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   <front>
      <journal-meta>
         <journal-id journal-id-type="publisher-id">MC</journal-id>
         <journal-title-group>
            <journal-title specific-use="original">Materiales de Construcci&#x00F3;n</journal-title>
            <abbrev-journal-title abbrev-type="publisher">Mater. constr.</abbrev-journal-title>
         </journal-title-group>
         <issn publication-format="electronic">1988-3226</issn>
         <issn-l>0465-2746</issn-l>
         <publisher>
            <publisher-name>Consejo Superior de Investigaciones Cient&#x00ED;ficas</publisher-name>
            <publisher-loc>
               <country>Espa&#x00F1;a</country>
            </publisher-loc>
         </publisher>
      </journal-meta>
      <article-meta>
         <article-id pub-id-type="doi">10.3989/mc.2024.395724</article-id>
         <article-id pub-id-type="publisher-id">mc.2024.395724</article-id>
         <article-categories>
            <subj-group subj-group-type="heading">
               <subject>Research Articles</subject>
            </subj-group>
         </article-categories>
         <title-group>
            <article-title>Fatigue of SFRC in compression:</article-title>
            <subtitle>Size effect &#x0026; autogenous self-healing</subtitle>
            <trans-title-group xml:lang="es">
               <trans-title>Fatiga del HRFA en compresi&#x00F3;n:</trans-title>
               <trans-subtitle>Efecto de escala &#x0026; autorreparaci&#x00F3;n aut&#x00F3;gena.</trans-subtitle>
            </trans-title-group>
         </title-group>
         <contrib-group>
            <contrib contrib-type="author" corresp="yes">
               <contrib-id contrib-id-type="orcid" authenticated="false">https://orcid.org/0000-0002-0352-0701</contrib-id>
               <name name-style="western">
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                  <surname>de la Rosa</surname>
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                  <surname>Tarifa</surname>
                  <given-names>M.</given-names>
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                  <sup>d</sup>
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                  <surname>Zhang</surname>
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                  <sup>a</sup>
               </label>
               <institution>ETSI Caminos, C. y P., Universidad de Castilla-La Mancha</institution>
               <city>Ciudad Real</city>
               <country country="ES">Espa&#x00F1;a</country>
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                  <sup>b</sup>
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               <institution>DIMME, Grupo de Durabilidad e Integridad Mec&#x00E1;nica de Materiales Estructurales, Universidad Rey Juan Carlos</institution>
               <city>M&#x00F3;stoles</city>
               <country country="ES">Espa&#x00F1;a</country>
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                  <sup>c</sup>
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               <institution>ETSI Minas y Energ&#x00ED;a, Universidad Polit&#x00E9;cnica de Madrid</institution>
               <city>Madrid</city>
               <country country="ES">Espa&#x00F1;a</country>
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                  <sup>d</sup>
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               <institution>ETSI Aeron&#x00E1;utica y del Espacio, Universidad Polit&#x00E9;cnica de Madrid</institution>
               <city>Madrid</city>
               <country country="ES">Espa&#x00F1;a</country>
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                  <sup>e</sup>
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               <institution>EI Minera e Industrial de Almad&#x00E9;n, Universidad de Castilla-La Mancha</institution>
               <city>Almad&#x00E9;n</city>
               <country country="ES">Espa&#x00F1;a</country>
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                  <sup>f</sup>
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               <institution>ETS Ingenier&#x00ED;a y Dise&#x00F1;o Industrial, Universidad Polit&#x00E9;cnica de Madrid</institution>
               <city>Madrid</city>
               <country country="ES">Espa&#x00F1;a</country>
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         <author-notes>
            <corresp id="corr-1-e356">
               <email xlink:href="gonzalo.ruiz@uclm.es">gonzalo.ruiz@uclm.es</email>
            </corresp>
         </author-notes>
         <pub-date date-type="pub"
                   publication-format="electronic"
                   iso-8601-date="2024-12-30">
            <day>30</day>
            <month>12</month>
            <year>2024</year>
         </pub-date>
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                   publication-format="electronic"
                   iso-8601-date="2024-12-30">
            <day>30</day>
            <month>12</month>
            <year>2024</year>
         </pub-date>
         <volume>74</volume>
         <issue>356</issue>
         <elocation-id>e356</elocation-id>
         <pub-history>
            <event>
               <event-desc>Recibido</event-desc>
               <date date-type="received" iso-8601-date="2024-10-04">
                  <day>04</day>
                  <month>10</month>
                  <year>2024</year>
               </date>
            </event>
            <event>
               <event-desc>Aceptado</event-desc>
               <date date-type="accepted" iso-8601-date="2024-11-10">
                  <day>10</day>
                  <month>11</month>
                  <year>2024</year>
               </date>
            </event>
            <event>
               <event-desc>Fecha de publicaci&#x00F3;n on-line</event-desc>
               <date date-type="pub" iso-8601-date="XXXX-XX-XX">
                  <day>XX</day>
                  <month>XX</month>
                  <year>XXXX</year>
               </date>
            </event>
         </pub-history>
         <permissions>
            <copyright-statement>&#x00A9; 2024 CSIC</copyright-statement>
            <copyright-year>2024</copyright-year>
            <copyright-holder>CSIC</copyright-holder>
            <ali:free_to_read/>
            <license license-type="open-access"
                     xlink:href="https://creativecommons.org/licenses/by-nc-nd/4.0/">
               <ali:license_ref>https://creativecommons.org/licenses/by-nc-nd/4.0/</ali:license_ref>
               <license-p>Este es un art&#x00ED;culo de acceso abierto distribuido bajo los t&#x00E9;rminos de la licencia de uso y distribuci&#x00F3;n Creative Commons Reconocimiento 4.0 Internacional (CC BY 4.0).</license-p>
            </license>
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         <self-uri xlink:href="XXXXXXXXXXXXXXXXXXXXXX"/>
         <abstract>
            <title>ABSTRACT:</title>
            <p>This review synthesizes prior research on size effect and autogenous self-healing in steel fiber-reinforced concrete (SFRC) under compressive fatigue. It explores the fatigue behavior of SFRC, focusing on fiber reinforcement&#x2019;s role in post-cracking toughness, crack propagation, and fatigue endurance. The review demonstrates that larger SFRC specimens have reduced fatigue lives, attributed to increased elastic energy driving microcrack growth, aligning with classical size effect theory. Additionally, it highlights autogenous self-healing, where fatigue-induced microcracks release occluded water, promoting rehydration and calcium carbonate precipitation, which enhances residual strength. The interaction between size effect, fiber content, and self-healing is examined, offering insights into improving SFRC&#x2019;s durability under cyclic loading. These findings have practical implications for designing SFRC structures subjected to compressive fatigue, such as wind turbine towers and railway slabs.</p>
         </abstract>
         <trans-abstract xml:lang="es">
            <title>RESUMEN:</title>
            <p>Este art&#x00ED;culo revisa investigaciones sobre el efecto de escala y la autorreparaci&#x00F3;n aut&#x00F3;gena en el hormig&#x00F3;n reforzado con fibras de acero (HRFA) bajo fatiga en compresi&#x00F3;n. Se centra en el papel de las fibras en la tenacidad postfisuraci&#x00F3;n, la propagaci&#x00F3;n de grietas y la resistencia a la fatiga. La revisi&#x00F3;n muestra que las probetas de mayor tama&#x00F1;o tienen vidas de fatiga reducidas debido a la mayor energ&#x00ED;a el&#x00E1;stica que impulsa el crecimiento de microgrietas, en consonancia con la teor&#x00ED;a cl&#x00E1;sica del efecto de escala. Adem&#x00E1;s, destaca la autorreparaci&#x00F3;n aut&#x00F3;gena, donde las microgrietas liberan agua ocluida, promoviendo la rehidrataci&#x00F3;n y la precipitaci&#x00F3;n de carbonato c&#x00E1;lcico, lo cual mejora la resistencia residual. Se examina la interacci&#x00F3;n entre el efecto de escala, el contenido de fibras y la autorreparaci&#x00F3;n, aportando ideas para mejorar la durabilidad del HRFA bajo carga c&#x00ED;clica en estructuras, por ejemplo, en torres de turbinas e&#x00F3;licas y placas ferroviarias.</p>
         </trans-abstract>
         <kwd-group>
            <kwd>Compressive fatigue of steel fiber reinforced concrete (SFRC)</kwd>
            <kwd>Size and shape effects</kwd>
            <kwd>Fatigue-induced autogenous self-healing</kwd>
         </kwd-group>
         <kwd-group xml:lang="es">
            <kwd>Fatiga de hormig&#x00F3;n reforzado con fibras de acero (HRFA) en compresi&#x00F3;n</kwd>
            <kwd>Efectos de escala y forma</kwd>
            <kwd>Autorreparaci&#x00F3;n aut&#x00F3;gena inducida por fatiga</kwd>
         </kwd-group>
         <support-group>
            <funding-group id="fug-1-e356">
               <award-group id="awg-1-e356">
                  <funding-source id="fus-1-e356">
                     <institution-wrap>
                        <institution>Ministerio de Ciencia e Innovaci&#x00F3;n</institution>
                     </institution-wrap>
                  </funding-source>
                  <award-id id="awi-1-e356">PID2019-110928RB-C31</award-id>
                  <award-id id="awi-2-e356">PID2023-147971OB-C31</award-id>
               </award-group>
               <award-group id="awg-2-e356">
                  <funding-source id="fus-2-e356">
                     <institution-wrap>
						<institution>Universidad de Castilla-La Mancha</institution>
                        <institution>Fondo Europeo de Desarrollo Regional</institution>
                     </institution-wrap>
                  </funding-source>
                  <award-id id="awi-3-e356">2022-GRIN-34124</award-id>
               </award-group>
               <funding-statement>The authors acknowledge the funding obtained from the Ministerio de Ciencia e Innovaci&#x00F3;n through the project PID2019-110928RB-C31 and PID2023-147971OB-C31, and from the Universidad de Castilla-La Mancha, Spain, and the Fondo Europeo de Desarrollo Regional through grant 2022-GRIN-34124</funding-statement>
            </funding-group>
         </support-group>
         <counts>
            <fig-count count="18"/>
            <table-count count="5"/>
            <equation-count count="2"/>
            <ref-count count="113"/>
            <page-count count="22"/>
         </counts>
      </article-meta>
   </front>
   <body>
      <sec sec-type="intro" id="sec-1-e356">
         <label>1.</label>
         <title>INTRODUCTION</title>
         <p>Concrete is a quasi-brittle material, meaning its fracture behavior is highly dependent on the size and shape of the structural element (<xref rid="ref-1-e356" ref-type="bibr">1</xref>). This size effect is a critical factor in concrete&#x2019;s mechanical response, particularly because the energy released in the fracture process zone for a given crack increment varies with the size of the element, influencing both crack propagation and the stress at which failure occurs. Extensive research has established that concrete&#x2019;s strength generally decreases as the size of the element increases, even when the geometry remains consistent across different scales (<xref rid="ref-1-e356 ref-2-e356 ref-3-e356 ref-4-e356" ref-type="bibr">1</xref>-<xref rid="ref-5-e356" ref-type="bibr">5</xref>). This size effect complicates the direct application of strength data obtained from laboratory specimens to larger structural elements, as the experimentally measured strength is typically higher than the effective strength in real structural applications.</p>
         <p>Compressive strength is the most widely used parameter for assessing concrete capacity, as concrete performs best under compressive loads. However, this property is also affected by the size effect. For large elements, compressive strength tends to a finite value, which is considered the intrinsic strength of the material (<xref rid="ref-2-e356" ref-type="bibr">2</xref>).</p>
         <p>While the size effect in concrete has been studied extensively under quasi-static loads, its influence on fatigue behavior, particularly under compressive fatigue, remains less explored. Given that concrete is primarily used in compression members in structures, understanding this relationship is crucial for predicting the long-term performance of concrete under cyclic loading.</p>
         <p>Most research on the fatigue of concrete has focused on flexural behavior, examining crack propagation under cyclic loading conditions. This work has largely been based on the application of the Paris-Erdogan law (<xref rid="ref-6-e356" ref-type="bibr">6</xref>), which relates the rate of crack growth to the range of stress intensity factors. Some studies have modeled fatigue crack growth by considering the cohesive stresses in the fracture process zone (<xref rid="ref-7-e356" ref-type="bibr">7</xref>). However, there is a relative lack of studies focused on compressive fatigue, especially regarding the size effect on fatigue life in concrete cubes. While studies on prismatic specimens under axial load (<xref rid="ref-8-e356" ref-type="bibr">8</xref>) and cyclic tests on cylinders of varying diameters and slenderness ratios (<xref rid="ref-9-e356" ref-type="bibr">9</xref>) have provided valuable insights, much remains to be understood about how concrete behaves under compressive fatigue loading.</p>
