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<front>
<journal-meta>
<journal-id journal-id-type="publisher-id">Front. Earth Sci.</journal-id>
<journal-title>Frontiers in Earth Science</journal-title>
<abbrev-journal-title abbrev-type="pubmed">Front. Earth Sci.</abbrev-journal-title>
<issn pub-type="epub">2296-6463</issn>
<publisher>
<publisher-name>Frontiers Media S.A.</publisher-name>
</publisher>
</journal-meta>
<article-meta>
<article-id pub-id-type="publisher-id">1116302</article-id>
<article-id pub-id-type="doi">10.3389/feart.2023.1116302</article-id>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Earth Science</subject>
<subj-group>
<subject>Original Research</subject>
</subj-group>
</subj-group>
</article-categories>
<title-group>
<article-title>Influence of normal stress on the shear strength of the structural plane considering the size effect</article-title>
<alt-title alt-title-type="left-running-head">Huang and Hu</alt-title>
<alt-title alt-title-type="right-running-head">
<ext-link ext-link-type="uri" xlink:href="https://doi.org/10.3389/feart.2023.1116302">10.3389/feart.2023.1116302</ext-link>
</alt-title>
</title-group>
<contrib-group>
<contrib contrib-type="author">
<name>
<surname>Huang</surname>
<given-names>Yuxi</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
<xref ref-type="aff" rid="aff2">
<sup>2</sup>
</xref>
</contrib>
<contrib contrib-type="author" corresp="yes">
<name>
<surname>Hu</surname>
<given-names>Gaojian</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/1616295/overview"/>
</contrib>
</contrib-group>
<aff id="aff1">
<sup>1</sup>
<institution>School of Mining</institution>, <institution>Liaoning Technical University</institution>, <addr-line>Fuxin</addr-line>, <country>China</country>
</aff>
<aff id="aff2">
<sup>2</sup>
<institution>School of Safety and Emergency Management Engineering, Taiyuan University of Technology</institution>, <addr-line>Taiyuan</addr-line>, <country>China</country>
</aff>
<aff id="aff3">
<sup>3</sup>
<institution>School of Civil Engineering</institution>, <institution>Shaoxing University</institution>, <addr-line>Shaoxing</addr-line>, <country>China</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/857687/overview">Xiaoping Zhou</ext-link>, Chongqing 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/879565/overview">Cao Rihong</ext-link>, Central South University, China</p>
<p>
<ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/2012649/overview">Nan Xiao</ext-link>, Changsha University of Science and Technology, China</p>
</fn>
<corresp id="c001">&#x2a;Correspondence: Gaojian Hu, <email>hugaojian8@163.com</email>
</corresp>
<fn fn-type="other">
<p>This article was submitted to Geohazards and Georisks, a section of the journal <italic>Frontiers in Earth Science</italic>
</p>
</fn>
</author-notes>
<pub-date pub-type="epub">
<day>20</day>
<month>01</month>
<year>2023</year>
</pub-date>
<pub-date pub-type="collection">
<year>2023</year>
</pub-date>
<volume>11</volume>
<elocation-id>1116302</elocation-id>
<history>
<date date-type="received">
<day>05</day>
<month>12</month>
<year>2022</year>
</date>
<date date-type="accepted">
<day>05</day>
<month>01</month>
<year>2023</year>
</date>
</history>
<permissions>
<copyright-statement>Copyright &#xa9; 2023 Huang and Hu.</copyright-statement>
<copyright-year>2023</copyright-year>
<copyright-holder>Huang and Hu</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>The shear strength of a structural plane is a critical parameter in the analysis of engineering rock stability. Significant differences exist due to the various normal stresses in the structural plane. Therefore, evaluating the rock deformation to effectively determine the influence of normal stresses at different scales on the shear strength of structural planes is of great significance. This study discusses the effects of normal stress and structural plane size on shear strength through numerical simulations and regression analysis. The results showed that the shear strength of the structural plane increases linearly with increasing normal stress. The shear strength of the structural plane decreases with increasing size, and the corresponding curve is exponential. The characteristic size and shear strength increase linearly with increasing normal stress. This paper presents the concrete form of these relationships, which can be used to calculate and predict the shear strength, which has significance in guiding engineering.</p>
</abstract>
<kwd-group>
<kwd>normal stress</kwd>
<kwd>characteristic shear strength</kwd>
<kwd>size effect</kwd>
<kwd>mathematical relationship</kwd>
<kwd>characteristic size</kwd>
</kwd-group>
<contract-sponsor id="cn001">Key Laboratory of Rock Mechanics and Geohazards of Zhejiang Province<named-content content-type="fundref-id">10.13039/100019165</named-content>
</contract-sponsor>
</article-meta>
</front>
<body>
<sec id="s1">
<title>1 Introduction</title>
<p>A structural plane is essential to rock mass and significantly affects rock mass stability. As shear strength is the critical parameter in the analysis of engineering rock stability, it is also a crucial parameter in the stability analysis of rock mass engineering.</p>
<p>Joints in rocks affect shear strength, including some sedimentary rocks, where they significantly affect shear strength. In addition, the normal stress of rock will cause different shear strengths of the structural plane (SSSP). <xref ref-type="bibr" rid="B2">Cheng (2019</xref>) investigated the effect of normal stress on the shear strength of coal bulk. <xref ref-type="bibr" rid="B10">Meng et al. (2022</xref>) analyzed the influence of particle size on shear behavior using PFC modeling. <xref ref-type="bibr" rid="B18">Xiao et al. (2021</xref>) developed four numerical models of various joint roughnesses using FLAC3D and examined the impact of joint roughness on shear mechanics. Zhou et al. (<xref ref-type="bibr" rid="B27">Zhou and Wang, 2016</xref>) (<xref ref-type="bibr" rid="B28">Zhou and Zhang, 2021</xref>) studied the effects of the specimen sizes and crack inclination angles on peak failure loads and evaluated the stress-induced damage progression in granite. The direct shear test was also used to study the influence of normal stress on shear strength. For example, <xref ref-type="bibr" rid="B22">Zhang et al. (2019</xref>) investigated the effects of initial normal stress bolt-grouting interface shear behavior using direct shear tests. <xref ref-type="bibr" rid="B25">Zhou et al. (2021a</xref>) assessed the strength characteristics of grouted joints of various thicknesses under different stress conditions by conducting shear tests on grouting rock samples. <xref ref-type="bibr" rid="B11">Niktabar et al. (2017</xref>) used a large direct shear testing machine to perform joint shear tests. <xref ref-type="bibr" rid="B26">Zhou et al. (2021b</xref>) discussed the development and contribution of experiments and numerical simulations in the compression-induced failure characteristics of flawed rock specimens. Accordingly, numerical simulations and on-site direct shear experiments were used to determine the effect of normal stress on the shear strength of the structural surface. Due to the size effect in rock, it is essential to determine the relationships of the size effect of the SSSP under normal stress. However, relatively few studies have reported on this topic.</p>
