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<front>
<journal-meta>
<journal-id journal-id-type="publisher-id">Front. Mech. Eng</journal-id>
<journal-title>Frontiers in Mechanical Engineering</journal-title>
<abbrev-journal-title abbrev-type="pubmed">Front. Mech. Eng</abbrev-journal-title>
<issn pub-type="epub">2297-3079</issn>
<publisher>
<publisher-name>Frontiers Media S.A.</publisher-name>
</publisher>
</journal-meta>
<article-meta>
<article-id pub-id-type="publisher-id">1126489</article-id>
<article-id pub-id-type="doi">10.3389/fmech.2023.1126489</article-id>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Mechanical Engineering</subject>
<subj-group>
<subject>Original Research</subject>
</subj-group>
</subj-group>
</article-categories>
<title-group>
<article-title>Numerical realization of a semi-active virtual acoustic black hole effect</article-title>
<alt-title alt-title-type="left-running-head">Soleimanian et al.</alt-title>
<alt-title alt-title-type="right-running-head">
<ext-link ext-link-type="uri" xlink:href="https://doi.org/10.3389/fmech.2023.1126489">10.3389/fmech.2023.1126489</ext-link>
</alt-title>
</title-group>
<contrib-group>
<contrib contrib-type="author" corresp="yes">
<name>
<surname>Soleimanian</surname>
<given-names>Sina</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
<xref ref-type="corresp" rid="c001">&#x2a;</xref>
<uri xlink:href="https://loop.frontiersin.org/people/2096875/overview"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Petrone</surname>
<given-names>Giuseppe</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
<uri xlink:href="https://loop.frontiersin.org/people/1372051/overview"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Franco</surname>
<given-names>Francesco</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
</contrib>
<contrib contrib-type="author">
<name>
<surname>De Rosa</surname>
<given-names>Sergio</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
<uri xlink:href="https://loop.frontiersin.org/people/166633/overview"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Ko&#x142;akowski</surname>
<given-names>Przemys&#x142;aw</given-names>
</name>
<xref ref-type="aff" rid="aff2">
<sup>2</sup>
</xref>
</contrib>
</contrib-group>
<aff id="aff1">
<sup>1</sup>
<institution>Department of Industrial Engineering</institution>, <institution>University of Naples Federico II</institution>, <addr-line>Naples</addr-line>, <country>Italy</country>
</aff>
<aff id="aff2">
<sup>2</sup>
<institution>Adaptronica sp z o o</institution>, <institution>R&#x26;D Company</institution>, <addr-line>&#x141;omianki</addr-line>, <country>Poland</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/1720676/overview">Francisco Beltran-Carbajal</ext-link>, Universidad Autonoma Metropolitana, Mexico</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/2150585/overview">Luis Gerardo Trujillo-Franco</ext-link>, Universidad Polit&#xe9;cnica de Pachuca, Mexico</p>
<p>
<ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/1718133/overview">Hugo Francisco Abundis-Fong</ext-link>, I.T. Pachuca, Mexico</p>
</fn>
<corresp id="c001">&#x2a;Correspondence: Sina Soleimanian, <email>sina.soleimanian@unina.it</email>
</corresp>
<fn fn-type="other">
<p>This article was submitted to Vibration Systems, a section of the journal Frontiers in Mechanical Engineering</p>
</fn>
</author-notes>
<pub-date pub-type="epub">
<day>15</day>
<month>03</month>
<year>2023</year>
</pub-date>
<pub-date pub-type="collection">
<year>2023</year>
</pub-date>
<volume>9</volume>
<elocation-id>1126489</elocation-id>
<history>
<date date-type="received">
<day>17</day>
<month>12</month>
<year>2022</year>
</date>
<date date-type="accepted">
<day>03</day>
<month>03</month>
<year>2023</year>
</date>
</history>
<permissions>
<copyright-statement>Copyright &#xa9; 2023 Soleimanian, Petrone, Franco, De Rosa and Ko&#x142;akowski.</copyright-statement>
<copyright-year>2023</copyright-year>
<copyright-holder>Soleimanian, Petrone, Franco, De Rosa and Ko&#x142;akowski</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>Noise mitigation by means of the acoustic black hole (ABH) effect is a well-known engineering solution. However, the conventional method of applying ABH effect which requires modification of the structure geometry has various limitations which encourage the research of virtual ABH concept. In this study, the effect of ABH was applied through introducing virtual stiffness by a shunt circuit. According to the force-voltage electric analogy, stiffness has an inverse relationship with capacitance. So that the ABH effect can be virtually realized by following a power law profile using an array of independent capacitive shunts. The concept is studied through finite element simulation developing a macro code in ANSYS Parametric Design Language (APDL). To evaluate the influence of capacitance profile on the acoustic radiated power, parametric studies are conducted. Based on the results of the parametric studies, the capacitance profile is tuned for minimum radiated power. It is revealed that the virtual acoustic black hole (ABH) effect can offer 10.29%, 6.37%, and 7.47% reduction in the radiated power from the first to the last targeted mode, respectively. The virtual ABH effect introduced in this study can be used for semi-active structural noise isolation without any weight or manufacturing penalty.</p>
</abstract>
<kwd-group>
<kwd>semi-active</kwd>
<kwd>shunt technique</kwd>
<kwd>ABH</kwd>
<kwd>finite element</kwd>
<kwd>noise</kwd>
</kwd-group>
<contract-sponsor id="cn001">Universit&#xe0; degli Studi di Napoli Federico II<named-content content-type="fundref-id">10.13039/100007195</named-content>
</contract-sponsor>
</article-meta>
</front>
<body>
<sec id="s1">
<title>1 Introduction</title>
<p>The increasing requirement for noise management in industries has led to a substantial research being conducted on noise cancellation methods (<xref ref-type="bibr" rid="B33">Simons and Waters, 2004</xref>; <xref ref-type="bibr" rid="B37">Wang, 2010</xref>; <xref ref-type="bibr" rid="B36">Towers et al., 2021</xref>). Sound emission can be generally classified to structure-borne and air-borne noise. Structure-born noise occurs when a mechanism vibrates due to direct mechanical contact with the vibration source. Air-borne noise is produced by a source which radiates directly to the air (<xref ref-type="bibr" rid="B4">Berendt et al., 1967</xref>). Usually, the structure-borne noise requires significant attention since it is a low-frequency tonal noise which cannot be controlled by conventional barrier or insulation methods (<xref ref-type="bibr" rid="B26">Ngai and Ng, 2003</xref>; <xref ref-type="bibr" rid="B9">Fathiah Waziralilah et al., 2018</xref>). Passive techniques are often adopted to dampen the structure-borne noise despite a significant weight penalty often associated.</p>
<p>The effectiveness of electronic damping as a low-cost and lightweight passive technique is examined for its vibroacoustic attenuation effect by many authors (<xref ref-type="bibr" rid="B28">Park and Inman, 2003</xref>; <xref ref-type="bibr" rid="B42">Zhao et al., 2016</xref>; <xref ref-type="bibr" rid="B35">Suryakant et al., 2022</xref>). A case study revealed 7&#xa0;dB reduction in sound transmission achieved by a shunt circuit for a clamped plate excited by a sound source in the frequency range of 10&#x2013;1,000&#xa0;Hz (<xref ref-type="bibr" rid="B1">Ahmadian and Jeric, 2001</xref>). Another study revealed at least a 57% reduction in radiated noise for a clamped plate excited by a shaker in the frequency range of 0&#x2013;245&#xa0;Hz (<xref ref-type="bibr" rid="B2">Ahmadian et al., 2001</xref>).</p>
