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J Appl Physiol 92: 455-460, 2002; doi:10.1152/japplphysiol.00643.2001
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Vol. 92, Issue 2, 455-460, February 2002

Empirical model for dynamic force-length behavior of airway smooth muscle

Ron C. Anafi and Theodore A. Wilson

Department of Aerospace Engineering and Mechanics, University of Minnesota, Minneapolis, Minnesota 55455


    ABSTRACT
TOP
ABSTRACT
INTRODUCTION
MODEL FOR MUSCLE DYNAMICS
RESULTS
DISCUSSION
REFERENCES

An empirical mathematical model that describes the relation between force and length for dynamic loading of maximally activated airway smooth muscle is described. The model consists of three first-order, ordinary differential equations: one for muscle shortening, one for lengthening, and a third that describes the evolution of an internal variable that depends on muscle history. The model fits data on the dynamic force-length behavior of maximally activated trachealis muscle for a range of amplitudes and rates of shortening and lengthening. The muscle model is incorporated into a model for an intact airway tethered to the surrounding parenchyma. As an example of its use, the model airway is subjected to the loading that occurs during a deep breath. After the breath, the rate of muscle shortening is determined by the interaction between muscle dynamics and the elastic load that is imposed by interdependence forces.

mechanics; lung constriction; asthma


    INTRODUCTION
TOP
ABSTRACT
INTRODUCTION
MODEL FOR MUSCLE DYNAMICS
RESULTS
DISCUSSION
REFERENCES

GUNST AND COLLEAGUES (3, 7, 14) have reported extensive data on the dynamic force (F)-length (L) behavior of maximally activated trachealis muscle. They imposed L oscillations with a range of amplitudes and frequencies and measured the F exerted by the muscle. These data show that the dynamic F-L curves of smooth muscle are quite different from the isometric F (Fiso)-L curve. The dynamic curves depend on amplitude and rate of change of muscle L.

During the last decade, mathematical models of constricted lungs have been proposed (2, 10). Although these models are intended to describe the mechanics of ventilated lungs, they use the Fiso-L curve to describe the behavior of smooth muscle. An empirical model of dynamic smooth muscle behavior would be useful in modeling dynamic airway and lung mechanics, and here we propose such a model. The model is not intended to describe the basic molecular processes that underlie the dynamic F-L curve. Instead, it is an entirely empirical model that is intended to be simple enough to be useful in modeling lung mechanics. The model consists of a set of three first-order, ordinary differential equations. The solutions to these equations match the main features of the data on dynamic F-L relations. This model for maximally activated smooth muscle is incorporated into a model for an airway in the lung, and, as an example of the use of the model, the recovery of airway constriction after a deep breath is analyzed.


    MODEL FOR MUSCLE DYNAMICS
TOP
ABSTRACT
INTRODUCTION
MODEL FOR MUSCLE DYNAMICS
RESULTS
DISCUSSION
REFERENCES

In formulating the model, we focused on the data of Shen et al. (14) shown in Fig. 1. In these experiments, Shen et al. oscillated the L of maximally activated trachealis muscle and measured the periodic F-L relation that was established after a number of cycles. The muscle was shortened at a constant rate and then returned to its original L, with a rate of lengthening equal to the rate of shortening. For the loops shown in Fig. 1A, the amplitudes of L oscillation are the same, but the rates of shortening and lengthening are different. The rates extend over a range of a factor of 80. For the loops shown in Fig. 1B, the rates of shortening are the same, but the amplitudes are different.


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Fig. 1.   Periodic force (F)-length (L) curves for maximally activated trachealis muscle for different frequencies (A) and different amplitudes (B). In all cases, maximum muscle L is 0.8 optimal length (Lo). Muscle F is nondimensionalized by the isometric force (Fiso) at maximum muscle L [Fiso(0.8 Lo)]. These curves are redrawn from data reported by Shen et al. (14).

We assume that measurements made at different muscle L values would be similar to the data shown in Fig. 1. That is, we assume that F at L scales with the Fiso at that L, and that F/Fiso depends on L as a fraction of optimal length (Lo). Thus, in terms of the dimensionless variables, l = L/Lo and f = F/Fiso, f(l) is assumed to be a universal function.

