<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article  PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd"><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article"><front><journal-meta><journal-id journal-id-type="publisher-id">JAMP</journal-id><journal-title-group><journal-title>Journal of Applied Mathematics and Physics</journal-title></journal-title-group><issn pub-type="epub">2327-4352</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/jamp.2015.32025</article-id><article-id pub-id-type="publisher-id">JAMP-53667</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  Turbulent-Induced Noise around a Circular Cylinder Using Permeable FW-H Method
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Woen-Sug</surname><given-names>Choi</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Suk-Yoon</surname><given-names>Hong</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Jee-Hun</surname><given-names>Song</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Hyun-Wung</surname><given-names>Kwon</given-names></name><xref ref-type="aff" rid="aff3"><sup>3</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Chul-Min</surname><given-names>Jung</given-names></name><xref ref-type="aff" rid="aff4"><sup>4</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Tae-Gyoung</surname><given-names>Kim</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><aff id="aff3"><addr-line>Department of Naval Architecture and Ocean Engineering, Koje College, Koje, Republic of Korea</addr-line></aff><aff id="aff2"><addr-line>Department of Naval Architecture and Ocean Engineering, Chonnam National University, Yeosu, Republic of Korea</addr-line></aff><aff id="aff1"><addr-line>Departmentof Naval Architecture and Ocean Engineering, Seoul National University, Seoul, Republic of Korea</addr-line></aff><aff id="aff4"><addr-line>Advanced Naval Technology Center, NSRDI, Agency for Defense Development, Chinhae, Republic of Korea</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>kickflipin@snu.ac.kr(WC)</email>;<email>syh@snu.ac.kr(SH)</email>;<email>jhs@jnu.ac.kr(JS)</email>;<email>khw1@snu.ac.kr(HK)</email>;<email>cmjung@add.re.kr(CJ)</email>;<email>taegyoung@snu.ac.kr(TK)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>30</day><month>01</month><year>2015</year></pub-date><volume>03</volume><issue>02</issue><fpage>161</fpage><lpage>165</lpage><history><date date-type="received"><day>19</day>	<month>November</month>	<year>2014</year></date></history><permissions><copyright-statement>&#169; Copyright  2014 by authors and Scientific Research Publishing Inc. </copyright-statement><copyright-year>2014</copyright-year><license><license-p>This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/</license-p></license></permissions><abstract><p>
 
 
   Varieties of research on turbulent-induced noise are conducted with combinations of acoustic analogy methods and computational fluid dynamic methods to analyse efficiently and accurately. Application of FW-H acoustic analogy without turbulent noise is the most popular method due to its calculation cost. In this paper, turbulent-induced noise is predicted using RANS turbulence model and permeable FW-H method. For simplicity, noise from 2D cylinder is examined using three different methods: direct method of RANS, FW-H method without turbulent noise and permeable FW-H method which can take into account of turbulent-induced noise. Turbulent noise was well predicted using permeable FW-H method with same computational cost of original FW-H method. Also, ability of permeable FW-H method to predict highly accurate turbulent-induced noise by applying adequate permeable surface is presented. The procedure to predict turbulent- induced noise using permeable FW-H is established and its usability is shown. 
