<?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">NS</journal-id><journal-title-group><journal-title>Natural Science</journal-title></journal-title-group><issn pub-type="epub">2150-4091</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/ns.2014.610068</article-id><article-id pub-id-type="publisher-id">NS-46944</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>BIOMEDICAL &amp; LIFE SCIENCES</subject><subject>CHEMISTRY &amp; MATERIALS SCIENCE</subject><subject>EARTH &amp; ENVIRONMENTAL SCIENCES</subject><subject>PHYSICS &amp; MATHEMATICS</subject></subj-group></article-categories><title-group><article-title>Nose and Sinus Air Flow Model</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>R.</surname><given-names>De Luca</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>M.</surname><given-names>Gamerra</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>G.</surname><given-names>Sorrentino</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>E.</surname><given-names>Cantone</given-names></name><xref ref-type="aff" rid="aff3"><sup>3</sup></xref></contrib></contrib-group><aff id="aff3"><addr-line>Department of Neuroscience, Reproductive and Odontostomatologic Science, ENT Unit, “Federico II” 
University, Naples, Italy</addr-line></aff><aff id="aff1"><addr-line>Department of Physics "E. R. Caianiello", University of Salerno, Fisciano, Italy</addr-line></aff><aff id="aff2"><addr-line>Divisione di Otorinolaringoiatria, Ospedale “S. Leonardo”-A.S.L. NA 3 sud, Castellammare di Stabia, Italy</addr-line></aff><pub-date pub-type="epub"><day>18</day><month>06</month><year>2014</year></pub-date><volume>06</volume><issue>10</issue><fpage>685</fpage><lpage>690</lpage><history><date date-type="received"><day>10</day>	<month>April</month>	<year>2014</year></date><date date-type="rev-recd"><day>10</day>	<month>May</month>	<year>2014</year>	</date><date date-type="accepted"><day>17</day>	<month>May</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>Air flow in nose and sinuses is studied by means of
a simple model based on the steady-state ideal fluid flow assumption and repeated use of Bernoulli’s equation. In particular, by
describing flow of air drawn in through the vestibulumnasi during inspiration,
we investigate how ventilation of the maxillary sinus is affected by surgical
removal of part of the lateral walls of the nasal cavity close to the ostiummeatal complex. We find that, according to the model
proposed, removal of tissues from this inner part of the nasal cavity may cause
a decrease of the flux rate from the maxillary sinus.

	
</p></abstract><kwd-group><kwd>Air Flow Model</kwd><kwd> Nose and Sinus</kwd><kwd> Bernoulli's Equation</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The human ventilation system works by means of gaseous exchanges, which takes place between the nose and sinus cavities, and between the latter and the blood circle through the mucosa [<xref ref-type="bibr" rid="scirp.46944-ref1">1</xref>] . During respiratory acts, air flowing in the nasal cavity reaches the paranasal sinuses through the hosts and their ducts [<xref ref-type="bibr" rid="scirp.46944-ref2">2</xref>] . Therefore, a cor- rect anatomical and physiological equilibrium which is able to generate effective pressure gradients inside the nasal cavity plays an important role in the ventilation of the sinus cavities. During a single inhalation, air flows from the vestibulum towards the coana and produces, by “sucking effect”, negative pressures into the ostium- metal complex [<xref ref-type="bibr" rid="scirp.46944-ref3">3</xref>] . As a result, at the beginning of each nasal inhalation action, a negative nose pressure is gen- erated, in such a way that air flows out from the sinus cavities, due to the effect of aspiration. Air successively re-enters these cavities when the inspiration phase ends, and thus one of the continuous life-long respiratory cy- cles is completed. A fundamental role for a correct ventilation is thus played by the anatomical conformation of the ostiummeatal complex [<xref ref-type="bibr" rid="scirp.46944-ref4">4</xref>] .