<?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">OJA</journal-id><journal-title-group><journal-title>Open Journal of Acoustics</journal-title></journal-title-group><issn pub-type="epub">2162-5786</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/oja.2014.41002</article-id><article-id pub-id-type="publisher-id">OJA-43754</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>
 
 
  Experimental Evaluation of Transmission Loss of a Glass Cylinder Tube Containing a Fluid
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>ader</surname><given-names>Mohammadi</given-names></name><xref ref-type="aff" rid="aff1"><sub>1</sub></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><aff id="aff1"><label>1</label><addr-line>Department of Mechanical Engineering, Islamic Azad University, Parand Branch, Tehran, Iran</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>nmohamady@ut.ac.ir</email></corresp></author-notes><pub-date pub-type="epub"><day>13</day><month>03</month><year>2014</year></pub-date><volume>04</volume><issue>01</issue><fpage>13</fpage><lpage>19</lpage><history><date date-type="received"><day>9</day>	<month>January</month>	<year>2014</year></date><date date-type="rev-recd"><day>9</day>	<month>February</month>	<year>2014</year>	</date><date date-type="accepted"><day>16</day>	<month>February</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>
 
 
  Transmission Loss
   
  (TL) of a glass cylinder tube containing a fluid is studied experimentally. This test specimen represents a typical double layer panel including a fluid. The tests are carried out 
  by 
  using a modified four-microphone standing-wave (impedance) tube for specimens with different lengths,
   
  15 and 30 mm. Each cylinder tube is tested filled with one of the fluids at a time. The fluids are air, water, motor oil and a nanoparticle
   
  fluid (in absence of magnetic field). The effects of the cylinder length (thickness), impedance tube terminations, and the containing fluid are discussed. 
  The 
  increasing
   of
   the thickness led to an increase of the TL values and a decrease in resonance frequencies. Also, the addition of liquid middle layer led to considerable increase of the TL.
 