The model for the relation between f and l for the shortening limbs was guided by the following features of the data. As shown in Fig. 1B, the shortening limbs for muscle contracting at the same rate from the same initial F and L coincide, independent of the previous stretch amplitude. Thus the F-L behavior during shortening appears to be determined by the current F, L, and velocity of shortening, independent of history. As shown in Fig. 1A, the shortening limb for the fastest rate of shortening appears to be an exponential. The curves for slower rates peel off the curve for the fastest rate as if F were relaxing toward f = 1. In fact, plots of the slope of the descending limb (df/dl) vs. f are straight lines with different slopes for different rates of shortening and a common intersection at f = 1. The following equation was, therefore, chosen to describe the F-L relation for shortening
<A><AC>f</AC><AC>˙</AC></A>=k<SUB>1</SUB>f<A><AC>l</AC><AC>˙</AC></A>+a<SUB>1</SUB>(1−f) <A><AC>l</AC><AC>˙</AC></A><0 (1)
where k1 and a1 are constants, and &fdot; and &ldot; are time derivatives of f and l, respectively. The first term on the right side of Eq. 1 represents a nonlinear spring. The second term describes a relaxation process. That is, if &ldot; were zero, this term would cause f to approach the equilibrium value of 1 with a rate that is proportional to the difference between the value of f and its equilibrium value. The effect of the second term is more pronounced at slower rates of shortening.

The lengthening limbs shown in Fig. 1 are more complicated. Despite beginning at different F and L values, all return to about the same F at the peak muscle L (0.8 Lo). The F-L behavior is thus dependent on history, effectively remembering the peak L attained during the cycle. Plots of df/dl vs. f for these curves are straight lines, but the slopes and intercepts depend not only on the rate of lengthening, but also on the amplitude of the oscillation. To describe the lengthening limbs, we, therefore, chose an equation similar to Eq. 1 but with an additional variable that depends on the history of the maneuver, g. This equation contains additional constants: k2, k3, a2, a3, and c1
<A><AC>f</AC><AC>˙</AC></A>=(k<SUB>2</SUB>f+k<SUB>3</SUB>g)<A><AC>l</AC><AC>˙</AC></A>+a<SUB>2</SUB>(g−f)+a<SUB>3</SUB>{1−exp[<IT>c</IT><SUB>1</SUB>(<IT>f−</IT>1)]} (2)

<IT> <A><AC>l</AC><AC>˙</AC></A>≥</IT>0
The three terms on the right side of Eq. 2 describe, in order, a nonlinear spring, a relaxation toward g, and a slower relaxation toward the Fiso. The exponential in the last term limits f from rising far above the Fiso.

The variable g in Eq. 2 contains information about the history of the maneuver. This variable is governed by the following equation in which the a's and c2 are constants.
<A><AC>g</AC><AC>˙</AC></A>=a<SUB>4</SUB>(f−g)+a<SUB>5</SUB>g{1−exp[<IT>c</IT><SUB>2</SUB>(<IT>f−</IT>1)]} (3)
where ġ is the time derivative of g. The first term on the right side of Eq. 3 describes a relaxation of g toward f. The rate constant for this relaxation is relatively small, and this term drives g toward the average value of f for the cycle. The second term describes a more complicated effect of f on g: for f < 1, this term is positive, and for f > 1, it is negative and large. Thus, for cyclic oscillations, this term adjusts the value of g so that the peak value of f is slightly bigger than 1. In the isometric limit, this term ensures that g, and hence f, equals 1.

Eqs. 1-3 contain a total of 10 constants. By an extensive trial-and-error process, the following values of these constants were chosen: k1 = 28, k2 = 10, k3 = 12, a1 = 0.12 s-1, a2 = 0.16 s-1, a3 = 0.001 s-1, a4 = 0.001 s-1, a5 = 0.002 s-1, c1 = 22, and c2 = 20.

The solution to Eqs. 1-3 gives muscle F as a fraction of Fiso, and Fiso depends on muscle L. For muscle L < Lo, Fiso(l) is described by the following equation, where Fo is the Fiso at Lo
F<SUB>iso</SUB>(<IT>l</IT>)<IT>=</IT>F<SUB>o</SUB>[1.25(<IT>l</IT>)<IT>−</IT>0.25] (4)
To determine F, Eqs. 1-3 are solved for f, and f is multiplied by Fiso, as given by Eq. 4.