</p><p>In sinus physiology, air exchange is also regulated by diffusive molecular mechanisms related to the chemical and physical characteristics of the inhaled air mixture. The correct and continuous sinus ventilation due to the physical phenomenon described above is the reason why air in the sinus cavities is always in motion. The shape of the nasal cavity can be assimilated to that of a tube to which, under stationary conditions and ideal fluid flow, Bernoulli’s equation can be applied. Under the hypothesis of applicability of Bernoulli’s equation, therefore, the single particles of the fluid are taken to describe laminar trajectories with no energy loss in all ducts.</p><p>In the present work, the problem of air flow through the ostiummeatal complex coming from the maxillary sinus is studied by means of repeated use of Bernoulli’s equation. The work is thus organized as follows. In the following section, we give a detailed description of the model adopted. In the third section, we solve the model equations by means of a first-order perturbation approach, deriving a direct analytic dependence between the flux rate in the infundibulum and the nose’s effective section. Conclusions are drawn in the last.</p></sec><sec id="s2"><title>2. The Model</title><p>We consider the schematic model of the ostium-meatal complex reported in <xref ref-type="fig" rid="fig1">Figure 1</xref>. In this figure we sche- matize the maxillary sinus as a spherical cavity (M), in which air at the atmospheric pressure is present. The os- tiummeatal complex is seen as a short duct linking the nasal cavity (N) to the maxillary sinus. In the schematic representation of <xref ref-type="fig" rid="fig1">Figure 1</xref>, during inspiration air enters the nose through the vestibulumnasi and comes out through the coana (C-posterior). This air-flow produces a depression in N close to the ostiummeatal complex, sucking air from the maxillary sinus.</p><p>By denoting with S<sub>0</sub> and S<sub>1</sub> the effective sections of the inner and outer portions of the nasal cavity, respec- tively, and by S<sub>2</sub> the effective section of the ostiummeatal complex, we assume that air behaves as an ideal fluid [<xref ref-type="bibr" rid="scirp.46944-ref5">5</xref>] through these cavities. Air flows with velocities V<sub>0</sub>, V<sub>1</sub>, and V<sub>2</sub> through the correspondingly indexed sections, so that, by continuity equation we can write the following relations for the flow rates in these sections:</p><disp-formula id="scirp.46944-formula4597"><label>. (1)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\36b56ee7-619d-49cf-be8b-78d80a7543f5.png"/></disp-formula><p>By extending Bernoulli’s equation to a Y-shaped tube [<xref ref-type="bibr" rid="scirp.46944-ref6">6</xref>] , in the absence of gravitational effects, we may write:</p><disp-formula id="scirp.46944-formula4598"><label>. (2)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\7e0abd90-c4d5-49c6-8a5e-8ca195f2523c.png"/></disp-formula><p>where p<sub>0</sub> and p<sub>1</sub> are the pressures in the inner and outer portions of the nasal cavity, respectively, and p<sub>2</sub> is the</p><fig id="fig1"><label>Figure 1</label><caption><p> A schematic representation of the ostium-meatal complex. Air, drawn trough the vestibulim nasi, enters the nasal cavity (N) with velocity V<sub>1</sub>. Air fromthe ostium-meatal complex, having velocity V<sub>2</sub>, mixes with inhaled air in the inner nasal cavity towards the coana (C) during inspiration. Air from the maxillary sinus (M) is assumed to be at rest at atmosperic pressure p<sub>a</sub></p></caption><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\cbb9309c-3da3-4f96-b5ca-6982ab1e5e84.png"/></fig><p>pressure in the ostiummeatal complex. Moreover, in Equation (2) ρ is the density of air, Δτ<sub>1</sub> is the volume of the inhaled