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SURFACE WAVES JEANNOT TRAMPERT
SURFACE WAVES Most seismograms are dominated by surface waves whose energy is concentrated near the earth’s surface. Geometric spreading (energy) is in 1/r (1/r2 for body waves) Rayleigh waves are trapped P-SV energy
Love waves are trapped SH energy
Because surface waves decay slowly they circle the Earth many times. Rayleigh Rn, Love Gn
Dispersion: waves with different frequencies travel with different speeds à spread out in time
SUMATRA EARTHQUAKE
RAYLEIGH WAVE IN A HOMOGENEOUS HALFSPACE Dispersion Equation
(C2
β 2− 2)(2− C
2
β 2)+ 4β 2 1− c
2
α 2 1− c2
β 2= 0
For a Poisson solid this has one root with phase velocity c=0.914β with elliptical particle motion and no dispersion (see exercise)
LOVE WAVE IN A LAYER OVER HOMOGENEOUS HALFSPACE
1β12∂2v∂t2
= (∂2v∂x2
+∂2v∂z2), 0 < z < h
1β22∂2v∂t2
= (∂2v∂x2
+∂2v∂z2), z > h
Equation of motion For displacement v In direction y
LOVE WAVE IN A LAYER OVER HOMOGENEOUS HALFSPACE Fourier Transform equation of motion
ν i2 =
ω 2
βi2 − k
2 =ω 2
βi2 −
ω 2
c2
Trial solution
v = [Aexp(−iν1z)+Bexp(iν1z)]expi(kx −ωt), 0 < z < hv = [C exp(−iν2z)+Dexp(iν2z)]expi(kx −ωt), z > h
LOVE WAVE IN A LAYER OVER HOMOGENEOUS HALFSPACE Boundary conditions give the constants A, B, C and D To have an inhomogeneous wave at the interface β1<=c<=β2 No energy at z=∞ à D=0
No traction at z=0 à A=B
Continuity of displacement and traction at z=h
tan[ωh 1β12 −
1c2]=
µ21c2−1β22
µ11β12 −
1c2
vn = 2Acos[ω1β12 −
1cn2 z]exp[i(knx −ωt)], 0 <= z <= h
vn = 2Acos[ω1β12 −
1cn2 h]exp[−ω
1cn2 −
1β22 (z− h)]− exp[i(knx −ωt)], z >= h
LOVE WAVE IN A LAYER OVER HOMOGENEOUS HALFSPACE The relative excitation of the different modes depends on the depth and nature of the seismic source. A way to separate the modes is to observe them at large distances where they arrive at different times due to the propagation with different group velocities The group velocity at a given frequency is the velocity at which an envelope of a wave packet is transported. The peaks, troughs and zeros are transported with the phase velocity.
STATIONARY PHASE APPROXIMATION The waveform for a single mode with spectral density F(ω) and initial phase ϕ(ω) can be written as
If non-dispersive f(x,t)=f(t-x/cn) (phase is constant)
If dispersive à stationary phase approximation
f (x, t) =1/ 2π | F | expi(Φ+ωt − knx)dω−∞
+∞
∫
ddω(ωt − knx) = 0 For fixed ω has solutions when t=x/U
STATIONARY PHASE APPROXIMATION
STATIONARY PHASE APPROXIMATION Taylor expansion of the phase around ω0 gives
And
If dU/dω=0: Airy phase à higher order terms
ωt − knx =ω0t − knx +x2d 2kndω 2 (ω −ω0 )
2
f (x, t) ~| F | /π 2πx | d 2kn / dω
2 |cos(ω0t − kn (ω0 )x ±π / 4)
