1550251515-Classical_Complex_Analysis__Gonzalez_

(jair2018) #1
Integration

y

vu

(^0) x
Fig. 7.31
is called the vorticity (at each point), and


C = k\i'^2 V


is the vorticity vector.

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The fl.ow may also be derived from the stream function V, which always
exists regardless of whether the motion is irrotational or not. In fact, we
have

-2i ~~ = -i(V., + iVy) =Vy - iV., = u +iv= w (7.29-12)


Suppose that z 0 E D is such that u + iv is continuously differentiable in
some deleted neighborhood NHzo), and such that the circulation integral

j Wr ds = j u dx + v dy
c+ c+
has a nonzero constant value k for all closed C around z 0 described once
in the positive direction and such that C* C N6(z 0 ). Then the point z 0
is called a vortex and the number k is termed the strength (or intensity)
of the vortex.
Similarly, suppose that the flux integral


j w,, ds = j u dy - v dx
c+ c+

has a nonzero constant value m for all closed C around z 0 described once
in the positive direction and with graph contained in Nf;(z 0 ). Then the


point z 0 is called a source if m > 0 and a sink if m < 0. In either case the

number !ml is said to be the strength of the source or sink. The vortices
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