I
Assessment of distributed arterial
network models
P. Segers 1
N. Stergiopuios 2
P. Verdonck 1
R. Verhoeven 1
1Hydraulics Laboratory, IBrrECH, University of Gent, Sint-Pietersnieuwstraat 41,
B-9000 Gent, Belgium
2Biomedical Engineering Laboratory, EPFL, Swiss Federal Institute of Technology, Lausanne,
PSE-Ecublens, 1015 Lausanne, Switzerland
AbstractmThe aim of this study is to evaluate the relative importance of elastic nonlinearities, viscoelasticity and resistance vessel modelling on arterial pressure and flow
wave contours computed with distributed arterial network models. The computational
resu/ts of a non-linear (time-domain) and a linear (frequency-domain) mode were compared using the same geometrical configuration and identical upstream and downstream
boundary conditions and mechanical properties. Pressures were computed at the ascending aorta, brachial and femoral artery. In spite of the identical problem definition,
computational differences were found in input impedance modulus (max. 15--20%),
systolic pressure (max. 5%) and pulse pressure (max. 10%). For the brachial artery,
the ratio of pulse pressure to aortic pulse pressure was practically identical for both
models (3%), whereas for the femoral artery higher values are found for the linear model
(+10%). The aortic/brachial pressure transfer function indicates that pressure harmonic
ampl/f/cation is somewhat higher in the linear model for frequencies lower than 6 Hz while
the opposite is true for higher frequencies. These computational disparities were attributed
to conceptual model differences, such as the treatment of geometric tapering, rather than
to elastic or convective non-linearities. Compared to the effect of viscoelasticity, the
discrepancy between the linear and non-linear model is of the same importance. At
peripheral locations, the correct representation of terminal impedance outweights the
computational differences between the linear and non-linear models.
Keywords--Arterial network model, Linear, Non-linear, Viscoelasticity
J
Med. Biol. Eng. Comput., 1997, 35, 729-736
1 Introduction
NETWORKMODELSof the arterial circulation range from early
electrical analogue (WESTERHOF et aL, 1969) to computer
models, eventually incorporating non-linearities and complex
boundary conditions (SNYDERe t aL, 1968; SCHAm and
ABBRECHT, 1972; WEMPLE and MOCKROS, 1972; AVOLIO,
1980; STERGIOPULOSet al., 1992; KRUS et al., 1991; SHENGet
al., I995). The computational results of these models are
similar: the intmt impedance of each of the models is equivalent to that measured in vivo (MILLS et al., 1970; MURGO et
aL, 1980), and each model computes the propagation of
pressure and flow waves along the arterial tree, mimicking
observed wave phenomena such as the systolic presmare rise,
diastolic pressure decay, wave attenuation and wave reflection.
Differences exist in the way boundary conditions are
treated, in the computational procedure and in the modelling
of non-linearities. The upstream boundary condition can be a
pressure or flow wave measured downstream of the aortic
valve (WEMPLEand MOCKROS, 1972; AVOLIO, 1980; STERGIOPULOSet al., 1992; SHF-NGet al., 1995); the cardiovascular
interaction may be modelled as well (SNYDERet al., 1968;
Correspondenceshould be addressedto Dr Patrick Segers;
emaiJ: Patrick.Segers@rug.ac.be
First received 18 December 1995and in final form 21 March 1997
IFMBE:1997
Medical & Biological Engineering & Computing
SCHAAF and ABBRECHT,1972; KRUS et al., 1991). Downstream, the arterioles and capillaries are modelled as simple
resistances (SCHAAF and ABBRECH'r, 1972; AVOLIO, 1980;
KRUS et al., 1991), or more complex impedance models
(SNYDER et al., 1968; WEMPLE and MOCKROS, 1972; STERGtOVULOSet al., 1992; S~mN6 et aL, 1995).
From a computational point of view, two approaches exist.
First, the imegral form of the continuity equation and the
momentum equations may be solved, complemented with an
expression for the pressure-area relationship and an expression for the shear stress. The computation is performed in the
time domain via an appropriate numerical technique (SNYDER
et aL, 1968; SCHAAF and ABBRECHT, 1972; WEMPLE and
MOCKROS, 1972; STERGIOPULOSet al., 1992; KRUS, et aL,
1991). This method enables the incorporation of a non-linear
pressure-area relation and the non-linear convective terms of
the Navier--Stokes equations. Secondly, based on the electrical
analogy and the Womersley theory, it is possible to treat the
arterial tree as a transmission line, consisting of line segments
over which the propagation of individual pressure and flow
harmonics can be computed (AVOLIO, 1980). Assuming linearity of the system, superposition of the different harmonics
yields the propagated pressure and flow waves. The computation is performed in the frequency domain and enables a direct
incorporation of viscoelasticity and a frequency-dependent
shear function.
