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Department of Aerospace Engineering and Mechanics, University of Minnesota, Minneapolis, Minnesota 55455
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ABSTRACT |
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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
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INTRODUCTION |
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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.
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MODEL FOR MUSCLE DYNAMICS |
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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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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
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(1) |



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
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(2) |
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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.
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(3) |

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
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(4) |
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RESULTS |
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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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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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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
m and
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 



m = 0.4.
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) acting on the outer surface
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(5) |
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(6) |
and
PA and x (9)
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(7) |
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(8) |
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(9) |
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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,
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
m at the value
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
m = 0.4.
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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m, and in Fig. 5C,
m is shown
as a function of time.
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DISCUSSION |
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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,
m increases slightly. During the expiration phase, F drops rapidly, and muscle L and
m decrease, but the decrease in
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.
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ACKNOWLEDGEMENTS |
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This work was supported, in part, by a Whitaker Foundation Graduate Fellowship.
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FOOTNOTES |
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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.
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