The Influence of Coriolis Forces on Flow Structures of - T-Space
Transcript of The Influence of Coriolis Forces on Flow Structures of - T-Space
The Influence of Coriolis Forces on Flow Structures of Channelized Large-Scale Turbidity Currents and their
Depositional Patterns
by
Remo Cossu
A thesis submitted in conformity with the requirements for the degree of Doctor of Philosophy
Department of Geology University of Toronto
© by Remo Cossu 2011
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The Influence of Coriolis Forces on Flow Structures of Channelized Large-Scale Turbidity Currents and their Depositional Patterns
Remo Cossu
Doctor of Philosophy
Department of Geology, University of Toronto
2011
Abstract
Physical experiments are used to investigate the influence of the Coriolis forces on flow
structures in channelized turbidity currents, and their implication for the evolution of straight and
sinuous submarine channels.
Initial tests were used to determine whether or not saline density currents are a good
surrogate for particle-laden currents. Results imply that this assumption is valid when turbidity
currents are weakly-depositional and have similar velocity and turbulence structures to saline
density currents. Second, the controls of Coriolis forces on flow structures in straight channel
sections are compared with two mathematical models: Ekman boundary layer dynamics and the
theory of Komar [1969]. Ekman boundary layer dynamics prove to be a more suitable
description of flow structures in rotating turbidity currents and should be used to derive flow
parameters from submarine channels systems that are subjected to Coriolis forces. The
significance of Coriolis forces for submarine channel systems were determined by evaluating the
dimensionless Rossby number RoW. The Rossby number is defined as the ratio of the flow
velocity, U, of a turbidity current to the channel width, W, and the rotation rate of the Earth
represented by the Coriolis parameter, f. Coriolis forces are very significant for channel systems
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with RoW ≤ O(1). Third, the effect of Coriolis forces on the internal flow structure in sinuous
submarine channels is considered. Since previous studies have only considered pressure gradient
and centrifugal forces, the Coriolis force provides a crucial contribution to the lateral momentum
balance in channel bends. In a curved channel, both the Rossby number RoW and the ratio of the
channel curvature radius R to the channel width W, determine whether Coriolis forces affect the
internal flow structure. The results demonstrate that Coriolis forces can cause a significant shift
of the density interface and the downstream velocity core of channelized turbidity currents. The
sediment transport regime in high-latitude channel systems, which have RoW << R/W, is therefore
strongly influenced by Coriolis forces. Finally, these findings are incorporated into a conceptual
model describing the evolution of submarine channels at different latitudes. For instance, the
Northern Hemisphere channels have a distinctly higher right levee system and migrate
predominantly to the left side and generally exhibit a low sinuosity. In contrast, low latitude
channel systems have RoW >> R/W so that centrifugal forces are more dominant. This results in
more sinuous submarine channel systems with varying levee asymmetries in subsequent channel
bends. In conclusion, Coriolis forces are negligible around the equator but should be considered
in high latitude systems, particularly when RoW ~ O(1) and RoW << R/W.
IV
Acknowledgements
There are many people I would like to thank for their help and support over the last four years. Without them I could not call my experience in Canada and the completion of my Phd an exciting one. • First, and foremost, my supervisor Mathew Wells for giving me the opportunity to come to Canada and to go on this adventurous journey. I am especially grateful for his truly unconditional support regarding all aspects of the scientific world. I enjoyed working with Mathew from the first to the very last minute of my PhD. With his guidance, teaching and understanding he was the most pleasant supervisor I could have asked for. Mathew, thank you for everything! • Members of my PhD Committee: Brian Greenwood, Nick Eyles, Joe Desloges and Julian Lowman for contributing timely and healthy criticism and inspiration. Special thanks go out to Brian for his help with the ADV, to Nick for extending my knowledge of glacial sedimentology/geology and Julian for his patient, nonchalant help with mathematics in the late stages of this thesis. • Bruce Sutherland for his helpful comments and suggestions for the thesis. Special thanks for his readiness and willingness to travel in from Edmonton to attend the thesis defense. • Jeff Peakall and Gareth Keevil for loaning me the the UDVP which I used for a major part of this thesis. Thank you Jeff, for all of your support, advice and input for my experiments and publications. • Anna Wåhlin for her mathematical modelling skills and contribution to this thesis. • Gary Parker and Carlos Pirmez for their intreguing discussions at the AGU Chapman conference in Oxnard. • I would also like to thank a few key influencers and mentors from back home who had guided me professionally in academia and industry: Birgit Brinkmann, Karl-Friedrich Daemrich and Joerg Osterwald. I would not have undertaken the step of going to Canada without your support, advice and help. • Ulrich Langer for proofreading gazillions of documents in preparation for my acceptance into the PhD program at UofT.
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• The province of Ontario for its financial support of this thesis project. • All of the administrative staff in the Geology Department, as well as the Department of Physical & Environmental Sciences. • Bob Ush and Joan Mills for being so supportive during those long nights of writing and editing. • C.C. for countless free coffees on my days out at UTSC. • Joerg Bollmann for being a great and generous friend and counsellor in academia and the weird ways of life. • Christoph Schrank for being a great schoolmate during the first years in Toronto. • The wild bunch of grad students who started this journey with me in 2007. You made my first year probably the most memorable. Cheers mates, the next international dinner is on me! • My various officemates I had over the years, especially Bronwyn and Taronish for enduring the occasional odor of gym gear with only minor complaints. I also want to thank Taronish for becoming a companion, who I could always rely on for down time and being such an awesome workout partner. • Many longtime and most loyal friends back home. Although separated by an ocean from you, I did not get lost being so far from home because I knew you were still there for me. You know who you are! “Wir werden immer laut durchs Leben ziehen, jeden Tag in jedem Jahr…” • The honorary final position is reserved for those that I owe the most: Kristina, for standing beside me along this journey. You helped me grow through things and have kept me in balance (not only with the rotating table!). Thank you for who you are! I finally want to thank my family and relatives: especially my magnificent sister and my wonderful, loving parents. Leaving home is never easy…You all rule!