Both approaches co-exist, but it is still not clear whether
non-linearities are important in human arterial circulation.
November 1997
729
Whereas the role of the convective acceleration terms is
thought to be small (SCHAAP and ABBP.ECWr, 1972; WEMPLE
and MOCKROS, 1972; REUDERINKet aL, 1989), the impact of
the non-linear vessel pressure-diameter relation is expected to
be more important. Nevertheless, based on experimental latex
tube studies, it has been suggested that 'even in cases where
non-linear effects are signifieamly present, it is better to use a
linear 1D model that includes a satisfactory description of the
fluid friction and the viscoelastic wall behaviour than a nonlinear 1D model in which these damping effects are strongly
underestimated' (REuDERIrO: et al., 1989).
Arterial network models axe becoming increasingly
common for applications such as the validation of compliance
estimation techniques (STERGIOI'ULOS et al., 1995), wave
reflection analysis (KARAMANOGLUer aL, 1994) or to provide
boundary conditions for more detailed numerical flow studies
(REUDER1NK et aL, 1993), replacing the human body as the
object of study. Thus it is important to know which physical
properties and quantities are essential to guarantee physiologically relevant results. In this study we evaluate the importance of i) elastic non-linearities, ii) viscoelasticity and iii)
boundary conditions.
2 Materials and methods
We compare the computational results of a linear and a nonlinear (STERG1OPULOSet aL I992) arterial network model. The
linear model is further used for the implementation of different
viscoelastic models and for the evaluation of the impact of the
terminal impedance model on pressure and flow wave morphology.
2.1 Non-linear arterial network model
An extensive description of this model is found in (STER-
GIOPULOSet al., 1992)..The model allows the computation of
pressure and flow wave propagation over the arterial tree. The
computations involve numerical integration of the continuity
and momentum equations, together with an expression for the
wall shear stress (YOUNG and TSAt, 1973) and the pressm-ediameter (or pressure-area) relation of the arteries. The
computations are performed in the time domain. Arterial
distensibility and compliance are non-linearly depeaxdent on
pressure (LANGEWOUTERSet al., 1984); this non-linear relation is expressed (STERGIOPUIs et al., 1994) as:
- - =
~
3P
~P loo=~ar~
(
(1)
a-t
1+
where A is the vessel cross-section, P is the pressure, a
and b are constants (taken as 0.4 and 5, respectively),
Pa = 2 0 m m Hg and Pb = 30trmaHg, and ('~'x~
\or/
is the
2.2 Linear arterial network model
The computational procedure for calculating pressure and
flow in the linear transmission line model used here is similar
to (AVOLIO, 1980). The computations are carried out in the
frequency domain. Pressure and flow are written as the sum of
a steady component (Poiseuille flow), on which sinusoidal
harmonics are superimposed. The computational procedure is
based on the theory of oscillatory flow (individual
harmonics) in uniform, longitudinally tethered elastic tubes
(WOMERSLEY, t957). The tapering arteries are modelled as a
sequence of cylindrical segments, with stepwise varying segment properties.
Each segment is modelled as a transmission line element
(Fig. 2) for which the following equations apply:
1110 m m H g
reference area compliance at 100 ram Hg. The arterial network
configuration of (STERGIOPULOSet al., 1992) consists of 55
arterial network segments (Fig. 1). More specifications about
the dimensions and configuration of the arteries, the terminating 3-element 'windkessel' models (representing the smallsized arteries, arterioles and capillaries) and the pressure-area
relation for the different vessels are found in (STERGIOPULO$
et aL, 1992).
730
Fig. 1 Geometrical configuration used for the comparison of the
linear and non-linear models of the arterial circulation. The
segments correspond to the non-linear model. The
computational results are compared at segment 3
(oacending aorta, 4cm), 7 (brachial artery, 44cm) and
50 (femoral artery, 80 cm)
1
(2)
where P is the pressure, Q the flow, 7 the complex wave
number, L the vessel segment length, Z0 the characteristic
impedance of the vessel segment and the indices are 1 for the
Medical & Biological Engineering & Computing
November 1997
tax
(
2.0 ":
rdx
~
I.
"
L~
!