<p>Another efficient solution for noise cancellation is the acoustic black hole (ABH) effect, a passive, lightweight, and economic technique. According to the ABH effect theory, the vibration wave can be focalized and diminished to zero due to an exponential reduction in the host structure thickness (<xref ref-type="bibr" rid="B21">Li and Ding, 2018</xref>; <xref ref-type="bibr" rid="B13">Hook et al., 2019</xref>; <xref ref-type="bibr" rid="B25">Mousavi et al., 2022</xref>). The thickness exponential function and position of ABH are determinative factors for the amount of energy trapped (<xref ref-type="bibr" rid="B31">Rothe et al., 2016</xref>; <xref ref-type="bibr" rid="B22">Liang et al., 2022</xref>). There exist several restrictions in the introduction of the ABH effect to the geometry. The dependency of ABH profile position on its efficiency limits its isolation effect to a few modes of resonance (<xref ref-type="bibr" rid="B41">Zhang et al., 2019</xref>; <xref ref-type="bibr" rid="B10">Gao et al., 2022</xref>). Another shortcoming of the ABH effect is its inadequacy at low frequencies (<xref ref-type="bibr" rid="B7">Denis et al., 2014</xref>; <xref ref-type="bibr" rid="B19">Li et al., 2021</xref>; <xref ref-type="bibr" rid="B23">Liang et al., 2021</xref>). In one study, the effective frequency range of ABH is broadened by integrating shunt damping and transferring the energy from low to high frequencies (<xref ref-type="bibr" rid="B40">Zhang et al., 2022</xref>). An inevitable condition for ABH geometries is that the host structure must be large enough to allow carving out the power law profile which is a limitation in vehicle and aero applications (<xref ref-type="bibr" rid="B14">Ji et al., 2018</xref>; <xref ref-type="bibr" rid="B29">Park et al., 2019</xref>). This constraint is overcome partially by using ABH-inspired active electronic dampening in conjunction with the force-current electric analogy by <xref ref-type="bibr" rid="B24">Maugan et al. (2019)</xref>.</p>
<p>The use of semi-active systems, also known as adaptive systems, for noise isolation has received attention in the last decade (<xref ref-type="bibr" rid="B3">Bein et al., 2008</xref>; <xref ref-type="bibr" rid="B43">Zhu et al., 2017</xref>; <xref ref-type="bibr" rid="B38">Wrona et al., 2021a</xref>). With the help of semi-active systems, certain resonant peaks can be attenuated while also adverse impacts of vibration absorbers on non-target modes may be prevented. Using the shunt technique in an adaptive manner, one may absorb noise and vibration at various modes by proper adjustment of the shunt circuit impedances (<xref ref-type="bibr" rid="B34">Soong and Spencer, 2000</xref>; <xref ref-type="bibr" rid="B5">Corr and Clark, 2001</xref>; <xref ref-type="bibr" rid="B27">Niederberger et al., 2003</xref>; <xref ref-type="bibr" rid="B3">Bein et al., 2008</xref>). Optimizing tuning variable which determines the control states is a common task for semi-active shunt approach (<xref ref-type="bibr" rid="B11">Gonzalez-Buelga et al., 2014</xref>). The control states can consist of ON and OFF modes (<xref ref-type="bibr" rid="B39">Wrona et al., 2021b</xref>), or it can take several states as reported by <xref ref-type="bibr" rid="B20">Li and Zhu (2021)</xref> using a rheostat to introduce numerous resistance levels.</p>
<p>Limitations associated with physical ABH execution such as low-frequency inefficiency (<xref ref-type="bibr" rid="B7">Denis et al., 2014</xref>; <xref ref-type="bibr" rid="B19">Li et al., 2021</xref>; <xref ref-type="bibr" rid="B23">Liang et al., 2021</xref>), space occupation (<xref ref-type="bibr" rid="B14">Ji et al., 2018</xref>; <xref ref-type="bibr" rid="B29">Park et al., 2019</xref>), and tunability to narrow frequency ranges (<xref ref-type="bibr" rid="B41">Zhang et al., 2019</xref>; <xref ref-type="bibr" rid="B10">Gao et al., 2022</xref>) motivates the research to apply the ABH effect virtually through a semi-active strategy.</p>
<p>In the present study, a beam structure is covered by an array of piezoelectric elements shunted by capacitors to impose the power law stiffness profile virtually. To attenuate the three resonant peaks of the beam which contribute in the radiated noise, the shunt circuit is tuned in terms of power law function. The present approach can be applied to ultra-thin structures where physically applying the ABH effect is impossible. To the best of our knowledge, this is the first study to introduce the concept of virtual ABH effect integrated with force-voltage analogy as a semi-active noise mitigation approach.</p>
</sec>
<sec sec-type="materials|methods" id="s2">
<title>2 Materials and methods</title>
<p>To explain the ABH effect, consider a wedge whose variable thickness follows a power law profile as <inline-formula id="inf1">
<mml:math id="m1">
<mml:mrow>
<mml:mi>h</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>x</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:mi>&#x3b5;</mml:mi>
<mml:msup>
<mml:mi>x</mml:mi>
<mml:mi>m</mml:mi>
</mml:msup>
</mml:mrow>
</mml:math>
</inline-formula> (<italic>&#x3b5;</italic> and <italic>m</italic> &#x3e; 0 ), shown by <xref ref-type="fig" rid="F1">Figure 1</xref>. If <inline-formula id="inf2">
<mml:math id="m2">
<mml:mrow>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>x</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
</inline-formula> is the local wave number of a flexural wave, the total wave transit time through the wedge can be derived by Eq. <xref ref-type="disp-formula" rid="e1">1</xref>.<disp-formula id="e1">
<mml:math id="m3">
<mml:mrow>
<mml:mi>&#x3c4;</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msubsup>
<mml:mo>&#x222b;</mml:mo>
<mml:mn>0</mml:mn>
<mml:mi>x</mml:mi>
</mml:msubsup>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>x</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mi>d</mml:mi>
<mml:mi>x</mml:mi>
</mml:mrow>
</mml:math>
<label>(1)</label>
</disp-formula>
</p>
<fig id="F1" position="float">
<label>FIGURE 1</label>
<caption>
<p>Ideal wedge shape with power law profile.</p>
</caption>
<graphic xlink:href="fmech-09-1126489-g001.tif"/>
</fig>
<p>Considering <italic>k</italic>
<sub>
<italic>p</italic>
</sub> as the wave number of quasi-longitudinal waves, the local wave number can be expressed by Eq. <xref ref-type="disp-formula" rid="e2">2</xref> for a wedge with a power-law profile.<disp-formula id="e2">
<mml:math id="m4">
<mml:mrow>
<mml:mi>k</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>x</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mn>12</mml:mn>
<mml:mfrac>
<mml:mrow>
<mml:mn>1</mml:mn>
</mml:mrow>
<mml:mrow>
<mml:mn>4</mml:mn>
</mml:mrow>
</mml:mfrac>
</mml:msup>
<mml:msub>
<mml:mi>k</mml:mi>
<mml:mi>p</mml:mi>
</mml:msub>
<mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>&#x3b5;</mml:mi>
<mml:msup>
<mml:mi>x</mml:mi>
<mml:mi>m</mml:mi>
</mml:msup>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mn>1</mml:mn>
<mml:mo>/</mml:mo>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:msup>
</mml:mrow>
</mml:math>
<label>(2)</label>
</disp-formula>
</p>
<p>By substitution of Eq. <xref ref-type="disp-formula" rid="e2">2</xref> into Eq. <xref ref-type="disp-formula" rid="e1">1</xref>, it can be seen that the integral diverges for <inline-formula id="inf3">