air, Δτ<sub>2</sub> is the volume of air drawn from the ostiummeatal complex and Δτ<sub>0</sub> is the volume of air flowing in the coana, given by:</p><disp-formula id="scirp.46944-formula4599"><label>. (3)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\73617ca8-4d46-4692-9e8b-1aafbc6220cb.png"/></disp-formula><p>Notice that Equation (3) is a mere consequence of Equation (1). In this way, Equation (2) can be rewritten in terms of the volume flow rates, defined in Equation (1), as follows:</p><disp-formula id="scirp.46944-formula4600"><label>(4)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\1d6cfecc-cfca-4c46-965b-6725d8df27bf.png"/></disp-formula><p>By Bernoulli’s equation, considering a point in M and a point in the ostiummeatal complex, we can write</p><disp-formula id="scirp.46944-formula4601"><label>(5)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\97d84d06-38af-4e9c-a1f8-5a82f3e64e9a.png"/></disp-formula><p>where p<sub>a</sub> is the atmospheric pressure. Moreover, by assuming that air flowing in the vestibulumnasi is drawn at constant velocity V<sub>L</sub> during inspiration, we have:</p><disp-formula id="scirp.46944-formula4602"><label>(6a)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\2bc649ed-9ca2-48e5-9c49-805d301c8ea8.png"/></disp-formula><disp-formula id="scirp.46944-formula4603"><label>. (6b)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\6695d6ca-8db4-40af-a2ad-d4a5c8db7ad4.png"/></disp-formula><p>where k<sub>V</sub> is a constant and S<sub>V</sub> is the effective section of the vestibulumnasi. In this respect, we need to specify that the assumption on V<sub>V</sub> is correlated to the patient’s needs of air intake, which can safely be assumed to be constant. On the other hand, the value of k<sub>V</sub> is the sum of the atmospheric pressure and of the dynamical pressure term linked to V<sub>V</sub>. This term, though varying from individual to individual, remains constant for a single patient. By now considering Equations (5) and (6a-b), we may rewrite Equation (4) in the following way:</p><disp-formula id="scirp.46944-formula4604"><label>, (7)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\4947e481-6e43-4d00-9518-68878040cb40.png"/></disp-formula><p>where Φ<sub>I</sub> = S<sub>2</sub>V<sub>2</sub> is the flux rate inside the ostiummeatal complex. By implicitly differentiating Equation (7) and by noticing that, by Equations (1) and (6b), dΦ<sub>I</sub> = d(S<sub>0</sub>V<sub>0</sub>), we write:</p><disp-formula id="scirp.46944-formula4605"><label>(8)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\4871c2cd-3d4e-48a8-897a-7e4bdc3dfa07.png"/></disp-formula><p>where the differential quantity dΦ<sub>I</sub> accounts for an infinitesimal variation of the flux rate in the ostiummeatal complex solely due to a corresponding infinitesimal variation S<sub>0</sub> of the coana effective section. In order to obtain a set of equations by which we can directly relate dΦ<sub>I</sub> with dS<sub>0</sub>, we introduce one further assumption, i.e., that air can flow at the same temperature inside the nasal cavity before and after the variation dS<sub>0</sub> has taken place, so that:</p><disp-formula id="scirp.46944-formula4606"><label>(9)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\11b74453-677f-4151-973c-20ff0ab079e9.png"/></disp-formula><p>By now substituting the above expression in Equation (8) we have:</p><disp-formula id="scirp.46944-formula4607"><label>. (10)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\64ac52f4-e9de-42b0-ab65-4c043e785b35.png"/></disp-formula><p>We notice that in Equation (10) dV<sub>0</sub> can be related to dS<sub>0</sub> by equating the expression dΦ<sub>I</sub> = d(S<sub>0</sub>V<sub>0</sub>), following from Equations (1) and (6b), to the expression for dΦ<sub>I</sub> obtained from Equation (10). In this way, we have:</p><disp-formula id="scirp.46944-formula4608"><label>. (11)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\7513a8a6-95be-4c42-8b95-880af4488b3a.png"/></disp-formula><p>By