~.a"
q-
~
Fig. 2 Schematic representation of an infinitesimal transmission
L6"
L4
- -
line model segment of length dx. r = resistance,
e = compliance and 1= inertance (all properties per unit
of length)
1,0 V
0
upstream and 2 for the downstream site. The characteristic
impedance of the line segment is given as
r•+-jcol
zo=V
|
1
I
2
|
3
I
4
I
5
I
6
I
7
I
8
I
9
I
10
frequency, Hz
(3)
14
12 I
with
9~ i '%e
........
AA
Pet2 sin(e'10),l = ~ c o s ( e ' 1 0 ) ,
r ---- rcg4Mi ~
7tK'MIO
o
d
2nR 3
c ----E(co)ph
the transmission line parameters representing resistance,
inertianee and compliance per unit of length dx. /z is the
dynamic blood viscosity (4.5mPa's), p the blood density
(I 050 kg m-~), R the vessel segment radius at mean pressure,
h the thickness a~ the angular frequency, E(co)p the complex
dynamic elasticity modulus (a function of co and mean
pressure), j the complex constant ~
and M~0 and e'10
complex functions of ~ the Womersley parameter (r~,VOMERSLEY, 1957). With known segment properties, one can calculate
the input impedance for each frequency and each location of
the arterial network in a retrograde computation, starting from
the downstream end of the peripheral segment where the
impedance is known. In a forward computation, the propagation of an individual harmonic, starting from the upstream
inlet boundary condition (either pressure or flow) is determined. Summation of all harmonics and the steady flow
component leads to the reconstruction of the propagating
pressure and flow wave.
The non-linear relation between instantaneous pressure and
elasticity modulus is difficult to implement since it is the
propagation of individual harmonics that is studied and so the
instantaneous pressure (sum of all harmonics) is unknown.
Nevertheless, AC and DC computations are uncoupled, and
since mean pressure is known at all locations, one can easily
account for a non-linear relation between the elastic (frequency-dependent) properties and mean medal pressure.
In analogy with STERO[OPULOSet al. (1995), this relation is
expressed as eqn. 2:
g(co)100ramus
E(co)p =
(4)
b
a-I
where E(co)1O0m~ns is Young's modulus measured at the
reference pressure of 100mmHg as a function of co; a and b
are constants taken as 0.4 and 5, and Po = 20mm Hg and
Pb = 30 mm Hg. The computational procedure thus starts with
the determination of mean arterial pressure (0 I-Iz harmonic,
independent of compliance) and the computation of Ep(co).
Computation in the frequency domain allows the incorporation of viscoelasticity into the model (AVOLIO, 1980),
which can be expressed as a complex, frequency-dependent
elasticity modulus ~ERGEL, 1960) with a modulus and a
phase angle (HARDUNG, 1953; BERGEL, 1960; LEAROYDand
TAYLOR, 1966). Fig. 3 (upper panel) gives the ratio of
Medical & Biological Engineering & Computing
10
~A
A~
e~
6~
A
4-2-o
0
~
I--i"q-
1
2
3
4
I'
5
lrequermy,
I
6
Hz
I
7
I
8
I
9
I
10
Fig. 3 Modulus (upper panel) and phase (lower panel) representation of theoretical viscoelastic models of ('[.ANGEWOUTERS e t
al., 1985; WESTXRttOFet al., 1970; WESSSLINGet al.. 1973:
HOLENSTEIN et al., 1980." th ao---thoracal aorta; abd ao:
abdominal aorta; other art: other arteries; (o): old subjects;
9 Westerhof- no; C' Langewouters- th ao (o); A Wesselingth ao (o); - - Holenstein; 9 Westerhof- other art," 9 Langewouters- abd ao (o); 9 W~seting- abd ao (0)
E(co)to0m~ ng/E(0)100 ~ rig for viscoelastic models proposed
by different authors (WES'rEP,HOF and NOORDEGRAAF, 1970;
WESSELLING et aL, 1973; HOLENSTEINet aL, 1980; LANGEWOUTERS et aL, 1985) where E(0)10omaas is the static
Young's modulus at 100mmHg. In general, the modulus
IE(co)t0omagl increases with frequency. For the aorta, Langewouters, Holeustein and Westerhof give a dynamic modulus
10 to 20% higher than its static value; Wesseling gives values
50 to 60% higher. The dynamic modulus increases for the
distal arteries. Because of viscoelasticity, there is a phase lag
between the pressure wave and the vessel wall movement,
given by the complex E-modulus phase angle (Fig. 3, lower
panel). Langewouters reports a negligible phase lag; the other
authors report values between 5e (Westerhof; aorta) and
12~
other arteries). The viscoelastic models of
Westerhof and Holenstein are incorporated in the linear network model and the impact on pressure wave propagation is
studied. For the Westerhof model, there is a distinction
between the aorta and the other arteries; the
Holenstein model is applied on all vessels.