<p>Size effect exists in rocks, and SSSP is affected by rock size, such as in some joint-rich sedimentary rocks, in which the size changes affect the changes in the shear strength of rocks. <xref ref-type="bibr" rid="B12">Shao et al. (2018</xref>) investigated the intensity parameters of samples with different sizes. <xref ref-type="bibr" rid="B5">Islam et al. (2019</xref>) examined the effects of particle size on the shear strength of sand. <xref ref-type="bibr" rid="B6">Li (2020</xref>) analyzed the effect of maximum particle size on the SRM shear characteristics of the soil&#x2013;rock mixture. <xref ref-type="bibr" rid="B13">Wang et al. (2018a</xref>) reported on the results of mechanical analysis and size effect. <xref ref-type="bibr" rid="B7">Li et al. (2018</xref>) explored the influence of crack size on the peak internal friction angle. Wang et al. studied the influence of flaw length (<xref ref-type="bibr" rid="B16">Wang et al., 2016</xref>) and flaw inclination angles (<xref ref-type="bibr" rid="B14">Wang et al., 2017</xref>) on crack propagation and proposed a novel 3D-conjugated bond-pair-based peridynamic model (<xref ref-type="bibr" rid="B15">Wang et al., 2018b</xref>). Collectively, these research findings demonstrated the presence of size effect in the SSSP. Therefore, the size effect of shear strength exists when normal stress is applied. Studying the size effect of SSSP and determining the relationship between SSSP and rock size under normal stress is of utmost importance. However, relatively few studies have addressed this topic.</p>
<p>The mineral composition and structure differ among various rocks. In addition, the solubility of different minerals varies. Therefore, different rock sizes are essential for rock weathering. Investigating the size effect of rocks is valuable for analyzing large blocks of terrain such as hills (<xref ref-type="bibr" rid="B8">Li et al., 2021</xref>). Scholars have examined the representative elementary volume (REV). <xref ref-type="bibr" rid="B21">Zertsalov et al. (2020</xref>) analyzed the deformation characteristics for different proportions of characteristic rock fragment sizes and their structural elements using numerical simulation. <xref ref-type="bibr" rid="B20">Ying et al. (2018</xref>) evaluated the REV of rock based on a statistical test. Zhang et al. (<xref ref-type="bibr" rid="B24">Zhang and Zhou, 2020a</xref>;<xref ref-type="bibr" rid="B23">Zhang and Zhou, 2020b</xref>) explored the fracture-related acoustic emission event rate characteristics at the unstable cracking phase in flawed rocks. <xref ref-type="bibr" rid="B17">Wu et al. (2014</xref>) studied the application effect of REV engineering based on the theory of equivalent continuous medium. <xref ref-type="bibr" rid="B19">Yang et al. (2017</xref>) reported that the characteristic shear strength size was not as sensitive as the permeability. <xref ref-type="bibr" rid="B4">Hu et al. (2022</xref>) determined the relationship between the number of joints and the SSSP. The aforementioned studies demonstrate the relatively limited research on the REV of the mechanical parameters of shear.</p>
<p>Therefore, the present study investigates the influence of i) normal stress and ii) size on the SSSP. These findings establish the relationship between i) SSSP and normal stress, ii) SSSP and size, iii) characteristic sizes of SSSP and normal stress, and (&#x2173;) characteristic SSSP and normal stress.</p>
</sec>
<sec id="s2">
<title>2 Numerical simulations</title>
<p>The research was conducted from two perspectives: 1) the influence of normal stress on SSSP, comprising programs 1&#x2013;5, with normal stress values of 1, 2, 3, 4, and 5&#xa0;MPa; and 2) the impact of structural plane size on SSSP, comprising programs 6&#x2013;10, with sizes of 100, 200, 300, 400, and 500&#xa0;mm, respectively. <xref ref-type="table" rid="T1">Table 1</xref> lists simulation programs.</p>
<table-wrap id="T1" position="float">
<label>TABLE 1</label>
<caption>
<p>Normal stress and size combinations.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th rowspan="2" align="center">Simulation program</th>
<th rowspan="2" align="center">Normal stress (MPa)</th>
<th align="center">Program 1</th>
<th align="center">Program 2</th>
<th align="center">Program 3</th>
<th align="center">Program 4</th>
<th align="center">Program 5</th>
</tr>
<tr>
<th align="center">Size 100&#xa0;mm</th>
<th align="center">Size 200&#xa0;mm</th>
<th align="center">Size 300&#xa0;mm</th>
<th align="center">Size 400&#xa0;mm</th>
<th align="center">Size 500&#xa0;mm</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">6</td>
<td align="center">1</td>
<td align="center">1 &#xd7; 100</td>
<td align="center">1 &#xd7; 200</td>
<td align="center">1 &#xd7; 300</td>
<td align="center">1 &#xd7; 400</td>
<td align="center">1 &#xd7; 500</td>
</tr>
<tr>
<td align="center">7</td>
<td align="center">2</td>
<td align="center">2 &#xd7; 100</td>
<td align="center">2 &#xd7; 200</td>
<td align="center">2 &#xd7; 300</td>
<td align="center">2 &#xd7; 400</td>
<td align="center">2 &#xd7; 500</td>
</tr>
<tr>
<td align="center">8</td>
<td align="center">3</td>
<td align="center">3 &#xd7; 100</td>
<td align="center">3 &#xd7; 200</td>
<td align="center">3 &#xd7; 300</td>
<td align="center">3 &#xd7; 400</td>
<td align="center">3 &#xd7; 500</td>
</tr>
<tr>
<td align="center">9</td>
<td align="center">4</td>
<td align="center">4 &#xd7; 100</td>
<td align="center">4 &#xd7; 200</td>
<td align="center">4 &#xd7; 300</td>
<td align="center">4 &#xd7; 400</td>
<td align="center">4 &#xd7; 500</td>
</tr>
<tr>
<td align="center">10</td>
<td align="center">5</td>
<td align="center">5 &#xd7; 100</td>
<td align="center">5 &#xd7; 200</td>
<td align="center">5 &#xd7; 300</td>
<td align="center">5 &#xd7; 400</td>
<td align="center">5 &#xd7; 500</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>This established 25 numerical models. <xref ref-type="fig" rid="F1">Figure 1</xref> depicts the schematic diagram of the programs.</p>
<fig id="F1" position="float">
<label>FIGURE 1</label>
<caption>
<p>Rock models. <bold>(A)</bold> Mechanical model. <bold>(B)</bold> Size model.</p>
</caption>
<graphic xlink:href="feart-11-1116302-g001.tif"/>
</fig>
<p>This study investigated rocks with different normal stresses and penetrating joints. Therefore, various sizes and normal stresses of rock models were imported into RFPA software. The model was subjected to two side displacements, each of which was incremented by 0.01&#xa0;mm. The model was divided into upper and bottom models. The upper model rate remained constant as it moved from left to right. However, the lower model remained stationary regardless of the movement of the upper model. The following parameters were set for the rocks and penetrating joints: a rock elastic modulus of 11,000&#xa0;MPa, a Poisson ratio of 0.25, and a joint elastic modulus of 1.2&#xa0;MPa. Regarding the strength parameters, the internal friction angle was 30&#xb0;, as shown in <xref ref-type="table" rid="T2">Table 2</xref>.</p>
<table-wrap id="T2" position="float">
<label>TABLE 2</label>
<caption>
<p>Rock mechanical parameters.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Material</th>
<th align="center">Elastic modulus (MPa)</th>
<th align="center">Compressive strength (MPa)</th>
<th align="center">Poisson&#x2019;s ratio</th>
<th align="center">Friction angle (&#xb0;)</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">Rock</td>
<td align="center">11,000</td>
<td align="center">80</td>
<td align="center">0.25</td>
<td align="center">30</td>
</tr>
<tr>
<td align="center">Joints</td>
<td align="center">1.2</td>
<td align="center">1.1</td>
<td align="center">0.30</td>
<td align="center">30</td>
</tr>
</tbody>
</table>
</table-wrap>
</sec>
<sec id="s3">
<title>3 Numerical simulation analysis</title>
<sec id="s3-1">
<title>3.1 Influence of the normal stress on the SSSP</title>
<sec id="s3-1-1">
<title>3.1.1 Stress&#x2013;strain curve analysis</title>
