Civil Engineering Reference
In-Depth Information
Equation (10.75) can be rewritten (see Equation (3.54))
k z
k N +
k x
k P = 1
(10.82)
Let θ 1 be the angle of the wave number vector k 1 of components k x and k z with the
Z axis. The angle θ 1 and the modulus of the wave number vector satisfy the relation
k 1 cos 2 θ 1
k N
k 1 sin 2 θ 1
k P
+
= 1
(10.83)
Using the asymptotic limit of the effective density at high frequency gives the fol-
lowing angular dependence for the apparent tortuosity α 1 )
cos 2 θ 1
α P
sin 2 θ 1
α N
1
α 1 )
+
=
(10.84)
where α P
is the tortuosity in the plane (X,Y) and α N
is the tortuosity in the direction
Z . Tortuosity measurements at ultrasonic frequencies by Castagnede et al . (1998) show
a good agreement with this angular dependence. Using the asymptotic limit of the
effective density at low frequency gives the same relation for the apparent flow resistivity
σ(θ 1 )
cos 2 θ 1
σ P
sin 2 θ 1
σ N
1
σ(θ 1 )
+
=
(10.85)
10.6
Mechanical excitation at the surface of the porous
layer
The excitation is a unit stress field τ zz applied at the free surface of the layer with a
space dependence exp (
jωx/c) . The boundary conditions at the free surface are given
by Equations (10.61) - (10.63) and Equation (10.64) is replaced by
+ τ zz = σ zz
p e
(10.86)
The unit stress creates a plane wave in air with a spatial dependence exp[
j(ωx/c
k 0 z cos θ) ]where k 0 is the wave number in the free air and cos θ is given by
(k 0 /ω) 2
( 1 /c) 2
cos θ
(10.87)
k 0
The choice in the physical Riemann sheet corresponds to Im cos θ 0. The pressure p e
and the velocity component v z are related by
p e
=− v z Z 0 / cos θ
(10.88)
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