Biomedical Engineering Reference
In-Depth Information
to curve downwards, the flow streamlines reflect this by pointing in the negative
y
-direction.
8.2.6
Flow Features in the Nasal Valve
Two cross-sectional areas located just proximal to the anterior nasal valve at
x
=
2
.
6cmand
x
3
.
2 cm were chosen to highlight the rapid changes in the flow field
since the anterior nasal valve was located at
x
=
2 cm posterior to the anterior nares.
The naming convention used in this paper for the left and right cavity takes on the side
that the cavity sits anatomically. The cross-section shown in Fig.
8.9
is from a frontal
perspective (positive flow into the paper) and therefore the right cavity is depicted on
the left side. Similar to Fig.
8.8
. contour plots of the axial velocity (
x
-component of
velocity) combined with streamlines of secondary flow (
y-z
component of velocity)
is shown here.
=
Fig. 8.9
Velocity field in the
coronal cross-section located
at 2.60 cm from the anterior
tip of the nose.
a
At flow rate
of 7.5 L/min and
b
At flow
rate of 15 L/min
Right
Left
a
7.5L/min
Right
Left
b
15L/min
By applying the directional streamlines, secondary flow features such as vortices
can be visualised. The air enters the vestibule region with a vertical direction. And
as the distance increases from the anterior tip of the nostrils, the nasal geometry
becomes narrow as the airstream turns posterior, approximately 90
◦
towards the
nasopharynx. This transition coupled with the narrowing geometry forces the flow to
emerge from the outer walls from the septum and be directed inwards. The presence
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