2.3 Geometrical data and boundary condition
The geometrical data-set of STERGIOPULOSet al. (1992) was
used for the comparative study (Fig. 1). The sum of the
compliance of the vessel segments at 100mmHg is
1.23 mlmmHg -~. The distal impedances, modelled as 3element 'windkessels,' add a constant compliance of 0.24
mlmmHg -~, so that the total compliance at 100mmHg is
N o v e m b e r 1997
731
1.47 ml mm Hg-~. The dam,set is determined for a 'reference
person" of 75 kg and 1.75 m tall; the compliance normalised
for body surface area is 0 ' 7 7 m l m m H g - ~ m -2. In the nonlinear model, geometrical tapering is automatically accounted
for in the segmentation process, whilst for the linear model
tapering is modelled as a sequence of cylindrical tubes.
For the non-linear model, 55 arterial segments cover the
arterial tree. For the linear model, a further segnaentation
results in a total of 156 different segments. An artery in the
linear model therefore consists of multiple segments. The
upstream and downstream artery diameters are matched. The
sum of the segment volumes equals the volume of the artery in
the non-linear model. In the linear model, the wall thicknesses
and Young's moduli are determined so that the (volume)
compliance of corresponding arteries is matched as well. In
the linear model, bifurcations are treated as parallel impedances, while for the non-linear approach continuity of pressure and flow is expressed. In both models, the resistance
vessels are modelled as 3-element 'windkessels.' A physiological aortic flow profile (MILNOR, 1989), representing flow in
a healthy subject at rest, is taken as the proximal boundary
condition. The heart rate is 60 beats min -1, mean flow
88mls -~ (cardiac output=5.21min - I ) and peak flow
450mls -1. For the computation with the linear model, tiffs
signal is decomposed into its Fourier-components and 10
harmonics are used.
Table 1 Derived haemodynamic parameters at the ascending aorta
and brachiaI andfemoral arteriesfor the linear and non-linear model
using the same geometrical and mechanical configuration, and
identical upstream and downstream boundary conditions
SDP
DBP
PP
PP*~n~
ascending aorta (4 era)
linear
non-linear
t 11.8
114.0
69.9
69.1
41.9
44.9
--
brachial artery (44 era)
linear
non-linear
125.4
132.0
66. I
66.6
59.3
65.4
1.41
1.46
femoral artery (80crn)
linear
non-linear
143.9
141.6
61.1
61.3
82.8
80.4
1.98
1.79
SBP = systolic blood pressure (ramHg), DBP = diastolic blood pressure (ramHg), PP = pressure pulse (ramHg), PPamp= (PP at measured location)/(PP at ascending aorta)
160 - aorta (4 crrl)
~4o~
E
femoral artery (80 cm)
brlchiaJ artery (44 cm)
12(]-
g
3 Results
3.1 Linear against non-linear modelling
Pressure and flow arc computed at the ascending aorta,
braehial and femoral artery (Table 1 and Fig. 4). These
locations are situated 4, 44 and 80 cm downstream of the
aortic valve, respectively. At the ascending aorta, mean
pressure is almost identical (91.3mmHg in the non-linear
(nl) and 90.SmmHg for the linear (l) ease), but higher
differences occur in systolic (114.0 (nO against 111.8
(1)mmHg), diastolic (69.1 (nl) against 69.9 (l)mmHg) and
hence pulse pressure (44.9 (hi) against 41.9 (t)mmHg). The
input impedance differences between both models are within
20% (Fig. 5), but especially for the low frequencies the input
impedance is higher for the non-linear model. At 1 Hz the nonlinear model input impedance modulus is 0.11 mm Hg m l - t s
against 0.09mmHgml-~s) in the linear model. The characteristic impedance is slightly increased in the non-linear case
(0.059 (nl) against 0.056 (1)mmHgml-ls). Fig. 6 gives the
ratio of braehial/aortic pressure harmonics in the linear and
non-linear cases. The harmonic ratio is similar for the two
cases between I and 6 Hz, but at 2 and 3 Hz the ratio is about
2 0 % higher in the non-linear case. For the higher harmonics
(> 6 Hz), damping is higher in the linearmodel. The values of
systolic and diastolic pressure, pulse pressure and pulse
pressui-e amplification are shown in Table I. In the nonlinear model, the higher systolic pressure and pulse pressure
at the aseending aorta are maintained at the brachial artery.
