<?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">OJMIP</journal-id><journal-title-group><journal-title>Open Journal of Molecular and Integrative Physiology</journal-title></journal-title-group><issn pub-type="epub">2162-2159</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/ojmip.2013.32009</article-id><article-id pub-id-type="publisher-id">OJMIP-31300</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></subj-group></article-categories><title-group><article-title>
 
 
  A new geometrical and mechanical relation in the respiratory system with airflow limitation—From the perspective of analytical respiratory mechanics
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>yongyob</surname><given-names>Min</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>Respiratory Division, Department of Internal Medicine, Itami City Hospital, Itami, Japan</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>in1007@poh.osaka-med.ac.jp</email></corresp></author-notes><pub-date pub-type="epub"><day>15</day><month>05</month><year>2013</year></pub-date><volume>03</volume><issue>02</issue><fpage>54</fpage><lpage>60</lpage><history><date date-type="received"><day>2</day>	<month>March</month>	<year>2013</year></date><date date-type="rev-recd"><day>6</day>	<month>April</month>	<year>2013</year>	</date><date date-type="accepted"><day>15</day>	<month>April</month>	<year>2013</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>
 
 
  Classic respiratory mechanics is a branch of vectorial mechanics, which aims to recognize all forces acting on the respiratory system. Another branch of mechanics, analytical mechanics, has been used for analyzing the motions of complicated systems with constraints through equilibrium among scalar quantities such as kinetic energy and potential energy. However, until now, there have not been any studies concerning about analytical respiratory mechanics. In this paper, the author has obtained two types of motion equations (linear and nonlinear) for the airflow limitation from formulation of the analytical respiratory mechanics. Reconstructed flow-volume trajectories of the linear equation revealed a new relationship among the slope of the linear portion of trajectory, the coefficient of the dissipation function and the coefficient of the potential function. Reconstructed trajectories of the nonlinear equation suggested that a curved flow-volume trajectory would be caused by the emergence of regional hypoventilated clusters with airtrapped lobules. In conclusion, analytical respiratory mechanics will provide the basis for analyzing the mechanical properties of the respiratory system con cerning pulmonary functional images made by newly developed technologies.
 
</p></abstract><kwd-group><kwd>Secondary Pulmonary Lobule; Analytical Mechanics; Airflow Limitation; Flow-Volume Trajectory; Regional Air-Trapping</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. INTRODUCTION</title><p>Since Newton laid the solid foundation of dynamics by formulating the laws of motion, the science of mechanics has developed along two main lines. One branch, which we shall call vectorial mechanics, starts directly from Newton’s laws of motion. It aims at recognizing all the forces acting on any given particle, its motion being uniquely determined by the known forces acting on it at every instant. The analysis and synthesis of forces and moments is thus the basic concern of vectorial mechanics [<xref ref-type="bibr" rid="scirp.31300-ref1">1</xref>]. Classic respiratory mechanics has been established as a branch of vectorial mechanics.</p><p>While in Newton’s mechanics the action of a force is measured by the momentum produced by that force, Liebniz advocated another quantity, kinetic energy, as the proper gauge for dynamical action of a force. Leibniz replaced the momentum of Newton with kinetic energy, and replaced the force of Newton with the work of force or the work function. Leibniz is the originator of the second branch of mechanics which usually called analytical mechanics, which bases the entire study of equilibrium and motion on two fundamental scalar quantities, kinetic energy and work function (this is frequently replaceable by the potential energy) [<xref ref-type="bibr" rid="scirp.31300-ref1">1</xref>]. The energy theorem, which states that the sum of kinetic and potential energies remains unchanged during the motion, yields only one equation.