    RESULTS
TOP
ABSTRACT
INTRODUCTION
MODEL FOR MUSCLE DYNAMICS
RESULTS
DISCUSSION
REFERENCES

The curves F(l), calculated from Eqs. 1-4 for the same cyclic L maneuvers as those in Fig. 1, are shown in Fig. 2.


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Fig. 2.   Periodic F-L curves computed from the model for the same oscillation parameters as those for the data shown in Fig. 1. A: different frequencies; B: different amplitudes.

An additional comparison between data and model is shown in Fig. 3. The data are redrawn from the results reported by Fredberg et al. (1). Fredberg et al. measured cyclic F-L curves for maneuvers that differed from those used by Shen et al. (14). The L oscillations were sinusoidal rather than saw-tooth, and mean L rather than peak L was held constant for different amplitudes.


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Fig. 3.   A: F vs. L/Lo for sinusoidal L oscillation, redrawn from data reported by Fredberg et al. (1). B: F as a fraction of maximum Fiso at Lo (Fo) vs. L/Lo computed from the model for the same L oscillation parameters.

Airway model. A model for the constricted airway embedded in lung parenchyma was described by Gunst et al. (6), and others have used similar models (10, 11). In these models, the airway is pictured as consisting of a circumferential band of muscle surrounding a layer of incompressible tissue, as shown in Fig. 4. The adventitia is ignored, and the radius of the muscle is assumed to be the same as the outer radius of the airway. The maximum outer radius of the unconstricted airway, and hence, the maximum radius of the muscle, is denoted by the constant ro. The radius of the muscle in the constricted state is denoted rm, and the radius of the airway lumen is denoted rl. The rm and the rl, nondimensionalized by ro, are denoted rho m and rho l, respectively. We assume that the fraction of the area of the unconstricted airway occupied by tissue is 0.16 and that this area remains constant when the airway contracts. Thus rho <UP><SUB>m</SUB><SUP>2</SUP></UP> - rho <UP><SUB>l</SUB><SUP>2</SUP></UP> = 0.16, and the lumen is closed when rho m = 0.4. 


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Fig. 4.   Model of airway embedded in the parenchyma. The radius of the band of smooth muscle at the outer edge of the airway wall is denoted rm, and the airway lumen radius is denoted rl. Lumen pressure (Plumen) acts on the inner surface of the airway, and alveolar pressure (Palv) and parenchymal tethering stress (tau ) contribute to peribronchial pressure.

The equilibrium state of the airway is described by a balance between the hoop stress provided by the muscle, F/rm, and the transmural pressure imposed by the difference between lumen pressure (Plumen) acting on the inner surface of the airway and alveolar pressure (PA) and parenchymal tissue stress (tau ) acting on the outer surface
F<IT>/r</IT><SUB>m</SUB><IT>=</IT>P<SUB>lumen</SUB><IT>−</IT>P<SC>a</SC><IT>+&tgr;</IT> (5)
Tissue stress depends on PA and on the mismatch between rm and the radius of the undeformed hole in the uniformly expanded lung (rh) (6, 9, 10). The value of rh is assumed to change in proportion to the cube root of lung volume and to match airway radius at total lung capacity (TLC). Thus rh = ro v1/3, where v is lung volume as a fraction of TLC. The difference between rh and rm, nondimensionalized by rh, is denoted x
x=1−&rgr;<SUB>m</SUB>/v<SUP>1/3</SUP> (6)
We use Lai-Fook's description of the relation between tau  and PA and x (9)
&tgr;=P<SC>a</SC>(1<IT>+</IT>1.4<IT>x+</IT>2.1<IT>x</IT><SUP>2</SUP>) (7)
Finally, the relation between v and PA must be given. A linear relation with a residual volume of 20% TLC and a lung compliance of 4% TLC/cmH2O is assumed
v<IT>=</IT>0.2<IT>+</IT>0.04P<SC>a</SC> (8)
By substituting from Eq. 6 into Eq. 5 and introducing nondimensional variables, the following equation is obtained
(F<SUB>o</SUB><IT>/r</IT><SUB>o</SUB>)[F<IT>/</IT>F<SUB>iso</SUB>(<IT>l</IT>)][F<SUB>iso</SUB>(<IT>l</IT>)<IT>/</IT>F<SUB>o</SUB>]<IT>/&rgr;</IT><SUB>m</SUB> (9)