</p></abstract><kwd-group><kwd>Transmission Loss; Impedance Tube; Transfer Matrix Method; Sound Pressure Measurement</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Sound transmission through multi-layered panels has been a subject of interest to many researchers since 1949 when Beranek and Work [<xref ref-type="bibr" rid="scirp.43754-ref1">1</xref>] derived the first model for predicting the Transmission Loss (TL) of multiple structures containing flexible blankets. Since then, due to the wide application of these panels in various fields such as aircraft, automotive and building industries, the acoustical performance of the panels has been studied closely. A number of theoretical models have been developed and evaluated by practical measurements [<xref ref-type="bibr" rid="scirp.43754-ref2">2</xref>] [<xref ref-type="bibr" rid="scirp.43754-ref3">3</xref>] .</p><p>In this paper, the TL of a glass cylinder tube when containing a fluid is studied experimentally. Evaluation of TL has been carried out by using a standing-wave tube. Both methods of two-load and anechoic termination which have been applied to measure the TL and the results have been analyzed. Cylindrical type glasses of different lengths (15 and 30 mm) are filled with a fluid. The effects of the cylinder length (thickness) and also the containing fluid are discussed. The cylinder walls are 1.5 mm thick and the cylinder diameter is 38 mm. The fluids used here are air, water, typical motor oil and a ferromagnetic nanoparticles fluid made by Iran Color Research Center (named NMF-128DV). This last one is tested in the absence of a magnetic field.</p></sec><sec id="s2"><title>2. TL Measurement Using a Standing-Wave Tube</title><p>The TL measurements with a standing wave tube are based on the transfer matrix method introduced by Munjal and Doige [<xref ref-type="bibr" rid="scirp.43754-ref4">4</xref>] . According to <xref ref-type="fig" rid="fig1">Figure 1</xref>, the sound field in each tube can be presented by the amplitudes of the waves travelling forward and backward in them the transmission loss matrix as follows</p><disp-formula id="scirp.43754-formula52523"><label>(1)</label><graphic position="anchor" xlink:href="htmlimages\2-1610096x\ddbfac7b-772d-4b4e-a4b7-6247d67f958f.png"  xlink:type="simple"/></disp-formula><p>The TL is then defined as</p><disp-formula id="scirp.43754-formula52524"><label>(2)</label><graphic position="anchor" xlink:href="htmlimages\2-1610096x\987f1578-185a-4fc1-822a-3bb466ce7022.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="tmlimages\2-1610096x\ef4a063e-0c34-4f66-a334-340a65936283.png" xlink:type="simple"/></inline-formula> is called the transmission loss factor, a frequency-dependant property of materials.</p><p>The four microphones measure the sound pressures at four indicated locations as follows</p><disp-formula id="scirp.43754-formula52525"><label>(3)</label><graphic position="anchor" xlink:href="htmlimages\2-1610096x\59461606-68a3-4396-99a2-700d56becaff.png"  xlink:type="simple"/></disp-formula><p>from which the four amplitudes can be uniquely calculated in terms of the four pressures, the wave number, and the geometric positioning of the microphones and the sample [<xref ref-type="bibr" rid="scirp.43754-ref5">5</xref>] . In order to calculate the TL, one has to determine the four interrelated parameters of the coefficients matrix in Equation (1), known as four-pole parameters [<xref ref-type="bibr" rid="scirp.43754-ref4">4</xref>] . To do so, two different techniques can be applied.</p><p>In the first method (namely two-load method), each sample is tested in two different tube termination conditions: closed by a rigid cap and left open (no cap). This will provide us with four equations in four unknowns which can be solved using the Kramer method. The transmission loss factor in this case is found to be</p><disp-formula id="scirp.43754-formula52526"><label>(4)</label><graphic position="anchor" xlink:href="htmlimages\2-1610096x\290d8bf7-03e0-4e4d-8990-974f1fce8993.png"  xlink:type="simple"/></disp-formula><p>The subscripts h and o here, denote the rigid cap and no cap, respectively. In the second method (i.e., the anechoic termination method), the backward-travelling wave D is cancelled by means of an anechoic termination at the tube end. This way the equations, in Equation (1), are decoupled and the transmission loss factor is easily found to be equal to the ratio of A to C.</p><p>The experimental results were obtained using the testing apparatus constructed for the TL measurements at Noise, Vibration and Acoustics (NVA) Research Center of the University of Tehran. Herein, both the two-load and anechoic termination methods have been carried out for each sample. A 10 cm rolled piece of glass wool is used at the tube termination for the open-cap tube-end condition. As for the cap-closed termination, no absorbent</p><p>is used so as to keep the two downstream boundary conditions of the tube more dissimilar. The fluid specimens were made of a Pyrex glass cylinder tube with 15 and 30 mm lengths, outer diameter 38 mm and 1.5 mm wall thickness (see <xref ref-type="fig" rid="fig2">Figure 2</xref>), filled with water, oil, and the nano-ferrofluid (NMF).</p></sec><sec id="s3"><title>3. Results and Discussion</title><p>The experimental TL values of several specimens are shown below in 1/3 Octave bands (630 Hz - 4 kHz) for different gaps (or fluid space) and various methods (i.e. two-load and anechoic termination methods), see Figures 3-6. According to the Figures, the use of a liquid as middle layer increases TL over the entire frequency range. At low frequencies, where the performance of middle air layer is poor, the liquid layer provides desirable performance. Fluid density affects the TL values more than other parameters (the wave velocity and the kinematic viscosity). Hence the TL s of the cylinder tube including water, oil, and nano-ferrofluid are close to each other. The application of the liquid layer increases the resonance frequencies and shifts them to higher frequencies, which might be an advantage.</p><p>In Figures 7-10, a comparison is made between the two-load method and the anechoic termination method. The results of both methods are close. However, the two-load method leads to smoother curve or less variation of TL values for a wide range of frequencies.</p><p> of similar densities result in a similar performance. Increasing the middle gap led to an increase of the TL values and a decrease in resonance frequencies. For example, in <xref ref-type="fig" rid="fig3">Figure 3</xref> (d = 15 mm), the resonance frequency of the air fluid is more than 5000 Hz and in  <xref ref-type="fig" rid="fig5">Figure 5</xref> (d = 30 mm), the resonance frequency is between 2000 Hz and 3000 Hz.</p><p>The results of both methods are close. However, the two-load method leads to smoother variation of TL values for a wide range of frequencies.</p></sec></body><back><ref-list><title>References</title><ref id="scirp.43754-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Beranek, L.L. and Work, G.A. (1949) Sound Transmission through Multiple Structures Containing Blankets. The Acoustical Society of America, 21, 419-428. http://dx.doi.org/10.1121/1.1906530</mixed-citation></ref><ref id="scirp.43754-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">London, A. (1950) Transmission of Reverberant Sound through Double Walls. The Acoustical Society of America, 22, 270-279. http://dx.doi.org/10.1121/1.1906601</mixed-citation></ref><ref id="scirp.43754-ref3"><label>3</label><mixed-citation publication-type="other" xlink:type="simple">Mulholland, K.A., Price, A.J. and Parbrook, H.D. (1968) Transmission Loss of Multiple Panels in a Random Incidence Field. The Acoustical Society of America, 43, 1432-1435. http://dx.doi.org/10.1121/1.1911003</mixed-citation></ref><ref id="scirp.43754-ref4"><label>4</label><mixed-citation publication-type="other" xlink:type="simple">Munjal, M.L. and Doige, A.G. (1990) Theory of a Two Source-Location Method for Direct Experimental Evaluation of the Four-Pole Parameters of an Aerospace Element. Journal of Sound and Vibration, 141, 323-333.http://dx.doi.org/10.1016/0022-460X(90)90843-O</mixed-citation></ref><ref id="scirp.43754-ref5"><label>5</label><mixed-citation publication-type="other" xlink:type="simple">Song, B.H. and Bolton, J.S. (2000) A Transfer-Matrix Approach for Estimating the Characteristic Impedance and Wave Numbers of Limp and Rigid Porous Materials. The Acoustical Society of America, 107, 1131-1152.http://dx.doi.org/10.1121/1.428404</mixed-citation></ref></ref-list></back></article>