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Table of Contents
Abstract II-III
Acknowledgements IV-V
Statement of authorship XII
Chapter 1: Introduction
1.1 The significance of turbidity currents 1-8
1.2 The importance of the Coriolis force 9-13
1.3.1 Physical models 13-16
1.3.2 Velocity structure 16-17
1.3.3 Secondary flow cells due to centrifugal forces 17-19
1.3.4 Secondary flow cells due to Coriolis forces 20-22
1.4. Motivation and thesis overview 22-24
References 24-30
Chapter 2: A comparison of the shear stress distribution in the bottom boundary layer of experimental density and turbidity currents
Abstract 31-32
2.1 Introduction 32-35
2.2 Shear stresses in the BBL 36-38
2.3 Method 38-42
2.4.1 General flow properties 42-44
2.4.2 Velocity fluctuations 45-46
2.4.3 Reynolds stresses 47-51
2.4.4 Turbulent kinetic energy profiles 51-52
2.4.5 Drag coefficients 53-54
2.5. Discussion 55-60
2.6. Summary and Conclusions 60-61
Acknowledgements 62
References 62-65
VII
Chapter 3: Influence of the Coriolis force on the velocity structure of gravity currents in straight submarine channel systems
Abstract 66-67
3.1 Introduction 67-71
3.2.Theory 72-80
3.3 Method 80-83
3.4.1 General observations 83-85
3.4.2 Observations of downstream velocity U 85-89
3.4.3 Slope of the interface with changing f 89-91
3.4.4 Secondary flow cells and across-stream velocities 91-95
3.5 Discussion 95-99
3.6 Conclusions 100-101
Acknowledgements 101
References 101-105
Chapter 4: Coriolis forces influence the secondary circulation of gravity currents flowing in large-scale sinuous submarine channel systems
Abstract 106
4.1 Introduction 106-109
4.2 Theory 109-110
4.3 Experiments 110-112
4.4 Results and Discussion 112-117
4.5 Conclusions 118
Acknowledgements 118
References 119-120
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Chapter 5: Flow structures and sedimentation processes in submarine channels under the influence of Coriolis forces: experimental observations in rotating gravity currents
Abstract 121
5.1 Introduction 122-124
5.2 Method 124-125
5.3 Results 125-128
5.4 Discussion 129-133
5.5 Summary and conclusions 133
Acknowledgements 134
References 134-135
Chapter 6: Final remarks
6.1 Summary and implication 136
6.2 1 Density currents as an analogue for turbidity currents 136-137
6.2.2 Coriolis forces in straight submarine channels 137-138
6.2.3 Coriolis forces in sinuous submarine channels and
their implication for the evolution of channel systems 138-140
6.2.4 Future work 140-141
References 141-142
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List of Tables
Chapter 2
Table 2.1: Summary of parameters for experimental gravity currents 44
Chapter 4
Table 4.1: Experimental conditions 112
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List of Figures
Chapter 1
Fig. 1.1: Environment of large-scale turbidity currents 3
Fig. 1.2: Bathymetric map of the Zaire Canyon 4
Fig. 1.3: Cross section of the Upper Indus and the NAMOC 5
Fig. 1.4: Sinuosity of submarine channels versus the latitude 8
Fig. 1.5: Particle motion on a rotating platform 9
Fig. 1.6: Downchannel components of a density current in the Faroe Bank Channel 13
Fig. 1.7: Velocity and density profile of an experimental turbidity current 16
Fig. 1.8: Velocity component of density currents in the Black Sea and Baltic Sea 18
Chapter 2
Fig. 2.1: Experimental setup 38
Fig. 2.2: Size distribution for particles 39
Fig. 2.3: Velocity distribution of the downstream velocity component 42
Fig. 2.4: Time series of downstream velocity components u 45
Fig. 2.5: Reynolds stress and viscous stress in the BBL 47
Fig. 2.6: Relation between the velocity gradient du/dz and Reynolds stresses 49
Fig. 2.7: Mixing length of saline and sediment-laden gravity currents 50
Fig. 2.8: Vertical TKE profiles 52
Fig. 2.9: Calculated drag coefficients 53
Fig. 2.10: Velocity profiles between natural and experimental gravity currents 57
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Chapter 3
Fig. 3.1: Channelized density current flowing down a submarine channel 73
Fig. 3.2: Velocity profiles in the Ekman boundary layer for various f 76
Fig. 3.3: Shapes of the interface for various f 79
Fig. 3.4: Experimental setup 80
Fig. 3.5: ADV and UDVP velocity profiles 82
Fig. 3.6: Measured downstream velocity U for various f 86
Fig. 3.7: Rossby number RoW and the Froude number Fr for various f 88
Fig. 3.8: Photographs of the interface for various RoW 90
Fig. 3.9: Deflection ΔΔΔΔh and RoW for various f 91
Fig. 3.10: Across-stream velocities for various f 92
Fig. 3.11: Relation between s/(dh/dy) and RoW for various f 94
Chapter 4
Fig. 4.1: Flow structures in channelized gravity currents for various geometries 108
Fig. 4.2: Experimental setup 111
Fig. 4.3: Photographs of experimental gravity currents for various RoR 113
Fig. 4.4: Secondary velocity fields for various RoR 115
Chapter 5
Fig.5.1: Experimental set-up 125
Fig. 5.2: Relationship between Fr 2 / RoW
and the tilt of the interface for various f 126
Fig. 5.3: Interface, distribution of the velocity core, across stream velocities
and distribution of the bottom downstream component for various f 128
Fig. 5.4: Conceptual model for channel evolution at different latitudes 130
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Statement of authorship
Chapter 2 has been submitted with M.G. Wells to the Journal of European Mechanics-
B/Fluids (Cossu and Wells, 2011). R. Cossu conducted the experiments, R. Cossu and M. Wells
analyzed the data and wrote the paper. Both authors participated in the discussion and
interpretation of the results. The paper has been accepted for publication for the Journal of
European Mechanics- B/Fluids.
Chapter 3 is co-authored by M.G. Wells and A.K. Wahlin. A.K. Wahlin derived the
analytical solutions, R. Cossu ran the physical experiments, developed the data evaluation
routines, and wrote the paper with M.G. Wells. All authors participated in the discussion and
interpretation of the results. This paper is published in the Journal of Geophysical Research
[Cossu et al., 2010].
Chapter 4 is authored by R. Cossu and M.G. Wells. R. Cossu performed the analogue
experiments. Both authors participated in the discussion and interpretation of the results. This
paper has been published in Geophysical Research Letters [Cossu and Wells, 2010].
Chapter 5 is authored by R. Cossu and M.G. Wells. R. Cossu performed the analogue
experiments. Both authors participated in the discussion and interpretation of the results. This
paper will be submitted to a scientific journal shortly.
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Chapter 1
Introduction
1.1 The significance of turbidity currents
The goal of this thesis is to investigate the influence of Coriolis forces on the internal
flow structure and depositional patterns of large-scale gravity currents in submarine channels.
Gravity currents are important environmental flows that are driven by a density difference with
the ambient fluid, usually caused by a difference in temperature, salinity or sediment mass
concentration. Gravity currents occur in the atmosphere and the ocean. For instance, sea-breeze
fronts and thunderstorm outflows represent gravity flows of cold, dense air. Atmospheric-
suspension gravity currents comprise snow avalanches or fiery avalanches and base surges from
gases and particles resulting from volcanic eruptions [Simpson, 1982; Middleton, 1993].
Subaqueous gravity currents consisting of suspended sediments are known as turbidity currents
and are important agents transporting sediments in lakes and oceans. On geological time-scales,
they form large-scale features such as submarine fan systems and thick layers of sedimentary
rock that are volumetrically the most important clastic accumulations within deep ocean basins
[Normark, 1993]. The study of turbidity current dynamics in these fan systems allows for
improving geologic models that help to understand deep-sea environments that are paramount for
deciphering the geologic record on the sea floor and exploring hydrocarbon energy sources.
On November 18th, 1929, a 7.2-magnitude earthquake caused a slope failure
approximately 200 km off the coast of Newfoundland. The earthquake triggered a debris flow
that ultimately turned into a turbidity current that continued down a main continental slope valley
and spread out on the abyssal plain. During its passage it broke several trans-Atlantic
communication cables [Heezen end Ewing, 1952]. Based upon timing of these breaks, a
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maximum propagation speed from 19 m s-1 up to 25 m s-1 was estimated [Piper et al., 1988;
Wells, 2009]. The sediment that was deposited on the ocean basin floor during this incident
covered an area of 280,000 km2 [Piper et al., 1985] with an approximate volume of 150 to 175
km3 [Piper et al., 1999]. This event demonstrates the significance of turbidity currents to
delivering coastal sediments to the deep ocean basins, but also indicates the hazard and power
emanating from these flows.
The reasons why the study of turbidity currents has become more popular are manifold.
Today, turbidity currents are known to be important agents for sediment transport from shallow
coastal areas to deep sea environments (Figure 1.1a), where they form vast sediment
accumulations [Curray et al., 2003], and the deposits often form significant deep-water
hydrocarbon reservoirs [Weimar and Slatt, 2007]. The transport of sediments by turbidity
currents is also environmentally important as they fill in lakes and ocean basins [De Cesare et al.,
2001]. Additionally, turbidity currents are hazardous flows that can damage or destroy seafloor
equipment [Khripounoff et al., 2003], or submarine cables as in the Grand Banks earthquake
turbidity flow [Heezen and Ewing, 1952]. Finally, their deposits are important as they help us to
understand the sedimentation record on the seafloor, which can be linked to prevailing climate
conditions during times of deposition [Pirmez, 1994].
Turbidity currents can be triggered by numerous mechanisms, such as when a sediment-
laden river enters a lake, when sloping layers of sediment on the continental shelf become
unstable due to loading, due to underground gas release or seismic activity [Piper and Normark,
2009; Meiburg and Kneller, 2010] or resuspension by wave action, tides or storm induced
downwelling events on the continental shelf [Palanques et al., 2006a]. In addition, some events
are even man-made; for instance, when mine tailings are dumped into Lake Superior [Normark,
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1989], into the Prince Rupert channel [Hay, 1987] or when material is dredged close to a canyon
head [Xu et al., 2004].
