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<front>
<journal-meta>
<journal-id journal-id-type="publisher-id">Front. Mater.</journal-id>
<journal-title>Frontiers in Materials</journal-title>
<abbrev-journal-title abbrev-type="pubmed">Front. Mater.</abbrev-journal-title>
<issn pub-type="epub">2296-8016</issn>
<publisher>
<publisher-name>Frontiers Media S.A.</publisher-name>
</publisher>
</journal-meta>
<article-meta>
<article-id pub-id-type="publisher-id">1126806</article-id>
<article-id pub-id-type="doi">10.3389/fmats.2023.1126806</article-id>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Materials</subject>
<subj-group>
<subject>Original Research</subject>
</subj-group>
</subj-group>
</article-categories>
<title-group>
<article-title>Crack sliding model for non-shear FRP-reinforced slender concrete elements under shear</article-title>
<alt-title alt-title-type="left-running-head">El-said et al.</alt-title>
<alt-title alt-title-type="right-running-head">
<ext-link ext-link-type="uri" xlink:href="https://doi.org/10.3389/fmats.2023.1126806">10.3389/fmats.2023.1126806</ext-link>
</alt-title>
</title-group>
<contrib-group>
<contrib contrib-type="author">
<name>
<surname>El-said</surname>
<given-names>Amr</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
<uri xlink:href="https://loop.frontiersin.org/people/2083110/overview"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Awad</surname>
<given-names>Ahmed</given-names>
</name>
<xref ref-type="aff" rid="aff2">
<sup>2</sup>
</xref>
<uri xlink:href="https://loop.frontiersin.org/people/2082112/overview"/>
</contrib>
<contrib contrib-type="author" corresp="yes">
<name>
<surname>El-Sayed</surname>
<given-names>Taha A.</given-names>
</name>
<xref ref-type="aff" rid="aff3">
<sup>3</sup>
</xref>
<xref ref-type="corresp" rid="c001">&#x2a;</xref>
<uri xlink:href="https://loop.frontiersin.org/people/501553/overview"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname>&#xd6;zk&#x131;l&#x131;&#xe7;</surname>
<given-names>Yasin Onuralp</given-names>
</name>
<xref ref-type="aff" rid="aff4">
<sup>4</sup>
</xref>
<uri xlink:href="https://loop.frontiersin.org/people/1687595/overview"/>
</contrib>
<contrib contrib-type="author" corresp="yes">
<name>
<surname>Deifalla</surname>
<given-names>A.</given-names>
</name>
<xref ref-type="aff" rid="aff5">
<sup>5</sup>
</xref>
<xref ref-type="corresp" rid="c001">&#x2a;</xref>
<uri xlink:href="https://loop.frontiersin.org/people/1367322/overview"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Tawfik</surname>
<given-names>Maged</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
<uri xlink:href="https://loop.frontiersin.org/people/2082123/overview"/>
</contrib>
</contrib-group>
<aff id="aff1">
<sup>1</sup>
<institution>Department of Civil Engineering</institution>, <institution>The Higher Institute of Engineering</institution>, <addr-line>El Shrouk</addr-line>, <addr-line>Cairo</addr-line>, <country>Egypt</country>
</aff>
<aff id="aff2">
<sup>2</sup>
<institution>Faculty of Engineering</institution>, <institution>October University for Modern Sciences and Arts</institution>, <addr-line>Giza</addr-line>, <country>Egypt</country>
</aff>
<aff id="aff3">
<sup>3</sup>
<institution>Department of Structural Engineering</institution>, <institution>Shoubra Faculty of Engineering -Benha University</institution>, <addr-line>Cairo</addr-line>, <country>Egypt</country>
</aff>
<aff id="aff4">
<sup>4</sup>
<institution>Necmettin Erbakan University</institution>, <institution>Faculty of Engineering</institution>, <institution>Department of Civil Engineering</institution>, <addr-line>Konya</addr-line>, <country>Turkey</country>
</aff>
<aff id="aff5">
<sup>5</sup>
<institution>Structural Engineering and Construction Management Department</institution>, <institution>Future University in Engineering</institution>, <addr-line>Cairo</addr-line>, <country>Egypt</country>
</aff>
<author-notes>
<fn fn-type="edited-by">
<p>
<bold>Edited by:</bold> <ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/1864834/overview">Zhiqiang Dong</ext-link>, Southeast University, China</p>
</fn>
<fn fn-type="edited-by">
<p>
<bold>Reviewed by:</bold> <ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/1093050/overview">Jun-Jie Zeng</ext-link>, Guangdong University of Technology, China</p>
<p>
<ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/2168169/overview">Daxu Zhang</ext-link>, Shanghai Jiao Tong University, China</p>
</fn>
<corresp id="c001">&#x2a;Correspondence: Taha A. El-Sayed, <email>taha.ibrahim@feng.bu.edu.eg</email>; A. Deifalla, <email>ahmed.deifalla@fue.edu.eg</email>
</corresp>
<fn fn-type="other">
<p>This article was submitted to Structural Materials, a section of the journal Frontiers in Materials</p>
</fn>
</author-notes>
<pub-date pub-type="epub">
<day>20</day>
<month>03</month>
<year>2023</year>
</pub-date>
<pub-date pub-type="collection">
<year>2023</year>
</pub-date>
<volume>10</volume>
<elocation-id>1126806</elocation-id>
<history>
<date date-type="received">
<day>18</day>
<month>12</month>
<year>2022</year>
</date>
<date date-type="accepted">
<day>28</day>
<month>02</month>
<year>2023</year>
</date>
</history>
<permissions>
<copyright-statement>Copyright &#xa9; 2023 El-said, Awad, El-Sayed, &#xd6;zk&#x131;l&#x131;&#xe7;, Deifalla and Tawfik.</copyright-statement>
<copyright-year>2023</copyright-year>
<copyright-holder>El-said, Awad, El-Sayed, &#xd6;zk&#x131;l&#x131;&#xe7;, Deifalla and Tawfik</copyright-holder>
<license xlink:href="http://creativecommons.org/licenses/by/4.0/">
<p>This is an open-access article distributed under the terms of the Creative Commons Attribution License (CC BY). The use, distribution or reproduction in other forums is permitted, provided the original author(s) and the copyright owner(s) are credited and that the original publication in this journal is cited, in accordance with accepted academic practice. No use, distribution or reproduction is permitted which does not comply with these terms.</p>
</license>
</permissions>
<abstract>
<p>Fiber-reinforced polymer (FRP)-reinforced concrete (RC) elements fail under one-way shear in a devastating and complicated manner with no adequate warning. In recent decades, there has been pioneering research in this area; however, there is no agreement among researchers regarding mechanically-based models. Thus, in this current study, a plasticity-based model is developed for FRP-RC elements under shear. A selected model was firstly assessed for its accuracy, consistency, and safety against an extensive experimental database. Secondly, a plasticity-based model (i.e., crack shear sliding model) was adapted, refined, and proposed for FRP-RC elements under one-way shear. The two proposed models were found to be reliable and more accurate with respect to selected existing methods. Modeling of FRP&#x2019;s axial rigidity is more consistent only under Young&#x2019;s modulus with respect to the experimental database. Several concluding remarks on the selected existing models are outlined and discussed to assist the future development of these models and design codes.</p>
</abstract>
<kwd-group>
<kwd>one-way shear</kwd>
<kwd>FRP</kwd>
<kwd>crack sliding model</kwd>
<kwd>plasticity</kwd>
<kwd>slender</kwd>
</kwd-group>
</article-meta>
</front>
<body>
<sec id="s1">
<title>1 Introduction</title>
<p>The dilemma of shear of reinforced concrete (RC) <inline-formula id="inf1">
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<mml:mi mathvariant="normal">n</mml:mi>
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</inline-formula>n old problem. This dilemma lacks robust mechanical models based on physics and is affected by several mechanisms and parameters (<xref ref-type="bibr" rid="B2">Ali et al., 2021</xref>; <xref ref-type="bibr" rid="B28">Ebid and Deifalla, 2021</xref>; <xref ref-type="bibr" rid="B3">Alkhatib and Deifalla, 2022</xref>; <xref ref-type="bibr" rid="B25">Deifalla and Salem, 2022</xref>; <xref ref-type="bibr" rid="B42">Salem and Deifalla, 2022</xref>). Fiber-reinforced polymer (FRP)-RC elements increase the ambiguity further by adding several effects, including and not limited to FRP&#x2019;s linear behavior up to failure and the variability of FRP&#x2019;s Young&#x2019;s modulus (<xref ref-type="bibr" rid="B32">Hassan and Deifalla, 2015</xref>; <xref ref-type="bibr" rid="B29">Elmeligy et al., 2017</xref>; <xref ref-type="bibr" rid="B17">Deifalla, 2020c</xref>; <xref ref-type="bibr" rid="B15">Deifalla, 2021a</xref>; <xref ref-type="bibr" rid="B24">Deifalla, 2022</xref>). Thus, the complexity associated with developing a physically-based mechanical model is considerable and requires further investigation of new representation approaches (<xref ref-type="bibr" rid="B21">Deifalla and Ghobarah, 2010a</xref>; <xref ref-type="bibr" rid="B18">Deifalla et al., 2013</xref>; <xref ref-type="bibr" rid="B22">Deifalla et al., 2014</xref>; <xref ref-type="bibr" rid="B26">Deifalla, 2015</xref>; <xref ref-type="bibr" rid="B23">Deifalla et al., 2015</xref>). This is imperative to attaining a much deeper understanding of failure under shear and, consequently, a base for optimum shear provisions in terms of reduced materials, prolonged life span, and improved reliability (<xref ref-type="bibr" rid="B20">Deifalla and Ghobarah, 2010b</xref>; <xref ref-type="bibr" rid="B19">Deifalla and Ghobarah, 2014</xref>; <xref ref-type="bibr" rid="B16">Deifalla, 2020b</xref>; <xref ref-type="bibr" rid="B13">Deifalla, 2021b</xref>; <xref ref-type="bibr" rid="B14">Deifalla, 2021d</xref>).</p>