<mml:math id="m5">
<mml:mrow>
<mml:mi>m</mml:mi>
<mml:mo>&#x2265;</mml:mo>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:math>
</inline-formula>. It means that if the wedge is designed ideally, the wave never reaches the edge. This perfect absorption is known as ABH effect which is imposed by geometry (<xref ref-type="bibr" rid="B17">Krylov and Tilman, 2004</xref>).</p>
<p>In the present study it is of interest to introduce the ABH effect imposed not by geometry but by applying the electric analogy. In this regard, consider a dynamic system consisting of a mass (<italic>m</italic>), a spring (<italic>k</italic>), and a damper (<italic>b</italic>) subjected to the excitation <italic>f</italic> as given by <xref ref-type="fig" rid="F2">Figure 2A</xref>. Moreover, take a basic electric circuit with resistance (<italic>R</italic>), inductance (<italic>I</italic>), capacitance (<italic>C</italic>), subjected to a voltage <italic>V</italic> as given by <xref ref-type="fig" rid="F2">Figure 2B</xref>.</p>
<fig id="F2" position="float">
<label>FIGURE 2</label>
<caption>
<p>
<bold>(A)</bold> Basic dynamic system, <bold>(B)</bold> analogeous electrical circuit.</p>
</caption>
<graphic xlink:href="fmech-09-1126489-g002.tif"/>
</fig>
<p>The force-voltage analogy can be established as<disp-formula id="e3">
<mml:math id="m6">
<mml:mrow>
<mml:mi>F</mml:mi>
<mml:mo>&#x2248;</mml:mo>
<mml:mi>V</mml:mi>
</mml:mrow>
</mml:math>
<label>(3)</label>
</disp-formula>
</p>
<p>Eq. <xref ref-type="disp-formula" rid="e3">3</xref> can be derived as<disp-formula id="e4">
<mml:math id="m7">
<mml:mrow>
<mml:mi>m</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:msup>
<mml:mi>d</mml:mi>
<mml:mn>2</mml:mn>
</mml:msup>
<mml:mi>x</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>d</mml:mi>
<mml:msup>
<mml:mi>t</mml:mi>
<mml:mn>2</mml:mn>
</mml:msup>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x2b;</mml:mo>
<mml:mi>b</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mi>d</mml:mi>
<mml:mi>x</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>d</mml:mi>
<mml:mi>t</mml:mi>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x2b;</mml:mo>
<mml:mi>k</mml:mi>
<mml:mi>x</mml:mi>
<mml:mo>&#x2248;</mml:mo>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>L</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mi>d</mml:mi>
<mml:mi>i</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mi>d</mml:mi>
<mml:mi>t</mml:mi>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x2b;</mml:mo>
<mml:mi>R</mml:mi>
<mml:mi>i</mml:mi>
<mml:mo>&#x2b;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mn>1</mml:mn>
</mml:mrow>
<mml:mrow>
<mml:mi>C</mml:mi>
</mml:mrow>
</mml:mfrac>
<mml:mo>&#x222b;</mml:mo>
<mml:mi>i</mml:mi>
<mml:mi>d</mml:mi>
<mml:mi>t</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(4)</label>
</disp-formula>
</p>
<p>Hence, Eq. <xref ref-type="disp-formula" rid="e4">4</xref> implies that capacitance is relevant to the reverse of stiffness (<xref ref-type="bibr" rid="B6">Darleux et al., 2022</xref>).</p>
<p>In this regard, the ABH effect imposed by geometry (see <xref ref-type="fig" rid="F3">Figure 3A</xref>) is virtually defined by considering <italic>i</italic> number of piezoelectric elements with equal distances attached on a beam surface (see <xref ref-type="fig" rid="F3">Figure 3B</xref>). Each piezoelectric element is shunted independently by a capacitor. The ideal ABH stiffness, ideal capacitance, and real capacitance for the beam structure are well noted by <italic>k</italic>, <italic>C</italic>
<sub>
<italic>i</italic>
</sub>
<italic>,</italic> and <italic>C,</italic> respectively (see <xref ref-type="fig" rid="F3">Figure 3C</xref>). Here, two points should be emphasized for a better understanding of the problem. First, the lower limit of real and ideal capacitance is always non-zero which means an artificial thickness is added along the beam. Second, the maximum value of capacitance is infinite for an ideal ABH (<italic>C</italic>
<sub>
<italic>i</italic>
</sub>) shown by <xref ref-type="fig" rid="F3">Figure 3C</xref>. However, the present modeling cannot simulate an ideal ABH for two reasons: (a) the beam initial thickness cannot be set to zero, and (b) there is a geometry constraint that corresponds to the distance between piezoelectric patches. So that the maximum capacitance is not infinite but as big as super capacitors.</p>
<fig id="F3" position="float">
<label>FIGURE 3</label>
<caption>
<p>
<bold>(A)</bold> physical ABH, <bold>(B)</bold> virtual ABH, <bold>(C)</bold> stiffness, and capacitance variations.</p>
</caption>
<graphic xlink:href="fmech-09-1126489-g003.tif"/>
</fig>
<p>By tuning the capacitive shunt technique, maximum capacitance should be defined at the beam antinode and effective noise isolation is expected, consequently. Since the antinode position is variable from mode to mode, a semi-active scheme can be adopted to change the power law profile, and attenuate several modes. So that the capacitance values can be switched among various states as depicted by <xref ref-type="fig" rid="F4">Figure 4</xref>. To absorb the <italic>j</italic>
<sup>th</sup> mode of resonance, a series of <italic>i</italic> number of capacitors can be considered as {<italic>C</italic>
<sub>
<italic>1j</italic>
</sub>
<italic>, C</italic>
<sub>
<italic>2j</italic>
</sub>
<italic>, ..., C</italic>
<sub>
<italic>ij</italic>
</sub>}, tunable to the corresponding mode according to power law as indicated by Eq. <xref ref-type="disp-formula" rid="e5">5</xref>.<disp-formula id="e5">
<mml:math id="m8">
<mml:mrow>
<mml:msub>
<mml:mi>C</mml:mi>
<mml:mrow>
<mml:mi>i</mml:mi>
<mml:mi>j</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mi>C</mml:mi>
<mml:mi mathvariant="italic">max</mml:mi>
</mml:msub>
<mml:msup>
<mml:msub>
<mml:mi>a</mml:mi>
<mml:mi>i</mml:mi>
</mml:msub>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>n</mml:mi>
</mml:mrow>
</mml:msup>
</mml:mrow>
</mml:math>
<label>(5)</label>
</disp-formula>Where <italic>C</italic>
<sub>
<italic>max</italic>
</sub> is the maximum value of capacitance which can be taken by one or more than one capacitors depending on the target mode to be tuned. Moreover, <italic>a</italic>
<sub>
<italic>i</italic>
</sub> represents the element of an arithmetic progression, the first term of which is 1 and the difference between terms is <italic>r</italic> as expressed by Eq. <xref ref-type="disp-formula" rid="e6">6</xref>.<disp-formula id="e6">
<mml:math id="m9">
<mml:mrow>
<mml:msub>
<mml:mi>a</mml:mi>
<mml:mi>i</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>i</mml:mi>
<mml:mo>&#x2212;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:math>
<label>(6)</label>
</disp-formula>
</p>
<fig id="F4" position="float">
<label>FIGURE 4</label>
<caption>
<p>Capacitive shunts apply semi-active scheme applied to shunted piezoelectric elements.</p>
</caption>
<graphic xlink:href="fmech-09-1126489-g004.tif"/>
</fig>
<p>The effectiveness of the proposed semi-active scheme can be evaluated by solving the harmonic analysis of the cantilever beam. The vibrating beam excites the surrounding air and emits noise. The sound power corresponding to the radiated noise can be represented as the integral of the acoustic intensity along the normal direction on a given surface &#x393; as<disp-formula id="e7">
<mml:math id="m10">
<mml:mrow>
<mml:mi>P</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mo>&#x222c;</mml:mo>