         <p>The incorporation of fibers into concrete as a distributed reinforcement leads to a more ductile material once the concrete matrix breaks, which is manifested in bending (<xref rid="ref-10-e356" ref-type="bibr">10</xref>), but also in tension (<xref rid="ref-11-e356" ref-type="bibr">11</xref>) and compression (<xref rid="ref-12-e356" ref-type="bibr">12</xref>), and can also lead to modifying the effect of the size (<xref rid="ref-13-e356" ref-type="bibr">13</xref>). Fiber reinforced concrete already plays a significant role in modern construction applications due to its enhanced ductility and post-cracking tensile strength, which makes it more enduring to fatigue compared to plain concrete (<xref rid="ref-14-e356" ref-type="bibr">14</xref>). Research shows that fiber reinforcement generally improves fatigue resistance, though the fibers&#x2019; influence under compressive stress is more limited, as they can sometimes act as crack initiation points (<xref rid="ref-14-e356 ref-15-e356" ref-type="bibr">14</xref>-<xref rid="ref-16-e356" ref-type="bibr">16</xref>). Fiber reinforced concrete demonstrates more uniform fatigue behavior across different loading frequencies, with steel fibers, in particular, helping to mitigate the detrimental effects of low-frequency loading (<xref rid="ref-17-e356" ref-type="bibr">17</xref>). However, it has been observed that there is an optimal fiber content, beyond which the fatigue life of the material decreases (<xref rid="ref-14-e356" ref-type="bibr">14</xref>). Additionally, few studies have examined the size effect specifically in fiber reinforced concrete. Some research, such as (<xref rid="ref-18-e356" ref-type="bibr">18</xref>), suggests that fiber addition shifts the brittle-to-ductile transition in bending tests, while other studies have found that increasing both matrix strength and fiber content reduces the size effect in compressive fatigue tests (<xref rid="ref-19-e356" ref-type="bibr">19</xref>).</p>
         <p>Parallel to the study of size effects on fatigue, there is growing interest in the phenomenon of autogenous self-healing in concrete under fatigue conditions. Contrary to the traditional view that cyclic loading degrades material properties over time, by the late 1900s and early 2000s some research showed that concrete can exhibit strength increases after undergoing fatigue loading. For example, Nelson <italic toggle="yes">et al.</italic> (<xref rid="ref-20-e356" ref-type="bibr">20</xref>) observed a remarkable 39&#x0025; strength increase in runout specimens, and Taliercio and Gobbi (<xref rid="ref-21-e356" ref-type="bibr">21</xref>) reported strength gains between 6&#x0025; and 33&#x0025; due to lateral confinement in axially fatigued concrete. Taher and Fawzy (<xref rid="ref-8-e356" ref-type="bibr">8</xref>) extended these findings, demonstrating that normal-strength concrete can exhibit strength gains of 15&#x0025; to 57&#x0025; after a limited number of fatigue cycles.  Cachim <italic toggle="yes">et al.</italic> (<xref rid="ref-22-e356" ref-type="bibr">22</xref>) confirmed similar results for both plain and fiber reinforced concrete, noting improvements up to 16&#x0025;. More recent studies, including those by Malek <italic toggle="yes">et al.</italic> (<xref rid="ref-23-e356" ref-type="bibr">23</xref>), Qiu <italic toggle="yes">et al.</italic> (<xref rid="ref-24-e356" ref-type="bibr">24</xref>), and Garijo <italic toggle="yes">et al.</italic> (<xref rid="ref-25-e356" ref-type="bibr">25</xref>), have further corroborated these observations, with strength increases as high as 42&#x0025;.</p>
         <p>The underlying mechanism for this strength increase is thought to be autogenous self-healing, where microcracks generated by cyclic loading allow occluded water to penetrate the material, rehydrating dormant cement particles and sealing the cracks (<xref rid="ref-25-e356 ref-26-e356 ref-27-e356" ref-type="bibr">25</xref>-<xref rid="ref-28-e356" ref-type="bibr">28</xref>). Various mechanisms have been proposed for this self-healing process, including calcium carbonate precipitation, the rehydration of unhydrated cement particles, the obstruction of cracks by impurities, and the swelling of the hydrated cement matrix (<xref rid="ref-29-e356 ref-30-e356 ref-31-e356 ref-32-e356 ref-33-e356"
                  ref-type="bibr">29</xref>-<xref rid="ref-34-e356" ref-type="bibr">34</xref>). Some researchers emphasize the role of calcium carbonate precipitation (<xref rid="ref-33-e356" ref-type="bibr">33</xref>, <xref rid="ref-35-e356" ref-type="bibr">35</xref>), while others highlight the importance of ongoing hydration reactions (<xref rid="ref-36-e356" ref-type="bibr">36</xref>). The ability of concrete to self-heal is dependent on several factors, including the availability of moisture, the size of the cracks, and the use of fibers to control crack width and propagate stress in a more distributed manner (<xref rid="ref-29-e356" ref-type="bibr">29</xref>, <xref rid="ref-36-e356 ref-37-e356" ref-type="bibr">36</xref>-<xref rid="ref-38-e356" ref-type="bibr">38</xref>).</p>
         <p>In addition, advances in nanotechnology have provided opportunities to enhance the autogenous self-healing capabilities of concrete by incorporating nanomaterials that act as nucleation sites for the formation of new hydration products (<xref rid="ref-39-e356" ref-type="bibr">39</xref>). This phenomenon has also been observed in ultra-high-performance concretes, where large amounts of cementitious material remain unhydrated. When exposed to moderately elevated temperatures, such as those exceeding 200&#x00B0;C, these materials exhibit strength increases due to the activation of dormant hydration processes (<xref rid="ref-40-e356" ref-type="bibr">40</xref>).</p>
         <p>Given the importance of both the size effect and autogenous self-healing in understanding the fatigue behavior of steel fiber reinforced concrete, we planned to investigate these two phenomena in detail. We focused on the compressive fatigue life of cubic and cylindrical specimens of varying sizes and explore how cyclic loading-induced microcracks contribute to the autogenous self-healing process. The research has already led to some publications that are summarized in this paper. The first two of them dealt with the size effect of cubes and cylinders of a single steel fiber reinforced concrete in fatigue (<xref rid="ref-26-e356" ref-type="bibr">26</xref>, <xref rid="ref-27-e356" ref-type="bibr">27</xref>). Their results manifested that there could be autogenous self-healing in the specimens that endured most, which made us prepare another research that eventually demonstrated the production of new hydration products due to fatigue (<xref rid="ref-28-e356" ref-type="bibr">28</xref>). In this paper, we want to give a comprehensive view of these coupled phenomena. By combining probabilistic analysis of fatigue life with detailed microstructural and fracture assessments, we seek to provide a comprehensive understanding of how size and self-healing influence the mechanical behavior of concrete under fatigue conditions.</p>
         <p>We also aim to familiarize the reader with the concept of steel fiber reinforced concrete (SFRC) fatigue in compression. This understanding is crucial for recognizing the significance of size effect and the initiation of autogenous self-healing caused by compressive fatigue loads. To achieve this, we delve into the study of concrete fatigue in compression, drawing from our own scientific research. This research has been driven by collaboration with industrial partners interested in investigating the fatigue of structural components, such as pylons for wind turbines (see <xref rid="fig-1-e356" ref-type="fig">Figure 1a</xref>), slabs for high-speed train tracks (<xref rid="fig-1-e356" ref-type="fig">Figure 1b</xref>) (<xref rid="ref-41-e356" ref-type="bibr">41</xref>, <xref rid="ref-42-e356" ref-type="bibr">42</xref>), and encased composite beams with steel fiber reinforced concrete (<xref rid="fig-1-e356" ref-type="fig">Figure 1c</xref>) (<xref rid="ref-43-e356" ref-type="bibr">43</xref>).</p>
         <fig id="fig-1-e356" position="float" orientation="portrait">
            <label>
               <bold>FIGURE 1.</bold>
            </label>
            <caption>
               <title>(a) SFRC-tower supporting a wind turbine. Fatigue tests of: (b) a reinforced concrete slab for high-speed ballastless tracks (<xref rid="ref-41-e356" ref-type="bibr">41</xref>, <xref rid="ref-42-e356" ref-type="bibr">42</xref>), and (c) an encased composite beam with steel fiber reinforced concrete (<xref rid="ref-43-e356" ref-type="bibr">43</xref>), both made in the Materials and Structures Laboratory at UCLM.</title>
            </caption>
            <graphic id="gra-1-e356"
                     xlink:href="fd09c54a6d764804a1b22ed8575c9858_001.jpeg"
                     position="anchor"
                     orientation="portrait"/>
         </fig>
         <p>We will first discuss the phenomenology of fatigue of steel fiber reinforced concrete in compression. This will include subsections covering basic aspects of representing fatigue results (Subsection 2.1), as well as the effects of experimental scatter (2.2), frequency (2.3), fiber content (2.4), and load eccentricity (2.5). Section 3 will focus on the impact of size on the compressive fatigue of the material, while Section 4 will deal with autogenous self-healing due to fatigue (Section 4). It follows a discussion on the principal effects influencing autogenous self-healing, namely mineral additions (Subsection 5.1), carbonation (5.2), steel fiber reinforcement (5.3), size effect (5.4), and time (5.5). Lastly, we will draw conclusions emphasizing the importance of taking these phenomena into account.</p>
      </sec>
      <sec id="sec-2-e356">
         <label>2.</label>
         <title>FATIGUE PHENOMENOLOGY IN CEMENTITIOUS MATERIALS</title>
         <p>Cyclic loading in concrete, whether compressive or tensile, causes the material to experience strain increments with each cycle. <xref rid="fig-2-e356" ref-type="fig">Figure 2a</xref> illustrates a typical setup of a compressive fatigue test on a concrete cube, whereas <xref rid="fig-2-e356" ref-type="fig">Figure 2b</xref> plots some compressive load-strain loops in a specimen that has been subjected to cycles running from 5&#x0025; to 70&#x0025; of its compressive strength. They correspond to a 76 <italic toggle="yes">&#x00D7;</italic> 76 <italic toggle="yes">&#x00D7;</italic> 302 mm<sup>3</sup> prism of a 36 MPa concrete tested by Jinawath (<xref rid="ref-44-e356" ref-type="bibr">44</xref>). The compression loops initially exhibit a convex shape during loading and a concave shape during unloading, but soon they feature a concave loading branch. The secant modulus of elasticity decreases as the number of cycles increases, as illustrated in <xref rid="fig-2-e356" ref-type="fig">Figure 2b</xref>. The strain increase is rapid during the first few cycles, then levels off and becomes linear with the number of cycles during a second phase, and eventually grows rapidly again before failure, as depicted by the strain-number of cycles curve in <xref rid="fig-3-e356" ref-type="fig">Figure 3</xref>. This curve is often referred to as the &#x201C;cyclic creep curve&#x201D; because it resembles the deformation caused by a sustained load on the material. The average of the cyclic loading affects the specimen, and the resulting deformation somehow responds to this mean load.</p>
         <fig id="fig-2-e356" position="float" orientation="portrait">
            <label>
               <bold>FIGURE 2.</bold>
            </label>
            <caption>
               <title>(a) Concrete cube tested in compressive fatigue and (b) stress-strain cycles in compression plotted with the stress-strain monotonic curve of the same material</title>
            </caption>
            <graphic id="gra-2-e356"
                     xlink:href="fd09c54a6d764804a1b22ed8575c9858_002.jpg"
                     position="anchor"
                     orientation="portrait"/>
            <attrib>(adapted from Figure 6.4, P. Jinawath PhD Thesis Report, University of Leeds, 1974 (<xref rid="ref-44-e356" ref-type="bibr">44</xref>), &#x0026; Figure 8.23 in (<xref rid="ref-45-e356" ref-type="bibr">45</xref>)).</attrib>
         </fig>
         <fig id="fig-3-e356" position="float" orientation="portrait">
            <label>
               <bold>FIGURE 3.</bold>
            </label>
            <caption>
               <title>Cyclic creep curve in cementitious materials.</title>
            </caption>
            <graphic id="gra-3-e356"
                     xlink:href="fd09c54a6d764804a1b22ed8575c9858_003.jpg"
                     position="anchor"
                     orientation="portrait"/>
         </fig>
         <p>The stress-strain loops show that there are internal surfaces and microcracks present in the concrete, caused by the loads, which then grow. These internal surfaces come into contact again when the test piece is compressed anew in the following cycles, leading to overall hardening that is reflected in the concavity of the load branch in compression (interestingly, no hardening is observed in tension because the surfaces do not come into contact (<xref rid="ref-46-e356" ref-type="bibr">46</xref>)). The area enclosed in the loops represents energy dissipation due to the generation and propagation of microcracks, and friction between internal surfaces. Failure occurs when the concrete reaches a critical deformation that it can no longer withstand. For example, in <xref rid="fig-2-e356" ref-type="fig">Figure 2b</xref>, the critical elongation of the last cycle approximately coincides with the elongation recorded in the static test for that level of compression, schematically represented by the solid red curve. This observation suggests that the static resistance curve can be considered as a failure curve of the fatigue loops, like an envelope of the cyclic loops. Indeed, it is usually considered that fatigue failure takes place once the loops reach the quasi-static envelope (<xref rid="ref-47-e356 ref-48-e356" ref-type="bibr">47</xref>-<xref rid="ref-49-e356" ref-type="bibr">49</xref>). It is confirmed that the deformations at the end of the second phase are similar to those of the envelope, while the critical deformations exceed those obtained in static tests (<xref rid="ref-48-e356" ref-type="bibr">48</xref>). However, due to the scatter of the post-peak part of the monotonic quasi-static curve, especially in concrete with fibers, and its dependence on the geometry of the specimen, this observation cannot be profitably used for predicting accurately the fatigue life (<xref rid="ref-12-e356" ref-type="bibr">12</xref>, <xref rid="ref-26-e356" ref-type="bibr">26</xref>, <xref rid="ref-50-e356" ref-type="bibr">50</xref>, <xref rid="ref-51-e356" ref-type="bibr">51</xref>).</p>
         <sec id="sec-3-e356">
            <label>2.1.</label>
            <title>Stress/strain vs. number of cycles curves in concrete</title>
            <p>
               <xref rid="fig-4-e356" ref-type="fig">Figure 4</xref> illustrates the relationship between the logarithm of the secondary strain rate per cycle (which corresponds to the constant strain rate during the second stage of the cyclic creep curve, as shown in <xref rid="fig-3-e356" ref-type="fig">Figure 3</xref>) and the logarithm of the number of cycles to failure for three different types of concrete with the same matrix (<xref rid="ref-17-e356" ref-type="bibr">17</xref>). The types are as follows: C1 is plain concrete, with a compressive strength of 56 MPa at 28 days; C2 is polypropylene fiber-reinforced concrete, with a compressive strength of 66 MPa and a fiber volume of 0.56&#x0025;; and C3 is steel fiber-reinforced concrete, with a compressive strength of 67 MPa and a fiber volume of 0.64&#x0025;.</p>
            <fig id="fig-4-e356" position="float" orientation="portrait">
