Vol. 91, Issue 1, 290-297, July 2001
Analysis of tracheal mechanics and applications
Ulrich
Holzhäuser and
Rodney K.
Lambert
Institute of Fundamental Sciences
Physics, Massey University,
Palmerston North, New Zealand 5331
 |
ABSTRACT |
We have
developed a mathematical model for a tracheal ring that consists of a
"horseshoe" of cartilage with its tips joined by a membrane. The
ring is subjected to a uniform transmural pressure (Ptm) difference.
The model was used to calculate the cross-sectional area (A)
of the trachea. Whereas the mechanics of the deformation of the
cartilage were analyzed using elastica theory, the posterior membrane
was treated as a simple membrane that is inextensible under changes in
Ptm. The membrane can be specified to be of any length less than
baseline and thus can represent a posterior membrane under tension. The
cartilage can have specifiable nonuniform unstressed curvature as well
as nonuniform bending stiffness. We have investigated the effect on the
tracheal A-Ptm curve of posterior membrane length and
tensile force in the membrane, cartilage shape and elasticity, and
localized weakening of the cartilage. The model predictions are in good
agreement with magnetic resonance imaging data from rabbit tracheas and
show that the shape of the horseshoe as well as the posterior membrane
force are important determinants of tracheal compliance.
tracheomalacia; saber-sheath trachea; chronic obstructive pulmonary
disease; airway resistance
 |
INTRODUCTION |
THE MAJOR
CONTRIBUTION TO expiratory resistance during quiet breathing
comes from the large central airways. Despite being the stiffest
airways of the bronchial tree, they nonetheless undergo significant
deformation at physiological pressures, and thus a coupling exists
between flow in the airway and the cross-sectional area of the airway.
An analysis of the interaction requires a knowledge of the
area-transmural pressure (A-Ptm) relationship of the airway
and how this changes with disease-induced alterations in tissue
properties, particularly the stiffness of the cartilage and, in the
trachea, the elasticity and muscular tone of the posterior membrane.
These considerations have relevance to chronic obstructive pulmonary
disease in which weakening of the wall structures of large airways has
been suggested (1). In addition, cartilage geometry and
elasticity appear to play roles in tracheomalacia (18,
19).
The trachea is an attractive airway for mechanical analysis because of
its reasonably regular and well-defined structure. However, only one
attempt at analyzing the mechanics of this airway has been published
(3). This study was limited by the available computer
power. There have been many roentgenographic, computerized tomography, and fiberoptic studies of tracheal behavior (e.g., Refs. 1, 5, 6, 18,
19), but few have produced A-Ptm data (e.g.,
Refs. 1, 19).
We have developed a model of tracheal mechanics using elastica theory.
This is the same theory that was used in analyzing the mechanics both
of a Starling resistor (4, 10, 16) and of folding of the
airway epithelial basement membrane (11) as well as in an
experimental study of tracheal cartilage elasticity (12).
Using this model, we have investigated the effect on the tracheal
A-Ptm curve of posterior membrane tension and length, cartilage shape and elasticity, and localized weakening of the cartilage. The model results show that unstressed cartilage geometry as
well as membrane tension are important determinants of tracheal compliance.
 |
MODEL |
Our conceptual model of the trachea consists of a
horseshoe-shaped cartilage "ring," a membrane containing smooth
muscle that joins the tips of the horseshoe [separation = membrane length (L) at Ptm = 0], and
intercartilage connective tissue as shown in Fig.
1. We chose a simple base case in which
the undeformed cartilage is a semicircle. The unstressed posterior
membrane is connected to the ends of this semicircle. The
cartilage-membrane system can be deformed in one of two ways. Either
the muscle shortens (L < LI, where LI
is the maximal, fully relaxed length of the posterior membrane) and
generates tension that forces the cartilage tips together and thus
deforms the cartilage, or Ptm causes the posterior membrane to
invaginate (Ptm < 0) into the lumen of the cartilage or to expand
out of the lumen (Ptm > 0). The invagination or expansion of the
posterior membrane can happen at any state of muscle shortening
(L
LI). We will ignore the
contribution of the intercartilage membrane in this analysis.

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Fig. 1.
Model tracheal cross sections under 4 conditions. The
thick curves indicate cartilage, and the thin lines indicate the
posterior membrane. L, length of the posterior membrane;
LI, maximal length; Ptm, transmural pressure
difference.
