Astron. Astrophys. 347, 734-738 (1999)
2. The Couette-Taylor experiment
The CT experimental apparatus consists of two coaxial rotating
cylinders of radius and
separated by a gap
, which is filled with a fluid of
viscosity . The cylinders can rotate
with different angular velocities and
; their height is in general much
larger than their radius, to minimize the effect of the boundaries.
The Reynolds number is usually defined in terms of the differential
rotation and by taking the gap width
as characteristic length:
![[EQUATION]](img11.gif)
where R is the mean radius
.
2.1. Critical parameters and transition to turbulence
When the inner cylinder is rotating and the outer one is at rest,
angular momentum decreases outward and the flow is linearly unstable
for Reynolds numbers higher than
(for narrow gap, cf. Taylor 1923). This well known instability takes
first the shape of steady toroidal, axisymmetric cells (the Taylor
vortices); it is very efficient in transporting angular momentum,
whose gradient is strongly reduced. At higher Re a wavy pattern
appears and after a series of bifurcations the flow becomes fully
turbulent. This case has been studied by many experimental teams, and
it is extremely well documented (see Andereck et al. 1986). It has
also been modeled successfully in three-dimensional numerical
simulations (Marcus 1984; Coughlin & Marcus 1996).
In the opposite case, when the outer cylinder is rotating and the
inner one is at rest, the angular momentum increases outward and the
flow is linearly stable. The only theoretical prediction concerning
the non-linear behavior is that by Serrin (1959), later refined by
Joseph and Munson (1970), who established that the flow is stable
against finite amplitude perturbations below
(in the narrow gap limit).
To this date, no numerical simulation has been able to demonstrate
the finite amplitude instability. But this instability does occur in
the laboratory, and it has been described already by Couette (1890).
It was studied in detail by Wendt (1933) and Taylor (1936), who showed
that for Reynolds numbers exceeding ,
the flow becomes unstable and immediately displays turbulent motions.
The critical Reynolds number depends on whether the angular speed is
increased or decreased in the experiment, a typical property of finite
amplitude instabilites. Moreover, it is sensitive to gap width, as
demonstrated by Taylor. Fig. 1 displays results from Wendt and Taylor:
is roughly constant below
, but above it increases as
, as was already noticed by Zeldovich
(1981), a behavior for which an explanation was proposed by Dubrulle
(1993). In the latter regime one can define another critical Reynolds
number involving, instead of gap
width, the gradient of angular velocity; since
![[EQUATION]](img24.gif)
the instability condition becomes
![[EQUATION]](img25.gif)
We see that two conditions must be satisfied for the finite
amplitude instability to occur: the first
is the classical criterion of shear
instability, valid also for plane parallel flows, whereas the second
, involving what we shall call the
gradient Reynolds number, is genuine to differential rotation.
In addition, to trigger the instability the strength of the
perturbation must exceed a certain threshold, which presumably also
depends on Re or .
![[FIGURE]](img22.gif) |
Fig. 1. Critical Reynolds number vs. aspect ratio; filled circles from Taylor (1936), open circles from Wendt (1933). Dotted line: critical Reynolds number for plane shear flow instability; dashed line: critical gradient Reynolds for circular shear flow in the limit of large gap (see text).
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2.2. Transport of angular momentum
In the turbulent regime, the torque measured by Taylor scales
approximately as for a given gap
width, where the exponent n tends to 2 for large
. The measurements made by Wendt
confirm that scaling with . It
suggests that the transport of angular momentum may be considered as a
diffusive process, and that the mean turbulent viscosity
increases linearly with
, or
. It is then natural to examine
whether this viscosity may be expressed as
![[EQUATION]](img33.gif)
with being a constant of order
unity, since the largest turbulent eddies would have a size
and a peripheral velocity
. The parameter
is easily derived from the torque
measurements, and the surprising result is that it decreases with gap
width (Fig. 2). For the smallest gaps,
scales as the inverse of
, but the slope steepens farther as
if the scaling would tend asymptotically to
![[EQUATION]](img44.gif)
(Comparing Wendt's experimental data of his two largest gaps, one
deduces an exponent )
We may therefore conclude that, in the limit of large gap, the mean
turbulent viscosity actually scales as
![[EQUATION]](img46.gif)
with .
This strongly suggests that the local value of the turbulent
viscosity is then independent of gap width, and that it is determined
only by the local shear:
![[EQUATION]](img48.gif)
r being the radial coordinate.
In principle, one should be able to verify this prescription for
by examining the rotation profiles
measured by Taylor and Wendt. According to (7), the conservation of
angular momentum requires that its flux, given by
![[EQUATION]](img50.gif)
varies as between the cylinders.
Therefore should be constant in the
turbulent part of the profile (as it is in the laminar flow).
But this constancy can be expected only if the transport of angular
momentum is achieved by the viscous and turbulent stresses alone. That
is not the case in Taylor's experiment: as acknowledged by him, an
Ekman circulation is induced by the ends of his apparatus, although he
tries to minimize the boundary effects by chosing a large aspect ratio
(height/radius). Moreover his rotation profiles are deduced from
pressure measurements made with a Pitot tube located at half height of
the cylinders, where the radial return flow has its maximum intensity.
Consequently, the torque inferred from these profiles is about half of
that measured directly at the inner cylinder.
The aspect ratio is less favorable in Wendt's experiment, but there
the top boundary is a free surface, and most of his measurements have
been made with the bottom boundary split in two annuli, attached
respectively to the inner and the outer cylinders, which reduces
drastically the circulation and renders his results more reliable. We
examined his rotation profiles obtained for the largest gap width
( ) and with 4 different speeds of the
inner cylinder ( ); we found that in
the bulk of the fluid, these profiles are compatible with the
constancy of the gradient Reynolds number, as predicted by (8).
However we cannot rule out a mild variation of
within the profile. Unfortunately,
Wendt gives the torque only for the case where the inner cylinder is
at rest; we draw from it the following value of the coefficient
:
![[EQUATION]](img56.gif)
The estimated uncertainty reflects that of the velocity
measurements: results from second
derivation of the shape of the fluid surface.
© European Southern Observatory (ESO) 1999
Online publication: June 30, 1999
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