<p>Since the 1950s, developing a mechanical model with a physical basis for the shear strength of steel-RC elements has been an ongoing area of investigation, with several models developed. The first were empirically based on simplified ones (<xref ref-type="bibr" rid="B51">Zsutty, 1968</xref>), which included the basic variables of concrete compressive strength, flexure reinforcement ratio, and element depth and width. Those variables were considered significant for shear strength by many researchers (<xref ref-type="bibr" rid="B35">Leonhardt et al., 1964</xref>). Later, the size effect was investigated and considered in those models (<xref ref-type="bibr" rid="B33">Hedman et al., 1978</xref>; <xref ref-type="bibr" rid="B5">Bazant and Kim, 1984</xref>; <xref ref-type="bibr" rid="B31">Ghannoum, 1998</xref>). Thereafter, researchers have considered the following variables: effect of the maximum nominal aggregate size (<xref ref-type="bibr" rid="B8">Bentz, 2005</xref>), fracture energy (<xref ref-type="bibr" rid="B6">Bazant and Planas, 1998</xref>), and element shear slenderness (<xref ref-type="bibr" rid="B51">Zsutty, 1968</xref>). These empirical models have included effective variables based on the results of experimental investigation; however, little attention has been directed to modeling the actual shear mechanism and behavior. Recently, research has aimed at achieving a more profound comprehension of shear behavior (<xref ref-type="bibr" rid="B46">Vecchio and Collins, 1986</xref>; <xref ref-type="bibr" rid="B39">Muttoni and Fern&#xe1;ndez Ruiz, 2008</xref>; <xref ref-type="bibr" rid="B44">Tung and Tue, 2016</xref>). With technological advances in experimental measurements and numerical analysis, a more refined grasp can be gained of the contribution of each shear mechanism. Therefore, several mechanical models have been developed (<xref ref-type="bibr" rid="B34">Huber et al., 2016</xref>; <xref ref-type="bibr" rid="B10">Cavagnis, 2017</xref>; <xref ref-type="bibr" rid="B11">Cladera et al., 2017</xref>). There are a handful of these in the literature for steel-RC elements under one-way shear, including but not limited to a compression chord model (<xref ref-type="bibr" rid="B50">Zink, 1999</xref>; <xref ref-type="bibr" rid="B49">Zararis and Papadakis, 2001</xref>). A compression field assumes that the governing mechanism is the aggregate interlock (<xref ref-type="bibr" rid="B46">Vecchio and Collins, 1986</xref>; <xref ref-type="bibr" rid="B9">Bentz et al., 2006</xref>). The critical shear displacement method (CSDM) (<xref ref-type="bibr" rid="B47">Yang, 2014</xref>; <xref ref-type="bibr" rid="B48">Yang et al., 2017</xref>) assumes that the delamination crack, which is at the level of flexural reinforcements, is the main trigger for shear failure developing, thus signifying the aggregate interlock effect. A fracture mechanics-based model accounts for residual concrete tensile stress after concrete cracking (<xref ref-type="bibr" rid="B5">Bazant and Kim, 1984</xref>; <xref ref-type="bibr" rid="B31">Ghannoum, 1998</xref>). The crack sliding shear model (CSSM) is based on a plasticity solution (i.e., upper and lower bound limit analysis theorem) (<xref ref-type="bibr" rid="B30">Fisker and Hagsten, 2016</xref>). CSSM thus accounts for the effect of concrete cracking and applies the tensile stress criterion to the flexural cracks&#x2019; tips, which connect with a shear crack (<xref ref-type="bibr" rid="B43">Tue et al., 2014</xref>). Critical shear crack theory (CSCT) includes several shear mechanisms: residual tensile stress in the shear crack, aggregate interlock, and dowel action in one united failure criterion (<xref ref-type="bibr" rid="B38">Muttoni and Fern&#xe1;ndez Ruiz, 2019</xref>). The multi-action model (MAM) is based on several shear mechanisms, including but not limited to the compression chord. Reineck&#x27;s model includes all shear mechanisms, especially, the compression zone direct shear mechanism in a kinematically consistent manner (<xref ref-type="bibr" rid="B41">Reineck, 1991</xref>). This model is based on the equilibrium between both internal and the external stresses due to shear acting upon cracked concrete teeth. The most recent model is shear crack propagation theory (SCPT), which predicts crack propagation and stresses in uncracked concrete, different shear mechanisms, and stresses at the tip of the crack over the loading history (<xref ref-type="bibr" rid="B12">Classen, 2020</xref>). However, SCPT is more of a tool for targeting the mechanical bases of one-way shear in steel-RC elements, to be implemented for developing design models.</p>
<p>Previous experimental studies have shown that the shear behavior of concrete elements can be clarified into four categories based on the shear span-to-depth ratio: 1) short elements (i.e., a/d &#x3c; 1); 2) deep elements (i.e., 1&#x3c; a/d &#x3c;2.5); 3) flexure shear dominated elements (i.e., 2.5&#x3c; a/d &#x3c;5.0); 4) flexure dominated elements (i.e., 5.0 &#x3c; a/d). In both short and deep elements, the behavior is dominated by the arch action, while the flexure and shear element is not.</p>
<p>This current study developed a physically based model for FRP-RC slender elements under one-way shear. The work is part of extensive research that aims to investigate the strength of reinforced concrete elements under shear, punching shear, and torsion (<xref ref-type="bibr" rid="B21">Deifalla and Ghobarah, 2010a</xref>; <xref ref-type="bibr" rid="B20">Deifalla and Ghobarah, 2010b</xref>; <xref ref-type="bibr" rid="B18">Deifalla et al., 2013</xref>; <xref ref-type="bibr" rid="B22">Deifalla et al., 2014</xref>; <xref ref-type="bibr" rid="B19">Deifalla and Ghobarah, 2014</xref>; <xref ref-type="bibr" rid="B26">Deifalla, 2015</xref>; <xref ref-type="bibr" rid="B23">Deifalla et al., 2015</xref>; <xref ref-type="bibr" rid="B32">Hassan and Deifalla, 2015</xref>; <xref ref-type="bibr" rid="B29">Elmeligy et al., 2017</xref>; <xref ref-type="bibr" rid="B16">Deifalla, 2020b</xref>; <xref ref-type="bibr" rid="B17">Deifalla, 2020c</xref>; <xref ref-type="bibr" rid="B15">Deifalla, 2021a</xref>; <xref ref-type="bibr" rid="B2">Ali et al., 2021</xref>; <xref ref-type="bibr" rid="B13">Deifalla, 2021b</xref>; <xref ref-type="bibr" rid="B14">Deifalla, 2021d</xref>; <xref ref-type="bibr" rid="B28">Ebid and Deifalla, 2021</xref>; <xref ref-type="bibr" rid="B3">Alkhatib and Deifalla, 2022</xref>; <xref ref-type="bibr" rid="B24">Deifalla, 2022</xref>; <xref ref-type="bibr" rid="B25">Deifalla and Salem, 2022</xref>; <xref ref-type="bibr" rid="B42">Salem and Deifalla, 2022</xref>). Many of these include the shear strength of FRP-reinforced concrete elements (<xref ref-type="bibr" rid="B2">Ali et al., 2021</xref>; <xref ref-type="bibr" rid="B28">Ebid and Deifalla, 2021</xref>). <xref ref-type="bibr" rid="B2">Ali et al. (2021</xref>) assessed the available design codes and provided a regression model. <xref ref-type="bibr" rid="B28">Ebid and Deifalla (2021</xref>) developed a machine learning model. The current study aims to develop a mechanical model based on the concept of plasticity. The CSSM applies to special cases of one-way shear and punching shear and was thus selected for this study. The original CSSM did not address the shear strength of FRP-RC beams and is only applicable to steel-RC beams. Thus, extending it, based on the experimental database, to FRP-RC beams is a significant refinement. A comprehensive literature review for experimental testing of elements under one-way shear was conducted. The CSSM was refined (RCSSM) to model behavior, and a new mechanical model is proposed for FRP-RC slender elements under one-way shear. A few models were selected from the literature to compare to the developed model; however, a comprehensive assessment of existing shear models for FRP-RC slender elements is not within the scope of this study. The RCSSM was used to compute the element&#x2019;s strength and compare it with existing models in the literature. Concluding remarks are outlined and discussed.</p>
</sec>
<sec id="s2">
<title>2 Experimental database</title>
<p>The present study adopts the most comprehensive database for FRP-RC beams available, consisting of 420 specimens tested in 57 studies (<xref ref-type="bibr" rid="B2">Ali et al., 2021</xref>; <xref ref-type="bibr" rid="B28">Ebid and Deifalla, 2021</xref>). Further details of the database are available in previous studies (<xref ref-type="bibr" rid="B2">Ali et al., 2021</xref>; <xref ref-type="bibr" rid="B28">Ebid and Deifalla, 2021</xref>). All these experimental tests utilized FRP as the flexure reinforcement. All elements were four-point static loading, which failed in shear. Shear strengthening and retrofitting using FRP is out of the scope for this study. <xref ref-type="table" rid="T1">Table 1</xref> show the frequency distribution of the mechanical and geometrical parameters of the test specimens while the details of all data are available in the supplementary file at the end of the paper. <xref ref-type="fig" rid="F1">Figure 1</xref> shows the frequency of the values used for the effective depth (d), the compressive strength of concrete (<inline-formula id="inf2">
<mml:math id="m2">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="normal">f</mml:mi>
<mml:mi mathvariant="normal">c</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>&#x2019;), the flexural reinforcement ratio (<inline-formula id="inf3">
<mml:math id="m3">
<mml:mrow>
<mml:mi mathvariant="normal">&#x3c1;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula>), and FRP&#x2019;s Young&#x2019;s modulus (<inline-formula id="inf4">
<mml:math id="m4">
<mml:mrow>