<mml:mi mathvariant="italic">&#x393;</mml:mi>
</mml:msub>
<mml:mover accent="true">
<mml:mi>I</mml:mi>
<mml:mo>&#x21c0;</mml:mo>
</mml:mover>
<mml:mo>.</mml:mo>
<mml:mover accent="true">
<mml:mi>n</mml:mi>
<mml:mo>&#x21c0;</mml:mo>
</mml:mover>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mi>d</mml:mi>
<mml:mi mathvariant="italic">&#x393;</mml:mi>
</mml:mrow>
</mml:math>
<label>(7)</label>
</disp-formula>where <italic>I</italic> is the acoustic intensity, <inline-formula id="inf4">
<mml:math id="m11">
<mml:mrow>
<mml:mover accent="true">
<mml:mi>n</mml:mi>
<mml:mo>&#x21c0;</mml:mo>
</mml:mover>
</mml:mrow>
</mml:math>
</inline-formula> is the normal vector, and <inline-formula id="inf5">
<mml:math id="m12">
<mml:mrow>
<mml:mi mathvariant="normal">&#x393;</mml:mi>
</mml:mrow>
</mml:math>
</inline-formula> is the structure-air interface. The power carried by the acoustic wave per unit area in the normal surface direction is known as the acoustic intensity given by (<xref ref-type="bibr" rid="B12">Hambric and Taylor, 1994</xref>)<disp-formula id="e8">
<mml:math id="m13">
<mml:mrow>
<mml:mover accent="true">
<mml:mi>I</mml:mi>
<mml:mo>&#x21c0;</mml:mo>
</mml:mover>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mn>1</mml:mn>
</mml:mrow>
<mml:mrow>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:mfrac>
<mml:mi>R</mml:mi>
<mml:mi>E</mml:mi>
<mml:mrow>
<mml:mo>(</mml:mo>
<mml:mrow>
<mml:mi>p</mml:mi>
<mml:mo>.</mml:mo>
<mml:mover accent="true">
<mml:mi>v</mml:mi>
<mml:mo>&#x21c0;</mml:mo>
</mml:mover>
</mml:mrow>
<mml:mo>)</mml:mo>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(8)</label>
</disp-formula>where <italic>p</italic> and <italic>v</italic> refer to the radiated acoustic pressure, and particle velocity vector of air, respectively. By establishing continuity of velocity at the solid/air interface, the structural velocity will be equaled to air particle velocity as<disp-formula id="e9">
<mml:math id="m14">
<mml:mrow>
<mml:msub>
<mml:mi>v</mml:mi>
<mml:mrow>
<mml:mi>s</mml:mi>
<mml:mo>,</mml:mo>
<mml:mi>n</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mi>v</mml:mi>
<mml:mrow>
<mml:mi>a</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mi>p</mml:mi>
<mml:mrow>
<mml:msub>
<mml:mi>&#x3c1;</mml:mi>
<mml:mrow>
<mml:mi>a</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:msub>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mrow>
<mml:mi>a</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:math>
<label>(9)</label>
</disp-formula>where <italic>v</italic>
<sub>
<italic>s</italic>,<italic>n</italic>
</sub>, <italic>v</italic>
<sub>
<italic>air</italic>
</sub>
<italic>, &#x3c1;</italic>
<sub>
<italic>air</italic>
</sub> (1.2041&#xa0;kg/m3), <italic>c</italic>
<sub>
<italic>air</italic>
</sub>, and <italic>p</italic> correspond to the structure normal velocity, air particle velocity, air density, sound speed in air, and acoustic pressure, respectively. The equivalent sound power released from the vibrating structure can be represented as a function of the structure&#x2019;s vibration velocity by substitution of Eq. <xref ref-type="disp-formula" rid="e9">9</xref> into Eq. <xref ref-type="disp-formula" rid="e8">8</xref>. As employed in this study, the equivalent radiated power (<italic>ERP</italic>) and its level (<italic>ERPL</italic>) can be obtained as (<xref ref-type="bibr" rid="B16">Kim et al., 2019</xref>)<disp-formula id="e10">
<mml:math id="m15">
<mml:mrow>
<mml:mi>E</mml:mi>
<mml:mi>R</mml:mi>
<mml:mi>P</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mfrac>
<mml:mrow>
<mml:mn>1</mml:mn>
</mml:mrow>
<mml:mrow>
<mml:mn>2</mml:mn>
</mml:mrow>
</mml:mfrac>
<mml:msub>
<mml:mi>&#x3c1;</mml:mi>
<mml:mrow>
<mml:mi>a</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:msub>
<mml:msub>
<mml:mi>c</mml:mi>
<mml:mrow>
<mml:mi>a</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:msub>
<mml:msub>
<mml:mo>&#x222b;</mml:mo>
<mml:mi mathvariant="italic">&#x393;</mml:mi>
</mml:msub>
<mml:msup>
<mml:mrow>
<mml:mfenced open="|" close="|" separators="|">
<mml:mrow>
<mml:msub>
<mml:mi>v</mml:mi>
<mml:mrow>
<mml:mi>s</mml:mi>
<mml:mo>,</mml:mo>
<mml:mi>n</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mn>2</mml:mn>
</mml:msup>
<mml:mi>d</mml:mi>
<mml:mi mathvariant="italic">&#x393;</mml:mi>
</mml:mrow>
</mml:math>
<label>(10)</label>
</disp-formula>
<disp-formula id="e11">
<mml:math id="m16">
<mml:mrow>
<mml:mi>E</mml:mi>
<mml:mi>R</mml:mi>
<mml:mi>P</mml:mi>
<mml:mi>L</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>10</mml:mn>
<mml:mo>&#x2061;</mml:mo>
<mml:mi>log</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mfrac>
<mml:mrow>
<mml:mi>E</mml:mi>
<mml:mi>R</mml:mi>
<mml:mi>P</mml:mi>
</mml:mrow>
<mml:msub>
<mml:mi>W</mml:mi>
<mml:mrow>
<mml:mi>r</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>f</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mfrac>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mrow>
<mml:mfenced open="[" close="]" separators="|">
<mml:mrow>
<mml:mi>d</mml:mi>
<mml:mi>B</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mi mathvariant="normal">w</mml:mi>
<mml:mi mathvariant="normal">h</mml:mi>
<mml:mi mathvariant="normal">e</mml:mi>
<mml:mi mathvariant="normal">r</mml:mi>
<mml:mi mathvariant="normal">e</mml:mi>
<mml:mtext>&#x2002;</mml:mtext>
<mml:msub>
<mml:mi>W</mml:mi>
<mml:mrow>
<mml:mi>r</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>f</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:msup>
<mml:mn>10</mml:mn>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mn>12</mml:mn>
</mml:mrow>
</mml:msup>
<mml:mrow>
<mml:mfenced open="[" close="]" separators="|">
<mml:mrow>
<mml:mi mathvariant="normal">W</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(11)</label>
</disp-formula>
</p>
<p>The present study proposes a finite element solution using APDL<xref ref-type="fn" rid="fn1">
<sup>1</sup>
</xref> to solve the harmonic problem. By finite element discretization of the integral in Eq. <xref ref-type="disp-formula" rid="e10">10</xref>, the power radiated all over the 3D beam faces can be calculated.</p>
<p>To minimize the radiated power, the power law profile of capacitance is required to be optimally tuned. By substitution of Eq. <xref ref-type="disp-formula" rid="e6">6</xref> into Eq. <xref ref-type="disp-formula" rid="e5">5</xref>, the capacitance profile can be expressed as<disp-formula id="e12">
<mml:math id="m17">
<mml:mrow>
<mml:msub>
<mml:mi>C</mml:mi>
<mml:mrow>
<mml:mi>i</mml:mi>
<mml:mi>j</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:msub>
<mml:mi>C</mml:mi>
<mml:mi mathvariant="italic">max</mml:mi>
</mml:msub>
<mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>1</mml:mn>
<mml:mo>&#x2b;</mml:mo>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>i</mml:mi>
<mml:mo>&#x2212;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mi>r</mml:mi>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mrow>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>n</mml:mi>
</mml:mrow>
</mml:msup>
</mml:mrow>
</mml:math>
<label>(12)</label>
</disp-formula>
</p>
<p>So that optimization of parameters <italic>r</italic> and <italic>n</italic> can offer minimum radiated noise. The area under frequency reponse curve which has been used as a performance measure in some studies (<xref ref-type="bibr" rid="B15">Joshi et al., 2010</xref>; <xref ref-type="bibr" rid="B32">Sarigul et al., 2018</xref>), is considered as the optimization objective function. The optimization algorithm is provided by Eq. <xref ref-type="disp-formula" rid="e13">13</xref>.<disp-formula id="e13">