               <label>
                  <bold>FIGURE 4.</bold>
               </label>
               <caption>
                  <title>Logarithm of the number of cycles to failure versus the logarithm of the secondary strain rate for three concretes with a shared matrix (<xref rid="ref-17-e356" ref-type="bibr">17</xref>).</title>
               </caption>
               <graphic id="gra-4-e356"
                        xlink:href="fd09c54a6d764804a1b22ed8575c9858_004.jpg"
                        position="anchor"
                        orientation="portrait"/>
            </fig>
            <p>Tests were conducted on 100 mm cubes at four different frequencies: 4 Hz, 1 Hz, 1/4 Hz, and 1/16 Hz. All data points generally align along a straight line, a trend first noted by Sparks and Menzies (<xref rid="ref-52-e356" ref-type="bibr">52</xref>) for plain concrete. Medeiros <italic toggle="yes">et al.</italic> (<xref rid="ref-17-e356" ref-type="bibr">17</xref>) further demonstrated that this relationship holds true regardless of the type of fiber or the testing frequency. The linear relationship can be expressed as:</p>
            <disp-formula id="dif-1-e356">
               <mml:math display="block" id="mml-1-e356">
                  <mml:mi>l</mml:mi>
                  <mml:mi>o</mml:mi>
                  <mml:mi>g</mml:mi>
                  <mml:mfrac>
                     <mml:mrow class="MJX-TeXAtom-ORD">
                        <mml:mo>&#x03F5;</mml:mo>
                     </mml:mrow>
                     <mml:mi>f</mml:mi>
                  </mml:mfrac>
                  <mml:mo>=</mml:mo>
                  <mml:mi>m</mml:mi>
                  <mml:mo>&#x002B;</mml:mo>
                  <mml:mi>s</mml:mi>
                  <mml:mi>l</mml:mi>
                  <mml:mi>o</mml:mi>
                  <mml:mi>g</mml:mi>
                  <mml:mi>N</mml:mi>
               </mml:math>
               <label>&#x005B;1&#x005D;</label>
            </disp-formula>
            <p>where  is the secondary strain rate per cycle, <italic toggle="yes">f</italic> is the frequency, and <italic toggle="yes">N</italic> is the number of cycles endured before failure (note that  =, where <italic toggle="yes">n</italic> represents the cycle number, not the cycle at failure).</p>
            <p>This feature of cyclic creep curves enables the derivation of a strain-based failure criterion. Poveda <italic toggle="yes">et al.</italic> (<xref rid="ref-14-e356" ref-type="bibr">14</xref>) extended the Sparks and Menzies&#x2019; law by integrating it to yield a failure criterion expressed as:</p>
            <disp-formula id="dif-2-e356">
               <mml:math display="block" id="mml-2-e356">
                  <mml:mstyle displaystyle="true">
                     <mml:mrow class="MJX-TeXAtom-ORD">
                        <mml:msub>
                           <mml:mi>&#x03F5;</mml:mi>
                           <mml:mrow class="MJX-TeXAtom-ORD">
                              <mml:mi>c</mml:mi>
                           </mml:mrow>
                        </mml:msub>
                        <mml:mo>=</mml:mo>
                        <mml:msub>
                           <mml:mi>&#x03F5;<!-- ϵ --></mml:mi>
                           <mml:mrow class="MJX-TeXAtom-ORD">
                              <mml:mi>m</mml:mi>
                              <mml:mi>a</mml:mi>
                              <mml:mi>x</mml:mi>
                           </mml:mrow>
                        </mml:msub>
                        <mml:mo>&#x002B;</mml:mo>
                        <mml:msup>
                           <mml:mn>10</mml:mn>
                           <mml:mrow class="MJX-TeXAtom-ORD">
                              <mml:mi>m</mml:mi>
                           </mml:mrow>
                        </mml:msup>
                        <mml:msup>
                           <mml:mi>N</mml:mi>
                           <mml:mrow class="MJX-TeXAtom-ORD">
                              <mml:mi>s</mml:mi>
                              <mml:mo>&#x002B;</mml:mo>
                              <mml:mn>1</mml:mn>
                           </mml:mrow>
                        </mml:msup>
                     </mml:mrow>
                  </mml:mstyle>
               </mml:math>
               <label>&#x005B;2&#x005D;</label>
            </disp-formula>
            <p>where 𝜖<sub>c</sub> is the critical strain at failure and 𝜖<sub>max</sub> is the maximum strain recorded in the first cycle. The red curve in <xref rid="fig-5-e356" ref-type="fig">Figure 5</xref> represents this criterion on a strain vs. number of cycles plot. Failure of a specimen occurs when the cyclic creep curve intersects this failure curve, as indicated by the black dots in <xref rid="fig-5-e356" ref-type="fig">Figure 5</xref>.</p>
            <fig id="fig-5-e356" position="float" orientation="portrait">
               <label>
                  <bold>FIGURE 5.</bold>
               </label>
               <caption>
                  <title>Graphical representation of the failure criterion based on the Sparks &#x0026; Menzies law by Poveda <italic toggle="yes">et al.</italic> (<xref rid="ref-14-e356" ref-type="bibr">14</xref>).</title>
               </caption>
               <graphic id="gra-5-e356"
                        xlink:href="fd09c54a6d764804a1b22ed8575c9858_005.jpg"
                        position="anchor"
                        orientation="portrait"/>
            </fig>
            <p>While strain-based failure criteria offer a convenient method for assessing fatigue behavior, the fatigue strength of concrete is often represented by <italic toggle="yes">S</italic>-<italic toggle="yes">N</italic> curves. In these curves, <italic toggle="yes">S</italic> represents the normalized stress (<italic toggle="yes">S</italic> = <italic toggle="yes">σ/f</italic>
               <sub>c</sub>) and <italic toggle="yes">N</italic> is the number of cycles to failure, typically shown on a logarithmic scale. For instance, the <italic toggle="yes">S</italic>-<italic toggle="yes">N</italic> curves proposed in the 2010 Model Code and developed by Lohaus <italic toggle="yes">et al.</italic> (<xref rid="ref-53-e356" ref-type="bibr">53</xref>) (see <xref rid="fig-6-e356" ref-type="fig">Figure 6</xref>) illustrate the relationship between maximum stress and <italic toggle="yes">N</italic>, with the minimum stress as a parameter. These curves are generally considered applicable to all types of concrete, as the influence of composition on fatigue behavior is relatively minor.</p>
            <fig id="fig-6-e356" position="float" orientation="portrait">
               <label>
                  <bold>FIGURE 6.</bold>
               </label>
               <caption>
                  <title>
                     <italic toggle="yes">S</italic>-<italic toggle="yes">N</italic> curves for concrete according to the Model Code 2010 (<xref rid="ref-55-e356" ref-type="bibr">55</xref>): (a) 3D representation from the model by Lohaus, Oneschkow, and Wefer (<xref rid="ref-53-e356" ref-type="bibr">53</xref>), and (b) 2D plot included in the standard.</title>
               </caption>
               <graphic id="gra-6-e356"
                        xlink:href="fd09c54a6d764804a1b22ed8575c9858_006.jpeg"
                        position="anchor"
                        orientation="portrait"/>
            </fig>
            <p>A distinction is often made between low-cycle and high-cycle fatigue. Low-cycle fatigue results from a small number of cycles at high stress levels, such as those during an earthquake, whereas high-cycle fatigue occurs over the structure&#x2019;s service life at lower stress levels. However, both fatigue types are driven by the same damage mechanisms, making the distinction largely formal. According to CEB Committee 188 (<xref rid="ref-54-e356" ref-type="bibr">54</xref>), the boundary between low-cycle and high-cycle fatigue lies between 10<sup>3</sup> and 10<sup>4</sup> cycles, but no clear discontinuity is observed in the <italic toggle="yes">S</italic>-<italic toggle="yes">N</italic> curves (<xref rid="fig-6-e356" ref-type="fig">Figure 6b</xref>).</p>
            <p>Unlike metals, concrete appears to lack an endurance limit, meaning no stress threshold guarantees infinite fatigue life. Tests beyond 10<sup>7</sup> cycles are uncommon, yet the Model Code curves (<xref rid="fig-6-e356" ref-type="fig">Figure 6b</xref>) extend up to 10<sup>20</sup> cycles. Reaching this extreme number of cycles at a frequency of 1 Hz would take approximately 230 times the time since the Big Bang&#x2014;about 13.8 billion years, which gives an idea of the absolute nonsense of extrapolating results in the logarithmic scale.</p>
            <p>Concrete&#x2019;s fatigue life is highly sensitive to both the stress level and the loading range, defined by the difference between maximum and minimum stress (&#x2206;<italic toggle="yes">σ</italic> = <italic toggle="yes">σ</italic>
               <sub>max</sub>
               <italic toggle="yes">&#x2212;σ</italic>
               <sub>min</sub>), or by the stress ratio <italic toggle="yes">R</italic> = <italic toggle="yes">σ</italic>
               <sub>min</sub>
               <italic toggle="yes">/σ</italic>
               <sub>max</sub>. A smaller stress range or higher stress ratio allows the concrete to withstand a greater maximum cyclic load. This relationship is shown in <xref rid="fig-6-e356" ref-type="fig">Figure 6b</xref>, where higher minimum stresses correspond to higher maximum stresses in cyclic loading.</p>
         </sec>
         <sec id="sec-4-e356">
            <label>2.2.</label>
            <title>Experimental scatter</title>
            <p>It is important to understand that concrete fatigue can vary significantly, meaning that a single average <italic toggle="yes">S</italic>-<italic toggle="yes">N</italic> curve may not fully represent all fatigue behaviors. <xref rid="fig-7-e356" ref-type="fig">Figure 7</xref> illustrates this by displaying the probability of failure versus the number of cycles for almost 100 identical compression fatigue tests conducted by Ortega <italic toggle="yes">et al.</italic> (<xref rid="ref-56-e356" ref-type="bibr">56</xref>). The compressive strength of the SFRC was 58.9 MPa, and it was reinforced with 13 mm straight steel fibers at a 0.2&#x0025; volumetric ratio. The results were analyzed using a two-parameter Weibull function. By randomly selecting test groups and plotting their failure probability functions, we can estimate the range of error associated with different sample sizes.</p>
            <fig id="fig-7-e356" position="float" orientation="portrait">
               <label>
                  <bold>FIGURE 7.</bold>
               </label>
               <caption>
                  <title>Effect of sample size (<italic toggle="yes">n</italic>) on the measurement of fatigue life. The shaded band represents the variability in failure probability for random groups of 25 tests. The right plot shows relative error curves for different sample sizes (<xref rid="ref-56-e356" ref-type="bibr">56</xref>).</title>
               </caption>
               <graphic id="gra-7-e356"
                        xlink:href="fd09c54a6d764804a1b22ed8575c9858_007.jpeg"
                        position="anchor"
                        orientation="portrait"/>
            </fig>
            <p>In <xref rid="fig-7-e356" ref-type="fig">Figure 7</xref>, the shaded area represents the range covered by random groups of 25 tests. It required half a million random groups to stabilize this band and have it aligned with the overall distribution obtained from all tests, represented by the thick black line, which is considered the correct distribution. From this, we can derive the probability density function for various failure probabilities and calculate confidence margins. For example, the green curve shows the density function for a 40&#x0025; failure probability, while the dashed blue line indicates the 95&#x0025; confidence margin. This means there is a 95&#x0025; likelihood that the distribution function of a random group of 25 tests will fall to the left of this curve.</p>
            <p>The right plot in <xref rid="fig-7-e356" ref-type="fig">Figure 7</xref> presents error curves for different sample sizes, enabling us to determine the associated error for each group size. For instance, the relative error for a group of 15 fatigue tests (orange error curve) is 5.7&#x0025; at a 50&#x0025; failure probability, rising to 10.5&#x0025; for groups of 5 tests (red curve), and decreasing to 4.1&#x0025; for groups of 25 tests (blue curve). If the failure probability is 10&#x0025;, the relative errors increase to 22.2&#x0025;, 10.9&#x0025;, and 7.5&#x0025; for groups of 5, 15, and 25 specimens, respectively.</p>
            <p>Even with large sample sizes, there is considerable variability in failure probabilities. In this example (<xref rid="fig-7-e356" ref-type="fig">Figure 7</xref>), the average fatigue life is approximately 10700 cycles, but at a 10&#x0025; failure probability, the fatigue life drops to just 1500 cycles. <italic toggle="yes">S</italic>-<italic toggle="yes">N</italic> curves are typically constructed using the average values of the failure distribution for each load case, necessitating a statistical approach to ensure adequate safety levels.</p>
         </sec>
         <sec id="sec-5-e356">
            <label>2.3.</label>
            <title>Effect of frequency</title>
            <p>The frequency of cyclic loading significantly affects fatigue life, especially at low frequencies (1 Hz and below) and high peak stresses (above 75&#x0025; of static strength). <xref rid="fig-8-e356" ref-type="fig">Figure 8</xref> presents fatigue life results at varying frequencies (4, 1, 1/4, and 1/16 Hz) for compression tests with a peak load of 85&#x0025; of the static strength (79 MPa for the C1 concrete, tested when it was approximately one year old) and a stress ratio of 0.3 (<xref rid="ref-17-e356" ref-type="bibr">17</xref>). A notable drop in fatigue life occurs when shifting from 4 Hz to 1 Hz, where log <italic toggle="yes">N</italic> decreases from 4.3 to 2.8, indicating a reduction in fatigue life by more than an order of magnitude. This reduction results from lower strain rates at reduced frequencies, which diminish static strength. Additionally, the interaction between the detrimental effects of compressive cycles and the beneficial self-healing due to fatigue may play a role in this behavior (discussed later in Section 5).</p>
            <fig id="fig-8-e356" position="float" orientation="portrait">
               <label>
                  <bold>FIGURE 8.</bold>
               </label>
               <caption>
                  <title>Effect of frequency on fatigue life for three concretes with the same matrix (<xref rid="ref-17-e356" ref-type="bibr">17</xref>): (a) plain concrete (C1), (b) polypropylene fiber reinforced concrete (C2), and (c) steel fiber reinforced concrete (C3).</title>
               </caption>
               <graphic id="gra-8-e356"
                        xlink:href="fd09c54a6d764804a1b22ed8575c9858_008.jpeg"
                        position="anchor"
                        orientation="portrait"/>