<mml:mi mathvariant="normal">E</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula>). The scope of this study includes slender elements which are either flexure shear-dominated or flexure-dominated elements. Thus, the database was filtered to eliminate short and deep elements&#x2014;defined as those with a shear span-to-depth ratio value of less than 2.5. Hence, a total of 278 specimens were used in this study. The developed models and conclusions in the current study are limited to slender elements and are not necessarily applicable for short and deep elements. Although FRP manufacturing and products have improved significantly over the years, the model depends on FRP&#x27;s mechanical properties, which are evaluated specifically for the FRP implemented in each research study; thus, the model analysis is not dependent on the quality of the FRP.</p>
<table-wrap id="T1" position="float">
<label>TABLE 1</label>
<caption>
<p>Database of parameters for slender FRP-RC elements under shear.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="left">Source</th>
<th align="left">Range</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="left">Database size</td>
<td align="left">420</td>
</tr>
<tr>
<td align="left">Studies in the database</td>
<td align="left">57</td>
</tr>
<tr>
<td align="left">
<inline-formula id="inf5">
<mml:math id="m5">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="normal">f</mml:mi>
<mml:mi mathvariant="normal">c</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> (MPa)</td>
<td align="left">20&#x2013;93</td>
</tr>
<tr>
<td align="left">b (mm)</td>
<td align="left">89&#x2013;1830</td>
</tr>
<tr>
<td align="left">d (mm)</td>
<td align="left">73&#x2013;938</td>
</tr>
<tr>
<td align="left">a (mm)</td>
<td align="left">299.6&#x2013;3096</td>
</tr>
<tr>
<td align="left">a/d</td>
<td align="left">1.08&#x2013;16.2</td>
</tr>
<tr>
<td align="left">
<inline-formula id="inf6">
<mml:math id="m6">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="normal">&#x3c1;</mml:mi>
<mml:mi mathvariant="normal">f</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> (%)</td>
<td align="left">0.09&#x2013;3.98</td>
</tr>
<tr>
<td align="left">
<inline-formula id="inf7">
<mml:math id="m7">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="normal">E</mml:mi>
<mml:mi mathvariant="normal">f</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> (GPa)</td>
<td align="left">29&#x2013;192</td>
</tr>
</tbody>
</table>
</table-wrap>
<fig id="F1" position="float">
<label>FIGURE 1</label>
<caption>
<p>Database frequency distribution.</p>
</caption>
<graphic xlink:href="fmats-10-1126806-g001.tif"/>
</fig>
</sec>
<sec id="s3">
<title>3 Assessment of selected models</title>
<p>Several methods have been developed over the last four&#xa0;decades for FRP-RC beams. The well-known design guide for FRP (ACI) (<xref ref-type="bibr" rid="B1">ACI-440.1R-15, 2015</xref>) is based on Tureyen and Frosh&#x2019;s model (<xref ref-type="bibr" rid="B45">Tureyen et al., 2006</xref>). In addition, a few mechanical models were found in the literature that address the shear of slender FRP-reinforced concrete elements. These are based on the following well-known shear models: 1) the M model (<xref ref-type="bibr" rid="B36">Mari et al., 2014</xref>), which is based on the compression chord model; 2) the DN model (<xref ref-type="bibr" rid="B27">Dhahir and Nadir, 2018</xref>), which is based on the compression field model; 3) the B model (<xref ref-type="bibr" rid="B4">Baghi et al., 2018</xref>), which is based on the modified compression field theory (MCFT) (<xref ref-type="bibr" rid="B7">Bentz et al., 2010</xref>). The details of these models are out of the scope of this study, and any further details about the application and derivation of these models can be found in the original manuscript (<xref ref-type="bibr" rid="B1">ACI-440.1R-15, 2015</xref>; <xref ref-type="bibr" rid="B45">Tureyen et al., 2006</xref>; <xref ref-type="bibr" rid="B36">Mari et al., 2014</xref>; <xref ref-type="bibr" rid="B27">Dhahir and Nadir, 2018</xref>; <xref ref-type="bibr" rid="B4">Baghi et al., 2018</xref>; <xref ref-type="bibr" rid="B7">Bentz et al., 2010</xref>). <xref ref-type="table" rid="T2">Table 2</xref> shows the five methods selected: ACI, M, DN, and B.</p>
<table-wrap id="T2" position="float">
<label>TABLE 2</label>
<caption>
<p>Summary of selected model and design codes.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="left">Method</th>
<th align="left">Shear resistance, <inline-formula id="inf8">
<mml:math id="m8">
<mml:mrow>
<mml:mi mathvariant="normal">V</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula>
</th>
<th align="left">Symbols</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="left">ACI (<xref ref-type="bibr" rid="B1">ACI-440.1R-15, 2015</xref>)</td>
<td align="left">Based on the model by Tureyen and Frosh (<xref ref-type="bibr" rid="B45">Tureyen et al., 2006</xref>), the ACI design code for conventional steel RC was modified such that: <inline-formula id="inf9">
<mml:math id="m9">
<mml:mrow>
<mml:mn>0.4</mml:mn>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msqrt>
<mml:mrow>
<mml:mn>2</mml:mn>
<mml:mi mathvariant="normal">n</mml:mi>
<mml:mi mathvariant="normal">&#x3c1;</mml:mi>
<mml:mo>&#x2b;</mml:mo>
<mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi mathvariant="normal">n</mml:mi>
<mml:mi mathvariant="normal">&#x3c1;</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mn>2</mml:mn>
</mml:msup>
</mml:mrow>
</mml:msqrt>
<mml:mo>&#x2212;</mml:mo>
<mml:mi mathvariant="normal">n</mml:mi>
<mml:mi mathvariant="normal">&#x3c1;</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:msqrt>
<mml:msup>
<mml:msub>
<mml:mi mathvariant="normal">f</mml:mi>
<mml:mi mathvariant="normal">c</mml:mi>
</mml:msub>
<mml:mo>&#x2032;</mml:mo>
</mml:msup>
</mml:msqrt>
<mml:mi mathvariant="normal">b</mml:mi>
<mml:mi mathvariant="normal">d</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="left">
<inline-formula id="inf10">
<mml:math id="m10">
<mml:mrow>
<mml:mi mathvariant="normal">n</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="normal">E</mml:mi>
<mml:mi mathvariant="normal">f</mml:mi>
</mml:msub>
</mml:mrow>
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="normal">E</mml:mi>
<mml:mi mathvariant="normal">c</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
</tr>
<tr>
<td align="left">M model (<xref ref-type="bibr" rid="B36">Mari et al., 2014</xref>)</td>
<td align="left">Based on the compression chord model, the model was developed such that: <inline-formula id="inf11">
<mml:math id="m11">
<mml:mrow>
<mml:msub>
<mml:mrow>
<mml:mi mathvariant="normal">&#x3be;</mml:mi>
<mml:mrow>
<mml:mfenced open="[" close="]" separators="|">
<mml:mrow>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>1.072</mml:mn>
<mml:mo>&#x2212;</mml:mo>
<mml:mn>0.01</mml:mn>
<mml:mi mathvariant="normal">n</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mi mathvariant="normal">c</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi mathvariant="normal">d</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>0.036</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mi mathvariant="normal">f</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi mathvariant="normal">c</mml:mi>
<mml:mi mathvariant="normal">t</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mi mathvariant="normal">b</mml:mi>
<mml:mi mathvariant="normal">d</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="left">
<inline-formula id="inf12">
<mml:math id="m12">
<mml:mrow>
<mml:mi mathvariant="normal">&#x3be;</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1.2</mml:mn>
<mml:mo>&#x2212;</mml:mo>
<mml:mn>0.2</mml:mn>
<mml:mfrac>
<mml:mrow>
<mml:mi mathvariant="normal">a</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi mathvariant="normal">d</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mi mathvariant="normal">d</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> <inline-formula id="inf13">
<mml:math id="m13">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mi mathvariant="normal">c</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi mathvariant="normal">d</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mo>&#x3d;</mml:mo>
<mml:mi mathvariant="normal">n</mml:mi>
<mml:mi mathvariant="normal">&#x3c1;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mn>1</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:msqrt>
<mml:mrow>
<mml:mn>1</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mfrac>
<mml:mn>2</mml:mn>
<mml:mrow>
<mml:mi mathvariant="normal">n</mml:mi>
<mml:mi mathvariant="normal">&#x3c1;</mml:mi>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:msqrt>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
</tr>
<tr>
<td align="left">DN model (<xref ref-type="bibr" rid="B27">Dhahir and Nadir, 2018</xref>)</td>
<td align="left">Based on the compression field, the model was developed such that: <inline-formula id="inf14">
<mml:math id="m14">
<mml:mrow>
<mml:mi mathvariant="normal">A</mml:mi>
<mml:mi mathvariant="normal">E</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mn>2.58</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:msqrt>
<mml:mrow>
<mml:mn>7.18</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mn>10506</mml:mn>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>0.15</mml:mn>
<mml:msub>
<mml:mi mathvariant="normal">l</mml:mi>
<mml:mi mathvariant="normal">b</mml:mi>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>0.72</mml:mn>
<mml:mi mathvariant="normal">c</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mi mathvariant="normal">b</mml:mi>
<mml:msubsup>
<mml:mi mathvariant="normal">f</mml:mi>
<mml:mi mathvariant="normal">c</mml:mi>
<mml:mo>&#x2032;</mml:mo>
</mml:msubsup>
</mml:mrow>
<mml:mrow>
<mml:mi mathvariant="normal">A</mml:mi>
<mml:mi mathvariant="normal">E</mml:mi>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:msqrt>
</mml:mrow>
<mml:mn>5253</mml:mn>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="left">
<inline-formula id="inf15">
<mml:math id="m15">
<mml:mrow>
<mml:mi mathvariant="normal">V</mml:mi>
<mml:mo>&#x2265;</mml:mo>