considering Equation (11), it is now not difficult to show that an implicit functional relation of V<sub>0</sub> in terms of S<sub>0</sub> is given by the following expression:</p><disp-formula id="scirp.46944-formula4609"><label>. (12)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\ccc1e926-bd26-4d5f-ba0d-4741277664f3.png"/></disp-formula><p>where k is a constant parameter referring to a specific group of patients. In order to obtain a meaningful order of magnitude for k, we might consider the main term in Equation (12), namely, the product p<sub>a</sub>V<sub>0</sub>S<sub>0</sub>. In this way, we notice that, for V<sub>0</sub> ≈ 5.0 cm/s and for S<sub>0</sub> ≈ 100 mm<sup>2</sup>, we have k of about 5.0 N∙m∙s<sup>−1</sup>. Equation (12) can now be inverted either numerically, either analytically, in order to obtain V<sub>0</sub> vs. S<sub>0</sub> curves, which we show in <xref ref-type="fig" rid="fig2">Figure 2</xref> for various values of the constant parameter k. Considering now Equations (10) and (11), we can set:</p><disp-formula id="scirp.46944-formula4610"><label>, (13)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\fdf0084c-a9e7-4d38-9cea-85cd1c305ae7.png"/></disp-formula><p>which directly relates the infinitesimal change dΦ<sub>I</sub> to dS<sub>0</sub>. By means of Equation (12) it could be possible to find how the flux rate Φ<sub>I</sub> depends explicitly on S<sub>0</sub>. However, in the following section, we shall adopt a perturbation approach to obtain this dependence.</p></sec><sec id="s3"><title>3. Perturbation Solution and Approximated Results</title><p>In the previous section we have obtained Equations (12) and (13), which represent the solution to the proposed problem of finding how the flux rate Φ<sub>I</sub> inside the ostiummeatal complex varies with respect to the effective area of the coana S<sub>0</sub>. Even though an analytic expression for such dependence can in principle be found, it is not convenient to proceed in this way, since a perturbation approach can be adopted, given that the dynamic pressure ρV<sub>0</sub><sup>2</sup>/2 is, for this type of system, much smaller than p<sub>a</sub>. With this in mind, to first order in the term ρV<sub>0</sub><sup>2</sup>/2p<sub>a</sub>, Equations (12) and (13) can be written in the following way:</p><disp-formula id="scirp.46944-formula4611"><label>, (14a)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\5195c1fa-64d6-4b00-82c5-2c8cf408272d.png"/></disp-formula><disp-formula id="scirp.46944-formula4612"><label>. (14b)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\2907d139-dd05-4496-94ec-f74c681c5251.png"/></disp-formula><p>Solving for V<sub>0</sub> in Equation (14a), we have:</p><disp-formula id="scirp.46944-formula4613"><label>, (15)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\fda6e618-87ac-4da2-8041-f45ad8905ebb.png"/></disp-formula><fig id="fig2"><label>Figure 2</label><caption><p> The velocity V<sub>0</sub> of air in the inner part of the nasal cavity as a function of the effective area S<sub>0</sub> for ρ = 1.29 kg∙m<sup>−3</sup>, p<sub>a</sub> = 1.0 atm and for the following values of the parameter k (from bottom to top): 6, 7, 8, 9 N∙m∙s<sup>−1</sup></p></caption><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\a770e347-2f00-4ed0-8ee1-5edda0c7159a.png"/></fig><p>In this expression we chose the minus sign in front of the square root, since it correctly gives a decreasing behavior of V<sub>0</sub> for small values of S<sub>0</sub> and take S<sub>0</sub><sup>2</sup> &gt; 2ρk<sup>2</sup>/p<sub>a</sub><sup>3</sup>. In <xref ref-type="fig" rid="fig2">Figure 2</xref>, we show the velocity V<sub>0</sub> of air in the inner part of the nasal cavity as a function of the effective area S<sub>0</sub>, as given by Equation (15), for ρ = 1.29 kg∙m<sup>−3</sup>, p<sub>a</sub> = 1.0 atm, and the following values of the parameter k (from bottom to top): 6, 7, 8, 9 N∙m∙s<sup>−1</sup>.