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Chapter 1
Introduction and motivation
Although Newton’s laws of motion were immediately successful when applied to
planetary motions, they were much less so when employed in the field of fluid me-
chanics. A good example of this is the 1999 solar eclipse which was predicted
correctly to the minute over a hundred years before the event. Whether the sky
would be clear or cloudy on the day however was not known even a day in advance.
Although both of these systems are governed by Newton’s second law of motion
the planetary orbit solutions are stable whilst those governing fluid flows in the
atmosphere are generally unstable.
In fluid dynamics stability takes the form of laminar flows whose clean, regu-
lar velocity profiles represent the most basic solutions to the hydrodynamic equa-
tions. Instability meanwhile is characterised by irregular, unpredictable turbulent
flows that generally break down into ever more complex patterns and structures.
This complicated behaviour is epitimised by the experimental results of Osbourne
Reynolds [1] who studied the, now classic, problem of flow in a pipe.
Owing to the unpredictable nature of turbulence, knowing where and when insta-
bility will appear is often of great interest in ‘real-life’ problems. In some situations,
e.g. aviation, turbulence is best avoided, whilst in other situations it may be essential
for the system to function correctly, e.g. mixing problems.
The study of hydrodynamic stability therefore is concerned with when and how
13
CHAPTER 1. INTRODUCTION AND MOTIVATION 14
these laminar flows break down, their subsequent development and eventual transi-
tion to turbulence. The subject has a long history beginning in the latter part of
the nineteenth century and, with many applications in fields such as engineering,
meteorology, oceanography, astrophysics and geophysics, it is widely recognised as
one of the fundamental problems of fluid mechanics.
1.1 Spherical Couette flow
The roots of the spherical Couette flow problem date back as far as 1890 when Mau-
rice Couette experimentally investigated the dynamics of a viscous fluid contained
between two concentric cylinders. Keeping the inner cylinder fixed whilst rotating
the outer one, Couette studied the moment of the drag exerted by the fluid on the
inner cylinder — his goal being to measure the viscosity of the fluid. He noticed
that for velocities above some threshold value, the rate at which this drag increased
with velocity changed significantly. This change in behaviour was attributed to a
transition of the system from steady, laminar flow to chaotic, turbulent motion.
The theoretical investigation of fluid flow bounded by concentric, rotating cylin-
ders was first considered by Lord Rayleigh (John Strutt, 3rd Baron Rayleigh) who
studied the stability of an inviscid fluid to axisymmetric disturbances (see [2],[3]).
Rayleigh concluded that for differentially rotating cylinders with a negative angular
momentum ratio, the flow would always be unstable. However for cylinders rotating
in the same direction, the flow could be stable if the angular momentum of the outer
cylinder exceeded that of the inner one. Roughly speaking this means that, in the
absence of viscosity, a basic state flow is stable if, and only if, the velocity profile
of the fluid exhibits the property that the absolute value of the angular momentum
increases monotonically outwards with radius. This statement can be thought of as
a direct application of Rayleigh’s circulation criterion (see [2],[4],[5]).
CHAPTER 1. INTRODUCTION AND MOTIVATION 15
Taylor–Couette flow
The above ideas were developed further by Sir Geoffrey Taylor who extended Rayleigh’s
inviscid analysis to include the effects of viscosity in his ground breaking paper of
1923 [6]. Driven by the experimental findings of Couette (and others), Taylor con-
structed a more advanced and accurate apparatus with which to visualise viscous
fluid flow between concentric rotating cylinders — now known as Taylor–Couette
flow.
Taylor’s findings showed that once the angular momentum ratio of the cylinders
reached a critical point, i.e. when the magnitude of the angular momentum on the
inner boundary was sufficiently larger than that of the outer one, the (purely zonal)
basic flow became unstable to a series of cellular, axisymmetric, toroidal vortices.
These vortices are now known as Taylor vortices and are illustrated by a schematic
drawing and an experimental photograph in Figure 1.1(a) and 1.1(b) respectively.