<mml:mn>0.14</mml:mn>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>0.15</mml:mn>
<mml:msub>
<mml:mi mathvariant="normal">l</mml:mi>
<mml:mi mathvariant="normal">b</mml:mi>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>0.72</mml:mn>
<mml:mi mathvariant="normal">c</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mi mathvariant="normal">b</mml:mi>
<mml:msubsup>
<mml:mi mathvariant="normal">f</mml:mi>
<mml:mi mathvariant="normal">c</mml:mi>
<mml:mo>&#x2032;</mml:mo>
</mml:msubsup>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
</tr>
<tr>
<td align="left">B model (<xref ref-type="bibr" rid="B4">Baghi et al., 2018</xref>)</td>
<td align="left">Based on the MCFT (<xref ref-type="bibr" rid="B7">Bentz et al., 2010</xref>), the model was developed such that: <inline-formula id="inf16">
<mml:math id="m16">
<mml:mrow>
<mml:mn>0.07</mml:mn>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mi mathvariant="normal">E</mml:mi>
<mml:mi mathvariant="normal">&#x3c1;</mml:mi>
<mml:mi mathvariant="normal">b</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:msubsup>
<mml:mi mathvariant="normal">f</mml:mi>
<mml:mi mathvariant="normal">c</mml:mi>
<mml:mo>&#x2032;</mml:mo>
</mml:msubsup>
<mml:mi mathvariant="normal">d</mml:mi>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mtext>&#x2009;</mml:mtext>
<mml:msqrt>
<mml:msubsup>
<mml:mi mathvariant="normal">f</mml:mi>
<mml:mi mathvariant="normal">c</mml:mi>
<mml:mo>&#x2032;</mml:mo>
</mml:msubsup>
</mml:msqrt>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mi mathvariant="normal">b</mml:mi>
<mml:mi mathvariant="normal">d</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="left">
<inline-formula id="inf17">
<mml:math id="m17">
<mml:mrow>
<mml:mn>0.05</mml:mn>
<mml:msqrt>
<mml:msubsup>
<mml:mi mathvariant="normal">f</mml:mi>
<mml:mi mathvariant="normal">c</mml:mi>
<mml:mo>&#x2032;</mml:mo>
</mml:msubsup>
</mml:msqrt>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mi mathvariant="normal">b</mml:mi>
<mml:mi mathvariant="normal">d</mml:mi>
<mml:mo>&#x2264;</mml:mo>
<mml:mi mathvariant="normal">V</mml:mi>
<mml:mo>&#x2264;</mml:mo>
<mml:mn>0.3</mml:mn>
<mml:msqrt>
<mml:msubsup>
<mml:mi mathvariant="normal">f</mml:mi>
<mml:mi mathvariant="normal">c</mml:mi>
<mml:mo>&#x2032;</mml:mo>
</mml:msubsup>
</mml:msqrt>
<mml:mi mathvariant="normal">b</mml:mi>
<mml:mi mathvariant="normal">d</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
</tr>
</tbody>
</table>
</table-wrap>
<sec id="s3-1">
<title>3.1 Overall</title>
<p>
<xref ref-type="fig" rid="F2">Figure 2</xref> shows measurements against calculated strength using the ACI, M, DN, and B methods, and the ideal 45-degree line as well as the best-fit-line and the <inline-formula id="inf18">
<mml:math id="m18">
<mml:mrow>
<mml:mi>&#x3c7;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> factor, which is calculated as the inverse of the best-fit-line slope. <inline-formula id="inf19">
<mml:math id="m19">
<mml:mrow>
<mml:mi>&#x3c7;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is an indication of the over- or underestimation of the used method. <xref ref-type="table" rid="T3">Table 3</xref> shows the statistical measures for the SR (i.e., the measured divided by the calculated strength) using different methods as well as the coefficient of correlation between the calculated and measured strengths. The SR statistical measures include the minimum, maximum, average, coefficient of variation, and median. ACI is overly conservative, with a SR average value of 2.02 and a <inline-formula id="inf20">
<mml:math id="m20">
<mml:mrow>
<mml:mi>&#x3c7;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> factor value of 1.87. The B model is the least conservative, with a SR average value of 0.46 and a <inline-formula id="inf21">
<mml:math id="m21">
<mml:mrow>
<mml:mi>&#x3c7;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> factor value of 0.43. For the other models, the SR average value ranged 0.61&#x2013;0.92 and the <inline-formula id="inf22">
<mml:math id="m22">
<mml:mrow>
<mml:mi>&#x3c7;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> factor ranged 0.50&#x2013;1.50. For consistency, the coefficient of variation ranged 42%&#x2013;53%, showing a serious lack of consistency. For safety, the lower 95% is calculated for the ACI; M is above 0.85, which is considered reasonable. However, that calculated for the B and DN models is lower than 0.85, which is needed for the higher safety factor for the purpose of design. The coefficient of correlation between measured strength and that calculated using various methods had values of 0.90, 0.86, 0.66, and 0.88 for the ACI, M, DN, and B methods, respectively, Thus, the strength calculated using various models is highly correlated to experimental measurements; however, the ACI, M, and B models are strongly correlated compared to DN.</p>
<fig id="F2" position="float">
<label>FIGURE 2</label>
<caption>
<p>Calculated versus measured strength for existing selected models.</p>
</caption>
<graphic xlink:href="fmats-10-1126806-g002.tif"/>
</fig>
<table-wrap id="T3" position="float">
<label>TABLE 3</label>
<caption>
<p>Statistical measures for SR.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="left"/>
<th align="left">ACI</th>
<th align="left">M</th>
<th align="left">DN</th>
<th align="left">B</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="left">Mean</td>
<td align="right">2.02</td>
<td align="right">0.93</td>
<td align="right">0.72</td>
<td align="right">0.46</td>
</tr>
<tr>
<td align="left">C.O.V.</td>
<td align="right">41%</td>
<td align="right">41%</td>
<td align="right">51%</td>
<td align="right">43%</td>
</tr>
<tr>
<td align="left">L.L. 99%</td>
<td align="right">1.92</td>
<td align="right">0.88</td>
<td align="right">0.68</td>
<td align="right">0.44</td>
</tr>
<tr>
<td align="left">Minimum</td>
<td align="right">0.66</td>
<td align="right">0.31</td>
<td align="right">0.09</td>
<td align="right">0.13</td>
</tr>
<tr>
<td align="left">Maximum</td>
<td align="right">7.75</td>
<td align="right">3.04</td>
<td align="right">2.68</td>
<td align="right">1.68</td>
</tr>
<tr>
<td align="left">Median</td>
<td align="right">1.82</td>
<td align="right">0.83</td>
<td align="right">0.68</td>
<td align="right">0.41</td>
</tr>
<tr>
<td align="left">Correlation coefficient</td>
<td align="right">0.90</td>
<td align="right">0.86</td>
<td align="right">0.66</td>
<td align="right">0.88</td>
</tr>
</tbody>
</table>
</table-wrap>
</sec>
<sec id="s3-2">
<title>3.2 Against size</title>
<p>
<xref ref-type="table" rid="T4">Table 4</xref> shows the coefficient of correlation between measured and calculated strengths for selected methods against element size. The correlation coefficient between size and calculated SR for ACI, M, DN, and B was 0.04, 0.28, 0.82, and 0.02, respectively. Thus, the calculated SR for all models, excepting DN, is weakly correlated to size compared to the DN model. In addition, <xref ref-type="fig" rid="F3">Figure 3</xref> shows the calculated SR for the ACI, M, DN, and B models against size and best-fit-line for each model. The best-fit-line slope for the calculated SR for the ACI, M, DN, and B models against size are 2.0E-4, 6.0E-4, 18E-4, and 0.3E-4, respectively. In all models, safety increases with increased concrete compressive strength. DN is less consistent with size than other models and needs further investigation into its size effect.</p>
<table-wrap id="T4" position="float">
<label>TABLE 4</label>
<caption>
<p>Correlation coefficient between various methods and variables.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="left"/>
<th align="left">ACI</th>
<th align="left">M</th>
<th align="left">DN</th>
<th align="left">B</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="left">Size</td>
<td align="right">0.04</td>
<td align="right">0.28</td>
<td align="right">0.82</td>
<td align="right">0.02</td>
</tr>
<tr>
<td align="left">Concrete compressive strength</td>
<td align="right">&#x2212;0.09</td>
<td align="right">&#x2212;0.12</td>
<td align="right">&#x2212;0.35</td>
<td align="right">&#x2212;0.12</td>
</tr>
<tr>
<td align="left">Flexure reinforcement axial rigidity</td>
<td align="right">&#x2212;0.40</td>
<td align="right">&#x2212;0.44</td>
<td align="right">&#x2212;0.01</td>
<td align="right">0.18</td>
</tr>
</tbody>
</table>
</table-wrap>
<fig id="F3" position="float">
<label>FIGURE 3</label>
<caption>
<p>SR calculated using selected model versus size.</p>
</caption>
<graphic xlink:href="fmats-10-1126806-g003.tif"/>
</fig>
</sec>
<sec id="s3-3">
<title>3.3 Against concrete compressive strength</title>
<p>From <xref ref-type="table" rid="T4">Table 4</xref>, the correlation coefficient between concrete compressive strength and calculated SR for ACI, M, DN, and B was &#x2212;0.09, &#x2212;0.12, &#x2212;0.35, and &#x2212;0.12, respectively. Thus, the calculated SR for all models except DN is weakly correlated with concrete compressive strength. In addition, <xref ref-type="fig" rid="F4">Figure 4</xref> shows the calculated SR for the ACI, M, DN, and B models against concrete compressive strength as well as the best-fit-line for each model. The best-fit-line slope for the calculated SR for the ACI, M, DN, and B models against concrete compressive strength is -47E-4, -28E-4, -81E-4, and -15E-4, respectively. For all models, safety decreases with increased concrete compressive strength. DN is less consistent with concrete compressive strength than other models, and needs further investigation into its concrete compressive strength.</p>
<fig id="F4" position="float">
<label>FIGURE 4</label>
<caption>
<p>SR calculated using selected model versus concrete compressive strength.</p>
</caption>
<graphic xlink:href="fmats-10-1126806-g004.tif"/>
</fig>
</sec>
<sec id="s3-4">
