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<front>
<journal-meta>
<journal-id journal-id-type="pmc">SV</journal-id>
<journal-id journal-id-type="nlm-ta">SV</journal-id>
<journal-id journal-id-type="publisher-id">SV</journal-id>
<journal-title-group>
<journal-title>Sound &#x0026; Vibration</journal-title>
</journal-title-group>
<issn pub-type="epub">2693-1443</issn>
<issn pub-type="ppub">1541-0161</issn>
<publisher>
<publisher-name>Tech Science Press</publisher-name>
<publisher-loc>USA</publisher-loc>
</publisher>
</journal-meta>
<article-meta>
<article-id pub-id-type="publisher-id">56968</article-id>
<article-id pub-id-type="doi">10.32604/sv.2024.056968</article-id>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Article</subject>
</subj-group>
</article-categories>
<title-group>
<article-title>Sound Transmission Loss of Helmholtz Resonators with Elastic Bottom Plate</article-title><alt-title alt-title-type="left-running-head">Sound Transmission Loss of Helmholtz Resonators with Elastic Bottom Plate</alt-title><alt-title alt-title-type="right-running-head">Sound Transmission Loss of Helmholtz Resonators with Elastic Bottom Plate</alt-title>
</title-group>
<contrib-group>
<contrib id="author-1" contrib-type="author">
<name name-style="western"><surname>Yang</surname><given-names>Liang</given-names></name>
<xref ref-type="aff" rid="aff-1">1</xref>
<xref ref-type="aff" rid="aff-2">2</xref>
</contrib>
<contrib id="author-2" contrib-type="author">
<name name-style="western"><surname>Zhang</surname><given-names>Jie</given-names></name>
<xref ref-type="aff" rid="aff-1">1</xref>
</contrib>
<contrib id="author-3" contrib-type="author">
<name name-style="western"><surname>Xia</surname><given-names>Jinfeng</given-names></name>
<xref ref-type="aff" rid="aff-1">1</xref>
</contrib>
<contrib id="author-4" contrib-type="author">
<name name-style="western"><surname>Zhang</surname><given-names>Siwen</given-names></name>
<xref ref-type="aff" rid="aff-1">1</xref>
</contrib>
<contrib id="author-5" contrib-type="author">
<name name-style="western"><surname>Yang</surname><given-names>Yang</given-names></name>
<xref ref-type="aff" rid="aff-3">3</xref>
</contrib>
<contrib id="author-6" contrib-type="author" corresp="yes">
<name name-style="western"><surname>Chu</surname><given-names>Zhigang</given-names></name>
<xref ref-type="aff" rid="aff-2">2</xref><email>zgchu@cqu.edu.cn</email>
</contrib>
<aff id="aff-1"><label>1</label><institution>State Key Laboratory of Intelligent Vehicle Safety Technology, Chongqing Changan Automobile Co., Ltd.</institution>, <addr-line>Chongqing, 401133</addr-line>, <country>China</country></aff>
<aff id="aff-2"><label>2</label><institution>College of Mechanical and Vehicle Engineering, Chongqing University</institution>, <addr-line>Chongqing, 400044</addr-line>, <country>China</country></aff>
<aff id="aff-3"><label>3</label><institution>Chongqing Automotive Power System Testing Engineering Technology Research Center, School of Vehicles Engineering, Chongqing Industry Polytechnic College</institution>, <addr-line>Chongqing, 401120</addr-line>, <country>China</country></aff>
</contrib-group><author-notes><corresp id="cor1"><label>&#x002A;</label>Corresponding Author: Zhigang Chu. Email: <email>zgchu@cqu.edu.cn</email></corresp></author-notes>
<pub-date date-type="collection" publication-format="electronic">
<year>2024</year></pub-date>
<pub-date date-type="pub" publication-format="electronic"><day>21</day><month>10</month><year>2024</year></pub-date>
<volume>58</volume>
<issue>00</issue>
<fpage>171</fpage>
<lpage>183</lpage>
<history>
<date date-type="received"><day>03</day><month>8</month><year>2024</year></date>
<date date-type="accepted"><day>30</day><month>9</month><year>2024</year></date>
</history>
<permissions>
<copyright-statement>&#x00A9; 2024 The Authors.</copyright-statement>
<copyright-year>2024</copyright-year>
<copyright-holder>Published by Tech Science Press.</copyright-holder>
<license xlink:href="https://creativecommons.org/licenses/by/4.0/">
<license-p>This work is licensed under a <ext-link ext-link-type="uri" xlink:type="simple" xlink:href="https://creativecommons.org/licenses/by/4.0/">Creative Commons Attribution 4.0 International License</ext-link>, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.</license-p>
</license>
</permissions>
<self-uri content-type="pdf" xlink:href="TSP_SV_56968.pdf"></self-uri>
<abstract>
<p>Helmholtz resonators are widely used to control low frequency noise propagating in pipes. In this paper, the elastic bottom plate of Helmholtz resonator is simplified as a single degree of freedom (SDOF) vibration system with acoustic excitation, and a one-dimensional lumped-parameter analytical model was developed to accurately characterize the structure-acoustic coupling and sound transmission loss (STL) of a Helmholtz resonator with an elastic bottom plate. The effect of dynamical parameters of elastic bottom plate on STL is analyzed by utilizing the model. A design criterion to circumvent the effect of wall elasticity of Helmholtz resonators is proposed, i.e., the structural natural frequency of the wall should be greater than three times the resonant frequency of the resonator to avoid the adverse effects of wall elasticity. This study can provide guidance for the rapid and effective design of Helmholtz resonators.</p>
</abstract>
<kwd-group kwd-group-type="author">
<kwd>Helmholtz resonator</kwd>
<kwd>bottom plate elasticity</kwd>
<kwd>sound transmission loss</kwd>
</kwd-group>
<funding-group>
<award-group id="awg1">
<funding-source>Open Foundation of the State Key Laboratory of Vehicle NVH and Safety Technology</funding-source>
<award-id>NVHSKL-202202</award-id>
</award-group>
</funding-group>
</article-meta>
</front>
<body>
<sec id="s1">
<label>1</label>
<title>Introduction</title>
<p>Helmholtz resonator is a common component for controlling noise propagation in pipes, and the study of its acoustic characteristics has always been an active topic in the field of noise control [<xref ref-type="bibr" rid="ref-1">1</xref>&#x2013;<xref ref-type="bibr" rid="ref-3">3</xref>]. Many scholars have done a lot of efforts on this topic and have achieved fruitful results. The effects of cavity shape and geometric parameters [<xref ref-type="bibr" rid="ref-4">4</xref>&#x2013;<xref ref-type="bibr" rid="ref-9">9</xref>], neck shape and position [<xref ref-type="bibr" rid="ref-10">10</xref>&#x2013;<xref ref-type="bibr" rid="ref-16">16</xref>], series-parallel connection form of the resonators [<xref ref-type="bibr" rid="ref-17">17</xref>&#x2013;<xref ref-type="bibr" rid="ref-19">19</xref>], resonator array configurations [<xref ref-type="bibr" rid="ref-20">20</xref>&#x2013;<xref ref-type="bibr" rid="ref-26">26</xref>], internal absorption materials [<xref ref-type="bibr" rid="ref-27">27</xref>,<xref ref-type="bibr" rid="ref-28">28</xref>] and other factors on the resonant frequency and the STL have been extensively investigated. From the study of the Khairuddin et al. [<xref ref-type="bibr" rid="ref-29">29</xref>] systematically summarizes the influences of resonator types, geometry, modifications, and arrangements on its attenuation capabilities, which provide helpful references for scholars studying Helmholtz resonators.</p>