<p>Stress&#x2013;strain curves obtained from numerical simulations were drawn to analyze the influence of normal stress on SSSP, as shown in <xref ref-type="fig" rid="F2">Figure 2</xref>.</p>
<fig id="F2" position="float">
<label>FIGURE 2</label>
<caption>
<p>Stress&#x2013;strain curves of different normal stresses.</p>
</caption>
<graphic xlink:href="feart-11-1116302-g002.tif"/>
</fig>
<p>
<xref ref-type="fig" rid="F2">Figure 2A</xref> through <xref ref-type="fig" rid="F2">Figure 2E</xref> indicate that as normal stress increases, the curve contours and trends are similar and their development trends are comparable. Using the curve with a normal stress of 1&#xa0;MPa in <xref ref-type="fig" rid="F2">Figure 2A</xref> as an example, under the influence of different normal stresses on the structural surface, after the shear stress peaked, it gradually decreased and then stabilized as the horizontal shear displacement increased. The shear strength then no longer varied significantly, showing a nearly straight line.</p>
<p>The results of the analysis of the effect of normal stress on the SSSP are shown in <xref ref-type="fig" rid="F2">Figure 2A</xref>. The relationship curves remained identical while the SSSP gradually increased when the normal stress increased from 1 to 5&#xa0;MPa. Therefore, the shear strength was associated with the normal stress. Based on the curves in <xref ref-type="fig" rid="F2">Figure 2</xref>, the SSSP was explored, as shown in <xref ref-type="table" rid="T3">Table 3</xref>.</p>
<table-wrap id="T3" position="float">
<label>TABLE 3</label>
<caption>
<p>Shear strengths.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th rowspan="3" align="center">Simulation program</th>
<th rowspan="3" align="center">Size (mm)</th>
<th colspan="5" align="center">SSSP (MPa)</th>
</tr>
<tr>
<th align="center">Program 6</th>
<th align="center">Program 7</th>
<th align="center">Program 8</th>
<th align="center">Program 9</th>
<th align="center">Program 10</th>
</tr>
<tr>
<th align="center">1&#xa0;MPa</th>
<th align="center">2&#xa0;MPa</th>
<th align="center">3&#xa0;MPa</th>
<th align="center">4&#xa0;MPa</th>
<th align="center">5&#xa0;MPa</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">1</td>
<td align="center">100</td>
<td align="center">22.015</td>
<td align="center">29.178</td>
<td align="center">35.836</td>
<td align="center">41.96</td>
<td align="center">48.004</td>
</tr>
<tr>
<td align="center">2</td>
<td align="center">200</td>
<td align="center">11.858</td>
<td align="center">14.234</td>
<td align="center">17.237</td>
<td align="center">19.865</td>
<td align="center">22.433</td>
</tr>
<tr>
<td align="center">3</td>
<td align="center">300</td>
<td align="center">6.938</td>
<td align="center">8.836</td>
<td align="center">10.595</td>
<td align="center">12.498</td>
<td align="center">14.017</td>
</tr>
<tr>
<td align="center">4</td>
<td align="center">400</td>
<td align="center">5.508</td>
<td align="center">7.162</td>
<td align="center">8.64</td>
<td align="center">10.114</td>
<td align="center">11.505</td>
</tr>
<tr>
<td align="center">5</td>
<td align="center">500</td>
<td align="center">4.413</td>
<td align="center">6.03</td>
<td align="center">7.208</td>
<td align="center">8.117</td>
<td align="center">9.189</td>
</tr>
</tbody>
</table>
</table-wrap>
</sec>
<sec id="s3-1-2">
<title>3.1.2 Relationship between normal stress and shear strength</title>
<p>
<xref ref-type="fig" rid="F3">Figure 3</xref> shows a scatter plot of the shear strength of the structural surface. Normal stress based on the data in <xref ref-type="table" rid="T3">Table 3</xref> was drawn using OriginLab software. The appropriate fitting relationship was then selected and regressed.</p>
<fig id="F3" position="float">
<label>FIGURE 3</label>
<caption>
<p>Fitting curves of SSSP.</p>
</caption>
<graphic xlink:href="feart-11-1116302-g003.tif"/>
</fig>
<p>
<xref ref-type="fig" rid="F3">Figure 3</xref> also shows that when the normal stress was 1&#xa0;MPa, the SSSP decreased from 22.015 to 4.413&#xa0;MPa as the size varied between 100 and 500&#xa0;mm, indicating that the shear strength was associated with the size. This regulation remained consistent even if the normal stress changes. As the normal stress increased from 1 to 5&#xa0;MPa, the SSSP increased from 22.015 to 48.004&#xa0;MPa at a size of 100&#xa0;mm. Hence, the SSSP rose gradually as the normal stress increased. Therefore, the SSSP was affected by normal stress.</p>
<p>The preceding results showed that SSSP was related to normal stress. The expressions for the relationship between the two are listed in <xref ref-type="table" rid="T4">Table 4</xref>.</p>
<table-wrap id="T4" position="float">
<label>TABLE 4</label>
<caption>
<p>Fitting relationships between SSSP and normal stress.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="left">Size of the structure plane/mm</th>
<th align="center">Fitting formula</th>
<th align="center">
<italic>R</italic>
<sup>2</sup>
</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">100</td>
<td align="center">
<inline-formula id="inf1">
<mml:math id="m1">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>15.971</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>6.476</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="center">0.999</td>
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<td align="center">200</td>
<td align="center">
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<mml:math id="m2">
<mml:mrow>
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<mml:mo>&#x3d;</mml:mo>
<mml:mn>9.091</mml:mn>
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<mml:mn>2.678</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
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<td align="center">0.999</td>
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<td align="center">300</td>
<td align="center">
<inline-formula id="inf3">
<mml:math id="m3">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
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<mml:mfenced open="(" close=")" separators="|">
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<mml:mi>&#x3c3;</mml:mi>
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<mml:mo>&#x3d;</mml:mo>
<mml:mn>5.231</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>1.782</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
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<td align="center">0.999</td>
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<td align="center">400</td>
<td align="center">
<inline-formula id="inf4">
<mml:math id="m4">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>4.102</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>1.495</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="center">0.999</td>
</tr>
<tr>
<td align="center">500</td>
<td align="center">
<inline-formula id="inf5">
<mml:math id="m5">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>3.5</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>1.164</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="center">0.988</td>
</tr>
</tbody>
</table>
</table-wrap>
</sec>
<sec id="s3-1-3">
<title>3.1.3 Relationship of shear strength and normal stress according to size change</title>
<p>From the results obtained in <xref ref-type="table" rid="T4">Table 4</xref>, which conform to the Coulomb criterion formula, the following relationship between SSSP and normal stress can be derived:<disp-formula id="e1">
<mml:math id="m6">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mi>c</mml:mi>
<mml:mo>&#x2b;</mml:mo>
<mml:mi>f</mml:mi>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
<mml:mo>,</mml:mo>
</mml:math>
<label>(1)</label>