The main pathways for sediments to deep ocean basins are submarine canyons and
submarine channels (Figure 1.1a) that are formed by turbidity currents and that are significant
morphological features on the continental slope and the ocean floor [Amos et al., 2010]. The
location of the upper pathway, the submarine canyon, is generally fixed and incised into the
continental slope. These canyon systems can exhibit widths up to 20 km and generally occur on
steeper gradients [Normark et al., 1993; Clark and Pickering, 1996].
Fig. 1.1: a) Schematic overview of the environment of large-scale turbidity currents flowing from the con-tinental shelf to the abyssal plain [after Normark et al., 1993] b) Schematic of a submarine channel-levee system [Migeon et al., 2004].
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In contrast, submarine channels form on the lower pathways and flow through
subaqueous channel systems that are confined by levees as sketched in Figure 1.1b. Further
downstream the channel geometry can disappear and turbidity currents are free to spread out
across the deep ocean basins so that they give rise to subaqueous fans and basin-plain deposits
[Middleton, 1993]. Deep submarine channels occur on slopes with gradients smaller than 0.5º
and can reach length scales of up to several thousand kilometres [Meiberg and Kneller, 2010]
such as in the Zaire Fan system in West Africa (Figure 1.2).
Fig. 1.2: Bathymetric map showing the general morphology of the Zaire Canyon and the modern Zaire meandering channel in the Gulf of Guinea [Migeon et al., 2004]
This thesis focuses on the lower pathways in mid-fan systems where submarine channels are free
to migrate by avulsion and lateral migration [Middleton, 1993] and their morphology reflects the
nature of sedimentary processes active on the fan [Clark et al., 1992]. Channel systems have
been documented from many sources, such as ancient sedimentary successions, the present-day
seafloor and from areas of subsurface hydrocarbon exploration and development [Clark and
Pickering, 1996]. The dimensions of channels can range from several kilometers in width, and
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several hundred meters deep [Weimar and Slatt, 2007], like the Upper Indus Fan channel
[Kenyon et al., 1995a], to small distal-lobe channels that are only 75 m wide and have depths
smaller than 2 m such as channels on the Outer Mississippi Fan [Twitchell et al., 1991].
Many channels are confined by prominent levees, which form by deposition of suspended
sediment on the slower moving margins of a turbidity current [Parsons et al., 2007] as shown in
Figure 1.3a and 1.3b. These levees can grow rapidly; for instance, the average sedimentation
rates during the active growth phases of the levees of the Amazon channel during the Pleistocene
were 1 to 2.5 cm year-1 [Shipboard Scientific Party, 1995]. The rapid growth has been attributed
to continuous deposition of suspended load. Suspended sediment can be delivered by successive
turbidity currents that transit the channel and spill over the channel margins along their entire
length [Hiscott et al., 1997; Peakall et al., 2000; Straub et al., 2008]. As a result, channel levee
systems can reach widths up to 50 km and heights up to 300 m above the surrounding seafloor,
as is observed in the Amazon Channel [Damuth et al., 1988] or the Indus Fan channel shown in
Figure 1.3a.
Fig. 1.3: a) Cross section of a submarine channel in the Upper Indus Fan [Kenyon et al., 1995a] b) Air gun seismic profile across the North Atlantic Mid-Ocean Channel [Skene et al., 2002].
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Levee deposits and their structure are described in many studies [e.g. Normark et al., 1980;
Damuth and Flood, 1985; Kolla and Coumes, 1987]. These overbank facies commonly consist of
fine-grained and thin bedded, current laminated sands and silts as well as graded mudstones.
Inside the channel the sediments are usually larger and deposits are more coarse-grained [Clark
and Pickering, 1996].
In plan view most channels are straight, sinuous or meandering or commonly show a
combination of the above with down-channel changes in their planform geometry. Sinuosity can
be defined as the ratio of the channel length to the valley length [e.g. Clark et al., 1992; Imran et
al., 1999]. Submarine channel sinuosity of approximately 1 to greater than 3 has been reported
[e.g. see Clark et al., 1992; Kolla et al., 2007; Wynn et al., 2007]. In the literature, sinuous
channels have been defined as having a sinuosity of greater than 1.2 [Wynn et al., 2007] and 1.15
[Clark et al., 1992; Clark and Pickering, 1996]. Previous classifications of submarine channels
and fans associate channel sinuosity with the slope gradient which in turn is linked to sediment
type and sediment cohesion [Clark et al., 1992; Reading and Richards, 1994; Piper and Normark,
2001], as is also classically observed for river channels [Schumm and Khan, 1972]. Clark and
Pickering [1996] differentiate between two end members in these classifications, one being a
high sinuosity, low slope gradient, fine-grained system, while the other is characterized by a low
sinuosity, high slope gradient, coarse-grained system.
Highly sinuous submarine channels are found in modern equatorial regions, for instance
the Bengal Fan, the Indus Fan, the Mississippi Fan, the Zaire Channel (Figure 1.2), or the
Amazon channel (Figure 1.4a) [Clark and Pickering, 1996; Abreu et al., 2003]. For instance, the
Amazon fan reveals a maximum (peak) sinuosity of 2.6 in its mid-fan region at 3°- 7° North
[Pirmez and Imran, 2003]. In contrast, high latitude systems reveal generally only small sinuosity
[Peakall et al., 2011] and can show distinct levee asymmetries [Menard, 1955]. Examples of low
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sinuosity channels are the North Atlantic Mid-Ocean Channel (NAMOC) with a sinuosity of
1.01-1.05 at 53°-59° North (Figure 1.4b) [Klaucke et al., 1997] and the Bering Sea channels with
a mean sinuosity of 1.05 at 55° North [Clark and Pickering, 1996].
The aforementioned features of submarine channel systems raise two challenging
questions that this thesis aims to address. The first is the apparent levee asymmetry with one side
being consistently higher than the other as discovered in the NAMOC and illustrated in Figure
1.3b. Secondly, the recently found relationship between the sinuosity of modern submarine
channels and the latitude as shown in Figure 1.4c. It can be argued that this inverse relation can
be attributed to several reasons, such as the seafloor or slope gradient, the prevailing topography
of the ocean floor, the tectonic setting, the flow type, and climate conditions during the time of
deposition [Normark et al., 1993; Peakall et al., 2011]. Nonetheless, Figure 1.4c reveals a much
better correlation between peak sinuosity and latitudes with R2=0.74 compared to the peak
sinuosity versus slope gradient illustrated in Figure 1.4d (with R2=0.24). Peakall et al. [2011]
discuss this relation in greater detail and find the most causative controls on this global
distribution to be the Coriolis force, the latitudinal variation of the flow and sediment type. The
observed levee asymmetry is also often attributed to the systematic change of Coriolis force
between the equator and the poles and indicates that the Earth’s rotation might have a large
influence on the growth patterns of these channel systems.
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Fig. 1.4: a) Seismic image of the Amazon Fan at approximately 5° North. b) Seismic image of the NAMOC at 60° North. The figures 1.4c and 1.4d show data of various submarine channels [modified from Peakall et al., 2011]. c) Peak sinuosity versus the Latitude. d) Peak sinuosity versus Slope gradient.
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1.2 The importance of the Coriolis force
Figure 1.5a illustrates the trajectory of a particle with a speed u at two different times, t1
and t2, on a counter-clockwise rotating platform with Ω being the rate of rotation. To an observer
spinning with the platform, the particle seems to have described a trajectory curved to the right
from t1 to its location at t2. However, Figure 1.5a also shows that the trajectory is actually
perfectly straight when it is noted from an observer not rotating with the platform indicated by
the dotted line. The apparent deflection from the perspective by an observer in the rotating frame
of reference is known as the Coriolis effect.
Fig. 1.5: a) Particle motion on a rotating platform. b) Definition of a local Cartesian framework on a rotating spherical Earth. The coordinate x is directed eastward, y northward and z upward and the corresponding velocity components are u (eastward), v (northward) and w (upward) [taken from Cushman-Roisin, 1994]. c) Dependence of the Coriolis force on the latitude φφφφ. The components of the angular velocity Ω of the Earth in the local Cartesian sytem are Ωx = 0, Ωy = Ωcosφ and Ωz = Ωsinφ [Kundu, 1990].
