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Axisymmetric wave propagation in multilayered poroelastic grounds due to a transient acoustic point
source
Julien Capeillère, Arnaud Mesgouez, Gaëlle Lefeuve-Mesgouez
To cite this version:
Julien Capeillère, Arnaud Mesgouez, Gaëlle Lefeuve-Mesgouez. Axisymmetric wave propagation in multilayered poroelastic grounds due to a transient acoustic point source. Soil Dynamics and Earth- quake Engineering, Elsevier, 2013, 52 (September 2013), pp.70-76. �10.1016/j.soildyn.2013.05.003�.
�hal-00734083v5�
Axisymmetric wave propagation in multilayered poroelastic grounds due to a transient acoustic point source
Julien Capeill` ere
a,, Arnaud Mesgouez
a,∗, Ga¨ elle Lefeuve-Mesgouez
a,a
Universit´ e d’Avignon et des Pays de Vaucluse, UMR EMMAH, Facult´ e des Sciences, 33 rue Louis Pasteur, F-84914 Avignon, France
Abstract
This paper deals with the study of axisymmetric wave propagation in various acoustic / porous stratified media coupling configurations. It presents the theoretical developments of a semi-analytical method, its validation for a limit test-case half-space ground, and an extension to a realistic multilayered seabed, when spherical waves are emitted from a transient point source in water.
Keywords: Stratified poroelastic seabed, Spherical acoustic wave, Axisymmetric geometry, Hankel-Fourier transforms.
1. Introduction
1
The study of wave propagation in seawater-seabed coupling configurations
2
is of interest for underwater acoustics and civil engineering [1, 2, 3]. On
3
the one hand, the acoustic equation models the physical phenomenon in the
4
seawater part, and on the other hand, the Biot equations describe the seabed
5
∗
Corresponding author
Email address: [email protected] (Arnaud Mesgouez)
part [4, 5]. In such problems, several boundary conditions between the fluid
6
and the top porous layer can be used to model hydraulic exchanges [1, 6, 7].
7
The proposed study focuses on transient wave propagation in a multi-region
8
medium composed of a fluid half-space representing seawater over a stratified
9
poroelastic medium representing the seabed. The source is located within the
10
seawater part and emits spherical transient waves. The purpose is to provide
11
a semi-analytical approach to solve this coupled problem in an axisymmetric
12
configuration.
13
Configurations are often restricted to 2D Cartesian geometries. Three-
14
dimensional Green’s function in axisymmetric configurations was first devel-
15
oped by [8] for an acoustic point source located near a half-space poroelastic
16
seabed. Nevertheless, the study was restricted to half-space situations.
17
Focusing on the stratified aspect of the problem, the strategies usually
18
adopted are based on transfer matrix, stiffness matrix or transmission and
19
reflexion matrix methods. The main difficulty deals with the conditioning
20
of matrices, that can be overcome using specific techniques [9]. These meth-
21
ods historically developed for electromagnetic and then viscoelastic problems
22
have been extended to poroelastic media. These developments have been pro-
23
posed for 2D Cartesian geometries with a free surface [9, 10] and then with a
24
coupling with a seawater interaction [11]. In the present article, we propose
25
to extend the previous work to an axisymmetric geometry and to couple the
26
stratified poroelastic medium to a fluid one. Thus, this work can be used
27
as benchmark solutions for numerical approaches, or for comparisons with
28
experimental results. Moreover it represents the first step of the Boundary
29
Element Method. The axisymmetric approach is based on Hankel-Fourier
30
transforms, providing thus an analytical matrix system for the fluid pressure
31
/ stresses / displacements / velocities in the frequency-wavenumber domain.
32
To obtain results in the time and space domain, integrations are then per-
33
formed numerically.
34
The paper is organized as follows. Section 2 describes the geometry under
35
study, and proposes analytical solutions to the acoustic equation and Biot
36
equations in the context of multilayered medium and axisymmetric geometry.
37
Section 3 presents a test case to validate the results by a comparison with
38
those of [8], and illustrates both the stratified aspect of the ground and the
39
interface with the seawater.
40
2. Model formulation
41
2.1. Geometry under study
42
The configuration under investigation is a fluid half-space Ω
0over a stack
43
of homogeneous and isotropic poroelastic layers Ω
n(n = 1, · · · , N ), as shown
44
in Fig. 1. The z geometrical axis points upward. The N plane and parallel
45
interfaces are located at z
n≤ 0, with z
0= 0. An acoustic point source
46
O
s( r
s= 0 ; z
s> 0) in the fluid emits transient spherical waves.