<mml:math id="m18">
<mml:mrow>
<mml:mfenced open="{" close="" separators="|">
<mml:mrow>
<mml:mtable columnalign="center">
<mml:mtr>
<mml:mtd>
<mml:mrow>
<mml:mi mathvariant="italic">Min</mml:mi>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mi>U</mml:mi>
</mml:mrow>
</mml:mtd>
</mml:mtr>
<mml:mtr>
<mml:mtd>
<mml:mrow>
<mml:mi>U</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:msubsup>
<mml:mo>&#x222b;</mml:mo>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mi mathvariant="italic">min</mml:mi>
</mml:msub>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mi mathvariant="italic">max</mml:mi>
</mml:msub>
</mml:msubsup>
<mml:mi>E</mml:mi>
<mml:mi>R</mml:mi>
<mml:mi>P</mml:mi>
<mml:mtext>&#x2009;</mml:mtext>
<mml:mi>d</mml:mi>
<mml:mi>f</mml:mi>
<mml:mo>,</mml:mo>
<mml:mo>&#x2003;</mml:mo>
<mml:msub>
<mml:mi>U</mml:mi>
<mml:mi mathvariant="italic">min</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mi>U</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msub>
<mml:mi>C</mml:mi>
<mml:mrow>
<mml:mi>o</mml:mi>
<mml:mi>p</mml:mi>
<mml:mi>t</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:mtd>
</mml:mtr>
<mml:mtr>
<mml:mtd>
<mml:mrow>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mi mathvariant="italic">min</mml:mi>
</mml:msub>
<mml:mo>&#x2b;</mml:mo>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mi mathvariant="italic">max</mml:mi>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>2</mml:mn>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mrow>
<mml:mi>r</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>s</mml:mi>
<mml:mi>o</mml:mi>
<mml:mi>n</mml:mi>
<mml:mi>a</mml:mi>
<mml:mi>n</mml:mi>
<mml:mi>c</mml:mi>
<mml:mi>e</mml:mi>
</mml:mrow>
</mml:msub>
</mml:mrow>
</mml:mtd>
</mml:mtr>
</mml:mtable>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:math>
<label>(13)</label>
</disp-formula>Where <italic>C</italic>
<sub>opt</sub> can be obtained based on optimum values of <italic>r</italic> and <italic>n</italic>. Thus, for semi-active noise isolation, the optimization must be conducted for frequency intervals centered by the resonance frequency. Then, the semi-active treatment function for a frequency range including <italic>N</italic> number of eigenfrequencies can be expressed as follows.<disp-formula id="e14">
<mml:math id="m19">
<mml:mrow>
<mml:msub>
<mml:mi>C</mml:mi>
<mml:mrow>
<mml:mi>s</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>m</mml:mi>
<mml:mi>i</mml:mi>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>a</mml:mi>
<mml:mi>c</mml:mi>
<mml:mi>t</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>v</mml:mi>
<mml:mi>e</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mrow>
<mml:munderover>
<mml:mstyle displaystyle="true">
<mml:mo>&#x2211;</mml:mo>
</mml:mstyle>
<mml:mrow>
<mml:mi>i</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
<mml:mi>N</mml:mi>
</mml:munderover>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:msub>
<mml:mi>C</mml:mi>
<mml:msub>
<mml:mrow>
<mml:mi>o</mml:mi>
<mml:mi>p</mml:mi>
<mml:mi>t</mml:mi>
</mml:mrow>
<mml:mi>i</mml:mi>
</mml:msub>
</mml:msub>
<mml:msup>
<mml:mi>H</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x2b;</mml:mo>
<mml:msub>
<mml:mi>C</mml:mi>
<mml:mrow>
<mml:mi>S</mml:mi>
<mml:mi>H</mml:mi>
<mml:mi>C</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mn>1</mml:mn>
<mml:mo>&#x2212;</mml:mo>
<mml:msup>
<mml:mi>H</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(14)</label>
</disp-formula>Where <italic>H</italic>
<sup>
<italic>&#x2a;</italic>
</sup> is a distribution function defined by Heaviside functions as given by Eq. <xref ref-type="disp-formula" rid="e15">15</xref>.<disp-formula id="e15">
<mml:math id="m20">
<mml:mrow>
<mml:msup>
<mml:mi>H</mml:mi>
<mml:mo>&#x2a;</mml:mo>
</mml:msup>
<mml:mo>&#x3d;</mml:mo>
<mml:mrow>
<mml:mi>H</mml:mi>
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<mml:mi>a</mml:mi>
<mml:mi>v</mml:mi>
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<mml:mi>i</mml:mi>
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<mml:mi>e</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>f</mml:mi>
<mml:mo>&#x2212;</mml:mo>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mi mathvariant="italic">min</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x2b;</mml:mo>
<mml:mrow>
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<mml:mi>e</mml:mi>
</mml:mrow>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="|">
<mml:mrow>
<mml:mi>f</mml:mi>
<mml:mo>&#x2212;</mml:mo>
<mml:msub>
<mml:mi>f</mml:mi>
<mml:mi mathvariant="italic">max</mml:mi>
</mml:msub>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(15)</label>
</disp-formula>
</p>
<p>The semi-active function (Eq. <xref ref-type="disp-formula" rid="e14">14</xref>) allows to select the frequency intervals for isolation based on the optimal capacitance profile, and deselect the frequency intervals where the isolator is not effective by short-circuiting the piezo-patches. Accordingly, the short circuit capacitance equals to zero (<italic>C</italic>
<sub>
<italic>SHC</italic>
</sub>). Therefore, the semi-active treatment function can be expressed as<disp-formula id="e16">
<mml:math id="m21">
<mml:mrow>
<mml:msub>
<mml:mi>C</mml:mi>
<mml:mrow>
<mml:mi>s</mml:mi>
<mml:mi>e</mml:mi>
<mml:mi>m</mml:mi>
<mml:mi>i</mml:mi>
<mml:mo>&#x2212;</mml:mo>
<mml:mi>a</mml:mi>
<mml:mi>c</mml:mi>
<mml:mi>t</mml:mi>
<mml:mi>i</mml:mi>
<mml:mi>v</mml:mi>
<mml:mi>e</mml:mi>
</mml:mrow>
</mml:msub>
<mml:mo>&#x3d;</mml:mo>
<mml:mrow>
<mml:munderover>
<mml:mstyle displaystyle="true">
<mml:mo>&#x2211;</mml:mo>
</mml:mstyle>
<mml:mrow>
<mml:mi>i</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>1</mml:mn>
</mml:mrow>
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</mml:munderover>
<mml:mrow>
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</mml:mrow>
</mml:mrow>
</mml:mrow>
</mml:math>
<label>(16)</label>
</disp-formula>
</p>
</sec>
<sec sec-type="results" id="s3">
<title>3 Results</title>
<p>At first, a validation study is carried out to check the accuracy of present numerical modeling. Next, the numerical model for realization of ABH effect is introduced and considered for parametric studies. Based on optimization of parametric studies results, a semi-active noise treatment is applied.</p>
<sec id="s3-1">
<title>3.1 Validation of numerical modeling</title>
<p>The present numerical model has been validated by comparison with numerical findings reported by Larbi and De&#xfc; (<xref ref-type="bibr" rid="B18">Larbi and De&#xfc;, 2019</xref>). Using solid elements for the host structure and Circu94 elements for the piezoelectric patch, calculations have been made for the eigenanalysis of a cantilever steel beam with a piezoelectric PIC 151 ceramic patch (see <xref ref-type="fig" rid="F5">Figure 5</xref>) which properties are given by <xref ref-type="table" rid="T1">Table 1</xref>. Both open- and short-circuit conditions are considered to obtain the results for the eigenanalysis. The discrepancy of results reported by <xref ref-type="table" rid="T2">Table 2</xref> attributes to different finite element modeling techniques as well as different elements type and number.</p>
<fig id="F5" position="float">
<label>FIGURE 5</label>
<caption>
<p>Cantilever beam with piezoelectric element attachment: dimensions.</p>
</caption>