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Hence, equations referring to motion in a rotating frame (such as the Earth) need an additional
term to describe correctly the motion of a fluid or particle. For instance, the Navier-Stokes
equation for incompressible fluids for a rotating frame in vector notation can be written as:
1
2pt
τρ
∂ + ⋅∇ = − ∇ + ∇ ⋅ − ×∂u
u u Ω u [1.1]
[e.g. Tritton, 1989]. The terms on the left represent the temporal and local change of the velocity
field (u and Ω represent vector quantities of the three dimensional flow field and the angular
speed of the Earth respectively). The terms on the right represent forces that act on the fluid
particle. The first term is the pressure gradient force. The second term is the viscous force
defined by the stress tensor, 2ij ijτ µε= ɺ , where µ is the dynamic viscosity and
1
2ji
ijj i
uu
x xε
∂∂= + ∂ ∂ ɺ the strain rate tensor [e.g. Kundu, 1990]. Horizontal scales and velocities are
usually more important than vertical scales and motions in the ocean so that the term w
x
∂∂
is
known to be negligible. The third term represents the Coriolis force (2Ω×u). For a detailed
discussion of how the Coriolis terms arise in this momentum equation, the reader is referred to
common textbooks on geophysical fluid dynamics [e.g. Cushman-Roisin, 1994]. Horizontal and
unforced motion of a particle that is free of any external force (so that viscous and pressure
forces can be neglected) in a rotating frame as in Figure 1.5a can be expressed as:
2Du
vDt
= + Ω [1.2a], 2Dv
uDt
= − Ω , [1.2b]
where u and v describe particle motion in x and y directions, respectively, and Ω is the rate of
rotation perpendicular to the x-y plane. Large-scale geophysical problems should be solved using
a spherical polar coordinate system. However, the horizontal length scales in this thesis are small
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enough so that the curvature of the Earth can be ignored and the motions can be expressed by
adopting a local Cartesian system on a tangent plane [e.g. Kundu, 1990]. Figure 1.5b illustrates a
rotating frame in a three dimensional Cartesian coordinate system with the axis of rotation being
in the north-south direction. Figure 1.5c shows that the Coriolis force changes with latitude φ and
the Coriolis parameter f is defined as f = 2Ω sinφ , where Ω = 7.29 ×10-5 rad s-1 is the Earth’s
rotation about its axis. By definition of the sense of rotation, f > 0 in the Northern Hemisphere
and f < 0 in the Southern Hemisphere, and f changes from f = ± 1.45 × 10 -4 rad s-1 at the poles to
f = 0 rad s-1 at the equator. The Coriolis effect vanishes at the equator as any horizontal motion in
the x-y plane simply translates with the Earth’s rotation at the equator, while the full effect of
rotation is experienced at the poles as here the axis of rotation is now perpendicular to the x-y
plane (Figure 1.5b). From Figure 1.5c it follows that the Coriolis force (and f) gets larger with
increasing distance from the equator and Eq. [1.2a] and Eq. [1.2b] can be rewritten as:
Dufv
Dt= [1.3a],
Dvfu
Dt= − . [1.3b]
For many types of fluid motion the Earth’s rotation can be neglected in the sense that
Coriolis forces are much smaller than the other forces such as friction, pressure gradient,
buoyancy or centrifugal forces. But for large-scale flows in the atmosphere, the ocean or the
Earth’s outer core, where the length scales are so large that transit time scales become
comparable to the timescale of the rotation period of the Earth, Coriolis forces are an important
term in the momentum balance. Assuming that Coriolis forces are large compared to the inertia
of the relevant motion implies that the two terms from Eq. [1.1] can be rewritten as:
|u·∇u| << |Ω×u| . [1.4]
Expressing these forces in terms of relevant scales yields:
U2/L << Ω U [1.5a] or U /LΩ << 1. [1.5b]
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The dimensionless parameter in Eq. [1.5b] can be defined as the Rossby number Ro = U/Lf
(where U is the mean horizontal speed of the fluid and L a characteristic horizontal length scale
[Cushin-Roisman, 1994]). This is an important dimensionless parameter in geophysical flows
that compares the velocity and length scales of motion to the rotation rate of the Earth. When Ro
~ 1 the travel time is comparable to a rotation period and the trajectory will be influenced by the
Earth’s rotation. The smaller the Rossby number gets the more important the rotation and
Coriolis forces become.
Due to the spatial extent of submarine channel systems and the associated long travel
time, the flow properties and environments of large-scale turbidity currents are likely to be
deflected by Coriolis forces [Menard, 1955; Komar, 1969; Wells, 2009] in mid- and high-latitude
systems. For the Grand Banks turbidity current with L = 800 km, f = 9.5 × 10-5 rad s-1 at
approximately 45° North and U = 20 m s-1 a Rossby number of Ro = 0.25 is obtained, which
indicates that Coriolis forces deflected the flow [e.g. Nof, 1996; Wells, 2009]. Even in lakes this
effect can be observed where sediment deposition patterns suggest that the deflection of the
turbidity current by Coriolis forces leads to sediment layers being thicker on the right-hand side
of the lake or fjord in the Northern Hemisphere [Pharo and Carmack, 1979; Syvitski, 1989;
Crookshanks and Gilbert, 2008]. Many direct observations of large-scale oceanographic density
currents confirm that Coriolis forces deflect the bulk of the gravity currents to the right in the
Northern Hemisphere [Davies et al., 2006; Wells, 2009; Sherwin et al., 2010]. Figure 1.6 shows
such a density current in the Faroe Bank channel at 61.5º North [Fer et al., 2010] where Coriolis
forces are balanced by pressure gradient forces which causes a lateral tilt of the interface (∆h) of
about 250 m across the channel of width varying between 5 km to 15 km (Figure 1.6a-c). This
tilt means that overbanking sediment flows are more likely to occur on the right-hand-side of the
channel (looking downstream) for mid- and high latitude systems in the Northern Hemisphere,
13
leading to an asymmetry between levee bank heights [Menard, 1955; Komar, 1969].
Observations of channel systems at higher latitudes have found that the right-hand-side channel
levee is consistently higher in the Northern Hemisphere [e.g. Klaucke et al., 1997] while the left-
hand-side channel levee is higher in the Southern Hemisphere [Droz and Mougenot, 1987; Carter
and Carter, 1988] which correlates with the opposite direction of the Coriolis force in both
Hemispheres. These differences in levee height can reach more than 100 m, as observed in the
NAMOC (shown in Figure 1.3b). The NAMOC exhibits a higher right levee system along a 950
km long section with a mean right-to-left difference of 65 m [Klaucke et al., 1997]. To show that
this asymmetry can be mainly attributed to Coriolis forces is one focal point of this thesis.
Fig. 1.6: a) Measuring locations in the Faroe Bank channel. b) Downchannel component of velocity of a density current deflected by Coriolis forces at location A, B and C in the Faroe Bank Channel [taken from Fer et al., 2010]. The current is displayed by the red color. Flow direction is into the page.
1.3.1 Physical models
Natural turbidity currents usually occur infrequently in remote and hostile environments,
so that field studies have remained fairly limited in their measurements of flow dynamics
[Chikita, 1990; Zeng et al., 1991; Xu et al., 2004; Best et al., 2005; Crookshanks and Gilbert,
14
2008]. Hence, the majority of previous investigations to improve the understanding of turbidity
current dynamics have used small-scale analogue laboratory experiments [e.g. Keulegan, 1957;
Ellison and Turner, 1959; Garcia and Parker, 1993; Simpson, 1972; 1997; Kneller et al., 1999;
Sutherland et al., 2004; Gray et al., 2006; Mohrig and Buttles, 2007; Straub et al., 2008; Islam
and Imran, 2010; Cossu and Wells, 2010]. Such experimental models have offered much insight
into the dynamic characteristics of turbidity currents such as velocity, turbulence and density
structures, and also helped to verify and to improve numerical modelling techniques.