</p><p>We encounter problems of mechanics for which the work function is a function not only of the position of particles but also of the time. For such systems, the law of conservation of energy does not hold. Hamilton has introduced a new formulation of the principle of least action asserting that the actual motion realized in nature is that particular motion for which the action (the time-integral of the difference between the kinetic and potential energies) assumes its smallest value. In the case of mechanical systems composed of two or more particles, two or three fundamental scalars contain the complete dynamics of even the most complicated system, provided that they are used as the basis of a principle [<xref ref-type="bibr" rid="scirp.31300-ref1">1</xref>].</p><p>It has generally been accepted that the secondary pulmonary lobule (SPL) is a fundamental unit of lung structure and function [2,3]. A pulmonary lobe is composed of a large number of SPLs, which a single bronchial tree integrates to the whole lung as a complicated system. Recent rapid progress in new technologies concerning pulmonary functional images has displayed regional and temporal functional images of the lung in vivo, which should be recognized as the complicated system of a large number of SPLs [2-4]. Thus, it is now demanded that physiologists reconstruct analytical respiratory mechanics based on SPLs in place of the classical vectorial, which will help us to accurately understand new pulmonary functional images produced by new technologies.</p><p>In this paper the author has reconstructed flow-volume trajectories of the airflow limitation by using the method of analytical mechanics. Reconstructed trajectories have revealed a new relationship among mechanical properties of the respiratory system in airflow limitation, and suggested a close relationship between the shapes of flowvolume trajectories and the emerged regional air-trapping in the lung.</p></sec><sec id="s2"><title>2. ANALYTICAL RESPIRATORY MECHANICS</title><sec id="s2_1"><title>2.1. Volume Variable, V</title><p>From the viewpoint of the secondary pulmonary lobule (SPL), the terminal branch of the bronchial tree should be the lobular bronchiole because each SPL is supplied by a single lobular bronchiole of about 1 mm in diameter [2,3]. The lung is composed of a large number (N) of SPLs by integration of the single fractal bronchial tree [<xref ref-type="bibr" rid="scirp.31300-ref4">4</xref>]. Thus, the volume variable (V [L]) of a respiratory system is a function of lobular volume variables<img src="2-1360048\501efd9d-c7a9-4290-a1ac-09dcebb23025.jpg" />;<img src="2-1360048\3f9755ae-1adc-4691-bb49-8a141c996114.jpg" />. During breathing, the volume variable of the respiratory system makes a trajectory in the space of the lobular volume variables.</p></sec><sec id="s2_2"><title>2.2. Flow Variable, F</title><p>Air inflow or outflow of an SPL is supplied by a single corresponding lobular bronchiole, and during breathing one would be able to see a flow <img src="2-1360048\b0f87638-301b-4d9f-ba37-f8e6a7d52d12.jpg" /> in each lobular bronchiole. A spirometry system measures airflow F [L/sec] at the mouth of the subject. The variable F is defined as a function of lobular flow variables;<img src="2-1360048\8a49b0c9-9617-4ae0-8337-87d6c402b7a8.jpg" />.