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|
The governing equations describing the deformation of the cartilage are
based on the physics of a shell and have already been presented several
times elsewhere (4, 10-12, 16). A brief derivation of
a form of the equations more general than published to date is given in
the APPENDIX for completeness. This analysis yields
Eq. 1, which is the normalized differential equation
describing the deformation of the cartilage;
is the angle the
cartilage makes with a reference direction, and subscript 0 indicates
the zero stress state. A prime indicates differentiation with respect to normalized arc length (
).
|
(1)
|
In developing the analysis, three issues had to be taken into
account. First, for maximal generality of the results, it is convenient
to work with normalized quantities. Thus, in Eq. 1, arc
length is normalized on the radius (R) of the initially
semicircular cartilage and q is the nondimensional pressure. A second
issue is the likely lack of uniformity in the mechanical and
geometrical properties of real cartilage. This is handled by the use of
a function f(
), which allows the
introduction of inhomogeneities through their effect on the flexural
rigidity (also known as bending stiffness) of the cartilage
(D). D is a measure of the stiffness of the
cartilage and depends on the cartilage Young modulus (E) and the
dimensions of the cartilage cross section. We assume that D
can vary along the length of the arc of the cartilage and express D as the product of a constant stiffness
(D0) and f(
), which is a
nondimensional function of arc length (Eq. 2)
|
(2)
|
f(
) is chosen such that it can take values only
between zero and one. Thus D0 is the maximal
value of the flexural rigidity. The pressure scale for q in Eq. 1 is then D0/wR3
(w is the width of the cartilage horseshoe).
A third issue is the effect of the unstressed cartilage shape on
tracheal compliance. It is uncommon for an unstressed cartilage horseshoe to be exactly semicircular (that is, to have constant
0). To accommodate this observation, we
allowed
0 to vary around the arc, as in a
previous study (12)
|
(3)
|
where C is the curvature at the midpoint of the
horseshoe, and B is related to how rapidly
0
changes with
. The posterior membrane is modeled as a membrane (as
opposed to a shell) penetrating into the lumen (q < 0) or
expanding out of the lumen (q > 0) (Fig. 1). Because it is a
membrane subjected to a uniform Ptm, its cross-section perpendicular to
the tracheal axis must be part of a circle. The radius and the
subtended angle of the circular segment bounded by the membrane can
then be calculated from geometry. L was assumed to be
constant regardless of the value of q. The entire A of the lumen is the area enclosed by the cartilage (AC)
plus (q > 0) or minus (q < 0) the area
(AM) of the circular segment bounded by the
membrane and the straight line joining the cartilage tips.
|
(4)
|
x and y are the nondimensional Cartesian
coordinates of a point on the cartilage horseshoe. The origin of this
coordinate system is the intersection of the cartilage and its axis of
symmetry (
= 0, Fig. 10). The subscript f
denotes the final coordinate; that is, the cartilage tip.
There is no known equation for
as a function of
that satisfies
Eq. 1. Therefore, numerical methods were used to obtain solutions (see APPENDIX).
 |
RESULTS |
Figure 2 shows calculated profiles
of the initially semicircular cartilage at several stages of
deformation, assuming a constant stiffness along the circumference of
the cartilage [f(
) = 1, Eq. 2]. Figure 2A shows the cartilage when the posterior
membrane is shortened to 50% of its maximal length
(LI) and q = 0, that is without any
pressure difference across the walls. Figure 2B shows the
effect of an external pressure field alone on tracheal collapse for
L = LI (the posterior membrane
is inextensible) at four values of q.

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Fig. 2.
Calculated tracheal cross sections. q, Nondimensional
Ptm. A: q is zero. Thin lines, zero tensile force in
posterior membrane; thick lines, posterior membrane shortened to 50%
of length at LI. B: L
remains at LI; 4 values of q (1, 0, 1, 2.5)
are shown.
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|
Whereas the most general presentation of results is achieved using q,
the presentation is more intelligible if dimensioned pressure is used.