<title>3.4 Against flexure reinforcement axial rigidity</title>
<p>From <xref ref-type="table" rid="T4">Table 4</xref>, the correlation coefficient between flexure reinforcement axial rigidity and calculated SR for ACI, M, DN, and B was &#x2212;0.40, &#x2212;0.44, &#x2212;0.01, and 0.18, respectively. Thus, the calculated SR for the DN and B methods is weakly correlated compared to the ACI and M models; they thus need further investigation into flexure reinforcement axial rigidity. In addition, <xref ref-type="fig" rid="F5">Figure 5</xref> shows the calculated SR for the ACI, M, DN, and B models against flexure reinforcement axial rigidity as well as the best-fit-line for each model. The best-fit-line slope for the calculated SR for the ACI, M, DN, and B models against flexure reinforcement axial rigidity is &#x2212;0.69, &#x2212;0.35, &#x2212;0.006, and 0.07, respectively. For all models except B, safety decreases with increased flexure reinforcement axial rigidity. This could be because existing models underestimate the dowel action component of lower values for flexure reinforcement axial rigidity. The ACI is less consistent with flexure reinforcement axial rigidity than other models and needs further investigation into its flexure reinforcement axial rigidity.</p>
<fig id="F5" position="float">
<label>FIGURE 5</label>
<caption>
<p>SR calculated using selected model versus flexure reinforcement axial rigidity.</p>
</caption>
<graphic xlink:href="fmats-10-1126806-g005.tif"/>
</fig>
</sec>
</sec>
<sec id="s4">
<title>4 Refinement of CSSM (RCSSM)</title>
<p>In this study, the CSSM was selected as it is based on plasticity and can be used for both shear and punching shear.</p>
<sec id="s4-1">
<title>4.1 Background of the crack shear sliding model (CSSM)</title>
<p>This section will briefly outline the original CSSM for one-way shear of concrete elements without stirrups. The CSSM is based on plasticity, where lower and upper boundary solutions for beams under shear are developed. Consider a four-point loading on rectangular beams without stirrups.</p>
<sec id="s4-1-1">
<title>4.1.1 Upper bound plasticity solution</title>
<p>An upper bound solution assumes that the beam is divided into two regions with a straight yield-line having an inclination angle &#x3b2; with the beam longitudinal axis, as shown in <xref ref-type="fig" rid="F6">Figure 6</xref> (<xref ref-type="bibr" rid="B40">Nielsen and Br&#xe6;strup, 1975</xref>). The middle region (I) is assumed to move vertically using a simple displacement field, while the outer region (II) is assumed to not move. Thus, the work equation is such that:<disp-formula id="e1">
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</mml:mrow>
</mml:mfrac>
<mml:mi mathvariant="normal">u</mml:mi>
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</mml:math>
<label>(1)</label>
</disp-formula>
</p>
<fig id="F6" position="float">
<label>FIGURE 6</label>
<caption>
<p>Upper bound solution of four-point loading beam.</p>
</caption>
<graphic xlink:href="fmats-10-1126806-g006.tif"/>
</fig>
<p>which represents the energy dissipation in the concrete, while the longitudinal reinforcements have negligible energy dissipation:<disp-formula id="e2">
<mml:math id="m24">
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<label>(2)</label>
</disp-formula>
</p>
<p>Finding the minimum <inline-formula id="inf23">
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<mml:math id="m27">
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<mml:mo>&#x3d;</mml:mo>
<mml:mn>0</mml:mn>
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</inline-formula>. However, <inline-formula id="inf26">
<mml:math id="m28">
<mml:mrow>
<mml:mi mathvariant="normal">&#x3b2;</mml:mi>
<mml:mo>&#x2265;</mml:mo>
<mml:msup>
<mml:mi>tan</mml:mi>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mn>1</mml:mn>
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</mml:msup>
<mml:mfrac>
<mml:mrow>
<mml:mi mathvariant="normal">h</mml:mi>
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<mml:mrow>
<mml:mi mathvariant="normal">a</mml:mi>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:math>
</inline-formula>; thus the upper bound solution for the shear strength is such that:<disp-formula id="e3">
<mml:math id="m29">
<mml:mrow>
<mml:mi mathvariant="normal">V</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mn>1</mml:mn>
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<mml:mn>2</mml:mn>
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<mml:mi mathvariant="normal">c</mml:mi>
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</mml:mrow>
<mml:mn>2</mml:mn>
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</mml:msqrt>
<mml:mo>&#x2212;</mml:mo>
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<mml:mrow>
<mml:mi mathvariant="normal">a</mml:mi>
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<mml:mrow>
<mml:mi mathvariant="normal">h</mml:mi>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mi mathvariant="normal">b</mml:mi>
<mml:mi mathvariant="normal">h</mml:mi>
</mml:mrow>
</mml:math>
<label>(3)</label>
</disp-formula>
</p>
</sec>
<sec id="s4-1-2">
<title>4.1.2 Lower bound plasticity solution</title>
<p>For the case of a four-point bending concrete beam, <xref ref-type="fig" rid="F7">Figure 7</xref> shows a schematic that can be used to develop a lower bound solution. Shear is transferred <italic>via</italic> a single strut in what is called an &#x201c;arch mechanism&#x201d;, where axial compression acts on region ABDE. The forces from the reinforcement to the arch are transferred through regions AEF and BCD; consequently, both regions are subjected to biaxial stresses. An anchor plate is used to transfer the anchoring force to the concrete, while the stress is taken as f<sub>c</sub>. Thus, the measure of the angle subtended by BDE is &#x3c0;/2, while the maximum shear resistance corresponds to the maximum BC, which is obtained at maximum CD. Since a circle having BE as diameter is the locus of point D, the maximum CD &#x3d; h/2, where BC is such that:<disp-formula id="e4">
<mml:math id="m30">
<mml:mrow>
<mml:mi mathvariant="normal">B</mml:mi>
<mml:mi mathvariant="normal">C</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mi mathvariant="normal">x</mml:mi>
<mml:mi mathvariant="normal">o</mml:mi>
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<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mn>1</mml:mn>
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<mml:mrow>
<mml:mn>2</mml:mn>
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<mml:mrow>
<mml:mfenced open="[" close="]" separators="|">
<mml:mrow>
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<mml:mn>2</mml:mn>
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<mml:msup>
<mml:mi mathvariant="normal">h</mml:mi>
<mml:mn>2</mml:mn>
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<mml:mi mathvariant="normal">a</mml:mi>
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</mml:math>
<label>(4)</label>
</disp-formula>
</p>
<fig id="F7" position="float">
<label>FIGURE 7</label>
<caption>
<p>Lower bound solution for beam without stirrups.</p>
</caption>
<graphic xlink:href="fmats-10-1126806-g007.tif"/>
</fig>
<p>while the maximum shear capacity is such that:<disp-formula id="e5">
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<mml:mi mathvariant="normal">c</mml:mi>
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</mml:mrow>
</mml:math>
<label>(5)</label>
</disp-formula>which can be written in a form like the upper bound solution such that:<disp-formula id="e6">
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<mml:mn>2</mml:mn>
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<mml:mrow>
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<mml:mrow>
<mml:mi mathvariant="normal">h</mml:mi>
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</mml:mfrac>
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</mml:mfenced>
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<mml:mi mathvariant="normal">b</mml:mi>
<mml:mi mathvariant="normal">h</mml:mi>
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</mml:math>
<label>(6)</label>
</disp-formula>which is identical to an upper bound solution. This is, therefore, a unique plastic solution for shear resistance.</p>
</sec>
<sec id="s4-1-3">
<title>4.1.3 Crack sliding model</title>
<p>
<xref ref-type="fig" rid="F8">Figure 8</xref> shows a cracking pattern, starting vertically at the maximum moment cross-section and is then followed by diagonal cracks due to shear. The first crack is usually vertical and close to the point load, starting at the beam bottom soffit; the next one is a diagonal crack directed towards the point load. The load required to initiate diagonal cracks increases with closeness to the support: the cracking load curve. On the other hand, the load resistance for crack sliding decreases with closeness to the support: the shear capacity curve. Therefore, the decrease in the shear span value decreases the angle of inclination of the yield-line and increases the load resistance. The yield-line is defined as the intersection of both the shear capacity and the cracking load. This method predicts much lower shear capacity with respect to the original plastic solution. The yield-line is named the &#x201c;critical diagonal crack&#x201d;, where the shear capacity is less than the cracking load. The CSCT is based on the observation that yield lines are formed as a transformation from the critical diagonal crack (<xref ref-type="bibr" rid="B37">Muttoni, 1990</xref>). This observation was confirmed by measuring the relative displacement along the critical diagonal crack. Initially, the relative displacement along the critical diagonal crack is perpendicular to the crack, while another component of the displacement is formed parallel to the critical diagonal crack. This indicates that the yield line is a transformation of the critical diagonal crack. The cracking moment and the shear capacity of a diagonal crack can be simplified by using an equivalent plastic distribution for the normal stress; the bending moment resistance of concrete element can be calculated as shown in <xref ref-type="fig" rid="F11">Figure 11</xref>. Thus, the cracking moment for concrete is such that:<disp-formula id="e7">