</p></sec><sec id="s2_3"><title>2.3. Energy Functions of Respiratory System in Motion</title><p>When an inertial quantity of mass (m<sub>j</sub>) was given to each lobule, the kinetic energy T was defined as follows,</p><disp-formula id="scirp.31300-formula51174"><label>(1)</label><graphic position="anchor" xlink:href="2-1360048\b583cc6b-c9f6-4737-8909-b75e5deb497d.jpg"  xlink:type="simple"/></disp-formula><p>When a work function <img src="2-1360048\c6d747d1-ed1e-4c7c-a0eb-7620ca1a4256.jpg" /> was given, the potential energy U was defined as the following,</p><p><img src="2-1360048\bf1773cf-d789-4c16-9a0f-59a58a030f2a.jpg" /><img src="2-1360048\7bf9865b-60f2-4292-b249-dfe969ac60ff.jpg" /> (2)</p><p>The respiratory system in motion is a dissipative system. After introduction of Rayleigh’s dissipation function, the dissipation of energy in the system was defined by the dissipation function D as follows,</p><disp-formula id="scirp.31300-formula51175"><label>(3)</label><graphic position="anchor" xlink:href="2-1360048\99f7b18e-c3da-4f0c-861c-89217d7435d1.jpg"  xlink:type="simple"/></disp-formula><p>The parameters <img src="2-1360048\35d1ef48-c213-40d6-ab8b-b552d6dd3e2b.jpg" /> indicate dissipation coefficients distributed to every flow variables of the system.</p></sec><sec id="s2_4"><title>2.4. Motion Equations of Respiratory System in Motion</title><p>The analytical mechanics is based on the principle of least action for actual motions of the system [<xref ref-type="bibr" rid="scirp.31300-ref1">1</xref>]. The characteristic quantity of action is the time-integral of the difference between the kinetic and potential energies<img src="2-1360048\7f760068-a2dd-4e3b-a5f2-f7fc35ada2f6.jpg" />. By use of the least action of <img src="2-1360048\59c10d77-81bc-427e-99cb-b81941a7b29b.jpg" /> and D, one obtained a set of motion equations for the respiratory system in motion as follows [<xref ref-type="bibr" rid="scirp.31300-ref1">1</xref>].</p><disp-formula id="scirp.31300-formula51176"><label>(4)</label><graphic position="anchor" xlink:href="2-1360048\87250625-de4d-4482-a4a4-1b4fe4ec9a62.jpg"  xlink:type="simple"/></disp-formula><p>where j is<img src="2-1360048\4242d40f-74e0-4c2e-a846-bfc9c8c2a3c3.jpg" />.</p></sec></sec><sec id="s3"><title>3. A MOTION EQUATION FOR THE RESPIRATORY SYSTEM IN A STATE OF AIRFLOW LIMITATION</title><sec id="s3_1"><title>3.1. Kinetic Energy, T(F)</title><p>The volume variable V is defined as a moving point in the space of<img src="2-1360048\c1c30988-8cec-44a7-bb48-789c31939355.jpg" />. During breathing, one would obtain a trajectory of the moving point in the space. According to Riemann geometry, the infinitesimal distance between two points on the trajectory or the line element <img src="2-1360048\688c9d32-863b-4c78-9c91-50553fc8aaec.jpg" /> was expressed by the following equation [<xref ref-type="bibr" rid="scirp.31300-ref1">1</xref>],<sup></sup></p><disp-formula id="scirp.31300-formula51177"><label>(5)</label><graphic position="anchor" xlink:href="2-1360048\75fe6081-68c5-4420-8182-1a1df8e38add.jpg"  xlink:type="simple"/></disp-formula><p>By use of Eqs.1 and 5, the kinetic energy T was defined as follows</p><disp-formula id="scirp.31300-formula51178"><label>(6)</label><graphic position="anchor" xlink:href="2-1360048\5899c93d-4be9-4446-a43a-218feba914ed.jpg"  xlink:type="simple"/></disp-formula><p>When <img src="2-1360048\ac2e4938-bdcd-4846-91da-5e356b35a628.jpg" />was measured as flow variable F by the spirometry system, the kinetic energy <img src="2-1360048\01bf326b-300a-48d7-9969-cb6266407d5e.jpg" /> was defined on the flow-volume plane by the following,</p><disp-formula id="scirp.31300-formula51179"><label>(7)</label><graphic position="anchor" xlink:href="2-1360048\e978c64f-a162-4dfb-9000-e475afe02ce8.jpg"  xlink:type="simple"/></disp-formula></sec><sec id="s3_2"><title>3.2. Potential Energy, U(V)</title><p>On the flow-volume plane, one can see two particular states of the respiratory system by use of geometrical patterns of flow-volume trajectories: a stable state of resting breathing or a critical state of airflow limitation (<xref ref-type="fig" rid="fig1">Figure 1</xref>). Geometrical patterns of the forced expiratory flow-volume (FEFV) trajectories around the point of forced end-expiration have suggested that the point of residual volume (RV) is a stable equilibrium point in terms of a dynamical system [<xref ref-type="bibr" rid="scirp.31300-ref5">5</xref>].