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Next we consider the gravity disturbance. Since
g =grad W,
(2-238)
γ
=grad U,
the gravity disturbance vector (2-231) becomes
∂T
∂x ,
.
∂T
∂y ,
∂T
∂z
δ g =grad( W
U ) = grad T
(2-239)
Then
∂W
∂n
∂U
∂n
∂U
∂n ,
=
g =
,
γ =
(2-240)
because the directions of the normals n and n almost coincide. Therefore,
the gravity disturbance is given by
∂W
∂n
=
∂W
∂n
∂U
∂n
∂U
∂n
δg = g P
γ P
=
(2-241)
or
∂T
∂n .
δg =
(2-242)
Since the elevation h is reckoned along the normal, we may also write
∂T
∂h .
δg =
(2-243)
Comparing (2-242) with (2-239), we see that the gravity disturbance δg ,be-
sides being the difference in magnitude of the actual and the normal gravity
vector, is also the normal component of the gravity disturbance vector δ g .
We now turn to the gravity anomaly ∆ g .Since
= γ Q + ∂γ
γ P
∂h N,
(2-244)
we have
∂T
∂h
∂γ
∂h N.
= δg = g P
γ P
= g P
γ Q
(2-245)
Remembering the definition (2-228) of the gravity anomaly and taking into
account Bruns' formula (2-237), we find the following equivalent relations:
∂T
∂h
∂γ
∂h N,
=∆ g
(2-246)
∂T
∂h + ∂γ
g =
∂h N,
(2-247)
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