 
</p></abstract><kwd-group><kwd>Turbulent-Induced Noise</kwd><kwd> Circular Cylinder</kwd><kwd> Acoustic Analogy</kwd><kwd> FW-H Method</kwd><kwd> Permeable FW-H Method</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Objects in motion in fluid disturb its surroundings to produce noise. Such noise can be predicted using Kirchhoff formula or Acoustic analogy [<xref ref-type="bibr" rid="scirp.53667-ref1">1</xref>]. The Acoustic analogy method has advantage over Kirchhoff formula due to its representation of noise in three pressure terms according to its physical meanings: thickness noise, loading noise and quadruple noise [<xref ref-type="bibr" rid="scirp.53667-ref2">2</xref>]. Meanwhile, in the view point of far-field radiation noise, turbulent-induced quadrupole noise term has usually been neglected to reduce computational cost [<xref ref-type="bibr" rid="scirp.53667-ref1">1</xref>]. Moreover, it has recently been found that the turbulent-induced noise is also important to understand characteristics of overall noise in far-field [<xref ref-type="bibr" rid="scirp.53667-ref3">3</xref>].</p><p>The turbulent-induced noise can be predicted correctly using DNS (Direct Numerical Simulation) method. However it is almost impossible because of high computational cost [<xref ref-type="bibr" rid="scirp.53667-ref4">4</xref>] [<xref ref-type="bibr" rid="scirp.53667-ref5">5</xref>]. Therefore, hybrid method to utilize computational fluid dynamics (CFD) with turbulent models and acoustic analogy introduced by Lighthill to reduce computational expense is being researched actively [<xref ref-type="bibr" rid="scirp.53667-ref1">1</xref>]. Based on Lighthill’s analogy [<xref ref-type="bibr" rid="scirp.53667-ref6">6</xref>], FW-H (Ffowcs Williams and Hawkings) analogy [<xref ref-type="bibr" rid="scirp.53667-ref2">2</xref>] without considering quadrupole term is commonly used to consider object moving in arbitrary motion [<xref ref-type="bibr" rid="scirp.53667-ref7">7</xref>].</p><p>In this study, the use of RANS (Reynolds Averaged Navier-Stokes) turbulent model of CFD and permeable FW-H which accommodates permeable surface is shown to predict turbulent-induced noise. Direct method to directly extract perturbing pressure, FW-H method without quadruple term, and permeable FW-H which includes the effects of turbulence are compared for 2-dimensional circular cylinder. Permeable FW-H method has shown to well predict the influence of turbulent noise compared to the method without quadruple term. Moreover, it is shown that careful selection of permeable surface can result in high accuracy from permeable FW-H method.</p></sec><sec id="s2"><title>2. Basic Theory of Acoustic Analogy</title><p>Lighthill has introduced the wave equation of acoustic analogy having the source derived by comparing the exact equations of motion of a fluid with the equations of sound propagation in a medium at rest as follows [<xref ref-type="bibr" rid="scirp.53667-ref6">6</xref>],</p><disp-formula id="scirp.53667-formula456"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/53667x4.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.53667-formula457"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/53667x5.png"  xlink:type="simple"/></disp-formula><p>Here <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x6.png" xlink:type="simple"/></inline-formula> density perturbation, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x7.png" xlink:type="simple"/></inline-formula>light hill’s stress tensor, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x8.png" xlink:type="simple"/></inline-formula>compressive stress tensor, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x9.png" xlink:type="simple"/></inline-formula>velocity of sound in fluid at rest, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x10.png" xlink:type="simple"/></inline-formula>component of velocity in direction<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x11.png" xlink:type="simple"/></inline-formula>.</p><p>Curle’s analogy have expanded the Lighthill’s theory considering rigid surface (Curle, 1995), an Ffowcs Williams and Hawkings have further generalized the theory considering rigid object in arbitrary motion as follows [<xref ref-type="bibr" rid="scirp.53667-ref2">2</xref>],</p><disp-formula id="scirp.53667-formula458"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/53667x12.png"  xlink:type="simple"/></disp-formula><p>Here, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x13.png" xlink:type="simple"/></inline-formula>represents body surface as function of<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x14.png" xlink:type="simple"/></inline-formula>; <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x15.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x16.png" xlink:type="simple"/></inline-formula> meaning inside and outside of rigid body, respectively. First term physically means unsteadiness inside the fluid expressed in quadruple source as Reynolds stress which is called turbulent-induced term. Second term is monopole source due to dilatation of boundaries and third term is dipole source modeled from fluctuating stresses on the surface. Second term and third term is called loading noise term and thickness noise terms, respectively.</p><p>Farassat’s formulation develops FW-H analogy equation into following integral forms [<xref ref-type="bibr" rid="scirp.53667-ref8">8</xref>],</p><disp-formula id="scirp.53667-formula459"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/53667x17.