An important outcome of this was the realisation that stability in a rotating
fluid can be characterised by a dimensionless quantity — now known as the Taylor
number, denoted Ta — which is, generally, proportional to the square of the Reynolds
number (although the precise definition may vary). Roughly speaking the Taylor
number of a system can be thought of as a measure of the ratio of the angular
momentum to the kinetmatic viscosity (or viscosity per unit density).
The key feature of this Taylor number is that all flows with Ta less than some
critical value Tac (say) will remain stable and the effect of viscosity will be to damp
any small disturbances by dissipation. However flows for which Ta exceeds Tac will
become unstable to axisymetric Taylor vortices as described previously. The finite
strength of the vortex structures will be a function of the angular velocity, and hence
the Taylor number, as shown by Taylor’s torque measurement experiments [7].
The experimental observations outlined above suggested some important simpli-
fications that could be made in the theoretical treatment of the problem and led
Taylor to seek disturbances to the basic flow in the form of axisymmetric vortices.
He expanded the, radially dependent, vortex amplitudes as series of Bessel functions,
CHAPTER 1. INTRODUCTION AND MOTIVATION 16
(a) (b)
Figure 1.1: Taylor vortex instabilities in the classical, cylindrical, Taylor–Couette
flow configuration (a) shows a schematic illustration of the vorticies whilst (b) depicts
Taylor vortices arising in a laboratory experiment.
each with its own wavenumber km, before solving numerically. (The critical Taylor
number Tac in this case would be the global minimum of Ta over all wavenumbers
km.)
The agreement between the values of Tac calculated using this theoretical ap-
proach and those seen in the experimental results was really rather good. In ad-
dition agreement between Taylor’s viscous results and the findings of Rayleigh for
the inviscid case were very good when both cylinders rotated in the same direction.
Namely Rayleigh’s circulation criterion held in this case and as the angular velocity
of the outer cylinder Tac approached the line of equal angular momenta for the inner
and outer boundaries (i.e. Rayleigh’s neutral stability point) from above. However
Rayleigh’s conclusion that inviscid fluid between two differentially rotating cylinders
would always be unstable did not hold as the presence of viscosity serves to stabilise
the system.
CHAPTER 1. INTRODUCTION AND MOTIVATION 17
Despite the generally excellent agreement between Taylor’s theoretical [6] and
experimental [6], [7] analyses, one key difference was evident; namely regarding the
temporal evolution of the system. Being concerned solely with whether or not dis-
turbances persisted or died out, Taylor’s analysis was limited to a linear theory
whereby he linearised his equations of motion about small amplitude disturbances.
This meant that, for unstable flows, Taylor’s theory predicted unbounded vortex
growth with time, in contrast to the existence of a finite amplite equilibrium sug-
gested by his experimental findings.
Following the development of weakly nonlinear theory in the 1950s, Davey [8]
employed an expansion about the small disturbance amplitude of the linear the-
ory and, by truncating to second order, constructed a weakly nonlinear analysis.
He identified a nonlinear amplitude equation governing the amplitude growth of
small Taylor vortex disturbances, now generally referred to as the Stuart–Landau
equation, whose solutions evolved towards a steady equilibrium as time progressed.
Spherical Couette flow
With the linear stability of cylindrical Taylor–Couette flow well known and under-
stood, the challange became to tackle the more complicated Spherical Couette flow
problem, which is more relevant in geophysical and astrophysical contexts.
The Spherical Couette flow problem consists of a viscous fluid, held at constant
temperature and pressure, confined between two concentric spherical shells of radius
R1 and R2 (with R1 < R2). The spherical shells rotate about a common axis with
angular velocities Ω1 and Ω2 respectively as depicted in Figure 1.2. However a
stationary outer sphere is generally favoured by experimentalists and so the majority
of numerical studies in this area have focused on this case, i.e. Ω2 = 0.