47
2.2. Multilayered porous medium
48
The poroelastic media are modeled using the Biot theory [1, 4, 5]. For
homogeneous and isotropic layers, the physical parameters do not depend
on the spatial coordinates and can be listed as follows: for the saturating
fluid, dynamic viscosity η and density ρ
f; for the elastic skeleton, density ρ
sand shear modulus µ as well as connected porosity φ, tortuosity a, absolute
permeability κ, Lam´ e coefficient of the dry matrix λ, and two Biot coeffi- cients β and m. Based on the constitutive equations and the conservation of momentum in porous media, one obtains
σ = (λ ∇.u − β p) I + 2 µ ε, (1a)
p = −m (β ∇.u + ∇.w) , (1b)
∇ σ = ρ¨ u + ρ
fw, ¨ (1c)
−∇ p = ρ
fu ¨ + a ρ
fφ w ¨ + η
κ Υ ∗ w, ˙ (1d)
where u, U and w = φ (U − u) are the solid displacement, the fluid displace- ment and the relative displacement vectors, respectively. I is the identity tensor, σ is the stress tensor, ε = 1/2 (∇ u + ∇
tu) is the strain tensor, and p is the pore pressure. ρ = φ ρ
f+ (1 − φ) ρ
sis the total density. The overlying dot denotes the derivative in terms of time t. ∗ stands for a convolution product in time. The quantity η
κ Υ ∗ w ˙ corresponds to the time domain drag force between the porous skeleton and the pore fluid [12, 13]. Expression for Υ ∗ w ˙ depends on the frequency range involved. In the low-frequency range, the relative motion between the fluid and the porous skeleton is of Poiseuille type, and then the expression is given by
Υ(t) = δ(t) ⇔ Υ(t) ∗ w(t) = ˙ ˙ w(t)
In the high-frequency range, the relative motion between the fluid and the
porous skeleton is dominated by the inertial effects. We adopt here the well-
known model proposed by [14] and written in the frequency domain. The
expression in the time domain is given in [13, 15] with the following form for
the convolution product
Υ(t) ∗ w(t) = ˙ 1
√ Ω (D + Ω)
1/2w(t) ˙ where Ω =
ωJKDχwith ω
JKD=
aκρηφf
the transition radial frequency between
49
the low- and high-frequency ranges. χ is the Pride number. The operator
50
(D + Ω)
1/2is a shifted order 1/2 fractional derivative. Note that the drag
51
force depends on the entire history of ˙ w(t).
52
Pressure and stress components are eliminated from Eqs. (1a)-(1b) and substituted in Eqs. (1c)-(1d), giving a (u, w) second-order wave formulation [9, 10]. By introducing the Helmholtz potentials for the solid (ϕ, Ψ) and relative (ϕ
r, Ψ
r) displacements, the wave formulation yields a system of partial differential equations associated to these potentials as follows
−µ (∆ψ
θ− ψ
θr
2) + ((1 − φ)ρ
s+ φρ
f) ¨ ψ
θ+ ρ
fψ ¨
θr= 0, (2a) ρ
fψ ¨
θ+ a ρ
fφ
ψ ¨
rθ+ η κ
√ 1
Ω (D + Ω)
1/2ψ ˙
rθ= 0, (2b) (λ + 2µ + m β
2) ∆ϕ + m β ∆ϕ
r− ρ ϕ ¨ − ρ
fϕ ¨
r= 0, (2c) m β ∆ϕ + m ∆ϕ
r− ρ
fϕ ¨ − a ρ
fφ ϕ ¨
r− η κ
√ 1
Ω (D + Ω)
1/2ϕ ˙
r= 0. (2d) Note that when projecting in the axisymmetric geometry, only the θ coordi-
53
nate is useful for the vector potentials: Ψ = ψ
θ(r, z, t) e
θ.
54
For an axisymmetric configuration, it is relevant to introduce the n th or-
55
der Hankel (or Fourier-Bessel) transform over the r variable, and the Fourier
56
transform over the t variable, of an integrable function f , defined as follows
57
[16]
58
f e
n(ξ) = Z
+∞0
rf (r)J
n(ξr)dr and f
∗(ω) = 1 2π
Z
+∞−∞
f (t)e
+iωtdt, (3)
where ξ is the transform Hankel parameter, ω the radial frequency and J
n59
the nth order Bessel function of the first kind.
