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<article xmlns:xlink="http://www.w3.org/1999/xlink">
  <front>
    <journal-meta />
    <article-meta>
      <title-group>
        <article-title>In uence of the Endothelial Surface Layer on Blood Flow in Microvessels: Computer Modeling and Simulation ? ??</article-title>
      </title-group>
      <contrib-group>
        <contrib contrib-type="author">
          <string-name>y Kovt</string-name>
          <email>andrei.kovtaniuk@tum.de</email>
        </contrib>
        <contrib contrib-type="author">
          <string-name>Altyn</string-name>
        </contrib>
        <contrib contrib-type="author">
          <string-name>i Muk</string-name>
        </contrib>
        <contrib contrib-type="author">
          <string-name>Turov</string-name>
          <email>turova@ma.tum.de</email>
          <xref ref-type="aff" rid="aff1">1</xref>
        </contrib>
        <aff id="aff0">
          <label>0</label>
          <institution>Mathematical Faculty, Chair of Mathematical Modelling, Technical University of Munich</institution>
          ,
          <addr-line>Garching</addr-line>
          ,
          <country country="DE">Germany</country>
        </aff>
        <aff id="aff1">
          <label>1</label>
          <institution>School of Medicine, Klinikum rechts der Isar, Orthopedic Department, Research Unit for Pediatric Neuroorthopedics and Cerebral Palsy of the Buhl-Strohmaier Foundation, Technical University of Munich</institution>
          ,
          <addr-line>Munich</addr-line>
          ,
          <country country="DE">Germany</country>
        </aff>
      </contrib-group>
      <fpage>153</fpage>
      <lpage>162</lpage>
      <abstract>
        <p>The paper describes a mathematical model of blood ow in capillaries with accounting for the endothelial surface layer (ESL). The in uence of ESL is modeled by a boundary layer with zero ow velocity. Numerical simulations for di erent levels of the discharge hematocrit are conducted using the nite element method. The reliability of the results obtained is veri ed using known experimental data.</p>
      </abstract>
      <kwd-group>
        <kwd>Capillary blood ow ement method</kwd>
      </kwd-group>
    </article-meta>
  </front>
  <body>
    <sec id="sec-1">
      <title>-</title>
      <p>Modeling blood circulation in human brain requires understanding the dynamics
of blood ow both in the entire vascular network and in an individual vessel.
Assuming the blood ow in a vessel as a moving laminar Newtonian uid, we
describe it by the Poiseuille's law [16]:</p>
      <p>Q =</p>
      <p>
        D4
p:
(
        <xref ref-type="bibr" rid="ref1">1</xref>
        )
Here, the ow Q (volume ow rate) through a cylindrical tube is a function of
the pressure di erence p, the tube diameter D, and the length L of the tube.
      </p>
      <p>The dynamic viscosity is a material property of the liquid, which re ects the
internal resistance to shearing motions. This law is a reasonable approximation
for the ow in large blood vessels. As the diameter of the blood vessel decreases,
the behavior of the blood ow increasingly deviates from the Poiseuille's law. For
small vessels, e.g. for capillaries, the blood cannot be considered as continuous
uid with a xed viscosity. Instead, it is regarded as plasma with suspended
red blood cells (RBCs), also called erythrocytes. Other elements of blood, as
for example, white blood cells and platelets have negligible e ects on the blood
ow due to their tiny volume fractions. Thus, the blood in a microvessel can
be considered as a two-phase liquid consisting of plasma and erythrocytes [2, 3],
wherein the RBCs phase is modeled by a high viscosity substance. Numerical
realization of the two-phase model of blood ow in capillaries can be carried out
using the nite element method (see, e.g., [3]).</p>
      <p>The RBCs have a tendency to migrate away from the vessel walls to the
centerline, which causes the formation of cell-free regions near the vessel walls.