<graphic xlink:href="fmech-09-1126489-g005.tif"/>
</fig>
<table-wrap id="T1" position="float">
<label>TABLE 1</label>
<caption>
<p>Material properties for the cantilever beam and piezoelectric ceramic patch.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th colspan="2" align="left">Material: PIC 151 <xref ref-type="bibr" rid="B30">Pereira Da Silva et al. (2015)</xref>
</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="left">Density</td>
<td align="left">7,780&#xa0;kg/m<sup>3</sup>
</td>
</tr>
<tr>
<td align="left">Elasticity Coefficient</td>
<td rowspan="2" align="left">{1.683, 1.900, &#x2212;0.5656, &#x2212;0.7107, 5.096, 4.497}(10<sup>&#x2212;11</sup>)</td>
</tr>
<tr>
<td align="left">{<inline-formula id="inf6">
<mml:math id="m22">
<mml:mrow>
<mml:msubsup>
<mml:mi>S</mml:mi>
<mml:mn>11</mml:mn>
<mml:mi>E</mml:mi>
</mml:msubsup>
<mml:mo>,</mml:mo>
<mml:msubsup>
<mml:mi>S</mml:mi>
<mml:mn>33</mml:mn>
<mml:mi>E</mml:mi>
</mml:msubsup>
<mml:mo>,</mml:mo>
<mml:msubsup>
<mml:mi>S</mml:mi>
<mml:mn>12</mml:mn>
<mml:mi>E</mml:mi>
</mml:msubsup>
<mml:mo>,</mml:mo>
<mml:msubsup>
<mml:mi>S</mml:mi>
<mml:mn>13</mml:mn>
<mml:mi>E</mml:mi>
</mml:msubsup>
<mml:mo>,</mml:mo>
<mml:msubsup>
<mml:mi>S</mml:mi>
<mml:mn>44</mml:mn>
<mml:mi>E</mml:mi>
</mml:msubsup>
<mml:mo>,</mml:mo>
<mml:msubsup>
<mml:mi>S</mml:mi>
<mml:mn>66</mml:mn>
<mml:mi>E</mml:mi>
</mml:msubsup>
</mml:mrow>
</mml:math>
</inline-formula>}</td>
</tr>
<tr>
<td align="left">Piezoelectric Coefficient</td>
<td rowspan="2" align="left">{-9.6, 15.10.12.00} N/Vm</td>
</tr>
<tr>
<td align="left">{<inline-formula id="inf7">
<mml:math id="m23">
<mml:mrow>
<mml:msub>
<mml:mi>e</mml:mi>
<mml:mn>31</mml:mn>
</mml:msub>
<mml:mo>,</mml:mo>
<mml:msub>
<mml:mi>e</mml:mi>
<mml:mn>33</mml:mn>
</mml:msub>
<mml:mo>,</mml:mo>
<mml:msub>
<mml:mi>e</mml:mi>
<mml:mn>15</mml:mn>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula>}</td>
</tr>
<tr>
<td align="left">Dielectric Coefficient</td>
<td rowspan="2" align="left">{9.82, 7.54}(10<sup>&#x2212;9</sup>) F/m</td>
</tr>
<tr>
<td align="left">{<inline-formula id="inf8">
<mml:math id="m24">
<mml:mrow>
<mml:msubsup>
<mml:mi>&#x3f5;</mml:mi>
<mml:mn>11</mml:mn>
<mml:mi>&#x3b5;</mml:mi>
</mml:msubsup>
<mml:mo>,</mml:mo>
<mml:msubsup>
<mml:mi>&#x3f5;</mml:mi>
<mml:mn>33</mml:mn>
<mml:mi>&#x3b5;</mml:mi>
</mml:msubsup>
</mml:mrow>
</mml:math>
</inline-formula>}</td>
</tr>
<tr>
<td colspan="2" align="left">Material: Aluminum <xref ref-type="bibr" rid="B18">Larbi and De&#xfc; (2019)</xref>
</td>
</tr>
<tr>
<td align="left">&#x2003;Density</td>
<td align="left">2,700&#xa0;kg/m<sup>3</sup>
</td>
</tr>
<tr>
<td align="left">&#x2003;Elasticity</td>
<td align="left">74&#xa0;GPa</td>
</tr>
<tr>
<td align="left">&#x2003;Poisson&#x2019;s ratio</td>
<td align="left">0.33</td>
</tr>
</tbody>
</table>
</table-wrap>
<table-wrap id="T2" position="float">
<label>TABLE 2</label>
<caption>
<p>Verification of numerical simulation for a cantilever with open/short shunt circuit.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th align="left">Mode type</th>
<th colspan="2" align="left">Short circuit frequencies [Hz]</th>
<th colspan="2" align="left">Open circuit frequencies [Hz]</th>
</tr>
<tr>
<th align="left"/>
<th align="left">
<xref ref-type="bibr" rid="B18">Larbi and De&#xfc; (2019)</xref>
</th>
<th align="left">Present study</th>
<th align="left">
<xref ref-type="bibr" rid="B18">Larbi and De&#xfc; (2019)</xref>
</th>
<th align="left">Present study</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="center">
<italic>F</italic>
</td>
<td align="left">71.89</td>
<td align="left">75.296</td>
<td align="left">73.48</td>
<td align="left">75.363</td>
</tr>
<tr>
<td align="center">
<italic>F</italic>
</td>
<td align="left">379.49</td>
<td align="left">390.83</td>
<td align="left">383.97</td>
<td align="left">392.35</td>
</tr>
<tr>
<td align="center">
<italic>F</italic>
<sub>
<italic>i</italic>
</sub>
</td>
<td align="left">587.02</td>
<td align="left">602.96</td>
<td align="left">587.02</td>
<td align="left">610.22</td>
</tr>
<tr>
<td align="center">
<italic>F</italic>
</td>
<td align="left">969.11</td>
<td align="left">981.06</td>
<td align="left">970.05</td>
<td align="left">988.25</td>
</tr>
<tr>
<td align="center">
<italic>T</italic>
</td>
<td align="left">1048.71</td>
<td align="left">1078.2</td>
<td align="left">1048.71</td>
<td align="left">1078.6</td>
</tr>
</tbody>
</table>
</table-wrap>
</sec>
<sec id="s3-2">
<title>3.2 Numerical realization of virtual ABH effect</title>
<p>For the numerical realization of virtual ABH effect, a steel cantilever beam with <italic>L</italic>
<sub>
<italic>b</italic>
</sub> &#x3d; 11.19&#xa0;cm length, <italic>W</italic>
<sub>
<italic>b</italic>
</sub> &#x3d; 5&#xa0;mm width, and <italic>T</italic>
<sub>
<italic>b</italic>
</sub> &#x3d; 1&#xa0;mm thickness is assumed. The beam is covered by 20 piezoelectric elements with <italic>L</italic>
<sub>
<italic>p</italic>
</sub> &#x3d; 5&#xa0;mm edge length, and <italic>T</italic>
<sub>
<italic>p</italic>
</sub> &#x3d; 0.3<italic>T</italic>
<sub>
<italic>b</italic>
</sub> thickness positioned at equal distances to each other. The beam is excited by harmonic out-of-plane displacement applied at the free end. A structural damping coefficient of 0.01 is adopted (<xref ref-type="bibr" rid="B8">Devasia et al., 1993</xref>).</p>
<p>The ERPL response for the beam structure with shorted shunt circuit is presented by <xref ref-type="fig" rid="F6">Figure 6</xref>. As a result, the three eigenmodes dominant in the <italic>ERPL</italic> response are targeted for attenuation.</p>
<fig id="F6" position="float">
<label>FIGURE 6</label>
<caption>
<p>ERPL response of the beam when the shunt circuit is shorted.</p>
</caption>
<graphic xlink:href="fmech-09-1126489-g006.tif"/>
</fig>
<sec id="s3-2-1">
<title>3.2.1 Parametric study</title>
<p>Parametric studies are carried out to figure out the influence of power law formulation constants (<italic>n</italic> and <italic>r</italic>) described by Eq. <xref ref-type="disp-formula" rid="e12">12</xref>, on the structure response. In this regard, particular capacitance profiles assigned for the first three modes of resonance which contribute to the overall radiated noise are given by <xref ref-type="fig" rid="F7">Figure 7</xref>. The capacitance profiles are minimum and maximum at nodes and antinodes of vibration displacement mode shape, respectively. Between each node and antinode, the capacitance varies according to power law formulation.</p>
<fig id="F7" position="float">
<label>FIGURE 7</label>
<caption>
<p>
<bold>(A)</bold> Capacitance profiles (<italic>r</italic> &#x3d; 0.02, <italic>n</italic> &#x3d; 4) adopted for different resonance modes, <bold>(B)</bold> eigenmode shapes.</p>
</caption>
<graphic xlink:href="fmech-09-1126489-g007.tif"/>
</fig>
<p>The results of parametric studies are reported by <xref ref-type="fig" rid="F8">Figures 8</xref>&#x2013;<xref ref-type="fig" rid="F13">13</xref>. It is well revealed that the capacitance profile constants (<italic>n</italic> and <italic>r</italic>) are the tuning parameters responsible for the radiated power response. Compared to the short-circuit case, the application of virtual ABH effect results a heavily fluctuant response due to trapping the elastic wave.</p>
<fig id="F8" position="float">
<label>FIGURE 8</label>
<caption>
<p>ERPL around the first mode of resonance, <italic>n</italic> &#x3d; 4, &#x336; short circuit, &#x336; r &#x3d; 0.02, &#x336; r &#x3d; 0.03, &#x336; r &#x3d; 0.04, &#x336; r &#x3d; 0.05.</p>
