Integrationyvu(^0) x
Fig. 7.31
is called the vorticity (at each point), and
C = k\i'^2 V
is the vorticity vector.513The 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 integralj 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