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<article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" article-type="review-article">
<front>
<journal-meta>
<journal-id journal-id-type="publisher-id">Front. Built Environ.</journal-id>
<journal-title>Frontiers in Built Environment</journal-title>
<abbrev-journal-title abbrev-type="pubmed">Front. Built Environ.</abbrev-journal-title>
<issn pub-type="epub">2297-3362</issn>
<publisher>
<publisher-name>Frontiers Media S.A.</publisher-name>
</publisher>
</journal-meta>
<article-meta>
<article-id pub-id-type="doi">10.3389/fbuil.2019.00065</article-id>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Built Environment</subject>
<subj-group>
<subject>Review</subject>
</subj-group>
</subj-group>
</article-categories>
<title-group>
<article-title>Fatigue Assessment and Deterioration Effects on Masonry Elements: A Review of Numerical Models and Their Application to a Case Study</article-title>
</title-group>
<contrib-group>
<contrib contrib-type="author" corresp="yes">
<name><surname>Casamassima</surname> <given-names>Vito Michele</given-names></name>
<xref ref-type="corresp" rid="c001"><sup>&#x0002A;</sup></xref>
<uri xlink:href="http://loop.frontiersin.org/people/608473/overview"/>
</contrib>
<contrib contrib-type="author">
<name><surname>D&#x00027;Amato</surname> <given-names>Michele</given-names></name>
<uri xlink:href="http://loop.frontiersin.org/people/580450/overview"/>
</contrib>
</contrib-group>
<aff><institution>DICEM, Department of European and Mediterranean Cultures (Architecture, Environment and Cultural Heritage), University of Basilicata</institution>, <addr-line>Matera</addr-line>, <country>Italy</country></aff>
<author-notes>
<fn fn-type="edited-by"><p>Edited by: Hussam Mahmoud, Colorado State University, United States</p></fn>
<fn fn-type="edited-by"><p>Reviewed by: Siro Casolo, Politecnico di Milano, Italy; Michele Betti, University of Florence, Italy</p></fn>
<corresp id="c001">&#x0002A;Correspondence: Vito Michele Casamassima <email>vitomic.casam&#x00040;gmail.com</email></corresp>
<fn fn-type="other" id="fn001"><p>This article was submitted to Earthquake Engineering, a section of the journal Frontiers in Built Environment</p></fn></author-notes>
<pub-date pub-type="epub">
<day>21</day>
<month>05</month>
<year>2019</year>
</pub-date>
<pub-date pub-type="collection">
<year>2019</year>
</pub-date>
<volume>5</volume>
<elocation-id>65</elocation-id>
<history>
<date date-type="received">
<day>18</day>
<month>02</month>
<year>2019</year>
</date>
<date date-type="accepted">
<day>30</day>
<month>04</month>
<year>2019</year>
</date>
</history>
<permissions>
<copyright-statement>Copyright &#x000A9; 2019 Casamassima and D&#x00027;Amato.</copyright-statement>
<copyright-year>2019</copyright-year>
<copyright-holder>Casamassima and D&#x00027;Amato</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>Safety assessment with respect to seismic and vertical loads of existing and very old masonry structures is currently a central topic for the scientific engineering community. In particular, there are many ancient bridges still in service that are subjected to higher and more frequent cyclic loads. For these structures, it is important to determine the actual fatigue strength, rather than the ultimate carrying capacity. In this way the remaining service life, with possible traffic load limitations, may be estimated. This paper reports an updated review of the state-of-the art on recently published fatigue models that account for deterioration effects under cyclic loads. In addition, results related to fatigue performance of a bridge are shown and comments are provided. The numerical comparisons among existing fatigue models reveal that the application of the available fatigue models is particularly problematic for ancient masonry elements, where appropriate stress-life curves are required.</p></abstract>
<kwd-group>
<kwd>masonry</kwd>
<kwd>fatigue assessment</kwd>
<kwd>fatigue deterioration</kwd>
<kwd>residual service life</kwd>
<kwd>stress-life curves</kwd>
</kwd-group>
<counts>
<fig-count count="6"/>
<table-count count="4"/>
<equation-count count="18"/>
<ref-count count="45"/>
<page-count count="10"/>
<word-count count="6180"/>
</counts>
</article-meta>
</front>
<body>
<sec sec-type="intro" id="s1">
<title>Introduction</title>
<p>To date, there have been conspicuous advances in simulating the response of ancient masonry structures, mainly with the aim of determining the ultimate vertical loads and capacity with respect the lateral seismic actions. For example, among other studies, modeling criteria for ancient bridges may be found in Laterza et al. (<xref ref-type="bibr" rid="B28">2017b</xref>) and D&#x00027;Amato et al. (<xref ref-type="bibr" rid="B14">2017</xref>), while for ancient churches they are reported in Pel&#x000E0; et al. (<xref ref-type="bibr" rid="B36">2009</xref>); Formisano and Marzo (<xref ref-type="bibr" rid="B18">2017</xref>); Betti et al. (<xref ref-type="bibr" rid="B5">2018</xref>); D&#x00027;Amato et al. (<xref ref-type="bibr" rid="B15">2018</xref>), Formisano et al. (<xref ref-type="bibr" rid="B19">2018</xref>); Fuentes et al. (<xref ref-type="bibr" rid="B20">2019</xref>); Ramirez et al. (<xref ref-type="bibr" rid="B37">2019</xref>), and Lopez et al. (<xref ref-type="bibr" rid="B29">2019</xref>), and they are discussed for towers in Shakya et al. (<xref ref-type="bibr" rid="B42">2016</xref>); Bartoli et al. (<xref ref-type="bibr" rid="B3">2018</xref>) and Sarhosis et al. (<xref ref-type="bibr" rid="B40">2018</xref>). Models of general historical buildings are discussed in Caprili et al. (<xref ref-type="bibr" rid="B9">2017</xref>) and Milani et al. (<xref ref-type="bibr" rid="B33">2018</xref>), while detailed study on <italic>in-situ</italic> tests may be found, among the others, in Krstevska et al. (<xref ref-type="bibr" rid="B26">2010</xref>); Bartoli et al. (<xref ref-type="bibr" rid="B4">2013</xref>), and Luchin et al. (<xref ref-type="bibr" rid="B30">2018</xref>).</p>
<p>Nowadays, the study of ancient masonry structures&#x00027; responses is a relevant topic since most of them are still in service without any kind of limitation.</p>
<p>By contrast, in the scientific community there is not yet the same level of interest for a correct understanding of fatigue effects and the prediction of the remaining service life of masonry elements under cyclic compressive loads. Among ancient masonry structures, it is known that arch bridges are affected by fatigue problems. This is due to the fact that they are currently subjected to higher and more frequent cyclic loads due to population growth, resulting in premature cracking and deterioration. As such, the available fatigue strength, that is the maximum stress acting in cyclic conditions, is significantly lower than the one obtained under quasi static loading conditions. Therefore, rather than the ultimate carrying capacity, it is important to know the actual fatigue strength, starting from which useful indications on the remaining service life with a possible traffic load limitation may be established. Moreover, the deterioration of materials and cyclic action may accelerate masonry deterioration and reduce carrying capacity. Clark (<xref ref-type="bibr" rid="B12">1994</xref>) and Roberts et al. (<xref ref-type="bibr" rid="B38">2006</xref>) performed cyclic tests on brick masonry columns and concluded that the stress limit of dry specimens was about 50% of the static compressive strength, whereas Choo and Hogg (<xref ref-type="bibr" rid="B11">1995</xref>) and Schueremans and Van Gemert (<xref ref-type="bibr" rid="B41">2001</xref>) instead suggested limiting the applied load to &#x0003C; 50% of the ultimate vertical load. Furthermore, in Melbourne et al. (<xref ref-type="bibr" rid="B31">2004</xref>) the cyclic vertical load capacity of multi-ring masonry arches varied between 37 and 57% of the static load carrying capacity. This significant reduction was due to a separation of rings, which was provoked by a shear failure mode among bricks and mortar joints instead of a four-hinge failure mechanism. Finally, in Melbourne et al. (<xref ref-type="bibr" rid="B32">2007</xref>), a unitary assessment procedure (named <italic>SMART</italic> procedure) was proposed for evaluating fatigue performance of masonry arches, involving the application of the fatigue model reported in Roberts et al. (<xref ref-type="bibr" rid="B38">2006</xref>).</p>