For the femoral artery, there is a reversal (Fig. 4 and Table 1).
At the ascending aorta and brachial artery, pressure peaks at
approximately the same time in both models; at the femoral
artery peaking is earlier in the non-linear model.
o.o
o.,
oo
,
os
~rf~, s
Fig. 4
Aortic, brachial and femoral pressure for the linear and nonlinear models. Input signal was a physiological flow wave
('MILNOR, 1989). ~ non-linear; . . . . . . linear
most models, damping is considerable at the brachial and
femoral artery. For the brachial artery, the pulse pressure
amplification is reduced by 15%; for the femoral artery, the
reduction is ",-23%.
3.3 Downstream boundary condition
To check the effect of the downstream boundary conditions,
we replaced the 3-clement 'windkessel' impedances by linear
resistances. In the first computation, we neglected the compliance present in the terminal windkessel' sections, so that the
actual compliance was only 1.23mlmmHg -1 at 100mmHg.
For the second computation, we compensated the loss of distal
compliance by adjusting the Young's modulus with a constant
factor, distributing the 0.24mlmmHg -1 over the entire tree.
In this way, total compliance is matched, but proximal
compliance is increased, lowering wave velocity, the ascending aorta input impedance, the characteristic impedance and
the pulse pressure. The computational results are shown in Fig.
8 and the derived haemodynamie parameters are surnmarised
in Table 3.
4 Discussion
3.2 Viscoelastic#y
Different viscoelastic models were implemented in the
linear arterial network model using the geometrical configuration described earlier. The computational results are presented
in Table 2 and Fig. 7 (Westerhof and Holenstein model). For
732
o.o
4.1 Linear against non-linear modelling
The comparison of a linear and a non-linear arterial network
model on a geometry with identical boundary conditions, total
compliance and peripheral resistance, reveals differences in
Medical & Biological Engineering & Computing
November 1997
~/r~'Hinaar
~scoe~.,.,~ty
~
r
-1
i
-o.1
0.1=
0.01
I
2
I
4
I
6
I
8
I
10
r
0
i
2
i
~,
frequency, Hz
i
6
"1
8
1
10
i
0
I
2
tre~lueney, Hz
'1
4
i ....
6
i
8
,0.01
10
frequency, Hz
,'-40
40-
o
O~
i +-
---80
1-
I
I
I
I
I
I
I
I
I
I
I
I
I
I
I
2
4
6
8
10
0
2
4
6
8
10
0
2
4
6
8
frequency, Hz .
Fig. 5
frequency, Hz
10
frequency, Hz
Ascending aorta input impedance (upper panel, modulus; lower panel, phase angle) computed at 4 cm downstream of the aortic valve.
Left: linear ( 0 ) against non-linear (A) model, middle: linear (0) against viscoelastic model (ix: Westerhof 0 : Holenstein); right:
resistive (A) against 3-element 'windkessel' (0) termination
3.0
160-
aoaa (4 era)
brachial artery (44 cm)
femoral artery (80 ern)
0.0
'
' 0.4
'
' 0 '.8 '
time, s
0.0
'
' 0,4
'
' 0i8 '
~402.5-
".
loo:
2.0-
'~
6o "-
1.5-
0.0 " ' 0.4 " " 0,8 '
_=
1.0
Fig. 7
0.5 84
0.0
0
|
I
I
I
l
I
I
!
I
I
1
2
3
4
5
6
7
8
9
1o
Pressure at the ascending aorta, brachial and femoral artery
incorporating different viscoelastz'c models in the linear
transmission line model. The solid line represents no ~scoelasticity
frequency, Hz
Fig. 6
Pressure transfer function modulus for the brachial artery
for both the linear and non-linear arterial network models.
linear; . . . A . . . non-linear
the computational results. These disparities may be due to
elastic and/or convective non-linearities, or to conceptual
differences arising from the treatment of geometric and elastic
taper, bifurcations, etc.
For the mamformation of the geometrical data set of 55
arteries or segments (STERGIOPULOSet aL, 1992) into a set for
the linear model (156 segments), attention was paid to the
following aspects: equal up- and downstream vessel radius and
wall thickness, equal volume and equal compliance. E varies
from 300kPa for the ascending aorta to 1000kPa for the
peripheral arteries (values are for a reference pressure of
100 mmHg), with wave velocities ranging from 4 m s - l in
the ascending aorta) to 13 ms -~ in the lower limb arteries. In
the linear model, the 55 arteries are subdivided into smaller
segments with the elastic modulus increasing with distance
Medical & Biological Engineering & Computing
from the heart. This can explain the observed higher wave
velocity in the non-linear model at the femoral location (Fig.