VARIATIONAL PRINCIPLES Hamilton’s principle: every mechanical system is defined by a Lagrangian function Satisfying is minimum Or The equations of motion are obtained by For an linear elastic body
L(q1,...,qn, q1,..., qn, t)
S = L(q, q, t)dtt1
t2∫
dS = d Ldtt1
t2∫ = (∂L∂q
dq+ ∂L∂ qt1
t2∫ d q)dt = 0
ddt∂L∂ q
−∂L∂q
= 0
L = 12ρ ui ui −[
12λ(ekk )
2 +µeijeij ]
VARIATIONAL PRINCIPLE FOR LOVE WAVES
< L >= 14ρω 2l1
2 −14µ[k2l1
2 + (dl1dz)2 ]
u = (0, l1(k, z,ω)expi(kx −ωt), 0)
(∂L∂l10
∞
∫ dl1)dz = 0
ω 2dI1 − k2dI2 − dI3 = 0 I1 =1/ 2 ρl1
20
∞
∫ dz
I2 =1/ 2 µl12
0
∞
∫ dz
I3 =1/ 2 µ(dl1dz0
∞
∫ )2dz
For a displacement The average Lagrangian is Hamilton’s principle says that Or where
VARIATIONAL PRINCIPLE FOR LOVE WAVES
ω 2I1 − k2I2 − I3Which means that
Is stationary for perturbations of the eigenfunction l1 We can further show that for an eigenfunction l1
ω 2I1 − k2I2 − I3 = 0
VARIATIONAL PRINCIPLE FOR LOVE WAVES
Which leads to three interesting applications
k2 = ω2 (I1 + dI1)− (I3 + dI3)
(I2 + dI2 )
U =dωdk
=I2cI1
dcc= −
dkk=
{[k2l12 + (dl1 / dz)
2 ]dµ −ω 2l12 dρ}dz
0
∞
∫2k2I2
VARIATIONAL PRINCIPLE FOR RAYLEIGH WAVES
Similar, but a bit more algebra (see Aki and Richards)
FUNDAMENTAL MODE SENSITIVITY KERNELS
FUNDAMENTAL MODE SENSITIVITY KERNELS
FUNDAMENTAL MODE SENSITIVITY KERNELS
NUMERICAL INTEGRATION TO FIND EIGEN-VALUES AND -VECTORS Transform wave equation (2nd order differential equation) into a first order coupled differential equation. d/dz (motion, stress)t = matrix * (motion, stress)t
à Propagator matrix f(z)=P(z,z0)f(z0)
à Trial solution (ω,k) at infinity so that stress = 0 at the surface
Rayleigh-Ritz method which uses the variational principles
l1=ΣciBi(z) and Bi verifies the BC at z=0 and z=∞
MEASURING SURFACE WAVE DISPERSION Fourier transform
F(ω) = f (t)exp(−iωt)dt−∞
+∞
∫ = Aexp(−iφ)
whereφ = k(ω)r +φs +φi
f (t) = 12π
Aexp[i(ωt − kr)]dω−∞
+∞
∫
MEASURING SURFACE WAVE DISPERSION Velocity of propagation of monochromatic wave Velocity of propagation of maximum energy
Useful relations
ωt − kr = constω(dt / dr)− k = 0tph = r / c
ddω(ωt − kr) = 0
tgr = (dk / dω)r = r /U
U = c+ k dcdk
U = c−λ dcdλ
U =c
1+ TcdcdT
PHASE VELOCITY MEASUREMENTS Sato (1955) uses FT for the first time n obvious at long periods à smooth dispersion curve Inter-station method eliminates source Cross-correlation makes phase difference numerically more stable
kr = φ −φs −φi + 2nπ
c = ω(r2 − r1)φ2 −φ1 −φi2 +φi1 + 2nπ
PHASE VELOCITY MEASUREMENTS Single-station method on world-circling paths eliminates source and instrument, for l the difference in the number of polar passages
Auto-correlation makes phase difference numerically more stable
c =
12ωlL
φ2 −φ1 + 2π (n+14l)
GROUP VELOCITY MEASUREMENTS Analytical signal associated to the seismogram
where e(t) is the envelope and Φ(t) the instantaneous phase