Analogue models are often limited in scale and hence use dimensionless similarity, where
the current is fully characterized by a number of dimensionless variables. As long as the
variables in laboratory currents are comparable with those of the natural current, the experiment
is adequately scaled with respect to the parameters included in that variable [Kneller and Buckee,
2000]. Two of the key parameters for gravity currents are the densiometric Froude number
Fr = U / g 'h (with g’ being the reduced gravity of the density interface and h the mean height
of the current) and the flow Reynolds number Re = U h/ ν, where ν is the kinematic viscosity of
water. These parameters represent the ratio of inertial to gravitational forces (Fr) and the ratio of
inertial to viscous forces (Re) that act on a gravity current. Dimensionless similarity implies that
the Froude number Fr, of the experiment takes the same value as the natural flow. However, it is
much more difficult to achieve similarity in Reynolds number, Re, as natural turbidity currents
often reveal Re at O(106) due to their spatial extent and larger propagation speeds. Viscous forces
can only be neglected if the laboratory flow is fully turbulent, which is generally achieved when
Re > 2000 in a Newtonian fluid [i.e. Leeder, 1982; Kneller and Buckee, 2000]. Large scale
turbidity currents often have speeds in the range of 1-10 m s-1, so if the laboratory flow has a
speed of 0.1 m s-1 the height can be reduced by a factor of 10-100 in order to achieve a similar
15
Froude number when the density difference between the experiment and the prototype is similar
[Middleton, 1993].
For physical models using a rotating framework the Rossby number, Ro, is also a
fundamental scaling parameter. Similar to Fr, the experimental and natural currents have to share
the same value of Ro, which can be achieved by properly scaling the flow velocity, length scale
and rotation rate in the experiment. In this thesis both the width, W, of a submarine channel and
the radius of curvature, R, of a channel bend can be used as a characteristic length scale, so that
two Rossby numbers,
RoW = U/Wf [1.6a] and RoR = U/Rf [1.6b]
are obtained. As U, W and R are usually much smaller in the experiment the rotation rate is
increased to achieve similarity in experimental and prototype Rossby numbers.
One specific problem that often arises is the scaling of sediment in experimental
sediment-laden flows as this also requires a similar dimensionless settling velocity between the
experimental and natural flow. This settling velocity is usually defined as the ratio between the
terminal settling velocity of the sediment and some characteristic velocity scale of the current
[Kneller and Buckee, 2000]. However, even if this parameter can be matched correctly,
electrostatic forces, different sediment particle sizes and concentrations might significantly
change the turbulence structure [Middleton, 1966a; Peakall et al., 1996]. Therefore, many studies
use brine or other dense solutions as a proxy for turbidity currents [e.g. Keevil et al., 2006; Islam
et al., 2008; Darelius, 2008]. This simplifies the current dynamics as deposition and erosion is
neglected in the flow. However, it is assumed that fine-grained turbidity currents are dynamically
similar to saline currents [Stacy and Bowen, 1988a] as low concentration and weakly
depositional turbidity currents exhibit concentration and velocity profiles that are very similar to
saline currents [Kneller and Buckee, 2000; Sequeiros, 2009]. This assumption is also made
16
throughout this thesis. However, so far it has only been shown for “bulk flow” and at the upper
interface in experimental gravity currents [Sequeiros, 2009; Islam and Imran, 2010]. It is
therefore necessary in this thesis to test if fine-grained turbidity currents reveal similar flow
properties near the bottom to saline currents so that this assumption is applicable for all parts of
gravity currents. This investigation is essential to verify the methodology and to transfer results
gained from experimental saline currents to fine-grained turbidity currents. Secondly, a similarity
between both flow types implies that observations from oceanographic studies could also be
applied to large-scale turbidity currents which are of larger interest to geologists.
1.3.2 Velocity structure
Figure 1.7a shows a photograph of an experimental turbidity current with a
corresponding sketch of a typical vertical profile of the downstream velocity (u) in Figure 1.7b.
Fig. 1.7: a) Experimental turbidity current [taken from Wells, 2011]. b) Schematic vertical velocity (u) and density (ρρρρ1111,,,,ρρρρ2222) profiles [modified after Meiberg and Kneller, 2010].
17
The vertical profile of the downstream velocity and turbulence structure of gravity currents has
been analyzed in numerous studies [i.e. Stacey and Bowen, 1988a; Kneller et al., 1999; Gray et
al.; 2006; Islam and Imran, 2010]. The largest velocity (umax) usually occurs close to the bottom
near the density maximum and separates the current into an inner and outer region. The height of
the velocity maximum is controlled by the ratio of the drag forces at the upper and lower
boundaries [Middleton, 1966c; Kneller et al., 1997, 1999]. Due to presence of those two
boundaries velocity profiles often exhibit a ‘bullet-nose’ profile [Middleton, 1993].
In addition, gravity currents exhibit density stratifications that can be classified into two
main profiles [Peakall et al., 2000]. A smooth density profile (ρ1), as depicted by the dashed grey
line in Figure 1.7b, which is usually seen in low-concentration, weakly depositional currents [e.g.
Garcia, 1994; Altinakar et al, 1996] and in saline currents [Ellison and Turner, 1959; Buckee et
al., 2001]. The second is a stepped or Rouse-type profile (ρ2), depicted by the dotted dark grey
line in Figure 1.7b, commonly observed in erosional currents [Garcia, 1993] which are not
discussed in this thesis. The concentration maxima are mostly close to the bottom and the
magnitudes can vary greatly depending on entrainment (autosuspension) or loss (deposition) of
sediment to the bottom. Hence, the description of the Reynolds stresses and drag coefficients at
the bottom are important in order to determine the transport capacity of turbidity currents and
their ability to travel long distances through channels systems.
1.3.3 Secondary flow cells due to centrifugal forces
The architecture, morphological evolution and associated depositional histories of channels is
highly influenced by flow dynamics within the channel, which determine where erosion and
deposition will occur. Hence, the main focus of more recent small-scale physical experiments
has been to investigate internal flow structures and particularly secondary circulations in channel
18
bends [i.e. Corney et al., 2006; Keevil et al., 2006, 2007; Peakall et al., 2007a; Straub et al.,
2008; Islam et al., 2008; Kane et al., 2008; Amos et al., 2010]. Figures 1.8a and 1.8b depict the
flow structure of a density current in a channel bend in the Black Sea [Parsons et al., 2010]. The
flow is forced toward the outer (right) channel bend and generates a cross stream velocity field
with a basal outward directed flow and a return flow above it as sketched in Figure 1.8b.
Fig. 1.8: a) Downstream (upper panel) and cross stream (lower panel) velocity component of a density current in the Black Sea [Parsons et al., 2010]. Flow direction is into the page. b) Location of the measurements and sketch of the corresponding secondary flow cell due to centrifugal forces acting in the channel bend. c) Downstream (upper panel) and cross stream (lower panel) velocity component of a density current in the Baltic Sea [Umlauf and Arneborg, 2009a]. Flow direction is out of the page. d) Location of the measurements and sketch of the corresponding secondary flow cell due to Coriolis forces acting in a straight submarine channel.
19
Previous studies have shown that a primary control on the sense of rotation of helicity is the
downstream velocity profile and especially the height of the downstream velocity maximum
above the bed [e.g. Corney et al., 2006, 2008] although other factors such as cross-sectional
geometry greatly influence flow processes [Islam et al., 2008; Straub et al., 2008]. Though there
has been a lively debate on the sense of rotation of the secondary flow structure in the bend apex,
both flow directions ultimately lead to comparable depositional features with a growth in
sinuosity of the channel [Amos et al., 2010].
The lateral momentum equation in a channel bend can be derived from Eq. [1.1] and is,
for instance, analyzed in greater detail in Nedziecko et al. [2009]. Under steady conditions and
the neglect of viscous forces and the non-linear advection terms it reduces to
2
0
1U pfU
R yρ∂= −∂
[1.7]
which represents the momentum balance between Coriolis forces (left-hand-side), centrifugal
forces and across-stream component of the pressure gradient forces on the right-hand-side
respectively. Sedimentation processes and channel evolution in bends have been attributed
mainly to the internal flow structure resulting from centrifugal and pressure gradient forces by
omitting Coriolis forces in Eq. [1.7]. For instance, centrifugal forces lead to a superelevation and
overspilling of the bank by the current and to a more prominent levee system at the outer bend
[e.g. Straub et al., 2008; Kane et al., 2010] and to sediment accumulations at the inner bend
inside the channel; the latter are called lateral accretion packages [Abreu et al., 2003].