            </fig>
            <p>This sensitivity to frequency is particularly relevant for structures like wind towers, which experience low oscillation frequencies. To improve fatigue life in such applications, reinforcing concrete with steel fibers is advisable, as they help extend fatigue life. For instance, concrete C3 (steel fiber reinforced) in <xref rid="fig-8-e356" ref-type="fig">Figure 8</xref> shows consistent performance across all studied frequencies, unlike C2 (polypropylene fiber reinforced), which is more frequency sensitive.</p>
         </sec>
         <sec id="sec-6-e356">
            <label>2.4.</label>
            <title>Effect of fiber content</title>
            <p>We investigated the effect of fiber content on the mechanical behavior of steel-fiber reinforced concrete (SFRC) under low-cycle fatigue (<xref rid="ref-14-e356" ref-type="bibr">14</xref>). Five self-compacting concrete mixtures were designed with fiber contents ranging from 0 to 0.8&#x0025; by volume. All mixtures shared the same concrete matrix, ensuring flowability and fiber-matrix adhesion. The base concrete had a compressive strength of 33.4 MPa. The steel fibers used were hook-ended, 35 mm in length, and 0.55 mm in diameter. The specimens were 100 mm cubes.</p>
            <p>In terms of static behavior, the fibers did not significantly enhance compressive strength. However, the presence of fibers resulted in a more gradual post-peak softening after maximum load. Regarding flexural behavior, increasing fiber content improved post-peak performance, though certain fiber amounts produced similar residual tensile strength. For example, concrete with 0.6&#x0025; fiber content exhibited post-peak behavior similar to that with 0.4&#x0025;.</p>
            <p>The addition of steel fibers markedly improved compressive fatigue performance, as fatigue life increased with fiber content (see <xref rid="fig-9-e356" ref-type="fig">Figure 9a</xref>). Low fiber contents did not substantially improve fatigue properties compared to plain concrete. However, intermediate fiber contents &#x2014;from 0.4&#x0025; to 0.6&#x0025;&#x2014; extended fatigue life up to five times longer than that of plain concrete (equivalent to a 31&#x0025; increase in the logarithmic average of resisted cycles). The optimal fiber dosage was found to be 45 kg/m<sup>3</sup> in this particular study. Interestingly, higher fiber contents reduced fatigue life, likely due to increased matrix imperfections and pore formation, which promote crack initiation.</p>
            <fig id="fig-9-e356" position="float" orientation="portrait">
               <label>
                  <bold>FIGURE 9.</bold>
               </label>
               <caption>
                  <title>Effect of fiber content on fatigue life of SFRC (<xref rid="ref-14-e356" ref-type="bibr">14</xref>): (a) Fatigue life as a function of fiber dosage; (b) Secondary strain rate vs. fatigue life following Sparks and Menzies&#x2019; model.</title>
               </caption>
               <graphic id="gra-9-e356"
                        xlink:href="fd09c54a6d764804a1b22ed8575c9858_009.jpg"
                        position="anchor"
                        orientation="portrait"/>
            </fig>
            <p>Notably, the Sparks and Menzies&#x2019; plot of secondary strain rate versus fatigue life showed a consistent linear relationship (<xref rid="fig-9-e356" ref-type="fig">Figure 9b</xref>), confirming that this relationship is independent of fiber content and primarily depends on the base concrete.</p>
            <p>The improvement in fatigue life with fiber content may be explained by the interplay between microcrack propagation and autogenous self-healing due to fatigue, which will be discussed further in Section 5.</p>
         </sec>
         <sec id="sec-7-e356">
            <label>2.5.</label>
            <title>Effect of load eccentricity</title>
            <p>We also examined how load positioning uncertainty affects the fatigue life and result variability of SFRC (<xref rid="ref-57-e356" ref-type="bibr">57</xref>), a factor often blamed on compressive strength scatter (<xref rid="ref-22-e356" ref-type="bibr">22</xref>, <xref rid="ref-45-e356" ref-type="bibr">45</xref>). While inhomogeneity at the mesoscale undoubtedly contributes to scatter, there may be experimental factors influencing fatigue life as well.</p>
            <p>To reduce unintended loading eccentricity, we developed an individualized ball-and-socket joint (i-BSJ) (see <xref rid="fig-10-e356" ref-type="fig">Figure 10a</xref>). Two types of tests were conducted: first, we used an instrumented aluminum cube to measure eccentricity under two conditions&#x2014;using the i-BSJ and without it. Second, two series of 15 monotonic compressive tests and two series of 15 cyclic compressive tests were performed on 40 mm SFRC cubes (using 15 kg/m<sup>3</sup> of straight, 13 mm long, and 0.20 mm in diameter fibers), again with and without the i-BSJ.</p>
            <fig id="fig-10-e356" position="float" orientation="portrait">
               <label>
                  <bold>FIGURE 10.</bold>
               </label>
               <caption>
                  <title>Impact of eccentricity on fatigue life (<xref rid="ref-57-e356" ref-type="bibr">57</xref>): (a) 40-mm SFRC cube tested with an individualized ball-and-socket joint (i-BSJ); (b) Probability density function for load eccentricity in two test series (90&#x0025; of results without i-BSJ fall within the grey area, while 90&#x0025; of results with i-BSJ fall within the red area); (c) Fatigue results for identical SFRC specimens tested with and without the i-BSJ.</title>
               </caption>
               <graphic id="gra-10-e356"
                        xlink:href="fd09c54a6d764804a1b22ed8575c9858_010.jpeg"
                        position="anchor"
                        orientation="portrait"/>
            </fig>
            <p>The results revealed that while average eccentricity values remained similar, their standard deviation was reduced by an order of magnitude when using the i-BSJ. <xref rid="fig-10-e356" ref-type="fig">Figure 10b</xref> illustrates the two-dimensional probability distribution of load position. Without the i-BSJ, load eccentricity had wider variation (grey-shaded area <xref rid="fig-10-e356" ref-type="fig">in Figure 10b</xref>), whereas with the i-BSJ, it was significantly more concentrated (red-shaded area). Thus, while some variability remained due to equipment tolerances and specimen geometry, the i-BSJ effectively minimized misalignments from manual specimen centering and other geometrical factors.</p>
            <p>In addition, when the i-BSJ was used in the SFRC cube tests, the average compressive strength increased by 10&#x0025; (from 53.6 MPa to 58.9 MPa). The average fatigue life also saw a significant increase, multiplying by six in the second series (refer to the red curve in <xref rid="fig-10-e356" ref-type="fig">Figure 10c</xref>). Furthermore, the standard deviation of fatigue life decreased, as indicated by the steeper slope of the red curve in <xref rid="fig-10-e356" ref-type="fig">Figure 10c</xref>. These results show that undesired loading eccentricity reduces fatigue life and increases result variation, beyond what can be explained by variations in compressive strength alone (<xref rid="ref-22-e356" ref-type="bibr">22</xref>, <xref rid="ref-45-e356" ref-type="bibr">45</xref>).</p>
            <p>In conclusion, when testing specimens in compressive fatigue, it is highly recommended to use an i-BSJ for minimizing the uncertainties caused by manual centering misalignments in both monotonic and cyclic compressive tests.</p>
         </sec>
      </sec>
      <sec id="sec-8-e356">
         <label>3.</label>
         <title>Size effect in fatigue of SFRC</title>
         <p>As anticipated in the introduction, we also studied the size effect on fatigue in self-compacting steel-fiber reinforced concrete specimens. Cubes of three sizes (40 mm, 80 mm, and 150 mm edge lengths) (<xref rid="ref-26-e356" ref-type="bibr">26</xref>) and cylinders of three heights (75 mm, 200 mm, and 300 mm) were tested, with slenderness 2 for the cylinders (<xref rid="fig-11-e356" ref-type="fig">Figure 11</xref>) (<xref rid="ref-27-e356" ref-type="bibr">27</xref>). All the specimens were made from the same self-compacting steel fiber reinforced concrete. The composition is detailed in <xref rid="taw-1-e356" ref-type="table">Table 1</xref>. The fiber content was 0.3&#x0025; by volume, and the type used was straight fibers, specifically Dramix OL 13/.20 from Bekaert, measuring 13 mm in length with an aspect ratio of 65. This length was selected to ensure that the fibers remained sufficiently short relative to the smallest specimen size, maintaining the homogeneity of mechanical properties throughout the material.</p>
         <fig id="fig-11-e356" position="float" orientation="portrait">
            <label>
               <bold>FIGURE 11.</bold>
            </label>
            <caption>
               <title>(a) SFRC cubes of three sizes: 40 mm, 80 mm, and 150 mm; (b) individualized ball and socket joints for the three cubes (<xref rid="ref-26-e356" ref-type="bibr">26</xref>); (c) SFRC cylinders of three heights: 150 mm, 200 mm, and 300 mm; (d) fatigue test of one of the medium cylinders (<xref rid="ref-27-e356" ref-type="bibr">27</xref>).</title>
            </caption>
            <graphic id="gra-11-e356"
                     xlink:href="fd09c54a6d764804a1b22ed8575c9858_011.jpg"
                     position="anchor"
                     orientation="portrait"/>
         </fig>
         <table-wrap id="taw-1-e356" position="float" orientation="portrait">
            <label>
               <bold>TABLE 1.</bold>
            </label>
            <caption>
               <title>SFRC dosage (size-effect study).</title>
            </caption>
            <table id="tab-1-e356"
                   frame="hsides"
                   rules="groups"
                   width="50&#x0025;">
               <thead>
                  <tr>
                     <th align="center"
                         style="width:218.4pt;border-top:1pt solid &#x0023;000;border-bottom:1pt solid &#x0023;000000;"
                         rowspan="1"
                         colspan="1">Component</th>
                     <th align="center"
                         style="width:98.3pt;border-top:1pt solid &#x0023;000;border-bottom:1pt solid &#x0023;000000;"
                         rowspan="1"
                         colspan="1">Content (kg/m<sup>3</sup>)</th>
                  </tr>
               </thead>
               <tbody>
                  <tr>
                     <td style="width:218.4pt;border-top:1pt solid &#x0023;000000;"
                         rowspan="1"
                         colspan="1">Cement CEM II/B-L 32.5 N</td>
                     <td align="center"
                         style="width:98.3pt;border-top:1pt solid &#x0023;000000;"
                         rowspan="1"
                         colspan="1">286</td>
                  </tr>
                  <tr>
                     <td style="width:218.4pt;" rowspan="1" colspan="1">Limestone filler</td>
                     <td align="center" style="width:98.3pt;" rowspan="1" colspan="1">195</td>
                  </tr>
                  <tr>
                     <td style="width:218.4pt;" rowspan="1" colspan="1">Water</td>
                     <td align="center" style="width:98.3pt;" rowspan="1" colspan="1">202</td>
                  </tr>
                  <tr>
                     <td style="width:218.4pt;" rowspan="1" colspan="1">Air reducer (MasterCast 212)</td>
                     <td align="center" style="width:98.3pt;" rowspan="1" colspan="1">1</td>
                  </tr>
                  <tr>
                     <td style="width:218.4pt;" rowspan="1" colspan="1">Superplasticizer (MasterEase 5025)</td>
                     <td align="center" style="width:98.3pt;" rowspan="1" colspan="1">2.86</td>
                  </tr>
                  <tr>
                     <td style="width:218.4pt;" rowspan="1" colspan="1">Sand 0.5 mm (feldspathic)</td>
                     <td align="center" style="width:98.3pt;" rowspan="1" colspan="1">921</td>
                  </tr>
                  <tr>
                     <td style="width:218.4pt;" rowspan="1" colspan="1">Coarse agg. 4-8 mm (siliceous, crushed)</td>
                     <td align="center" style="width:98.3pt;" rowspan="1" colspan="1">712</td>
                  </tr>
                  <tr>
                     <td style="width:218.4pt;border-bottom:1pt solid &#x0023;000;"
                         rowspan="1"
                         colspan="1">Steel fiber OL 13/.20</td>
                     <td align="center"
                         style="width:98.3pt;border-bottom:1pt solid &#x0023;000;"
                         rowspan="1"
                         colspan="1">23.55</td>
                  </tr>
               </tbody>
            </table>
         </table-wrap>
         <p>Cubes and cylinders were stored in a humid chamber maintained at 20&#x00B0;C and 97&#x0025; relative humidity for at least one year after demolding. The mean compressive strength of the hardened concrete was measured at 28 days. The results showed an average of 26.4 MPa from cylinders with a diameter of 75 mm and a height of 150 mm, and 28.2 MPa from cubes with an edge length of 100 mm. Additionally, the compressive strength of cylinders with the same dimensions was tested at 56 days and yielded an average of 30.6 MPa. The properties exhibited a high degree of homogeneity, as indicated by their small standard deviations (<xref rid="ref-26-e356" ref-type="bibr">26</xref>, <xref rid="ref-27-e356" ref-type="bibr">27</xref>).</p>
         <p>For each size, 10 quasi-static tests were conducted right before fatigue testing to determine their reference compressive strength, followed by 15 fatigue tests with cyclic loads ranging from 0.20 to 0.85 of the compressive strength. As strain along the loading direction in cubes is not uniform due to the confining effect of friction in contact with the platens, we preferred taking the average strain, i.e. total deformation over the cube&#x2019;s edge length, measured as the average between the readings of two LVDTs as a representative value. As for the cylinders, they have a slenderness of 2, so the influence of the contact with the platens in the central section is negligible, and thus we took the strain in the central point of the height, actually the average between the recordings of three strain gauges at 120<italic toggle="yes">
               <sup>&#x25E6;</sup>
            </italic>.</p>
         <p>A key strength of this methodology lies in the use of diverse equipment to control tests and assess internal changes, including ball-and-socket joints to minimize misalignment and devices like a computed tomography scanner and mercury porosimeter to analyze internal structure and failure modes. Additionally, the number of specimens allowed for a more accurate representation of the probabilistic nature of both quasi-static and fatigue results.</p>