Since the velocity increases towards the vessel centerline, the velocities of RBCs
are higher than the average blood velocity. This means that there is a di erence
between the tube hematocrit (the volume fraction of RBCs in the vessel at a
given time instant) and the discharge hematocrit (the volume fraction of RBCs
collected at the end of the tube at a given time period); the latter is higher
than the tube hematocrit. This phenomenon is called Fahr us e ect [14]. The
discharge hematocrit level has a signi cant impact on the parameters of blood
ow in microvessels [14{16].</p>
      <p>
        As noted above, Poiseuille's law does not apply to microvessels. However, to
estimate the resistance to blood ow in microvessels, it is possible, on the base
of (
        <xref ref-type="bibr" rid="ref1">1</xref>
        ), to de ne the apparent or e ective viscosity of blood, that is, the viscosity
of a Newtonian uid that would give the same volume ow rate for a given tube
geometry and pressure di erence. According to (
        <xref ref-type="bibr" rid="ref1">1</xref>
        ), the apparent viscosity is
determined as
app = 128 L
      </p>
      <p>D4</p>
      <p>
        p
Q
:
(
        <xref ref-type="bibr" rid="ref2">2</xref>
        )
      </p>
      <p>
        By calculating the blood ow Q for a given pressure drop p using the nite
element method, we can nd the apparent viscosity by formula (
        <xref ref-type="bibr" rid="ref2">2</xref>
        ) and compare
it with experimental data to estimate the adequacy of the mathematical model.
      </p>
      <p>Note that the microcirculatory hemodynamic parameters (e.g., on the
apparent viscosity and ow resistance) are signi cantly in uenced by the endothelial
surface layer (ESL). The e ect of ESL on blood circulation, as well as its
characteristics are discussed in [12{14, 16]. Following [13], the term \Endothelial surface
layer" (ESL) is used for a boundary layer in which the plasma motion is signi
cantly retarded. In particular, the ESL includes the glycocalyx layer. A. Copley
studied the endothelium-plasma interface and developed a concept in which an
immobile layer of plasma at the vessel wall is present [4, 5]. In the present paper,
the in uence of ESL on the apparent viscosity is investigated by means of the
boundary layer with zero velocity.</p>
      <p>Construction of a mathematical model of blood ow in microvessels
accounting for the in uence of ESL allows us to determine adequate vessels resistances
in the brain capillary network. It is important to calculate the cerebral pressure
distribution, for example, using the algorithm proposed in [2]. In particular, it
can be applied to nd most dangerous pressure gradients to estimate the risk of
bleeding in the germinal matrix of preterm infants.
2</p>
      <p>Experimental Observations of the Apparent Viscosity
The dependence of the relative apparent viscosity rel (the ratio of apparent
viscosity to plasma viscosity) on the discharge hematocrit and vessel diameter
both in vitro and in vivo is provided by T. Secomb and A. Pries [15]. The in
vitro data corresponding to blood ow in a glass tube are represented by the
following equation:
where
and
rel = 1 + ( 0:45
1)
(1
(1</p>
      <p>HD)C
0:45)C
In these equations, D denotes the diameter of the vessel (glass tube) in m,
and HD is the discharge hematocrit. The parameter 0:45 is the viscosity for
HD = 0:45 which is a typical hematocrit for humans.</p>
      <p>
        The plots of the relative viscosity obtained by the formula (
        <xref ref-type="bibr" rid="ref3">3</xref>
        ) (in vitro data)
for the levels of discharge hematocrit of 0.1, 0.3, and 0.5 are shown in Fig. 1.
      </p>
      <p>Similar measurements in vivo are di cult due to technicalities of measuring
the pressure drop in capillaries. Therefore, it was assumed that the reduction of
the viscosity with increasing diameter of living vessels was similar to that in glass
tubes. However, the estimates of the apparent viscosity obtained by Lipowsky
et al. [7, 8] for blood ow in microvessels were much higher than expected from
the in vitro data. An alternative parametric description that is consistent with
the observed behavior in vivo was found by Pries et al. [11]:
rel =
1 + ( 0:45
1)
(1
(1</p>
      <p>
        HD)C
0:45)C
and C remains the same as in equation (
        <xref ref-type="bibr" rid="ref5">5</xref>
        ).
      </p>
      <p>
        The plots of the relative viscosity obtained by the formula (
        <xref ref-type="bibr" rid="ref6">6</xref>
        ) (in vivo data)
for the levels of discharge hematocrit of 0.1, 0.3, and 0.5 are shown in Fig. 2.
      </p>
      <p>
        The di erence between the in vivo and in vitro data can be explained by the
presence of the endothelial surface layer on the inner surface of blood vessels,
which has a signi cant e ect on the blood ow.
