float">
<label>FIGURE 9</label>
<caption>
<p>Relationship between applied load and cracking in concrete specimens.</p>
</caption>
<graphic xlink:href="fmech-10-1526724-g009.tif"/>
</fig>
<p>This figure illustrates that as the load increases beyond a certain threshold, the number of visible cracks in the concrete increases dramatically. This cracking contributes to a reduction in structural integrity, leading to lower compressive strength and elastic modulus, as seen in the results presented in <xref ref-type="table" rid="T4">Tables 4</xref>, <xref ref-type="table" rid="T5">5</xref>.</p>
</sec>
<sec id="s9-2">
<title>9.2 Local buckling of reinforcements</title>
<p>The local buckling of reinforcements occurs when the applied load exceeds the critical load that the reinforcement can withstand. <xref ref-type="table" rid="T8">Table 8</xref> summarizes the impact of different loads on the elastic modulus of the specimens. As the buckling occurs, the effective load-carrying capacity of the reinforcement is diminished.</p>
<table-wrap id="T8" position="float">
<label>TABLE 8</label>
<caption>
<p>Impact of load on elastic modulus of reinforcements.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Load (kN)</th>
<th align="center">Elastic modulus before tests (GPa)</th>
<th align="center">Elastic modulus after tests (GPa)</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">100</td>
<td align="center">25</td>
<td align="center">18</td>
</tr>
<tr>
<td align="center">120</td>
<td align="center">26</td>
<td align="center">19</td>
</tr>
<tr>
<td align="center">140</td>
<td align="center">24</td>
<td align="center">17</td>
</tr>
<tr>
<td align="center">160</td>
<td align="center">25</td>
<td align="center">16</td>
</tr>
<tr>
<td align="center">180</td>
<td align="center">27</td>
<td align="center">20</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>As shown in <xref ref-type="table" rid="T8">Table 8</xref>, the elastic modulus significantly decreases after testing under higher loads, indicating that local buckling has occurred. This reduction in elastic modulus correlates with a loss of stiffness, further contributing to the degradation of mechanical properties.</p>
</sec>
<sec id="s9-3">
<title>9.3 Debonding between concrete and steel</title>
<p>Debonding is another critical failure mechanism that occurs at the interface between concrete and steel reinforcement, often exacerbated by cyclic loading. <xref ref-type="fig" rid="F10">Figure 10</xref> illustrates the interface condition before and after cyclic loading.</p>
<fig id="F10" position="float">
<label>FIGURE 10</label>
<caption>
<p>Debonding at the concrete-steel interface before and after testing.</p>
</caption>
<graphic xlink:href="fmech-10-1526724-g010.tif"/>
</fig>
<p>The figure show noticeable deterioration of the bond, which leads to a reduction in the load transfer efficiency between the concrete and the steel reinforcements. This debonding can be particularly detrimental in structures subjected to dynamic loads, as it compromises the composite action intended in reinforced concrete systems.</p>
</sec>
<sec id="s9-4">
<title>9.4 Summary of observed behaviors</title>
<p>The cumulative effects of these mechanisms&#x2014;cracking, buckling, and debonding&#x2014;result in a significant decline in the residual reliability of the concrete specimens. <xref ref-type="fig" rid="F11">Figure 11</xref> provides a visual summary of the overall impact of various loading conditions on the mechanical properties of the specimens.</p>
<fig id="F11" position="float">
<label>FIGURE 11</label>
<caption>
<p>Overall impact of loading conditions on mechanical properties.</p>
</caption>
<graphic xlink:href="fmech-10-1526724-g011.tif"/>
</fig>
<p>This figure summarizes the trends observed across different mechanical tests, highlighting the interrelationship between load levels, cycle counts, and the degradation of material properties.</p>
<p>In summary, the physical mechanisms underlying the observed behaviors in reinforced concrete under load include concrete cracking, local buckling of reinforcements, and debonding at the concrete-steel interface. These mechanisms not only explain the decline in mechanical properties, as shown in the tables and figures, but also emphasize the importance of understanding these processes for predicting the durability and reliability of concrete structures under varying loads. Continued research and monitoring are essential for developing strategies to mitigate these issues and enhance the performance of reinforced concrete in practical applications.</p>
</sec>
</sec>
<sec id="s10">
<title>10 Comparison of results with literature data</title>