         <p>For cubes, the reference compressive strength was consistent across all sizes, with means of 30.5 MPa, 30.6 MPa, and 30.7 MPa for small, intermediate, and large cubes, respectively. This lack of size effect reflects the material&#x2019;s high post-peak ductility from fiber reinforcement, leading to a failure closer to plastic behavior than quasi-brittle. This may change for larger sizes (<xref rid="ref-1-e356" ref-type="bibr">1</xref>, <xref rid="ref-2-e356" ref-type="bibr">2</xref>, <xref rid="ref-13-e356" ref-type="bibr">13</xref>). In contrast, the quasi-static reference compressive strength of cylinders displayed a slight inverse size effect: the mean compressive strength increased from 26.3 MPa for small cylinders to 32.5 MPa for large ones. This was attributed to a reduction in porosity near the cylinder surfaces as size increased, as detected by the computed tomography study (<xref rid="ref-27-e356" ref-type="bibr">27</xref>, <xref rid="ref-58-e356" ref-type="bibr">58</xref>). The inverse size effect impacts fatigue behavior: smaller cylinders experience lower maximum and minimum loads, contributing to longer fatigue lives, while larger cylinders benefit from higher static strength. However, other size-dependent factors may counteract these effects.</p>
         <p>In terms of fatigue life, 80 mm and 150 mm cubes showed similar Weibull distributions, while 40 mm cubes exhibited much higher scatter, spanning over two orders of magnitude at 50&#x0025; failure probability (<xref rid="fig-12-e356" ref-type="fig">Figure 12</xref>). Many smaller cubes survived longer cycles, indicating an autogenous self-healing effect. Post-fatigue monotonic tests on run-out cubes revealed a 42&#x0025; strength increase compared to initial values (43.2 MPa compared with the initial 30.5 MPa). This could be due to cyclic loading inducing microcracks, allowing water to react with unhydrated cement and thus improving strength. Cylinders followed a similar pattern: small cylinders had longer lives compared to larger ones, suggesting self-healing, though not as pronounced as with cubes. No runouts occurred in the cylinder tests.</p>
         <fig id="fig-12-e356" position="float" orientation="portrait">
            <label>
               <bold>FIGURE 12</bold>.</label>
            <caption>
               <title>Plot representing the cumulative probability of failure vs. fatigue life of cubes and cylinders of three sizes made of the same SFRC (<xref rid="ref-26-e356" ref-type="bibr">26</xref>, <xref rid="ref-27-e356" ref-type="bibr">27</xref>).</title>
            </caption>
            <graphic id="gra-12-e356"
                     xlink:href="fd09c54a6d764804a1b22ed8575c9858_012.jpg"
                     position="anchor"
                     orientation="portrait"/>
         </fig>
         <p>It is important to emphasize that all the cylinder and cube specimens, which results are shown in <xref rid="fig-12-e356" ref-type="fig">Figure 12</xref> covering seven orders of magnitude in <italic toggle="yes">N</italic>, were made of the same material, and all tests were conducted at 20&#x0025; to 85&#x0025; of the reference compressive strength of the respective series. The findings indicate that the size of the specimen has a significant impact on fatigue life. Additionally, the specimen&#x2019;s shape has a considerable effect on fatigue behavior, with cylinders being more conservative than cubes. We believe that cubes provide more confinement to the material, facilitating the extension of micro-damage in a stable manner and allowing self-healing to happen in all these damaged regions, as discussed in the next section. These results highlight the significant size effect in fatigue testing, cautioning against using small specimen data to characterize structural element behavior.</p>
      </sec>
      <sec id="sec-9-e356">
         <label>4.</label>
         <title>Autogenous self-healing due to fatigue</title>
         <p>During our study of fatigue aspects of SFRC, we observed significant improvement in the material after compressive fatigue loading. However, there were various hypotheses to explain this behavior that lacked sufficient evidence. To address this, we initiated further research to identify the changes in the material&#x2019;s microstructure caused by compressive fatigue and to determine if there is an increase in the production of hydrated compounds due to the fatigue mechanical actions.</p>
         <p>As we had found that cubes, not cylinders, experienced runouts (see previous section), we suspected that the confinement by friction against the platens was causing extensive microdamage due to fatigue, which we believe is associated with the autogenous self-healing phenomenon. Cylinders with a slenderness of 2 have less volume affected by friction with the platens. So, microdamage extension is smaller than in cubes, making them less likely to develop autogenous self-healing. Note that this does not mean cylinders do not experience self-healing since small cylinders endure longer than taller ones, but it is less noticeable than in cubes. Thus, we used only cubes for our new experimental campaign, subjecting specimens to programmed fatigue loading.</p>
         <p>For this research on autogenous self-healing induced by fatigue, we collaborated with experts in the chemistry of cement and concrete at the Institute for Construction Sciences &#x201C;Eduardo Torroja&#x201D;. They designed and fabricated the SFCR (see the composition in <xref rid="taw-2-e356" ref-type="table">Table 2</xref>) and conducted and analyzed physical tests that complemented our fatigue tests. The result was a publication on the autogenous self-healing of SFRC (<xref rid="ref-28-e356" ref-type="bibr">28</xref>), which we will describe in this section.</p>
         <table-wrap id="taw-2-e356" position="float" orientation="portrait">
            <label>
               <bold>TABLE 2.</bold>
            </label>
            <caption>
               <title>SFRC dosage (autogenous self-healing study).</title>
            </caption>
            <table id="tab-2-e356"
                   frame="hsides"
                   rules="groups"
                   width="50&#x0025;">
               <thead>
                  <tr>
                     <th style="width:224.25pt;border-top:1pt solid &#x0023;000;border-bottom:1pt solid &#x0023;000000;"
                         rowspan="1"
                         colspan="1">Component</th>
                     <th style="width:98.3pt;border-top:1pt solid &#x0023;000;border-bottom:1pt solid &#x0023;000000;"
                         rowspan="1"
                         colspan="1">Content (kg/m<sup>3</sup>)</th>
                  </tr>
               </thead>
               <tbody>
                  <tr>
                     <td style="width:224.25pt;border-top:1pt solid &#x0023;000000;"
                         rowspan="1"
                         colspan="1">Cement CEM I 52.5 N</td>
                     <td align="center"
                         style="width:98.3pt;border-top:1pt solid &#x0023;000000;"
                         rowspan="1"
                         colspan="1">465</td>
                  </tr>
                  <tr>
                     <td style="width:224.25pt;" rowspan="1" colspan="1">Silica fume</td>
                     <td align="center" style="width:98.3pt;" rowspan="1" colspan="1">46</td>
                  </tr>
                  <tr>
                     <td style="width:224.25pt;" rowspan="1" colspan="1">Limestone filler</td>
                     <td align="center" style="width:98.3pt;" rowspan="1" colspan="1">74</td>
                  </tr>
                  <tr>
                     <td style="width:224.25pt;" rowspan="1" colspan="1">Water</td>
                     <td align="center" style="width:98.3pt;" rowspan="1" colspan="1">181</td>
                  </tr>
                  <tr>
                     <td style="width:224.25pt;" rowspan="1" colspan="1">Superplasticizer (MasterEase 3690)</td>
                     <td align="center" style="width:98.3pt;" rowspan="1" colspan="1">7.3</td>
                  </tr>
                  <tr>
                     <td style="width:224.25pt;" rowspan="1" colspan="1">Sand 4 mm (siliceous)</td>
                     <td align="center" style="width:98.3pt;" rowspan="1" colspan="1">811</td>
                  </tr>
                  <tr>
                     <td style="width:224.25pt;" rowspan="1" colspan="1">Coarse agg. 4-12 mm (siliceous, crushed)</td>
                     <td align="center" style="width:98.3pt;" rowspan="1" colspan="1">803</td>
                  </tr>
                  <tr>
                     <td style="width:224.25pt;border-bottom:1pt solid &#x0023;000;"
                         rowspan="1"
                         colspan="1">Steel fiber 4D 65/35 BG</td>
                     <td align="center"
                         style="width:98.3pt;border-bottom:1pt solid &#x0023;000;"
                         rowspan="1"
                         colspan="1">60</td>
                  </tr>
               </tbody>
            </table>
         </table-wrap>
         <sec id="sec-10-e356">
            <label>4.1.</label>
            <title>Mechanical tests</title>
            <sec id="sec-11-e356">
               <label>4.1.1.</label>
               <title>Compressive tests</title>
               <p>Compressive tests were conducted on six 100 mm cubes, all made with the corresponding ball-and-socket joint, to determine their reference compressive strength just before the beginning of fatigue tests, when the SFRC was four months old. The cubes were kept in a humid chamber until then. In <xref rid="fig-13-e356" ref-type="fig">Figure 13a</xref>, one of the cubes is shown immediately after testing. The average value obtained was 77.6 MPa, with a small standard deviation of 2.4 MPa, resulting in a coefficient of variation of only 3&#x0025;. This indicates that the mechanical behavior of this concrete for this specimen size is very consistent. Using the ball-and-socket joint contributed to this result by eliminating the source of scatter caused by load eccentricity, which is unrelated to the material (as shown in Subsection 2.5).</p>
               <fig id="fig-13-e356" position="float" orientation="portrait">
                  <label>
                     <bold>FIGURE 13.</bold>
                  </label>
                  <caption>
                     <title>(a) 80 mm cube of a series of high strength SFRC tested monotonically; (b) fatigue results of this material for four stress levels (<xref rid="ref-28-e356" ref-type="bibr">28</xref>); the dashed black straight line is the <italic toggle="yes">S</italic>-<italic toggle="yes">N</italic> curve given by the Model Code 2010 (<xref rid="ref-54-e356" ref-type="bibr">54</xref>) and the dashed grey line is given by the model of Saucedo <italic toggle="yes">et al.</italic> (<xref rid="ref-59-e356" ref-type="bibr">59</xref>) for a probability of failure of 50&#x0025;.</title>
                  </caption>
                  <graphic id="gra-13-e356"
                           xlink:href="fd09c54a6d764804a1b22ed8575c9858_013.jpg"
                           position="anchor"
                           orientation="portrait"/>
               </fig>
            </sec>
            <sec id="sec-12-e356">
               <label>4.1.2.</label>
               <title>Fatigue tests</title>
               <p>After determining the mean strength, we carried out fatigue tests at four stress ranges, all starting from minimum stress of 5&#x0025; the minimum reference strength to 70&#x0025;, 75&#x0025;, 80&#x0025;, and 90&#x0025; the reference strength. The number of tests for each stress level was determined based on the expected chances of specimen failure. In <xref rid="fig-13-e356" ref-type="fig">Figure 13b</xref>, the <italic toggle="yes">S</italic>-<italic toggle="yes">N</italic> curves show the relationship between the maximum stress level <italic toggle="yes">S</italic>
                  <sub>c,</sub>
                  <sub>max</sub> = <italic toggle="yes">σ</italic>
                  <sub>max</sub>
                  <italic toggle="yes">/f</italic>
                  <sub>c</sub> and the logarithm of the number of cycles <italic toggle="yes">N</italic>. As expected, the mean number of cycles and the number of runout specimens increase as the maximum stress decreases. Runout specimens are denoted by markers with an arrow that mainly overlap, as they represent points with similar coordinates (for instance, there were 3 runouts for <italic toggle="yes">S</italic>
                  <sub>c,</sub>
                  <sub>max</sub> = 0.8, and 5 for <italic toggle="yes">S</italic>
                  <sub>c,</sub>
                  <sub>max</sub> = 0.75, which are almost overlapped in <xref rid="fig-13-e356" ref-type="fig">Figure 13b</xref>). The distribution of the results is compared with the fatigue life prediction model included in the Model Code 2010 (<xref rid="ref-54-e356" ref-type="bibr">54</xref>) for the minimum stress level used. Most of the points lie to the right of the model, so its prediction can be considered conservative, at least for this type of fiber reinforced concrete.</p>
               <p>To accurately describe the material&#x2019;s behavior, the probabilistic model by Saucedo <italic toggle="yes">et al.</italic> (<xref rid="ref-59-e356" ref-type="bibr">59</xref>) has been applied to fit the experimental data.  This model incorporates the initial distribution, corresponding to quasi-static tests as the failure limit for one cycle while accounting for the dynamic effects of loading frequency. Consequently, the extrapolation for log <italic toggle="yes">N</italic> = 0 exceeds <italic toggle="yes">S</italic>
                  <sub>c,</sub>
                  <sub>max</sub> = 1. The fatigue data fitting was performed for <italic toggle="yes">S</italic>
                  <sub>c,</sub>
                  <sub>max</sub> = 0.9, a case with no runouts, providing complete statistical information. The model line in <xref rid="fig-13-e356" ref-type="fig">Figure 13b</xref> represents a 50&#x0025; failure probability, illustrating the estimated mean behavior for other stress levels, assuming the life estimate given by the Sparks and Menzies&#x2019; law (<xref rid="ref-52-e356" ref-type="bibr">52</xref>) for the runouts.</p>
            </sec>
            <sec id="sec-13-e356">
               <label>4.1.3.</label>
               <title>Fatigue strain</title>