<p>In most of the existing literature, the wall of Helmholtz resonant cavity is assumed to be rigid, i.e., the effect of cavity wall elasticity on the acoustic properties is ignored. However, in many practical situations, the wall elasticity cannot be ignored [<xref ref-type="bibr" rid="ref-30">30</xref>&#x2013;<xref ref-type="bibr" rid="ref-34">34</xref>]. The investigation on the effect of wall elasticity on the acoustic properties of a Helmholtz resonator can be traced back to the work of Photiadis [<xref ref-type="bibr" rid="ref-30">30</xref>,<xref ref-type="bibr" rid="ref-31">31</xref>], who found that the wall elasticity has a significant influence on the resonant frequency, radiation impedance and acoustic scattering of spherical Helmholtz resonators in water medium. Zhou et al. [<xref ref-type="bibr" rid="ref-32">32</xref>] studied the STL of a water-filled cylindrical Helmholtz resonator with elastic wall and confirmed that the coupling between elastic wall and heavy fluid has a remarkable influence on lowering the resonant frequency. Later, Nudehi et al. [<xref ref-type="bibr" rid="ref-33">33</xref>,<xref ref-type="bibr" rid="ref-34">34</xref>] demonstrated that the coupling between elastic wall and light fluid produces multiple peak frequencies of the STL instead of a single resonant frequency and also lowers the first resonant frequency. Both of them indicated that the bottom plate elasticity of the cylindrical Helmholtz resonator has a greater effect on the noise reduction than the side-wall elasticity. In this study, we find that the elasticity of the resonator wall also allows the STL of Helmholtz resonator to change from a single resonant frequency to two resonant frequencies in the frequency range of interest, which has important implication for the accurate design of Helmholtz resonator.</p>
<p>In this paper, a simplified one-dimensional lumped-parameter analytical model was developed to accurately characterize the structure-acoustic coupling and STL of a Helmholtz resonator with an elastic bottom plate. The effects of the equivalent stiffness, mass and damping of the elastic bottom plate on the peak frequency and its corresponding amplitude of the STL are analyzed, and then a design criterion to circumvent the effect of wall elasticity of Helmholtz resonators is proposed. Namely, the structural natural frequency of the wall should be greater than three times the resonant frequency of the resonator to avoid the adverse effects of wall elasticity of Helmholtz resonators. These findings are validated by one-dimensional analysis and three-dimensional finite element simulations as well, which provide guidance for the rapid and effective design of Helmholtz resonators.</p>
</sec>
<sec id="s2">
<label>2</label>
<title>Mathematical Modeling</title>
<p>To facilitate mathematical modeling, the following assumptions and simplifications are made. The cross section of the main pipe is a square with a side length of <inline-formula id="ieqn-1">
<mml:math id="mml-ieqn-1"><mml:mi>a</mml:mi></mml:math>
</inline-formula>. Both the cavity and the neck of Helmholtz resonator are cylindrical pipes. The cross-sectional radius and length of the neck are <inline-formula id="ieqn-2">
<mml:math id="mml-ieqn-2"><mml:mrow><mml:msub><mml:mi>r</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:math>
</inline-formula> and <inline-formula id="ieqn-3">
<mml:math id="mml-ieqn-3"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:math>
</inline-formula>, respectively, and those of the cavity are <inline-formula id="ieqn-4">
<mml:math id="mml-ieqn-4"><mml:mrow><mml:msub><mml:mi>r</mml:mi><mml:mn>2</mml:mn></mml:msub></mml:mrow></mml:math>
</inline-formula> and <inline-formula id="ieqn-5">
<mml:math id="mml-ieqn-5"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn>2</mml:mn></mml:msub></mml:mrow></mml:math>
</inline-formula>, respectively. The bottom plate of the Helmholtz resonator cavity is elastic and is reduced to a SDOF vibration system, while the other walls of cavity are assumed to be rigid. Thus, a simplified model based on plane wave propagation is shown in <xref ref-type="fig" rid="fig-1">Fig. 1</xref>, where <inline-formula id="ieqn-6">
<mml:math id="mml-ieqn-6"><mml:mi>M</mml:mi></mml:math>
</inline-formula>, <inline-formula id="ieqn-7">
<mml:math id="mml-ieqn-7"><mml:mi>K</mml:mi></mml:math>
</inline-formula> and <inline-formula id="ieqn-8">
<mml:math id="mml-ieqn-8"><mml:mi>C</mml:mi></mml:math>
</inline-formula> are equivalent mass, stiffness and damping of the SDOF system, respectively.</p>
<fig id="fig-1">
<label>Figure 1</label>
<caption>
<title>Schematic diagram of simplified model of Helmholtz resonator with elastic bottom plate</title></caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="SV_56968-fig-1.tif"/>
</fig>
<p>As shown in <xref ref-type="fig" rid="fig-1">Fig. 1</xref>, at the entrance of the neck (i.e., <inline-formula id="ieqn-9">
<mml:math id="mml-ieqn-9"><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math>
</inline-formula>), the complex sound pressure of the incident wave with angular frequency <inline-formula id="ieqn-10">
<mml:math id="mml-ieqn-10"><mml:mi>&#x03C9;</mml:mi></mml:math>
</inline-formula> is denoted as <inline-formula id="ieqn-11">
<mml:math id="mml-ieqn-11"><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow></mml:math>
</inline-formula> (where &#x201C;&#x002B;&#x201D; indicates propagation along the positive direction of the axis <inline-formula id="ieqn-12">
<mml:math id="mml-ieqn-12"><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:math>
</inline-formula>), then the complex sound pressure of the incident wave at any position, <inline-formula id="ieqn-13">
<mml:math id="mml-ieqn-13"><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:math>
</inline-formula> can be expressed as<disp-formula id="eqn-1"><label>(1)</label>
<mml:math id="mml-eqn-1" display="block"><mml:mrow><mml:msup><mml:mi>p</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow><mml:mo stretchy="false">(</mml:mo><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow><mml:mo stretchy="false">)</mml:mo><mml:mo>=</mml:mo><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mi>j</mml:mi><mml:mi>k</mml:mi><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:msup></mml:mrow></mml:math>
</disp-formula>where <inline-formula id="ieqn-14">
<mml:math id="mml-ieqn-14"><mml:mi>j</mml:mi><mml:mo>=</mml:mo><mml:msqrt><mml:mo>&#x2212;</mml:mo><mml:mn>1</mml:mn></mml:msqrt></mml:math>
</inline-formula> is the imaginary unit, <inline-formula id="ieqn-15">
<mml:math id="mml-ieqn-15"><mml:mi>k</mml:mi><mml:mo>=</mml:mo><mml:mi>&#x03C9;</mml:mi><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow></mml:math>
</inline-formula> is the wavenumber of the plane sound wave, and <inline-formula id="ieqn-16">
<mml:math id="mml-ieqn-16"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow></mml:math>
</inline-formula> is the speed of sound. According to the relationship between sound pressure and particle velocity, the particle velocity corresponding to the incident sound wave can be expressed as<disp-formula id="eqn-2"><label>(2)</label>