60
In the following, we perform a Fourier transform in time of Eqs. (2a)-(2b)-
61
(2c)-(2d). Then, 0th- and 1st-order Hankel transforms are applied to the
62
scalar and vector potentials, respectively. From equation (2b), a proportion-
63
ality relation between ψ f
θr∗1(ξ, z, ω) and ψ f
θ∗1(ξ, z, ω) is obtained
64
f ψ
θr∗1(ξ, z, ω) = − ρ
fω a ρ
fω
φ + i η
κ Υ
∗(ω) ψ f
θ∗1(ξ, z, ω) = G
∗(ω) f ψ
θ∗1(ξ, z, ω). (4) Then, the introduction of the above relation in the doubly transformed do-
65
main formulation of Eq. (2a) provides the partial differential equation rela-
66
tive to the S shear wave
67
∂
2ψ f
θ∗ 1
∂z
2(ξ, z, ω)+
ω
2µ ((1 − φ)ρ
s+ (φ + G
∗(ω)ρ
f)) − ξ
2ψ f
θ∗1(ξ, z, ω) = 0. (5) Similarly, relative and absolute scalar potentials are linked by
68
ϕ e
r∗0j(ξ, ω) = ρ
fω
2− m β(k
P2j
+ ξ
2) m(k
P2j
+ ξ
2) − a ρ
fω
2φ − i η ω κ Υ
∗(ω)
ϕ e
∗0j(ξ, ω) = f F
j∗(ξ, ω) ϕ e
∗0j(ξ, ω), (6) where j = 1, 2. The formulation of Eqs. (2c) and (2d) in the doubly trans-
69
formed domain results in two coupled partial differential equations relative
70
to the P
1and P
2compressional waves, defined as
71
∂
2∂z
2− ξ
2K
P+ ω
2M + i ω C
Φ e
∗0= 0, (7)
where Φ e
∗0=
ϕ e
∗0(ξ, z, ω) ϕ e
r∗0(ξ, z, ω)
, stiffness, mass and damping matrices being
72
respectively
73
K
P=
λ + 2µ + mβ
2mβ
mβ m
, M =
ρ ρ
fρ
faρ
fφ
, C =
0 0
0 η κ Υ
∗(ω)
. (8) From Eqs. (5) and (7), we introduce global wavenumbers k
Sand k
Pjby the
74
relations k
S2= k
2zS+ ξ
2=
ωµ2((1 − φ)ρ
s+ (φ + G
∗(ω)ρ
f)) and k
P2j= k
z2Pj+
75
ξ
2. k
zS, k
zPjand ξ are the associated vertical wavenumbers and the radial
76
wavenumber, respectively. Applying the Fourier transform over the z variable
77
defined as follows
78
f (k
z) = 1 2π
Z
+∞−∞
f(z)e
−ikzzdz (9)
to system (7), yields the dispersion relation when the determinant of matrix is
79
equal to zero. Then, the general solution relative to the solid phase Helmholtz
80
potentials of system (5)-(7) can be written as
81
f ψ
θ∗1(ξ, z, ω) = f ψ
θ∗I1(ξ, ω)e
−ikzSz+ ψ f
θ∗R1(ξ, ω)e
ikzSz, (10)
82
ϕ e
∗0(ξ, z, ω) = ϕ e
∗I01(ξ, ω)e
−ikzP1z+ ϕ e
∗R01(ξ, ω)e
ikzP1z+ ϕ e
∗I02(ξ, ω)e
−ikzP2z+ ϕ e
∗R02(ξ, ω)e
ikzP2z, (11) where I and R state the ‘incident’ (or downward) and the ‘reflected’ (or
83
upward) waves, respectively.
84
The choice of an upward (z) axis, implies that the conditions =m{k
zS} ≥ 0
85
as well as =m{k
zPj} ≥ 0 (j = 1, 2) should be satisfied to have a bounded
86
field far away from the ground surface (z −→ −∞).
87
Besides, for an axisymmetric geometry
88
u e
r∗1
(ξ, z, ω) = − ξ ϕ e
∗0(ξ, z, ω) − ∂f ψ
θ∗1∂z (ξ, z, ω), (12)
89
u e
∗z0(ξ, z, ω) = ∂ ϕ e
∗0∂z (ξ, z, ω) + ξ f ψ
θ∗1(ξ, z, ω). (13) Obviously, analogous expressions are obtained for the radial and vertical relative displacement components of vector w by substituting Helmholtz po- tentials for the solid displacement by relative ones.
Then, the expressions of u e
r∗1and u e
z∗0as functions of the scalar ‘incident’ and
‘reflected’ Helmholtz potentials, are obtained from Eqs. (10)-(11) substituted in Eqs. (12)-(13). The same developments are performed for w f
r∗1and w f
z∗0with relative Helmholtz potentials. In the present axisymmetric configura- tion, the exact stiffness matrix approach is based on vectors of transformed displacement and stress components [9, 10], defined as
e u
∗= ( u e
r∗1, i u e
z∗0, i w f
z∗0)
t, Σ e
∗= ( σ f
rz∗1, i σ f
zz∗0, − i p e
∗0)
t.