               <p>During each fatigue test, strain evolution relative to the number of loading cycles <italic toggle="yes">n</italic> was recorded. As illustrated in <xref rid="fig-3-e356" ref-type="fig">Figure 3</xref>, the strain evolution until failure typically follows three stages: primary strain, characterized by rapid growth in the initial cycle interval; secondary strain, exhibiting uniform and stable behavior for most of the test; and tertiary strain, marked by accelerated strain before failure. The stability and duration of the secondary strain make it representative of the material&#x2019;s fatigue creep behavior. The average slope of this phase, or secondary strain rate per cycle <italic toggle="yes">d𝜖/dn</italic>, is related to the cycles to failure <italic toggle="yes">N</italic>. For all failed specimens, the data align along a straight line, confirming Sparks and Menzies&#x2019; law (<xref rid="ref-52-e356" ref-type="bibr">52</xref>) (see <xref rid="fig-4-e356" ref-type="fig">Figure 4</xref>). Fitting the strain-based failure model of Eq. 1 to the experimental data yields parameters <italic toggle="yes">s</italic> = -1.103 and <italic toggle="yes">m</italic> = -2.466, with a determination coefficient of 0.984. Previous studies (<xref rid="ref-14-e356" ref-type="bibr">14</xref>, <xref rid="ref-26-e356" ref-type="bibr">26</xref>, <xref rid="ref-52-e356" ref-type="bibr">52</xref>) demonstrated this relationship remains constant across variables such as loading frequency (<xref rid="ref-17-e356" ref-type="bibr">17</xref>), specimen size (<xref rid="ref-26-e356" ref-type="bibr">26</xref>, <xref rid="ref-27-e356" ref-type="bibr">27</xref>), and fiber content (<xref rid="ref-14-e356" ref-type="bibr">14</xref>) for fiber reinforced concrete.</p>
               <p>While prior work focused on a single stress range, this study extended theanalysis to three stress ranges, considering only fatigue-failed specimens. The results confirm the relationship between <italic toggle="yes">dE/dn</italic> and <italic toggle="yes">N</italic> remains constant across stress levels. Higher fatigue loads correspond to higher strain rates and shorter fatigue lives (points shift left), while lower loads result in lower strain rates and longer fatigue lives. However, all points follow the same linear trend, suggesting this relationship is a material property. As mentioned above, for runout specimens, the fatigue life can be estimated from the secondary strain rate given by the second stretch of their cyclic creep curves (<xref rid="ref-14-e356" ref-type="bibr">14</xref>), or also using the master cyclic curve developed by Blas&#x00F3;n <italic toggle="yes">et al.</italic> (<xref rid="ref-60-e356" ref-type="bibr">60</xref>, <xref rid="ref-61-e356" ref-type="bibr">61</xref>).</p>
            </sec>
            <sec id="sec-14-e356">
               <label>4.1.4.</label>
               <title>Compressive strength of runout specimens</title>
               <p>Runout specimens were immediately tested under quasi-static conditions until failure after the fatigue tests. Nine runout specimens were tested, yielding a new mean strength of 95.4 MPa, 23&#x0025; higher than the original strength. The low standard deviation, with a coefficient of variation around 2&#x0025;, indicates that the strength increase occurred consistently across all specimens. While strength gain due to aging could be a factor, the specimens were tested at different ages over three months, yet no significant strength evolution was observed. Additionally, the compressive strength of the material at the end of the fatigue tests was checked using the last remaining specimen, yielding compressive strength = 87.8 MPa. Although this single value reflects a 13&#x0025; natural strength increase due to aging, it is still lower than the strength observed in the fatigue-tested specimens. Thus, a significant part of the strength increase in the runout specimens is likely attributable to the cyclic loading.</p>
               <p>The following subsections present analyses of microstructural and compositional changes in concrete subjected to cyclic loads compared to a control specimen.</p>
            </sec>
         </sec>
         <sec id="sec-15-e356">
            <label>4.2.</label>
            <title>Physical tests</title>
            <p>Physical tests were performed on one of the runouts and on one intact cube serving as a control specimen. The selected runout corresponds to the sixth specimen from the maximum stress level of 0.75 compressive strength, representing the last fatigue test performed. Both runout and control specimens were preserved under the same conditions. Core samples were taken from them and dried in an oven at 100&#x00B0;C for 24 hours to remove moisture and slow down the hydration process as much as possible. Ideally, the samples should have been immersed in ethanol or propanol to completely stop hydration, but since both samples underwent the same treatment, this fact is not highly relevant when comparing their results to observe the effect of fatigue loads on the self-healing process. After the 24-hour drying period, the samples were analyzed, and physical tests (X-ray diffraction, thermogravimetric analysis, etc.) were performed immediately, with all analyses completed within the following 24 hours.</p>
            <sec id="sec-16-e356">
               <label>4.2.1.</label>
               <title>X-Ray Diffraction (XRD)</title>
               <p>The X-ray diffraction (XRD) results for the control and runout samples are presented in <xref rid="fig-14-e356" ref-type="fig">Figure 14a</xref>. No significant differences were observed between the two samples, either in the types of crystalline hydrates formed or their relative amounts. Therefore, if the self-healing process that occurred during the fatigue tests is associated with the formation of hydrated phases, it is likely related to the less crystalline ones, primarily calcium-silicate-hydrate (C-S-H) gels.</p>
               <fig id="fig-14-e356" position="float" orientation="portrait">
                  <label>
                     <bold>FIGURE 14.</bold>
                  </label>
                  <caption>
                     <title>Results of physical tests for one the runouts and the non-fatigued control specimen: (a) X-Ray diffractogram; (b) thermogravimetric analysis; and (c) differential thermal analysis (<xref rid="ref-28-e356" ref-type="bibr">28</xref>).</title>
                  </caption>
                  <graphic id="gra-14-e356"
                           xlink:href="fd09c54a6d764804a1b22ed8575c9858_014.jpg"
                           position="anchor"
                           orientation="portrait"/>
               </fig>
            </sec>
            <sec id="sec-17-e356">
               <label>4.2.2.</label>
               <title>Thermogravimetric Analysis (TGA) and Differential Thermal Analysis (DTA)</title>
               <p>
                  <xref rid="fig-14-e356" ref-type="fig">Figure 14b</xref> illustrates the endothermic heat flow, while <xref rid="fig-14-e356" ref-type="fig">Figure 14c</xref> depicts the weight loss of the samples during the decomposition process as the temperature rises. The typical peaks observed in cementitious materials are present: the first peak corresponds primarily to the dehydration of ettringite and calcium silicate hydrate (C-S-H) gels; the second peak is associated with the dehydration of portlandite; and the third peak relates to carbonated phases (<xref rid="ref-62-e356" ref-type="bibr">62</xref>).</p>
               <p>Although both concretes show similar results, a key difference arises when comparing hydrate contents from TGA results. The portlandite content is similar in both concretes (<xref rid="taw-3-e356" ref-type="table">Table 3</xref>), but the bound water content is higher in the runout sample, indicating an increase in hydrates due to fatigue exposure. This increase could be attributed to further hydration of anhydrous phases or pozzolanic reactions between portlandite and silica fume. Since portlandite content is unchanged, cement hydration seems to be the primary mechanism, although pozzolanic reactions cannot be ruled out.</p>
               <table-wrap id="taw-3-e356" position="float" orientation="portrait">
                  <label>
                     <bold>TABLE 3.</bold>
                  </label>
                  <caption>
                     <title>Portlandite and bound water measured by DTA/TG (in weight percentage).</title>
                  </caption>
                  <table id="tab-3-e356"
                         frame="hsides"
                         rules="groups"
                         width="50&#x0025;">
                     <thead>
                        <tr>
                           <th style="width:50.65pt;border-top:1pt solid &#x0023;000;border-bottom:1pt solid &#x0023;000000;"
                               rowspan="1"
                               colspan="1">Sample</th>
                           <th align="left"
                               style="width:69.6pt;border-top:1pt solid &#x0023;000;border-bottom:1pt solid &#x0023;000000;"
                               rowspan="1"
                               colspan="1">Portlandite</th>
                           <th align="left"
                               style="width:77.85pt;border-top:1pt solid &#x0023;000;border-bottom:1pt solid &#x0023;000000;"
                               rowspan="1"
                               colspan="1">Bound water</th>
                        </tr>
                     </thead>
                     <tbody>
                        <tr>
                           <td style="width:50.65pt;border-top:1pt solid &#x0023;000000;"
                               rowspan="1"
                               colspan="1">Runout</td>
                           <td style="width:69.6pt;border-top:1pt solid &#x0023;000000;"
                               rowspan="1"
                               colspan="1">2.0</td>
                           <td style="width:77.85pt;border-top:1pt solid &#x0023;000000;"
                               rowspan="1"
                               colspan="1">9.7</td>
                        </tr>
                        <tr>
                           <td style="width:50.65pt;border-bottom:1pt solid &#x0023;000;"
                               rowspan="1"
                               colspan="1">Control</td>
                           <td style="width:69.6pt;border-bottom:1pt solid &#x0023;000;"
                               rowspan="1"
                               colspan="1">2.0</td>
                           <td style="width:77.85pt;border-bottom:1pt solid &#x0023;000;"
                               rowspan="1"
                               colspan="1">9.4</td>
                        </tr>
                     </tbody>
                  </table>
               </table-wrap>
               <p>The additional 3&#x0025; of hydrates formed in the runout sample, though modest, may contribute to healing microcracks generated during fatigue cycles or at least to a partial self-healing process. Detachment of small particles during fatigue may also fill these microcracks, enhancing compressive strength. However, backscattered scanning electron microscopy (BSEM) evaluations in the next section do not clearly detect such detached particles, though hydrated phases are observed growing within microcracks.</p>
               <p>These findings underscore the formation of new C-S-H gel after cyclic compressive loading, crucial for early-age strength gains. Notably, no increase in carbonate phases is observed in the runout sample, suggesting carbonation is not the primary driver of self-healing. However, this does not rule out its occurrence, as discussed in the next section. The movement of free water within the concrete matrix, promoted by cyclic loading, likely facilitates hydrate formation, healing incipient cracks generated by the load.</p>
            </sec>
            <sec id="sec-18-e356">
               <label>4.2.3.</label>
               <title>Backscattered Scanning Electron Microscopy (BSEM)</title>
               <p>
                  <xref rid="fig-15-e356" ref-type="fig">Figure 15a</xref> presents an BSEM image of the surface of the runout sample, highlighting the fatigue-induced damage. Cracks are visible in the aggregate particle and cementitious matrix, particularly in the C-S-H gel phases, surrounding nonhydrated cement particles, portlandite crystals, or near pores, which act as stress concentration zones. Some cracks stop propagating and fade out.</p>
               <fig id="fig-15-e356" position="float" orientation="portrait">
                  <label>
                     <bold>FIGURE 15.</bold>
                  </label>
                  <caption>
                     <title>(a) BSEM image of a runout specimen, and (b) its corresponding spectral analysis (<xref rid="ref-28-e356" ref-type="bibr">28</xref>).</title>
                  </caption>
                  <graphic id="gra-15-e356"
                           xlink:href="fd09c54a6d764804a1b22ed8575c9858_015.jpeg"
                           position="anchor"
                           orientation="portrait"/>
               </fig>
               <p>
                  <xref rid="fig-15-e356" ref-type="fig">Figure 15b</xref> shows the spectral analysis of the minerals within the rectangular area in <xref rid="fig-15-e356" ref-type="fig">Figure 15a</xref>, focusing on a smooth surface identified as a siliceous aggregate particle through spectral analysis. Additional images and analyses, particularly of the interfacial transition zone (ITZ), reveal new C-S-H gel phases overlapping cracks in the ITZ and new hydrated C-S-H phases near a silica fume particle, likely formed by pozzolanic reactions, halting crack propagation (see Figures <xref rid="fig-10-e356 fig-11-e356" ref-type="fig">10</xref>-<xref rid="fig-12-e356" ref-type="fig">12</xref> in (<xref rid="ref-28-e356" ref-type="bibr">28</xref>)). A significant aluminum peak suggests the formation of C-A-S-H gels, as previously reported (<xref rid="ref-63-e356 ref-64-e356" ref-type="bibr">63</xref>-<xref rid="ref-65-e356" ref-type="bibr">65</xref>), which consist of longer silica chains and play a role in halting crack propagation. Additionally, potential portlandite carbonation may form calcite, releasing water into the system (<xref rid="ref-66-e356" ref-type="bibr">66</xref>, <xref rid="ref-67-e356" ref-type="bibr">67</xref>), further promoting hydration under cyclic compressive loads. Thus, SEM analysis suggests that self-healing under compressive cyclic loading is driven by both hydration of anhydrous phases and pozzolanic reactions forming C-A-S-H gels.</p>
            </sec>
            <sec id="sec-19-e356">
               <label>4.2.4.</label>
               <title>Mercury Intrusion Porosimetry (MIP)</title>
               <p>
                  <xref rid="fig-16-e356" ref-type="fig">Figure 16</xref> shows the pore size distribution for both specimens, with peaks corresponding to predominant pore sizes that account for higher void volume. Peaks below 1 &#x00B5;m are similarly distributed, but beyond this size, differences emerge. Around 10 &#x00B5;m, the runout specimen exhibits a peak above the control specimen, indicating greater void volume, likely due to crack openings caused during compressive testing. These openings would depend on the damage level of each specimen. Conversely, smaller size differences are more indicative of the concrete matrix&#x2019;s microstructure. Notably, the runout specimen shows a clear reduction in pore volume around 0.04 &#x00B5;m, and between 1 &#x00B5;m and 5 &#x00B5;m, as seen in the logarithmic plot of injected mercury per sample mass (<xref rid="fig-16-e356" ref-type="fig">Figure 16</xref>).</p>
               <fig id="fig-16-e356" position="float" orientation="portrait">
                  <label>
                     <bold>FIGURE 16.</bold>
                  </label>
                  <caption>