</disp-formula>where &#x3c3; is the normal stress, &#x3c4;(&#x3c3;) is the shear strength, c is the cohesion, and f is the friction angle coefficient.</p>
<p>Eq. <xref ref-type="disp-formula" rid="e1">1</xref> is the general formula for the relationship between the SSSP and normal stress considering the size effect, which applies to the rough undulating structural plane without filling. This formula contains parameters <italic>c</italic> and <italic>f</italic> related to rock size. Once the rock size is determined, the SSSP under various normal forces can be calculated using Eq. <xref ref-type="disp-formula" rid="e1">1</xref>.</p>
<p>When the rock size changes, c and f can be determined based on the fitting formula in <xref ref-type="table" rid="T4">Table 4</xref>. The cohesion and friction angle coefficient are shown in <xref ref-type="table" rid="T5">Table 5</xref> and are related to the size, as shown in <xref ref-type="fig" rid="F4">Figure 4</xref>.</p>
<table-wrap id="T5" position="float">
<label>TABLE 5</label>
<caption>
<p>Values of <italic>c</italic> and <italic>f</italic>.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Size of the structure plane/<italic>l</italic>/mm</th>
<th align="center">100</th>
<th align="center">200</th>
<th align="center">300</th>
<th align="center">400</th>
<th align="center">500</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">
<italic>c</italic> (MPa)</td>
<td align="center">15.971</td>
<td align="center">9.091</td>
<td align="center">5.231</td>
<td align="center">4.102</td>
<td align="center">3.5</td>
</tr>
<tr>
<td align="center">
<italic>F</italic>
</td>
<td align="center">6.476</td>
<td align="center">2.678</td>
<td align="center">1.782</td>
<td align="center">1.495</td>
<td align="center">1.164</td>
</tr>
</tbody>
</table>
</table-wrap>
<fig id="F4" position="float">
<label>FIGURE 4</label>
<caption>
<p>Fitting curves of the parameters. <bold>(A)</bold> Cohesion, c. <bold>(B)</bold> Friction angle coefficient, f.</p>
</caption>
<graphic xlink:href="feart-11-1116302-g004.tif"/>
</fig>
<p>The following relationship between the cohesion c and the friction angle coefficient f and size is derived from the curve in <xref ref-type="fig" rid="F4">Figure 4</xref>:<disp-formula id="e2">
<mml:math id="m7">
<mml:mrow>
<mml:mi>c</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>28.928</mml:mn>
<mml:msup>
<mml:mi>e</mml:mi>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>l</mml:mi>
</mml:mrow>
<mml:mn>127.516</mml:mn>
</mml:mfrac>
</mml:msup>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>2.816</mml:mn>
</mml:mrow>
<mml:mo>,</mml:mo>
</mml:math>
<label>(2)</label>
</disp-formula>
<disp-formula id="e3">
<mml:math id="m8">
<mml:mrow>
<mml:mi>f</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>18.438</mml:mn>
<mml:msup>
<mml:mi>e</mml:mi>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>l</mml:mi>
</mml:mrow>
<mml:mn>79.234</mml:mn>
</mml:mfrac>
</mml:msup>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>1.273</mml:mn>
</mml:mrow>
<mml:mo>.</mml:mo>
</mml:math>
<label>(3)</label>
</disp-formula>
</p>
<p>The relationship between shear strength and normal stress can be obtained from Eq. <xref ref-type="disp-formula" rid="e1">1</xref> through Eq. <xref ref-type="disp-formula" rid="e3">3</xref> as follows:<disp-formula id="e4">
<mml:math id="m9">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>28.928</mml:mn>
<mml:msup>
<mml:mi>e</mml:mi>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>l</mml:mi>
</mml:mrow>
<mml:mn>127.516</mml:mn>
</mml:mfrac>
</mml:msup>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>2.816</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>18.438</mml:mn>
<mml:msup>
<mml:mi>e</mml:mi>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>l</mml:mi>
</mml:mrow>
<mml:mn>79.234</mml:mn>
</mml:mfrac>
</mml:msup>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>1.273</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
<mml:mo>,</mml:mo>
</mml:math>
<label>(4)</label>
</disp-formula>where <italic>l</italic> is the size.</p>
<p>Eq. <xref ref-type="disp-formula" rid="e4">4</xref> is an engineering-relevant formula that can be used to calculate the corresponding SSSP when the normal stress changes. The corresponding SSSP value can be calculated using the normal stress and given size.</p>
</sec>
</sec>
<sec id="s3-2">
<title>3.2 Size effect of SSSP</title>
<sec id="s3-2-1">
<title>3.2.1 Stress&#x2013;strain curve analysis</title>
<p>To analyze the influence of structural plane size on the SSSP, the stress&#x2013;strain curves obtained from numerical simulation are depicted in <xref ref-type="fig" rid="F5">Figure 5</xref>.</p>
<fig id="F5" position="float">
<label>FIGURE 5</label>
<caption>
<p>Stress&#x2013;strain curves for different normal stress values.</p>
</caption>
<graphic xlink:href="feart-11-1116302-g005.tif"/>
</fig>
<p>
<xref ref-type="fig" rid="F5">Figure 5A</xref> through <xref ref-type="fig" rid="F5">Figure 5E</xref> demonstrate the similar curve laws. A curve with a normal stress of 2 in <xref ref-type="fig" rid="F5">Figure 5B</xref> was used to analyze the relationship between shear stress and shear displacement. Before reaching the peak shear strength, the shear stress initially increased as the shear displacement grew; afterward, the shear strength hardly changed, exhibiting a nearly straight-line state.</p>
<p>
<xref ref-type="fig" rid="F5">Figure 5B</xref> shows the results of the analysis of the impact of size on the SSSP. Similar relationships were observed between shear stress and shear displacement for sizes of 100, 200, 300, 400, and 500&#xa0;mm, respectively. <xref ref-type="fig" rid="F5">Figure 5B</xref> shows that at a normal stress of 1&#xa0;MPa, the shear strength gradually decreased as the size increased from 100 to 500&#xa0;mm. This demonstrated that the shear strength was affected by the size.</p>
<p>The shear strength is shown in <xref ref-type="fig" rid="F5">Figure 5</xref> and listed in <xref ref-type="table" rid="T6">Table 6</xref>.</p>
<table-wrap id="T6" position="float">
<label>TABLE 6</label>
<caption>
<p>Shear strengths.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th rowspan="3" align="center">Simulation program</th>
<th rowspan="3" align="center">Normal stress (MPa)</th>
<th colspan="5" align="center">Shear strength (MPa)</th>
</tr>
<tr>
<th align="center">Program 1</th>
<th align="center">Program 2</th>
<th align="center">Program 3</th>
<th align="center">Program 4</th>
<th align="center">Program 5</th>
</tr>
<tr>
<th align="center">100&#xa0;mm</th>
<th align="center">200&#xa0;mm</th>
<th align="center">300&#xa0;mm</th>
<th align="center">400&#xa0;mm</th>
<th align="center">500&#xa0;mm</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">6</td>
<td align="center">1</td>
<td align="center">22.015</td>
<td align="center">11.858</td>
<td align="center">6.938</td>
<td align="center">5.508</td>
<td align="center">4.413</td>
</tr>
<tr>
<td align="center">7</td>
<td align="center">2</td>
<td align="center">29.178</td>
<td align="center">14.234</td>
<td align="center">8.836</td>
<td align="center">7.162</td>
<td align="center">6.03</td>
</tr>
<tr>
<td align="center">8</td>
<td align="center">3</td>
<td align="center">35.836</td>
<td align="center">17.237</td>
<td align="center">10.595</td>
<td align="center">8.64</td>
<td align="center">7.208</td>
</tr>
<tr>
<td align="center">9</td>
<td align="center">4</td>
<td align="center">41.96</td>
<td align="center">19.865</td>
<td align="center">12.498</td>
<td align="center">10.114</td>
<td align="center">8.117</td>
</tr>
<tr>
<td align="center">10</td>
<td align="center">5</td>
<td align="center">48.004</td>
<td align="center">22.433</td>