<p>The results obtained in this study reveal trends that are consistent with existing literature on the behavior of composite materials subjected to buckling and post-buckling loads. For instance, previous research by <xref ref-type="bibr" rid="B67">Yoo and Lee (2011)</xref> and <xref ref-type="bibr" rid="B25">Kashani et al. (2013)</xref> has documented similar degradation patterns in reinforced concrete when exposed to extreme loads. These studies reported reductions in compressive strength and modulus of elasticity that align with the findings of this study, thereby reinforcing the understanding of how cyclic loading impacts the mechanical properties of reinforced concrete.</p>
<p>However, this study provides crucial new data indicating that the absolute values of the residual properties of reinforced concrete are significantly lower than those documented for advanced composites, such as carbon or glass fiber composites. For instance, <xref ref-type="bibr" rid="B56">Vasiliev and Morozov (2013)</xref> observed that carbon/epoxy composites could retain a higher percentage of their load-bearing capacity after buckling, suggesting superior resilience compared to reinforced concrete.</p>
<p>This disparity underscores the heterogeneous and less performant nature of reinforced concrete, which is critical for engineering applications. While reinforced concrete is widely used due to its cost-effectiveness and availability, these findings highlight the limitations of its mechanical properties under critical loading conditions. The identification of specific failure mechanisms, such as cracking and delamination, further contributes to this body of knowledge, as these mechanisms have been less frequently documented in previous studies.</p>
<p>In summary, the new data presented in this study not only confirm existing knowledge but also provide a more nuanced understanding of the performance limitations of reinforced concrete. This underscores the imperative for more rigorous design practices and further research into alternative materials or composite reinforcements that could enhance the durability and reliability of concrete structures under severe loading scenarios.</p>
<sec id="s10-1">
<title>10.1 Comparison of mechanical properties</title>
<p>The measured mechanical properties, such as the elastic modulus and compressive strength, were evaluated from the experimental results. <xref ref-type="table" rid="T9">Table 9</xref> presents a comparison of the average values obtained in this study with those found in the literature.</p>
<table-wrap id="T9" position="float">
<label>TABLE 9</label>
<caption>
<p>Comparison of mechanical properties.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Property</th>
<th align="center">This study (MPa)</th>
<th align="center">Literature (MPa)</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">Compressive Strength</td>
<td align="center">22</td>
<td align="center">40&#x2013;60</td>
</tr>
<tr>
<td align="center">Elastic Modulus</td>
<td align="center">18,000</td>
<td align="center">25,000&#x2013;30,000</td>
</tr>
<tr>
<td align="center">Elongation at Rupture</td>
<td align="center">1.24</td>
<td align="center">2.5&#x2013;3.5</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>The values obtained in this study show that the compressive strength and elastic modulus of reinforced concrete are significantly lower than those of advanced composites. This can be attributed to the complex microstructure and inherent variability of concrete, which impact its performance under load.</p>
<p>Specifically, the irregular arrangement of aggregates and the bonding characteristics between the cement matrix and reinforcement lead to a less uniform stress distribution. Additionally, the presence of microcracks and voids in the concrete can initiate failure mechanisms under high loads, resulting in reduced strength and stiffness. Comparatively, advanced composites, such as carbon or glass fiber-reinforced materials, benefit from a more consistent microstructure and superior tensile strength, allowing them to maintain better mechanical properties under similar loading conditions. This disparity highlights the need for careful consideration of design and material selection in applications where high load-bearing capacity and durability are critical, emphasizing the importance of understanding the limitations of reinforced concrete in structural engineering.</p>
</sec>
<sec id="s10-2">
<title>10.2 Impact of buckling</title>
<p>
<xref ref-type="fig" rid="F12">Figure 12</xref> illustrates the results of the buckling test, showing the relationship between the applied load and the deformation of the reinforced concrete samples.</p>
<fig id="F12" position="float">
<label>FIGURE 12</label>
<caption>
<p>Relationship between applied load and deformation under buckling.</p>
</caption>
<graphic xlink:href="fmech-10-1526724-g012.tif"/>
</fig>
<p>This figure demonstrates that, unlike advanced composites that exhibit better resistance to buckling, the reinforced concrete samples show significant deformation at lower loads. This confirms observations in the literature regarding the vulnerability of reinforced concrete to buckling.</p>