Therefore, we chose to convert q to Ptm by calculating a representative
conversion factor. The normalization factor for the pressure difference
across the cartilage horseshoe is
D/wR3 where D = ECIA and EC is
the Young modulus for the cartilage and IA is
the second moment of area of the cross section. We approximated the
cross section as an ellipse. Thus IA = (
/4)ab3, where a and
b are the lengths of the semimajor and semiminor axes of the
ellipse, respectively. We used the following data for human tracheal
cartilage taken from Begis et al. (3): a = 1.8 mm, b = 0.8 mm, and R = 10 mm,
where R is the average radius of the trachea. We chose 10 MPa as a representative value for E (22). The conversion
is then
Thus, for simplicity, we will use Ptm = 20q cmH2O
to represent the case of human tracheal cartilage.
To investigate the effect of shortening of the posterior membrane on
tracheal mechanics, we computed the A-Ptm curves for the
initially semicircular cartilage for four lengths
LI. These are shown in Fig.
3. A0 is the area
at Ptm = 0. In Fig. 3A, the curves are normalized on
the area of the base case and thus give the relative sizes of the
airway lumens and compliances. In Fig. 3B, the curves are
normalized on their own value of A0, which enables comparison of the specific compliances. The A-Ptm
curves have been computed from Ptm = 20 cmH2O to the
value of Ptm (< 0) at which the posterior membrane touched the inner
wall of the cartilage. At this point, the boundary conditions on the
problem change, and it is not clear to us how to model the changed
conditions.

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Fig. 3.
Simulated human lumen area (A)-Ptm curves at 4 values of L. A: area normalized on area of base
case (L = LI, Ptm = 0).
B: area of each curve normalized on area at Ptm = 0 for
that curve's value of L.
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|
Because the length-tension relationship of the trachealis is unknown
under conditions of changing Ptm, we investigated the interrelationship
between membrane length, membrane tensile force, and pressure for the
deformation of an initially semicircular cartilage. The nondimensional
tensile force (T) in the posterior membrane was dimensioned using the
force conversion factor D/R2. With
the values from Begis et al. (3) given above, the
dimensioned membrane tensile force (F) is given by
0.072 N is the weight of 7.3 g. F was calculated as a
function of Ptm at four stages of shortening of the posterior membrane (Fig. 4A). These data have
been added to and replotted in Fig. 4B to show how F depends
on membrane length at constant Ptm for values of
L/LI
0.25. This value was chosen
as a lower limit because the muscle is unlikely to shorten further in
vivo (9).

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Fig. 4.
Relationship between Ptm and L and tensile
force (simulated human). A: membrane force as a function of
Ptm at 4 values of (constant) membrane length. B: membrane
force as a function of length at constant pressure difference. Ptm
measured in cmH2O.
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|
The importance of the A-Ptm curves lies in the fact that
they determine the resistance of the trachea as a function of Ptm. We
evaluated the expiratory flow resistance using the empirically derived
formula (23) used in other models of expiratory flow (15, 17) and normalized the results on the resistance of
our base case at Ptm = 0. The results are shown in Fig.
5 for the A-Ptm curves given
in Fig. 3.

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Fig. 5.
Tracheal resistance normalized on the resistance of the
base case (unstressed posterior membrane at 0 Ptm) at 4 values of
membrane length. Ptm scale is from human data. Raw, airway
resistance.
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|
Cartilage is unlikely to have uniform stiffness around its
circumference. To investigate this, we studied three cases of variable stiffness by choosing the periodic functions for
f(
) given below (Eqs. 5,
6, and 7). In these, the magnitude of the
stiffness is controlled by choosing a value for the parameter
between 0 and 1;
= 0 corresponds to constant stiffness.
Because the radius of the undeformed semicircular cartilage is used as
the length scale of the problem and the problem is solved over half the
cartilage length (the cartilage is assumed to be symmetrical),
takes values between 0 (at the line of symmetry) and
/2 at the
cartilage tip
|
(5)
|
|
(6)
|
|
(7)
|
Each function puts the point of maximum weakness in a different
location: Eq. 5 at the line of symmetry ("center"),
Eq. 6 halfway between the line of symmetry and the tip
("mid-arc"), and Eq. 7 at the tip. Results from these
investigations are presented in Fig. 6 in
which
was kept constant at a value of 0.5 and the unstressed
cartilage was semicircular.

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Fig. 6.
A-Ptm curves showing the effect of variable
bending stiffness (D) along the cartilage length (simulated
human). See text for details.