<p>Stress-life curves for masonry elements, indicated as <italic>S-N</italic> curves, are usually established in a limited number of experimental tests and, very often, are not adequate to reproduce the elements of ancient masonry. Moreover, in many of the actual design codes&#x02014;among which are (<xref ref-type="bibr" rid="B34">Ministerial Decree D.M. 14/01/2008 (NTC-08)</xref>, <xref ref-type="bibr" rid="B34">2008</xref>), with the related (Italian Design Code Instructions (NTC-08 Instructions), <xref ref-type="bibr" rid="B22">2009</xref>), and Eurocode 3 (EC3, <xref ref-type="bibr" rid="B17">2003</xref>)&#x02014;appropriate indications for evaluating the fatigue strength of masonry elements are still missing, contrarily to steel elements. Nevertheless, as highlighted from laboratory tests carried out on prototype models cast in a reduced scale, cycling loads related to in-service conditions may provoke fatigue failure for a vertical load significantly lower than the one related to the ultimate condition (Melbourne et al., <xref ref-type="bibr" rid="B31">2004</xref>).</p>
<p>In this study, an updated review is provided for the main stress-life curve models available in the literature for estimating the fatigue strength of masonry elements. In particular, the models proposed by Ronca et al. (<xref ref-type="bibr" rid="B39">2004</xref>), Roberts et al. (<xref ref-type="bibr" rid="B38">2006</xref>), Casas (<xref ref-type="bibr" rid="B10">2009</xref>), Tomor and Verstrynge (<xref ref-type="bibr" rid="B43">2013</xref>), and Koltsida et al. (<xref ref-type="bibr" rid="B24">2018a</xref>) are considered. At first, they are separately described and shown. Then, the considered models are applied to a case study, an ancient masonry arch bridge. In particular, the main arch fatigue strength is assessed by considering the numerical simulations for repeated vertical loads reported in a previous study (Laterza et al., <xref ref-type="bibr" rid="B27">2017a</xref>).</p></sec>
<sec id="s2">
<title>Models to predict the Masonry Fatigue Life Under Compressive Loading</title>
<sec>
<title>Ronca et al. (2004)</title>
<p>Ronca et al. (<xref ref-type="bibr" rid="B39">2004</xref>) conducted, in accordance with BS EN998-2 (<xref ref-type="bibr" rid="B7">2003</xref>), a series of tests applying repeated vertical loads on masonry specimens that contained M4 mortar, with an average strength in compression of 48.86 N/mm<sup>2</sup> and an average ultimate strength in compression ranged between 10 and 13 MPa. The tests were performed in order to evaluate the role of loading rate on material response, with the aim of deriving a fatigue model in terms of <italic>S-N</italic> curves. In the tests, the specimens were subjected to heavy sustained loads with small perturbations, mostly due to environmental conditions (for example traffic vibrations and thermal excursion, among others). The brickwork prisms were tested under very high vertical loads applied axially (65&#x02013;80% of the ultimate compressive strength) and by imposing a small variation of the alternating loads with three different frequencies: 1, 5, and 10 Hz.</p>
<p><xref ref-type="table" rid="T1">Table 1</xref> summarizes the ratios <italic>S</italic><sub><italic>min</italic></sub><italic>/S</italic><sub><italic>max</italic></sub>, and <italic>S</italic><sub><italic>a</italic></sub><italic>/S</italic><sub><italic>u</italic></sub> reached in each test, where <italic>S</italic><sub><italic>a</italic></sub> is the stress induced with the alternating load (in absolute value); <italic>S</italic><sub><italic>u</italic></sub> is the compressive strength of the investigated masonry; <italic>S</italic><sub><italic>max</italic></sub> and <italic>S</italic><sub><italic>min</italic></sub> are the maximum and the minimum stresses induced during the cycle, respectively; <italic>R</italic> is a parameter given by the ratio of <italic>S</italic><sub><italic>min</italic></sub> to <italic>S</italic><sub><italic>max</italic></sub>; while <italic>S</italic> is the ratio of <italic>S</italic><sub><italic>max</italic></sub> to <italic>S</italic><sub><italic>u</italic></sub>, measuring how far the maximum stress is cyclically induced from the monotonic masonry compressive strength. In particular, during the tests the <italic>R</italic> ratio ranged from 0.73 to 0.88, while the <italic>S</italic> ratio ranged from 0.7 to 0.90. <xref ref-type="fig" rid="F1">Figure 1</xref> shows, in the semi-logarithmic plane <italic>logN</italic>-<italic>S</italic><sub><italic>a</italic></sub><italic>/S</italic><sub><italic>u</italic></sub>, the experimental values obtained from each test together with the stress-life curves proposed by the same authors. It is important to note that fatigue strength increases as the number of cycles, <italic>N</italic>, decreases.</p>
<table-wrap position="float" id="T1">
<label>Table 1</label>
<caption><p>Tests results obtained by Ronca et al. (<xref ref-type="bibr" rid="B39">2004</xref>).</p></caption>
<table frame="hsides" rules="groups">
<thead><tr>
<th valign="top" align="left"><bold>Number of samples</bold></th>
<th valign="top" align="left"><bold>f (Hz)</bold></th>
<th valign="top" align="left"><bold>Sa/Su</bold></th>
<th valign="top" align="left"><bold>R&#x0003D;Smin/Smax</bold></th>
<th valign="top" align="left"><bold>S &#x0003D; Smax/Su</bold></th>
</tr>
</thead>
<tbody>
<tr>
<td valign="top" align="left">3</td>
<td valign="top" align="left">1</td>
<td valign="top" align="left">0.1</td>
<td valign="top" align="left">0.78</td>
<td valign="top" align="left">0.90</td>
</tr>
<tr>
<td valign="top" align="left">3</td>
<td valign="top" align="left">1</td>
<td valign="top" align="left">0.075</td>
<td valign="top" align="left">0.83</td>
<td valign="top" align="left">0.88</td>
</tr>
<tr>
<td valign="top" align="left">3</td>
<td valign="top" align="left">1</td>
<td valign="top" align="left">0.05</td>
<td valign="top" align="left">0.88</td>
<td valign="top" align="left">0.85</td>
</tr>
<tr>
<td valign="top" align="left">1</td>
<td valign="top" align="left">1</td>
<td valign="top" align="left">0.1</td>
<td valign="top" align="left">0.73</td>
<td valign="top" align="left">0.75</td>
</tr>
<tr>
<td valign="top" align="left">2</td>
<td valign="top" align="left">5</td>
<td valign="top" align="left">0.1</td>
<td valign="top" align="left">0.73</td>
<td valign="top" align="left">0.75</td>
</tr>
<tr>
<td valign="top" align="left">1</td>
<td valign="top" align="left">10</td>
<td valign="top" align="left">0.05</td>
<td valign="top" align="left">0.86</td>
<td valign="top" align="left">0.70</td>
</tr>
</tbody>
</table>
</table-wrap>
<fig id="F1" position="float">
<label>Figure 1</label>
<caption><p>Ronca et al. (<xref ref-type="bibr" rid="B39">2004</xref>) fatigue curves: experimental data obtained.</p></caption>
<graphic xlink:href="fbuil-05-00065-g0001.tif"/>
</fig></sec>
<sec>
<title>Roberts et al. (2006)</title>
<p>Roberts et al. (<xref ref-type="bibr" rid="B38">2006</xref>) conducted experimental tests on different types of masonry prisms considering also different levels of water saturation degree. Starting from the obtained results, Equation (1) was proposed, representing a lower bound for the fatigue strength:</p>