(
        <xref ref-type="bibr" rid="ref3">3</xref>
        )
(
        <xref ref-type="bibr" rid="ref4">4</xref>
        )
(
        <xref ref-type="bibr" rid="ref5">5</xref>
        )
(
        <xref ref-type="bibr" rid="ref6">6</xref>
        )
(
        <xref ref-type="bibr" rid="ref7">7</xref>
        )
      </p>
      <p>
        4
3
3.5
Fig. 2. Dependence in vivo of the relative viscosity ( rel) on the vessel diameter (D) for
di erent values of the discharge hematocrit: HD = 0:1 (solid line), HD = 0:3 (dashed
line), and HD = 0:5 (dot-dashed line). The data represented by (
        <xref ref-type="bibr" rid="ref6">6</xref>
        ), (
        <xref ref-type="bibr" rid="ref7">7</xref>
        ) correspond to
the blood ow in microvessels of animals.
      </p>
    </sec>
    <sec id="sec-2">
      <title>Finite Element Modeling</title>
      <p>As it was proposed in [2, 3], the RBCs and blood plasma are considered as one
ow with two di erent viscosities (much larger viscosity for red blood cells):
the viscosity of blood plasma is assumed to be 1 = 0:001 Pa s, whereas the
viscosity of RBCs is set to be 2 = 0:1 Pa s to make RBCs e ectively rigid.
Moreover, it is assumed that the ow is steady-state, without transition e ects.
Therefore, the model is described by the steady state Stokes equation with space
variable viscosity.</p>
      <p>Assume that the ow is axisymmetric, that is all variables depend only on
the radial and longitudinal coordinates, r and z. Let ur and uz be the radial
and longitudinal ow velocities, respectively, and p the pressure. Therefore, it is
possible to reduce the problem to two dimensions (see Fig. 3). Here, the radius
r0 determines the boundary of the sequence of RBCs and hence rc r0 is the
thickness of the plasma gap between the RBCs and the vessel wall.</p>
      <p>Denote = (0; rc) (0; L). The model is mathematically formulated in [17]
in a weak form, which allows us to use spatially discontinuous viscosity functions.
With x1 = r, x2 = z, u1 = ur, u2 = uz, u = (u1; u2)T , p(r; 0) = p0, p(r; L) = 0,
the weak formulation reads in cylindrical coordinates as follows:
Z</p>
      <p>2
x1 2 (x1; x2) X Dij (u)Dij (v) + u1v1 dx</p>
      <p>Z
i;j=1
x1 p div(v)dx =</p>
      <p>x1 p0 v2 dx;
Z
0
x2
1
"</p>
      <p>Z
where</p>
      <p>Z
x1pq dx
x1 div(u) q dx = 0;
" = 10 6;
uj 2 = 0;
vj 2 = 0;
Dij (u) =</p>
      <p>Functions v = (v1; v2)T , and q are the test ones. The viscosity distribution
(x1; x2) is equal to 0.001 Pa s in the plasma part and 0.1 Pa s in the RBCs
part.</p>
      <p>
        Thus, the RBCs are modeled as uid with the high viscosity to make them
e ectively rigid. The model (
        <xref ref-type="bibr" rid="ref8">8</xref>
        ), (
        <xref ref-type="bibr" rid="ref9">9</xref>
        ) is equivalent to the following one:
where
      </p>
      <p>Z</p>
      <p>2
x1 2 (x1; x2) X Dij (u)Dij (v) + ux1v21 + rpv dx = 0;</p>
      <p>1
"</p>
      <p>Z
x1 pq</p>
      <p>
        div(u)q dx = 0;
pj 0 = p0; pj 1 = 0; uj 2 = 0; vj 2 = 0;
rp =
:
(
        <xref ref-type="bibr" rid="ref10">10</xref>
        )
(
        <xref ref-type="bibr" rid="ref11">11</xref>
        )
(
        <xref ref-type="bibr" rid="ref12">12</xref>
        )
      </p>
      <p>To set the value of the pressure drop at a capillary with the length L, rst,
we estimate the pressure drop in the capillary network (pressure di erence
between inlets and outlets). For the estimation, the cerebral ow rate and total
resistance of the capillary network are required. According to [18], the cerebral
blood ow rate Q = 600 ml/min is a realistic value for an adult brain. Moreover,
a cerebrovascular network model from [10] yields the total resistance RT of the
capillary system to be equal to 0:1Pa s=mm3, which gives the pressure drop to
be equal to 1000 Pa (computed as Q RT ). Following [10], where the parallel
topology for capillaries with the length of 600 m and radius of 2.8 m is utilized,
we consider in further modeling that the pressure drop of 1000 Pa corresponds
to the capillary length of 600 m. Therefore, for the capillary length equals to L,
the pressure drop is 5L=3 Pa. In the numerical modeling, the capillary length
is chosen in the range from 50 to 150 m in accordance with the level of the
hematocrit.</p>
      <p>
        When conducting computer simulations, along with specifying the radius of
the vessel, it is required to determine the radius r0 of the core zone lled with
RBCs and the linear dimensions of RBCs. To specify r0, we use the following
approximation [2]:
r0 = 0:3 m + 0:8rc:
(
        <xref ref-type="bibr" rid="ref13">13</xref>
        )
The length of an erythrocyte is determined on the base of its mean volume equals
to 88 m3 [9] and the value of r0.