<mml:math id="mml-eqn-2" display="block"><mml:mrow><mml:msup><mml:mi>u</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow><mml:mo stretchy="false">(</mml:mo><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow><mml:mo stretchy="false">)</mml:mo><mml:mo>=</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mn>1</mml:mn><mml:mrow><mml:mrow><mml:msub><mml:mi>&#x03C1;</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mi>j</mml:mi><mml:mi>k</mml:mi><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:msup></mml:mrow></mml:mstyle></mml:math>
</disp-formula>where <inline-formula id="ieqn-17">
<mml:math id="mml-ieqn-17"><mml:mrow><mml:msub><mml:mi>&#x03C1;</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow></mml:math>
</inline-formula> is the air density.</p>
<p>Similarly, at the entrance of the neck (i.e., <inline-formula id="ieqn-18">
<mml:math id="mml-ieqn-18"><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math>
</inline-formula>), the complex sound pressure of the reflect sound waves with angular frequency <inline-formula id="ieqn-19">
<mml:math id="mml-ieqn-19"><mml:mi>&#x03C9;</mml:mi></mml:math>
</inline-formula> is denoted as <inline-formula id="ieqn-20">
<mml:math id="mml-ieqn-20"><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow></mml:math>
</inline-formula> (where &#x201C;<inline-formula id="ieqn-21">
<mml:math id="mml-ieqn-21"><mml:mo>&#x2212;</mml:mo></mml:math>
</inline-formula>&#x201D; indicates propagation along the negative direction of the axis <inline-formula id="ieqn-22">
<mml:math id="mml-ieqn-22"><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:math>
</inline-formula>), then the complex sound pressure and particle velocity of the reflect wave at any position <inline-formula id="ieqn-23">
<mml:math id="mml-ieqn-23"><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:math>
</inline-formula> can be expressed as<disp-formula id="eqn-3"><label>(3)</label>
<mml:math id="mml-eqn-3" display="block"><mml:mrow><mml:msup><mml:mi>p</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mrow><mml:mo>+</mml:mo><mml:mi mathvariant="normal">j</mml:mi></mml:mrow><mml:mi>k</mml:mi><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:msup></mml:mrow></mml:math>
</disp-formula><disp-formula id="eqn-4"><label>(4)</label>
<mml:math id="mml-eqn-4" display="block"><mml:mrow><mml:msup><mml:mi>u</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mn>1</mml:mn><mml:mrow><mml:mrow><mml:msub><mml:mi>&#x03C1;</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mrow><mml:mo>+</mml:mo><mml:mi mathvariant="normal">j</mml:mi></mml:mrow><mml:mi>k</mml:mi><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:msup></mml:mrow></mml:mstyle></mml:math>
</disp-formula></p>
<p>Then, the particle velocity <inline-formula id="ieqn-24">
<mml:math id="mml-ieqn-24"><mml:mrow><mml:msub><mml:mi>u</mml:mi><mml:mi>p</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:mrow><mml:mo>)</mml:mo></mml:mrow></mml:math>
</inline-formula> at an arbitrary position <inline-formula id="ieqn-25">
<mml:math id="mml-ieqn-25"><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:math>
</inline-formula> is<disp-formula id="eqn-5"><label>(5)</label>
<mml:math id="mml-eqn-5" display="block"><mml:mrow><mml:msub><mml:mi>u</mml:mi><mml:mi>p</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:mrow><mml:msup><mml:mi>u</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mrow><mml:msup><mml:mi>u</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mn>1</mml:mn><mml:mrow><mml:mrow><mml:msub><mml:mi>&#x03C1;</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mi>j</mml:mi><mml:mi>k</mml:mi><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:msup></mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mrow><mml:mo>+</mml:mo><mml:mi mathvariant="normal">j</mml:mi></mml:mrow><mml:mi>k</mml:mi><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:msup></mml:mrow></mml:mrow><mml:mo>)</mml:mo></mml:mrow></mml:mstyle></mml:math>
</disp-formula></p>
<p>Since the sound pressure is continuous and the mass flux of particles is conserved, there is an equality relationship at <inline-formula id="ieqn-26">
<mml:math id="mml-ieqn-26"><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow><mml:mo>=</mml:mo><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:math>
</inline-formula> (i.e., <inline-formula id="ieqn-27">
<mml:math id="mml-ieqn-27"><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>2</mml:mn></mml:msub></mml:mrow><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math>
</inline-formula>) as follows:<disp-formula id="eqn-6"><label>(6)</label>
<mml:math id="mml-eqn-6" display="block"><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mo stretchy="false">(</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mi>j</mml:mi><mml:mi>k</mml:mi><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow><mml:mo stretchy="false">)</mml:mo></mml:mrow></mml:msup></mml:mrow><mml:mo>+</mml:mo><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mo>+</mml:mo><mml:mi>j</mml:mi><mml:mi>k</mml:mi><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:msup></mml:mrow><mml:mo>=</mml:mo><mml:mrow><mml:msup><mml:mi>B</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow><mml:mo>+</mml:mo><mml:mrow><mml:msup><mml:mi>B</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow></mml:math>
</disp-formula><disp-formula id="eqn-7"><label>(7)</label>
<mml:math id="mml-eqn-7" display="block"><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mi>j</mml:mi><mml:mi>k</mml:mi><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:msup></mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mrow><mml:mo>+</mml:mo><mml:mi mathvariant="normal">j</mml:mi></mml:mrow><mml:mi>k</mml:mi><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:msup></mml:mrow></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mi>C</mml:mi></mml:msub></mml:mrow><mml:mo>=</mml:mo><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mrow><mml:msup><mml:mi>B</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mrow><mml:msup><mml:mi>B</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mi>V</mml:mi></mml:msub></mml:mrow></mml:math>
</disp-formula>where <inline-formula id="ieqn-28">
<mml:math id="mml-ieqn-28"><mml:mrow><mml:msup><mml:mi>B</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow></mml:math>
</inline-formula> and <inline-formula id="ieqn-29">
<mml:math id="mml-ieqn-29"><mml:mrow><mml:msup><mml:mi>B</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow></mml:math>
</inline-formula> are the complex sound pressures of the forward and reverse sound waves propagating along the axis <inline-formula id="ieqn-30">
<mml:math id="mml-ieqn-30"><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>2</mml:mn></mml:msub></mml:mrow></mml:math>
</inline-formula> in the cavity, <inline-formula id="ieqn-31">
<mml:math id="mml-ieqn-31"><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mi>C</mml:mi></mml:msub></mml:mrow></mml:math>
</inline-formula> is the cross-sectional area of the neck, and <inline-formula id="ieqn-32">