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.53667-formula460"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/53667x18.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.53667-formula461"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/53667x19.png"  xlink:type="simple"/></disp-formula><p>Here, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x20.png" xlink:type="simple"/></inline-formula>is Doppler factor, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x21.png" xlink:type="simple"/></inline-formula>, and all terms evaluated in retarded time<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x20.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x22.png" xlink:type="simple"/></inline-formula>.</p><p>Turbulent term which is represented as quadrupole source is in volume integration. Decision of the volumes in fluid around rigid body to integrate and evaluation of the integration kernel is difficult [<xref ref-type="bibr" rid="scirp.53667-ref9">9</xref>]. Permeable FW-H method starts from setting the permeable surface by modifyingthe assumption of surface <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x23.png" xlink:type="simple"/></inline-formula> that the normal velocity of fluid <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x24.png" xlink:type="simple"/></inline-formula> and normal velocity of rigid body <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x25.png" xlink:type="simple"/></inline-formula> is equal <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x25.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/53667x26.png" xlink:type="simple"/></inline-formula> to be unequal. By so, calculation of thickness and loading noise on permeable surface (Inner-Cell) includes the turbulent-induced noise inside the surface [<xref ref-type="bibr" rid="scirp.53667-ref1">1</xref>] [<xref ref-type="bibr" rid="scirp.53667-ref8">8</xref>].</p></sec><sec id="s3"><title>3. Noise Analysis of 2-Dimensional Circular Cylinder</title><sec id="s3_1"><title>3.1. Construction of Mesh</title><p>To analyze the circular cylinder with 20 mm diameter, total of 218,268 cells are constructed. Receiver points for acoustic analysis are place at perpendicular to the flow direction downward from the cylinder in distance of 10 mm, 70 mm. Dimensionless Wall Distance (Wall Y+) is set to lower than 1 to accurately calculate boundary layers. In addition, overall mesh takes from of C-H for better quality such as skewness and orthogonality around the cylinder.</p><p>Permeable surface (Inner-Cell) for permeable FW-H method is set to include boundary layers and 3 - 4 vortex shedding as in <xref ref-type="fig" rid="fig1">Figure 1</xref>.</p></sec><sec id="s3_2"><title>3.2. Simulation of Turbulent Flow</title><p>Ansys FLUENT v14.5 is used for CFD calculation and also FW-H method without turbulent term and permeable FW-H with Inner-Cell boundary condition [<xref ref-type="bibr" rid="scirp.53667-ref7">7</xref>]. CFD calculation is done in pressure based, transient 2nd-or- der implicit in time and 3rd-order MUSCL in space with SIMPLE scheme and results are shown in <xref ref-type="fig" rid="fig2">Figure 2</xref>. To verify the flow simulation, the results are compared with the reference [<xref ref-type="bibr" rid="scirp.53667-ref10">10</xref>].</p><p><xref ref-type="fig" rid="fig2">Figure 2</xref>(a) and <xref ref-type="fig" rid="fig2">Figure 2</xref>(b) show flow simulation results of dynamic pressure and pressure coefficient. <xref ref-type="fig" rid="fig2">Figure 2</xref>(b) shows good agreement with the reference [<xref ref-type="bibr" rid="scirp.53667-ref11">11</xref>]. In <xref ref-type="table" rid="table1">Table 1</xref>, it is verified the Strouhal number of simulation compared to references [<xref ref-type="bibr" rid="scirp.53667-ref10">10</xref>] [<xref ref-type="bibr" rid="scirp.53667-ref11">11</xref>].</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Structured mesh with permeable surface (Inner-Cell), 218,168 volume cells</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53667x27.png"/></fig><fig-group id="fig2"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> CFD results of the circular cylinder: left: dynamic pressure; right: pressure coefficient.</title></caption><fig id ="fig2_1"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53667x28.png"/></fig><fig id ="fig2_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53667x29.png"/></fig></fig-group><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Comparison of Strouhal number</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >K − ω SST</th><th align="center" valign="middle" >Strouhal No. (S<sub>t</sub>)</th></tr></thead><tr><td align="center" valign="middle" >Experiment (Park, 2012)</td><td align="center" valign="middle" >0.195</td></tr><tr><td align="center" valign="middle" >Experiment (Norberg, 2003)</td><td align="center" valign="middle" >0.190</td></tr><tr><td align="center" valign="middle" >Simulations (Park, 2012)</td><td align="center" valign="middle" >0.198</td></tr><tr><td align="center" valign="middle" >Simulations (Orselli, 2009)</td><td align="center" valign="middle" >0.247</td></tr><tr><td align="center" valign="middle" >Result</td><td align="center" valign="middle" >0.222</td></tr></tbody></table></table-wrap></sec><sec id="s3_3"><title>3.3. Turbulent-Induced Noise Analysis</title><p><xref ref-type="fig" rid="fig3">Figure 3</xref> shows results due to different methodology to predict turbulent-induced noise. Direct method to directly extract perturbing pressure, FW-H without quadruple term which means turbulent noise (FW-H w/0 Quad.) and Permeable FW-H method by using permeable surface (Inner-Cell) are compared. The difference between the FW-H w/o Quad. and Permeable FW-H can be considered as the noise due to the turbulence with the magnitude of 10 dB ref 20 μPa. The results shows good results except the results at receiver 1 which is inside the permeable surface.