<disp-formula id="E1"><label>(1)</label><mml:math id="M1"><mml:mtable class="eqnarray" columnalign="right center left"><mml:mtr><mml:mtd><mml:mrow><mml:mi>F</mml:mi><mml:mo stretchy='false'>(</mml:mo><mml:mi>S</mml:mi><mml:mo stretchy='false'>)</mml:mo><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:msup><mml:mrow><mml:mo stretchy='false'>(</mml:mo><mml:mo>&#x00394;</mml:mo><mml:mtext>&#x000A0;</mml:mtext><mml:mi>S</mml:mi><mml:mi>S</mml:mi><mml:mi>m</mml:mi><mml:mi>a</mml:mi><mml:mi>x</mml:mi><mml:mo stretchy='false'>)</mml:mo></mml:mrow><mml:mrow><mml:mn>0</mml:mn><mml:mo>,</mml:mo><mml:mn>5</mml:mn></mml:mrow></mml:msup></mml:mrow><mml:mrow><mml:mi>S</mml:mi><mml:mi>u</mml:mi></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mn>0.7</mml:mn><mml:mo>&#x02212;</mml:mo><mml:mn>0.05</mml:mn><mml:mi>l</mml:mi><mml:mi>o</mml:mi><mml:mi>g</mml:mi><mml:mi>N</mml:mi></mml:mrow></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<p>where <italic>F(S)</italic> is the function of the induced stress range, <italic>S</italic><sub><italic>max</italic></sub> is the maximum stress amplitude, &#x00394;<italic>S</italic> is the difference between <italic>S</italic><sub><italic>max</italic></sub> and <italic>S</italic><sub><italic>min</italic></sub>, <italic>S</italic><sub><italic>u</italic></sub> is the compressive strength and <italic>N</italic> is the number of cycles to failure.</p>
<p>Three types of specimens were tested for simulating more closely the masonry arch barrels, while considering both dry and saturated conditions. A vertical load eccentricity ratio <italic>e/d</italic> ranging from 0 to 0.256 (where <italic>e</italic> is the vertical load eccentricity and <italic>d</italic> the specimen depth) was applied. The load frequency was kept constant to 5 Hz until failure. The test series indicated that the high cycle fatigue strength of wet and submerged brick masonry specimens was only slightly less than that of dry specimens. The mortar was mixed in order to reproduce the representative mortar used for ancient brick masonry arches. It was shown that the compressive strength measured at 28 days ranged between 0.45 MPa and 2.78 MPa. The masonry compressive strength, determined by assuming a linear stress distribution along the specimens, varied between 6 and 14 MPa.</p>
<p>By introducing in Equation (1) the stress ratio <italic>R</italic> &#x0003D; <italic>S</italic><sub><italic>min</italic></sub><italic>/S</italic><sub><italic>max</italic></sub>, and substituting &#x00394;<italic>S</italic> for the difference <italic>S</italic><sub><italic>max</italic></sub>-<italic>S</italic><sub><italic>min</italic></sub>, the formulation proposed by Roberts et al. (<xref ref-type="bibr" rid="B38">2006</xref>) may be rewritten in the familiar form of stress-life curve <italic>logN- S</italic><sub><italic>max</italic></sub><italic>/S</italic><sub><italic>u</italic></sub> as follows:</p>
<disp-formula id="E2"><label>(2)</label><mml:math id="M2"><mml:mtable class="eqnarray" columnalign="right center left"><mml:mtr><mml:mtd><mml:mi>S</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mi>S</mml:mi><mml:mi>m</mml:mi><mml:mi>a</mml:mi><mml:mi>x</mml:mi></mml:mrow><mml:mrow><mml:mi>S</mml:mi><mml:mi>u</mml:mi></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mn>1</mml:mn><mml:mo>-</mml:mo><mml:mn>0</mml:mn><mml:mo>.</mml:mo><mml:mn>05</mml:mn><mml:mi>l</mml:mi><mml:mi>o</mml:mi><mml:mi>g</mml:mi><mml:mi>N</mml:mi></mml:mrow><mml:mrow><mml:msqrt><mml:mrow><mml:mn>1</mml:mn><mml:mo>-</mml:mo><mml:mi>R</mml:mi></mml:mrow></mml:msqrt></mml:mrow></mml:mfrac></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<p>In Equation (2), the fatigue strength <italic>S</italic> depends only on the imposed number of cycles <italic>N</italic> and on the amplitude of the induced stresses range <italic>R</italic> (the lower the <italic>R</italic> ratio the higher the interval amplitude of stresses).</p></sec>
<sec>
<title>Casas (2009)</title>
<p>Based on the test results from Roberts et al. (<xref ref-type="bibr" rid="B38">2006</xref>) , Casas (<xref ref-type="bibr" rid="B10">2009</xref>) post-processed the experimental results using a probabilistic approach. A new stress life curve for different survival probability levels was proposed for masonry under compressive loading, in accordance with Equation (3):</p>
<disp-formula id="E3"><label>(3)</label><mml:math id="M3"><mml:mtable class="eqnarray" columnalign="right center left"><mml:mtr><mml:mtd><mml:mi>S</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mi>S</mml:mi><mml:mi>m</mml:mi><mml:mi>a</mml:mi><mml:mi>x</mml:mi></mml:mrow><mml:mrow><mml:mi>S</mml:mi><mml:mi>u</mml:mi></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mi>A</mml:mi><mml:msup><mml:mrow><mml:mi>N</mml:mi></mml:mrow><mml:mrow><mml:mo>-</mml:mo><mml:mi>B</mml:mi><mml:mrow><mml:mo stretchy="false">(</mml:mo><mml:mrow><mml:mn>1</mml:mn><mml:mo>-</mml:mo><mml:mi>R</mml:mi></mml:mrow><mml:mo stretchy="false">)</mml:mo></mml:mrow></mml:mrow></mml:msup></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<p>where <italic>N</italic> is the number of cycles to failure, <italic>R</italic> &#x0003D; <italic>S</italic><sub><italic>min</italic></sub><italic>/S</italic><sub><italic>max</italic></sub> is the ratio between minimum and maximum induced stresses, and <italic>S</italic> &#x0003D; <italic>S</italic><sub><italic>max</italic></sub><italic>/S</italic><sub><italic>u</italic></sub> is the ratio between the maximum induced stress and compressive strength of the masonry. The coefficients <italic>A</italic> and <italic>B</italic> are reported in <xref ref-type="table" rid="T2">Table 2</xref>, defined as a function of the survival probability levels, while <xref ref-type="fig" rid="F2">Figure 2</xref> shows the stress-life curves obtained with Equation (3) by varying the stress ratio <italic>R</italic> from 0 to 0.9.</p>
<table-wrap position="float" id="T2">
<label>Table 2</label>
<caption><p>Casas (<xref ref-type="bibr" rid="B10">2009</xref>) coefficients for different values of survival probability (Pb).</p></caption>
<table frame="hsides" rules="groups">
<thead><tr>
<th valign="top" align="left"><bold>Pb</bold></th>
<th valign="top" align="left"><bold>0.95</bold></th>
<th valign="top" align="left"><bold>0.90</bold></th>
<th valign="top" align="left"><bold>0.80</bold></th>
<th valign="top" align="left"><bold>0.70</bold></th>
<th valign="top" align="left"><bold>0.60</bold></th>
<th valign="top" align="left"><bold>0.50</bold></th>
</tr>
</thead>
<tbody>
<tr>
<td valign="top" align="left">A</td>
<td valign="top" align="left">1.106</td>
<td valign="top" align="left">1.303</td>
<td valign="top" align="left">1.458</td>
<td valign="top" align="left">1.494</td>
<td valign="top" align="left">1.487</td>
<td valign="top" align="left">1.464</td>
</tr>
<tr>
<td valign="top" align="left">B</td>
<td valign="top" align="left">0.0998</td>
<td valign="top" align="left">0.110</td>
<td valign="top" align="left">0.109</td>
<td valign="top" align="left">0.102</td>
<td valign="top" align="left">0.094</td>
<td valign="top" align="left">0.087</td>
</tr>
</tbody>
</table>
</table-wrap>
<fig id="F2" position="float">
<label>Figure 2</label>
<caption><p>Casas (<xref ref-type="bibr" rid="B10">2009</xref>) fatigue curves, referred to a 5% of failure probability.</p></caption>
<graphic xlink:href="fbuil-05-00065-g0002.tif"/>
</fig>
<p>Starting from the Casas (<xref ref-type="bibr" rid="B10">2009</xref>) formulation, Tomor and Verstrynge (<xref ref-type="bibr" rid="B43">2013</xref>) proposed a probabilistic fatigue model, introducing the correction coefficient <italic>C</italic> set equal to 0.62 for accounting for the joined fatigue and creep deterioration simultaneously. In this model the material deterioration due to fatigue damage is more relevant for lower stress, while the creep effects dominate the cyclic response at higher stresses. In accordance with this work, Equation (4) was proposed, where the values of <italic>A</italic> and <italic>B</italic> are equal to 1 and 0.04, respectively:</p>
<disp-formula id="E4"><label>(4)</label><mml:math id="M4"><mml:mtable class="eqnarray" columnalign="right center left"><mml:mtr><mml:mtd><mml:mi>S</mml:mi><mml:mi>m</mml:mi><mml:mi>a</mml:mi><mml:mi>x</mml:mi><mml:mo>=</mml:mo><mml:mi>A</mml:mi><mml:msup><mml:mrow><mml:mi>N</mml:mi></mml:mrow><mml:mrow><mml:mo>-</mml:mo><mml:mi>B</mml:mi><mml:mrow><mml:mo stretchy="false">(</mml:mo><mml:mrow><mml:mn>1</mml:mn><mml:mo>-</mml:mo><mml:mi>C</mml:mi><mml:mi>R</mml:mi></mml:mrow><mml:mo stretchy="false">)</mml:mo></mml:mrow></mml:mrow></mml:msup></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<p>For completeness, <xref ref-type="fig" rid="F3">Figure 3</xref> illustrates a series of fatigue curves obtained according to the model proposed by Tomor and Verstrynge (<xref ref-type="bibr" rid="B43">2013</xref>) by considering 5% of failure probability.</p>