<mml:math id="mml-ieqn-32"><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mi>V</mml:mi></mml:msub></mml:mrow></mml:math>
</inline-formula> is the cross-sectional area of the cavity, respectively.</p>
<p>Similarly, the following relationship exists at the elastic bottom plate (i.e., <inline-formula id="ieqn-33">
<mml:math id="mml-ieqn-33"><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>2</mml:mn></mml:msub></mml:mrow><mml:mo>=</mml:mo><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn>2</mml:mn></mml:msub></mml:mrow></mml:math>
</inline-formula>) of the cavity<disp-formula id="eqn-8"><label>(8)</label>
<mml:math id="mml-eqn-8" display="block"><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mn>1</mml:mn><mml:mrow><mml:mrow><mml:msub><mml:mi>&#x03C1;</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:mfrac></mml:mrow><mml:mo stretchy="false">(</mml:mo><mml:mrow><mml:msup><mml:mi>B</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mo stretchy="false">(</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mi>j</mml:mi><mml:mi>k</mml:mi><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn>2</mml:mn></mml:msub></mml:mrow><mml:mo stretchy="false">)</mml:mo></mml:mrow></mml:msup></mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mrow><mml:msup><mml:mi>B</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mo>+</mml:mo><mml:mi>j</mml:mi><mml:mi>k</mml:mi><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn>2</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:msup></mml:mrow><mml:mo stretchy="false">)</mml:mo><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mi>V</mml:mi></mml:msub></mml:mrow><mml:mo>=</mml:mo><mml:mrow><mml:msub><mml:mi>v</mml:mi><mml:mi>P</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mi>V</mml:mi></mml:msub></mml:mrow></mml:mstyle></mml:math>
</disp-formula>where <inline-formula id="ieqn-34">
<mml:math id="mml-ieqn-34"><mml:mrow><mml:msub><mml:mi>v</mml:mi><mml:mi>P</mml:mi></mml:msub></mml:mrow></mml:math>
</inline-formula> is the normal vibration velocity of the elastic bottom plate, which satisfies<disp-formula id="eqn-9"><label>(9)</label>
<mml:math id="mml-eqn-9" display="block"><mml:mrow><mml:msub><mml:mi>v</mml:mi><mml:mi>P</mml:mi></mml:msub></mml:mrow><mml:mo>=</mml:mo><mml:mrow><mml:msub><mml:mi>H</mml:mi><mml:mi>V</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>F</mml:mi><mml:mi>P</mml:mi></mml:msub></mml:mrow></mml:math>
</disp-formula></p>
<p>Here, <inline-formula id="ieqn-35">
<mml:math id="mml-ieqn-35"><mml:mrow><mml:msub><mml:mi>F</mml:mi><mml:mi>P</mml:mi></mml:msub></mml:mrow></mml:math>
</inline-formula> is the force of the sound pressure inside the cavity on the elastic bottom plate, <inline-formula id="ieqn-36">
<mml:math id="mml-ieqn-36"><mml:mrow><mml:msub><mml:mi>H</mml:mi><mml:mi>V</mml:mi></mml:msub></mml:mrow><mml:mtext>&#x00A0;</mml:mtext></mml:math>
</inline-formula> is the vibration velocity transfer function of the SDOF system. <inline-formula id="ieqn-37">
<mml:math id="mml-ieqn-37"><mml:mrow><mml:msub><mml:mi>F</mml:mi><mml:mi>P</mml:mi></mml:msub></mml:mrow></mml:math>
</inline-formula> and <inline-formula id="ieqn-38">
<mml:math id="mml-ieqn-38"><mml:mrow><mml:msub><mml:mi>H</mml:mi><mml:mi>V</mml:mi></mml:msub></mml:mrow></mml:math>
</inline-formula> [<xref ref-type="bibr" rid="ref-35">35</xref>] can be expressed as<disp-formula id="eqn-10"><label>(10)</label>
<mml:math id="mml-eqn-10" display="block"><mml:mrow><mml:msub><mml:mi>F</mml:mi><mml:mi>P</mml:mi></mml:msub></mml:mrow><mml:mo>=</mml:mo><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mrow><mml:msup><mml:mi>B</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mi>j</mml:mi><mml:mi>k</mml:mi><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn>2</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:msup></mml:mrow><mml:mo>+</mml:mo><mml:mrow><mml:msup><mml:mi>B</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mrow><mml:mo>+</mml:mo><mml:mi mathvariant="normal">j</mml:mi></mml:mrow><mml:mi>k</mml:mi><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn>2</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:msup></mml:mrow></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mi>V</mml:mi></mml:msub></mml:mrow></mml:math>
</disp-formula><disp-formula id="eqn-11"><label>(11)</label>
<mml:math id="mml-eqn-11" display="block"><mml:mrow><mml:msub><mml:mi>H</mml:mi><mml:mi>V</mml:mi></mml:msub></mml:mrow><mml:mo>=</mml:mo><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mi>j</mml:mi><mml:mi>&#x03C9;</mml:mi></mml:mrow><mml:mrow><mml:mi>K</mml:mi><mml:mo>&#x2212;</mml:mo><mml:mi>M</mml:mi><mml:mrow><mml:msup><mml:mi>&#x03C9;</mml:mi><mml:mn>2</mml:mn></mml:msup></mml:mrow><mml:mo>+</mml:mo><mml:mi>j</mml:mi><mml:mi>C</mml:mi><mml:mi>&#x03C9;</mml:mi></mml:mrow></mml:mfrac></mml:mrow></mml:mstyle></mml:math>
</disp-formula></p>
<p>At the interface between the main pipe and the resonator, the following equation also exists<disp-formula id="eqn-12"><label>(12)</label>
<mml:math id="mml-eqn-12" display="block"><mml:mrow><mml:msup><mml:mi>C</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow><mml:mo>+</mml:mo><mml:mrow><mml:msup><mml:mi>C</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow><mml:mo>=</mml:mo><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow><mml:mo>+</mml:mo><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow><mml:mo>=</mml:mo><mml:mrow><mml:msup><mml:mi>D</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow></mml:math>
</disp-formula><disp-formula id="eqn-13"><label>(13)</label>
<mml:math id="mml-eqn-13" display="block"><mml:mtext>&#x00A0;</mml:mtext><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mrow><mml:msup><mml:mi>C</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mrow><mml:msup><mml:mi>C</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mi>P</mml:mi></mml:msub></mml:mrow><mml:mo>=</mml:mo><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mi>C</mml:mi></mml:msub></mml:mrow><mml:mo>+</mml:mo><mml:mrow><mml:msup><mml:mi>D</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mi>P</mml:mi></mml:msub></mml:mrow></mml:math>
</disp-formula>where <inline-formula id="ieqn-39">
<mml:math id="mml-ieqn-39"><mml:mrow><mml:msup><mml:mi>C</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow></mml:math>
</inline-formula> and <inline-formula id="ieqn-40">
<mml:math id="mml-ieqn-40"><mml:mrow><mml:msup><mml:mi>C</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow></mml:math>
</inline-formula> are the complex sound pressure of the incident wave and reflected wave in main pipe upstream of Helmholtz resonator, <inline-formula id="ieqn-41">
<mml:math id="mml-ieqn-41"><mml:mrow><mml:msup><mml:mi>D</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow></mml:math>
</inline-formula> is the complex sound pressure of the transmitted wave in main pipe downstream of Helmholtz resonator, and <inline-formula id="ieqn-42">
<mml:math id="mml-ieqn-42"><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mi>P</mml:mi></mml:msub></mml:mrow></mml:math>
</inline-formula> is the cross-sectional area of the main pipe, respectively.</p>