                     <title>Porosimetries of both runout and control specimens (<xref rid="ref-28-e356" ref-type="bibr">28</xref>).</title>
                  </caption>
                  <graphic id="gra-16-e356"
                           xlink:href="fd09c54a6d764804a1b22ed8575c9858_016.jpg"
                           position="anchor"
                           orientation="portrait"/>
               </fig>
               <p>
                  <xref rid="taw-4-e356" ref-type="table">Table 4</xref> presents additional MIP analysis results. The runout specimen shows a lower total pore area and average pore diameter compared to the control specimen. Tortuosity, defined as the ratio of actual flow path length to the straight distance between the path ends, is also reduced, with the runout specimen at 56&#x0025; of the control&#x2019;s value. These results suggest a reduction in pore volume and closure of microcracking paths after the application of cyclic compressive loads.</p>
               <table-wrap id="taw-4-e356" position="float" orientation="portrait">
                  <label>
                     <bold>TABLE 4.</bold>
                  </label>
                  <caption>
                     <title>Parameters obtained by MIP.</title>
                  </caption>
                  <table id="tab-4-e356"
                         frame="hsides"
                         rules="groups"
                         width="50&#x0025;">
                     <thead>
                        <tr>
                           <th align="center"
                               style="width:157.65pt;border-top:1pt solid &#x0023;000;border-bottom:1pt solid &#x0023;000000;"
                               rowspan="1"
                               colspan="1">Parameter</th>
                           <th align="center"
                               style="width:50.5pt;border-top:1pt solid &#x0023;000;border-bottom:1pt solid &#x0023;000000;"
                               rowspan="1"
                               colspan="1">Runout</th>
                           <th align="center"
                               style="width:50.65pt;border-top:1pt solid &#x0023;000;border-bottom:1pt solid &#x0023;000000;"
                               rowspan="1"
                               colspan="1">Control</th>
                        </tr>
                     </thead>
                     <tbody>
                        <tr>
                           <td style="width:157.65pt;border-top:1pt solid &#x0023;000000;"
                               rowspan="1"
                               colspan="1">Total pore area (m<sup>2</sup>/g)</td>
                           <td align="center"
                               style="width:50.5pt;border-top:1pt solid &#x0023;000000;"
                               rowspan="1"
                               colspan="1">2.23</td>
                           <td align="center"
                               style="width:50.65pt;border-top:1pt solid &#x0023;000000;"
                               rowspan="1"
                               colspan="1">2.80</td>
                        </tr>
                        <tr>
                           <td style="width:157.65pt;" rowspan="1" colspan="1">Average pore diameter (nm)</td>
                           <td align="center" style="width:50.5pt;" rowspan="1" colspan="1">55.6</td>
                           <td align="center" style="width:50.65pt;" rowspan="1" colspan="1">68.4</td>
                        </tr>
                        <tr>
                           <td style="width:157.65pt;border-bottom:1pt solid &#x0023;000;"
                               rowspan="1"
                               colspan="1">Tortuosity</td>
                           <td align="center"
                               style="width:50.5pt;border-bottom:1pt solid &#x0023;000;"
                               rowspan="1"
                               colspan="1">5.17</td>
                           <td align="center"
                               style="width:50.65pt;border-bottom:1pt solid &#x0023;000;"
                               rowspan="1"
                               colspan="1">9.18</td>
                        </tr>
                     </tbody>
                  </table>
               </table-wrap>
            </sec>
         </sec>
      </sec>
      <sec sec-type="discussion" id="sec-20-e356">
         <label>5.</label>
         <title>Discussion</title>
         <p>The results support the notion that cyclic compressive loads induce an autogenous self-healing process in the material. The primary causes of this phenomenon are analyzed below.</p>
         <p>Considering the types of water and voids within the hydrated cement paste is crucial to understanding autogenous self-healing in concrete. Capillary water, which is not bound to the solid surface, plays a vital role in the self-healing process. Capillary voids&#x2014;spaces not filled by hydration products, see <xref rid="taw-5-e356" ref-type="table">Table 5</xref> &#x2014;depend on the degree of hydration (<xref rid="ref-68-e356" ref-type="bibr">68</xref>). For autogenous self-healing to take place, there must be sufficient free water available. The movement of water into cracks is influenced by factors such as porosity, pore structure, and connectivity (<xref rid="fig-16-e356" ref-type="fig">Figure 16</xref>, <xref rid="taw-4-e356" ref-type="table">Table 4</xref>). Although the concrete examined in the previous section has a low water-binder ratio, its short age and humid curing conditions are conducive to potential self-healing.</p>
         <table-wrap id="taw-5-e356" position="float" orientation="portrait">
            <label>
               <bold>TABLE 5.</bold>
            </label>
            <caption>
               <title>Pore size classification in hydrated cement pastes (modified from Mindess and Young (<xref rid="ref-68-e356" ref-type="bibr">68</xref>, <xref rid="ref-69-e356" ref-type="bibr">69</xref>)).</title>
            </caption>
            <table id="tab-5-e356"
                   frame="hsides"
                   rules="groups"
                   width="50&#x0025;">
               <thead>
                  <tr>
                     <th style="width:85.45pt;border-top:1pt solid &#x0023;000;border-bottom:1pt solid &#x0023;000000;"
                         rowspan="1"
                         colspan="1">Type of pore</th>
                     <th align="center"
                         style="width:116pt;border-top:1pt solid &#x0023;000;border-bottom:1pt solid &#x0023;000000;"
                         rowspan="1"
                         colspan="1">Denomination</th>
                     <th align="center"
                         style="width:85.4pt;border-top:1pt solid &#x0023;000;border-bottom:1pt solid &#x0023;000000;"
                         rowspan="1"
                         colspan="1">Size</th>
                  </tr>
               </thead>
               <tbody>
                  <tr>
                     <td style="width:85.45pt;border-top:1pt solid &#x0023;000000;"
                         rowspan="1"
                         colspan="1">Gel pore</td>
                     <td align="left"
                         style="width:116pt;border-top:1pt solid &#x0023;000000;"
                         rowspan="1"
                         colspan="1">Interlayer micropore</td>
                     <td align="left"
                         style="width:85.4pt;border-top:1pt solid &#x0023;000000;"
                         rowspan="1"
                         colspan="1">
                        <italic toggle="yes">&#x003E;</italic> 0.5 nm</td>
                  </tr>
                  <tr>
                     <td style="width:85.45pt;" rowspan="1" colspan="1">Gel pore</td>
                     <td align="left" style="width:116pt;" rowspan="1" colspan="1">Micropore</td>
                     <td align="left" style="width:85.4pt;" rowspan="1" colspan="1">0.5 nm-2.5 nm</td>
                  </tr>
                  <tr>
                     <td style="width:85.45pt;" rowspan="1" colspan="1">Gel pore</td>
                     <td align="left" style="width:116pt;" rowspan="1" colspan="1">Small capillary (gel)</td>
                     <td align="left" style="width:85.4pt;" rowspan="1" colspan="1">2.5 nm-10 nm</td>
                  </tr>
                  <tr>
                     <td style="width:85.45pt;" rowspan="1" colspan="1">Capillary pore</td>
                     <td align="left" style="width:116pt;" rowspan="1" colspan="1">Medium capillary</td>
                     <td align="left" style="width:85.4pt;" rowspan="1" colspan="1">10 nm-50 nm</td>
                  </tr>
                  <tr>
                     <td style="width:85.45pt;" rowspan="1" colspan="1">Capillary pore</td>
                     <td align="left" style="width:116pt;" rowspan="1" colspan="1">Large capillary</td>
                     <td align="left" style="width:85.4pt;" rowspan="1" colspan="1">0.05 &#x00B5;m-10 &#x00B5;m</td>
                  </tr>
                  <tr>
                     <td style="width:85.45pt;border-bottom:1pt solid &#x0023;000;"
                         rowspan="1"
                         colspan="1">Air</td>
                     <td align="left"
                         style="width:116pt;border-bottom:1pt solid &#x0023;000;"
                         rowspan="1"
                         colspan="1">Entrapped air</td>
                     <td align="left"
                         style="width:85.4pt;border-bottom:1pt solid &#x0023;000;"
                         rowspan="1"
                         colspan="1">0.01 mm-1 mm</td>
                  </tr>
               </tbody>
            </table>
         </table-wrap>
         <p>Cyclic compressive loads exert simultaneous damage and healing effects. Whether healing or damage dominates influences the residual compressive strength and fatigue life (as sketched in Figure <xref rid="fig-17-e356" ref-type="fig">17</xref>). As cyclic loads generate microcracks, water moves through them (<xref rid="ref-70-e356" ref-type="bibr">70</xref>, <xref rid="ref-71-e356" ref-type="bibr">71</xref>), reaching other areas via flow and diffusion (<xref rid="ref-70-e356" ref-type="bibr">70</xref>), as schematically represented in <xref rid="fig-18-e356" ref-type="fig">Figure 18</xref>. The dynamic pressure from water at crack tips induces stress, potentially deepening cracks (<xref rid="ref-72-e356" ref-type="bibr">72</xref>). Higher pressure and larger crack openings accelerate microcrack growth, reducing fatigue life if no self-healing occurs (<xref rid="ref-73-e356" ref-type="bibr">73</xref>).</p>
         <fig id="fig-18-e356" position="float" orientation="portrait">
            <label>
               <bold>FIGURE 18.</bold>
            </label>
            <caption>
               <title>Plausible autogenous self-healing mechanisms of cracks in SFRC &#x005B;<xref rid="ref-28-e356" ref-type="bibr">28</xref>&#x005D;.</title>
            </caption>
            <graphic id="gra-18-e356"
                     xlink:href="fd09c54a6d764804a1b22ed8575c9858_018.jpg"
                     position="anchor"
                     orientation="portrait"/>
         </fig>
         <p>However, self-healing comes about through the hydration of non-hydrated particles in young concrete, while carbonation dominates in older concrete (<xref rid="ref-74-e356" ref-type="bibr">74</xref>). Water movement through cracks (<xref rid="fig-18-e356" ref-type="fig">Figure 18</xref>) promotes ongoing hydration, carbonation, and dissolution reactions, creating complex chemical processes that influence self-healing (<xref rid="ref-75-e356" ref-type="bibr">75</xref>). Crack morphology affects healing, with faster product formation at crack tips (<xref rid="ref-76-e356" ref-type="bibr">76</xref>).</p>
         <p>The primary physical cause of self-healing is the expansion of hydration products near microcracks when exposed to water (<xref rid="ref-77-e356" ref-type="bibr">77</xref>). The main product is CaCO<sub>3</sub> (<xref rid="ref-77-e356" ref-type="bibr">77</xref>), and non-hydrated particles also form portlandite and C-S-H gel. However, C-S-H gel primarily accumulates on crack surfaces, not within cracks (<xref rid="ref-77-e356" ref-type="bibr">77</xref>). Self-healing near crack surfaces is driven by rapid crystalline precipitation. Continuous hydration enhances early-age self-healing due to higher portlandite and moisture content (<xref rid="ref-36-e356" ref-type="bibr">36</xref>), although carbonation may play a greater role (<xref rid="ref-36-e356" ref-type="bibr">36</xref>). These reactions alter concrete&#x2019;s microstructure, affecting porosity, permeability, and hydration (<xref rid="ref-78-e356" ref-type="bibr">78</xref>, <xref rid="ref-79-e356" ref-type="bibr">79</xref>).</p>
         <sec id="sec-21-e356">
            <label>5.1.</label>
            <title>Effect of the mineral additions</title>
            <p>Mineral additions with pozzolanic activity (e.g., silica fume) participate in hydration, while non-pozzolanic additions (e.g., limestone powder) act as nucleation sites, both contributing to C-S-H gel formation and pore refinement (<xref rid="ref-80-e356" ref-type="bibr">80</xref>, <xref rid="ref-81-e356" ref-type="bibr">81</xref>). This reduces stress concentrations at defects, which are linked to fractures (<xref rid="ref-80-e356" ref-type="bibr">80</xref>, <xref rid="ref-82-e356" ref-type="bibr">82</xref>). Mineral additions also enhance autogenous self-healing via delayed hydration, depending on their reactivity during microcracking (<xref rid="ref-36-e356" ref-type="bibr">36</xref>, <xref rid="ref-83-e356" ref-type="bibr">83</xref>).</p>
            <p>Optimal limestone powder content (10&#x0025;) improves fiber-matrix bonding by increasing C-S-H gel density and reducing porosity, while excess powder leads to low-density C-S-H, weakening this bond (<xref rid="ref-84-e356" ref-type="bibr">84</xref>). Pozzolanic additions reduce gel porosity but may increase capillary pores due to C-S-H gel carbonation (<xref rid="ref-66-e356" ref-type="bibr">66</xref>). Continued hydration and pozzolanic reactions may promote long-term self-healing at greater depths (<xref rid="ref-77-e356" ref-type="bibr">77</xref>, <xref rid="ref-85-e356" ref-type="bibr">85</xref>).</p>
         </sec>
         <sec id="sec-22-e356">
            <label>5.2.</label>
            <title>Effect of the carbonation</title>
            <p>In carbonation, portlandite &#x2014;Ca(OH)<sub>2</sub>&#x2014; reacts with CO<sub>2</sub>, along with C-S-H gel and unreacted cement, water being essential for these reactions. This process, governed by exposure conditions, alters porosity and pore size distribution, sometimes increasing strength due to structural changes in the C-S-H gel. However, this can lead to carbonation-induced cracking, making it difficult to assess the overall impact on mechanical and transport properties (<xref rid="ref-86-e356" ref-type="bibr">86</xref>). The C-S-H gel, which contains the most calcium, exhibits complex carbonation behavior influenced by the original Ca/Si ratio, CO<sub>2</sub> concentration, and portlandite presence (<xref rid="ref-66-e356" ref-type="bibr">66</xref>, <xref rid="ref-87-e356" ref-type="bibr">87</xref>).</p>