<fig id="F3" position="float">
<label>Figure 3</label>
<caption><p>Tomor and Verstrynge (<xref ref-type="bibr" rid="B43">2013</xref>) fatigue curves, referred to a 5% of failure probability.</p></caption>
<graphic xlink:href="fbuil-05-00065-g0003.tif"/>
</fig></sec>
<sec>
<title>Koltsida et al. (2018a)</title>
<p>In order to develop new stress life curves for masonry under compressive loading, Koltsida et al. (<xref ref-type="bibr" rid="B24">2018a</xref>) performed a series of experimental fatigue tests on low-strength masonry prisms under compressive cyclic load, proposing stress-life curves for different values of survival probability. They tested 64 brick full-size masonry prisms according to ASTM (<xref ref-type="bibr" rid="B2">2014</xref>) . Static and cyclic tests were performed with a frequency of 2 Hz. The tests showed an average compressive strength of 4.86 MPa for bricks and of 2.94 MPa for the masonry. The minimum induced stress during the tests was set to 10% of the masonry compressive strength, while the maximum induced stress ranged between 55 and 80%. The limit on the number of cycles up to failure was fixed as 10<sup>7</sup>. For a given survival probability <italic>L</italic>, the fatigue curve may be described as follows (Koltsida et al., <xref ref-type="bibr" rid="B24">2018a</xref>):</p>
<disp-formula id="E5"><label>(5)</label><mml:math id="M5"><mml:mrow><mml:mtable><mml:mtr><mml:mtd><mml:mrow><mml:mi>L</mml:mi><mml:mo>=</mml:mo><mml:msup><mml:mrow><mml:mn>10</mml:mn></mml:mrow><mml:mrow><mml:mo>&#x02212;</mml:mo><mml:mn>0.1127</mml:mn><mml:msup><mml:mrow><mml:mo stretchy='false'>(</mml:mo><mml:mi>S</mml:mi><mml:mi>m</mml:mi><mml:mi>a</mml:mi><mml:mi>x</mml:mi><mml:mtext>&#x000A0;</mml:mtext><mml:mo>&#x00394;</mml:mo><mml:mi>S</mml:mi><mml:mo stretchy='false'>)</mml:mo></mml:mrow><mml:mrow><mml:mn>3.9252</mml:mn></mml:mrow></mml:msup><mml:msup><mml:mrow><mml:mo stretchy='false'>(</mml:mo><mml:mi>l</mml:mi><mml:mi>o</mml:mi><mml:mi>g</mml:mi><mml:mi>N</mml:mi><mml:mi>f</mml:mi><mml:mo stretchy='false'>)</mml:mo></mml:mrow><mml:mrow><mml:mn>3.8322</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:msup></mml:mrow></mml:mtd></mml:mtr></mml:mtable></mml:mrow></mml:math></disp-formula>
<p>In <xref ref-type="fig" rid="F4">Figure 4</xref>, Equation 5 is reported by considering different values of R ratios, assuming L &#x0003D; 0.05 (i.e., by assuming a 5% failure probability).</p>
<fig id="F4" position="float">
<label>Figure 4</label>
<caption><p>Koltsida et al. (<xref ref-type="bibr" rid="B24">2018a</xref>) fatigue curves, referred to a 5% of failure probability.</p></caption>
<graphic xlink:href="fbuil-05-00065-g0004.tif"/>
</fig></sec></sec>
<sec id="s3">
<title>Deterioration of the Elastic Modulus in Masonry Elements Under Compressive Loads</title>
<p>Koltsida et al. (<xref ref-type="bibr" rid="B25">2018b</xref>) investigated deterioration of the elastic modulus of masonry during compressive cyclic loading. This study was conducted starting from similar studies regarding concrete specimens, as reported in Crumley and Kennedy (<xref ref-type="bibr" rid="B13">1977</xref>); Holmen (<xref ref-type="bibr" rid="B21">1982</xref>); Cachim et al. (<xref ref-type="bibr" rid="B8">2002</xref>); Mu and Shah (<xref ref-type="bibr" rid="B35">2005</xref>); Breitenbucher and Ibuk (<xref ref-type="bibr" rid="B6">2006</xref>); Zanuy et al. (<xref ref-type="bibr" rid="B45">2011</xref>);Vicente et al. (<xref ref-type="bibr" rid="B44">2014</xref>).</p>
<p>Specifically, Crumley and Kennedy (<xref ref-type="bibr" rid="B13">1977</xref>) in their tests concluded that the elastic modulus decreased by about 40% over the concrete usable life, and that a remarkable reduction of elastic modulus arose often at 75% of the fatigue life. In Holmen (<xref ref-type="bibr" rid="B21">1982</xref>) the elastic modulus of concrete cylinders consisted of three different phases: a first rapid decrease from 0 to about 10% of the number of failure cycles, a constant decrease from 10 up to 80% of the number of failure cycles, and then a sudden decrease until the specimen&#x00027;s fatigue failure. These reductions resulted from increasing the number of cycles up to the failure. In addition, during the performed tests it was found that the absorbed energy at failure was the same for static and fatigue loads with different intensities. Mu and Shah (<xref ref-type="bibr" rid="B35">2005</xref>) performed experimental fatigue tests on the concrete cylinders to evaluate the damage evolution in the case of biaxial fatigue loading, compression and torsion. The results showed that the evolution of cracks in the material may be divided into two phases: the first phase was characterized by a deceleration of the crack, and the second one by a sudden acceleration. The authors proposed the following relationship:</p>
<disp-formula id="E6"><label>(6)</label><mml:math id="M6"><mml:mtable class="eqnarray" columnalign="right center left"><mml:mtr><mml:mtd><mml:mo class="qopname">log</mml:mo><mml:mrow><mml:mo stretchy="false">(</mml:mo><mml:mrow><mml:mi>N</mml:mi><mml:mi>f</mml:mi></mml:mrow><mml:mo stretchy="false">)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:mo>-</mml:mo><mml:mn>0</mml:mn><mml:mo>.</mml:mo><mml:mn>82</mml:mn><mml:mo>&#x000B7;</mml:mo><mml:mo class="qopname">log</mml:mo><mml:mrow><mml:mo stretchy="true">(</mml:mo><mml:mrow><mml:mfrac><mml:mrow><mml:mi>d</mml:mi><mml:mi>k</mml:mi></mml:mrow><mml:mrow><mml:mi>d</mml:mi><mml:mi>N</mml:mi></mml:mrow></mml:mfrac></mml:mrow><mml:mo stretchy="true">)</mml:mo></mml:mrow><mml:mo>&#x0002B;</mml:mo><mml:mn>2</mml:mn><mml:mo>.</mml:mo><mml:mn>8</mml:mn></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<p>where <italic>k, N</italic> and <italic>N</italic><sub><italic>f</italic></sub> are the elastic modulus, cycle and fatigue life, respectively. It should be noted that this relationship is independent of the fatigue load range. A different approach for predicting the elastic modulus of concrete under repeated compressive loads was proposed by Zanuy et al. (<xref ref-type="bibr" rid="B45">2011</xref>). In accordance with this model, the maximum strain (&#x003B5;<sub><italic>max</italic></sub>) and the elastic modulus (<italic>E</italic>) were directly related to the number of cycles:</p>
<disp-formula id="E7"><label>(7)</label><mml:math id="M7"><mml:mtable class="eqnarray" columnalign="right center left"><mml:mtr><mml:mtd><mml:msub><mml:mrow><mml:mi>&#x003B5;</mml:mi></mml:mrow><mml:mrow><mml:mo class="qopname">max</mml:mo></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mrow><mml:mi>&#x003B5;</mml:mi></mml:mrow><mml:mrow><mml:mo class="qopname">max</mml:mo></mml:mrow></mml:msub><mml:mrow><mml:mo stretchy="false">(</mml:mo><mml:mrow><mml:mfrac><mml:mrow><mml:mi>N</mml:mi></mml:mrow><mml:mrow><mml:mi>N</mml:mi><mml:mi>f</mml:mi></mml:mrow></mml:mfrac></mml:mrow><mml:mo stretchy="false">)</mml:mo></mml:mrow></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<disp-formula id="E8"><label>(8)</label><mml:math id="M8"><mml:mtable class="eqnarray" columnalign="right center left"><mml:mtr><mml:mtd><mml:mi>E</mml:mi><mml:mo>=</mml:mo><mml:mi>E</mml:mi><mml:mrow><mml:mo stretchy="false">(</mml:mo><mml:mrow><mml:mfrac><mml:mrow><mml:mi>N</mml:mi></mml:mrow><mml:mrow><mml:mi>N</mml:mi><mml:mi>f</mml:mi></mml:mrow></mml:mfrac></mml:mrow><mml:mo stretchy="false">)</mml:mo></mml:mrow></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<p>The deterioration influence on Equation (7) and Equation (8) depends on the maximum and the minimum stresses (&#x003C3;<sub><italic>max</italic></sub><italic>/f</italic><sub><italic>c</italic></sub>, &#x003C3;<sub><italic>min</italic></sub><italic>/f</italic><sub><italic>c</italic></sub>). In particular, the authors defined three different deterioration stages. In Stage 1, concrete deterioration was due to micro-cracks forming at the aggregate-paste interface. This stage covered approximately 10&#x02013;15% of the fatigue life. In Stage 2, micro-cracks grew steadily, with a constant reduction of the elastic modulus. This stage covered about 80&#x02013;90% of the fatigue life. In Stage 3, micro-cracks converged to form a macro-crack causing specimen failure. The expressions proposed to determine elastic modulus in the transition from Stage 1 to Stage 2 and the rate of modulus decline in fatigue Stage 2 were as follows (Zanuy et al., <xref ref-type="bibr" rid="B45">2011</xref>):</p>