<p>According to the <xref ref-type="disp-formula" rid="eqn-5">Eq. (5)</xref>, at the entrance of the neck (i.e., <inline-formula id="ieqn-43">
<mml:math id="mml-ieqn-43"><mml:mrow><mml:msub><mml:mi>x</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math>
</inline-formula>), <inline-formula id="ieqn-44">
<mml:math id="mml-ieqn-44"><mml:mrow><mml:msub><mml:mi>u</mml:mi><mml:mi>p</mml:mi></mml:msub></mml:mrow><mml:mo>=</mml:mo><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mrow><mml:msub><mml:mi>&#x03C1;</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow></mml:math>
</inline-formula>. Let <inline-formula id="ieqn-45">
<mml:math id="mml-ieqn-45"><mml:mrow><mml:msub><mml:mi>&#x03C1;</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>u</mml:mi><mml:mi>p</mml:mi></mml:msub></mml:mrow><mml:mo>=</mml:mo><mml:mn>1</mml:mn></mml:math>
</inline-formula> and combine <xref ref-type="disp-formula" rid="eqn-6">Eqs. (6)</xref>&#x2013;<xref ref-type="disp-formula" rid="eqn-13">(13)</xref>, we obtain<disp-formula id="eqn-14"><label>(14)</label>
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columnspacing="1em"><mml:mtr><mml:mtd><mml:mrow><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mrow><mml:mrow><mml:msup><mml:mi>A</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mrow><mml:mrow><mml:msup><mml:mi>B</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mrow><mml:mrow><mml:msup><mml:mi>B</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mrow><mml:mrow><mml:msup><mml:mi>C</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mrow><mml:mrow><mml:msub><mml:mi>C</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msub></mml:mrow></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mrow><mml:mrow><mml:msup><mml:mi>D</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow></mml:mrow></mml:mtd></mml:mtr></mml:mtable></mml:mrow><mml:mo>]</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:mrow><mml:mo>[</mml:mo><mml:mrow><mml:mtable rowspacing="4pt" columnspacing="1em"><mml:mtr><mml:mtd><mml:mn>0</mml:mn></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mn>0</mml:mn></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mn>0</mml:mn></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mn>0</mml:mn></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mn>0</mml:mn></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mn>0</mml:mn></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mn>1</mml:mn></mml:mtd></mml:mtr></mml:mtable></mml:mrow><mml:mo>]</mml:mo></mml:mrow></mml:math>
</disp-formula></p>
<p>Further, we can obtain STL as follows:<disp-formula id="eqn-15"><label>(15)</label>
<mml:math id="mml-eqn-15" display="block"><mml:mrow><mml:mi mathvariant="normal">S</mml:mi><mml:mi mathvariant="normal">T</mml:mi><mml:mi mathvariant="normal">L</mml:mi></mml:mrow><mml:mo>=</mml:mo><mml:mn>20</mml:mn><mml:mtext>&#x00A0;</mml:mtext><mml:mrow><mml:mi>l</mml:mi><mml:mi>o</mml:mi><mml:msub><mml:mi>g</mml:mi><mml:mrow><mml:mn>10</mml:mn></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mo>|</mml:mo><mml:mrow><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mrow><mml:mfrac><mml:mrow><mml:mrow><mml:msup><mml:mi>C</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow></mml:mrow><mml:mrow><mml:mrow><mml:msup><mml:mi>D</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow></mml:mrow></mml:mfrac></mml:mrow></mml:mstyle></mml:mrow><mml:mo>|</mml:mo></mml:mrow></mml:math>
</disp-formula></p>
<p>It should be mentioned that in this paper, we corrected the neck length from <inline-formula id="ieqn-46">
<mml:math id="mml-ieqn-46"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow></mml:math>
</inline-formula> to <inline-formula id="ieqn-47">
<mml:math id="mml-ieqn-47"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow><mml:mo>+</mml:mo><mml:mn>0.85</mml:mn><mml:mrow><mml:msub><mml:mi>r</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mn>1</mml:mn><mml:mo>&#x2212;</mml:mo><mml:mn>1.25</mml:mn><mml:mrow><mml:msub><mml:mi>r</mml:mi><mml:mn>1</mml:mn></mml:msub></mml:mrow><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mrow><mml:msub><mml:mi>r</mml:mi><mml:mn>2</mml:mn></mml:msub></mml:mrow></mml:mrow><mml:mo>)</mml:mo></mml:mrow></mml:math>
</inline-formula> by referring to the study of the Selamet et al. [<xref ref-type="bibr" rid="ref-5">5</xref>].</p>
</sec>
<sec id="s3">
<label>3</label>
<title>Parameters Setting and Model Validation</title>
<p><xref ref-type="table" rid="table-1">Table 1</xref> lists the structural dimensions and medium properties of the model shown in <xref ref-type="fig" rid="fig-1">Fig. 1</xref>, which are consistent with the data in the study of the Selamet et al. [<xref ref-type="bibr" rid="ref-10">10</xref>]. To better investigate the coupling between the elastic plate vibration and the sound pressure inside the cavity of Helmholtz resonator, the structural natural frequency <italic>f</italic> of the elastic bottom plate remains the same as the resonant frequency <italic>f</italic><sub>0</sub> of the Helmholtz resonator. The material of the elastic bottom plate is Polyvinyl Chloride (PVC) whose parameters are also listed in <xref ref-type="table" rid="table-1">Table 1</xref>. In the one-dimensional analytical calculation, when considering the resonator bottom plate elasticity, the equivalent mass <italic>M</italic> and stiffness <italic>K</italic> parameters of the SDOF vibration system on the elastic bottom plate are obtained as 0.06036 kg and 26,623.8 N/m, respectively, according to the kinetic energy equivalence principle. The equivalent damping <italic>C</italic> of the bottom plate is set to 1.6036 Ns/m (i.e., the damping ratio is 0.02). When the bottom plate of the resonator degrades to rigid, <inline-formula id="ieqn-48">
<mml:math id="mml-ieqn-48"><mml:mrow><mml:msup><mml:mi>B</mml:mi><mml:mo>+</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mi>j</mml:mi><mml:mi>k</mml:mi><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn>2</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:msup></mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mrow><mml:msup><mml:mi>B</mml:mi><mml:mo>&#x2212;</mml:mo></mml:msup></mml:mrow><mml:mrow><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mi>j</mml:mi><mml:mi>k</mml:mi><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn>2</mml:mn></mml:msub></mml:mrow></mml:mrow></mml:msup></mml:mrow></mml:math>
</inline-formula> and <inline-formula id="ieqn-49">
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</inline-formula> are set to 0.</p>
<table-wrap id="table-1"><label>Table 1</label>
<caption>
<title>Structural dimensions and medium properties of model</title></caption>
<table><colgroup>
<col/>
<col/>
<col/>
<col/>
</colgroup>
<thead>
<tr>
<th colspan="2">Parameter</th>
<th>Unit</th>
<th>Value</th>
</tr>
</thead>
<tbody>
<tr>
<td>Radius of neck</td>
<td><italic>r</italic><sub>1</sub></td>
<td>m</td>
<td>0.02</td>
</tr>
<tr>
<td>Radius of cavity</td>
<td><italic>r</italic><sub>2</sub></td>
<td>m</td>
<td>0.0762</td>
</tr>
<tr>
<td>Length of neck</td>
<td><italic>l</italic><sub>1</sub></td>
<td>m</td>
<td>0.085</td>
</tr>
<tr>
<td>Length of cavity</td>