<mml:math id="m33">
<mml:mrow>
<mml:msub>
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<mml:mrow>
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<mml:mrow>
<mml:mn>2</mml:mn>
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<mml:mi mathvariant="normal">b</mml:mi>
<mml:msup>
<mml:mi mathvariant="normal">h</mml:mi>
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<mml:msub>
<mml:mi mathvariant="normal">f</mml:mi>
<mml:mrow>
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<mml:mi mathvariant="normal">e</mml:mi>
<mml:mi mathvariant="normal">f</mml:mi>
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</mml:math>
<label>(7)</label>
</disp-formula>where <inline-formula id="inf27">
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<mml:mi mathvariant="normal">f</mml:mi>
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</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the effective tensile strength calculated as <inline-formula id="inf28">
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</inline-formula>, where <inline-formula id="inf29">
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<mml:mrow>
<mml:mn>0.26</mml:mn>
<mml:msubsup>
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</inline-formula> is taken the constant value of 0.6, and <inline-formula id="inf32">
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<mml:mrow>
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</inline-formula> is the width. In addition, the size effect can be considered using a Weibull factor s(h) on <inline-formula id="inf33">
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<mml:msub>
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<mml:mi mathvariant="normal">f</mml:mi>
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</inline-formula>, such that:<disp-formula id="e8">
<mml:math id="m41">
<mml:mrow>
<mml:mi>s</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>h</mml:mi>
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<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mi>h</mml:mi>
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<mml:mrow>
<mml:mn>100</mml:mn>
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</mml:mfenced>
</mml:mrow>
<mml:mrow>
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<label>(8)</label>
</disp-formula>
</p>
<fig id="F8" position="float">
<label>FIGURE 8</label>
<caption>
<p>Cracking of beams without stirrups.</p>
</caption>
<graphic xlink:href="fmats-10-1126806-g008.tif"/>
</fig>
<p>where the depth is in mm. Thus, the concrete tensile stress is such that:<disp-formula id="e9">
<mml:math id="m42">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="normal">f</mml:mi>
<mml:mrow>
<mml:mi mathvariant="normal">t</mml:mi>
<mml:mi mathvariant="normal">e</mml:mi>
<mml:mi mathvariant="normal">f</mml:mi>
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</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.6</mml:mn>
<mml:msub>
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<mml:mi mathvariant="normal">t</mml:mi>
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<mml:mtext>&#x2009;</mml:mtext>
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</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(9)</label>
</disp-formula>
</p>
<p>For a concrete element with inclined cracks shown in <xref ref-type="fig" rid="F9">Figure 9</xref>, assuming a straight-line from point A to point B, a statically equivalent uniform tensile stress (<inline-formula id="inf34">
<mml:math id="m43">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="normal">f</mml:mi>
<mml:mrow>
<mml:mi mathvariant="normal">t</mml:mi>
<mml:mi mathvariant="normal">e</mml:mi>
<mml:mi mathvariant="normal">f</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>) equivalent to the uniform tensile stresses along the curve from point A to point B. Thus, taking the moment equilibrium at point A, the cracking load is calculated such that:<disp-formula id="e10">
<mml:math id="m44">
<mml:mrow>
<mml:msub>
<mml:mi>M</mml:mi>
<mml:mrow>
<mml:mi mathvariant="normal">c</mml:mi>
<mml:mi mathvariant="normal">r</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mn>1</mml:mn>
</mml:mrow>
<mml:mrow>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:mfrac>
<mml:mi mathvariant="normal">b</mml:mi>
<mml:msup>
<mml:mi>h</mml:mi>
<mml:mn>2</mml:mn>
</mml:msup>
<mml:mrow>
<mml:mfenced open="[" close="]" separators="|">
<mml:mrow>
<mml:mn>1</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mi>x</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>h</mml:mi>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mn>2</mml:mn>
</mml:msup>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:msub>
<mml:mi mathvariant="normal">f</mml:mi>
<mml:mrow>
<mml:mi mathvariant="normal">t</mml:mi>
<mml:mi mathvariant="normal">e</mml:mi>
<mml:mi mathvariant="normal">f</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
<label>(10)</label>
</disp-formula>where x is the critical diagonal crack horizontal component.</p>
<fig id="F9" position="float">
<label>FIGURE 9</label>
<caption>
<p>Stress distribution across diagonal crack.</p>
</caption>
<graphic xlink:href="fmats-10-1126806-g009.tif"/>
</fig>
<p>Shear resistance is reached due to the failure along the two diagonal yield-lines and the upper face of the reinforcements in tension, which can be calculated if the yield-line could be simplified into a straight line, as shown in <xref ref-type="fig" rid="F10">Figure 10</xref>. In addition, an over-RC element can be assumed; thus, the relative horizontal displacement along the yield-lines and the tensile failure at the reinforcement are negligible.</p>
<fig id="F10" position="float">
<label>FIGURE 10</label>
<caption>
<p>Shear failure of a concrete beam with four-point bending loading.</p>
</caption>
<graphic xlink:href="fmats-10-1126806-g010.tif"/>
</fig>
<p>Hence, replacing a with x &#x3d; a &#x2212; x&#x2032; in the upper bound plasticity solution, shear resistance (V) may be calculated such that:<disp-formula id="e11">
<mml:math id="m45">
<mml:mrow>
<mml:mi mathvariant="normal">V</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi mathvariant="normal">x</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mn>1</mml:mn>
</mml:mrow>
<mml:mrow>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:mfrac>
<mml:msub>
<mml:mi mathvariant="normal">f</mml:mi>
<mml:mi>c</mml:mi>
</mml:msub>
<mml:mrow>
<mml:mfenced open="[" close="]" separators="|">
<mml:mrow>
<mml:msqrt>
<mml:mrow>
<mml:mn>1</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mi>x</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>h</mml:mi>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mn>2</mml:mn>
</mml:msup>
</mml:mrow>
</mml:msqrt>
<mml:mo>&#x2212;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mi>x</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>h</mml:mi>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mi mathvariant="normal">b</mml:mi>
<mml:mi mathvariant="normal">h</mml:mi>
</mml:mrow>
</mml:math>
<label>(11)</label>
</disp-formula>
</p>
<p>The cracking load (<inline-formula id="inf35">
<mml:math id="m46">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="normal">V</mml:mi>
<mml:mrow>
<mml:mi>c</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>) is calculated from <inline-formula id="inf36">
<mml:math id="m47">
<mml:mrow>
<mml:msub>
<mml:mi>M</mml:mi>
<mml:mrow>
<mml:mi mathvariant="normal">c</mml:mi>
<mml:mi mathvariant="normal">r</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> while neglecting the contribution of the longitudinal flexure reinforcement, such that:<disp-formula id="e12">
<mml:math id="m48">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="normal">V</mml:mi>
<mml:mrow>
<mml:mi>c</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi mathvariant="normal">x</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mn>1</mml:mn>
</mml:mrow>
<mml:mrow>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:mfrac>
<mml:mfrac>
<mml:mrow>
<mml:mi mathvariant="normal">b</mml:mi>
<mml:mrow>
<mml:mfenced open="[" close="]" separators="|">
<mml:mrow>
<mml:msup>
<mml:mi>h</mml:mi>
<mml:mn>2</mml:mn>
</mml:msup>
<mml:mo>&#x2b;</mml:mo>
<mml:msup>
<mml:mi>x</mml:mi>
<mml:mn>2</mml:mn>
</mml:msup>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:msub>
<mml:mi mathvariant="normal">f</mml:mi>
<mml:mrow>
<mml:mi mathvariant="normal">t</mml:mi>
<mml:mi mathvariant="normal">e</mml:mi>
<mml:mi mathvariant="normal">f</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>a</mml:mi>
<mml:mo>&#x2b;</mml:mo>
<mml:mfrac bevelled="true">
<mml:mrow>
<mml:msub>
<mml:mi>L</mml:mi>
<mml:mi>o</mml:mi>
</mml:msub>
</mml:mrow>
<mml:mrow>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:math>
<label>(12)</label>
</disp-formula>
</p>
<p>where <inline-formula id="inf37">
<mml:math id="m49">
<mml:mrow>
<mml:msub>
<mml:mi>L</mml:mi>
<mml:mi>o</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is the support length. Therefore, the critical shear crack location and the minimum shear strength can be calculated by equating both the <inline-formula id="inf38">
<mml:math id="m50">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="normal">V</mml:mi>
<mml:mrow>
<mml:mi>c</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> and the <inline-formula id="inf39">
