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Dispersion Formula of Rayleigh Wavesjoint work with
Chi-Sing Man (Univ. of Kentucky)
Kazumi Tanuma (Gunma Univ.).
Gen Nakamura
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1. Introduction
NDT(nondestructive testing) using ultrasound(i.e. elastic waves)
Rayleigh wave(R-wave)propagate along the free boundary
speed < speed of body waves (i.e. subsonic)
elliptically polarized
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Chi-Sing Man et al
dispersion formula of the speed of R-wave
i.e. v(k) = v0 +1
kv−1 + · · ·
under the conditions:
flat boundary
material is only depth dependent
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?
- free surface
homogeneous isotropic mediumwith residual stress
Assumptions:
residual stress
T depends only on the depth z
all components of the residual stress vanish except
T 11(z) = σ1(z),
T 22(z) = σ2(z)
Consider Rayleigh wave propagating along the surface in
the 1-direction.
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Constitutive Equation
σ =
T + C[E] + D[
T ,E]
=
T + λ(tr E)I + 2µE
+β1(tr E)(tr
T )I + β2(tr
T )E
+β3((tr E)
T + (tr E
T )I) + β4(E
T + TE)
σ second Piola-Kirchhoff stressT residual stressE infinitesimal strain tensorI second-order identify tensorC fourth-order elasticity tensor
D sixth-order acoustoelastic tensor bilinear inT and E
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High-Frequency Asymptotics
v − v0
v0
= K11σ1(0) + K12σ2(0)
+1
k(H11σ
′1(0) + H12σ
′2(0))
+O
(
1
k2
)
k wave numberv phase velocity of Rayleigh wavev0 phase velocity of Rayleigh wave when σ1 = σ2 ≡ 0Hij ,Kij acoustoelastic constantsσ′i(0) derivative of σi at z = 0
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Cause of the dispersion of R-wave
curved boundary
inhomogeneity
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Question:What about the cases
· curved boundary
· inhomogeneous also in the tangential direction
?
Aim of the study:Want to derive the dispersion formula of R-wave in the general
case.
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Known and related results(i) isotropic
D.Gregory (’71)homogeneous, curved boundary
(ii) anisotropicV.E. Nomofilov (’74)
general caseBut its validity is unknown
(iii) related resultG. Nakamura (’91)
necessary and sufficient condition for the existence ofR-wave for the general case
(i.e. generalized Barnett-Lothe condition)
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2. Outline of deriving the formula
methods:• semiclassical analysis
pseudodifferential operator (ΨDO)
Fourier integral operator (FIO)
• Stroh formalism
• stationary phase method
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Main steps
• Poisson operator in the elliptic region
• factorization of the operator and Neumann operator
• block diagonalization of the Neumann operator
(generalized Barnett-Lothe condition and extracting the hyperbolicpart)
• stationary phase method
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Set up
Ω ⊂ R3; domain, ∂Ω; C∞
ρ(x) ∈ C∞(Ω); density
C=(Cijkl(x)) ∈ C∞(Ω); elasticity tensor
hyperelasticity (symmetry)
strong convexity
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Step 1
flattening the boundary
x0 ∈ ∂Ω; fix
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Claim
ρ∂t2u = div(C∇u) = ∇ · (C∇u)
(C∇u)ν = 0
ν; outer unit normal vector
=⇒
ρ∂t2u = ∇ · (B∇u)
(B∇u)
−10
0
= 0
ρ := |det∇F |−1ρ etc.
B; hyperelastic, strongly convex
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Notations
ρ = ρ
Dt = −√−1∂t, Dyr = −
√−1∂yr
y′ = (y2, y3)
η1 ←→ y1, η′ = (η2, η3)←→ (y2, y3)
M = ρDt2 + L
Lu = −D · (BDu)(analogous to ∇ · (C∇u))
The rest of the arguments are microlocalized to t = 0, y1 = 0, y′ = 0,
η′ = η0′
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Goal
Speed of R-wave passing y′ = 0 in the direction η0′ at t = 0
= λ(0, η0′)− 1k
Reδ(y′, λ(0, η0′), η0′) ,
where
δ = δ(y′, η′, τ); positive homog. deg. 0 part of the symbol of D11(k)
D11(k); (1, 1) block of the diagonalized symbol of Neumann operator
σ(D11(k)) = k(τ − λ(y′, η′))