</p><p>Substituting now Equation (15) in Equation (14), we finally have:</p><disp-formula id="scirp.46944-formula4614"><label>, (16)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\9d2a9cf5-1cb6-4ac0-9253-a05f51a300ab.png"/></disp-formula><p>By now calling A = p<sub>a</sub><sup>5</sup>/ρ<sup>2</sup>∙k<sup>3</sup> and B = 2 ρk<sup>2</sup>/p<sub>a</sub><sup>3</sup>, we may easily integrate Equation (16), obtaining</p><disp-formula id="scirp.46944-formula4615"><label>, (17)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\4ba285ef-569a-453e-beaf-b6ae73797de6.png"/></disp-formula><p>where c is a constant. Since we are only interested in finite variations of Φ<sub>I</sub>, we do not need to calculate the con- stant c. Moreover, we make take Equation (16) as the first-order approximation of the flux rate variation ΔΦ<sub>I</sub> due to a finite variation of the nasal cavity effective section ΔS<sub>0</sub>, so that</p><disp-formula id="scirp.46944-formula4616"><label>(18)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\04e9139c-acc0-4f83-9fe1-b501ebbd23ba.png"/></disp-formula><p>The above equation can be considered as an approximation to the solution to the problem we considered in the present work. For some typical values of the parameters in Equation (18) and for an effective section of about one tenth of a square centimeter, the coefficient linking ΔΦ<sub>I</sub> and ΔS<sub>0</sub> is found to be numerically equal to 8.6 &#215; 10<sup>−3</sup> m∙s<sup>−1</sup>. In this way, by taking, for example, ΔS<sub>0</sub> = 1.0 mm<sup>2</sup>, we have ΔΦ<sub>I</sub> = −8.6 mm<sup>3</sup>∙s<sup>−1</sup>. The deriva- tive dΦ<sub>I</sub>/dS<sub>0</sub>, as it can be obtained from Equation (16), is represented, as a function of S<sub>0</sub>, in <xref ref-type="fig" rid="fig3">Figure 3</xref> for ρ = 1.29 kg∙m<sup>−3</sup>, p<sub>a</sub> = 1.0 atm, and for the following values of the parameter k (from top to bottom): 6, 7, 8, 9 N∙m∙s<sup>−1</sup>. From <xref ref-type="fig" rid="fig3">Figure 3</xref> and from Equation (18) it can be seen that the derivative dΦ<sub>I</sub>/dS<sub>0</sub> is negative, so that any positive variation of S<sub>0</sub> causes a decrease of the flux rate in the ostiummeatal complex. In this respect, one might argue that surgical removal of anatomical structures close to the ostiummeatal complex might worsen the venti- lation functional efficacy of the maxillary sinus. This particular aspect has been already observed when analyz- ing the effectiveness of sinus ventilation with the aid of nose and sinus manometric measurements [<xref ref-type="bibr" rid="scirp.46944-ref7">7</xref>] . In these particular studies it was found that better functional results can be achieved by using a conservative surgical technique preserving nose anatomy rather than a non-conservative endoscopic surgery.</p></sec><sec id="s4"><title>4. Conclusion</title><p>Air flow in the nasal cavity is studied by means of a simple model resting on the stationary ideal fluid flow hy-</p><fig id="fig3"><label>Figure 3</label><caption><p> The derivative dΦ<sub>I</sub>/dS<sub>0</sub> represented as a fiunction of S<sub>0</sub> for ρ = 1.29 kg∙m<sup>−3</sup>, p<sub>a</sub> = 1.0 atm and for the follow- ing values of the parameter k (from top to bottom): 6, 7, 8, 9 N∙m∙s<sup>−1</sup>. The units of the derivative are purposely express- ed as “(mm<sup>3</sup>/s)/mm<sup>2</sup>” instead of “mm/s”</p></caption><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\1-8302325x\acca71bd-165c-4cde-99da-419dac537f98.png"/></fig><p>pothesis. Under these assumptions, Bernoulli’s equation can be used. The model might thus be used to give an elementary description of nose and sinus ventilation. Under these simplifying assumptions, the present analysis predicts that the flow rate of air sucked from the maxillary sinus towards the nasal cavity decreases as the area close to the ostiummeatal complex increases. 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