<IT>=</IT>P<SUB>lumen</SUB><IT>+</IT>P<SC>a</SC>(1.4<IT>x+</IT>2.1<IT>x</IT><SUP>2</SUP>)
The parameter Fo/ro describes the amount of muscle in the airway, and the value of this parameter is obtained from the data of Gunst et al. (4, 5): Fo/ro = 40 cmH2O.

The mechanics of the airway are described by Eqs. 6, 8, and 9. The model for the dynamic F-L relation for airway smooth muscle can be incorporated into this model. The variable f in the muscle model is the same as F/Fiso(l), and the relation between the L scales for the muscle and airway is fixed by assuming that Lo ro and, therefore, that l = rho m. Then, for Plumen and PA given as functions of time, the airway response is obtained from the simultaneous solution to Eqs. 1-4, 6, 8, and 9.

Example. As an example of an application of the model described above, we analyze the response of a constricted airway to a deep breath. Before the deep breath, the airway is assumed to be closed. In the closed state, rho l = 0, and the inner walls of the airway are in contact. The contact pressure provides a value of Plumen that is required to hold rho m at the value rho m = 0.4. It is assumed that the closed state has been held for sufficient time for F to relax to Fiso(0.4). Thus, in the initial state, the airway is closed and the F in the smooth muscle is the Fiso for rho m = 0.4.

The deep breath is modeled by increasing Plumen to the point where the airway begins to open. At that point, flow occurs, and PA equilibrates with Plumen. We begin the calculation at that point. That is, we assume that, during the deep breath, Plumen = PA and that both commence at the value that satisfies the equilibrium equations for the airway with rho m = 0.4 and F = Fiso. We assume that, during the deep breath, PA rises from its initial value to 15 cmH2O and then returns to a value for which the airway can close, namely 7 cmH2O. The assumed time history of PA is shown in Fig. 5.


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Fig. 5.   A: assumed form of the curve of PA vs. time during a deep breath. B: computed curve of F nondimensionalized by maximum Fiso Fo vs. muscle radius. The Fiso-L curve is shown by the dashed line. C: muscle radius vs. time. The lumen of the airway is closed at nondimensionalized muscle radius (rho m) = 0.4.

The simultaneous equations for muscle dynamics and airway mechanics were solved numerically to obtain the results shown in Fig. 5. In Fig. 5B, F/Fo is shown plotted against rho m, and in Fig. 5C, rho m is shown as a function of time.


    DISCUSSION
TOP
ABSTRACT
INTRODUCTION
MODEL FOR MUSCLE DYNAMICS
RESULTS
DISCUSSION
REFERENCES

We set out to generate an empirical model that describes the dynamic F-L behavior of airway smooth muscle and that could be used in models of airway dynamics. Our model, unlike other models of smooth muscle dynamics (8, 12, 16), is not based on concepts of molecular dynamics of smooth muscle contraction. Ours is a purely empirical model, and its form is simpler than the models based on molecular dynamics.

The model consists of three ordinary differential equations. The first describes the F-L curve for muscle shortening. It consists of a combination of a nonlinear spring and a linear relaxation toward the Fiso. This simple relation is remarkably effective at matching the data for muscle shortening for a wide range of rates of shortening.

The model for muscle lengthening is more complicated because it appears that the F developed during muscle lengthening is history dependent. An internal variable g that depends on muscle history appears in the equation for lengthening. The equation for lengthening includes a nonlinear spring with a spring constant that depends on both f and g and two relaxation terms, a relaxation of f toward g and a slower relaxation of f toward 1.

A separate equation governs the evolution of g. The first term in this equation describes a slow relaxation of g toward f. For cyclic L histories, this term drives g toward the average value of f. However, we found that the data could not be matched without including a second term in this equation. This term adjusts g slightly. For slow, large-amplitude oscillations, g is slightly lower than the average value of f, and, for faster, smaller amplitude oscillations, g is slightly bigger than the average value of f. We have no physical analog for this term, akin to a nonlinear spring or F relaxation; it simply provides an ad hoc method for adjusting the F-L loops so that peak F and Fiso coincide.