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Step 2Construction of Poisson operator P(k):
(P (k)g)(t, y) = (k
2π)3∫∫
e√−1k(t−s)τ+(y′−z′)·η′P (t, y, τ, η′, k)
g(s, z′, τ, η′)dsdz′dτdη′(ΨDO)
M(P (k)g)(t, y) = O(k−∞) and C∞
(P (k)g)|y1=0 = g
(t, y′, τ, η′) ∈ ε; elliptic region
i.e. det(ρτ 2δij −3∑
j,l=1
Bijklηjηl)|y1=0 6= 0 (η1 ∈ R)
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Step 3
Computing the Neumann operator
By the factorization−M = (Dy1 −B∗(y,Dt, Dy′, k) + G0(y,Dt, Dy′, k))T (y)(Dy1 −B(y,Dt, Dy′, k))
andthe Stroh formalism,the Neumann operator N(k):
N(k)g := (B∇(P (k)g))
−1
0
0
has the principal part (i.e. principal symbol):
σ(N(k)) = k(|τ | + |η′|)Z(y′, τ, η′)
Z(y′, τ, η′); surface impedance tensor
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Z(y′, τ, η′) := −V −1(y′, τ, η′)−√−1V −1(y′, τ, η′)Y (y′, τ, η′)
V (y′, τ, η′) := −(2π)−1∫ 2π
0< ω, ω >−1 dφ
Y (y′, τ, η′) := −(2π)−1∫ 2π
0< ω, ω >−1< ω, ζ > dφ
< ζ, ω >= (< ζ, ω >ik)
< ζ, ω >ik:=3∑
j,l=1
(Bijkl − |η′|−4ρτ2ηjηlδik)ζjωl
ζ = (ζ1, ζ2, ζ3) = (sinφ, |η′|−1(cosφ)η′)ω = (ω1, ω2, ω3) = (cosφ,−|η′|−1(sinφ)η′)
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Step 4
Extracting the hyperbolic part from the Neumann operator
Assume the generalized Barnett-Lotte condition at (y′, η′) = (0, η0′):
limv↑vL(0,η0′)
Z(0, v|η0′|, η0′) < 0
or
limv↑vL(0,η0′)
(traceZ(0, v|η0′|, η0′))2 − traceZ2(0, v|η0′|, η0′) < 0
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vL(0, η0′); limiting velocity
outermost slowness curve
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By Nakamura’s result, there exists an intertwining ΨDO Ψ(k)
N(k)Ψ(k) ∼ Ψ(k)D(k)
D(k) =
[
D11(k)
0
0
D22(k)
]
; block diagonal ΨDO
σ(D11(k)) = k(τ − λ(y′, η′)),λ(y′, η′); positive homog. deg. 1, C∞, real valued
σ(D22(k))
σ(Ψ(k))
; positive homog. deg.
1
0
, C∞, invertible
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Moreover, there exists an intertwining ΨDO q(k):
D11(k)q(k) ∼ q(k)Op(σ(D11(k)))
Op(σ(D11(k))); the principal part of D11(k)
(−iHτ−λ + δ)σ(q(k)) = 0
Hτ−λ = ∂t −∇η′λ · ∇y′ +∇y′λ · ∇η′; Hamilton field of τ − λ
δ; positive homog. deg. 0 part of the symbol of D11(k)
Note that, symbolically
σ(q(k)) = e−iH−1τ−λ
δ
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Step 5
Solving Op(σ(D11(k)))h = 0 for h
h can be given by FIO aφf :
(aφf)(t, y′, k) = (k
2π)2∫∫
e√−1k(φ(t,y′,η′)−z′·η′)
a(t, y′, z′, η′)f(z′, k)dz′dη′
∂tφ− λ(y,∇y′φ) = 0 Hamilton-Jacobi eq.
φ|t=0 = y′ · η′
Dtσ(a)−∇η′λ(y′,∇y′φ)Dy′σ(a) + imσ(a) = 0
m = 12
∑
|α|=2
∂αη′λ(y′,∇y′φ)∂αy′φ
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Step 6
Summing up Step 2∼ Step 5, the solution u describing R-wave isgiven by:
u = P (k)Φ(k)
q(k)aφf
0
0
N.B.
N(k)Φ(k) ∼ Φ(k)D(k)D11(k)q(k) ∼ q(k)Op(σ(D11(k)))
Op(σ(D11(k))) aφf = 0
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Step 7
Analyze the asymptotic of u|y1=0 using the stationary phase method
Let the initial source f of R-wave be
f = eiky′·η0′
f(y′)f(y′); supported near y′ = 0
Then, the leading term of u|y1=0 is
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exp
[
ik(φ(t, y′, η0′)− k−1
∫ t
0
δ(Hs,τ (z′, ζ′), τ)ds)∣
∣
∣
∣
∣
(z′,ζ′)=H−1t,τ
(y′,η0′)
τ=φt(t,y′,η′0)
]
exp(∫ t
0
m(s, Vs,η0′(z′), η0′)ds
)∣
∣
∣
∣z′=V −1
s,η0′(y′)
f(∇η′φ(t, y′, η′0))σ(Φ(k))[1](t, y′, φt(t, y′, η0′),∇y′φ(t, y′, η0′))
where σ(Φ(k))[1]; 1 st column vector of σ(Φ(k))
(polarization vector)
m =1
2
∑
|α|=2
∂αη′λ(y′,∇y′φ)∂αy′φ
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Ht,τ : (z′, ζ′) 7−→ (y′, η′)
dy′dt
= −∇η′λ,dη′dt
= ∇y′λ
(y′, η′)|t=0 = (z′, ζ′)
Vt,η0′ : z′ 7−→ y′
dy′dt
= −∇η′λ(y′,∇y′φ(t, y′, η0′))
y′|t=0 = z′
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Speed of R-wave passing y′ = 0 in the direction η0′ at t = 0
= λ(0, η0′)− 1k
Reδ(y′, λ(0, η0′), η0′) ,
where δ = δ(y′, η′, τ); positive homog. deg. 0 part of the symbol of
D11(k)
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Conclusion and future problems
• We derived the dispersion formula in the coord.
flattening the boundary
• Have to separate the geometric and material quantities.
• Apply it to identify residual stress or texture.
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