In the area labelled ``Rotation'' in Fig
,
flows are time dependent.
Unsteady flows show periodical motions.
Figures 5 and 6 show
the time variation of the mean enstrophy
at
= 0.5 and Re = 600, 1500.
is given by
![]() |
(4) |
where S is an integral domain and A is the area of a meridional section.
Figure 7 shows the contours of the stream function
at time
points shown in Fig
.
While the time variation of
is almost sinusoidal at Re = 600,
the flow at Re = 1500 is not monotonic and
is reduced
suddenly from time point 4 to time point 5.
The mean kinetic energy in the (r, z) plane exhibits a similar variation to
that of the mean enstrophy.
The time variation of flow field at Re = 1500 is shown in Fig
.
The time points from 1 to 6 correspond to those shown in Fig
.
At time point 1 in Fig
(a), the flow has four vortices
in the radial direction.
As
increases, the vortex closest to the outer cylinder
decays and three vortices remain (Fig
(b)).
When
increases further, the
vortices at the two
sides of the cylinder merge
(Fig
(c)), and
a flow field with two large vortices appears at the time point where
was maximized (Fig
(d)).
Then each vortex is split by the other and four vortices emerge
(Figs
(e)(f)).
Taking into account the fact that the pattern in Fig
(f) is
the vertical reverse of the pattern in Fig
(a),
we can say that the two periods in the
graph
correspond to one period of unsteady motion.
When Re is 600, flows are weak and each of the vortices is not split by the other.
When the aspect ratio was less than 0.6, we confirmed that the
unsteady motion predicted by the present calculation is found
experimentally.
As well, the calculated and experimental results of the range of
and Re in
which the unsteady mode appears show good agreement.