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|
We used Eq. 3 to study other profiles: curvature that is
constant but greater than that for a semicircle (B = 0, C = 1.5) and the cases of semicircular curvature at the
line of symmetry but the curvature increasing (B = 0.3, C = 1.0) or decreasing (B =
0.3,
C = 1.0) toward the cartilage tips (Fig.
7A). Deformations of the
profiles shown in Fig. 7A were computed with constant
D (
= 0 in Eqs. 5-7). A comparison
of the A-Ptm curves for L = LI is presented in Fig. 7B. The curves are self-normalized;
that is, A0 is the zero-pressure area for each
case.

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Fig. 7.
Effect of initial cartilage profiles on A-Ptm
curves (simulated human). A: cartilage profiles for 4 sets
of values of B and C. B:
A-Ptm curves corresponding to profiles in A. Area
of each curve normalized on own area at Ptm = 0.
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|
A-Ptm curves for rabbit tracheal cartilage rings obtained
using magnetic resonance imaging (MRI) were published several years ago
(14). These data are compared with our predictions in Fig. 8 in which the following values for
rabbit tracheal cartilage were used: EC = 10 MPa,
b = 0.25 mm, and R = 4 mm, which yield Ptm = 960q Pa or 10q cmH2O (approximately);
b is the length of the semiminor axis of the elliptical
cross section. The value of EC is the same as that used in
our calculations for human data for want of rabbit data, whereas the
values of b and R were estimated from the MRI
images.

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Fig. 8.
Comparison of rabbit model results with magnetic
resonance imaging (MRI) data from rabbit tracheas.
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|
Finally, we used the model to study the mechanics of two airway
pathologies: saber-sheath trachea (6) and lunate trachea (18). The results for these are given in Fig.
9 in which Fig. 9A shows the
profiles with both a relaxed posterior membrane and a membrane
shortened to 75% of its unstressed length. The relaxed semicircular
case is included for reference.

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Fig. 9.
Simulation of 2 tracheal disease conditions: lunate
trachea and saber sheath trachea (simulated human). A: model
cartilage profiles. Thick curve, base case (refer to Fig. 2); dotted
lines, lunate trachea; thin lines, saber sheath trachea. In all cases,
Ptm is zero, outer profile is with zero tension in posterior membrane,
and inner profile has membrane shortened to 75% of its unstressed
length. B: lumen A-Ptm curves. Lumen area is
normalized on that of the base case. Human pressure scale is used.
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|
 |
DISCUSSION |
We have developed an analysis of tracheal mechanics that yields
predictions of the A-Ptm characteristics of the tracheal
cartilage-posterior membrane system. We analyzed the trachea rather
than other cartilaginous airways because its well-defined geometry
permits the formulation of a relatively straightforward model. We
expect other cartilaginous airways to be more compliant and the
compliance to increase as the quantity of cartilage in the wall
decreases. Thus it should be possible to interpolate between the
A-Ptm curve of the trachea and those of the membranous
bronchioles for which models are starting to be formulated (13,
24).
We used a well-established analytical technique to develop the model.
The technique is valid for this situation of large displacement but
small strain and has been used successfully in the past to study the
mechanics of deformable tubes (4, 10, 11, 16) and
cartilage rings (12). The small strain requirement can be gauged by the thickness-to-radius ratio (t/R) of
the deformed structure. This is of the order of 0.1 for our model
cartilage ring. Whereas this does not strictly satisfy the required
smallness criterion (t/R
1), it leads
to the relatively small error of 3% in the predicted displacement of
the cartilage tips (12). We believe that this is
sufficiently small for the analysis to have reasonable quantitative
validity. This is borne out by the comparison with the MRI data (Fig.
8). Further validation would require us to use our rabbit model to
predict results under other conditions, for instance, after the trachea
had been challenged with a muscle agonist. We do not have access to
appropriate experimental results.
Our treatment of the posterior membrane as being inextensible is a
simplification. The membrane probably does change length with changes
in the pressure field, especially for Ptm < 0 (20), but the length changes will be dependent on the tone in the smooth muscle, its previous stress history, and the time course of the pressure change, since the tissue is viscoelastic. We have assumed that
the membrane inserts into the cartilage tips. This is a reasonable assumption for humans but is not valid for all species. In particular, rabbit posterior membrane inserts on the outside of the cartilage horseshoe away from the tips. However, the results in Fig. 8 suggest that this is not significant except, perhaps, at very negative values
of Ptm.