The basic flow is strongly zonal although, unlike the classical Taylor–Couette
problem, there is also a (much weaker) meridional circulation between the equator
and the poles. When the inner sphere rotates faster than the outer one, the centrifu-
gal forces that drive the instability are greatest in the vicinity of the equator. Once
CHAPTER 1. INTRODUCTION AND MOTIVATION 18
Ω1
Ω2
R1
R2
εR1
Figure 1.2: The spherical Couette flow configuration. Fluid is confined between two
spherical shells of radius R1 and R2 (R1 < R2) that rotate about a common axis
with angular velocities Ω1 and Ω2 respectively. The configuration is characterised
by the dimensionless parameter ε, the ratio of the gap width to the radius of the
inner sphere.
again stability can be characterised by the dimensionless Taylor number Ta which is,
as in the cylindrical case, a measure of the circulation of the flow (roughly speaking
proportional to the square of the angular momentum and inversely proportional to
the square of the kinematic viscosity).
The findings of Marcus and Tuckerman [9], [10] suggested that configurations
could be classified according to the size of the gap aspect ratio ε, defined to be the
ratio of the gap width to the radius of the inner cylinder (i.e. R2 − R1 : R1). They
identified narrow, medium and wide gap regimes. In the narrow and medium gap
cases, where the ratio was approximately less than a quarter, axisymmetric Taylor–
CHAPTER 1. INTRODUCTION AND MOTIVATION 19
Equator
Figure 1.3: A sketch showing equatorially symmetric, toroidal, Taylor vortices in
the spherical Couette flow configuration.
vortex type instabilities were observed at the onset of instability in the vicinity of
the equator.
These findings were confirmed by the theoretical and experimental investigations
of Buhler [11] who identified equatorially symmetric instabilities in which vortices
appeared in pairs with one either side of the equator. He isolated modes invoving
zero, one and two vortex pairs. Figure 1.3 shows a schematic representation of the
equatorially symmetric, single pair, vortex pattern. Buhler also identified asymmet-
ric vortex patterns whereby a single pair of vortices arose in the region of the equator
with one noticably larger in diameter than the other. In this case the streamline
defining the boundary between the vortex cells was located away from the equator.
1.2 The narrow-gap problem
The study of the stability of spherical Couette flow in the narrow-gap limit (ε small)
has a long history beginning with Walton [12]. When the gap aspect ratio ε is
CHAPTER 1. INTRODUCTION AND MOTIVATION 20
small, the expected mode of instability takes the form of Taylor vortices whose
angular, latitudinal, length scale is comparable to the gap width, as Wimmer’s
[13],[14] experiments confirm.
In this small ε limit the local equatorial geometry resembles concentric cylinders.
Walton [12] extended this infinite cylinder idea by employing a multiple scale analysis
based on the small parameter ε and expanding about the local critical value of the
Taylor number Tac — the critical value for the cylinder problem.
This rather simplistic analysis failed to correctly incorporate the true influence of
the effects of boundary curvature and the basic state meridional circulation. These
are both significant features and contribute towards a physical mechanism known as
phase mixing. Phase mixing is characterised in the WKB formulation by a non-zero
frequency gradient at the equator and has the effect of shortening the latitudinal
length scale and increasing viscous dissipation. The consequence of this phase mixing
therefore is that, as time progresses, vortices generated at the local cylinder critical
value of the Taylor number, Tac, ultimately decay to zero. In fact the stabilising
process is so strong that it causes the global critical Taylor number Tag to exceed
the local cylinder critical value Tac even in the limiting case as ε tends to zero!
Walton failed to fully appreciate the significance of phase mixing, the result being
that the value of the critical Taylor number predicted by [12] was too low.
The correct asymptotic solution was later developed by Soward and Jones [15]
who undertook their linear analysis in the vicinity of a complex latitude away from
the equator. They obtained the true global critical Taylor number, Tag, without
expanding about local values, and showed that it exceeded the local cylinder value
Tac. Unfortunately attempts to apply these techniques to a weakly nonlinear exten-
sion, with the inclusion of the Stuart–Landau term identified by Davey [8], proved
too complicated.
To get around this problem Harris, Bassom and Soward [16] allowed the outer
shell to move and considered the case of almost co-rotation. In doing so they intro-
duced another small, dimensionless parameter related to the departure from unity
CHAPTER 1. INTRODUCTION AND MOTIVATION 21
of the angular momentum ratio of the two shells. As this parameter approaches zero
then so does the difference between the global and local Taylor numbers, Tag − Tac
as well as the complex latitude value used by Soward and Jones [15]. Using these
asumptions they were able to extend the linear analysis of [15] into the weakly
nonlinear regime.