<disp-formula id="E9"><label>(9)</label><mml:math id="M10"><mml:mtable columnalign='left'><mml:mtr><mml:mtd><mml:mi>E</mml:mi><mml:mo>=</mml:mo><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mi>N</mml:mi><mml:mo>=</mml:mo><mml:mn>0.1</mml:mn><mml:mi>N</mml:mi><mml:mi>f</mml:mi></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:mtext>&#x000A0;</mml:mtext><mml:mrow><mml:mo>[</mml:mo><mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mn>0.09</mml:mn><mml:mo>+</mml:mo><mml:mn>8.19</mml:mn><mml:mo>+</mml:mo><mml:mfrac><mml:mrow><mml:mi>&#x003C3;</mml:mi><mml:mi>m</mml:mi><mml:mi>i</mml:mi><mml:mi>n</mml:mi></mml:mrow><mml:mrow><mml:mi>f</mml:mi><mml:mi>c</mml:mi></mml:mrow></mml:mfrac></mml:mrow><mml:mo>)</mml:mo></mml:mrow></mml:mrow></mml:mrow><mml:mtext>&#x000A0;</mml:mtext></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mrow><mml:mrow><mml:mtext>&#x000A0;&#x000A0;&#x000A0;&#x000A0;&#x000A0;&#x000A0;&#x000A0;&#x000A0;&#x000A0;&#x000A0;&#x000A0;&#x000A0;&#x000A0;&#x000A0;&#x000A0;&#x000A0;&#x000A0;</mml:mtext><mml:mo>+</mml:mo><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mn>0.84</mml:mn><mml:mo>+</mml:mo><mml:mn>8.19</mml:mn><mml:mfrac><mml:mrow><mml:mi>&#x003C3;</mml:mi><mml:mi>m</mml:mi><mml:mi>i</mml:mi><mml:mi>n</mml:mi></mml:mrow><mml:mrow><mml:mi>f</mml:mi><mml:mi>c</mml:mi></mml:mrow></mml:mfrac></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mfrac><mml:mrow><mml:mi>&#x003C3;</mml:mi><mml:mi>m</mml:mi><mml:mi>a</mml:mi><mml:mi>x</mml:mi></mml:mrow><mml:mrow><mml:mi>f</mml:mi><mml:mi>c</mml:mi></mml:mrow></mml:mfrac></mml:mrow><mml:mo>]</mml:mo></mml:mrow><mml:mi>E</mml:mi><mml:mi>c</mml:mi><mml:mo>&#x02264;</mml:mo><mml:mn>0.93</mml:mn><mml:mi>E</mml:mi><mml:mi>c</mml:mi></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<disp-formula id="E10"><label>(10)</label><mml:math id="M11"><mml:mtable class="eqnarray" columnalign="right center left"><mml:mtr><mml:mtd><mml:mfrac><mml:mrow><mml:mi>d</mml:mi><mml:mi>E</mml:mi></mml:mrow><mml:mrow><mml:mi>d</mml:mi><mml:mrow><mml:mo stretchy="false">(</mml:mo><mml:mrow><mml:mfrac><mml:mrow><mml:mi>N</mml:mi></mml:mrow><mml:mrow><mml:mi>N</mml:mi><mml:mi>f</mml:mi></mml:mrow></mml:mfrac></mml:mrow><mml:mo stretchy="false">)</mml:mo></mml:mrow></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mrow><mml:mo stretchy="true">(</mml:mo><mml:mrow><mml:mn>0</mml:mn><mml:mo>.</mml:mo><mml:mn>1</mml:mn><mml:mo>&#x0003C;</mml:mo><mml:mfrac><mml:mrow><mml:mi>N</mml:mi></mml:mrow><mml:mrow><mml:mi>N</mml:mi><mml:mi>f</mml:mi></mml:mrow></mml:mfrac><mml:mo>&#x0003C;</mml:mo><mml:mn>0</mml:mn><mml:mo>.</mml:mo><mml:mn>8</mml:mn></mml:mrow><mml:mo stretchy="true">)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:mtext>&#x000A0;</mml:mtext><mml:mfrac><mml:mrow><mml:mn>0</mml:mn><mml:mo>.</mml:mo><mml:mn>25</mml:mn></mml:mrow><mml:mrow><mml:mn>0</mml:mn><mml:mo>.</mml:mo><mml:mn>61</mml:mn><mml:mo>-</mml:mo><mml:mfrac><mml:mrow><mml:mi>&#x003C3;</mml:mi><mml:mi>m</mml:mi><mml:mi>i</mml:mi><mml:mi>n</mml:mi></mml:mrow><mml:mrow><mml:mi>f</mml:mi><mml:mi>c</mml:mi></mml:mrow></mml:mfrac></mml:mrow></mml:mfrac></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mrow><mml:mo stretchy="true">(</mml:mo><mml:mrow><mml:mn>0</mml:mn><mml:mo>.</mml:mo><mml:mn>39</mml:mn><mml:mo>&#x0002B;</mml:mo><mml:mfrac><mml:mrow><mml:mi>&#x003C3;</mml:mi><mml:mi>m</mml:mi><mml:mi>i</mml:mi><mml:mi>n</mml:mi></mml:mrow><mml:mrow><mml:mi>f</mml:mi><mml:mi>c</mml:mi></mml:mrow></mml:mfrac><mml:mo>-</mml:mo><mml:mfrac><mml:mrow><mml:mi>&#x003C3;</mml:mi><mml:mi>m</mml:mi><mml:mi>a</mml:mi><mml:mi>x</mml:mi></mml:mrow><mml:mrow><mml:mi>f</mml:mi><mml:mi>c</mml:mi></mml:mrow></mml:mfrac></mml:mrow><mml:mo stretchy="true">)</mml:mo></mml:mrow><mml:mi>E</mml:mi><mml:mi>c</mml:mi><mml:mo>&#x02264;</mml:mo><mml:mn>0</mml:mn></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<p>where <italic>E</italic><sub><italic>c</italic></sub> is the static modulus of deformation.</p>
<p>Starting from the previous studies, a few research groups have proposed similar formulations by considering, instead of concrete, the masonry material. Among these groups, it is worth mentioning the studies conducted by (Alshebani and Sinha, <xref ref-type="bibr" rid="B1">2001</xref>). In this work, the authors concluded that deterioration of the elastic modulus began at 20% of the compressive load capacity. Moreover, the strength and stiffness deterioration depended on the number and intensity of cyclic loads, and in particular the degradation increased as the load and number of cycles increased.</p>
<p>As mentioned above, Koltsida et al. (<xref ref-type="bibr" rid="B25">2018b</xref>) recently proposed a different formulation to describe the evolution of the stiffness degradation under cyclic loading. The tests highlighted that until 95% of the fatigue life, the variation of the elastic modulus remained constant, while beyond the 95% mark it rapidly decreased until failure. To describe the evolution of the elastic modulus during cyclic loading, a linear model was proposed as described by Equation 11 and Equation 12, where <italic>E/E</italic><sub>0</sub> represents the ratio between the elastic modulus and initial elastic modulus, and <italic>N/N</italic><sub><italic>f</italic></sub> is the ratio between the number of cycles and the number of cycles to failure. In Equation 12 the coefficient <italic>a</italic> is the gradient coefficient, while <italic>b</italic> is the intercept coefficient of the linear equation:</p>
<disp-formula id="E11"><label>(11)</label><mml:math id="M13"><mml:mtable class="eqnarray" columnalign="right center left"><mml:mtr><mml:mtd><mml:mfrac><mml:mrow><mml:mi>E</mml:mi></mml:mrow><mml:mrow><mml:msub><mml:mrow><mml:mi>E</mml:mi></mml:mrow><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msub></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mi>a</mml:mi><mml:mfrac><mml:mrow><mml:mi>N</mml:mi></mml:mrow><mml:mrow><mml:mi>N</mml:mi><mml:mi>f</mml:mi></mml:mrow></mml:mfrac><mml:mo>&#x0002B;</mml:mo><mml:mi>b</mml:mi></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<disp-formula id="E12"><label>(12)</label><mml:math id="M14"><mml:mtable class="eqnarray" columnalign="right center left"><mml:mtr><mml:mtd><mml:mfrac><mml:mrow><mml:mi>d</mml:mi><mml:mfrac><mml:mrow><mml:mi>E</mml:mi></mml:mrow><mml:mrow><mml:msub><mml:mrow><mml:mi>E</mml:mi></mml:mrow><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msub></mml:mrow></mml:mfrac></mml:mrow><mml:mrow><mml:mi>d</mml:mi><mml:mfrac><mml:mrow><mml:mi>N</mml:mi></mml:mrow><mml:mrow><mml:mi>N</mml:mi><mml:mi>f</mml:mi></mml:mrow></mml:mfrac></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mi>a</mml:mi></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<p>In Koltsida et al. (<xref ref-type="bibr" rid="B25">2018b</xref>) the following function was found as the best fit curve of the maximum induced stress:</p>