The model contains 10 constants. This is a large, but not unreasonable, number of constants for a system of three equations. No biochemical significance is ascribed to these constants, and our aim is not to obtain values of biochemical rates or affinities by fitting the model to a limited set of data. Our aim is to generate an empirical model that can be used in modeling the mechanics of constricted airways. Therefore, questions about the uncertainty of the parameter values are not pertinent.

The curves computed from the model and shown in Figs. 2 and 3 match the experimental data for oscillatory forcing with a range of frequencies and amplitudes reasonably well. We would like to point out two other qualitative comparisons between data on smooth muscle F-L relations and the model. First, energy dissipation during a cycle was measured by Shen et al. (14). They report that hysteresivity decreases with increasing frequency of oscillation. This implies that the primary dissipative mechanism is a relaxation mechanism rather than a viscous mechanism, and the dissipative mechanisms in the model are relaxation mechanisms. Second, the variable g in the model is an unobservable internal variable. However, its value would be displayed by certain L histories. If, during a cyclic oscillation, the shortening were stopped at the midpoint, Eq. 2 predicts that f would relax relatively rapidly toward g and then f and g would relax slowly toward 1. Conversely, if muscle lengthening were interrupted, Eq. 2 predicts that f would initially decrease as f relaxes toward g, and then the two would relax more slowly toward 1. Data for interrupted shortening reported by Gunst (3) show the first behavior, and recent data for the second maneuver (7) show the second behavior.

As an application of the model, the effect of a deep breath on airway constriction was analyzed. The L history of the muscle during this maneuver is different from the L histories for which direct experimental measurements have been made, and this example, therefore, illustrates the usefulness of the model. In the initial state, muscle F equals the Fiso. In the first phase of the maneuver, transmural pressure rises rapidly, the muscle is forced to lengthen, and F rises above Fiso. After the inspiration phase, PA remains constant, and F relaxes toward Fiso. As F decreases, rho m increases slightly. During the expiration phase, F drops rapidly, and muscle L and rho m decrease, but the decrease in rho m is small because the dynamic F-L curve for rapid shortening is steep. Muscle behavior during these two phases could be estimated from the data on F-L relations. After the expiration, PA remains constant as the airway closes. The value of the model lies in the prediction of the time course of muscle shortening during this phase of the maneuver. Eq. 1 is applicable during muscle shortening, and this equation together with the airway equations are solved for the two unknowns, f and l, as functions of time. The rate of recovery of f is affected both by muscle dynamics and by the stiffness of the load against which it shortens, just as the rate of relaxation of a viscoelastic element in series with a spring depends on both the time constant of the viscoelastic element and the spring constant. The time history of muscle F during shortening is peculiar. Although f recovers toward its equilibrium value of 1, the muscle shortens, and Fiso(l) decreases. As a result, F remains nearly constant. However, the hoop stress and the interdependence F both increase as r decreases and the airway closes.

The predicted time course of airway closure can be compared with data in the literature that describe the rise of lung impedance after a deep breath. Shinozuka et al. (15) measured the impedance of constricted dog lungs after a deep breath, and Pellegrino et al. (13) measured the recovery of impedance after a deep breath in bronchoconstricted human subjects. The time course of recovery of impedance was 20-30 s in both of these experiments. The time of recovery of airway closure obtained from the model and shown in Fig. 5C agrees with these data. If the mass of muscle in the airway were bigger or if airway and parenchyma were less tightly coupled, the deep breath would have less effect, and closure would occur more rapidly.


    ACKNOWLEDGEMENTS

This work was supported, in part, by a Whitaker Foundation Graduate Fellowship.


    FOOTNOTES

Address for reprint requests and other correspondence: T. A. Wilson, 107 Akerman Hall, 110 Union St. SE, Minneapolis, MN 55455 (E-mail: wilson{at}aem.umn.edu).

The costs of publication of this article were defrayed in part by the payment of page charges. The article must therefore be hereby marked "advertisement" in accordance with 18 U.S.C. Section 1734 solely to indicate this fact.