20
1.3.4 Secondary flow cells due to Coriolis forces
As shown in Figure 1.6, Coriolis forces can influence gravity currents through the
deflection of the flow. In a straight channel (where no centrifugal forces act on the current) the
across stream momentum balance for quasi-steady motion can be expressed by:
2
2
1E
p vfU
y zν
ρ∂ ∂= − +∂ ∂
, [1.8]
where viscous forces are now considered through the eddy viscosity approach represented by the
second term on the right-hand side with νE being the eddy viscosity coefficient [Tritton, 1989].
Viscous forces are only important near the upper and lower boundary regions (Ekman boundary
layers, see Chapter 3), but they can give rise to secondary flows throughout the entire current
thickness. The Figures 1.8c and 1.8d illustrate observations of a density current in a straight
channel in the Baltic Sea [Umlauf and Arneborg, 2009a]. The flow exhibits a secondary flow
field similar in magnitude to the one in the Black Sea in Figure 1.8a and 1.8b, but now due to the
presence of Coriolis forces. In the Northern Hemisphere Ekman boundary layer flows will be
deflected to the left and flow in the interior of the current will be deflected to the right channel
wall so that a secondary transverse circulation is superimposed on the downstream flow, as
sketched in Figure 1.8d. Qualitatively similar secondary flows to Figure 1.8d driven by Coriolis
forces have been monitored in oceanic gravity currents, i.e. in the Vema channel [Johnson et al.,
1976], in the Faroe Bank Channel [Johnson and Sanford, 1992; Fer et al., 2010] or in the Ellet
Gully [Sherwin, 2010]. These oceanographic studies found that rotating gravity currents rapidly
come into a geostrophic balance, where the trajectory of the density current is determined by a
balance between buoyancy forces, friction and Coriolis forces as described in Eq. [1.8]. The
basic features of such rotating currents have also been seen in several laboratory experiments
21
[Benton and Boyer, 1966; Hart, 1971; Johnson and Ohlsen, 1994; Davies et al., 2006; Darelius,
2008; Wåhlin et al., 2008].
Turbidity currents in channels should also experience similar secondary flow patterns to
large-scale oceanic density currents in channels, when the flows are at large enough scales that
Coriolis forces become important. This is significant as secondary flow structures in turbidity
currents are known to play a major role for the growth and evolution of submarine channel
systems. Though the influence of Coriolis forces upon turbidity currents is acknowledged in
several studies [Middleton, 1993; Nof, 1996; Klaucke et al., 1997; Emms, 1999; Imran et al.,
1999; Pirmez and Imran, 2003] it has almost been neglected in the majority of geological studies
of submarine channel systems. When Coriolis forces are mentioned it is usually in the context of
the theory of Komar [1969] who introduced a momentum balance similar to Eq. [1.7] for gravity
currents flowing in a channel bend. This mathematical description of the tilt of the interface is
2 , dh hf h
Frdy U R
= +
[1.9]
where dh/dy represents the interface slope across the channel. This theory has been used to
derive flow parameters from morphological settings [Bowen et al., 1984; Klaucke et al., 1997]
and has been cited numerous times in the geological literature but no experiment has ever tested
its validity. In addition, the standard usage of Eq. [1.9] assumes that the Froude number remains
constant at a value of one and that rotation has no control on the velocity of the current.
However, this is contradictory to the observations of Cenedese et al. [2004] and Cenedese and
Adduce [2008] who report a large reduction in velocity when the Coriolis parameter is high.
Another significant issue in the theory of Komar [1969] is the neglect of boundary friction which
can be described more accurately by traditional bottom boundary layer dynamics in
oceanographic studies. Therefore this thesis aims to gain more insight into the applicability of
22
Eq. [1.9] in order to derive flow parameters more accurately from geological settings in
channels.
1.4 Motivation and thesis overview
Many observations of oceanographic density currents have shown that Coriolis forces are
important for the flow dynamics as they deflect the fluid to the right-hand-side in the Northern
Hemisphere. However, observations of levee asymmetries suggest that turbidity currents
transporting sediment through large channel systems are also influenced by the Earth’s rotation.
To date, geological studies refer mostly to the theory of Komar [1969], which led to reasonable
estimates of flow parameters of turbidity currents. However, as outlined in the previous section,
this simple momentum balance does not describe the internal flow structure adequately, as it
neglects frictional effects, nor has it ever been tested against a physical model. With conceptual
models that aim to explain the evolution and growth of submarine channels, the focus has
recently been on more accurate descriptions of the flow field in turbidity currents. But due to the
neglect of Coriolis forces, previous experimental studies are insufficient to explain levee
asymmetry at only one bank or varying sinuosity observed in channel systems at different
latitudes.
This thesis contributes to the understanding of the internal flow structure of large-scale
turbidity currents driven by the interplay of centrifugal, pressure gradient and Coriolis forces, by
using physical modelling. This helps to develop further conceptual models [Clark and Pickering,
1996; Peakall et al., 2000; Amos et al., 2010] that describe the evolution of submarine channel
systems that are influenced by the rotation of the Earth. This thesis consists of four independent
papers that aim to answer the aforementioned problems step by step.
23
The methodology is based on physical modelling techniques that underlie the assumption
that saline experimental currents are dynamically similar to weakly-depositional sediment-laden
currents. This has been proven predominantly for the center and upper part of gravity currents
[e.g. Sequerios et al., 2009; Islam and Imran, 2010] but not for the bottom boundary region.
Chapter 2 examines the turbulence structure between saline and sediment-laden experimental
flows at this lower boundary and systematically investigates if saline density currents are a good
surrogate for turbidity currents. The experimental results are described and compared with
similar experiments in other studies. Particular attention is given to the Reynolds stress
distribution and drag coefficients in the bottom boundary layer.
Chapter 3 analyzes the influence of Coriolis forces on the dynamics of gravity currents
flowing in straight submarine channels. Due to the straight channel geometry no centrifugal
forces arise so that the momentum balance is reduced to the simple form of pressure gradient and
Coriolis forces. The transverse velocity structure, downstream velocity and interface slope are
investigated and compared with the theory of Komar [1969]. A more complex mathematical
model using Ekman boundary layer dynamics [Wåhlin et al., 2008; Darelius, 2008] is introduced
and also compared with experimental measurements. The results are discussed in terms of
observations in modern submarine channels.
Chapter 4 transfers the problem of Chapter 3 to more complex channel geometries. The
internal flow structure in sinuous submarine channels under the influence of Coriolis and
centrifugal forces using laboratory experiments is examined. Both forces can drive the secondary
circulation of turbidity currents in sinuous channels and determine where erosion and deposition
of sediment occur. The relative importance of Coriolis and centrifugal forces is described in
terms of the Rossby number RoR based upon the radius of curvature, which can be used to
classify if a channel system is dominated by Coriolis or centrifugal forces.
24
Previous conceptual models [e.g. Clark and Pickering, 1996; Peakall et al., 2000; Amos
et al., 2010] are able to describe the evolution of submarine channels, the growth of sinuosity and
levee deposits, but are unable to explain the relation between sinuosity and latitude described in
Figure 1.4c [Peakall et al., 2011]. In Chapter 5 this relation is investigated by an analysis of how
strongly the internal flow structure in gravity currents is influenced by Coriolis forces. These
observations are combined with an existing conceptual model for sedimentation and erosion in
sinuous channels. Depositional patterns between high and low latitudes are contrasted by
including Coriolis forces and their implication for the evolution of submarine channel systems is
discussed.
The main conclusions of this thesis are summarized in Chapter 6 and suggestions are
made for future work.
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Chapter 2 A comparison of the shear stress distribution in the bottom boundary layer of experimental density and turbidity currents Remo Cossu and Mathew G. Wells Abstract
The internal stress distribution within weakly depositional turbidity currents has often been
assumed to be similar to saline gravity currents. This assumption is investigated by analyzing a
series of experiments to quantify and compare the shear stress distribution in the bottom
boundary layer (BBL) of saline and particle-laden gravity currents. Vertical profiles of Reynolds
stresses, viscous stresses and turbulent kinetic energy (TKE) were obtained from the mean
downstream velocity profiles and turbulent velocity fluctuations, and were broadly similar in
both flow types, suggesting that saline gravity currents are a good analogue to turbidity currents.