      </p>
      <p>Comparison of the results of the nite element modeling (conducted by using
FreeFEM++ package [6]) with in vitro data shows a signi cant di erence (see
Fig. 4). This is because the velocity no-slip condition, uj 2 = 0, is not suitable
for modeling the blood ow in glass tubes. More adequate is using the velocity
slip condition: u1j 2 = 0 and @u2=@x1 + u2j 2 = 0. By appropriate choosing
the parameter in numerical modeling, we can provide a closer approximation
of the in vitro data.</p>
      <p>4
3
3.5
4.5
5
5.5 6 6.5
Vessel diameter, μm
7
7.5
8</p>
      <p>To take into account the in uence of ESL in modeling the blood ow in
microvessels, we assume zero ow velocity in some neighborhood of the vessel
wall, that is u = 0 for r &lt; r rc (r &gt; r0). The presence of the sublayer of ESL
with zero ow velocity is mentioned in particular in [14], where the longitudinal
velocity pro le measured in a rat venule is presented. Note that a similar e ect
regarding zero velocity in a neighborhood of the surface somewhat akin to ESL
is also observed [1] in modeling of elasto-optical biosensors.</p>
      <p>
        To t the results of nite elements modeling to experimental data described
by (
        <xref ref-type="bibr" rid="ref6">6</xref>
        ) and (
        <xref ref-type="bibr" rid="ref7">7</xref>
        ), we use the following representation of the boundary of the layer
with zero ow velocity:
r = 0:366 m + 0:725rc + 0:024rc2:
(
        <xref ref-type="bibr" rid="ref14">14</xref>
        )
The formula (
        <xref ref-type="bibr" rid="ref14">14</xref>
        ) is obtained by the minimization of the mean square error
between the results of the nite element modeling and in vivo data given by (
        <xref ref-type="bibr" rid="ref6">6</xref>
        ).
Note that the representation (
        <xref ref-type="bibr" rid="ref14">14</xref>
        ) was obtained under the assumption of the
consistency of the approximation (
        <xref ref-type="bibr" rid="ref13">13</xref>
        ). Re ning the formula (
        <xref ref-type="bibr" rid="ref13">13</xref>
        ) will result in a
corresponding adjustment of the formula (
        <xref ref-type="bibr" rid="ref14">14</xref>
        ).
      </p>
      <p>
        The computed values of the relative viscosity and in vivo data calculated
with (
        <xref ref-type="bibr" rid="ref6">6</xref>
        ) and (
        <xref ref-type="bibr" rid="ref7">7</xref>
        ) are shown in Fig. 5.
      </p>
      <p>It is worth to note that taking into account the in uence of ESL through
the layer with zero ow velocity is characterized by a signi cant increase of the
relative viscosity and, respectively, by a proportional increase of the microvessel
resistance. As a consequence, it leads to a proportional decrease in the
longitudinal velocity. The results of a numerical experiment for the vessel diameter of
6 m and HD = 0:3 are shown in Fig. 6.</p>
      <p>22
20
18
16
5.5 6 6.5
Vessel diameter, μm
7
7.5
8</p>
      <p>In the example considered, accounting for the ESL leads to the 3.9-fold
increase of the viscosity and, respectively, to the 3.9-fold decrease of the blood
ow.
4</p>
    </sec>
    <sec id="sec-3">
      <title>Conclusion</title>
      <p>The mathematical model of blood ow in capillaries containing the endothelial
surface layer was proposed. The ESL in uence is described by the presence of the
boundary layer with zero ow velocity. The reliability of the results obtained has
been veri ed for di erent values of the discharge hematocrit and vessel diameter
using experimental data from the literature.</p>
      <p>Further e orts of the authors will be aimed at applying this approach to
calculate the characteristics of the cerebral capillary network with the subsequent
calculation of the blood ow and pressure drop distributions in the germinal
matrix of preterm infants.</p>
    </sec>
  </body>
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