<?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">WJM</journal-id><journal-title-group><journal-title>World Journal of Mechanics</journal-title></journal-title-group><issn pub-type="epub">2160-049X</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/wjm.2011.15030</article-id><article-id pub-id-type="publisher-id">WJM-8162</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Engineering</subject><subject> Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  Analytical Solution for Acoustic Waves Propagation in Fluids
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>ohamed</surname><given-names>I. A. Othman</given-names></name><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Mohamed</surname><given-names>Galal Sayed Ali</given-names></name><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Roushdi</surname><given-names>Mohamed Farouk</given-names></name><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><author-notes><corresp id="cor1">* E-mail:<email>m_i_othman@yahoo.com(OIAO)</email>;<email>mgalal09@yahoo.com(MGSA)</email>;<email>rmfarouk1@yahoo.com(RMF)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>25</day><month>10</month><year>2011</year></pub-date><volume>01</volume><issue>05</issue><fpage>243</fpage><lpage>246</lpage><history><date date-type="received"><day>July</day>	<month>12,</month>	<year>2011</year></date><date date-type="rev-recd"><day>August</day>	<month>20,</month>	<year>2011</year>	</date><date date-type="accepted"><day>September</day>	<month>2,</month>	<year>2011</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>
 
 
  This paper presents a mathematical model of linear acoustic wave propagation in fluids. The benefits of a mathematical model over a normal mode analysis are first discussed, then the mathematical model for acoustic propagation in the test medium is developed using computer simulations. The approach is based on a analytical solution to the homogeneous wave equation for fluid medium. A good agreement between the computational presented results with published data.
 
</p></abstract><kwd-group><kwd>Acoustic Waves</kwd><kwd> Normal Mode Analysis</kwd><kwd> Fluid Medium</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>In recent years, physical acoustic wave modeling has become a successful tool in diagnostic and therapeutic ultrasound application. There are several wave equations available for describing acoustic wave propagation [1-4]. Numerical methods can be used as a tool for sound field simulation. Discrete-time simulation algorithms for wave propagation can be derived by numerically solving a acoustic wave equation in terms of the variables for sound pressure and particle velocity. Initial conditions for time derivatives and boundary conditions for space derivatives are necessary to provide a complete set of solutions of the wave equation. These equations are most commonly solved by propagation in time. However, when propagating over large distances, such methods are expensive in terms of memory and computational costs [<xref ref-type="bibr" rid="scirp.8162-ref5">5</xref>].</p><p>The normal mode method analysis gives exact solutions without any assumed restrictions on pressure and velocity components distributions. It is applied to wide range of problems in different branches (Othman [6-8], Sharma et al. [<xref ref-type="bibr" rid="scirp.8162-ref9">9</xref>], Othman and Kumar [<xref ref-type="bibr" rid="scirp.8162-ref10">10</xref>], Othman and Singh [<xref ref-type="bibr" rid="scirp.8162-ref11">11</xref>] and Othman et al. [<xref ref-type="bibr" rid="scirp.8162-ref12">12</xref>]). It can be applied to boundary-layer problems, which are described by the linearized Navier-stokes equations in electrohydrodynamic (Othman [<xref ref-type="bibr" rid="scirp.8162-ref13">13</xref>]).</p><p>In this paper, the normal mode analysis can be employed to solve linear acoustic wave equation analytically. The technique focuses on description of a linear model and discuses the conditions under which using this technique. The propagation of acoustic pressure wave by the normal mood analysis in a medium with two-dimensional spatially-variable acoustic properties has been explained.</p></sec><sec id="s2"><title>2. Acoustic Wave Equation</title><p>Consider sound waves propagating in the water. Instead of the wave equation, we base our work on the basic Euler’s equation and the equation of continuity. For simplicity, the discussion is confined to a two-dimensional space. In a 2-D Cartesian coordinate system, the sound pressure <img src="4-4900038\4c7433d6-9b50-4fce-a4fe-19d24d4099f4.jpg" /> and the particle velocity v satisfy the following linear equations:</p><disp-formula id="scirp.8162-formula96394"><label>, (1)</label><graphic position="anchor" xlink:href="4-4900038\d63f1fe7-5110-4cb5-a5be-7ba30e6b68a8.