Maximum positive Reynolds stresses occur where the velocity gradient is largest in the BBL but
below this maximum the Reynolds stresses decrease significantly and are balanced by an
increase of viscous stresses. The bulk drag coefficient CD is defined for both flows using three
methods: i) a log-fit method based on the law of the wall, ii) the observed maximum total stress
and iii) direct measurements of turbulent velocities. The CD values of both flow types were
broadly similar but each method led to CD values of different orders of magnitude. The log-fit
method yielded the largest drag coefficients of O(10-2) whereas measurements of turbulent
velocities gave relatively small values of O(10-4). The best correlation with drag coefficients
observed in field measurements of O(10-3) was obtained by using the maximum total stresses
32
next to the wall. The variation of CD is discussed in relationship to parameterization methods in
experimental and numerical modelling.
2.1 Introduction
Gravity currents are important environmental flows that are driven by a density
difference with the ambient water, usually caused in a difference in temperature, salinity or due
to suspended sediment. Gravity currents that are driven by suspended sediments are known as
turbidity currents and are important agents to transport sediments in lakes and oceans. Turbidity
currents can be triggered by numerous mechanisms. For example, from a sediment-laden river
entering a lake, or the sloping layers of sediment on the continental shelf becoming unstable
because of loading, underground gas release or seismic activity [Piper and Normark, 2009;
Meiburg and Kneller, 2010]. A key feature of turbidity currents is that they have the ability to
erode sediment if they are moving fast enough so that shear stresses exceed a critical threshold
appropriate to entrain bed material; a process known as self-acceleration and autosuspension
[Bagnold, 1962; Garcia and Parker, 1993; Sequeiros et al., 2009]. Due to this process turbidity
currents can travel large distances before they finally deposit sediment as the currents slow and
shear stresses decrease. On geological time-scales a series of such turbidity currents can form
large-scale features such as submarine fans and thick layers of sedimentary rock within deep
ocean basins [Normark et al., 1993; Weimer and Slatt, 2007].
As natural turbidity currents usually occur in remote and hostile environments, field
studies have been fairly limited in their measurements of flow dynamics [Chikita, 1990; Zeng et
al., 1991; Xu et al., 2004; Best et al., 2005; Crookshanks and Gilbert, 2008]. Hence, the majority
of previous investigations into the dynamics of turbidity currents have used analogue laboratory
experiments [e.g. Garcia and Parker, 1993; Simpson 1972, 1997; Kneller et al.; 1999; Gray et al.,
33
2006; Mohrig and Buttles, 2007; Straub et al., 2008; Islam and Imran, 2010; Cossu and Wells,
2010] to describe the relationship between the velocity and density difference, or to determine
the internal turbulence structure that leads to erosion and transport of sediment. The internal
turbulent dynamics and shear stress distributions of oceanic saline density currents have received
considerable attention [Johnson et al., 1994; Dallimore et al., 2001; Peters and Johns, 2006;
Umlauf and Arneborg, 2009a] in contrast to sediment-laden flows that are usually hard to
monitor in the field. An open question remains as to how relevant the internal dynamics of either
large-scale oceanographic overflows or laboratory-scale saline density currents are to
understanding the dynamics of sediment laden turbidity currents, as has often been implicitly
assumed in experimental studies that describe turbidity current dynamics using saline density
currents [e.g. Kneller et al., 1999; Garcia and Parsons, 1998; Keevil et al., 2006]. The important
issue is to determine the differences between saline and turbidity currents that arise due to the
potential settling of particles in turbidity currents. For instance, in experiments with similar
density currents and turbidity currents, Gray et al. [2006] found larger Reynolds stresses and
turbulent kinetic energy (TKE) in the turbidity currents. In these experiments they used glass
ballotini with a mean diameter of 70 µm. In contrast, Islam and Imran [2010] noticed a good
agreement of Reynolds stresses and TKE between similar turbidity and density currents, when
using silica powder with a mean diameter of 25 µm for the particulate gravity currents. This
discrepancy in findings between the two studies might be attributed to the use of different
particle sizes and suggests a necessity to further distinguish turbidity currents, e.g. between
strongly depositional and non-depositional or weakly depositional currents based on the grain
size they transport. A question that motivates the present study is to determine how similar the
near bed turbulent shear stresses in turbidity currents are to the more widely studied saline
currents.
34
Most previous experimental studies of gravity current dynamics [e.g. Kneller et al., 1999;
Gray et al., 2006; Islam and Imran, 2010; Buckee et al., 2001] have mainly focused on the
turbulence structure at the upper boundary, and only a few measurements have been reported
very close to the bottom, so that flow properties in the bottom boundary layer (BBL) are still
poorly understood. The area between the maximum downstream velocity (umax) and the bottom
of gravity currents is called the inner region, and here the velocity generally reveals a non-linear
profile caused by friction at the lower boundary [Kneller et al., 1999; Altinakar et al., 1996]. For
instance, some studies on gravity currents [Garcia and Parker, 1993; Kneller et al., 1999;
Dallimore et al., 2001; Peters and Johns, 2006; Odier et al., 2009; Sherwin, 2010] have shown
that the BBL is only a small fraction of the total flow depth d of gravity currents and hence is
generally difficult to resolve in laboratory experiments. We note that other experimental studies
[Sequeiros et al., 20010a,b] report a larger inner region based on a subcritical Froude number
(Fr) or a rougher surface of the boundary. The BBL occupies the lowest part of inner region
where a significant increase in velocity can be observed [Tritton, 1989]. Despite having a small
proportion of the total depth, the turbulence structure and resulting Reynolds shear stresses in
this layer are very important because they define whether turbidity currents will have a
depositional or an erosive character [Garcia and Parker, 1993] which in turn strongly influences
the dynamics and the persistence of turbidity currents. Based on our observations of the velocity
profiles described in section 4.1 (of Chapter 2) we assume that the thickness of BBL is less than
10% of the total thickness h of our experimental flows so that z/h < 0.1 with z being the vertical
distance from the boundary.
The magnitude of the bottom stress is often parameterized in terms of a dimensionless
drag coefficient (CD) which relates the friction velocity u* to the mean downstream velocity U of
a flow. For instance, empirical values of CD have been used to estimate the bottom stress and to
35
determine the erosional capacity of density currents in depth-averaged mathematical models.
However, laboratory estimates of CD of gravity currents [e.g. Garcia and Parker, 1993; Straub et
al., 2008] are often of O(10-2), which is much higher than suggested by direct field observations
[Peters and Johns, 2006; Umlauf and Arneborg, 2009a] where CD = 10-3. Part of this difference
could be due to the variations in the nature of the boundary or due to the differences in how CD is
estimated in the experimental flow.
In this study we investigate flow properties for both turbidity currents and saline gravity
currents by making high resolution velocity and turbulence measurements within the BBL. The
shear stress distribution in the BBL of turbidity and saline density currents is investigated using
several measurement points within the bottom centimetre of the flow with a high resolution
Acoustic Doppler Velocimeter (ADV). In addition, we determine the Prandtl mixing length in
the BBL which relates the Reynolds stresses to the mean velocity gradient and compare it with
results observed outside the BBL by Odier et al. [2009]. Finally we determine CD values using
three different methods: (i) a log-fit method based upon the law of the wall [Kneller et al., 1999;
Straub et al., 2008], (ii) the maximum total bottom stress and (iii) direct observations of turbulent
velocities near the base as used by Dallimore et al. [2001]. We compare the CD values and
discuss each method in terms of its applicability. Some basic physical boundary layer processes
associated with turbulence structure are introduced in section 2. The experimental setup is
described in section 3. Results for the velocity, Reynolds stress and TKE distribution as well as
CD values are presented in section 4. We finish with a discussion of our observations and
compare them with field observations of oceanographic scale gravity currents in section 5 and
our conclusions in section 6.