10.1152/japplphysiol.00643.2001

Received 25 June 2001; accepted in final form 24 September 2001.


    REFERENCES
TOP
ABSTRACT
INTRODUCTION
MODEL FOR MUSCLE DYNAMICS
RESULTS
DISCUSSION
REFERENCES

1.   Fredberg, JJ, Inouye D, Miller B, Nathan M, Jafari S, Raboudi SH, Bulter JP, and Shore SA. Airway smooth muscle, tidal stretches, and dynamically determined contractile states. Am J Respir Crit Care Med 156: 1752-1759, 1997[Abstract/Free Full Text].

2.   Gillis, HL, and Lutchen KR. Airway remodeling in asthma amplifies heterogeneities in smooth muscle shortening causing hyperresponsiveness. J Appl Physiol 86: 2001-2012, 1999[Abstract/Free Full Text].

3.   Gunst, SJ. Contractile force of canine airway smooth muscle during cyclical length changes. J Appl Physiol 55: 759-769, 1983[Abstract/Free Full Text].

4.   Gunst, SJ, and Stropp JQ. Pressure-volume and length-stress relationships in canine bronchi in vitro. J Appl Physiol 64: 2522-2531, 1988[Abstract/Free Full Text].

5.   Gunst, SJ, Stropp JQ, and Service J. Mechanical modulation of pressure-volume characteristics of contracted canine airways in vitro. J Appl Physiol 68: 2223-2229, 1990[Abstract/Free Full Text].

6.   Gunst, SJ, Warner DO, Wilson TA, and Hyatt RE. Parenchymal interdependence and airway response to methacholine in excised dog lobes. J Appl Physiol 65: 2490-2497, 1988[Abstract/Free Full Text].

7.   Gunst, SJ, and Wu MF. Selected contribution: Plasticity of airway smooth muscle stiffness and extensibility: role of length-adaptive mechanisms. J Appl Physiol 90: 741-749, 2001[Abstract/Free Full Text].

8.   Hai, CM, and Murphy RA. Cross-bridge phosphorylation and regulation of latch state in smooth muscle. Am J Physiol Cell Physiol 254: C99-C106, 1988[Abstract/Free Full Text].

9.   Lai-Fook, SJ. A continuum mechanics analysis of pulmonary vascular interdependence in isolated dog lobes. J Appl Physiol 46: 419-429, 1979[Abstract/Free Full Text].

10.   Lambert, RK, Wiggs BR, Kuwano K, Hogg JC, and Pare PD. Functional significance of increased airway smooth muscle in asthma and COPD. J Appl Physiol 74: 2771-2781, 1993[Abstract/Free Full Text].

11.   Macklem, PM. A theoretical analysis of the effect of airway smooth muscle load on airway narrowing. Am J Respir Crit Care Med 153: 83-89, 1996[Abstract].

12.   Mijailovich, SM, Butler JP, and Fredberg JJ. Perturbed equilibria of myosin binding in airway smooth muscle: bond-length distributions, mechanics, and ATP metabolism. Biophys J 79: 2667-2681, 2000[Abstract/Free Full Text].

13.   Pellegrino, R, Wilson O, Jenouri G, and Rodarte JR. Lung mechanics during induced bronchoconstriction. J Appl Physiol 81: 964-975, 1996[Abstract/Free Full Text].

14.   Shen, X, Wu MF, Tepper RS, and Gunst SJ. Mechanisms for the mechanical response of airway smooth muscle to length oscillations. J Appl Physiol 83: 731-738, 1997[Abstract/Free Full Text].

15.   Shinozuka, N, Lavoie J, Martin JP, and Bates JHT Effect of time-varying load on degree of bronchoconstriction in the dog. J Appl Physiol 85: 1464-1470, 1998[Abstract/Free Full Text].

16.   Yu, SN, Crago PE, and Chiel HJ. A nonisometric kinetic model for smooth muscle. Am J Physiol Cell Physiol 272: C1025-C1039, 1997[Abstract/Free Full Text].


J APPL PHYSIOL 92(2):455-460
8750-7587/02 $5.00 Copyright © 2002 the American Physiological Society



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