4): total compliance of the femoral artery is equal, but not its
distribution. Apparently the compliance of the proximal part
of the femoral artery is lower for the non-linear model, with a
consequently higher wave velocity and decreased pulse pressure amplification.
In spite of identical downstream boundary conditions, total
compliance and resistance, the input impedance is not identical. Especially at the lowest frequencies, the input impedance
modulus is higher in the non-linear case (note that strictly
speaking, the input impedance is a non-existing feature in the
non-linear model). This difference may arise from the elastic
nonlinearity: the most important harmonics load the vessel up
to higher pressures, where compliance is lower. While we
compared the model under control conditions, these aspects
can be expected to be more pronounced under exercise
conditions. Another aspect contributing to the input impedance difference is the treatment of geometric and elastic
taper. Whereas for the non-linear model the tapering is
November 1997
733
Table 2 Derived haemodynamlc 15arameters at the brachial and
femoral arteries for different viscoelastic models. Computaaons were
made with the linear model, and for the same geometrical setup
SBP.
DBP
PP
ascending aorta
linear model
Westerhof (1970)
Wesseling (y) (1973)
Wesseling (o) (1973)
Langcwouters (1984)
Holenstein (1980)
111,7
113.1
69.9
71.1
70,9
70.8
70.0
71.7
113.1
113.7
112.4
112.0
(4
PPm,,
era)
SBP
41.8
42.0
42.2
43.0
t25.4
121.6
122.9
124.5
125.8
122.6
g+slt~red C
3 el WK
R
42.4
108.9
111.7
112.0
40.3
66.1
70.3
69.5
69.1
66.7
69.8
DBF
PP
PPa~,
ascending aorta (4 era)
70.3
69.9
67.5
38.6
41.8
44.5
--
brachial artery (44 cm)
braehial artery (44 crn)
linear model
Westerhof (1970)
Wesseling 0') (1973)
Wesseling (o) (1973)
Langewouters (1984)
Holenstein (1980)
Table 3 Derived haemodynamic parameters at the brachial and
femoral artery for a) resistance terminations with total:compliance
compensation (R+altered C), b) 3.-element "windhessel termination'
3 el Wk and c) resistance termination without compensation f o r lost
compliance (R)
59.3
51.4
53.4
55.4
59.1
52.8
1.42
1.22
1.26
1.29
1.39
1.31
femoral artery (80 cm)
R+altered C
3 el Wk
R
127.2
125.4
132.7
66.9
66.1
64.4
60.3
59.3
68.3
1.56
1.42
1.53
femoral artery (80cm)
R+altered C
3 el Wk
R
138. l
143.9
149.3
62.6
61.1
54.7
75.5
82.8
94.3
1.95
1.98
2.12
1.98
1.54
1.56
1.53
1.93
1.65
SBP =~ystolic blood pressure (ram Hg), DBP =diastolic blood pressure (mm Hg), PP = pressure pulse (mm Hg), PP,,~p = (PP at measured location)/(PP at ascending aorta)
SBP = systolic blood pressure (ramHg), DBP = diastolic blood pressure (mm Hg), PP=pressure pulse (mm Hg), PPo,w=(PP at measured location)/(PP at ascending aorta), y =young, o =oM
pressure is further transmitted towards the periphery. At the
peripheral sites, the morphological agreement is better,
although the absolute pressure differences are maintained.
At the bracial artery, the pulse pressure is further amplified;
at the femoral artery, there is less difference.
Evaluating the ratio of pressure harmonics at the brachial
artery and ascending aorta (transfer function; Fig. 6), it is
noted that for frequencies below 6 Hz, the general pattern is
similar. At 2 and 3 Hz the modulus is --'20~ higher in the nonlinear case. For both models a peak value of 2.5 is found at
6 Hz. For frequencies above 6 Hz there is better damping for
the linear model: a sharp peak (2.8) is found at 8 Hz for the
non-linear model. This phenomenon, that non-linear models
tend to under-estimate damping at higher frequencies, agrees
with the findings of REUDERINKet al. (1989).
linear model
Westerhof (1970)
Wesseling (y) (1973)
Wesseling (o) (1973)
Langewouters (1984)
Holenstein (1980)
143.9
133.3
133.5
134.1
143.9
134.7
aorta (4 cm)
160
~ 1
61.1
68.5
67.6
68.6
62.3
68.3
~."ter
82.8
64.8
65.9
65.6
81.7
66.5
cm)
femoralmlery (80 cm)
~. 14o
12o
i,~176
8O
6O
I
0.0
(
0.4
|
I """1
0.8
I
0.0
~
I
th'~,
~g. 8
I
0.4
I
0.8
1
~
0-0
[
1
0.4
I
I
!