It is likely that the cartilage is inhomogeneous in both its elastic
and geometric properties. Whereas there is some experimental evidence
for this, the experiments did not quantify the inhomogeneity (12). Our attempt to simulate inhomogeneity (Fig. 6) by
making the stiffness of the cartilage change by 50% along the
circumference produced only a very modest change to the normalized
A-Ptm curves. A 50% decrease in stiffness could be
generated in many ways. Two examples are a 50% decrease in the Young
modulus of the cartilage or a 14% decrease in thickness. It appears
that the force in the posterior membrane (Fig. 3) and the shape of the
horseshoe (Fig. 7) are more important determinants of tracheal stiffness.
It is apparent that the MRI data match the theoretically predicted
compliance curve for a trachea in which the posterior membrane is
shortened to 50% of its tension-free length at zero Ptm (Fig. 8). That
the agreement is with a case that has a prestressed posterior membrane
is in accord with our (unpublished) observation that the mucosal
membrane in rabbits is in tension. It is also in accord with
observations of porcine and canine tracheas (8). The
predictions of the magnitude of the posterior membrane tensile force
(Fig. 4) are in accord with tracheal data from 20- to 25-kg mongrel dogs (7) and with bronchial data from adult humans
(9). The graphs show that, for positive Ptm, F increases
with Ptm, as one would expect; the trachea is being blown up like a
balloon. For negative Ptm, it is not quite as obvious what will happen. If the pressure difference were applied to the cartilage alone, the
membrane would become slack. However, the membrane must also support
the pressure difference and meet the boundary conditions even as its
radius of curvature changes. Thus there must be tensile force in the
membrane, but, as Fig. 4A shows, this force depends not only
on the pressure but also on the initial length of the membrane. For the
case with the shortest membrane (L = 25%
LI), F steadily reduces as the pressure
difference is increased, whereas the longer membranes all require
greater F (Fig. 4B). The case of constant F appears to be
between 25% and 50% LI.
Under normal conditions of quiet breathing, tracheal Ptm is positive
and the overall resistance of the total human airway system is low,
with the intrathoracic trachea accounting for ~20% of that
resistance. However, when the flow is elevated, as it is during
exertion and cough, tracheal Ptm can become negative with possibly
large increases in tracheal resistance. We used our model
A-Ptm curves to estimate the changes in tracheal resistance under changing Ptm (Fig. 5). It can be seen that the resistance of the
highly compliant base case increases very rapidly with increasingly
negative values of Ptm and exceeds the resistance of the less compliant
cases for Ptm less than
4 cmH2O. Resistance at negative
Ptm is reduced by a shortening of the posterior membrane but at the
cost of increased resistance when Ptm > 0.
Our ability to alter the cartilage profile (Fig. 7) showed that
unstressed cartilage shape is an important determinant of compliance.
In particular, it is apparent that greater separation of the cartilage
tips results in greater airway compliance. This led us to investigate
two documented pathological profiles: saber-sheath trachea and lunate
trachea (Fig. 9). The A-Ptm curves in Fig. 9B
illustrate the complex interaction between profile and F. The unstressed lunate trachea is life-threateningly compliant near Ptm = 0. However, some tension in the posterior membrane (L < LI) greatly stiffens the airway at the cost of
decreased area for Ptm > 0. The effect of F on the saber-sheath
trachea is almost entirely restricted to positive values of Ptm. This
shape is very stiff. The clinical implications are clear. Treatment of
saber-sheath trachea with bronchodilators will achieve very little
because the shape is so intrinsically stiff. On the other hand,
bronchodilator treatment of a lunate trachea in which there is some
trachealis tension and a weakened mucosal membrane would make the
trachea life-threateningly compliant.
 |
APPENDIX |
The analysis of tracheal cartilage deformation is based on
elastica theory as was the case in a previous study (12).
The main features of the analysis are as follows.
The free-body diagram for a small section of a ring of arc length
ds and constant width w is shown in Fig.
10. S is the shear force, M is the
bending moment, and
is the angle between the tangent to wall and
the x-axis, Ptm is the applied pressure difference (internal
pressure minus external pressure), and s is the arc length.
The requirements of static equilibrium lead to Eqs.