<td><italic>l</italic><sub>2</sub></td>
<td>m</td>
<td>0.2032</td>
</tr>
<tr>
<td>Side length of main pipe</td>
<td><italic>a</italic></td>
<td>m</td>
<td>0.043</td>
</tr>
<tr>
<td>Density of air</td>
<td><italic>&#x03C1;</italic><sub>0</sub></td>
<td>kg/m<sup>3</sup></td>
<td>1.21</td>
</tr>
<tr>
<td>Speed of sound</td>
<td><italic>c</italic><sub>0</sub></td>
<td>m/s</td>
<td>343</td>
</tr>
<tr>
<td>Height of elastic bottom plate</td>
<td><italic>h</italic></td>
<td>m</td>
<td>0.001</td>
</tr>
<tr>
<td>Density of elastic bottom plate</td>
<td><italic>&#x03C1;</italic><sub>p</sub></td>
<td>kg/m<sup>3</sup></td>
<td>1760</td>
</tr>
<tr>
<td>Young&#x2019;s modulus of elastic bottom plate</td>
<td><italic>E</italic></td>
<td>MPa</td>
<td>2900</td>
</tr>
<tr>
<td>Poisson&#x2019;s ratio of elastic bottom plate</td>
<td><italic>&#x03BC;</italic></td>
<td>&#x2013;</td>
<td>0.36</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>The three-dimensional finite element model (FEM) of Helmholtz resonator with elastic bottom plate is established corresponding to the parameters in <xref ref-type="table" rid="table-1">Table 1</xref>, as shown in <xref ref-type="fig" rid="fig-2">Fig. 2</xref>. All the walls are set to be rigid when the elasticity of the bottom plate is not considered, and the rest of the walls of the resonator other than the bottom plate are set to be rigid when considered. The damping ratio of elastic bottom plate is also set to 0.02. The air domain is discretized using tetrahedral elements, while the structural domain is discretized using shell elements and triangular mesh. <xref ref-type="table" rid="table-2">Table 2</xref> shows the mesh irrelevance test and the resonant frequencies of the Helmholtz resonator for different grid size. When the maximum grid size in the computational domain is less than 0.03 m, the change of the resonant frequencies is less than 1%, which meets the requirements for mesh irrelevance. In order to balance calculation accuracy and efficiency, the maximum mesh size is set to 0.02 m.</p>
<fig id="fig-2">
<label>Figure 2</label>
<caption>
<title>Three-dimensional FEM of Helmholtz resonator with elastic bottom plate</title></caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="SV_56968-fig-2.tif"/>
</fig><table-wrap id="table-2"><label>Table 2</label>
<caption>
<title>Mesh irrelevance test</title></caption>
<table><colgroup>
<col/>
<col/>
<col/>
<col/>
</colgroup>
<thead>
<tr>
<th>Maximum grid size/m</th>
<th>Resonant frequency with rigid bottom plates/Hz</th>
<th>1th resonant frequency with elastic bottom plates/Hz</th>
<th>2th resonant frequency with elastic bottom plates/Hz</th>
</tr>
</thead>
<tbody>
<tr>
<td>0.05</td>
<td>97.8</td>
<td>69.3</td>
<td>144.0</td>
</tr>
<tr>
<td>0.04</td>
<td>97.7</td>
<td>70.1</td>
<td>144.3</td>
</tr>
<tr>
<td>0.03</td>
<td>97.6</td>
<td>70.7</td>
<td>144.5</td>
</tr>
<tr>
<td>0.02</td>
<td>97.5</td>
<td>71.1</td>
<td>144.6</td>
</tr>
<tr>
<td>0.01</td>
<td>97.5</td>
<td>71.3</td>
<td>144.6</td>
</tr>
</tbody>
</table>
</table-wrap>
<p><xref ref-type="fig" rid="fig-3">Fig. 3a</xref> compares the STL curves of the resonator with rigid bottom plate obtained using <xref ref-type="disp-formula" rid="eqn-15">Eq. (15)</xref>, from the study of the Selamet et al. [<xref ref-type="bibr" rid="ref-10">10</xref>], and three-dimensional FEM. It shows that the STL curves obtained by the three methods are almost consistent, and the difference of the resonant frequencies between three methods is less than 1.5 Hz, indicating that the simplified theoretical model with rigid bottom plate in this paper is correct. <xref ref-type="fig" rid="fig-3">Fig. 3b</xref> compares the STL curves of the resonator with elastic bottom plate obtained using <xref ref-type="disp-formula" rid="eqn-15">Eq. (15)</xref> and three-dimensional FEM. It shows that the results obtained by the two methods are almost consistent, indicating that the established one-dimensional lumped-parameter analytical model considering structure-acoustic coupling in this paper is also correct.</p>
<fig id="fig-3">
<label>Figure 3</label>
<caption>
<title>Comparison of sound transmission loss of resonators with rigid and elastic bottom plates. (a) Rigid bottom plate [<xref ref-type="bibr" rid="ref-10">10</xref>] (b) Elastic bottom plate</title></caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="SV_56968-fig-3.tif"/>
</fig>
</sec>
<sec id="s4">
<label>4</label>
<title>Effect Analysis of Parameters</title>
<p>It can be seen from comparing the STL curves in <xref ref-type="fig" rid="fig-3">Fig. 3a</xref>,<xref ref-type="fig" rid="fig-3">b</xref> that the elasticity of the bottom plate makes the STL peak of resonator split into two peaks, due to the strong coupling between the structural vibration of the elastic bottom plate and the acoustic pressure inside the resonator cavity. The influence of the dynamic parameters (stiffness, mass, damping) of the elastic bottom plate on the STL of the Helmholtz resonator is analyzed using one-dimensional lumped-parameter analytical model and discussed in the following sections.</p>
<sec id="s4_1">
<label>4.1</label>
<title>Change of Equivalent Stiffness</title>
<p>When only changing the stiffness of the SDOF vibration system as shown in <xref ref-type="table" rid="table-3">Table 3</xref> to increase the natural frequency of the bottom plate, the vibration velocity response of the elastic bottom plate and the STL of the resonator are calculated and shown in <xref ref-type="fig" rid="fig-4">Fig. 4</xref>. The results in <xref ref-type="fig" rid="fig-4">Fig. 4a</xref> show that the peak frequency of the vibration velocity response increases with increasing the stiffness, while the amplitude gradually decreases. It can be seen from <xref ref-type="table" rid="table-3">Table 3</xref> that the difference of the resonant frequencies of the elastic bottom plate with and without considering the coupling gradually decreases with increasing the stiffness, indicating that the coupling between the elastic bottom plate vibration and the acoustic pressure inside the resonator cavity gradually weakens. As shown in <xref ref-type="fig" rid="fig-4">Fig. 4b</xref>, the first peak frequency and amplitude of the STL increase with increasing the stiffness; the second peak frequency increases with increasing the stiffness, while the peak amplitude decreases; when the natural frequency of the bottom plate reaches three times the acoustic resonant frequency of the resonator, the first peak frequency and amplitude of the STL are close to those of the rigid bottom plate case, and the second peak almost disappears, which means that the vibration of the elastic bottom plate and the acoustic pressure inside the resonator cavity are decoupled.</p>
<table-wrap id="table-3"><label>Table 3</label>
<caption>
<title>Resonant frequency <italic>vs</italic>. equivalent stiffness of SDOF vibration system before and after considering coupling</title></caption>
<table><colgroup>
<col/>
<col/>
<col/>
<col/>
<col/>
<col/>
</colgroup>
<thead>
<tr>
<th>Equivalent mass</th>
<th>Equivalent stiffness</th>
<th>Equivalent damping</th>
<th>Resonant frequency without coupling/Hz</th>