By using matrix notations, after setting Φ e
∗I/R= ( ϕ e
∗I/R01, ϕ e
∗I/R02, f ψ
θ∗I/R1)
t, one
90
can deduce
91
u e
∗(ξ, z
n−1, ω) e u
∗(ξ, z
n, ω)
=
Mat
IMat
RZ Mat
IZ Mat
R
Φ e
0∗I(ξ, ω) Φ e
0∗R(ξ, ω)
, (14)
where Φ e
0∗I/Rare modified potentials to have a better conditioning of Eq.
92
(14) [9]. Mat
I/R= h
mat
I/Rpqi
; p = 1, 2, 3 ; q = 1, 2, 3 with
93
94
mat
I/R11= mat
I/R12= −ξ; mat
I13= −mat
R13= + i k
zS; mat
I21= −mat
R21= + k
zP1; mat
I22= −mat
R22= + k
zP2;
mat
I/R23= + i ξ; mat
I31= −mat
R31= + k
zP1f F
1∗(ξ, ω);
mat
I32= −mat
R32= + k
zP2f F
2∗
(ξ, ω); mat
I/R33= + i ξG
∗(ω).
95
96
Z = Diag[e
ikzP1hn, e
ikzP2hn, e
ikzShn] where Diag represents the terms of a diag-
97
onal matrix. h
n= z
n−1− z
n> 0 is the height of a specific layer “n” bordered
98
by the upper and the lower depth coordinates, z
n−1and z
n, respectively.
99
Using the Biot behaviour law, stress components can be expressed in
100
terms of transformed displacements
101
σ f
rz∗
1
(ξ, z, ω) = µ ∂ u e
r∗1
∂z (ξ, z, ω) − ξ u e
z∗0
(ξ, z, ω)
, (15)
102
σ f
zz∗0(ξ, z, ω) = (λ + m β
2) ξ u e
r∗1(ξ, z, ω) + (λ + 2µ + m β
2) ∂ u e
z∗0∂z (ξ, z, ω) + m β ξ w f
r∗
1
(ξ, z, ω) + m β ∂ w f
z∗ 0
∂z (ξ, z, ω). (16)
Besides, regarding the pore pressure, the equivalent of Eq. (1b) in the doubly
103
transformed domain is
104
p e
∗0(ξ, z, ω) = − m
β
ξ u e
r∗1(ξ, z, ω) + ∂ u e
z∗0∂z (ξ, z, ω)
+ ξ f w
r∗1(ξ, z, ω) + ∂ w f
z∗0∂z (ξ, z, ω)
. (17)
Then, the relation between stresses and Helmholtz potentials is given by
105
Σ e
∗(ξ, z
n−1, ω)
− Σ e
∗(ξ, z
n, ω)
=
S
IS
RZ -S
IZ -S
R
Φ e
0∗I(ξ, ω) Φ e
0∗R(ξ, ω)
, (18)
where S
I/R= h s
I/Rpqi
; p = 1, 2, 3 ; q = 1, 2, 3 with
106
107
s
I11= −s
R11= + 2 i µξk
zP1; s
I12= −s
R12= + 2 i µξk
zP2; s
I/R13= +µ(k
z2S− ξ
2); s
I21= s
R21= − i [(k
z2P1+ ξ
2)(λ+
m β
2+ m βf F
1∗(ξ, ω)) + 2µk
z2P1];
s
I22= s
R22= − i [(k
z2P2+ ξ
2)(λ+
m β
2+ m βf F
2∗(ξ, ω)) + 2µk
z2P2]; s
I23= −s
R23= + 2µξk
zS; s
I/R31= − i m(k
2zP1+ ξ
2)(f F
1∗
(ξ, ω) + β);
s
I/R32= − i m(k
2zP2+ ξ
2)(f F
2∗(ξ, ω) + β); s
I/R33= 0.
108
109
Finally, analytical expressions for transformed displacement vectors are
110
written in condensed form as
111
T
layern6×6
e u
∗(ξ, z
n−1, ω) e u
∗(ξ, z
n, ω)
=
Σ e
∗(ξ, z
n−1, ω)
− Σ e
∗(ξ, z
n, ω)
. (19)
A conventional assembling technique between the layers is then performed
112
[17, 18]. As [T
layern] is a 6 × 6 matrix, the global resulting matrix system has
113
dimension 3(N + 1) × 3(N + 1).
114
2.3. Acoustic medium
115
This part presents the analytical model formulation of wave propagation
116
coming from an acoustic point source applied at O
s(Fig. 1), in the water
117
semi-infinite domain Ω
0, characterized by celerity of waves c and by density
118
ρ
f, assumed to be the same as in the porous media Ω
n.
119
The acoustic equations are written as follows
U(r, z, t) = ¨ − 1
ρ
f∇p(r, z, t), (20a)
∆ p(r, z, t) − 1
c
2p(r, z, t) = ¨ −s(r, z, t) = −S(t) δ(r − r
s) δ(z − z
s)(20b)
where p is the acoustic pressure, U is the fluid displacement and s(r, z, t) is
120
the impulse transient superpressure emitted from point O
s. S(t) is a causal
121
source term and δ is the Dirac function.