<sup> </sup>Around the point of stable equilibrium, the potential function U(V) was expressed as the first approximation by the following,</p><disp-formula id="scirp.31300-formula51180"><label>(8)</label><graphic position="anchor" xlink:href="2-1360048\f28eb065-978d-4135-8787-27c7d26e7c47.jpg"  xlink:type="simple"/></disp-formula><p>where the volume variable V was measured from RV (thus, V is zero or a negative value), and the parameter ω is a potential coefficient of the respiratory system.</p></sec><sec id="s3_3"><title>3.3. Energy Dissipation, D(F)</title><p>It is well known that choked flows are independent from expiratory efforts of the subject [<xref ref-type="bibr" rid="scirp.31300-ref6">6</xref>]. Therefore, we adopted the assumption that distributed dissipation coefficients <img src="2-1360048\2bdd93b9-aa77-4cbb-9aac-ff9b2c206e41.jpg" />of Eq.3 would be fixed to a single value <img src="2-1360048\a48538e5-fa3e-4d8a-b7f7-fc1a9415dbcd.jpg" /> during the state of airflow-limitation [<xref ref-type="bibr" rid="scirp.31300-ref7">7</xref>] (<xref ref-type="fig" rid="fig2">Figure 2</xref>). The energy dissipation of the system in the state of airflow-limitation was defined by the dissipation function D(F),</p><disp-formula id="scirp.31300-formula51181"><label>(9)</label><graphic position="anchor" xlink:href="2-1360048\2f70e0c2-2baf-4b5b-806e-663dc02a2f86.jpg"  xlink:type="simple"/></disp-formula></sec><sec id="s3_4"><title>3.4. Motion Equations of Airflow Limitation</title><p>By use of Eqs.7-9, from Eq.4 we obtained the ordinary differential equations for the state of airflow limitation as follows,</p><disp-formula id="scirp.31300-formula51182"><label>(10a)</label><graphic position="anchor" xlink:href="2-1360048\b298564d-8f7d-41fd-a38a-4175c4c4c0de.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.31300-formula51183"><label>(10b)</label><graphic position="anchor" xlink:href="2-1360048\2f9f54ad-a731-4ab0-a573-eb213f98b98c.jpg"  xlink:type="simple"/></disp-formula></sec></sec><sec id="s4"><title>4. RECONSTRUCTED FLOW-VOLUME TRAJECTORIES OF AIRFLOW LIMITATION</title><sec id="s4_1"><title>4.1. Straight Patterns of Reconstructed Flow-Volume Trajectories</title><p>Reconstructed flow-volume trajectories from several initial values of V and F by numerical solutions of Eq. 10 with the midpoint method (see Appendix) were drawn in <xref ref-type="fig" rid="fig3">Figure 3</xref>(a). These reconstructed trajectories showed a common straight trajectory in their descending legs. The slope of straight trajectory <img src="2-1360048\eb70adc8-eb83-4e64-ae4a-f8909ff2234a.jpg" /> was dependent on parameters of <img src="2-1360048\42cafc3b-42e5-4354-86a7-cc1d4301dc43.jpg" /> and<img src="2-1360048\be6066d2-9c1a-4b36-b920-546a1c9caa89.jpg" />; the higher the parameter <img src="2-1360048\07fa0dcb-05e6-41d1-934a-2d237dd3d400.jpg" /> was or the lower the parameter <img src="2-1360048\6ef2aab1-3bd8-4340-9af5-f17878a53653.jpg" /> was, the flatter the trajectory became (Figures 4(a) and (b)).</p><p>The straight trajectory seemed to have the property of the descending leg of the maximal expiratory flowvolume (MEFV) curve. Theoretical analysis of the linear ordinary differential equations of Eq.10 has shown that the straight trajectory has a specified slope <img src="2-1360048\82c3122c-4947-4a3d-b3c9-3538563dea2b.jpg" /> which must satisfy the following equation, [<xref ref-type="bibr" rid="scirp.31300-ref5">5</xref>]</p><disp-formula id="scirp.31300-formula51184"><label>(11)</label><graphic position="anchor" xlink:href="2-1360048\31ee309a-242b-47d5-bb16-11c61be8f8d8.jpg"  xlink:type="simple"/></disp-formula><p>As the slope <img src="2-1360048\5a71f38d-4018-4df8-9ec9-021a6c15aaee.jpg" /> is a real number, the relation of <img src="2-1360048\b5148f1b-3038-46a5-af50-83608d62540e.jpg" /> is necessary.