            <p>Using pozzolanic mineral additions, like silica fume as in the case study above (see <xref rid="taw-2-e356" ref-type="table">Table 2</xref>), alters the role of portlandite in carbonation. As pozzolanic material increases, portlandite production during hydration decreases, while its consumption in the pozzolanic reaction rises. Adding silica fume may enhance carbonation in concrete, helping to seal cracks. However, DTA and TGA results show that the carbonated phase content is similar in both the reference sample and the one under compressive cyclic loads (see <xref rid="taw-3-e356" ref-type="table">Table 3</xref>). Therefore, we do not anticipate that faster carbonation under these loads will significantly improve the self-healing process.</p>
         </sec>
         <sec id="sec-23-e356">
            <label>5.3.</label>
            <title>Effect of the steel fiber reinforcement</title>
            <p>Fibers play a crucial role in the autogenous self-healing process under compressive cyclic loads by controlling microcrack width and propagation (<xref rid="ref-88-e356 ref-89-e356 ref-90-e356 ref-91-e356 ref-92-e356 ref-93-e356 ref-94-e356 ref-95-e356 ref-96-e356 ref-97-e356 ref-98-e356"
                     ref-type="bibr">88</xref>-<xref rid="ref-99-e356" ref-type="bibr">99</xref>). Microcracks narrower than 50 &#x00B5;m may fully seal (<xref rid="ref-88-e356" ref-type="bibr">88</xref>, <xref rid="ref-100-e356 ref-101-e356" ref-type="bibr">100</xref>-<xref rid="ref-102-e356" ref-type="bibr">102</xref>). Fiber reinforcement also increases the tortuosity and roughness of microcracks (<xref rid="ref-103-e356" ref-type="bibr">103</xref>), enhancing autogenous self-healing <xref rid="fig-18-e356" ref-type="fig">(Figure 18</xref>). However, excessive fiber content can introduce weak interfaces, reducing reinforcement effectiveness (<xref rid="ref-14-e356" ref-type="bibr">14</xref>, <xref rid="ref-80-e356" ref-type="bibr">80</xref>).</p>
            <p>Crack opening rate affects internal water pressure distribution: a slower rate allows pressure to build up, while a faster rate prevents the waterfront from advancing along the crack front. When a saturated fracture zone closes rapidly, water can become trapped, acting as a wedge that induces tensile stresses (<xref rid="ref-104-e356" ref-type="bibr">104</xref>). As tensile stresses increase and crack surfaces begin to separate, the cohesive force of water slows crack initiation and propagation.</p>
         </sec>
         <sec id="sec-24-e356">
            <label>5.4.</label>
            <title>Effect of the damage distribution and size effect</title>
            <p>The self-healing process competes with fatigue-induced damage, and understanding their interaction is crucial, as the material response depends on which mechanism dominates (<xref rid="fig-17-e356" ref-type="fig">Figure 17</xref>). Fatigue damage in cementitious materials primarily arises from the initiation and propagation of microcracks (<xref rid="ref-105-e356" ref-type="bibr">105</xref>). To interpret overall fatigue behavior, including the interfacial transition zone (ITZ), it is important to examine fatigue behavior at different scales.</p>
            <fig id="fig-17-e356" position="float" orientation="portrait">
               <label>
                  <bold>FIGURE 17.</bold>
               </label>
               <caption>
                  <title>Effect of the autogenous self-healing due to fatigue on the cyclic creep curves. Blue curves schematically represent specimens experiencing significant self-healing, thus enduring longer &#x2014;solid line&#x2014; or surviving &#x2014;dashed line&#x2014; than another specimen of the same material with no or minimal self-healing &#x2014;orange curve&#x2014;.</title>
               </caption>
               <graphic id="gra-17-e356"
                        xlink:href="fd09c54a6d764804a1b22ed8575c9858_017.jpg"
                        position="anchor"
                        orientation="portrait"/>
            </fig>
            <p>At the nanoscale, crack propagation is governed by the breaking of nanoparticle connections, particularly the rupture of C-S-H gel, which propagates until merging into the main crack (<xref rid="ref-105-e356" ref-type="bibr">105</xref>). Weakening localized stress concentrations through pore structure refinement or connecting nano-cracks allows a broader distribution of microcracks, promoting energy dissipation. Nano-crack propagation can be slowed by the bonding effect of nano-cracks and by the formation of denser C-S-H gel with higher polymerization, along with smaller calcium hydroxide crystals (<xref rid="ref-70-e356" ref-type="bibr">70</xref>, <xref rid="ref-80-e356" ref-type="bibr">80</xref>, <xref rid="ref-106-e356" ref-type="bibr">106</xref>).</p>
            <p>At the microscale, existing cracks, especially in the ITZ, coalesce with fatigue cracks in the cement matrix (<xref rid="ref-105-e356" ref-type="bibr">105</xref>). Due to its porosity, the ITZ is highly vulnerable to fatigue, exhibiting a higher likelihood of crack initiation and propagation compared to the matrix (105, 107-109). Faster crack growth in the ITZ accelerates damage, while increased damage distribution enhances autogenous self-healing by generating more microcracks and facilitating energy dissipation, thus strengthening the material.</p>
            <p>The internal stress distribution, influenced by specimen size, further affects self-healing potential, as previously noted in Section 3 (<xref rid="ref-26-e356" ref-type="bibr">26</xref>). Scale effects on crack propagation and fatigue life can be analyzed from the micro- to the macroscale (<xref rid="ref-110-e356" ref-type="bibr">110</xref>, <xref rid="ref-111-e356" ref-type="bibr">111</xref>). From this perspective, smaller specimens result in a more distributed arrangement of microcracks, making them more susceptible to significant self-healing compared to larger specimens of the same material (<xref rid="ref-26-e356" ref-type="bibr">26</xref>, <xref rid="ref-27-e356" ref-type="bibr">27</xref>).</p>
         </sec>
         <sec id="sec-25-e356">
            <label>5.5.</label>
            <title>Effective time for autogenous self-healing</title>
            <p>Autogenous self-healing is induced over a specific period. By 10 hours into hydration, significant amounts of C-S-H gel, portlandite, and ettringite are present, especially the latter. At 50 hours, C-S-H gel and portlandite increase notably, while ettringite decreases. Calcite content is crucial as it controls available carbonates and influences the formation of hemicarboaluminate phases over ettringite and monosulfate phases (<xref rid="ref-112-e356" ref-type="bibr">112</xref>).</p>
            <p>The extent of crack repair depends on the repair type, duration, and crack characteristics. If the volume of cracks is insufficient for complete closure, repair efficiency decreases due to the exponential growth of cracks (<xref rid="ref-113-e356" ref-type="bibr">113</xref>). When damage progresses rapidly, self-healing cannot counteract it, as seen in tests at 90&#x0025; of the compressive strength in <xref rid="fig-13-e356" ref-type="fig">Figure 13</xref>, where the longest fatigue life was under one hour. For other loading conditions, the longest fatigue life for fatigue-failed specimens was about eight hours, after which a stable strain phase occurs. Analogously, low frequencies in steel-fiber reinforced concrete fatigue can also favor the self-healing process by providing the time needed for it, as described in subsection 2.3 (<xref rid="ref-17-e356" ref-type="bibr">17</xref>). In summary, slower damage progression increases the likelihood of self-healing controlling crack propagation.</p>
         </sec>
      </sec>
      <sec sec-type="conclusions" id="sec-26-e356">
         <label>6.</label>
         <title>Conclusions</title>
         <p>This article examined the effect of size on the compressive fatigue of steel fiber reinforced concrete, described the autogenous self-healing of this material resulting from compressive fatigue, and the interactions between them. Additionally, it included a review of fatigue phenomenology to familiarize the reader with the topic, drawing mainly from the authors&#x2019; contributions to the state of the art. The research outlined in the paper yielded several relevant conclusions:</p>
         <list id="lst-1-e356" list-type="bullet">
            <list-item>
               <p>
                  <bold>Role of fibers in fatigue behavior &#x0026; effect of frequency:</bold> Steel fibers significantly enhance the fatigue life of SFRC, particularly at low to intermediate fiber contents, by improving post-cracking behavior and reducing crack propagation through fiber pull-out mechanisms. However, excessive fiber content can have adverse effects, as it introduces matrix imperfections and air voids, which may serve as crack initiation points. Therefore, there is an optimal fiber dosage, beyond which the benefits of fiber reinforcement decline. Additionally, fibers promote a denser microcrack pattern that evolves gradually, increasing the material&#x2019;s stability and toughness by absorbing the released elastic energy. This controlled evolution of cracks may also allow sufficient time for self-healing processes to take place, particularly under low-frequency loading.</p>
            </list-item>
            <list-item>
               <p>
                  <bold>Size effect in compressive fatigue:</bold> Specimen size significantly affects the fatigue life of SFRC. Larger specimens tend to exhibit reduced fatigue life due to the increased likelihood of microcracks and large pores acting as stress concentrators. These microcracks can become unstable because of the large amount of elastic energy available to drive their propagation with each cycle. This behavior aligns with classical size effect theory, where larger elements show lower strength under cyclic loading because of their greater potential for crack growth. Conversely, the confined conditions in smaller specimens, particularly cubes, along with their increased relative capacity for energy dissipation, make them more resistant to fatigue. This phenomenon may interact with fatigue-induced additional hydration, which requires extensive microcracking and time to fully develop, heal, and even improve the material&#x2019;s properties. These insights are essential for scaling fatigue performance from small laboratory specimens to real-world structural elements.</p>
            </list-item>
            <list-item>
               <p>
                  <bold>Autogenous self-healing:</bold> A key finding is the substantial role of autogenous self-healing in enhancing fatigue resistance. Fatigue-induced microcracks allow occluded moisture to penetrate the concrete matrix, which rehydrates dormant cementitious particles and promotes the precipitation of calcium carbonate. These processes help seal microcracks and improve the material&#x2019;s residual strength. This effect was particularly evident in specimens subjected to fatigue loading that stood prolonged cycles, exhibiting a notable increase in compressive strength post-fatigue. These positive effects are often overlooked in concrete technology, but they present a promising opportunity to harness and leverage the material improvements induced by cyclic loads in SFRC, which is naturally prone to self-healing under fatigue conditions.</p>
            </list-item>
            <list-item>
               <p>
                  <bold>Interaction between size effect and autogenous self-healing:</bold> The size effect interacts with the self-healing process. Smaller specimens, with more extensive microcracking relative to their volume, provide greater opportunities for self-healing mechanisms to activate. However, the effectiveness of self-healing is contingent on factors such as the availability of unhydrated particles and occluded water.</p>
            </list-item>
            <list-item>
               <p>
                  <bold>Implications for structural design:</bold> These results have important implications for the design of SFRC in structural applications, particularly for elements subjected to cyclic compressive loads, such as wind turbine towers and high-speed railway slabs. The size effect must be accounted for in fatigue design, and the potential for autogenous self-healing should be considered as a factor that can enhance long-term durability.</p>
            </list-item>
         </list>
         <p>Overall, this research highlights the complex interaction between fatigue loading, size effect, fiber reinforcement, and autogenous self-healing in SFRC. It underscores the need for careful consideration of these phenomena in both material design and the scaling of experimental results to full-scale structural elements.</p>
      </sec>
   </body>
   <back>
      <sec sec-type="apoyo" id="sec-27-e356">
         <title>Funding Sources</title>
         <p>The authors acknowledge the funding obtained from the <italic toggle="yes">Ministerio de Ciencia e Innovaci&#x00B4;on</italic> through the project PID2019-110928RB-C31 and PID2023-147971OB- C31, and from the <italic toggle="yes">Universidad de Castilla-La Mancha</italic>, Spain, and the <italic toggle="yes">Fondo Europeo de Desarrollo Regional</italic> through grant 2022-GRIN-34124.</p>
      </sec>
      <sec sec-type="author-contributions" id="sec-28-e356">
         <title>Authorship contribution statement</title>
         <p>
            <bold>Gonzalo Ruiz</bold>: Conceptualization, Methodology, Experiments, Calculations, Writing - original draft, Writing - review &#x0026; editing, Supervision, Resources, Funding acquisition.</p>
         <p>
            <bold>&#x00C1;ngel De La Rosa</bold>: Methodology, Experiments, Calculations, Writing - original draft, Writing - review &#x0026; editing.</p>
         <p>
            <bold>Jos&#x00E9; Joaqu&#x00ED;n Ortega</bold>: Methodology, Experiments, Calculations, Writing - original draft, Writing - review &#x0026; editing.</p>
         <p>
            <bold>Elisa Poveda</bold>: Methodology, Experiments, Calculations, Writing - review &#x0026; editing.</p>
         <p>
            <bold>Rena C. Yu</bold>: Methodology, Experiments, Calculations, Writing - review &#x0026; editing.</p>
         <p>
            <bold>Manuel Tarifa</bold>: Methodology, Experiments, Calculations, Writing - review &#x0026; editing.</p>
         <p>
            <bold>Xiaoxin X. Zhang</bold>: Methodology, Experiments, Calculations, Writing - review &#x0026; editing.</p>
         <p>
            <bold>Luc&#x00ED;a Garijo</bold>: Methodology, Experiments, Calculations, Writing - review &#x0026; editing.</p>
      </sec>
      <sec sec-type="transparency-statement" id="sec-29-e356">
         <title>Declaration of competing interest</title>
         <p>The authors of this article declare that they have no financial, professional or personal conflicts of in-terest that could have inappropriately influenced this work.</p>
      </sec>
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