0.8
s
Pressure at the ascending aorta, brachial and femoral artery
for different models o f the resistance vessels: pure resistance, with compensation for the loss in compliance (0:
'R+altered C') ; pure resistance, without compensation (0:
'R "); 3-element "windkessel impedance" (---: '3-el WTC'J
embedded in the equations, the converging vessel is replaced
by a sequence of uniform segments in the linear case.
The morphological pressure wave differences between both
models are most pronounced at the ascending aorta, computed
4 em downstream from the a o ~ c valve (Fig. 4). It is likely that
this is an effect of the specific geometry used for the computation (Fig. 1): the right common carotid and axiliary artery
originate from the inominate artery, a short segment with large
diameter and severe tapering (length 3.4 era, proximal radius
1.01cm, distal radius 0.62cm). In the linear model, the
inominate artery has been replaced by three cylindrical segments, creating important local changes in characteristic
impedance and thus reflection sites.
Different systolic and diastolic pressure levels are observed
at all locations (Table I). They are in part explained by the
higher input impedance at 1 Hz in the non-linear model (Fig.
5). For the same input flow wave, the ascending aorta pulse
pressure is higher in the non-linear model and this higher pulse
734
4.2 Viscoelasticity
Viscoelasticity enhances peripheral pressure and flow wave
damping (Table 2). Pulse pressure amplification is reduced
from 1.42 to --- 1.25 for the brachial artery ( - 12%), and from
1.98 to 1.55 for the femoral artery ( - 2 2 % ) . Comparison with
the data shown in Table 1 suggests that the impact of
viscoelasticity on the pulse pressure propagation is more
important than the impact of elastie non-linearities. The
effect of viscoelasticity on pressure values and pressure
wave morphology is most pronounced at the peripheral sites.
However, its effect is also reflected in the input impedance
pattern (Fig. 5). The dynamic elasticity modulus is higher than
the static value, and it increases with frequency (Fig. 3, upper
panel). Consequently, the input impedance modulus is higher
in the viscoelastic case. The characteristic impedance is only
slightly increased (+ 6%).
We implemented different viscoelastic models, expressed as
a complex frequency-dependent elasticity modulus, in the
linear arterial network model. The disparity between most
models is restricted, due to the fact that they are derived from
the same data (HARDtr~G, 1953; BERGEL, 1960; LEAROYDand
TAYLOR, 1966). The only significantly different model is
proposed by LANGEWOtrI'ERSet aL (1985) for aged arteries,
Medical & Biological Engin~ring & Computing
November 1997
exhibiting an almost complete loss of viscoelasticity. Implementation of this model yields results that are very close to the
linear case, with respect to both the magnitude and morphology of the pressure curves.
Table 4 IL~lS-value (in mn, Hg) of computed pre.~v.rea Pc.~. at the
ascending aorta (4r
brachial (44cm) and#moral artery (80 cm)
compared to the linear case
Plin I~MS = V
4.3 Linear resistance against 3-element 'windkessel'
Representation of the resistive vascular beds is found to be
critical for the morphology and amplitude of the peripheral
pressure. This feature is especially important if one intends to
use arterial network models for the computation of transfer
functions, wave reflection analysis (KARAMANOGLU et aL,
1994) or for the evaluation of other models or diagnostic
techniques (STEROIOPULOSet al., 1995). Attention should be
paid not to create reflection zones, which are not present in
vivo.
We modelled the capillary beds as a linear resistance and as
a 3-element 'windkessel' model, including some distal compliance, and studied the effect on the pressure wave magnitude
and contour. However, simple qualitative and quantitative
analysis is difficult, because omitting distal compliance (for
the resistive model) changes the total compliance of the
configuration from 1.47 to 1.23 ml mm Hg -1. This has only
a limited effect on the input impedance (Fig. 5, right panel)
and hence proximal pressures (Fig. 8, ascending aorta), but
increased systolic pressure and pulse pressure are found at
peripheral sites.
To cover this distal loss in compliance, we lowered the Emoduli throughout the arterial tree (by a factor of 0.84) in
order to restore the total compliance to 1.47 ml mm H g - 1.