<th>Resonant frequency with coupling/Hz</th>
<th>&#x2206;/Hz</th>
</tr>
</thead>
<tbody>
<tr>
<td><italic>M</italic></td>
<td><italic>K</italic></td>
<td><italic>C</italic></td>
<td>105.7</td>
<td>126.1</td>
<td>20.4</td>
</tr>
<tr>
<td><italic>M</italic></td>
<td>9<italic>K</italic>/4</td>
<td><italic>C</italic></td>
<td>158.5</td>
<td>171.6</td>
<td>13.1</td>
</tr>
<tr>
<td><italic>M</italic></td>
<td>4<italic>K</italic></td>
<td><italic>C</italic></td>
<td>211.4</td>
<td>219.8</td>
<td>8.4</td>
</tr>
<tr>
<td><italic>M</italic></td>
<td>9<italic>K</italic></td>
<td><italic>C</italic></td>
<td>317.0</td>
<td>320.3</td>
<td>3.2</td>
</tr>
</tbody>
</table>
</table-wrap><fig id="fig-4">
<label>Figure 4</label>
<caption>
<title>Vibration velocity response of elastic bottom plate and STL of resonator for different equivalent stiffness (Reference value of vibration velocity is 1 &#x00D7; 10<sup>&#x2212;9</sup> m/s, the same below and omitted). (a) Vibration velocity response, (b) Sound transmission loss</title></caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="SV_56968-fig-4.tif"/>
</fig>
</sec>
<sec id="s4_2">
<label>4.2</label>
<title>Change of Equivalent Mass</title>
<p>When only changing the mass of the SDOF vibration system as shown in <xref ref-type="table" rid="table-4">Table 4</xref> to increase the natural frequency of the bottom plate, the vibration velocity response of the elastic bottom plate and the STL of the resonator are calculated and shown in <xref ref-type="fig" rid="fig-5">Fig. 5</xref>. The results in <xref ref-type="fig" rid="fig-5">Fig. 5a</xref> show that the peak frequency of the vibration velocity response increases with decreasing the mass, while the amplitude gradually increases. It can be seen from <xref ref-type="table" rid="table-4">Table 4</xref> that the difference of the resonant frequencies of the elastic bottom plate with and without considering the coupling gradually decreases with increasing the mass, indicating that the coupling between the elastic bottom plate vibration and the acoustic pressure inside the resonator cavity gradually weakens. As shown in <xref ref-type="fig" rid="fig-5">Fig. 5b</xref>, the first peak frequency and amplitude of the STL increase with decreasing the mass; the second peak frequency increases with decreasing the mass, while the peak amplitude decreases; when the natural frequency of the bottom plate reaches two times the acoustic resonant frequency of the resonator, the first peak frequency of the STL basically tends to constant value, and is less than the frequency corresponding to rigid bottom plate; when the natural frequency of the bottom plate reaches three times the acoustic resonant frequency of the resonator, the second peak of STL still exist, which indicated that the vibration of the elastic bottom plate and the acoustic pressure inside the resonator cavity are still coupled. On the other word, the decoupling between the vibration of the elastic bottom plate and the acoustic pressure inside the resonator cavity is more difficult to achieve by changing mass alone than by changing stiffness alone.</p>
<table-wrap id="table-4"><label>Table 4</label>
<caption>
<title>Resonant frequency <italic>vs</italic>. equivalent mass of SDOF vibration system before and after considering the coupling</title></caption>
<table><colgroup>
<col/>
<col/>
<col/>
<col/>
<col/>
<col/>
</colgroup>
<thead>
<tr>
<th>Equivalent mass</th>
<th>Equivalent stiffness</th>
<th>Equivalent damping</th>
<th>Resonant frequency without coupling/Hz</th>
<th>Resonant frequency with coupling/Hz</th>
<th>&#x2206;/Hz</th>
</tr>
</thead>
<tbody>
<tr>
<td><italic>M</italic></td>
<td><italic>K</italic></td>
<td><italic>C</italic></td>
<td>105.7</td>
<td>126.1</td>
<td>20.4</td>
</tr>
<tr>
<td>4<italic>M</italic>/9</td>
<td><italic>K</italic></td>
<td><italic>C</italic></td>
<td>158.5</td>
<td>186.3</td>
<td>27.8</td>
</tr>
<tr>
<td><italic>M</italic>/4</td>
<td><italic>K</italic></td>
<td><italic>C</italic></td>
<td>211.4</td>
<td>243</td>
<td>31.6</td>
</tr>
<tr>
<td><italic>M</italic>/9</td>
<td><italic>K</italic></td>
<td><italic>C</italic></td>
<td>317.1</td>
<td>341.6</td>
<td>24.5</td>
</tr>
</tbody>
</table>
</table-wrap><fig id="fig-5">
<label>Figure 5</label>
<caption>
<title>Vibration velocity response of elastic bottom plate and STL of resonator for different equivalent masses. (a) Vibration velocity response, (b) Sound transmission loss</title></caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="SV_56968-fig-5.tif"/>
</fig>
</sec>
<sec id="s4_3">
<label>4.3</label>
<title>Change of Thickness</title>
<p>For the homogeneous plate, the plate mass is proportional to the thickness and bending stiffness is proportional to the third power of the thickness. As shown in <xref ref-type="table" rid="table-5">Table 5</xref>, the natural frequency of the resonator elastic bottom plate is adjusted by changing the plate thickness, i.e., simultaneously change equivalent mass and stiffness of the SDOF system. The vibration velocity response of the elastic bottom plate and the STL of the resonator for different thickness of elastic bottom plate are calculated and shown in <xref ref-type="fig" rid="fig-6">Fig. 6</xref>. The results in <xref ref-type="fig" rid="fig-6">Fig. 6a</xref> show that the peak frequency of the vibration velocity response increases with increasing the thickness, while the amplitude gradually decreases. It can be seen from <xref ref-type="table" rid="table-5">Table 5</xref> that the difference of the natural frequencies of the elastic bottom plate with and without considering the coupling gradually decreases with increasing the thickness, indicating that the coupling between the elastic bottom plate vibration and the acoustic pressure inside the resonator cavity gradually weakens. As shown in <xref ref-type="fig" rid="fig-6">Fig. 6b</xref>, the first peak frequency of the STL increase with increasing the thickness; the second peak frequency increases with increasing the thickness, while the peak amplitude decreases; when the natural frequency of the bottom plate reaches three times the acoustic resonant frequency of the resonator, the first peak frequency and amplitude of the STL are close to those of the rigid bottom plate case, and the second peak almost disappears, which means that the vibration of the elastic bottom plate and the acoustic pressure inside the resonator cavity are decoupled.</p>
<table-wrap id="table-5"><label>Table 5</label>
<caption>
<title>Resonant frequency <italic>vs</italic>. equivalent mass and stiffness of SDOF vibration system before and after considering coupling</title></caption>
<table><colgroup>
<col/>
<col/>
<col/>
<col/>
<col/>
<col/>
</colgroup>
<thead>
<tr>
<th>Equivalent mass</th>
<th>Equivalent stiffness</th>
<th>Equivalent damping</th>
<th>Resonant frequency without coupling/Hz</th>
<th>Resonant frequency with coupling/Hz</th>
<th>&#x2206;/Hz</th>
</tr>
</thead>
<tbody>
<tr>
<td><italic>M</italic></td>
<td><italic>K</italic></td>
<td><italic>C</italic></td>
<td>105.7</td>
<td>126.1</td>
<td>20.4</td>
</tr>
<tr>
<td>3<italic>M</italic>/2</td>
<td>27<italic>K</italic>/8</td>