122
In the following, we introduce the fluid global wavenumber k
f, linked to its
123
vertical (k
zf) and radial (ξ) components by k
2f= k
2zf+ ξ
2=
ωc22, and use the
124
mathematical property
125
e δ
0(ξ) = Z
+∞0
rδ(r)J
0(ξr)dr = 1
2π . (21)
Then, the partial differential equation relative to the pressure wave is ob-
126
tained from the formulation of Eq. (20b) in the Fourier and 0th-order Hankel
127
transform domain, as
128
∂
2e p
∗0∂z
2(ξ, z, ω) + k
zf2e p
∗0(ξ, z, ω) = − S
∗(ω)
2π δ(z − z
s). (22) The solution to the above inhomogeneous equation results in the summation
129
of two components:
130
- the complementary part f p
C∗0(ξ, z, ω) corresponding to the solution of the
131
homogeneous equation associated to Eq. (22),
132
- the principal part p f
P∗0(ξ, z, ω) which is a specific solution of Eq. (22).
133
On the one hand, the complementary part of the solution is given by
134
f p
C∗0(ξ, z, ω) = P e
∗(ξ, ω)e
ikzfz+ Q e
∗(ξ, ω)e
−ikzfz, (23) P e
∗(ξ, ω) and Q e
∗(ξ, ω) being the amplitudes, Q e
∗(ξ, ω) = 0 and =m(k
zf) > 0
135
to satisfy the convergence condition when z −→ +∞.
136
On the other hand, the calculation of the principal part of the solution is
137
inspired by [19, 20]. Concisely, the key steps are:
138
(i) Setting the principal part of the solution as a simple Fourier integral
139
expression
140
f p
P∗0(ξ, z, ω) = Z
+∞−∞
A(κ
z) e
iκzzdκ
z. (24) (ii) Searching function A(κ
z) by introducting Eq. (24) in Eq. (22), multi-
141
plying the obtained equation by e
−iκzz(where κ
z∈ R ), integrating over the
142
z variable from - ∞ to + ∞, and using some mathematical properties of the
143
Dirac function to obtain
144
A(κ
z) = − S
∗(ω) (2π)
2e
−iκzzsk
zf2− κ
z2. (25)
(iii) Rewriting the principal part of the solution gives
145
f p
P∗0(ξ, z, ω) = S
∗(ω)
(2π)
2I(z − z
s, k
zf), (26) where [19]
146
I(z − z
s, k
zf) = Z
+∞−∞
e
iκz(z−zs)k
zf2− κ
z2dκ
z= ± i π e
i±kzf|z−zs|k
zf. (27)
(iv) Finally obtaining the single physically valid solution, satifying the Som-
147
merfeld condition [20]
148
149
f p
P∗0(ξ, z, ω) = i S
∗(ω) 4π
e
ikzf|z−zs|k
zf. (28)
Solution (28) corresponds to the one obtained in [8, 20]. Indeed, these authors
150
provide a Green’s function as a solution of a cylindrical Helmholtz equation,
151
which corresponds to the Fourier transform in time of Eq. (20b). Then, they
152
calculate f p
P∗0(ξ, z, ω) by using a Sommerfeld integral decomposition of the
153
simply transformed domain solution.
154
2.4. Interface equations
155
The geometry under study leads to a set of interface equations along the
156
N plane interfaces z
n(n = 0, · · · , N − 1). For this purpose, we denote [g]
n157
the jump in a function g from Ω
nto Ω
n+1across z
nas
158
[g]
n= lim
ε→0,ε>0
g(r, z
n+ ε, t) − lim
ε→0,ε>0
g(r, z
n− ε, t)
= (g)
+n− (g)
−n.
(29)
- The porous / porous interfaces z
n(n = 1, · · · , N − 1) are assumed to be in
159
perfect bonded contact [1]
160
[u
r(r, z, t)]
n= 0, [u
z(r, z, t)]
n= 0, [w
z(r, z, t)]
n= 0,
[σ
rz(r, z, t)]
n= 0, [σ
zz(r, z, t)]
n= 0, [p(r, z, t)]
n= 0. (30) - The fluid / porous interface z
0= 0 is modeled with the following interface conditions [1, 6, 7]
(u
z(r, z, t))
−0+ (w
z(r, z, t))
−0= (U
z(r, z, t))
+0, (31a)
(σ
rz(r, z, t))
−0= 0, (31b)
(σ
zz(r, z, t))
−0= −(p(r, z, t))
+0, (31c)
−[p(r, z, t)]
0= 1
K ( ˙ w
z(r, z, t))
−0. (31d) where K is the hydraulic permeability of the interface. The case K → +∞
161
describes open pores. For K → 0, Eq. (31d) is replaced by ( ˙ w
z(r, z, t))
−0=
162
0, stating sealed pores. An intermediate state for K ∈ ] 0 ; +∞[ describes
163
imperfect pores.