<td align="center">14.017</td>
<td align="center">11.505</td>
<td align="center">9.189</td>
</tr>
</tbody>
</table>
</table-wrap>
</sec>
<sec id="s3-2-2">
<title>3.2.2 Relationships between shear strength and size</title>
<p>The scatter plot of shear strength and size in <xref ref-type="table" rid="T6">Table 6</xref> was drawn using OriginLab software. A suitable fitting relationship was selected, as shown in <xref ref-type="fig" rid="F6">Figure 6</xref>.</p>
<fig id="F6" position="float">
<label>FIGURE 6</label>
<caption>
<p>Fitting curves for shear strength.</p>
</caption>
<graphic xlink:href="feart-11-1116302-g006.tif"/>
</fig>
<p>
<xref ref-type="fig" rid="F6">Figure 6</xref> shows that the SSSP decreased from 11.858 to 22.433&#xa0;MPa as the normal stress rose from 1 to 5&#xa0;MPa at a size of 200&#xa0;mm, indicating that the SSSP is affected by the normal stress. When normal stress grows, SSSP improves. This regulation remains consistent even if the normal stress becomes different. The SSSP drops from 29.178 to 6.03&#xa0;MPa as the size varies between 100 and 500&#xa0;mm when the normal stress is 2&#xa0;MPa. So the SSSP reduces gradually while size increases.</p>
<p>
<xref ref-type="fig" rid="F6">Figure 6</xref> illustrates the relationship between the SSSP and size. <xref ref-type="table" rid="T7">Table 7</xref> lists the expressions for the relationship between the two.</p>
<table-wrap id="T7" position="float">
<label>TABLE 7</label>
<caption>
<p>Fitting model between SSSP and sizes.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Normal stress (MPa)</th>
<th align="center">Fitting formula</th>
<th align="center">
<italic>R</italic>
<sup>2</sup>
</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">1</td>
<td align="center">
<inline-formula id="inf6">
<mml:math id="m10">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>3.814</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>42.079</mml:mn>
<mml:msup>
<mml:mi>e</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>l</mml:mi>
</mml:mrow>
<mml:mn>119.521</mml:mn>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="center">0.999</td>
</tr>
<tr>
<td align="center">2</td>
<td align="center">
<inline-formula id="inf7">
<mml:math id="m11">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>5.809</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>64.504</mml:mn>
<mml:msup>
<mml:mi>e</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>l</mml:mi>
</mml:mrow>
<mml:mn>98.454</mml:mn>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="center">0.999</td>
</tr>
<tr>
<td align="center">3</td>
<td align="center">
<inline-formula id="inf8">
<mml:math id="m12">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>6.989</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>80.831</mml:mn>
<mml:msup>
<mml:mi>e</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>l</mml:mi>
</mml:mrow>
<mml:mn>97.017</mml:mn>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="center">0.999</td>
</tr>
<tr>
<td align="center">4</td>
<td align="center">
<inline-formula id="inf9">
<mml:math id="m13">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>8.084</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>95.392</mml:mn>
<mml:msup>
<mml:mi>e</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>l</mml:mi>
</mml:mrow>
<mml:mn>96.475</mml:mn>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="center">0.999</td>
</tr>
<tr>
<td align="center">5</td>
<td align="center">
<inline-formula id="inf10">
<mml:math id="m14">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>9.235</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>111.714</mml:mn>
<mml:msup>
<mml:mi>e</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>l</mml:mi>
</mml:mrow>
<mml:mn>94.389</mml:mn>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="center">0.999</td>
</tr>
</tbody>
</table>
</table-wrap>
</sec>
<sec id="s3-2-3">
<title>3.2.3 Relationship between the SSSP and the size</title>
<p>From the results shown in <xref ref-type="table" rid="T7">Table 7</xref>, the relationship between SSSP and size can be obtained as follows:<disp-formula id="e5">
<mml:math id="m15">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mi>h</mml:mi>
<mml:mo>&#x2b;</mml:mo>
<mml:mi>d</mml:mi>
<mml:msup>
<mml:mi>e</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>l</mml:mi>
</mml:mrow>
<mml:mi>g</mml:mi>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:msup>
</mml:mrow>
<mml:mo>,</mml:mo>
</mml:math>
<label>(5)</label>
</disp-formula>where <italic>&#x3c4;</italic> (<italic>l</italic>) is the SSSP; <italic>l</italic> is the size; and <italic>d</italic>, <italic>g</italic>, and <italic>h</italic> are parameters.</p>
<p>
<xref ref-type="table" rid="T8">Table 8</xref> displays parameters that can be extracted easily based on the results presented in <xref ref-type="table" rid="T7">Table 7</xref>. The fitting curves for parameters <italic>d</italic>, <italic>g</italic>, and <italic>h</italic> are well-fitted with normal stress, as shown in <xref ref-type="fig" rid="F7">Figure 7</xref>.</p>
<table-wrap id="T8" position="float">
<label>TABLE 8</label>
<caption>
<p>Values of parameters <italic>d</italic>, <italic>g</italic>, and <italic>h</italic>.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th rowspan="2" align="center">Parameter</th>
<th colspan="5" align="center">Normal stress (MPa)</th>
</tr>
<tr>
<th align="center">1</th>
<th align="center">2</th>
<th align="center">3</th>
<th align="center">4</th>
<th align="center">5</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">
<italic>D</italic>
</td>
<td align="left">42.079</td>
<td align="left">64.504</td>
<td align="left">80.831</td>
<td align="left">95.392</td>
<td align="left">111.714</td>
</tr>
<tr>
<td align="center">
<italic>G</italic>
</td>
<td align="left">119.521</td>
<td align="left">98.454</td>
<td align="left">97.017</td>
<td align="left">96.475</td>
<td align="left">94.389</td>
</tr>
<tr>
<td align="center">
<italic>H</italic>
</td>
<td align="left">3.814</td>
<td align="left">5.809</td>
<td align="left">6.989</td>
<td align="left">8.084</td>
<td align="left">9.235</td>
</tr>
</tbody>
</table>
</table-wrap>
<fig id="F7" position="float">
<label>FIGURE 7</label>
<caption>
<p>Fitting curve diagram of the parameters.</p>
</caption>
<graphic xlink:href="feart-11-1116302-g007.tif"/>
</fig>
<p>Based on the curve in <xref ref-type="fig" rid="F7">Figure 7</xref>, the following relationship exists between each parameter and the normal stress:<disp-formula id="e6">
<mml:math id="m16">
<mml:mrow>
<mml:mi>d</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>27.857</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>17.016</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
<mml:mo>,</mml:mo>
</mml:math>
<label>(6)</label>
</disp-formula>
<disp-formula id="e7">
<mml:math id="m17">
<mml:mrow>
<mml:mi>g</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>190.925</mml:mn>
<mml:msup>
<mml:mi>e</mml:mi>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
<mml:mn>0.480</mml:mn>
</mml:mfrac>
</mml:msup>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>95.743</mml:mn>
</mml:mrow>
<mml:mo>,</mml:mo>
</mml:math>
<label>(7)</label>
</disp-formula>
<disp-formula id="e8">
<mml:math id="m18">
<mml:mrow>
<mml:mi>h</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>2.851</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>1.312</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
<mml:mo>.</mml:mo>
</mml:math>
<label>(8)</label>
</disp-formula>
</p>
<p>The expression between SSSP and size be obtained by combining Eq. <xref ref-type="disp-formula" rid="e5">5</xref> through Eq. <xref ref-type="disp-formula" rid="e8">8</xref> as follows:<disp-formula id="e9">