</p></sec><sec id="s4_2"><title>4.2. Curved Patterns of Reconstructed Flow-Volume Trajectories</title><p>Forced expiratory flow-volume (FEFV) curves often approach the point of RV as the tangent of the volume axis. This phenomenon always accompanies curving transformation of FEFV curves. Eq.10 always reproduced a straight trajectory, but never a curved one (Figures 4(a) and (b)). A curved trajectory was reproduced only when the potential function U(V) was defined by a higher approximation of U around the stable equilibrium point of zero as follows (Figures 3(b), 5(a) and (b)),</p><disp-formula id="scirp.31300-formula51185"><label>(12)</label><graphic position="anchor" xlink:href="2-1360048\eb5167e4-cad1-45ef-b5f4-83fc567d6cbe.jpg"  xlink:type="simple"/></disp-formula><p>Therefore, the motion equation for a curved MEFV trajectory approaching tangent to RV was obtained as follows,</p><disp-formula id="scirp.31300-formula51186"><label>(13)</label><graphic position="anchor" xlink:href="2-1360048\714dece6-c70a-4563-8523-9a4d4ec012e1.jpg"  xlink:type="simple"/></disp-formula></sec></sec><sec id="s5"><title>5. DISCUSSION</title><sec id="s5_1"><title>5.1. Vectorial Mechanics and Analytical Mechanics</title><p>Lanczos compared the difference between Newtonian mechanics (vectorial mechanics) and analytical mechanics [<xref ref-type="bibr" rid="scirp.31300-ref1">1</xref>], and summarized four principal viewpoints: 1) vectorial mechanics isolates the particle and considers it as an individual, but analytic mechanics considers the system as a whole; 2) vectorial mechanics constructs a separate acting force for each moving particle, but analytical mechanics considers one single function the work function (the potential function); 3) if strong forces maintain a definite relation between the coordinates of a system, and that relation is empirically given, the analytical treatment takes the given relation for granted, without requiring knowledge of the forces which maintain it; and 4) in the analytical method, the entire set of equations of motion can be developed from one unified principle of least action. In the case of free particles, i.e., particles whose motion is not restricted by given constraints, the two forms of description lead to equivalent</p><p>results. But for systems with constraints, the analytical treatment is simpler and more economical. The given constraints are taken into account in a natural way by letting the system move along all the tentative paths in harmony with them.</p><p>It is easy to obtain paths of motion of the respiratory system as flow-volume trajectories from a patient in standard clinical practices. Since the flow-volume trajectory is a path of motion, it is possible to recognize it as the actual one chosen by the principle of least action according to the analytical mechanics. The most important trajectory is the forced expiratory flow-volume curve, which suggests the existence of the critical condition of airflow limitation in the respiratory system (<xref ref-type="fig" rid="fig1">Figure 1</xref>(b)). Based on geometrical properties of maximal expiratory flow-volume (MEFV) curves two assumptions were adopted at the state of airflow-limitation: 1) according to dynamical patterns of FEFV trajectories, the potential function of U would be defined by either Eq.8 or Eq.12; 2) the distributed regional flow resistances or the regional dissipation coefficients would be fixed to a single value of the whole system according to the wave-speed theory [<xref ref-type="bibr" rid="scirp.31300-ref7">7</xref>]<sup> </sup>(<xref ref-type="fig" rid="fig2">Figure 2</xref>). Thus, the respiratory system during the airflow limitation would be completely described by two variables: the volume and the choked flow. However, the flow-volume trajectories of spontaneous breathing (<xref ref-type="fig" rid="fig1">Figure 1</xref>(a)) would not be described by the equations of two variables because more regional volume and flow variables would be necessary. In order to describe spontaneous breathing in terms of analytical mechanics, it should be necessary to evaluate the number of variables such as regional flows and volumes for each spontaneous motion. Recent advances are being made in technologies concerning the making of images of pulmonary regional function based on the lobular structures, and these advances are providing new information for insights on solving this problem.