</p><p>Considering the fact that the FW-H without quadruple term cannot represent the noise by the turbulence implies that the permeable FW-H method has well predicted the turbulence-induced noise. It can be stated from the result that the procedure to predict turbulent-induced noise is established. Also, it is shown that the Permeable FW-H method is robust compared to the standard FW-H method.</p></sec><sec id="s3_4"><title>3.4. Turbulent-Induced Noise Analysis Underwater</title><p><xref ref-type="fig" rid="fig4">Figure 4</xref> shows results by the same procedure but underwater environment. Considering the Reynolds number, the fluid velocity is set to be 10 m/s. Comparing to the results that of the air, the noise due to the turbulence shows the magnitude of 20 dB 10 μPa and also the quadruple noise reduces overall noise at the range over 200 Hz.</p><p>Here, permeable FW-H also shows good agreement toward the direct method showing the similar characteristics that of the results in air. This also represents the robustness of the permeable FW-H method.</p><p>Accurate results can be obtained from FW-H methods inside the permeable surface both in air and underwater. In <xref ref-type="fig" rid="fig5">Figure 5</xref>, it is shown that the results of the permeable FW-H method by using the reversed permeable surface well match the direct method inside the permeable surface. In conclusion, the choice of Inner-Cell has great influence in the final prediction of turbulence noise.</p><fig-group id="fig3"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Comparison of sound pressure level spectrum obtained from different method at 30 m/s, Receiver 1 (10 mm), Receiver 4 (70 mm).</title></caption><fig id ="fig3_1"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53667x30.png"/></fig><fig id ="fig3_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53667x31.png"/></fig></fig-group><fig-group id="fig4"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Comparison of sound pressure level spectrum underwater obtained from different method at 10 m/s, Receiver 1 (10 mm), Receiver 4 (70 mm).</title></caption><fig id ="fig4_1"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53667x32.png"/></fig><fig id ="fig4_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53667x33.png"/></fig></fig-group><fig-group id="fig5"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Comparison of sound pressure level spectrum underwater having permeable FW-H method with reversed normal vector at 10 m/s, Receiver 1 (10 mm), Receiver 4 (70 mm).</title></caption><fig id ="fig5_1"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53667x34.png"/></fig><fig id ="fig5_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/53667x35.png"/></fig></fig-group></sec></sec><sec id="s4"><title>4. Conclusions</title><p>Prediction of the turbulence-induced noise around 2-dimensional circular cylinder is done by the three different methods: direct method to directly extract perturbing pressure, FW-H without quadruple term which represents the noise due to the turbulence and permeable FW-H method which includes the turbulent-induced noise.</p><p>The difference between the direct method and the FW-H without quadruple term represents the magnitude of the noise due to the turbulence. Permeable FW-H method shows good agreement with the direct method. The robustness of the permeable FW-H method is shown from different results that the permeable FW-H method can well predict the noise produced from turbulence. By reversing the normal vector of the permeable surface, the near-field prediction could improve its accuracy. In conclusion, the procedure to predict turbulent-induced noise by using the permeable FW-H method is established and its usefulness is shown.</p><p>In further studies, the selection of Inner-Cell considering not only the size of the surface but also the length and frequency of vortex shedding and turbulent-induced noise prediction in more complex geometries are considered to generalize the current procedure of predicting the turbulent-induced noise.</p></sec><sec id="s5"><title>Cite this paper</title><p>Woen-Sug Choi,Suk-Yoon Hong,Jee-Hun Song,Hyun-Wung Kwon,Chul-Min Jung,Tae-Gyoung Kim, (2015) Turbulent-Induced Noise around a Circular Cylinder Using Permeable FW-H Method. Journal of Applied Mathematics and Physics,03,161-165. doi: 10.4236/jamp.2015.32025</p></sec><sec id="s6"><title>NOTES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.53667-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Wang, M., Freund, J.B. and Lele, S.K. (2006) Computational Prediction of Flow-Generated Sound. Annual Review of Fluid Mechanics, 38, 483-512. http://dx.doi.org/10.1146/annurev.fluid.38.050304.092036</mixed-citation></ref><ref id="scirp.53667-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">Ffowcs Williams, J.E. and Hawkings, D.L. (1969) Sound Generation by Turbulence and Surfaces in Arbitrary Motion. 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