The governing equation studied by Harris, Bassom and Soward is the complex
Ginzburg–Landau equation
∂a
∂t=
(
λ − Υ2
ε x2 + ix)
a +∂2a
∂x2− |a|2a , (1.1)
rescaled here in keeping with this work (the true equation studied can be found
in Appendix A). The relevance of this equation, and the motivation behind its
existence, is described in Chapter 2 of this thesis; at this stage however, only an
understanding of what the individual terms represent is needed.
The equation (1.1) governs the amplitude modulation a(x, t) of toroidal, Taylor
vortex instabilities in space x and time t. The spatial variable x is related to the
latitude, albeit locally in the vicinity of the equator. The dimensionless parameter
Υε is a measure of the degree of co-rotation in the system and, being inversely pro-
portional to the departure from unity of the angular momentum ratio, is essentially
zero unless the angular velocities of the two spheres are very close. Meanwhile the
parameter λ is related to the excess Taylor number (i.e. the difference between Ta
and Tac) and can be thought of as driving the instability in the system. The dif-
fusion and temporal evolution of the amplitude function are governed by the terms
∂2a/∂x2 and ∂a/∂t respectively, whilst phase mixing enters the system through the
term ixa. Finally the term −|a|2a, the Stuart–Landau term obtained from Davey’s
weakly nonlinear analysis, captures the effects of nonlinearity in the system.
Pulse-train solutions
Following a complicated bifurcation sequence Harris, Bassom and Soward [17] (hence-
forth referred to as HBS) identified a global bifurcation to travelling wave solutions
valid in this co-rotation regime and located close to the equator. Being periodic in
CHAPTER 1. INTRODUCTION AND MOTIVATION 22
(a) (b)
Figure 1.4: (a) An example of a pulse train solution. (b) An isolated pulse extracted
from the pulse-train solution shown in (a). The pulse has an amplitude structure
which is centered about the origin and is effectively zero outside the range [-2,2]
time these solutions can be expanded in terms of a series of Fourier modes whose
amplitudes are purely dependent on latitude. Upon closer inspection it seems that
these modes are only non-zero over a small range of latitude values with each mode
centred a distinct distance from the equator and oscillating at a distinct frequency.
Isolated functions such as those found above, where the amplitude is only signifi-
cantly different from zero over a small range of the independent variable, are known
as pulses. Additionally, a sequence of these pulses located at regularly spaced inter-
vals are known as pulse trains. An example of a pulse-train solution can be seen in
Figure 1.4(a) whilst an isolated pulse, extracted from the pulse-train in the vicinity
of the origin, can be found in Figure 1.4(b).
The results of HBS therefore suggested the existence of pulse-train solutions in
the spherical Couette flow problem for Taylor numbers close to the local, cylin-
der critical value Tac. This idea had previously been suggested by Soward [18]
who, whilst studying the related problem of thermal convection in a rotating, self-
gravitating sphere, proposed that the effects of phase mixing could be counteracted
by those of nonlinearity. However, despite some interest in the area, no such be-
haviour was ever identified. Furthermore the investigations of Ewen and Soward
CHAPTER 1. INTRODUCTION AND MOTIVATION 23
[19], [20], who included a form of the HBS complex Ginzburg–Landau equation as
a special case, comprehensively ruled out the existence of pulse-trains.
In light of the above therefore, the results of HBS proved both interesting and
surprising. They pointed the way for Bassom and Soward [21] (henceforth referred
to as BS) to bypass the weakly nonlinear theory and develop solutions in the form
of inter-connected trains of pulses. It is the study of these pulse-trains, within the
context of equation (1.1), that provides the motivation for the first part of this
thesis.
1.3 The problem of thermal convection in a rapidly
rotating, self-gravitating sphere
Related to the spherical Couette flow problem is the problem of thermal convection
in a rapidly rotating, self-gravitating sphere. The problem is defined by a fluid
filled sphere which is uniformly heated throughout and maintained at a constant
temperature on the bounding surface. The fluid is assumed to satisfy the Boussinesq
approximation, which states that variations in density, and other parameters such
as viscosity, owing to changes in temperature can safely be ignored save for where
they appear in the external forcing, gravity, term (see [4] for further explanation).