</p><p>Computational models previously published such as Lambert’s model [<xref ref-type="bibr" rid="scirp.31300-ref8">8</xref>] and Solway’s transistor model [<xref ref-type="bibr" rid="scirp.31300-ref9">9</xref>] were based on the mechanical property of the site of airflow limitation or the choke point. However, the location of the choke point at the condition of airflow-limitation has not been revealed yet, thus the mechanical property of the choke point is only a proposal assumption for adapting experimental data from MEFVC. In the case of the model proposed in this paper, it is not necessary to define the location and the property of the choke point, but the dynamical characterization of pulmonary system in the airflow-limitation is necessary through kinematic properties of flow-volume trajectories.</p></sec><sec id="s5_2"><title>5.2. Forced Expiratory Flow Rates at Low Lung Volumes and Hysteresis</title><p>Forced expiratory flow rates at low lung volumes often differ between maximal (i.e., initiated from total lung capacity) and partial (i.e., initiated from below total lung capacity) forced expiratory maneuvers because of the effects of a deep inhalation (DI) on expiratory flowvolume relationships. On average, healthy adults display slightly higher forced expiratory flow at a specified lung volume during a maximal expiratory maneuver than during a partial expiratory maneuver [<xref ref-type="bibr" rid="scirp.31300-ref10">10</xref>]. Lim et al. reported that asthmatic patients who went to a hospital for treatment of severe attacks were assessed for level of obstruction and the effects of deep inhalation (DI) on degree of obstruction at various stages of their treatment and after recovery over several days, and suggested that the more severe the obstruction was, the greater the constrictor effect of a DI would be [<xref ref-type="bibr" rid="scirp.31300-ref11">11</xref>]. According to our results of Eq.11, the ratio of maximal and partial forced expiratory flows was transformed to the ratio<img src="2-1360048\88196fa3-b448-4aeb-8f6f-a42c18dcb5b4.jpg" />, where <img src="2-1360048\27aab368-6fc9-4c8d-883e-55065f8439c7.jpg" /> and <img src="2-1360048\6d5d2eae-f62b-4929-8f9d-ab693ada8bba.jpg" /> were the slope of the MEFV curve at partial and maximal forced expiratory maneuvers, respectively. Then, the relationship of <img src="2-1360048\7d8156c6-47a0-4d9b-a0e1-7aff42fc4408.jpg" />is expressed between mechanical properties approximately by the following equation when <img src="2-1360048\f33ff6c6-61fe-4cea-bc96-b2e1e7a6e9da.jpg" />and<img src="2-1360048\604bf98e-1318-4d20-8f5f-b5617bbe2ff4.jpg" />,</p><disp-formula id="scirp.31300-formula51187"><label>(14)</label><graphic position="anchor" xlink:href="2-1360048\3bb0d330-04ca-4d04-85e1-ac9adb49fb63.jpg"  xlink:type="simple"/></disp-formula><p>Eq.14 has shown that the difference of expiratory flows in the specified lung volume during a maximal maneuver and a partial maneuver was explained as the difference in the ratio of the dissipation coefficient to potential coefficient in a respiratory system composed of many lobules. Venegas et al. showed the hypoventilated lobular clusters emerging in asthmatics having an attack by use of reconstructed images of PET-CT [<xref ref-type="bibr" rid="scirp.31300-ref12">12</xref>]. Thus, the hysteresis or the dependency with volume history of the respiratory system should be explained in terms of emerged patterns in hypoventilated lobular clusters in the lung, and the mechanical properties of the respiratory system should be also explained in terms of relationships with the pattern of hypoventilated lobular clusters.</p></sec><sec id="s5_3"><title>5.3. Curved Maximal Expiratory Flow-Volume Curves and Regional Air-trapping</title><p>The transforming of a straight MEFV trajectory to a curved one has been recognized clinically as an indicator to detect early stages of chronic obstructive pulmonary disease (COPD) or small airways disease [<xref ref-type="bibr" rid="scirp.31300-ref13">13</xref>]. Expiratory air trapping on high resolution CT images was never observed in the 10 healthy subjects, but was observed in 21 (72%) of 29 patients with predominantly small airways obstruction (abnormal flow-volume curve and FEV1: vital capacity &gt; or = 80%) [<xref