<mml:math id="m19">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>27.857</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>17.016</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:msup>
<mml:mi mathvariant="normal">e</mml:mi>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>l</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mn>190.925</mml:mn>
<mml:mi>e</mml:mi>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
<mml:mn>0.48</mml:mn>
</mml:mfrac>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>95.743</mml:mn>
</mml:mrow>
</mml:mfrac>
</mml:msup>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>2.851</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>1.312</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
<mml:mo>.</mml:mo>
</mml:math>
<label>(9)</label>
</disp-formula>
</p>
<p>Eq. <xref ref-type="disp-formula" rid="e9">9</xref> is an engineering application formula that can be used to calculate the corresponding SSSP when the changes occur. When the normal stress for engineering sites is provided, the corresponding SSSP value can be determined based on the size.</p>
</sec>
</sec>
<sec id="s3-3">
<title>3.3 Relationships of the CSSS, CSS, and normal stress</title>
<sec id="s3-3-1">
<title>3.3.1 Derived formula for the CSSS of the structural plane</title>
<p>SSSP has a size effect. However, when the size reaches a specific critical value, the SSSP tends to remain constant. This critical size is the characteristic size of the shear strength (CSSS).</p>
<p>It is not easy to quantify the exact characteristic size. <xref ref-type="bibr" rid="B9">Liang et al. 2013</xref>) proposed one method to determine the characteristic size by calculating the derivative of Eq. <xref ref-type="disp-formula" rid="e5">5</xref>. The CSSS is determined as follows:<disp-formula id="e10">
<mml:math id="m20">
<mml:mrow>
<mml:msup>
<mml:mi>&#x3c4;</mml:mi>
<mml:mo>&#x2032;</mml:mo>
</mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mo>&#x2212;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mi>d</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>g</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:msup>
<mml:mi>e</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>l</mml:mi>
</mml:mrow>
<mml:mi>g</mml:mi>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:msup>
</mml:mrow>
<mml:mo>,</mml:mo>
</mml:math>
<label>(10)</label>
</disp-formula>
<disp-formula id="e11">
<mml:math id="m21">
<mml:mrow>
<mml:mrow>
<mml:mfenced open="|" close="|" separators="|">
<mml:mrow>
<mml:msup>
<mml:mi>&#x3c4;</mml:mi>
<mml:mo>&#x2032;</mml:mo>
</mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x2264;</mml:mo>
<mml:mi>&#x3b1;</mml:mi>
</mml:mrow>
<mml:mo>,</mml:mo>
</mml:math>
<label>(11)</label>
</disp-formula>
<disp-formula id="e12">
<mml:math id="m22">
<mml:mrow>
<mml:mi>l</mml:mi>
<mml:mo>&#x2265;</mml:mo>
<mml:mi>g</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mi>ln</mml:mi>
<mml:mfrac>
<mml:mrow>
<mml:mi>d</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>g</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>g</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mi>ln</mml:mi>
<mml:mo>&#x2061;</mml:mo>
<mml:mi>&#x3b1;</mml:mi>
</mml:mrow>
<mml:mo>,</mml:mo>
</mml:math>
<label>(12)</label>
</disp-formula>where <italic>&#x3b1;</italic> is the acceptable absolute value of the slope.</p>
</sec>
<sec id="s3-3-2">
<title>3.3.2 Relationship between CSSS and normal stress</title>
<p>Eq. <xref ref-type="disp-formula" rid="e12">12</xref> can be regarded as the characteristic size, into which the fitting parameters are substituted to determine their values. Supposing that the CSSS can be obtained, <xref ref-type="table" rid="T9">Table 9</xref> lists the relationships between the CSSS of the structural plane and the normal stress. The CSSS was solved when the normal stress increased from 1 to 5&#xa0;MPa. The regression curve of the CSSS and normal stress is depicted in <xref ref-type="fig" rid="F8">Figure 8</xref>.</p>
<table-wrap id="T9" position="float">
<label>TABLE 9</label>
<caption>
<p>Relationships between CSSS and normal stress.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Normal stress (MPa)</th>
<th align="center">1</th>
<th align="center">2</th>
<th align="center">3</th>
<th align="center">4</th>
<th align="center">5</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">CSSS (mm)</td>
<td align="center">316.125</td>
<td align="center">321.552</td>
<td align="center">340.176</td>
<td align="center">354.796</td>
<td align="center">364.096</td>
</tr>
</tbody>
</table>
</table-wrap>
<fig id="F8" position="float">
<label>FIGURE 8</label>
<caption>
<p>Fitting curve between the normal stress and characteristic size.</p>
</caption>
<graphic xlink:href="feart-11-1116302-g008.tif"/>
</fig>
<p>
<xref ref-type="fig" rid="F8">Figure 8</xref> shows that as the normal stress increased, the CSSS increased gradually. The curve&#x2019;s function is linear. Therefore, the following particular relationship is obtained:<disp-formula id="e13">
<mml:math id="m23">
<mml:mrow>
<mml:mi>D</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>300.594</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>12.918</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
<mml:mo>,</mml:mo>
</mml:math>
<label>(13)</label>
</disp-formula>where <italic>D</italic>(<italic>&#x3c3;</italic>) is the CSSS and <italic>&#x3c3;</italic> is the normal stress.</p>
<p>Eq. <xref ref-type="disp-formula" rid="e13">13</xref> is a formula with engineering application value, which can be used to calculate the corresponding CSSS when the normal stress changes. Given the normal stress, the corresponding CSSS can be calculated on the engineering site.</p>
</sec>
<sec id="s3-3-3">
<title>3.3.3 Relationship between CSS and normal stress</title>
<p>After substitution of the CSSS and normal stress values into Eq. <xref ref-type="disp-formula" rid="e5">5</xref>, the characteristic shear strength (CSS) of the structural plane is solved and listed in <xref ref-type="table" rid="T10">Table 10</xref>. Based on the results obtained in <xref ref-type="table" rid="T10">Table 10</xref>, CSS and normal stress were regressed, as shown in <xref ref-type="fig" rid="F9">Figure 9</xref>.</p>
<table-wrap id="T10" position="float">
<label>TABLE 10</label>
<caption>
<p>Relationships between CSS and normal stress.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="center">Normal stress (MPa)</th>
<th align="center">1</th>
<th align="center">2</th>
<th align="center">3</th>
<th align="center">4</th>
<th align="center">5</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">CSS/MPa</td>
<td align="center">7.349</td>
<td align="center">7.856</td>
<td align="center">9.078</td>
<td align="center">10.461</td>
<td align="center">11.931</td>
</tr>
</tbody>
</table>
</table-wrap>
<fig id="F9" position="float">
<label>FIGURE 9</label>
<caption>
<p>Fitting curve between CSS and normal stress.</p>
</caption>
<graphic xlink:href="feart-11-1116302-g009.tif"/>
</fig>
<p>
<xref ref-type="fig" rid="F9">Figure 9</xref> indicates a linear relationship between the CSS and normal stress. As the normal stress improves, the CSS gradually increases. Consequently, the relationship is derived as follows:<disp-formula id="e14">
<mml:math id="m24">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3c4;</mml:mi>
<mml:mi>w</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>5.804</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>1.177</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
<mml:mo>,</mml:mo>
</mml:math>
<label>(14)</label>
</disp-formula>where <italic>&#x3c4;</italic>
<sub>