<disp-formula id="E13"><label>(13)</label><mml:math id="M15"><mml:mtable class="eqnarray" columnalign="right center left"><mml:mtr><mml:mtd><mml:mfrac><mml:mrow><mml:mi>d</mml:mi><mml:mfrac><mml:mrow><mml:mi>E</mml:mi></mml:mrow><mml:mrow><mml:msub><mml:mrow><mml:mi>E</mml:mi></mml:mrow><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msub></mml:mrow></mml:mfrac></mml:mrow><mml:mrow><mml:mi>d</mml:mi><mml:mfrac><mml:mrow><mml:mi>N</mml:mi></mml:mrow><mml:mrow><mml:mi>N</mml:mi><mml:mi>f</mml:mi></mml:mrow></mml:mfrac></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mi>a</mml:mi><mml:mo>=</mml:mo><mml:mo>-</mml:mo><mml:mn>3</mml:mn><mml:mo>.</mml:mo><mml:mn>0181</mml:mn><mml:msubsup><mml:mrow><mml:mi>S</mml:mi></mml:mrow><mml:mrow><mml:mi>m</mml:mi><mml:mi>a</mml:mi><mml:mi>x</mml:mi></mml:mrow><mml:mrow><mml:mn>3</mml:mn></mml:mrow></mml:msubsup><mml:mo>&#x0002B;</mml:mo><mml:mn>5</mml:mn><mml:mo>.</mml:mo><mml:mn>6894</mml:mn><mml:msubsup><mml:mrow><mml:mi>S</mml:mi></mml:mrow><mml:mrow><mml:mi>m</mml:mi><mml:mi>a</mml:mi><mml:mi>x</mml:mi></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msubsup><mml:mo>-</mml:mo><mml:mn>3</mml:mn><mml:mo>.</mml:mo><mml:mn>5118</mml:mn><mml:msub><mml:mrow><mml:mi>S</mml:mi></mml:mrow><mml:mrow><mml:mi>m</mml:mi><mml:mi>a</mml:mi><mml:mi>x</mml:mi></mml:mrow></mml:msub></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<p>By substituting the previous Equation (13) into Equation (11), the following relationship describing the reduction of the elastic modulus under cycling loading was proposed:</p>
<disp-formula id="E14"><label>(14)</label><mml:math id="M16"><mml:mtable class="eqnarray" columnalign="left"><mml:mtr><mml:mtd><mml:mfrac><mml:mrow><mml:mi>E</mml:mi></mml:mrow><mml:mrow><mml:msub><mml:mrow><mml:mi>E</mml:mi></mml:mrow><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msub></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mn>1</mml:mn><mml:mo>-</mml:mo><mml:mrow><mml:mo stretchy="false">(</mml:mo><mml:mrow><mml:mn>3</mml:mn><mml:mo>.</mml:mo><mml:mn>0181</mml:mn><mml:msubsup><mml:mrow><mml:mi>S</mml:mi></mml:mrow><mml:mrow><mml:mi>m</mml:mi><mml:mi>a</mml:mi><mml:mi>x</mml:mi></mml:mrow><mml:mrow><mml:mn>3</mml:mn></mml:mrow></mml:msubsup><mml:mo>-</mml:mo><mml:mn>5</mml:mn><mml:mo>.</mml:mo><mml:mn>6894</mml:mn><mml:msubsup><mml:mrow><mml:mi>S</mml:mi></mml:mrow><mml:mrow><mml:mi>m</mml:mi><mml:mi>a</mml:mi><mml:mi>x</mml:mi></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msubsup><mml:mo>&#x0002B;</mml:mo><mml:mn>3</mml:mn><mml:mo>.</mml:mo><mml:mn>5118</mml:mn><mml:msub><mml:mrow><mml:mi>S</mml:mi></mml:mrow><mml:mrow><mml:mi>m</mml:mi><mml:mi>a</mml:mi><mml:mi>x</mml:mi></mml:mrow></mml:msub><mml:mo>-</mml:mo><mml:mn>0</mml:mn><mml:mo>.</mml:mo><mml:mn>6175</mml:mn></mml:mrow><mml:mo stretchy="false">)</mml:mo></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mrow><mml:mtext>&#x000A0;&#x000A0;&#x000A0;&#x000A0;&#x000A0;&#x000A0;&#x000A0;&#x000A0;&#x000A0;&#x000A0;</mml:mtext><mml:mo stretchy="false">(</mml:mo><mml:mrow><mml:mfrac><mml:mrow><mml:mi>N</mml:mi></mml:mrow><mml:mrow><mml:msub><mml:mrow><mml:mi>N</mml:mi></mml:mrow><mml:mrow><mml:mi>f</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mfrac></mml:mrow><mml:mo stretchy="false">)</mml:mo></mml:mrow></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
</sec>
<sec id="s4">
<title>Comparison Among the Stress-life Curves Considered</title>
<p>In <xref ref-type="fig" rid="F5">Figure 5</xref> the comparisons among the stress&#x02013;life curves considered in this work are reported and illustrated in the semi-logarithmic plane <italic>Log N- S</italic>. In the comparisons the following values of the ratio <italic>R</italic> &#x0003D; <italic>S</italic><sub><italic>min</italic></sub><italic>/S</italic><sub><italic>max</italic></sub> are considered: 0.2, 0.4, 0.6, and 0.8. Moreover, the curves proposed by Casas (<xref ref-type="bibr" rid="B10">2009</xref>) and Koltsida et al. (<xref ref-type="bibr" rid="B24">2018a</xref>) are drawn by referring to the 5% of failure probability, as considered by the EC3 and NTC-08 for the material nominal compressive strength. Also, <xref ref-type="fig" rid="F5">Figure 5</xref> reports the Tomor and Verstrynge (<xref ref-type="bibr" rid="B43">2013</xref>) stress life curves, and the ones proposed by Ronca et al. (<xref ref-type="bibr" rid="B39">2004</xref>), related to the ratio <italic>R</italic> equal to 0.8, since 0.8 is approximately the average value of the imposed <italic>R</italic> in all the performed tests. In all the graphs, the fatigue endurance limit <italic>S</italic> &#x0003D; <italic>0.5</italic> is also highlighted. It is important to outline that all the considered models may predict a low number of cycles at failure, even lower than the stress level corresponding to the classic endurance limit. From the comparisons, it is possible to highlight that when the stress ratio <italic>R</italic> decreases, i.e., the stress fluctuation between the minimum and maximum compressive stress increases, the number of cycles to failure decreases for any value of ratio <italic>S</italic> &#x0003D; <italic>S</italic><sub><italic>max</italic></sub><italic>/S</italic><sub><italic>u</italic></sub>. Moreover, it can be observed that for <italic>R</italic> equal to 0.6 and 0.8, the fatigue strength becomes significantly higher than the endurance limit, very high also for a number of cycles. Finally, the curves proposed by Tomor and Verstrynge (<xref ref-type="bibr" rid="B43">2013</xref>) indicated very different values for the number of cycles to failure compared to the other curves, especially for high values of ratio <italic>S</italic>, where the effect of the plastic deformations are more influent.</p>
<fig id="F5" position="float">
<label>Figure 5</label>
<caption><p>Comparisons between stress life curves for different values of the ratio R, referred to the 5% of failure probability.</p></caption>
<graphic xlink:href="fbuil-05-00065-g0005.tif"/>
</fig></sec>
<sec id="s5">
<title>Application to a Case Study</title>
<p>In this paper fatigue assessment related to a case study is discussed. In particular, the results related to the main and secondary arches of an ancient masonry arch bridge are shown.</p>
<p>The case study, &#x0201C;Cavone Bridge,&#x0201D; was built in Italy before the Second World War and is currently still open to the traffic. It takes its name from the river it crosses and consists of seven arches of brick masonry. The bridge is 140 m in length and 5.6 m wide, and it is composed of three main arches with span lengths of 22 m and three secondary arches with span lengths of 10 m. The arches are supported by two piers of which 14 m are outside the riverbed. The piers have a total height from the foundation plane of about 24 m.</p>
<p>The bridge serves a provincial road according to the Italian Transport Classification (<xref ref-type="bibr" rid="B23">1992</xref>). The bridge was subjected to some <italic>in situ</italic> tests to identify the typology and the thickness of all its elements and components. The tests showed that the piers, abutments and spandrel walls consist of an external leaf of regular stone blocks. The piers have a core of cohesive backfill, while the bridge deck is formed by an incoherent backfill that has the function of spreading the traffic loads to the supporting arches. More details about numerical investigations carried out on this bridge for fatigue and seismic performance may be found performance in Laterza et al. (<xref ref-type="bibr" rid="B27">2017a</xref>,<xref ref-type="bibr" rid="B28">b</xref>) and D&#x00027;Amato et al. (<xref ref-type="bibr" rid="B14">2017</xref>). In particular, in this section the numerical investigations illustrated in Laterza et al. (<xref ref-type="bibr" rid="B27">2017a</xref>) regarding the most unfavorable section for fatigue assessment verifications are discussed.</p>
<p>As for the load scheme, in this study <italic>Fatigue Model 3</italic>, which has two axles with a load of 120 kN/axle, is used. In accordance with Eurocode 1 (EC1, <xref ref-type="bibr" rid="B16">2003</xref>) the considered fatigue model is more appropriate for typical heavy traffic on European main roads or motorways. In addition, a <italic>Traffic Category 2</italic> has been assumed, resulting in 5 &#x000D7; 10<sup>5</sup> passages for the year (<italic>N</italic><sub><italic>cat</italic></sub>). Since there is an absence of a relative procedure for masonry elements, in this study the fatigue assessment for steel elements has been applied, as proposed in the Italian Design Code Instructions (NTC-08 Instructions) (<xref ref-type="bibr" rid="B22">2009</xref>) and EC3 (<xref ref-type="bibr" rid="B17">2003</xref>), while applying fatigue stress-strain curves for masonry.</p>
