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146 Advanced Topics in Applied Mathematics
3.15 FINITE HILBERT TRANSFORM
Integral equations of the form
1
π
∗1
−1
u(ξ )dξ
x −ξ
=v(x), −1 < x < 1, (3.281)
where u(x) has to be found, appear in thin airfoil theory and in elas-
ticcontactandcrackproblems(seeMilne-Thomson,1958,Gladwell,
1980).Inthinairfoiltheory,circulationaroundanidealized2Dair-
foil is created using distributed vortices of unknown strength along its
chord, and the condition that the incompressible fluid velocity has to be
tangent to the airfoil profile is used to solve for the unknown. In elas-
ticity, an unknown pressure distribution on the contact line or crack
length is related to the known displacement caused by the pressure.
The finite Hilbert transform also has applications in image processing.
We may define the finite Hilbert transform as
T [v]≡
1
π
∗1
−1
v(ξ )dξ
x −ξ
. (3.282)
Note the kernel has the form 1/(x −ξ)unlike the regular Hilbert trans-
form. This can be related to a line integral in the complex plane in two
ways: the Cauchy integral representation of analytic functions and the
Plemelj formulas.
3.15.1 Cauchy Integral
As before, consider a unit circle C in the complex z-plane described
parametrically by s = e
iφ
,−π<φ<π. Using the Cauchy integral
theorem, we define an analytic function inside C by
F(z) =
1
2πi
C
F(s)ds
s −z
, |z|< 1. (3.283)