<td><italic>C</italic></td>
<td>158.5</td>
<td>166.7</td>
<td>8.2</td>
</tr>
<tr>
<td>2<italic>M</italic></td>
<td>8<italic>K</italic></td>
<td><italic>C</italic></td>
<td>211.4</td>
<td>215.7</td>
<td>4.3</td>
</tr>
<tr>
<td>3<italic>M</italic></td>
<td>27<italic>K</italic></td>
<td><italic>C</italic></td>
<td>317.1</td>
<td>318.2</td>
<td>1.1</td>
</tr>
</tbody>
</table>
</table-wrap><fig id="fig-6">
<label>Figure 6</label>
<caption>
<title>Vibration velocity response of elastic bottom plate and STL of resonator for different combinations of equivalent mass and stiffness (corresponding to different thickness of rigid bottom plate). (a) Vibration velocity response, (b) Sound transmission loss</title></caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="SV_56968-fig-6.tif"/>
</fig>
<p>The STLs obtained by finite element method for different bottom plate thicknesses (by adjusting the real constants of the shell element thickness of finite element model) are shown in <xref ref-type="fig" rid="fig-7">Fig. 7a</xref>,<xref ref-type="fig" rid="fig-7">b</xref> shows the frequencies corresponding to the first peak of the STLs of resonators with different ratio between the structural natural frequency <inline-formula id="ieqn-50">
<mml:math id="mml-ieqn-50"><mml:mi>f</mml:mi></mml:math>
</inline-formula> of the bottom plate and the acoustic resonant frequency <inline-formula id="ieqn-51">
<mml:math id="mml-ieqn-51"><mml:mrow><mml:msub><mml:mi>f</mml:mi><mml:mn>0</mml:mn></mml:msub></mml:mrow></mml:math>
</inline-formula> of the Helmholtz resonator, obtained not only by the one-dimensional analytical method but also the three-dimensional finite element method. As shown in <xref ref-type="fig" rid="fig-7">Fig. 7a</xref>, when the natural frequency of the elastic bottom plate reaches three times the acoustic resonant frequency of the resonator, the peak frequency of the STL between the elastic bottom plate and the fully rigid wall differs by only 1.08 Hz, with a small relative error of less than 2%, which basically realizes the decoupling of the structural vibration of the elastic bottom plate and the sound pressure inside the cavity. As shown in <xref ref-type="fig" rid="fig-7">Fig. 7b</xref>, the higher the structural natural frequency of the elastic bottom plate, the closer the first peak frequency of the STL obtained by either the analytical method or the finite element method is to the peak frequency in the case of the rigid bottom plate. Combining <xref ref-type="fig" rid="fig-7">Fig. 7a</xref>,<xref ref-type="fig" rid="fig-7">b</xref>, it can be concluded that when the natural frequency of the elastic bottom plate reaches three times the resonant frequency of the resonator, the effect of the bottom plate elasticity on the STL is almost negligible.</p>
<fig id="fig-7">
<label>Figure 7</label>
<caption>
<title>Effect of natural frequency of elastic bottom plate on sound transmission loss and its first peak frequency. (a) Sound transmission loss, (b) First peak frequency of STL</title></caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="SV_56968-fig-7.tif"/>
</fig>
</sec>
<sec id="s4_4">
<label>4.4</label>
<title>Change of Equivalent Damping</title>
<p><xref ref-type="fig" rid="fig-8">Fig. 8a</xref>,<xref ref-type="fig" rid="fig-8">b</xref> show the STL of the resonator and the vibrational velocity response of the elastic bottom surface obtained by changing only the damping of the SDOF system, respectively. At this time, the natural frequency of the elastic bottom plate remains the same as the resonant frequency of the Helmholtz resonator. As can be seen from <xref ref-type="fig" rid="fig-8">Fig. 8a</xref>, the vibration velocity response of the elastic bottom plate in the analyzed frequency band decreases significantly with increasing damping. As can be seen in <xref ref-type="fig" rid="fig-8">Fig. 8b</xref>, the peak frequency of the STL decreases slightly with increasing damping, but the amplitude at the peak frequency decreases significantly, indicating that the sound attenuation capability of the resonator decreases with increasing damping of the cavity bottom plate.</p>
<fig id="fig-8">
<label>Figure 8</label>
<caption>
<title>Vibration velocity response of elastic bottom plate and STL of resonator for different damping. (a) Vibration velocity response, (b) Sound transmission loss</title></caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="SV_56968-fig-8.tif"/>
</fig>
</sec>
</sec>
<sec id="s5">
<label>5</label>
<title>Conclusion</title>
<p>In this paper, a one-dimensional lumped-parameter analytical model is derived to analyze the STL of a Helmholtz resonator with an elastic bottom plate, which takes into account the structure-acoustic coupling between the structural vibrations of the resonator wall and the sound pressure inside the resonator cavity. The effect of the dynamic parameters of the elastic bottom plate on the STL is then investigated. The following conclusions were obtained. (1) If the structural natural frequency of the elastic wall is close to the resonant frequency of the resonator (i.e., there exists strong coupling), the wall elasticity has a significant effect on the STL of a Helmholtz resonator, and the STL peak of the resonator will be split into two peaks. (2) The vibration of the elastic wall and the acoustic pressure in the Helmholtz resonator cavity can be effectively decoupled by increasing the stiffness and thickness of elastic wall. (3) When the natural frequency of the elastic wall reaches three times the acoustic resonant frequency of the resonator, the effect of the wall elasticity on the STL can be ignored. These conclusions provide guidance for the rapid and effective design of Helmholtz resonators.</p>
</sec>
</body>
<back>
<ack>
<p>The authors would like to acknowledge the support from the Open Foundation of the State Key Laboratory of Vehicle NVH and Safety Technology and the facilities provided by Chongqing Changan Automobile Co., Ltd. for the experimental research.</p>
</ack>
<sec>
<title>Funding Statement</title>
<p>This research was funded by the Open Foundation of the State Key Laboratory of Vehicle NVH and Safety Technology (Grant No. NVHSKL-202202).</p>
</sec>
<sec>
<title>Author Contributions</title>
<p>Writing&#x2014;original draft: Liang Yang, Jie Zhang; Supervision, funding acquisition: Zhigang Chu; Methodology: Liang Yang, Jie Zhang, Jinfeng Xia; Simulation: Jie Zhang, Siwen Zhang; Validation: Jinfeng Xia, Siwen Zhang; Writing&#x2014;review and editing: Siwen Zhang, Yang Yang, Zhigang Chu. All authors reviewed the results and approved the final version of the manuscript.</p>
</sec>
<sec sec-type="data-availability">
<title>Availability of Data and Materials</title>
<p>The data used to support the findings of this study are available from the corresponding author upon request.</p>
</sec>
<sec>
<title>Ethics Approval</title>
<p>Not applicable.</p>
</sec>
<sec sec-type="COI-statement">
<title>Conflicts of Interest</title>
<p>The authors declare that they have no conflicts of interest to report regarding the present study.</p>
</sec>
<ref-list content-type="authoryear">
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