</caption>
<graphic xlink:href="fmech-09-1126489-g008.tif"/>
</fig>
<fig id="F9" position="float">
<label>FIGURE 9</label>
<caption>
<p>ERPL around the first mode of resonance, <italic>n</italic> &#x3d; 5, &#x336; short circuit, &#x336; r &#x3d; 0.02, &#x336; r &#x3d; 0.03, &#x336; r &#x3d; 0.04, &#x336; r &#x3d; 0.05.</p>
</caption>
<graphic xlink:href="fmech-09-1126489-g009.tif"/>
</fig>
<fig id="F10" position="float">
<label>FIGURE 10</label>
<caption>
<p>ERPL around the second mode of resonance, <italic>n</italic> &#x3d; 4, &#x336; short circuit, &#x336; r &#x3d; 0.02, &#x336; r &#x3d; 0.03, &#x336; r &#x3d; 0.04, &#x336; r &#x3d; 0.05.</p>
</caption>
<graphic xlink:href="fmech-09-1126489-g010.tif"/>
</fig>
<fig id="F11" position="float">
<label>FIGURE 11</label>
<caption>
<p>ERPL around the second mode of resonance, <italic>n</italic> &#x3d; 5, &#x336; short circuit, &#x336; r &#x3d; 0.02, &#x336; r &#x3d; 0.03, &#x336; r &#x3d; 0.04, &#x336; r &#x3d; 0.05.</p>
</caption>
<graphic xlink:href="fmech-09-1126489-g011.tif"/>
</fig>
<fig id="F12" position="float">
<label>FIGURE 12</label>
<caption>
<p>ERPL around the third mode of resonance, <italic>n</italic> &#x3d; 4, &#x336; short circuit, &#x336; r &#x3d; 0.02, &#x336; r &#x3d; 0.03, &#x336; r &#x3d; 0.04, &#x336; r &#x3d; 0.05.</p>
</caption>
<graphic xlink:href="fmech-09-1126489-g012.tif"/>
</fig>
<fig id="F13" position="float">
<label>FIGURE 13</label>
<caption>
<p>ERPL around the third mode of resonance, <italic>n</italic> &#x3d; 5, &#x336; short circuit, &#x336; r &#x3d; 0.02, &#x336; r &#x3d; 0.03, &#x336; r &#x3d; 0.04, &#x336; r &#x3d; 0.05.</p>
</caption>
<graphic xlink:href="fmech-09-1126489-g013.tif"/>
</fig>
</sec>
<sec id="s3-2-2">
<title>3.2.2 Semi-active noise isolation</title>
<p>The results of parametric studies reported by <xref ref-type="fig" rid="F8">Figures 8</xref>&#x2013;<xref ref-type="fig" rid="F13">13</xref> are considered for optimization. So that the optimal values of <italic>r</italic> and <italic>n</italic> are chosen for each mode of resonance. The vibrating beam is treated semi-actively considering optimal parameters of (<italic>r</italic>, <italic>n</italic>) taken as (0.02, 5), (0.04, 5), and (0.05, 4), respectively for the first, the second and the third targeted modes of resonance. The treatment is applied at the vicinity of resonance with a radius of 10&#xa0;Hz. The semi-active treatment function is expressed as follows.<disp-formula id="e17">
<mml:math id="m25">
<mml:mrow>
<mml:mtable columnalign="left">
<mml:mtr>
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<mml:mi>c</mml:mi>
<mml:mi>t</mml:mi>
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</mml:mrow>
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<mml:mo>&#x3d;</mml:mo>
<mml:msub>
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<mml:mrow>
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<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.02</mml:mn>
<mml:mo>,</mml:mo>
<mml:mi>n</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>5</mml:mn>
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</mml:mrow>
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<mml:mo>&#x2a;</mml:mo>
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</mml:msup>
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<mml:mrow>
<mml:mi>f</mml:mi>
<mml:mo>&#x2212;</mml:mo>
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</mml:mrow>
</mml:mfenced>
</mml:mrow>
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<mml:msup>
<mml:mi>H</mml:mi>
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<mml:mrow>
<mml:mi>f</mml:mi>
<mml:mo>&#x2212;</mml:mo>
<mml:mn>335</mml:mn>
</mml:mrow>
</mml:mfenced>
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</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:mtd>
</mml:mtr>
<mml:mtr>
<mml:mtd>
<mml:mrow>
<mml:mo>&#x2b;</mml:mo>
<mml:mo>&#x2026;</mml:mo>
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<mml:mi>C</mml:mi>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="&#x7c;">
<mml:mrow>
<mml:mi>r</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>0.04</mml:mn>
<mml:mo>,</mml:mo>
<mml:mi>n</mml:mi>
<mml:mo>&#x3d;</mml:mo>
<mml:mn>5</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:msub>
<mml:mo>&#x2a;</mml:mo>
<mml:mrow>
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</mml:msup>
<mml:mrow>
<mml:mfenced open="(" close=")" separators="&#x7c;">
<mml:mrow>
<mml:mi>f</mml:mi>
<mml:mo>&#x2212;</mml:mo>
<mml:mn>1042</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
<mml:mo>&#x2b;</mml:mo>
<mml:msup>
<mml:mi>H</mml:mi>
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<mml:mrow>
<mml:mfenced open="(" close=")" separators="&#x7c;">
<mml:mrow>
<mml:mi>f</mml:mi>
<mml:mo>&#x2212;</mml:mo>
<mml:mn>1062</mml:mn>
</mml:mrow>
</mml:mfenced>
</mml:mrow>
</mml:mrow>
</mml:mfenced>
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</mml:mtr>
</mml:mtable>
</mml:mrow>
</mml:math>
<label>(17)</label>
</disp-formula>
</p>
<p>The results of this semi-active treatment is represented by <xref ref-type="fig" rid="F14">Figure 14</xref>. The radiated power is attenuated by the rates of 10.29%, 6.37%, and 7.47% from the first to the last targeted modes, respectively.</p>
<fig id="F14" position="float">
<label>FIGURE 14</label>
<caption>
<p>ERPL frequency response with and without semi-active treatment.</p>
</caption>
<graphic xlink:href="fmech-09-1126489-g014.tif"/>
</fig>
<p>In order to assess the influence of loading, harmonic excitations with <inline-formula id="inf9">
<mml:math id="m26">
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<mml:mi>u</mml:mi>
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</inline-formula>, and <inline-formula id="inf10">
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</mml:mrow>
<mml:mn>0</mml:mn>
</mml:msub>
</mml:mrow>
</mml:math>
</inline-formula> amplitudes are imposed. The results reported by <xref ref-type="fig" rid="F15">Figure 15</xref> indicate the system is linear for all studied resonances with and without treatment.</p>
<fig id="F15" position="float">
<label>FIGURE 15</label>
<caption>
<p>ERPL frequency response with different excitation amplitudes.</p>
</caption>
<graphic xlink:href="fmech-09-1126489-g015.tif"/>
</fig>
</sec>
</sec>
</sec>
<sec sec-type="conclusion" id="s4">
<title>4 Conclusion</title>
<p>A numerical model is developed to realize the ABH effect virtually with the help of capacitive shunt circuits. The main objective is to attenuate structure-born noise for several resonance modes by proposing a semi-active approach. Theoretically, virtually imposing the ABH effect is feasible through the electrical analogy which equalizes stiffness with capacitance.</p>
<p>A noteworthy advantage of virtual ABH effect is the potential for semi-active use which is obviously impossible with the ABH effect imposed by geometry. In addition, the geometrical restrictions related to the physical manifestation of the ABH effect do not apply to the virtual method.</p>
<p>For two main reasons the virtual ABH effect deviates from the ideal ABH effect: 1. Since the energy conversion rate in piezoelectric material is not 100%, the ABH effect can never be idealized. 2. The capacitance profile is discrete along the beam due to the distance between piezoelectric elements which is unavoidable.</p>