<mml:math id="m51">
<mml:mrow>
<mml:mi mathvariant="normal">V</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula>. The calculations are numerically long; thus, for the purpose of design, ignoring the support plate width (<inline-formula id="inf40">
<mml:math id="m52">
<mml:mrow>
<mml:msub>
<mml:mi>L</mml:mi>
<mml:mi>o</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>) [75], the following equation can be used to find the critical crack position, such that:<disp-formula id="e13">
<mml:math id="m53">
<mml:mrow>
<mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mi>x</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>h</mml:mi>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mn>3</mml:mn>
</mml:msup>
<mml:mo>&#x2b;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mi>x</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>h</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mo>&#x2212;</mml:mo>
<mml:mn>4</mml:mn>
<mml:mfrac>
<mml:mrow>
<mml:msub>
<mml:mi>&#x3c4;</mml:mi>
<mml:mi>c</mml:mi>
</mml:msub>
</mml:mrow>
<mml:mrow>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mrow>
<mml:mi>t</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>f</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:mfrac>
<mml:mfrac>
<mml:mrow>
<mml:mi>a</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>h</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0</mml:mn>
</mml:mrow>
</mml:math>
<label>(13)</label>
</disp-formula>
</p>
<p>In addition, the calculated shear strength is compared with the measured ones; thus, a softening factor <inline-formula id="inf41">
<mml:math id="m54">
<mml:mrow>
<mml:mi>&#x3c5;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is proposed such that:<disp-formula id="e14">
<mml:math id="m55">
<mml:mrow>
<mml:mi>&#x3c5;</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mi>&#x3c5;</mml:mi>
<mml:mi>s</mml:mi>
</mml:msub>
<mml:msub>
<mml:mi>&#x3c5;</mml:mi>
<mml:mi>o</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
<label>(14)</label>
</disp-formula>
<disp-formula id="e15">
<mml:math id="m56">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3c5;</mml:mi>
<mml:mi>s</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.5</mml:mn>
</mml:mrow>
</mml:math>
<label>(15)</label>
</disp-formula>
<disp-formula id="e16">
<mml:math id="m57">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3c5;</mml:mi>
<mml:mi>o</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mn>0.88</mml:mn>
</mml:mrow>
<mml:mrow>
<mml:msqrt>
<mml:msup>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mi>c</mml:mi>
</mml:msub>
<mml:mo>&#x2032;</mml:mo>
</mml:msup>
</mml:msqrt>
</mml:mrow>
</mml:mfrac>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>1</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:msqrt>
<mml:mfrac>
<mml:mrow>
<mml:mn>1000</mml:mn>
</mml:mrow>
<mml:mrow>
<mml:mi>h</mml:mi>
</mml:mrow>
</mml:mfrac>
</mml:msqrt>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>1</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>0.26</mml:mn>
<mml:mi>&#x3c1;</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(16)</label>
</disp-formula>where <inline-formula id="inf42">
<mml:math id="m58">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3c5;</mml:mi>
<mml:mi>s</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is a reduction factor for the sliding, and <inline-formula id="inf43">
<mml:math id="m59">
<mml:mrow>
<mml:msup>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mi>c</mml:mi>
</mml:msub>
<mml:mo>&#x2032;</mml:mo>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula> is the concrete compressive strength in MPa, h in meters, and <inline-formula id="inf44">
<mml:math id="m60">
<mml:mrow>
<mml:mi>&#x3c1;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is the flexure reinforcement ratio in percentage. The shear resistance can be simplified such that:<disp-formula id="e17">
<mml:math id="m61">
<mml:mrow>
<mml:mi>V</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>x</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mi>&#x3c4;</mml:mi>
<mml:mi>c</mml:mi>
</mml:msub>
<mml:mfrac>
<mml:mn>2</mml:mn>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac bevelled="true">
<mml:mrow>
<mml:mi>x</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>h</mml:mi>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mfrac>
<mml:mi>b</mml:mi>
<mml:mi>h</mml:mi>
</mml:mrow>
</mml:math>
<label>(17)</label>
</disp-formula>where<disp-formula id="e18">
<mml:math id="m62">
<mml:mrow>
<mml:msub>
<mml:mi mathvariant="normal">&#x3c4;</mml:mi>
<mml:mi>c</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mn>1</mml:mn>
</mml:mrow>
<mml:mrow>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:mfrac>
<mml:mrow>
<mml:mfenced open="[" close="]" separators="|">
<mml:mrow>
<mml:msqrt>
<mml:mn>5</mml:mn>
</mml:msqrt>
<mml:mo>&#x2212;</mml:mo>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:msub>
<mml:mi>&#x3bd;</mml:mi>
<mml:mi>s</mml:mi>
</mml:msub>
<mml:msub>
<mml:mi>&#x3bd;</mml:mi>
<mml:mi>o</mml:mi>
</mml:msub>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mi>c</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
<label>(18)</label>
</disp-formula>
</p>
</sec>
</sec>
<sec id="s4-2">
<title>4.2 Model refinement</title>
<p>Based on the observed FRP-RC elements&#x2019; behavior, the FRP-RC beams&#x2019; different from the steel RC elements is the variable Young&#x2019;s modulus for FRP, or it is different in the axial rigidity of FRP reinforcements (<xref ref-type="bibr" rid="B32">Hassan and Deifalla, 2015</xref>; <xref ref-type="bibr" rid="B2">Ali et al., 2021</xref>; <xref ref-type="bibr" rid="B28">Ebid and Deifalla, 2021</xref>). Thus, two refined models are proposed&#x2014;RCSSM-1 and RCSSM-2&#x2014;where the effect of Young&#x2019;s modulus and FRP axial rigidity, respectively, are included.</p>
<sec id="s4-2-1">
<title>4.2.1 First model</title>
<p>In this model, Young&#x2019;s modulus was included in the CSSM using multivariable non-linear regression (RCSSM-1); thus, the shear resistance is such that:<disp-formula id="e19">
<mml:math id="m63">
<mml:mrow>
<mml:mi>V</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>x</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mi>&#x3c4;</mml:mi>
<mml:mi>c</mml:mi>
</mml:msub>
<mml:mfrac>
<mml:mn>2</mml:mn>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac bevelled="true">
<mml:mrow>
<mml:mi>x</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>h</mml:mi>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mfrac>
<mml:mi>b</mml:mi>
<mml:mi>h</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>0.87</mml:mn>
<mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:msub>
<mml:mi>E</mml:mi>
<mml:mi>f</mml:mi>
</mml:msub>
</mml:mrow>
<mml:mrow>
<mml:msub>
<mml:mi>E</mml:mi>
<mml:mi>s</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mn>0.2</mml:mn>
</mml:msup>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(19)</label>
</disp-formula>
</p>
<p>where <inline-formula id="inf45">
<mml:math id="m64">
<mml:mrow>
<mml:msub>
<mml:mi>E</mml:mi>
<mml:mi>f</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is FRP&#x2019;s Young&#x2019;s modulus in GPa, and <inline-formula id="inf46">
<mml:math id="m65">
<mml:mrow>
<mml:msub>
<mml:mi>E</mml:mi>
<mml:mi>s</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is steel&#x2019;s Young&#x2019;s modulus in GPa.</p>
</sec>
<sec id="s4-2-2">
<title>4.2.2 Second model</title>
<p>In this model, the flexure re/inforcement axial rigidity was included in the CSSM using multivariable non-linear regression (RCSSM-2); thus, the shear resistance is such that:<disp-formula id="e20">
<mml:math id="m66">
<mml:mrow>
<mml:mi>V</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>x</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mi>&#x3c4;</mml:mi>
<mml:mi>c</mml:mi>
</mml:msub>
<mml:mfrac>
<mml:mn>2</mml:mn>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac bevelled="true">
<mml:mrow>
<mml:mi>x</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>h</mml:mi>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mfrac>
<mml:mi>b</mml:mi>
<mml:mi>h</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>0.80</mml:mn>
<mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>&#x3c1;</mml:mi>
<mml:mfrac>
<mml:mrow>
<mml:msub>
<mml:mi>E</mml:mi>
<mml:mi>f</mml:mi>
</mml:msub>
</mml:mrow>
<mml:mrow>
<mml:msub>
<mml:mi>E</mml:mi>
<mml:mi>s</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mn>0.11</mml:mn>
</mml:msup>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(20)</label>
</disp-formula>
</p>
<p>where <inline-formula id="inf47">
<mml:math id="m67">
<mml:mrow>
<mml:msub>
<mml:mi>E</mml:mi>
<mml:mi>f</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is FRP&#x2019;s Young&#x2019;s modulus in GPa, and <inline-formula id="inf48">
<mml:math id="m68">
<mml:mrow>
<mml:msub>
<mml:mi>E</mml:mi>
<mml:mi>s</mml:mi>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> is steel&#x2019;s Young&#x2019;s modulus in GPa.</p>
</sec>
</sec>
</sec>
<sec id="s5">
<title>5 Assessment of the RCSSM</title>
<p>The developed model was assessed by comparing its performance to that of the selected models with respect to the overall performance of the selected parameter.</p>
<sec id="s5-1">
<title>5.1 Overall</title>
<p>
<xref ref-type="fig" rid="F11">Figure 11</xref> shows the measured strength against the calculated strength using the CSSM, RCSSM-1, and RCSSM-2 methods, respectively, as well as the ideal 45-degree line, and the best-fit-line and the <inline-formula id="inf49">
<mml:math id="m69">
<mml:mrow>
<mml:mi>&#x3c7;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> factor. <xref ref-type="table" rid="T5">Table 5</xref> shows the statistical measures for the calculated SR for different methods. The CSSM model is the least conservative, with an SR average value of 0.71 and a <inline-formula id="inf50">
