A Lamb-Oseen vortex in a planar straining field is known to be subject to 3
D (three-dimensional) short-wave instabilities which are due to the resonan
ce of the straining field and two stationary Kelvin waves characterized by
the same axial wave number and by azimuthal wave numbers equal to -1 and +1
. The linear regime has been described by Moore and Saffman (1975). In this
article, we extend this analysis to the weakly nonlinear regime. The emerg
ing eigenmode is characterized by a complex amplitude A=\A\e(i phi), whose
behavior is governed by an amplitude equation. It is shown that the unstabl
e perturbation corresponds to an oscillation of the vortex in a plane incli
ned at an angle phi, while the amplitude of these oscillations is proportio
nal to \A\. The vortex centers are defined as the points where the velocity
of the vortex is zero, which also corresponds to the points where the pres
sure is minimum. We show that these instabilities saturate. The saturation
amplitudes are evaluated numerically and expressed in terms of oscillation
amplitudes of the vortex centers. If a denotes the internal radius of the v
ortex and if the straining field is due to a counter-rotating vortex of sam
e strength, located at a distance b, then the maximum amplitude Delta of th
e vortex oscillations is Delta/b=6.1a(2)/b(2). This result is in agreement
with those of the experiments of Leweke and Williamson (1998) for which a/b
=0.2. It also shows that in aeronautical situations, for which a/b is small
er, i.e., a/b < 0.1, the considered short-wave instability will saturate at
very low amplitude. (C) 2000 American Institute of Physics. [S1070-6631(00
)02607-6].