<p>The results of present numerical modeling for the first eigenmodes which contribute in overall radiated noise revealed at least 6.37% improvement for noise radiation. The attenuation is well achieved by breaking down each peak to many more peaks which results an effective absorption effect. Although the present approach targets the first three eigenmodes, expanding the effective frequency range requires an increasing of the number of piezo-patches to tune the shunt impedance with respect to the eigenmode shapes.</p>
<p>Finally, due to the weight and space limitation in vehicle and aero applications, the structures are too thin to be carved out for an ABH geometric profile. Thus, the virtual ABH effect can be considered as a solution not only to overcome the mentioned restriction, but also to apply a multi-mode structural noise isolation.</p>
</sec>
</body>
<back>
<sec sec-type="data-availability" id="s5">
<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="s6">
<title>Author contributions</title>
<p>SS conceived and formulated the problem, developed the macro-code, analyzed the results, and wrote the paper. GP, FF, and SD supervised the research work as academic supervisors and reviewed the manuscript. PK supervised the research as an industry supervisor.</p>
</sec>
<sec id="s7">
<title>Funding</title>
<p>This project has received funding from the European Union&#x2019;s Horizon 2020 research and innovation program under the Marie Sk&#x142;odowska-Curie grant agreement No 860243.</p>
</sec>
<ack>
<p>The author would like to acknowledge all the Institutions and Partners involved within the LIVE-I project.</p>
</ack>
<sec sec-type="COI-statement" id="s8">
<title>Conflict of interest</title>
<p>Author PK was employed by the company Adaptronica sp z o o, R&#x26;D Company.</p>
<p>The remaining 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="s9">
<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>
<fn-group>
<fn id="fn1">
<label>1</label>
<p>ANSYS Parametric Design Language.</p>
</fn>
</fn-group>
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<sec id="s10">
<title>Nomenclature</title>
<def-list>
<def-item>
<term id="G1-fmech.2023.1126489">
<bold>
<italic>a</italic>
</bold>
<sub>
<bold>
<italic>i</italic>
</bold>
</sub>
</term>
<def>
<p>arithmetic progression element</p>
</def>
</def-item>
<def-item>
<term id="G2-fmech.2023.1126489">
<bold>
<italic>b</italic>
</bold>
</term>
<def>
<p>damping coefficient</p>
</def>
</def-item>
<def-item>
<term id="G3-fmech.2023.1126489">
<bold>
<italic>C</italic>
</bold>
</term>
<def>
<p>capacitance</p>
</def>
</def-item>
<def-item>
<term id="G4-fmech.2023.1126489">
<bold>
<italic>c</italic>
</bold>
<sub>
<bold>
<italic>air</italic>
</bold>
</sub>
</term>
<def>
<p>sound speed in air</p>
</def>
</def-item>
<def-item>
<term id="G5-fmech.2023.1126489">
<bold>
<italic>C</italic>
</bold>
<sub>
<bold>
<italic>i</italic>
</bold>
</sub>
</term>
<def>
<p>the capacitance corresponding to the i<sup>th</sup> capacitor</p>
</def>
</def-item>
<def-item>
<term id="G6-fmech.2023.1126489">
<bold>
<italic>C</italic>
</bold>
<sub>
<bold>
<italic>max</italic>
</bold>
</sub>
</term>
<def>
<p>maximum capacitance</p>
</def>
</def-item>
<def-item>
<term id="G7-fmech.2023.1126489">
<bold>
<italic>C</italic>
</bold>
<sub>
<bold>
<italic>opt</italic>
</bold>
</sub>
</term>
<def>
<p>Optimal capacitance profile</p>
</def>
</def-item>
<def-item>
<term id="G8-fmech.2023.1126489">
<bold>
<italic>C</italic>
</bold>
<sub>
<bold>
<italic>semi-active</italic>
</bold>
</sub>
</term>
<def>
<p>Semi-active treatment function</p>
</def>
</def-item>
<def-item>
<term id="G9-fmech.2023.1126489">
<bold>
<italic>F</italic>
</bold>
</term>
<def>
<p>force</p>
</def>
</def-item>
<def-item>
<term id="G10-fmech.2023.1126489">
<bold>
<italic>H</italic>
</bold>
<sup>
<bold>
<italic>&#x2a;</italic>
</bold>
</sup>
</term>
<def>
<p>A distribution function</p>
</def>
</def-item>
<def-item>
<term id="G11-fmech.2023.1126489">
<bold>
<italic>I</italic>
</bold>
</term>
<def>
<p>sound intensity</p>
</def>
</def-item>
<def-item>
<term id="G12-fmech.2023.1126489">
<bold>
<italic>k</italic>
</bold>
</term>
<def>
<p>stiffness</p>
</def>
</def-item>
<def-item>
<term id="G13-fmech.2023.1126489">
<bold>
<italic>k</italic>
</bold>
<sub>
<bold>
<italic>p</italic>
</bold>
</sub>
</term>
<def>
<p>wave number of quasi-longitudinal waves</p>
</def>
</def-item>
<def-item>
<term id="G14-fmech.2023.1126489">
<bold>
<italic>L</italic>
</bold>
</term>
<def>
<p>inductance</p>
</def>
</def-item>
<def-item>
<term id="G15-fmech.2023.1126489">
<bold>
<italic>l</italic>
</bold>
<sub>
<bold>
<italic>1</italic>
</bold>
</sub> and <bold>
<italic>l</italic>
</bold>
<sub>
<bold>
<italic>2</italic>
</bold>
</sub>
</term>
<def>
<p>the portions of length on a typical beam</p>
</def>
</def-item>
<def-item>
<term id="G16-fmech.2023.1126489">
<bold>
<italic>m</italic>
</bold>
</term>
<def>
<p>mass</p>
</def>
</def-item>
<def-item>
<term id="G17-fmech.2023.1126489">
<bold>
<italic>n</italic>
</bold>
</term>
<def>
<p>the power corresponding to power law</p>
</def>
</def-item>
<def-item>
<term id="G18-fmech.2023.1126489">
<bold>
<italic>p</italic>
</bold>
</term>
<def>
<p>sound pressure</p>
</def>
</def-item>
<def-item>
<term id="G19-fmech.2023.1126489">
<bold>
<italic>P</italic>
</bold>
</term>
<def>
<p>sound power</p>
</def>
</def-item>
<def-item>
<term id="G20-fmech.2023.1126489">
<bold>
<italic>r</italic>
</bold>
</term>
<def>
<p>the common difference between terms in an arithmetic progression</p>
</def>
</def-item>
<def-item>
<term id="G21-fmech.2023.1126489">
<bold>
<italic>t</italic>
</bold>
</term>
<def>
<p>time</p>
</def>
</def-item>
<def-item>
<term id="G22-fmech.2023.1126489">
<bold>
<italic>u</italic>
</bold>
</term>
<def>
<p>displacement</p>
</def>
</def-item>
<def-item>
<term id="G23-fmech.2023.1126489">
<bold>
<italic>v</italic>
</bold>
</term>
<def>
<p>velocity</p>
</def>
</def-item>
<def-item>
<term id="G24-fmech.2023.1126489">
<bold>
<italic>v</italic>
</bold>
<sub>
<bold>
<italic>s,n</italic>
</bold>
</sub>
</term>
<def>
<p>the velocity normal to a surface element</p>
</def>
</def-item>
<def-item>
<term id="G25-fmech.2023.1126489">
<bold>
<italic>v</italic>
</bold>
<sub>
<bold>
<italic>air</italic>
</bold>
</sub>
</term>
<def>
<p>air velocity</p>
</def>
</def-item>
<def-item>
<term id="G26-fmech.2023.1126489">
<bold>
<italic>V</italic>
</bold>
</term>
<def>
<p>voltage</p>
</def>
</def-item>
<def-item>
<term id="G27-fmech.2023.1126489">
<bold>
<italic>W</italic>
</bold>
<sub>
<bold>
<italic>ref</italic>
</bold>
</sub>
</term>
<def>
<p>reference power</p>
</def>
</def-item>
<def-item>
<term id="G28-fmech.2023.1126489">
<bold>
<italic>&#x393;</italic>
</bold>
</term>
<def>
<p>area</p>
</def>
</def-item>
<def-item>
<term id="G29-fmech.2023.1126489">
<bold>
<italic>&#x3c1;</italic>
</bold>
<sub>
<bold>
<italic>air</italic>
</bold>
</sub>
</term>
<def>
<p>air density</p>
</def>
</def-item>
<def-item>
<term id="G30-fmech.2023.1126489">
<bold>
<italic>&#x3c4;</italic>
</bold>
</term>
<def>
<p>wave transit time through a wedge</p>
</def>
</def-item>
</def-list>
<sec>
<title>Subscriptions</title>
<def-list>
<def-item>
<term id="G31-fmech.2023.1126489">
<bold>
<italic>ERP</italic>
</bold>
</term>
<def>
<p>equivalent radiated power</p>
</def>
</def-item>
<def-item>
<term id="G32-fmech.2023.1126489">
<bold>
<italic>ERPL</italic>
</bold>
</term>
<def>
<p>equivalent radiated power level</p>
</def>
</def-item>
</def-list>
</sec>
</sec>
</back>
</article>