Biomedical Engineering Reference
In-Depth Information
The relation for the longitudinal impedance in function of aerodynamic variables
is obtained from ( 4.43 ), and gives
μδ 2
πR 4 M 1
jωρ
πR 2 M 1
e j( 2 ε 1 )
e 1
Z l =
=
πR 4 M 1 sin 1 ) + j cos 1 )
μδ 2
=
(4.56)
respectively, in terms of transmission line parameters, the longitudinal impedance is
given by Z l = r x + jωl x .
By equivalence of the two relations we find that the resistance per unit distance
is
μδ 2
πR 4 M 1
r x =
sin 1 )
(4.57)
R ω μ
μδ 2
πR 4 M 1
It follows that ωl x =
cos 1 ) and recalling that δ
=
, the inductance
per unit distance is
ρ
πR 2
cos 1 )
M 1
l x =
(4.58)
4.2.1 Elastic Tube Walls
In case of an elastic pipeline , the characteristic impedance is obtained using rela-
tions ( 4.43 ), ( 4.44 ), and ( 4.50 ), leading to
Eh
2 ρR
ρ
πR 2
1
1
M 1
e j ε 2
Z 0 =
(4.59)
ν P
1
and for a lossless line (no air losses trough the airway walls, thus conductance g x is
zero ), the transversal impedance is
Z 0
1
jωc x =
Eh
(j ω( 2 πR 3 ( 1
Z t =
Z l =
(4.60)
ν P ))
from where the capacity per unit distance can be extracted:
2 πR 3 ( 1
ν P )
Eh
c x =
(4.61)
Thus, from the geometrical (R, h) and mechanical (E, ν P ) characteristics of the
airway tube, and from the air properties (μ, ρ) one can express the r x , l x and c x
parameters. In this way, the dynamic model can be expressed in an equivalent loss-
less transmission line by Eqs. ( 4.57 )-( 4.61 ). Notice that the compliance parameter
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