</sec>
<sec id="s10-3">
<title>10.3 Analysis of residual properties</title>
<p>The residual properties of the samples after buckling tests were also evaluated. <xref ref-type="table" rid="T10">Table 10</xref> presents the results of the residual properties compared to advanced composites.</p>
<table-wrap id="T10" position="float">
<label>TABLE 10</label>
<caption>
<p>Residual properties after buckling.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Property</th>
<th align="center">Residual property after buckling (MPa)</th>
<th align="center">Advanced composites (MPa)</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">Compressive Strength</td>
<td align="center">15</td>
<td align="center">30&#x2013;50</td>
</tr>
<tr>
<td align="center">Elastic Modulus</td>
<td align="center">14,000</td>
<td align="center">20,000&#x2013;25,000</td>
</tr>
<tr>
<td align="center">Elongation at Rupture</td>
<td align="center">0.95</td>
<td align="center">1.5&#x2013;2.0</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>The data indicate that the residual properties of reinforced concrete degrade more significantly after buckling compared to advanced composites, which retain a larger portion of their initial properties. This emphasizes the importance of material design in structural applications.</p>
<p>In conclusion, the results of this study align with trends observed in the literature, but the absolute properties of reinforced concrete remain inferior to those of advanced composites. These differences can be attributed to the heterogeneous and less performant nature of reinforced concrete, as well as its sensitivity to buckling and failure phenomena. A deep understanding of these mechanisms is essential for improving the performance of reinforced concrete in critical structural applications. Future research should focus on developing hybrid composite materials that could combine the advantages of concrete and advanced materials to enhance the reliability and durability of structures.</p>
</sec>
</sec>
<sec id="s11">
<title>11 Conclusion and perspectives</title>
<sec id="s11-1">
<title>11.1 Summary of main conclusions of the study</title>
<p>This study has provided valuable insights into the performance of reinforced concrete subjected to buckling and post-buckling loads, revealing critical findings regarding the degradation of its mechanical properties. The experimental tests demonstrated a significant decrease in compressive strength and modulus of elasticity as the applied loads and number of cycles increased. These findings are consistent with previous studies, such as those by <xref ref-type="bibr" rid="B67">Yoo and Lee (2011)</xref> and <xref ref-type="bibr" rid="B25">Kashani et al. (2013)</xref>, which also reported similar degradation patterns under extreme loading conditions.</p>
<p>Microscopic observations identified key failure mechanisms, including cracking, local buckling of the reinforcement, and delamination between concrete and steel, all of which contribute to this degradation. Scanning Electron Microscopy (SEM) observations provided crucial visual evidence of these damage mechanisms, as illustrated in <xref ref-type="fig" rid="F13">Figure 13</xref>.</p>
<fig id="F13" position="float">
<label>FIGURE 13</label>
<caption>
<p>Illustrating these failure mechanisms.</p>
</caption>
<graphic xlink:href="fmech-10-1526724-g013.tif"/>
</fig>
<p>This image reveals the extent of cracks and delamination, underscoring the complex behavior of reinforced concrete under stress.</p>
<p>Overall, these results indicate that the residual reliability of reinforced concrete is lower than that of advanced composites, emphasizing the necessity for rigorous design practices to ensure the durability and safety of reinforced concrete structures under extreme loading conditions. This study contributes to a deeper understanding of the limitations of reinforced concrete and its behavior under complex stresses, aligning with the conclusions drawn in earlier research (e.g., <xref ref-type="bibr" rid="B15">Gioncu and Mazzolani, 2013</xref>).</p>
</sec>
<sec id="s11-2">
<title>11.2 Original contributions of the article</title>
<p>This article makes a significant contribution by offering detailed experimental data on the residual reliability of reinforced concrete under buckling and post-buckling tests&#x2014;an area that has often been overlooked in the literature. By identifying specific failure mechanisms and contrasting the results with those of advanced composite materials, this study enhances our understanding of the inherent limitations of reinforced concrete. Additionally, it proposes a rigorous methodology for assessing residual reliability, which includes tailored experimental protocols and advanced analytical methods. This approach could serve as a benchmark for future research and encourage the development of more robust testing standards for composite materials. The findings also highlight the importance of a multidisciplinary approach that integrates knowledge from material science, mechanics, and structural engineering.</p>
