Biomedical Engineering Reference
In-Depth Information
Fig. 5.7
Velocity profiles at different locations of diameter distances from the inlet for
u
in
= 0.01 m/s
and dynamic viscosity of
a
μ
1
=4
10
−
5
s, and
b
μ
2
=10
−
5
×
kg/m
·
kg/m
·
s
these cases, the inlet profile can be prescribed with a uniform velocity inlet, but this
neglects the upstream flow conditions developed by the upper respiratory airway. To
account for some flow development, studies in the literature have used a parabolic
profile at the tracheobronchial inlet for a laminar steady flow (Liu et al. 2003) while
more recent studies also include the influence of the laryngeal jet effect (Luo and
Liu 2009; Zhang et al. 2005a). The development of the velocity flow profile through
internal flows is primarily due to the diffusion term in the momentum equation. To il-
lustrate this, let us consider an internal pipe flow, which again may represent a highly
simplified trachea that has a uniform velocity profile applied to the inlet. Here, the
dimensions of the pipe are given as height
L
= 15 cm and diameter
D
= 2 cm. Using
CFD, the development of the velocity profiles between the inlet and the outlet can
be visualized with air (density
ρ
= 1.2 kg/m
3
) as the working fluid, for a fixed inlet
velocity
u
in
= 0.05 m/s, and with dynamic viscosities
μ
1
=4
10
−
5
kg/m
×
·
s (Case 1)
or
μ
2
=10
−
5
s (Case 2).
Although the dynamic viscosity
μ
is used in the cases above, it is related to the
kinematic viscosity which is presented in Eq. (5.13) by
ν
kg/m
·
μ/ρ
. Therefore the influ-
ence of the diffusion term is represented by the variation in the dynamic viscosities in
Case 1 and Case 2. Based on a CFD simulation, Fig.
5.7
shows the velocity profiles
at different downstream locations measured by the diameter distances from the inlet
=
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