Gravity is assumed to act radially inwards, as appropriate for a self-gravitating,
uniform density fluid, and the whole system rotates rapidly at a constant angular
velocity.
The dynamics of the problem gives it relevance to the study of many large
celestial bodies such as the Earth’s liquid core, the Sun and other stellar objects
as well as large fluid planets like Jupiter. Thermal convection in rapidly rotating
fluid spheres plays a key role in these astronomical flows where convection is often
the main source of mixing and heat transport. Therefore, knowledge of the general
behaviour of thermal convection in rapidly rotating systems is central to gaining an
understanding of these important geophysical and astrophysical problems.
CHAPTER 1. INTRODUCTION AND MOTIVATION 24
Figure 1.5: A sketch showing non-axisymmetric convective motions in an internally
heated, rotating sphere arising in the form of tall, thin columns (after Busse [23]).
Early studies of buoyancy driven convective motions in rapidly rotating systems
showed that non-axisymmetric critical disturbances are generally preferred to ax-
isymmetric ones, see Roberts [22] and Busse [23]. Busse predicted that instability
first appears close to thin vertical cylindrical surfaces aligned parallel to the axis of
rotation, as shown in Figure 1.5 (see also [23] Figure 1). These columns intersect the
sphere at a latitude of roughly 63and propagate slowly in the direction of rotation.
This prediction was subsequently verified by the experimental findings of Busse and
Carrigan [24].
As a simplification to the spherical convection problem, Busse [23] approximated
the geometry by a cylindrical annulus about the axis of rotation with sloping upper
and lower boundaries. Taking gravity to act perpendicular to the axis of rotation and
by considering a small boundary slope (low curvature effects) the vertical velocity
will be small when compared with the horizontal velocities. This means that the
z-dependence can be integrated out of the problem and thus Busse’s analysis was
CHAPTER 1. INTRODUCTION AND MOTIVATION 25
greatly simplified.
Yano [25] extended the Busse annulus model to include fully spherical boundaries
and showed that this modified Busse annulus model incorporated the effects of phase
mixing. He applied the z-averaging technique used in the original Busse annulus
model even though, with the small slope assumption no longer being valid, there
was little physical justification for it. Inspite of this Jones et al. [26] showed that
the approximation gives qualitatively reasonable results when compared with the
full three-dimensional linear analysis. This modified Busse annulus approximation
is now known as the quasi-geostrophic approximation (after Aubert et al. [27]).
Relaxation oscillations in rapidly rotating spherical systems
Three-dimensional time-dependent simulations of rapidly rotating spherical convec-
tion are limited by the availability of computational resources to somewhat mod-
erate values of the Ekman number E. In order to attain lower Ekman numbers
(or equivalently, higher Taylor numbers), closer to those believed to be appropri-
ate for astrophysical bodies, Cole [28] utilised the computationally less expensive
quasi-geostrophic model (see Appendix C).
He expanded his dependent variables in terms of Fourier functions in the az-
imuthal direction and, as a further simplification, considered only the behaviour at
onset by retaining only one azimuthal mode (the critical mode). In doing so he de-
veloped a sixteenth order PDE system of amplitude equations (see (C.3) and (C.4))
dependent on four non-dimensional parameters; namely the Rayleigh, Ekman, and
Prandtl numbers as well as the critical azimuthal wavenumber.
Cole sought travelling wave solutions to his system of equations which he used
as a starting point for the derivation of fully time-dependent solutions. Plotting the
kinetic energy of these solutions in time revealed a periodic time-series for which,
over the course of a period, the velocity component was only clearly distinguishable
from zero less than half of the time. This behaviour, where the amplitude of a
periodic (or quasi-periodic) system relaxes to a comparitively small magnitude over
CHAPTER 1. INTRODUCTION AND MOTIVATION 26
Figure 1.6: Relaxation oscillation behaviour clearly visible in a plot of kinetic energy
versus time taken from Cole’s results [28]. The thick (lower amplitude) lines repre-
sent the mean part of the kinetic energy and thin (higher amplitude) lines represent
the fluctuating part (see Appendix C for more details).
the course of a period (or quasi-period), is called a relaxation oscillation and is
exemplified by the plot in Figure 1.6.