164
The formulation of the fluid /porous interface equations (31a)-(31c)-(31d)
165
in the doubly transformed domain enables both to determine the amplitude
166
P e
∗(ξ, ω) of the ‘reflected’ pressure wave in the fluid, and as a result to provide
167
the following matrix block
168
− i ρ
fω
2k
zf− i ρ
fω
2k
zf− i ρ
fω
2k
zf− i ρ
fω
2k
zf− i ω
K
i ( u e
z∗0(ξ, z, ω))
−0i ( w f
z∗0(ξ, z, ω))
−0
=
− i ( σ f
zz∗
0
(ξ, z, ω))
−0+ S
∗(ω) 2 π e
ikzfzsk
zfi ( p e
∗0(ξ, z, ω))
−0+ S
∗(ω) 2 π e
ikzfzsk
zf
. (32)
Eq. (32) is assembled to Eq. (19) to give the radial and vertical solid and
169
relative displacements at each interface. The transformed displacements,
170
stresses, velocities and acoustic pressure everywhere inside each domain Ω
n171
can then be obtained analytically. The latter quantities are subsequently
172
calculated in the spatio-temporal domain by means of inverse Hankel-Fourier
173
transforms. For example, the acoustic or pore pressure can be written as
174
follows
175
p(r, z, t) = Z
+∞0
2 <e
Z
+∞0
ξ p e
∗0(ξ, z, ω)J
0(ξr)dξ
e
−iωtdω (33)
The integral over the radial wavenumber, which presents an oscillatory be-
176
havior due to factor J
0(ξr) and for which the envelope of the maximum am-
177
plitudes shows sharp peaks, is performed using an adaptive Filon quadrature,
178
[21, 22]. The adaptive procedure consists in dividing the entire interval into
179
several parts based on what is known about p e
∗0(ξ, z, ω). Because of the sharp
180
changes in the integrand occurring around the wavenumbers of the propagat-
181
ing waves, the wavenumbers are calculated and sorted out. The quadrature
182
is performed by discretizing finely in their neighborhood and more coarsely
183
farther away. The integral is truncated depending on the highest wavenum-
184
ber and adapted to each frequency. As for the numerical processing over ω,
185
the quadrature is done using a Simpson scheme. Numerical values used for
186
the various discretizations are those of [11].
187
3. Results and discussion
188
In this section, we propose firstly to validate the above theoretical for-
189
mulation by using a half-space porous medium such as in [8]. To do that,
190
we consider a limit test-case of the stratified configuration, composed of two
191
layers presenting the same physical properties. Once the semi-analytical ap-
192
proach validated, we present new results coming from a seabed [23, 24] made
193
of ten layers presenting various properties, as an extension of the half-space
194
porous ground.
195
3.1. Half-space test-case configuration
196
Porous and fluid parameters are [8]: λ = 10.0 × 10
9Pa, µ = 5.0 × 10
9Pa, ρ
s= 2.5 × 10
3kg.m
−3, ρ
f= 1.0 × 10
3kg.m
−3, a = 3, β = 0.7, m = 10.0 × 10
9Pa, φ = 0.33, η = 1.0 × 10
−3Pa.s, κ = 10
−8m
2as well as,
Υ
∗(ω) = 1 + i ω
Ω
1/2, Ω = η φ
a κ ρ
fχ with χ = 0.5 [14].
In the water domain Ω
0: ρ
f= 1.0 × 10
3kg.m
−3, c = 1414.0 m.s
−1.
197
The emission point source is located at z
s= 10 m and the observation ones
198
are pointed by r = 20 m and z = ± 20 m. Such as in [8], S(t) is a Ricker
199
wavelet and S
∗(ω) its Fourier transform
200
S(t) = ((1 − 2 ˆ α
2(t − β) ˆ
2)e
−ˆα2(t−β)ˆ2and S
∗(ω) = ω
24 ˆ α
3√
π e
(i ˆβω−ω2 4 ˆα2)
, (34)
where ˆ α = ω
0/2 and ˆ β = t
s, ω
0= 2πf
0(f
0= 1.0 × 10
3Hz) and t
s= 2.5 ×
201
10
−3s being, respectively the central angular frequency and a shift in time.
202
As regards time evolution of pore pressure and fluid pressure, Fig. 2 shows
203
that there is an excellent agreement between the results proposed by [8] and
204
those obtained from our calculations. Both in permeable and impermeable
205
cases, it checks the validity of the analytical approach in the half-space limit
206
test-case.
