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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