It is relaxation oscillations like the ones found by Cole that provide the moti-
vation for the second half of this thesis where we extend the HBS model (1.1) and
attempt to replicate this relaxation behaviour.
Although the Cole and HBS problems are not the same (at the very least the
Cole problem is non-axisymmetric) the amplitude equations studied by Cole, (C.3)
and (C.4), have a lot in common with those studied by HBS (1.1); in so much as
many of the features present in Cole’s model also play a part in HBS’s (e.g. phase
mixing, nonlinear forcing and diffusion).
We therefore extend the HBS model (1.1) as follows
∂a
∂t=
[
λ − Υ2
εx2 + ix
]
a +∂Θ
∂xa +
∂2a
∂x2, (1.2a)
1
κT
∂Θ
∂t=
∂
∂x|a|2 +
∂2Θ
∂x2. (1.2b)
CHAPTER 1. INTRODUCTION AND MOTIVATION 27
The terms here are the same as in (1.1) save for the addition of Θ and κT which can be
thought of as the mean temperature profile and the thermal diffusivity respectively.
These equations will be motivated further in Chapter 8 but at this point we only
highlight the fact that we can easily recover the HBS equations by taking the infinite
κT limit.
It is the study of this extended HBS model (1.2) that comprises Part II of this
work. However it is important to be clear here that we do not solve the thermal
convection problem in this thesis, neither do we attempt to improve upon Cole’s
analysis. Instead we extend the HBS equations and attempt to capture some of the
features of Cole’s amplitude equations with the hope of reproducing this interesting
relaxation oscillation behaviour in our, relatively, much simpler system.
1.4 Outline of this work
In Part I of this thesis we extend the narrow-gap problem, outlined above in Section
§1.2, with a view to building upon the ideas introduced by BS [21] and HBS [17].
In Chapter 2 we expand upon the details given in Section §1.2 by reviewing
the ideas and developments made by other researchers working in this area. In
doing so we highlight the steps taken in [16], and prior publications, to derive the
complex Ginzburg-Landau equation governing the amplitude modulation of Taylor-
vortex type instabilities (1.1). We then set up the HBS co-rotation model and the
BS pulse-train model in non-dimensional units and briefly describe their findings
before ending the chapter with a summary of previous work on narrow-gap spherical
Couette flow.
Chapter 3 is concerned with drawing comparisons between the results of HBS
and BS and extending their ideas. New solutions of the HBS equations are sought
to provide a link between the two models and the methodology used to identify
these solutions is documented. We end the chapter by exploring the possibility of
extending the work of BS.
In Chapter 4 we explore the symmetries of the BS–model equations and develop a
CHAPTER 1. INTRODUCTION AND MOTIVATION 28
general framework for identifying and classifying pulse-train solutions. New periodic,
pulse-train solutions found within this framework are reported in Chapter 6 whilst
the methodology used to obtain them is detailed in Chapter 5 along with a brief
outline of our tests for stability and robustness. We end Part I with some summary
remarks in Chapter 7.
In Part II of this thesis we study the extended HBS–model (1.2) and try to
reproduce some of the interesting relaxation oscillation behaviour identified by Cole
[28] in this much simpler, model system.
In Chapter 8 we further motivate the extended HBS equations (1.2) and recreate
some of the HBS solutions found in [17] by considering the infinite κT limit. We
investigate the behaviour of (1.2) when the parameter κT is small and identify chaotic
relaxation oscillations in this regime.
In Chapter 9 we study the behaviour of the system as the parameter κT is reduced
from infinity down into the relaxation regime for one particular set of parameter
values taken from the work of HBS. We document the bifurcation sequence taken
by the solution as it transitions from the regular HBS solution with large κT , to the
chaotic relaxation oscillation solution, at small κT . In doing so we identify some
interesting multi-frequency quasi-periodic behaviour which we investigate further in
Chapter 10 with a frequency power spectra analysis.
Finally, we summarise the findings of Part II with some concluding comments in
Chapter 11.
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