207
3.2. Extension to a stratified poroelastic seabed
208
The regarded configuration is built from mechanical data taken from [23, 24]. It corresponds to a more realistic description of a seabed. To model the stratified ground and to illustrate the capabilities of our approach, we have chosen a ten layer geometry coupled to a half-space configuration. In the porous medium, the unchanged parameters are: a = 1.25, ρ
s= 2.65 × 10
3kg.m
−3as well as the compressibility of the solid skeleton, χ
s= 36 GPa, and of the fluid volume, χ
f= 2 GPa. The Lam´ e constants are linked in this study by λ = 2µ. Ranges of physical characteristics from the first layer to the half-space are: φ ∈ [0.5 ; 0.2], κ ∈ [10
−9; 10
−12] m
2and µ ∈ [10
7; 10
9] Pa. From one stratum to another, only one of these three parameter values is modified as indicated in Tab. 1, as well as the related ones. The two Biot coefficients β and m are given by
β = 1 − χ
oχ
s, 1
m = β − φ χ
s+ φ
χ
f, where χ
o= λ + 2 3 µ.
Parameters relative to the nature of the point source and to the water are
209
the same as for the half-space test-case situation, the only differences are:
210
z
s= 5 m and the observation points are located at r = 1 m and z = ± 1 cm
211
or z = − 80 cm.
212
213
Layer n Height Porosity Absolute Shear
h
n(m) φ permeability κ (m
2) modulus µ (Pa)
n = 1 0.1 0.5 1 × 10
−91 × 10
7n = 2 0.1 0.5 1 × 10
−95 × 10
7n = 3 0.4 0.4 1 × 10
−95 × 10
7n = 4 0.4 0.4 5 × 10
−105 × 10
7n = 5 1.0 0.4 5 × 10
−101 × 10
8n = 6 1.0 0.3 5 × 10
−101 × 10
8n = 7 2.0 0.3 1 × 10
−111 × 10
8n = 8 5.0 0.3 1 × 10
−115 × 10
8n = 9 5.0 0.2 1 × 10
−115 × 10
8n = 10 10.0 0.2 1 × 10
−111 × 10
9Half-space + ∞ 0.2 1 × 10
−121 × 10
9Table 1: Height of each layer and parameter values changing from one layer to another in the seabed
Firstly, Fig. 3 shows very similar time evolutions of fluid pressure at z = 1 cm observation height, both for sealed, imperfect and open pore in- terfaces between seawater and seabed. This means that the nature of the contact does not have any influence on the fluid pressure for the configu- ration under study. Secondly, considering only the impermeable cases, Fig.
3 emphasizes the fact that the properties of the first layer force the fluid
pressure behaviour in the seabed when observation point is very close of the z
0= 0 interface. Thirdly, central arrival time of the acoustic compressional wave is given by
t
f=
p (z
s− z)
2+ r
2c + t
s= 6.1 ms.
214
In contrast, Fig. 4 clearly proves that the hydraulic permeability coefficient
215
value has a strong impact on temporal variation of the vertical displacement
216
at z = − 1 cm observation height, in the first layer of the seabed. Note
217
that this trend is very attenuated when considering stresses in the seabed,
218
not shown here.
219
Besides the comparison beween Fig. 4 and Fig. 5 highlights the multiple
220
wave reflections at the porous / porous intefaces in the seabed. In addition,
221
the confrontation between half-space and multilayered results yields higher
222
differences in the intermediate case than those obtained in the extreme situ-
223
ations.
224
In the fourth layer, at z = − 80 cm observation height (Fig. 6), the nature
225
of the contact does not have influence on the first displacement peaks any
226
more. This time, the differences due to the kind of hydraulic interface is seen
227
on the part of the response relative to the reflection waves (t > 9 ms).
228
4. Conclusions
229
An axisymmetric model of wave propagation in poroelastic / acoustic
230
configurations, has been presented, validated and extended by using a semi-
231
analytical method. The theoretical development has been based on a matrix
232
block assembling technique for the porous layers and the fluid domain and
233
takes into account various interface conditions. A half-space porous ground
234
as a limit test-case of our multilayered medium has been considered to vali-
235
date the analytical model. Indeed, regarding pore and fluid pressures, there
236
is a very good agreement between the results coming from [8] and our calcu-
237
lations, whatever the pore nature. Then, the approach has been applied to
238
a stratified seabed, as an extension of the half-space porous soil, providing
239
new results which emphasize the variations in time of mechanical quantities.
240
From the obtained displacements and stresses, a future investigation con-
241
sists in estimating mechanical and hydrological parameters of the systems
242
under study. In parallel, the results could be compared to those issuing
243
from finite difference, element and/or volume approaches or other analytical
244
formulations such as transfer or transmission and reflexion matrices.
245
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1868.