<p>In accordance with the Italian Design Code Instructions (NTC-08 Instructions) (<xref ref-type="bibr" rid="B22">2009</xref>), two different values for the masonry compressive strength associated with <italic>Knowledge Level 1</italic> (<italic>KL1</italic>) and <italic>Knowledge Level 3</italic> (<italic>KL3</italic>) have been considered for the arches (NTC-08). Precisely, the compressive strength of masonry is assumed equal to 2.4 MPa for <italic>KL1</italic> and 3.2 MPa for <italic>KL3</italic>. The strength is further reduced by a confidence factor <italic>FC</italic> &#x0003D; 1.35 for <italic>KL1</italic> and <italic>FC</italic> &#x0003D; 1 for <italic>KL3</italic>.</p>
<p><xref ref-type="fig" rid="F6">Figure 6</xref> reports the comparisons of the fatigue curves considered in this study, plotted for main and secondary arches. It should be noted that, in accordance with the NTC-08 and EC3 methods, all the curves are factorized, i.e., the fatigue strength is divided by &#x003B3;<sub><italic>Mf</italic></sub> (fatigue strength partial factor), assumed in this case equal to 1.35 by supposing a high consequence of arch failure due to the fatigue strength achievement. Meanwhile, the stress range &#x00394;&#x003C3;<sub><italic>i</italic></sub>, due to the stresses fluctuation resulting from the transit of the load along the arch, is amplified by &#x003B3;<sub><italic>Ff</italic></sub> &#x0003D; 1, where &#x003B3;<sub><italic>Ff</italic></sub> is the partial factor for equivalent constant amplitude stress range &#x00394;&#x003C3;<sub>i</sub>.</p>
<fig id="F6" position="float">
<label>Figure 6</label>
<caption><p>Main arch (left) and secondary arch (right): calculation of the life cycles at the failure.</p></caption>
<graphic xlink:href="fbuil-05-00065-g0006.tif"/>
</fig>
<p>As far as the stress fluctuation is concerned, three different sections (2 haunches section, and 1 key section) for each arch have been numerically investigated in Laterza et al. (<xref ref-type="bibr" rid="B27">2017a</xref>) by means of FEM models. However, in this study only the most unfavorable section for fatigue assessment in terms of &#x00394;&#x003C3;<sub><italic>i</italic></sub> fluctuation is considered, which is the haunch section for the main arches and the key for the secondary ones. For these sections the ratio <italic>S</italic><sub><italic>min</italic></sub><italic>/S</italic><sub><italic>max</italic></sub> results in value equal to 0.868 for the main arches and to 0.872 for the secondary ones, where <italic>S</italic><sub><italic>min</italic></sub> and <italic>S</italic><sub><italic>max</italic></sub> are the minimum and maximum axial stresses. In <xref ref-type="table" rid="T3">Tables 3</xref>, <xref ref-type="table" rid="T4">4</xref>, the numerical results are summarized for the main and secondary arches, reporting the ratios <italic>S</italic><sub><italic>max</italic></sub><italic>/S</italic><sub><italic>u</italic></sub> (maximum stress <italic>S</italic><sub><italic>max</italic></sub> over the ultimate strength in compression <italic>S</italic><sub><italic>u</italic></sub>) for both <italic>KL1</italic> and <italic>KL3</italic>.</p>
<table-wrap position="float" id="T3">
<label>Table 3</label>
<caption><p>Residual service life evaluation of the main arches.</p></caption>
<table frame="hsides" rules="groups">
<thead><tr>
<th valign="top" align="left"><bold>S-N curve <italic>R</italic> &#x0003D; 0.868</bold></th>
<th valign="top" align="center"><bold>S<sub><bold>max</bold></sub>/S<sub><bold>u</bold></sub> KL1</bold></th>
<th valign="top" align="center"><bold>S<sub><bold>max</bold></sub>/S<sub><bold>u</bold></sub> KL3</bold></th>
<th valign="top" align="center"><bold>logN</bold></th>
<th valign="top" align="center"><bold><italic>N</italic></bold></th>
<th valign="top" align="center"><bold>Ncat traffic category 2</bold></th>
<th valign="top" align="center"><bold>Residual life (years) N/Ncat</bold></th>
</tr>
</thead>
<tbody>
<tr>
<td valign="top" align="left">(Casas, <xref ref-type="bibr" rid="B10">2009</xref>)</td>
<td valign="top" align="center">0.790</td>
<td valign="top" align="center">0.440</td>
<td valign="top" align="center">1.17</td>
<td valign="top" align="center">14.63</td>
<td valign="top" align="center">5 &#x000D7; 10<sup>5</sup></td>
<td valign="top" align="center">&#x02248; 0</td>
</tr>
<tr>
<td valign="top" align="left">(Roberts et al., <xref ref-type="bibr" rid="B38">2006</xref>)</td>
<td valign="top" align="center">0.790</td>
<td valign="top" align="center">0.440</td>
<td valign="top" align="center">6.25</td>
<td valign="top" align="center">1.78 &#x000D7; 10<sup>6</sup></td>
<td valign="top" align="center">5 &#x000D7; 10<sup>5</sup></td>
<td valign="top" align="center">3.56</td>
</tr>
<tr>
<td valign="top" align="left">(Koltsida et al., <xref ref-type="bibr" rid="B24">2018a</xref>)</td>
<td valign="top" align="center">0.790</td>
<td valign="top" align="center">0.440</td>
<td valign="top" align="center">4.8</td>
<td valign="top" align="center">6.31 &#x000D7; 10<sup>4</sup></td>
<td valign="top" align="center">5 &#x000D7; 10<sup>5</sup></td>
<td valign="top" align="center">&#x02248; 0</td>
</tr>
<tr>
<td valign="top" align="left">(Tomor and Verstrynge, <xref ref-type="bibr" rid="B43">2013</xref>)</td>
<td valign="top" align="center">0.790</td>
<td valign="top" align="center">0.440</td>
<td valign="top" align="center">NA</td>
<td valign="top" align="center">-</td>
<td valign="top" align="center">5 &#x000D7; 10<sup>5</sup></td>
<td valign="top" align="center">-</td>
</tr>
<tr>
<td valign="top" align="left">(Ronca et al., <xref ref-type="bibr" rid="B39">2004</xref>)</td>
<td valign="top" align="center">0.790</td>
<td valign="top" align="center">0.440</td>
<td valign="top" align="center">NA</td>
<td valign="top" align="center">-</td>
<td valign="top" align="center">5 &#x000D7; 10<sup>5</sup></td>
<td valign="top" align="center">-</td>
</tr>
</tbody>
</table>
</table-wrap>
<table-wrap position="float" id="T4">
<label>Table 4</label>
<caption><p>Residual service life evaluation of the secondary arches.</p></caption>
<table frame="hsides" rules="groups">
<thead><tr>
<th valign="top" align="left"><bold>S-N curve <italic>R</italic> &#x0003D; 0.872</bold></th>
<th valign="top" align="center"><bold>S<sub><bold>max</bold></sub>/S<sub><bold>u</bold></sub> KL1</bold></th>
<th valign="top" align="center"><bold>S<sub><bold>max</bold></sub>/S<sub><bold>u</bold></sub> KL3</bold></th>
<th valign="top" align="center"><bold>logN</bold></th>
<th valign="top" align="center"><bold><italic>N</italic></bold></th>
<th valign="top" align="center"><bold>Ncat traffic category 2</bold></th>
<th valign="top" align="center"><bold>Residual life (years) N/Ncat</bold></th>
</tr>
</thead>
<tbody>
<tr>
<td/>
<td/>
<td/>
<td/>
<td/>
<td/>
<td/>
</tr>
<tr>
<td valign="top" align="left">(Casas, <xref ref-type="bibr" rid="B10">2009</xref>)</td>
<td valign="top" align="center">0.494</td>
<td valign="top" align="center">0.275</td>
<td valign="top" align="center">NA</td>
<td valign="top" align="center">-</td>
<td valign="top" align="center">5 &#x000D7; 10<sup>5</sup></td>
<td valign="top" align="center">-</td>
</tr>
<tr>
<td valign="top" align="left">(Roberts et al., <xref ref-type="bibr" rid="B38">2006</xref>)</td>
<td valign="top" align="center">0.494</td>
<td valign="top" align="center">0.275</td>
<td valign="top" align="center">NA</td>
<td valign="top" align="center">-</td>
<td valign="top" align="center">5 &#x000D7; 10<sup>5</sup></td>
<td valign="top" align="center">-</td>
</tr>
<tr>
<td valign="top" align="left">(Koltsida et al., <xref ref-type="bibr" rid="B24">2018a</xref>)</td>
<td valign="top" align="center">0.494</td>
<td valign="top" align="center">0.275</td>
<td valign="top" align="center">NA</td>
<td valign="top" align="center">-</td>