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.8162-formula96395"><label>, (2)</label><graphic position="anchor" xlink:href="4-4900038\368f80e0-1c09-4787-9a91-56def4c3d397.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.8162-formula96396"><label>. (3)</label><graphic position="anchor" xlink:href="4-4900038\e2ab074a-c672-4be2-b80f-8c69e2defd5f.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="4-4900038\c13f57ea-ad4a-490e-ad8e-945e566d9604.jpg" /> is the particle velocity, p(x, y, t) is the pressure and <img src="4-4900038\c8c200d1-5c17-49b6-ac0a-b07e16a27b02.jpg" /> is the density of the fluid with wave number <img src="4-4900038\89487a25-43dd-4555-b63a-b29630897790.jpg" /> where</p><p><img src="4-4900038\d5940e8f-7823-4ca0-b4af-21c49984fbab.jpg" />, <img src="4-4900038\ebbbd3de-3f82-4455-b5d8-0f156fc2f5aa.jpg" />is the angular frequency, c and <img src="4-4900038\13367a1b-1677-4f9b-afcf-de932f2f568e.jpg" /> are the speed of sound and attenuation in inhomogeneous medium, respectively.</p></sec><sec id="s3"><title>3. Normal Mode Analysis</title><p>The solution of considered physical variable can be decomposed in terms of normal modes as the following form</p><disp-formula id="scirp.8162-formula96397"><label>(4)</label><graphic position="anchor" xlink:href="4-4900038\17c4bb12-cedd-4414-a737-6b751e9e5dfe.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="4-4900038\8c9f897d-50c5-4ad6-a9d4-d08cb96dcc3d.jpg" /> are the amplitude of the functions <img src="4-4900038\c8de0e88-e972-46e3-ba9d-d2b48e3452d3.jpg" /> respectively.</p><p>Equations (1)-(3) become</p><disp-formula id="scirp.8162-formula96398"><label>(5)</label><graphic position="anchor" xlink:href="4-4900038\f3f916e7-dcec-4184-ad28-50e3617fb8ec.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.8162-formula96399"><label>, (6)</label><graphic position="anchor" xlink:href="4-4900038\da2e06d6-148f-40ad-97bb-ad8586105320.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.8162-formula96400"><label>. (7)</label><graphic position="anchor" xlink:href="4-4900038\9574b9a3-246c-4c1c-95cf-c80825c29d27.jpg"  xlink:type="simple"/></disp-formula><p>where,<img src="4-4900038\2dad1303-12fe-44f9-a651-61a533d7085e.jpg" />.</p><p>Equations (5)-(7) form a coupled system Eliminating <img src="4-4900038\eea3c9a5-8ced-48dc-855b-31b7977c86f4.jpg" /> and <img src="4-4900038\951ca277-3366-4741-98c1-c7f7cc346b25.jpg" /> between Equations (5)-(7) we obtain</p><disp-formula id="scirp.8162-formula96401"><label>(8)</label><graphic position="anchor" xlink:href="4-4900038\15cfda1c-97ee-4357-9fe9-92af4b600fed.jpg"  xlink:type="simple"/></disp-formula><p>where,<img src="4-4900038\f4f7c9ed-31e0-44c3-99ff-94f972639778.jpg" />.</p><p>The solution of Equation (8) has the form</p><disp-formula id="scirp.8162-formula96402"><label>. (9)</label><graphic position="anchor" xlink:href="4-4900038\4099fef2-107f-4127-8d56-bd893f184775.jpg"  xlink:type="simple"/></disp-formula><p>where<img src="4-4900038\b427fd00-0471-4bea-b370-2eb848cd17c6.jpg" />, and <img src="4-4900038\7927cad1-ab10-43da-8566-6c1f7a0a676d.jpg" /> are the roots of the characteristic equation</p><disp-formula id="scirp.8162-formula96403"><label>(10)</label><graphic position="anchor" xlink:href="4-4900038\497b9a20-4e4e-4db9-9932-2119cfa62e73.jpg"  xlink:type="simple"/></disp-formula><p>The solution of Equation (8) is given by</p><disp-formula id="scirp.8162-formula96404"><label>(11)</label><graphic position="anchor" xlink:href="4-4900038\37711793-f373-497e-beab-6bb88d106b4c.jpg"  xlink:type="simple"/></disp-formula><p>From Equations (6) and (11) we can obtain</p><disp-formula id="scirp.8162-formula96405"><label>(12)</label><graphic position="anchor" xlink:href="4-4900038\45dffc7f-2931-4845-9dc2-9e156fc93e4b.jpg"  xlink:type="simple"/></disp-formula><p>where,</p><disp-formula id="scirp.8162-formula96406"><label>(13)</label><graphic position="anchor" xlink:href="4-4900038\f1205cfc-8f7d-4eab-ac54-08f36506ea01.jpg"  xlink:type="simple"/></disp-formula><p>From Equations (7) and (11) we can obtain</p><disp-formula id="scirp.8162-formula96407"><label>(14)</label><graphic position="anchor" xlink:href="4-4900038\297c09ea-f1cb-46df-83b1-8b880b09799d.jpg"  xlink:type="simple"/></disp-formula><p>where,</p><disp-formula id="scirp.8162-formula96408"><label>(15)</label><graphic position="anchor" xlink:href="4-4900038\795c8cd8-0a3e-402c-ade1-207784c1c98f.jpg"  xlink:type="simple"/></disp-formula></sec><sec id="s4"><title>4. Boundary Conditions</title><p>On the surface at x = 0</p><disp-formula id="scirp.8162-formula96409"><label>(16)</label><graphic position="anchor" xlink:href="4-4900038\64d2ea04-cd27-41bd-9a59-7f6d4bfefa79.jpg"  xlink:type="simple"/></disp-formula><p>Substituting from (4) into (16) then Equations (11) and (14)</p><disp-formula id="scirp.8162-formula96410"><label>(17)</label><graphic position="anchor" xlink:href="4-4900038\8453c214-dfe3-4d9a-89b7-5ef3989f81f8.