314
z
e
re
θe
zO
y
Os r = 0 z > 0 ss Ω0
Fluid
Ω1
Porous
Ω2
ΩN
Porous
Ω3
Porous z
0= 0
z
1z
2z
3z
N - 1h
1h
3Water column
bottom
θ
Porous h
2h
Nx
M
r z
Figure 1: Axisymmetric geometry used for the multilayered poroelastic / acoustic media
0 , 0 1 5 0 , 0 2 0 0 , 0 2 5 0 , 0 3 0 - 0 , 0 4
- 0 , 0 3 - 0 , 0 2 - 0 , 0 1 0 , 0 0 0 , 0 1 0 , 0 2
p e r m e a b l e c a s e ( L u e t a l .) p e r m e a b l e c a s e ( o u r c a l c u l a t i o n s ) i m p e r m e a b l e c a s e ( L u e t a l .) i m p e r m e a b l e c a s e ( o u r c a l c u l a t i o n s)
Fluid pressure (Pa)
T i m e ( s )
(a)
0 , 0 1 5 0 , 0 2 0 0 , 0 2 5 0 , 0 3 0 0 , 0 3 5 0 , 0 4 0
- 0 , 0 1 0 0 - 0 , 0 0 7 5 - 0 , 0 0 5 0 - 0 , 0 0 2 5 0 , 0 0 0 0 0 , 0 0 2 5 0 , 0 0 5 0 0 , 0 0 7 5
Pore pressure (Pa)
T i m e ( s ) p e r m e a b l e c a s e ( L u e t a l .) p e r m e a b l e c a s e ( o u r c a l c u l a t i o n s ) i m p e r m e a b l e c a s e ( L u e t a l .) i m p e r m e a b l e c a s e ( o u r c a l c u l a t i o n s)
(b)
Figure 2: Time evolution of fluid pressure (up) and pore pressure (down) for permeable
and impermeable cases, obtained by [8] and our calculations
0.000 0.001 0.002 0.003 0.004 0.005 0.006 0.007 0.008 0.009 0.010 -0.020
-0.015 -0.010 -0.005 0.000 0.005 0.010
Fluid pressure (Pa)
Time (s)
Seabed: permeable case Seabed: intermediate case Seabed: impermeable case
Half-space: impermeable case
Figure 3: Time evolution of fluid pressure at z = 1 cm observation height, for permeable
and intermediate (K = 5 × 10
−10m.s
−1.Pa
−1) cases in the seabed configuration, and for
impermeable case in both the seabed and the half-space corresponding situation
0 . 0 0 0 0 . 0 0 2 0 . 0 0 4 0 . 0 0 6 0 . 0 0 8 0 . 0 1 0 - 1 . 0 x 1 0- 1 2
- 5 . 0 x 1 0- 1 3 0 . 0 5 . 0 x 1 0- 1 3 1 . 0 x 1 0- 1 2
Vertical displacement inΩ1 (m)
T i m e ( s )
S e a b e d : p e r m e a b l e c a s e S e a b e d : i n t e r m e d i a t e c a s e S e a b e d : i m p e r m e a b l e c a s e
Figure 4: Time evolution of vertical displacement in the first layer at z = − 1 cm obser-
vation height, for permeable, intermediate (K = 5 ×10
−10m.s
−1.Pa
−1) and impermeable
cases in the seabed configuration
0 . 0 0 0 0 . 0 0 2 0 . 0 0 4 0 . 0 0 6 0 . 0 0 8 0 . 0 1 0 - 1 . 0 x 1 0- 1 2
- 5 . 0 x 1 0- 1 3 0 . 0 5 . 0 x 1 0- 1 3 1 . 0 x 1 0- 1 2
Vertical displacement inΩ1 (m)
T i m e ( s )
H a l f - s p a c e : p e r m e a b l e c a s e H a l f - s p a c e : i n t e r m e d i a t e c a s e H a l f - s p a c e : i m p e r m e a b l e c a s e
Figure 5: Time evolution of vertical displacement in the half-space corresponding situation
to that of Fig. 3
0 . 0 0 0 0 . 0 0 2 0 . 0 0 4 0 . 0 0 6 0 . 0 0 8 0 . 0 1 0 0 . 0 1 2 0 . 0 1 4 - 8 . 0 x 1 0- 1 3
- 6 . 0 x 1 0- 1 3 - 4 . 0 x 1 0- 1 3 - 2 . 0 x 1 0- 1 3 0 . 0 2 . 0 x 1 0- 1 3 4 . 0 x 1 0- 1 3 6 . 0 x 1 0- 1 3
Vertical displacement inΩ4 (m)
T i m e ( s )
S e a b e d : p e r m e a b l e c a s e S e a b e d : i n t e r m e d i a t e c a s e S e a b e d : i m p e r m e a b l e c a s e