<td valign="top" align="center">5 &#x000D7; 10<sup>5</sup></td>
<td valign="top" align="center">-</td>
</tr>
<tr>
<td valign="top" align="left">(Tomor and Verstrynge, <xref ref-type="bibr" rid="B43">2013</xref>)</td>
<td valign="top" align="center">0.494</td>
<td valign="top" align="center">0.275</td>
<td valign="top" align="center">NA</td>
<td valign="top" align="center">-</td>
<td valign="top" align="center">5 &#x000D7; 10<sup>5</sup></td>
<td valign="top" align="center">-</td>
</tr>
<tr>
<td valign="top" align="left">(Ronca et al., <xref ref-type="bibr" rid="B39">2004</xref>)</td>
<td valign="top" align="center">0.494</td>
<td valign="top" align="center">0.275</td>
<td valign="top" align="center">NA</td>
<td valign="top" align="center">-</td>
<td valign="top" align="center">5 &#x000D7; 10<sup>5</sup></td>
<td valign="top" align="center">-</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>The fatigue performance is evaluated through the calculation of the residual service life, expressing the residual time (in year) before the failure to fatigue. This is given by the following ratio:</p>
<disp-formula id="E15"><label>(15)</label><mml:math id="M18"><mml:mtable class="eqnarray" columnalign="right center left"><mml:mtr><mml:mtd><mml:mi>R</mml:mi><mml:mi>e</mml:mi><mml:mi>s</mml:mi><mml:mi>i</mml:mi><mml:mi>d</mml:mi><mml:mi>u</mml:mi><mml:mi>a</mml:mi><mml:mi>l</mml:mi><mml:mtext>&#x000A0;</mml:mtext><mml:mi>S</mml:mi><mml:mi>e</mml:mi><mml:mi>r</mml:mi><mml:mi>v</mml:mi><mml:mi>i</mml:mi><mml:mi>c</mml:mi><mml:mi>e</mml:mi><mml:mtext>&#x000A0;</mml:mtext><mml:mi>L</mml:mi><mml:mi>i</mml:mi><mml:mi>f</mml:mi><mml:mi>e</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mi>N</mml:mi></mml:mrow><mml:mrow><mml:msub><mml:mrow><mml:mi>N</mml:mi></mml:mrow><mml:mrow><mml:mi>c</mml:mi><mml:mi>a</mml:mi><mml:mi>t</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mfrac><mml:mtext>&#x000A0;</mml:mtext><mml:mrow><mml:mo stretchy="false">(</mml:mo><mml:mrow><mml:mi>y</mml:mi><mml:mi>e</mml:mi><mml:mi>a</mml:mi><mml:mi>r</mml:mi><mml:mi>s</mml:mi></mml:mrow><mml:mo stretchy="false">)</mml:mo></mml:mrow></mml:mtd></mml:mtr></mml:mtable></mml:math></disp-formula>
<p>where <italic>N</italic> is the cycle number to failure obtained from the stress-life curve and <italic>N</italic><sub><italic>cat</italic></sub> is the number of passages per year assumed for the category of the bridge (<italic>N</italic><sub><italic>cat</italic></sub> &#x0003D; 5 &#x000D7; 10<sup>5</sup> passages/year).</p>
<p>It should be noted that for <italic>KL3</italic>, by referring to the main arches, and for <italic>KL1</italic> and <italic>KL3</italic> in the case of secondary ones, the cycles&#x00027; number to failure <italic>N</italic> are always very high (greater than 10<sup>8</sup>) so that, substantially, the residual life may be considered infinite.</p>
<p>On the other hand, the fatigue assessment results drastically change if the <italic>KL1</italic> is considered for main arches. In this case, the models of Tomor and Verstrynge (<xref ref-type="bibr" rid="B43">2013</xref>) and Ronca et al. (<xref ref-type="bibr" rid="B39">2004</xref>) are not applicable, since the stress level <italic>S</italic><sub><italic>max</italic></sub><italic>/S</italic><sub><italic>u</italic></sub> &#x0003D; 0.790 falls beyond the stress-life curves for any value of <italic>logN</italic>. As for the model proposed by Casas (<xref ref-type="bibr" rid="B10">2009</xref>) and Koltsida et al. (<xref ref-type="bibr" rid="B24">2018a</xref>), the residual life is &#x0003C; 1 year. Meanwhile, according to the Roberts et al. (<xref ref-type="bibr" rid="B38">2006</xref>) model, the residual life is about 3.5 years.</p>
<p>By comparing the chosen models, it is possible to conclude that the models proposed by Koltsida et al. (<xref ref-type="bibr" rid="B24">2018a</xref>), Tomor and Verstrynge (<xref ref-type="bibr" rid="B43">2013</xref>) and Casas (<xref ref-type="bibr" rid="B10">2009</xref>) actually represent the most complete models, since they have been derived from experimental results considered with a probabilistic approach. Differently from the Ronca et al. (<xref ref-type="bibr" rid="B39">2004</xref>) model (derived by imposing a small variation of the alternating loads), both the Roberts et al. (<xref ref-type="bibr" rid="B38">2006</xref>) and Casas (<xref ref-type="bibr" rid="B10">2009</xref>) models estimate, at a number of cycles that is not too high, fatigue strength ratios (S<sub>max</sub>/S<sub>u</sub>) significantly lower than 0.5, which is the value usually indicated as the fatigue endurance limit. This demonstrates the importance of an appropriate evaluation of the fatigue strength that may lead, if simplified methods are applied (such as the endurance limit criterion), to an overestimation of the actual fatigue strength.</p></sec>
<sec sec-type="conclusions" id="s6">
<title>Conclusions</title>
<p>In this paper, a critical review has been made and we have applied some fatigue models to a case study, considering also the deterioration of the masonry due to the effect of the cyclic loads.</p>
<p>In particular, different fatigue curves have been considered for evaluating the damage accumulation due to traffic load, in compliance with the procedure proposed by the EC3 (<xref ref-type="bibr" rid="B17">2003</xref>) and NTC-08 (2008). Since in the examined codes no clear indication is reported for masonry elements, the fatigue performance approach has been applied similarly to the one proposed for steel elements, with masonry fatigue curves.</p>
<p>Different stress-life curves have been considered in accordance with the models proposed by Ronca et al. (<xref ref-type="bibr" rid="B39">2004</xref>), Roberts et al. (<xref ref-type="bibr" rid="B38">2006</xref>), Casas (<xref ref-type="bibr" rid="B10">2009</xref>), Tomor and Verstrynge (<xref ref-type="bibr" rid="B43">2013</xref>) and Koltsida et al. (<xref ref-type="bibr" rid="B24">2018a</xref>), which are also capable of estimating the degradation of the material due to fatigue.</p>
<p>By comparing the chosen models, it possible to conclude that the models proposed by Casas (<xref ref-type="bibr" rid="B10">2009</xref>), Tomor and Verstrynge (<xref ref-type="bibr" rid="B43">2013</xref>), and Koltsida et al. (<xref ref-type="bibr" rid="B24">2018a</xref>) actually represent the most complete models, since they have been derived from the experimental results considered with a probabilistic approach. It must be remarked, however, that they have been derived from laboratory tests performed on masonry specimens having compressive strength values higher than the usual ones encountered in existing masonry. To this aim, particular attention should be also paid to the influence on the fatigue capacity of the cyclic load frequency. As a matter of fact, the fatigue models examined in this study have been proposed for cycled loads having frequencies (more than 1 Hz) higher than the ones associated with traffic loads indicated in the considered codes (for example, in the case analyzed the traffic load frequency results equal to 0.015 Hz). A first approach has been adopted to evaluate the degradation of the material due to the fatigue effects by using the recent model proposed by Koltsida et al. (<xref ref-type="bibr" rid="B25">2018b</xref>).</p>
<p>Finally, new laboratory tests focused on ancient masonry specimens will permit researchers to study in a more in-depth manner the fatigue behavior and the evolution of the material degradation of masonry, which have not yet been fully detailed.</p></sec>
<sec id="s7">
<title>Data Availability</title>
<p>The datasets generated for this study are available on request to the corresponding author.</p></sec>
<sec id="s8">
<title>Author Contributions</title>
<p>All authors listed have made a substantial, direct and intellectual contribution to the work, and approved it for publication.</p>
<sec>
<title>Conflict of Interest Statement</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>
</body>
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