This obviously influences the relative distribution of elasticity
and results in a lower input impedance and lower proximal
pressures. Nevertheless, distal compliance is still neglected
and wave reflection intensity is definitely increased at the
peripheral sites, influencing the peripheral pressure and ftow
wave contour. With the higher proximal compliance, the
effects are modest, but still clearly present.
When a purely resistive peripheral model is assumed, the
trough following the steep pressure decay (at the end of
systole) is deeper. Peripheral systolic pressure and pulse
pressure are higher, as well as pulse pressure amplification.
The effects are most pronounced close to the terminal (reflection) point. The most distal reflection point is 35 cm away for
the brachial artery and 65 cm away for the femoral artery; the
impact of the terminal impedance model is therefore more
clear at the brachial artery. Nevertheless, one should not
conclude that the choice of the peripheral model is unimportant for the pressure computed in the central aorta. Abdominal
capillary beds in the kidneys, liver and other abdominal organs
capture a large portion of the stroke volume and have been
designated an important role in aortic wave reflection (KARAMANOGLUet aL, 1994; LATHAMet aL, 1985). These beds are
situated close to the aorta and may therefore play a very
important role in the pattern of pressure and flow wave
propagation. They should therefore be modelled accurately
in order to match their in vivo input impedance spectra. The
choice of terminal model should also be related to the order of
branching included in the model. With a higher level of
bifurcation the distal beds become isolated from the central
aorta and their impact will be smaller, as waves reflected at
these beds will not reach the aorta due to re-reflection at the
bifurcations.
4.4 Elastic non-linearity against viscoelasticity and terminal
impedance model
In this study, we have evaluated the relative importance of
elastic non-linearities compared to viscoelasticity and the
Medical & Biological Engineering & Computing
NL
VE
VE
PM
PM
Westerhof
Holenstein
R+altered C
R
N
brachial
femoral
aorta
artery
artery
1.89
1.91
1.49
1.81
1.61
2.92
3.34
2.36
3.70
4.04
8.82
7.13
5.00
6.71
4.50
NL = nonlinearity, FE = viscoelasticity, PM = peripheral model
terminal impedance model used for the small arteries, arterioles and capillaries. Table 4 gives the mean deviation (RMS
value) of pressures computed under different conditions with
respect to reference pressures, computed with the linear
arterial network model, no visco-elasticity and 3-element
'windkessel' terminations. It is shown that the RMS-value
for the non-linear model is of the same order of magnitude as
the values arising from viscoelasticity and the terminal impedance model. Linear and non-linear arterial network models
do give different computational results, but the impact on
pressure wave amplitude and morphology is less important
than the impact of viscoelasticity or the choice of the distal
terminating model. The similarity of the pressure transfer
function (and thus individual harmonic treatment) in the
linear and non-linear model suggests that neither convective
acceleration, nor elastic nonlinearities are the most important
determinants of the arterial pressure and flow. It is also shown
that the harmonics > 6 Hz are more damped in the linear than
in the non-linear model.
A purely resistive terminal impedance model augments
pressure wave reflection and consequently systolic pressure
and pulse pressure amplification. This effect was less clear for
the pressure computed at the femoral artery, where the
distance to the distal reflection site is larger and wave damping
along the transmission path is more important.
Viscoelasticity enhances peripheral pressure wave damping,
with lower systolic and higher diastolic pressures and reduced
pulse pressure amplification. In the central aorta, the damping
is overruled by the increased dynamic elasticity modulus.
Further away from the heart, the net effect is wave damping,
and the difference with the reference computations becomes
significant.
We believe that the combination of different modelling
features (e.g. resistive distal model and viscoelasticity) may
result in an adequate simulation of arterial pressure wave
propagation- However, this does not necessarily imply that the
model parameters correspond to actual biomechameal properties of the vessels and their boundary conditions.
Aclmowledgments~This research is funded by a specialisation grant
fi'om the Flemish Institute for the Promotion of Scientific-Technological Research in Industry (IWT 943065), and a concerted action
programme of the University of Gent, supported by the Flemish
government (GOA 95003).
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Author's biography
Patrick Segers was born in Ninove, Belgium in 1968. He obtained
his M.Sc. in Civil Engineering at the Faculty of Applied Sciences of
the University of Gent, Belgium in 1991. In April 1997 he obtained
his Ph.D. at the Hydraulics Laboratory, member of the Institute of
Biomedical Technology (IBITECH) at the University of Gent. His
research interests are in the cardiovascular domain: mathematical and
physical models of the cardiovascular circulation, blood theology and
compliance estimation techniques.
Medical & Biological Engineering & Computing
November 1997