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.8162-formula96411"><label>(18)</label><graphic position="anchor" xlink:href="4-4900038\677bbd46-972f-4966-bae8-8bc9a4c48109.jpg"  xlink:type="simple"/></disp-formula><p>By adding Equations (17) and (18) we obtain</p><disp-formula id="scirp.8162-formula96412"><label>(19)</label><graphic position="anchor" xlink:href="4-4900038\3f84c3bf-85f2-499b-9e09-e227a3291d99.jpg"  xlink:type="simple"/></disp-formula><p>By subtracting Equations (17) and (18) we get</p><disp-formula id="scirp.8162-formula96413"><label>(20)</label><graphic position="anchor" xlink:href="4-4900038\c7eb1c65-f966-4da8-ac0a-572b799a49b2.jpg"  xlink:type="simple"/></disp-formula><p>By substituting from Equations (19) and (20) into Equations (11), (12) and (14)</p><disp-formula id="scirp.8162-formula96414"><label>(21)</label><graphic position="anchor" xlink:href="4-4900038\9fbcc43a-f4bc-4b0b-864b-7656ff89977c.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.8162-formula96415"><label>(22)</label><graphic position="anchor" xlink:href="4-4900038\47a089aa-2478-4fc3-adff-bef9bc1fbdbd.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.8162-formula96416"><label>(23)</label><graphic position="anchor" xlink:href="4-4900038\b9e7ef31-3bf6-4b59-bf04-950c930ac6e8.jpg"  xlink:type="simple"/></disp-formula></sec><sec id="s5"><title>5. Computational Results</title><p>To study the wave propagation phenomenon in viscous medium and under different frequencies, we can apply the theoretical acoustic viscous wave Equation (21). Using water as the medium, the parameters are given as following: <img src="4-4900038\f9b5b231-07d0-4ec3-9dd0-2a44b16f36e7.jpg" />and<img src="4-4900038\67ac0dcb-a552-44aa-9c5f-b164ff682fcf.jpg" />. Let the wave peak amplitude be <img src="4-4900038\aeea26ba-790f-4e05-9dce-48a9ab551ec1.jpg" /> Pa and <img src="4-4900038\8be5b8fc-e084-427c-abda-84dd2b8a4d57.jpg" /> m/sec at the source (x = 0), we simulate the pressure wave peak amplitude, in Equation (21), vs. the distance from the source at various frequencies. The results are shown in <xref ref-type="fig" rid="fig1">Figure 1</xref> (in dB and linear scale). As expected, the peak wave amplitude becomes smaller as we move further from the source. We can also notice that as the wave frequency goes higher, more attenuation can be observed at any given location. The peak pressure as function of frequency shown in <xref ref-type="fig" rid="fig2">Figure 2</xref> for fixed distance at x = 2 cm. It is clear from this figure that the magnitude of peak of pressure little changes with the frequency. The predicted results are very agreement to the recorded by Wang [<xref ref-type="bibr" rid="scirp.8162-ref14">14</xref>].</p><p>Let us consider a 2-D simulation in which the pressure varies in the x and y directions. <xref ref-type="fig" rid="fig3">Figure 3</xref> shows the 2-D pressure computational as function in the plane x-y. From this figure, it can be seen that the pressure amplitude becomes smaller when moving in the x-y plane further from the source.</p></sec><sec id="s6"><title>6. Conclusions</title><p>A normal mode analysis which accurately the pressure acoustic wave equation, has been developed. This technique has a number of attractive features, foremost of which is the speed and simplicity with which it can be designed and implemented. The model could be used in</p><p>the future to incorporate non-linear propagation effects.</p></sec><sec id="s7"><title>REFERENCES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.8162-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">L. E. Kinsler, A. R. Frey, A. B. Coppens and J. V. Sanders, “Fundamentals of Acoustics,” 4th Edition, Wiley, New York, 2000.</mixed-citation></ref><ref id="scirp.8162-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">S. W. Rienstra and A. Hirschberg, “An Introduction to Acoustics,” Eindhoven University of Technology, Eindhoven, 2009.</mixed-citation></ref><ref id="scirp.8162-ref3"><label>3</label><mixed-citation publication-type="other" xlink:type="simple">S. W. 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