<mml:math id="m70">
<mml:mrow>
<mml:mi>&#x3c7;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> factor value of 0.707. For the proposed models, the SR average value is 1.03 and the <inline-formula id="inf51">
<mml:math id="m71">
<mml:mrow>
<mml:mi>&#x3c7;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> factor value is 1.06. For consistency, the coefficient of variation for all models ranged between 24% and 26%, showing good consistency. For safety, the lower 95% calculated for the RCSSM-1 and RCSSM-2 is above 0.85, which is considered reasonable. However, that calculated for the CSSM is lower than 0.85, which needs a higher safety factor for the purpose of design.</p>
<fig id="F11" position="float">
<label>FIGURE 11</label>
<caption>
<p>Calculated versus measured strength of proposed models.</p>
</caption>
<graphic xlink:href="fmats-10-1126806-g011.tif"/>
</fig>
<table-wrap id="T5" position="float">
<label>TABLE 5</label>
<caption>
<p>Statistical measures for calculated SR for proposed models.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="left"/>
<th align="center">CSSM</th>
<th align="center">RCSSM-1</th>
<th align="center">RCSSM-2</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="left">Mean</td>
<td align="right">0.70</td>
<td align="right">1.03</td>
<td align="right">1.03</td>
</tr>
<tr>
<td align="left">C.O.V.</td>
<td align="right">26%</td>
<td align="right">24%</td>
<td align="right">25%</td>
</tr>
<tr>
<td align="left">L.L. 99%</td>
<td align="right">0.68</td>
<td align="right">1.01</td>
<td align="right">1.00</td>
</tr>
<tr>
<td align="left">Minimum</td>
<td align="right">0.25</td>
<td align="right">0.38</td>
<td align="right">0.37</td>
</tr>
<tr>
<td align="left">Maximum</td>
<td align="right">1.46</td>
<td align="right">1.91</td>
<td align="right">2.19</td>
</tr>
<tr>
<td align="left">Median</td>
<td align="right">0.66</td>
<td align="right">1.01</td>
<td align="right">0.99</td>
</tr>
<tr>
<td align="left">Correlation coefficient</td>
<td align="right">0.92</td>
<td align="right">0.92</td>
<td align="right">0.92</td>
</tr>
</tbody>
</table>
</table-wrap>
</sec>
<sec id="s5-2">
<title>5.2 Against size</title>
<p>
<xref ref-type="table" rid="T6">Table 6</xref> shows the coefficient of correlation between measured strength and that calculated using various methods against size. The correlation coefficient between size and calculated SR for ACI, M, DN, B, CSSM, RCSSM-1, and RCSSM-2 is 0.04, 0.28, 0.82, 0.02, 0.13, 0.19, and 0.24, respectively. Thus, the calculated SR for the proposed models is weakly correlated to size. In addition, <xref ref-type="fig" rid="F12">Figure 12</xref> shows the calculated SR for ACI, M, DN, and B models against the size as well as the best-fit-line for each model. The best-fit-line slope for the calculated SR for ACI, M, DN, B, CSSM, RCSSM-1, and RCSSM-2 against size is 2.0E-4, 6.0E-4, 18E-4, 0.3E-4, 1E-4, 2E-4, and 3E-4. For all proposed models, safety increases with increased concrete compressive strength. The proposed models are consistent in size compared to other models.</p>
<table-wrap id="T6" position="float">
<label>TABLE 6</label>
<caption>
<p>Correlation coefficient between proposed models and variables.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="left"/>
<th align="center">CSSM</th>
<th align="center">RCSSM-1</th>
<th align="center">RCSSM-2</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="left">Size</td>
<td align="right">0.13</td>
<td align="right">0.19</td>
<td align="right">0.24</td>
</tr>
<tr>
<td align="left">Concrete compressive strength</td>
<td align="right">&#x2212;0.27</td>
<td align="right">&#x2212;0.29</td>
<td align="right">&#x2212;0.35</td>
</tr>
<tr>
<td align="left">Flexure reinforcement axial rigidity</td>
<td align="right">0.49</td>
<td align="right">0.32</td>
<td align="right">0.16</td>
</tr>
</tbody>
</table>
</table-wrap>
<fig id="F12" position="float">
<label>FIGURE 12</label>
<caption>
<p>SR calculated using proposed models versus size.</p>
</caption>
<graphic xlink:href="fmats-10-1126806-g012.tif"/>
</fig>
</sec>
<sec id="s5-3">
<title>5.3 Against concrete compressive strength</title>
<p>
<xref ref-type="table" rid="T6">Table 6</xref> shows the coefficient of correlation between measured and calculated strength for the selected methods against concrete compressive strength. The correlation coefficient between concrete compressive strength and calculated SR for CSSM, RCSSM-1, and RCSSM-2 is &#x2212;0.27, &#x2212;0.29, and &#x2212;0.35, respectively. Thus, the calculated SR for the proposed models is moderately correlated to concrete compressive strength. In addition, <xref ref-type="fig" rid="F13">Figure 13</xref> shows the calculated SR for CSSM, RCSSM-1, and RCSSM-2 against concrete compressive strength as well as the best-fit-line for each model. The best-fit-line slope for the calculated SR for CSSM, RCSSM-1, and RCSSM-2 against concrete compressive strength is 31E-4, 45E-4, and 56E-4. For proposed models, safety increases with increased concrete compressive strength&#x2014;consistent with concrete compressive strength compared to other models.</p>
<fig id="F13" position="float">
<label>FIGURE 13</label>
<caption>
<p>SR calculated using proposed models versus concrete compressive strength.</p>
</caption>
<graphic xlink:href="fmats-10-1126806-g013.tif"/>
</fig>
</sec>
<sec id="s5-4">
<title>5.4 Against flexure reinforcement axial rigidity</title>
<p>
<xref ref-type="table" rid="T6">Table 6</xref> shows the coefficient of correlation between measured and calculated strength for the selected methods against flexure reinforcement axial rigidity. The correlation coefficient between flexure reinforcement axial rigidity and calculated SR for ACI, M, DN, B, CSSM, RCSSM-1, and RCSSM-2 is 0.40, 0.40, &#x2212;0.01, 0.18, 0.49, 0.32, and 0.16, respectively. Thus, the calculated SR for RCSSM-2 is more weakly correlated to the flexure reinforcement axial rigidity than RCSSM-1 and CSSM. In addition, <xref ref-type="fig" rid="F14">Figure 14</xref> shows the calculated SR for CSSM, RCSSM-1, and RCSSM-2 models the flexure reinforcement axial rigidity as well as the best-fit-line for each model. The best-fit-line slope for the calculated SR for ACI, M, DN, B, CSSM, RCSSM-1, and RCSSM-2 against flexure reinforcement axial rigidity is &#x2212;0.69, &#x2212;0.35, &#x2212;0.006, 0.07, 0.19, 0.16, and 0.08. For all proposed models, safety increases with increased flexure reinforcement axial rigidity. RCSSM-1 is more consistent with flexure reinforcement axial rigidity than RCSSM-1 and CSSM.</p>
<fig id="F14" position="float">
<label>FIGURE 14</label>
<caption>
<p>SR calculated using proposed models versus flexure reinforcement axial rigidity.</p>
</caption>
<graphic xlink:href="fmats-10-1126806-g014.tif"/>
</fig>
</sec>
</sec>
<sec sec-type="conclusion" id="s6">
<title>6 Conclusion</title>
<p>This study selected five methods and evaluated them with respect to an intensive experimental database; it concluded that:<list list-type="simple">
<list-item>
<p>- ACI is overly conservative, while the B model is the least conservative.</p>
</list-item>
<list-item>
<p>- The DN model is less consistent than other models with respect to the size effect and concrete compressive strength.</p>
</list-item>
<list-item>
<p>- The ACI and M models are less consistent with respect to flexure reinforcement axial rigidity than other models.</p>
</list-item>
</list>
</p>
<p>In addition, the critical shear sliding model was adapted and further refined to include the effect of Young&#x2019;s modulus to fit the experimentally observed strength. The concluding remarks are:<list list-type="simple">
<list-item>
<p>- Adding the effect of Young&#x2019;s modulus improved the strength predictions with respect to those measured. However, the proposed model was not consistent with flexure reinforcement axial rigidity.</p>
</list-item>
<list-item>
<p>- Adding the effect of flexural reinforcement axial rigidity improved the strength and consistency with respect to flexural reinforcement axial rigidity.</p>
</list-item>
</list>
</p>
</sec>
</body>
<back>
<sec sec-type="data-availability" id="s7">
<title>Data availability statement</title>
<p>The original contributions presented in the study are included in the article/Supplementary Material; further inquiries can be directed to the corresponding authors.</p>
</sec>
<sec id="s8">
<title>Author contributions</title>
<p>Conceptualization, AE-s, TE-S, and AD; methodology, MT, YO, and TE-S; software, MT; validation, AD; formal analysis, AA and YO; investigation, AD and MT; resources, TE-S and AE-s; data curation, AE-s; writing&#x2014;original draft preparation, AA, TE-S, and AD; writing&#x2014;review and editing, AE-s, AA, TE-S, YO, AD, and MT; visualization, AD; supervision, AE-s and AD; funding acquisition, AA. All authors have read and agreed to the published version of the manuscript.</p>
</sec>
<sec sec-type="COI-statement" id="s9">
<title>Conflict of interest</title>
<p>The authors declare that the research was conducted in the absence of any commercial or financial relationships that could be construed as potential conflicts of interest.</p>
</sec>
<sec sec-type="disclaimer" id="s10">
<title>Publisher&#x2019;s note</title>
<p>All claims expressed in this article are solely those of the authors and do not necessarily represent those of their affiliated organizations, or those of the publisher, the editors, and the reviewers. Any product that may be evaluated in this article, or claim that may be made by its manufacturer, is not guaranteed or endorsed by the publisher.</p>
</sec>
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