The measurement of U is related to its definition: we evaluate
To first order, we can show that de(t)/dt=0 if t=r/U
the maximum of the envelope corresponds to the group arrival time
s(t) = s(t)− iH (s(t)) = e(t)exp(iφ(t))
hn (t) =12π
S(ω)H (ωn,ω)exp(iωt)dω−∞
+∞
∫
AUTOMATIC WAVEFROM INVERSION FOR PHASE VELOCITY Trampert and Woodhouse, 1995 Ekstrom, Tromp and Larson, 1997
RAYLEIGH WAVE GROUP VELOCITY AT 40 S
RAYLEIGH WAVE GROUP VELOCITY AT 125 S
GREEN’S FUNCTION FOR SURFACE WAVES Solution for surface waves generated by a point force with time dependence exp(-iωt) buried at depth h. It is most useful to use a cylindrical reference frame. The derivation follows Saito (1967)
GREEN’S FUNCTION FOR SURFACE WAVES The Helmholtz decomposition separates the displacement field into P-, SV- and SH-wave components
u =∇Φ+∇×∇(0, 0,Ψ)+∇× (0, 0,Χ)Φ(r,ω) =Yk
m[Aexp(−γz)+Bexp(γz)]exp(−iωt)Ψ(r,ω) =Yk
m[C exp(−νz)+Dexp(νz)]exp(−iωt)Χ(r,ω) =Yk
m[E exp(−νz)+F exp(νz)]exp(−iωt)whereYk
m = Im (kr)exp(imϕ )
γ = ω 2
α 2 − k2
ν = ω 2
β 2− k2
GREEN’S FUNCTION FOR SURFACE WAVES The Helmholtz decomposition separates the displacement field into P-, SV- and SH-wave components, All potentials satisfy the scalar wave equation, A, B, C, D, E and F are constants
Im is the mth order Bessel function
Ykm is a horizontal wave function
We will write the wave as coupled first order differential equation df/dz A = f For Love waves f=(l1,l2)t is the motion-stress vector
GREEN’S FUNCTION FOR LOVE WAVES
uSH = (1r∂Χ∂ϕ,−∂Χ
∂r, 0)
stress+BC...u = l1(k, z,ω)Tk
m (r,ϕ )exp(iωt)T = l2 (k, z,ω)Tk
m (r,ϕ )exp(iωt)where
Tkm 1kr∂Yk
m
∂ϕr + 1
k∂Yk
m
∂rϕ
GREEN’S FUNCTION FOR LOVE WAVES Love generated by a point force at r=0 and z=h The applied for is equivalent to a discontinuity in traction
Method:
① Decompose the discontinuity in (k,m) components
② Solve df\dz A = f for each (k,m) component where f is the z-dependent motion-stress vector with the discontinuity at z=h
③ The total solution is the sum of all (k,m) components
T (h+ )−
T (h− ) = −
F exp(−iωt)∂(x)∂(y)
GREEN’S FUNCTION FOR LOVE WAVES
−F exp(−iωt)∂(x)∂(y) = exp(−iωt) / 2π k[ fT0
∞
∫m∑ (k,m)Tk
m ]dk
fT (k,1) =1/ 2(Fy + iFx )fT (k,−1) =1/ 2(−Fy + iFx )
For all other m fT=0 which finally gives asymptotically
u = exp(−iωt)(Fy cosϕ −Fx sinϕ )l1(kn,h,ω)
8cUI1n∑ 2
πknr[l1(kn, z,ω)expi(knr +π / 4)
ϕ ]
GREEN’S FUNCTION FOR LOVE WAVES
G =
l1(kn,h,ω)l1(kn, z,ω)8cUI1n
∑sin2ϕ −sinϕ cosϕ 0
−sinϕ cosϕ cos2ϕ 00 0 0
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&
'
((((
2πknr
exp[i(knr +π / 4)]
u = l1(kn, z,ω)8cUI1n
∑ 2πknr
exp[i(knr +π / 4)]
{iknl1(h)[Mxx sinϕ cosϕ −Mxy cos2ϕ +Mxy sin
2ϕ −Myy sinϕ cosϕ ]
dl1(h)dz
[Mxz sinϕ −Myz cosϕ ]}−sinϕcosϕ0
#
$
%%%%
&
'
((((
Where I used ui=MpqGip,q