</sec>
<sec id="s11-3">
<title>11.3 Future research perspectives</title>
<p>Future research should focus on innovative strategies to enhance the performance of reinforced concrete, such as the integration of hybrid composite materials that leverage the strengths of both concrete and advanced composites. Investigating the effects of various treatments and additives, including synthetic fibers or polymers, on the failure resistance and ductility of concrete would be particularly relevant. Furthermore, the development of new testing protocols that simulate realistic and diverse loading conditions&#x2014;including thermal and environmental effects&#x2014;could yield valuable insights into the long-term durability of structures.</p>
<p>Finally, a comprehensive investigation of fatigue mechanisms in reinforced concrete, taking into account the long-term impacts of repeated loading cycles, could facilitate the design of more durable and reliable structures. Addressing these contemporary challenges in civil engineering will be crucial for meeting evolving building codes and ensuring public safety.</p>
</sec>
</sec>
<sec id="s12">
<title>12 List of terminologies</title>
<p>
<list list-type="simple">
<list-item>
<p>&#x2022; Compressive strength before testing: The ability of a specimen to withstand compressive forces before testing</p>
</list-item>
<list-item>
<p>&#x2022; Compressive strength after testing: The ability of a specimen to withstand compressive forces after testing</p>
</list-item>
<list-item>
<p>&#x2022; Elastic modulus before testing: A measure of a material&#x2019;s stiffness before any load is applied</p>
</list-item>
<list-item>
<p>&#x2022; Elastic modulus after testing: A measure of a material&#x2019;s stiffness after it has undergone testing</p>
</list-item>
<list-item>
<p>&#x2022; Elongation at break before testing: The maximum deformation of a specimen before rupture, measured prior to testing</p>
</list-item>
<list-item>
<p>&#x2022; Elongation at break after testing: The maximum deformation of a specimen before rupture, measured after testing</p>
</list-item>
<list-item>
<p>&#x2022; Residual property after buckling: The mechanical characteristics of a material after it has experienced buckling</p>
</list-item>
<list-item>
<p>&#x2022; Advanced composites: Composite materials with superior mechanical properties, used in demanding applications</p>
</list-item>
</list>
</p>
</sec>
</body>
<back>
<sec sec-type="data-availability" id="s13">
<title>Data availability statement</title>
<p>The original contributions presented in the study are included in the article/supplementary material, further inquiries can be directed to the corresponding author.</p>
</sec>
<sec sec-type="author-contributions" id="s14">
<title>Author contributions</title>
<p>AN: Conceptualization, Formal Analysis, Methodology, Writing&#x2013;original draft. UN: Conceptualization, Formal Analysis, Methodology, Writing&#x2013;original draft. FO: Supervision, Validation, Writing&#x2013;review and editing.</p>
</sec>
<sec sec-type="funding-information" id="s15">
<title>Funding</title>
<p>The author(s) declare that no financial support was received for the research, authorship, and/or publication of this article.</p>
</sec>
<ack>
<p>The author would like to thank the reviewers for their time and effort. Their constructive comments and helpful suggestions helped me to clarify the research contributions of the main paper and to improve its quality.</p>
</ack>
<sec sec-type="COI-statement" id="s16">
<title>Conflict of interest</title>
<p>The authors declare that the research was conducted in the absence of any commercial or financial relationships that could be construed as a potential conflict of interest.</p>
</sec>
<sec sec-type="ai-statement" id="s17">
<title>Generative AI statement</title>
<p>The author(s) declare that no Generative AI was used in the creation of this manuscript.</p>
</sec>
<sec sec-type="disclaimer" id="s18">
<title>Publisher&#x2019;s note</title>
<p>All claims expressed in this article are solely those of the authors and do not necessarily represent those of their affiliated organizations, or those of the publisher, the editors and the reviewers. Any product that may be evaluated in this article, or claim that may be made by its manufacturer, is not guaranteed or endorsed by the publisher.</p>
</sec>
<sec id="s22">
<title>Abbreviations</title>
<p>
<italic>P</italic>, Applied Load (kN); <italic>E</italic>, Modulus of Elasticity (GPa); <italic>&#x3c3;</italic>, Compressive Strength (MPa); <italic>&#x3b4;</italic>, Deformation (%); <italic>&#x3b1;</italic>, Degradation coefficient.</p>
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