ref-type="bibr" rid="scirp.31300-ref14">14</xref>]. According to reconstructed flow-volume trajectories in this study, this transforming of the MEFV curve was caused by transformation of the potential function U and was independent from the dissipation coefficient or the respiratory resistance (Figures 5(a) and (b)). By use of Eq.12, driving pressure P of the respiratory system in the airflow-limitation is expressed as<img src="2-1360048\ecf6b92f-5997-4e1e-94ff-cc425672fb4f.jpg" />, which shows that driving pressure P would decline rapidly during the end of expiration (<xref ref-type="fig" rid="fig5">Figure 5</xref>(c)). Mead et al. revealed that the pressure P was equal to the elastic recoil pressure of the lung [<xref ref-type="bibr" rid="scirp.31300-ref15">15</xref>]. When the regional airtrappings would appear extensively as clusters of lobules in the lung, the elastic recoil pressure would decline rapidly. When the regional air-trappings would appear extensively as clusters of lobules in the lung, the elastic recoil pressure would decline rapidly. Therefore, the curve transformation of flow-volume trajectory should be analyzed in relation to regional clusters of air-trapped lobules emerged in the lung.</p></sec></sec><sec id="s6"><title>6. CONCLUSION</title><p>In this paper, the author has proposed the formulation of analytical respiratory mechanics applied to the system of secondary pulmonary lobules, which are integrated by a fractal bronchial tree. Based on analytical respiratory mechanics, two types of motion equations (linear and nonlinear) were obtained for describing the airflow limitation. Reconstructed flow-volume trajectories from the linear equation have shown a new relationship between geometrical and mechanical properties of the respiratory system with airflow-limitation. Reconstructed curved flow-volume trajectories from the nonlinear equation have suggested the possibility to detect the degree of air-trapped regional clusters of lobules through a change in the shape of the MEFV curve. In conclusion, analytical respiratory mechanics will provide the basis for transforming previous functional data into newly emerging functional images.</p></sec><sec id="s7"><title>REFERENCES</title></sec><sec id="s8"><title>APPENDIX</title><p>In numerical analysis, a branch of applied mathematics, the midpoint method is a one-step method for numerically solving the differential equation. When a differrential equation <img src="2-1360048\dc1eebe1-9c82-419e-b75a-f0074c48f8d2.jpg" />is given with initial values V<sub>0</sub> and F<sub>0</sub>,</p><p><img src="2-1360048\ca00fa23-b058-45d2-a322-6d1af0faacec.jpg" /></p><p><img src="2-1360048\d9368aab-eb14-4704-965a-4e5ab8249ebd.jpg" /></p><p>for n=1, 2, 3, ...&#160;and, h is the step size—a small positive number (h = 0.01). For reconstruction of flow-volume trajectories, the function of f is defined as follows,</p><p><img src="2-1360048\700e77a3-7ef2-4934-947f-1f47fbc44909.jpg" /></p><p>for Eq.10.</p><p><img src="2-1360048\05b93c9b-6207-4434-8f28-0d959a6ec633.jpg" /><img src="2-1360048\6591117e-50b7-4ff0-bd24-7dbbb233eb7a.jpg" /></p><p>for Eq.13.</p><p>Several sets of initial values were given as (V<sub>0</sub>,F<sub>0</sub>) = (−3,0), (−2,0), (−1.5,0), (−1,0), (−2,2.5), (−1.5,2), (−1, 1.5). The name of the method comes from the fact that in the formula above, the function f is evaluated at V = V<sub>n</sub> + h/2 which is the midpoint between V<sub>n</sub> at which the value of F is known and V<sub>n</sub><sub>+1</sub> at which the value of F needs to be found. The local error at each step of the midpoint method is of order O(h<sup>3</sup>), giving a global error of order O(h<sup>2</sup>). Several series of values (V<sub>n</sub>,F<sub>n</sub>) were obtained by using Excel 2007 in accordance with the midpoint method under the given sets of mechanical parameters γ, ω. These series of values were plotted on the flow-volume plane as shown in Figures 3-5.</p></sec></body><back><ref-list><title>References</title><ref id="scirp.31300-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Lanczos, C. 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