A1-A3
|
(A1)
|
|
(A2)
|
|
(A3)
|
Because the structure is statically indeterminate, a
constitutive relationship is also required. Equation A4 is
Winkler's development of Euler's constitutive equation
(2). It links the difference in curvature (
) between
the deformed (
= d
/ds) and the undeformed
(
0 = d
0/ds) states with
the bending moment M.
|
(A4)
|
D, the flexural rigidity of the ring, is
given by Eq. A5.
|
(A5)
|
E is the Young modulus of the ring material and
IA is a geometric factor that depends on the
shape of the cross-section of the ring. At least one experiment on the
flexibility of tracheal cartilage indicated that the cartilage's
flexural properties were not necessarily uniform around the
circumference nor was the cartilage of constant undeformed curvature
(12). The analysis of that experiment allowed for the
nonuniform initial curvature by making
0 depend on
s. In this analysis, we again made
0 depend
on s. D was also made to depend on s
to allow for nonuniform elastic properties and cross section (Eq. A6)
|
(A6)
|
By introducing the normalized arc length,
[
0(0)s], scaling Ptm
on its natural scale factor, and eliminating S, T, and M between
Eqs. A1 and A4, Eq. A7 is obtained for
the deformation of the ring in terms of
and
with q (q
R
wPtm/D0) as parameter. A prime in Eq. A7 indicates differentiation
with respect to
|
(A7)
|
The coordinates (x1,
y1) of any point of the ring can be calculated
using the integrals given in Eq. A8
|
(A8)
|
Whereas cartilage horseshoes are not necessarily
symmetric about the midline, it seemed to us that the effort of solving the asymmetric problem would not yield sufficient new information to
justify the extra cost in time and computational difficulty. Therefore,
we chose to solve the problem where the cartilage is symmetric about
the midline (Fig. 1).

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Fig. 10.
Free-body diagram for analyzing mechanics of deforming
cartilage horseshoe. The dashed curve represents part of the cartilage.
The short thick curve is a small section of the arc of the cartilage on
which the indicated forces and bending moments are acting. See text for
details of abbreviations.
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|
Four boundary conditions are required to solve Eq. A7.
Symmetry provides one of these; namely, S at the symmetry axis must be
zero. The other conditions can be elucidated by applying the conditions
of static equilibrium to the deformed cartilage as a whole. Deformation
is caused either by the trachealis muscle shortening and generating a
force, TM, or an external, uniform, pressure field, Ptm, is
applied.
|
(A9)
|
where TMx and TMy
are the x and y components of the normalized
tensile force generated by the contraction of the muscle,
T(0) is the normalized tensile force in the cartilage at
the midline (
= 0), and
x and
y are the forces generated by the external
pressure field. xf and yf
are the final coordinates of the cartilage at
=
f. The bending moment condition is given in
Eq. A10
|
(A10)
|
Mq is the bending moment caused by the pressure field.
Equation A7 had to be solved numerically.
This was done as follows. At
= 0,
and
" are zero.
Because the other two derivatives of
are unknown, initial guesses
were made as to their values and Eq. A7 integrated
numerically to the tip of the half-ring (
=
f)
using a Bulirsch-Stoer algorithm (21). At this point, the
boundary conditions given in Eqs. A9 and A10
apply. However, these conditions could not be used directly because
they contain the unknown force and bending moment applied by the
attached membrane. Therefore, the forces in the ring were evaluated and
equated to the force applied to the tip by the membrane.
Mx and My were
calculated from this. Because the membrane force must be tangential to
the membrane at the point of attachment and the membrane has the same
axis of symmetry as the cartilage, the curvature and thus the
L of the membrane could be calculated. In all of the results
presented here, the membrane was held at some specified constant
length. The difference between the computed and required lengths
(L
Lcomp) was calculated.
From these calculations, a cost function (CF) was evaluated
|
|
The guessed initial conditions were then varied to find the
values that minimized CF. Simulated annealing was used for the minimization (21). When a value of CF of
<10
3 had been achieved, the result was accepted as the
required solution.
 |
ACKNOWLEDGEMENTS |
This study was supported in part by the Palmerston North Medical
Research Foundation.
 |
FOOTNOTES |
Address for reprint requests and other correspondence:
R. K. Lambert, Institute of Fundamental Sciences-Physics, Massey
Univ., Palmerston North, New Zealand 5331 (E-mail:
R.Lambert{at}massey.ac.nz).
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.
Received 12 December 2000; accepted in final form 28 February 2001.
 |
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