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q 1
q 1
p 2 c i
T.p/ D 2 X
i
1
pm i
s i h i
p 2 c iC1
D
I
q s i p 2 I s i >p
(9.57)
i
D
0;1;:::;n
1
(9.60)
where h i is the thickness of the i -th layer. When
the velocity model has continuous gradients, the
approximate solutions ( 9.56 )and( 9.57 )arein-
adequate, because of the large number of quasi-
homogeneous layers that would be needed to
obtain reliable results. In this instance, a better
approach is to assume a velocity model such
that c D c ( z ) is a broken line and evaluate the
expressions ( 9.53 )and( 9.55 ) for each segment.
For example, if c i ( i D 0,2, :::, n )are n C 1rep-
resentative control points at depths z i along an
experimental velocity profile, we can assume that
the velocity varies linearly between any pair of
successive control points, so that:
Similarly,
z iC1
s iC1
Z
Z
s 2 . z /d z
p s 2 . z / p 2 D
ds
p s 2
1
m i
T i .p/ D
p 2
z i
s i
m i ln s C p s 2
p 2 LJ LJ LJ
s iC1
1
D
s i
c i 2 p 2 i LJ LJ LJ
m i ln h
m i . z z i /Cc i C q
z iC1
1
1
1
Πm i . z z i /
D
C
z i
ln 1
q 1 p 2 c iC1
v iC1 1 C
1
m i
D
ln v i
1 C
q 1 p 2 c i
(9.61)
c i C 1 c i
z iC1 z i
c. z / D
. z z i / C c i m i . z z i / C c i I
The final arrival time T ( p ) and range X ( p )
are then obtained summing these contributions
over the index i and multiplying the result by
two. Let us consider now the generalization of
the previous solutions to the spherical Earth. We
know that in this instance the horizontal distance
X is substituted by the angular distance ,so
that dX D Rd , R being the Earth's radius. In
this case, the ray parameter coincides with the
slowness at the turning point only when c is a
continuous and mostly increasing function of the
depth. To generalize ( 9.49 ), we start as before
from ( 9.43 ). However, in this case Snell's law
in the form ( 9.40 ) must be substituted by ( 9.42 ).
Therefore,
for z i z z iC1 I i D 0;1; ;n 1 (9.58)
In this case, the variation of slowness with
depth will be given by:
ds
dc dc. z / D
1
c 2 . z / dc. z /
ds. z / D
m i
c 2 . z / d z D m i s 2 . z /d z I
D
for z i < z < z iC1 I i D 0;1; ;n 1
(9.59)
If we substitute the functions ( 9.58 ) into the
integrals ( 9.53 )and( 9.55 ) and change the inte-
gration variable to ds , we have that each segment
gives a contribution X i to the total range X that
can be expressed as follows:
dT
d D R dT
dX D R p
R D p
(9.62)
This is the generalization of ( 9.49 ) to a spher-
ical Earth. Solutions for the arrival time T ( p )and
the range X ( p ) can be found easily using the same
approach discussed previously for the flat Earth
approximation. We obtain:
z iC1
Z
d z
p s 2 . z / p 2
X i .p/
D
p
z i
LJ LJ LJ LJ LJ
p s 2
s iC1
Z
s iC1
p 2
m i ps
p
m i
ds
s 2 p s 2
D
p 2 D
Z
R
s i
s i
LJ LJ LJ LJ LJ LJ LJ
q 1
1
r p r 2 s 2 .r/ p 2 dr (9.63)
z iC1
.p/ D 2p
c i 2
p 2 Œm i . z
z i /
C
D
pm i
r min
z i
 
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