<italic>w</italic>
</sub> is the CSS.</p>
<p>Eq. <xref ref-type="disp-formula" rid="e15">15</xref> is a valuable engineering formula that can calculate the corresponding CSS when the normal stress varies. When the normal stress is provided, the CSS can be determined.</p>
</sec>
</sec>
<sec id="s3-4">
<title>3.4 Experimental verification analysis</title>
<p>Experimental data from <xref ref-type="bibr" rid="B1">Chen et al. (2021</xref>) were used to verify and analyze the correctness of Eq. <xref ref-type="disp-formula" rid="e1">1</xref> and its applicability in engineering. <xref ref-type="bibr" rid="B1">Chen et al. (2021</xref>) also investigated the effect of various normal stresses on the SSSP for different sizes. As shown in <xref ref-type="table" rid="T11">Table 11</xref>, the normal stresses were 3, 4, 5, and 6&#xa0;MPa, with sizes of 50 &#xd7; 50&#xa0;mm, 75 &#xd7; 75&#xa0;mm, 100 &#xd7; 100&#xa0;mm, 125 &#xd7; 125&#xa0;mm, and 150 &#xd7; 150&#xa0;mm.</p>
<table-wrap id="T11" position="float">
<label>TABLE 11</label>
<caption>
<p>SSSP (<xref ref-type="bibr" rid="B1">Chen et al., 2021</xref>).</p>
</caption>
<table>
<thead valign="top">
<tr>
<th rowspan="2" align="center">Size/mm</th>
<th colspan="4" align="center">Normal stress (MPa)</th>
</tr>
<tr>
<th align="center">3</th>
<th align="center">4</th>
<th align="center">5</th>
<th align="center">6</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">50&#xd7;50</td>
<td align="center">0.72</td>
<td align="center">0.95</td>
<td align="center">1.12</td>
<td align="center">1.24</td>
</tr>
<tr>
<td align="center">75&#xd7;75</td>
<td align="center">0.49</td>
<td align="center">0.66</td>
<td align="center">0.71</td>
<td align="center">0.82</td>
</tr>
<tr>
<td align="center">100&#xd7;100</td>
<td align="center">0.48</td>
<td align="center">0.63</td>
<td align="center">0.67</td>
<td align="center">0.81</td>
</tr>
<tr>
<td align="center">125&#xd7;125</td>
<td align="center">0.44</td>
<td align="center">0.61</td>
<td align="center">0.63</td>
<td align="center">0.67</td>
</tr>
<tr>
<td align="center">150&#xd7;150</td>
<td align="center">0.29</td>
<td align="center">0.32</td>
<td align="center">0.34</td>
<td align="center">0.37</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>The SSSP under different normal stresses was chosen for verification based on the data in <xref ref-type="table" rid="T11">Table 11</xref> for the sizes 50 &#xd7; 50&#xa0;mm, 100 &#xd7; 100&#xa0;mm, and 150 &#xd7; 150&#xa0;mm. A scatter diagram of shear strength, normal stress, and their relationships, was plotted using OriginLab software, as shown in <xref ref-type="fig" rid="F10">Figure 10A</xref>. <xref ref-type="fig" rid="F10">Figure 10B</xref> shows a scatter diagram of the shear strength and size for the SSSP for normal stresses of 3 and 6&#xa0;MPa.</p>
<fig id="F10" position="float">
<label>FIGURE 10</label>
<caption>
<p>Fitting curves. <bold>(A)</bold> SSSP and normal stress. <bold>(B)</bold> SSSP and size.</p>
</caption>
<graphic xlink:href="feart-11-1116302-g010.tif"/>
</fig>
<p>
<xref ref-type="fig" rid="F10">Figure 10A</xref> demonstrates that the shear strength tended to rise as normal stress increased. Thus, the following relationship was obtained:<disp-formula id="e15">
<mml:math id="m25">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.229</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>0.173</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
<mml:mo>,</mml:mo>
</mml:math>
<label>(15)</label>
</disp-formula>
<disp-formula id="e16">
<mml:math id="m26">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>100</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.184</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>0.103</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
<mml:mo>,</mml:mo>
</mml:math>
<label>(16)</label>
</disp-formula>
<disp-formula id="e17">
<mml:math id="m27">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>150</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.213</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>0.026</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
<mml:mo>.</mml:mo>
</mml:math>
<label>(17)</label>
</disp-formula>
</p>
<p>
<xref ref-type="bibr" rid="B3">Gao (2020</xref>) (Page 28) addressed the changing trend of the shear strength of the structural plane in the normal stress range of 0.3&#x2013;0.8&#xa0;MPa by applying size effect analysis to different groups of test pieces. These relationships are shown in <xref ref-type="table" rid="T12">Table 12</xref>.</p>
<table-wrap id="T12" position="float">
<label>TABLE 12</label>
<caption>
<p>Fitting model between shear strengths of structural planes and sizes (<xref ref-type="bibr" rid="B3">Gao, 2020</xref>).</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="left">Size of the structure plane (mm)</th>
<th align="center">Fitting formula</th>
<th align="center">
<italic>R</italic>
<sup>2</sup>
</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">50</td>
<td align="left">
<inline-formula id="inf11">
<mml:math id="m28">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.2290</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>0.4325</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="left">0.980</td>
</tr>
<tr>
<td align="center">75</td>
<td align="left">
<inline-formula id="inf12">
<mml:math id="m29">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.2206</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>0.5843</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="left">0.955</td>
</tr>
<tr>
<td align="center">100</td>
<td align="left">
<inline-formula id="inf13">
<mml:math id="m30">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.1840</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>1.0300</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="left">0.960</td>
</tr>
<tr>
<td align="center">125</td>
<td align="left">
<inline-formula id="inf14">
<mml:math id="m31">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.2680</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>1.1094</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula>
</td>
<td align="left">0.995</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>The expressions in Eqs <xref ref-type="disp-formula" rid="e15">15</xref>&#x2013;<xref ref-type="disp-formula" rid="e17">17</xref> and <xref ref-type="table" rid="T12">Table 12</xref> are consistent with those proposed in Eq. <xref ref-type="disp-formula" rid="e1">1</xref>. Hence, the findings of the numerical simulations and experimental results in the present study agree. The relationship expression proposed in Eq. <xref ref-type="disp-formula" rid="e1">1</xref> is suitable for calculating the SSSP when the normal stress changes.</p>
<p>
<xref ref-type="fig" rid="F10">Figure 10B</xref> demonstrates that the SSSP decreases gradually as the size increases. Consequently, the following relationship is established:<disp-formula id="e18">
<mml:math id="m32">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>3</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.9798</mml:mn>
<mml:msup>
<mml:mi>e</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>l</mml:mi>
</mml:mrow>
<mml:mn>70.40</mml:mn>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:msup>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>0.22</mml:mn>
</mml:mrow>
<mml:mo>,</mml:mo>
</mml:math>
<label>(18)</label>
</disp-formula>
<disp-formula id="e19">
<mml:math id="m33">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>6</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>2.441</mml:mn>
<mml:msup>
<mml:mi>e</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>l</mml:mi>
</mml:mrow>
<mml:mn>195.69</mml:mn>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:msup>
<mml:mo>&#x2212;</mml:mo>
<mml:mn>0.706</mml:mn>
</mml:mrow>
<mml:mo>.</mml:mo>
</mml:math>
<label>(19)</label>
</disp-formula>
</p>
<p>Comparing Eq. <xref ref-type="disp-formula" rid="e18">18</xref> and Eq. <xref ref-type="disp-formula" rid="e19">19</xref> obtained by verifying Eq. <xref ref-type="disp-formula" rid="e5">5</xref> shows that Eq. <xref ref-type="disp-formula" rid="e16">16</xref> corresponds to Eq. <xref ref-type="disp-formula" rid="e5">5</xref>. Hence, the finding of the numerical simulations and experimental results in this study are consistent. The expressions proposed in Eq. <xref ref-type="disp-formula" rid="e16">16</xref> are suitable for calculating SSSP when the size changes.</p>
</sec>
</sec>
<sec sec-type="discussion" id="s4">
<title>4 Discussion</title>
<p>Under normal stress, SSSP exhibits a size effect. This study proposes a method to calculate the SSSP by combining numerical simulation and experimental verification. The conclusions are as follows:<list list-type="simple">
<list-item>
<p>1) The relationship between SSSP and normal stress is obtained by numerically simulating various normal stresses and analyzing the SSSP with normal stress. While previous studies have investigated the effect of normal stress on the SSSP using numerical simulations (<xref ref-type="bibr" rid="B2">Cheng, 2019</xref>) and field direct shear tests (<xref ref-type="bibr" rid="B22">Zhang et al., 2019</xref>), they did not consider the size. Eq. <xref ref-type="disp-formula" rid="e4">4</xref> quantifies and simplifies the solution of SSSP with normal stress and can calculate the corresponding SSSP when provided with the normal stresses.</p>
</list-item>
<list-item>
<p>2) The relationship between SSSP and size is derived utilizing the numerical simulation of different sizes by analyzing SSSP with size. While previous studies determined the regulation of the size impact of SSSP from the particle size (<xref ref-type="bibr" rid="B5">Islam et al., 2019</xref>) and cracks (<xref ref-type="bibr" rid="B7">Li et al., 2018</xref>), they did not consider normal stress. Eq. <xref ref-type="disp-formula" rid="e9">9</xref> quantifies the size effect of the SSSP and can compute the corresponding SSSP when provided with the sizes.</p>
</list-item>
<list-item>
<p>3) The relationship between CSSS, CSS, and normal stress is determined by analyzing the CSSS and CSS with normal stress change. While the REV of CSSS has been investigated (<xref ref-type="bibr" rid="B4">Hu et al., 2022</xref>), the exact CSSS formula for normal stress was not derived. Eqs <xref ref-type="disp-formula" rid="e13">13</xref> and <xref ref-type="disp-formula" rid="e14">14</xref> quantify and simplify the calculation of CSSS and CSS for rocks with normal stress. Hence, when the normal stress applied to the project is known, the CSSS and CSS can be computed.</p>
</list-item>
</list>
</p>
</sec>
<sec sec-type="conclusion" id="s5">
<title>5 Conclusion</title>
<p>This study investigated the impact of normal stress and size on the SSSP and analyzed the size effect of the SSSP for different sizes and normal stresses. The obtained formulas are as follows:<list list-type="simple">
<list-item>
<p>(1) The relationship between SSSP and normal stress is</p>
</list-item>
</list>
<disp-formula id="equ1">
<mml:math id="m34">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mi>c</mml:mi>
<mml:mo>&#x2b;</mml:mo>
<mml:mi>f</mml:mi>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
<mml:mo>.</mml:mo>
</mml:math>
</disp-formula>
</p>
<p>The parameters <italic>c</italic> and <italic>f</italic> were determined, and the formula is<disp-formula id="equ2">
<mml:math id="m35">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>28.928</mml:mn>
<mml:msup>
<mml:mi>e</mml:mi>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>l</mml:mi>
</mml:mrow>
<mml:mn>127.516</mml:mn>
</mml:mfrac>
</mml:msup>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>2.816</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>18.438</mml:mn>
<mml:msup>
<mml:mi>e</mml:mi>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>l</mml:mi>
</mml:mrow>
<mml:mn>79.234</mml:mn>
</mml:mfrac>
</mml:msup>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>1.273</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
<mml:mo>.</mml:mo>
</mml:math>
</disp-formula>
<list list-type="simple">
<list-item>
<p>(2) The relationship between SSSP and size is</p>
</list-item>
</list>
<disp-formula id="equ3">
<mml:math id="m36">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mi>h</mml:mi>
<mml:mo>&#x2b;</mml:mo>
<mml:mi>d</mml:mi>
<mml:msup>
<mml:mi>e</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>l</mml:mi>
</mml:mrow>
<mml:mi>g</mml:mi>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:msup>
</mml:mrow>
<mml:mo>.</mml:mo>
</mml:math>
</disp-formula>
</p>
<p>After calculating the parameters <italic>d</italic>, <italic>g</italic>, and <italic>h</italic>, the formula becomes<disp-formula id="equ4">
<mml:math id="m37">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>l</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>27.857</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>17.016</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:msup>
<mml:mi mathvariant="normal">e</mml:mi>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>l</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mn>190.925</mml:mn>
<mml:mi>e</mml:mi>
<mml:mfrac>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
<mml:mn>0.48</mml:mn>
</mml:mfrac>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>95.743</mml:mn>
</mml:mrow>
</mml:mfrac>
</mml:msup>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>2.851</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>1.312</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
<mml:mo>.</mml:mo>
</mml:math>
</disp-formula>
<list list-type="simple">
<list-item>
<p>(3) The CSS is relevant to normal stress; thus, the simulation provides the following specific form:</p>
</list-item>
</list>
<disp-formula id="equ5">
<mml:math id="m38">
<mml:mrow>
<mml:mi>D</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>300.594</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>12.918</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
<mml:mo>.</mml:mo>
</mml:math>
</disp-formula>
<list list-type="simple">
<list-item>
<p>(4) The CSSS is related to normal stress; thus, the simulation reveals the following specific form:</p>
</list-item>
</list>
<disp-formula id="equ6">
<mml:math id="m39">
<mml:mrow>
<mml:msub>
<mml:mi>&#x3c4;</mml:mi>
<mml:mi>w</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>5.804</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mn>1.177</mml:mn>
<mml:mi>&#x3c3;</mml:mi>
</mml:mrow>
<mml:mo>.</mml:mo>
</mml:math>
</disp-formula>
</p>
</sec>
</body>
<back>
<sec sec-type="data-availability" id="s6">
<title>Data availability statement</title>
<p>The original contributions presented in the study are included in the article/Supplementary Material, Further inquiries can be directed to the corresponding author.</p>
</sec>
<sec id="s7">
<title>Author contributions</title>
<p>YH: data curation, investigation, methodology, and writing and preparing the original draft. GH: conceptualization, investigation, and funding acquisition.</p>
</sec>
<sec id="s8">
<title>Funding</title>
<p>This work was supported by a project from the Key Laboratory of Rock Mechanics and Geohazards of Zhejiang Province (ZGRMG-2019-07).</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 a potential conflict 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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