36
2.2 Shear stresses in the BBL
Reynolds stresses play a dominant role in the mean momentum transfer by turbulent
motion and reflect stresses that are imposed by the turbulent velocity fluctuations on the mean
flow [Gray et al., 2006]. The magnitude of the shear stress in the BBL determines the sediment
transport capacity of turbidity currents and whether deposition or erosion processes dominate the
regime at the bottom boundary. In the literature the shear stress term in the momentum equation
of gravity currents is often related to the downstream velocity gradient using
( )R v E
u
zτ τ τ υ µ ∂= + = +
∂ [2.1]
[Stacey and Bowen, 1988] where τ is the total shear stress, τR the Reynolds and τv the viscous
stress respectively, µ is the molecular viscosity, νE is the eddy viscosity coefficient of
momentum and u the downstream velocity. The BBL can be further subdivided into a very thin
viscous sublayer at the base, where viscous forces are dominant, and a layer above it, where
viscous forces can be neglected and instead the velocity gradient depends on the shear stress and
the eddy viscosity [Tritton, 1989].
The shape of the velocity profile at the bottom of a gravity current in the viscous boundary layer
(log-boundary layer) is often described by a logarithmic profile of the form:
( ) *
o
u zu z ln
k z
=
[2.2]
where κ = 0.41 is the von Kármán constant, and u(z) is the velocity taken at the height z above
the bed and z0 represents the zero-velocity roughness height [Tennekes and Lumley, 1972;
Kneller at al., 1999]. We note that u* is a constant that represents a bulk value (vertically
averaged) of the friction velocity in the inner region. The oceanographic observations of Johnson
et al. [1994] showed that in a 200 m deep density current only the bottom 20 m had a well-
37
resolved logarithmic velocity profile where there was a constant shear-stress layer which is
assumed in deriving the logarithmic profile (and hence u*) in Eq. [2.2]. If the same proportions
hold in laboratory density currents (which are usually less than 0.3 m in thickness) that exhibit a
similar velocity structure as observed by Johnson et al. [1994], the log-boundary layer described
by Eq. [2.2] would only occupy a small region above the bottom unlike in channel flows where
the full depth of the flow is a log-boundary layer. Hence it is more difficult to resolve accurately
such a logarithmic boundary layer in a laboratory scale gravity current.
The friction velocity u* of gravity currents is related to the bottom stress τB near the wall
and the density ρ by using
τρ
*= Bu , [2.3]
[e.g. Tennekes and Lumley, 1972]. The relation between u* and the vertically averaged mean
flow velocity U of gravity currents can then be used to define CD as:
CD = u *2
U2, [2.4]
[e.g. Garcia and Parker, 1993]. In this study we determine the friction velocity u* both from log-
fit curves (using Eq. [2.2]) of the measured velocity and from direct measurement of the
maximum bottom stress τB (following Eq. [2.3]).
In addition, we use a third method reported in Dallimore et al. [2001] to calculate CD values
where Reynolds stress terms u'w' (along the flow) and v 'w' (perpendicular to the flow) were
measured to determine a turbulent velocity with
[ ] 41
22 )''()''( wvwuut += . [2.5]
In order to use Eq. [2.5] to calculate CD and compare it with the other methods we treat this
38
turbulent velocity as a bulk parameter by averaging it over the thickness of the BBL and use the
notation ût to distinguish it from u* hereafter.
2.3 Method
To investigate the BBL dynamics such as the velocity and turbulence structure in both
saline and particulate-laden gravity currents we conducted a series of lock-release experiments in
a horizontal tank. This popular experimental set-up has been used in many studies [Middleton,
1966; Kneller et al., 1999; Shin et al., 2004; Monaghan et al., 2009] to study the dynamics of
gravity currents. The tank consists of two compartments separated by a vertical lock as shown in
Figure 2.1. A fluid with a higher density is generated in the smaller separated compartment, and
when the lock is removed this denser fluid exits and flows as a gravity current beneath the lighter
fluid. The experimental apparatus used for the present work consisted of a horizontal tank with a
lock exchange section and a smooth floor (Figure 2.1).
Fig. 2.1: Schematic of the dam-break experimental setup.
The tank had a width of 0.30 m and total length of 6 m, of which the lock compartment
occupied about 1.40 m. The tank was filled with tap water at 13-15 °C to a depth of 0.28 m so
that the volume of the lock compartment comprised approximately 120 L. The aspect ratio
defined by tank width to water depth was therefore comparable to the previous laboratory
39
experiments studying turbidity currents [e.g. Kneller et al., 1999; Buckee et al., 2001; Gray et al.,
2006; Islam and Imran, 2010; Monaghan et al., 2009; Gladstone and Pritchard, 2010].
In order to compare meaningfully the shear stress dynamics in the BBL between turbidity
and saline density currents, the initial density contrast was kept constant in all experiments. The
denser fluid was produced by adding either sediment or salt to the lock compartment and stirring
it with two agitators until a well mixed suspension or brine was achieved. The agitators were
switched off 15 s before the lock was removed and the denser fluid was then released into the
main body of the tank. In all the experiments either 1.5 kg of sediment or salt were added to the
lock compartment so that initial density contrast was almost identical for each flow with ∆ρ =
11.9 kg/m3. The sediment used for the sediment-laden flows was silicon carbide (SiC), which has
a density of 3220 kg m-3 and a mean diameter of 27.5 µm. The particle size distribution is
illustrated in Figure 2.2.
Fig. 2.2: Distribution for the SiC particles. The mean grain size diameter is approximately 27.5 µm.
40
The particle settling velocity wp of these fine sediments can be estimated using the
empirical equation
ρ ρ
ν× × ×= ×
2 0.281 ( - )18P
s or g Ew [2.6]
[Dietrich, 1982] with r the mean radius of the particle, g the gravitational acceleration, ρo the
density of the ambient fluid, ρs the density of the sediment,ν the kinematic viscosity of water and
E the Janke shape factor of the particle [Dietrich, 1982]. For non-spherical particles this factor is
always smaller than unity but for an upper boundary we used the maximum shape factor E = 1.
This yields a maximum settling velocity of approximately wp = 9.1 × 10-4 m s-1. Hence, the
settling velocity is of the same order as in Monaghan et al. [2009] who also used SiC with a
mean diameter of 26 µm (wp = 8.18 × 10-4 m s-1) but with a smaller settling velocity than
wp = 4 × 10-3 m s-1 in Gray et al. [2006]. Flow velocities were measured at a point with a
NORTEK Vectrino ADV at a sampling rate of 100 Hz. The ADV is an acoustic velocity sensor
(consisting of one transmitter and three receivers) which uses the Doppler shift of the reflected
pulses to determine the fluid velocity. The receivers are slanted at 30o from the axis of the
transducer and focus on a common sample volume of 160 mm3 (averaging vertically over 5-6
mm), that is 50 mm away from the probes. This ensures nearly non-intrusive flow measurements
within the flow field of the current. The ADV makes simultaneous measurements of the three
velocity components at high sampling rates [Voulgaris and Throwbridge, 1998]. All ADV
measurements were taken 1.8 m away from the lock gate. The accuracy of the ADV instrument
is 0.5% of the measured velocity and hence the error is negligible for the velocity range
described in the next section.
A typical experiment lasted for 150 s after the lock gate was lifted and the higher density
fluid started to exit the compartment. The front of the dense current formed a head with the
41
typical overhanging nose [Simpson, 1969] that reached the measuring location after
approximately 30-35 s. Behind the head the density current was thinner, which is associated with
the characteristics of the body of the current. After the passage of the head the flow conditions
remained fairly constant. Several test runs demonstrated that both the distance and the time
between the release of the current and the start of the recording were sufficiently large enough so
that the gravity currents were not biased by any initial conditions, for instance, the removal of the
lock gate or the stirring of the agitators. For instance, we found very good agreement of velocity
profiles and turbulent parameters between the measuring location at 1.8 m and 2.8 m away from
the lock which showed typical distributions known from other studies [Gray et al., 2006; Islam
and Imran, 2010]. On the other hand, at a 0.8 m distance in particular, the Reynolds stress
distribution had not fully developed as it was still biased by initial conditions.
In most of the analyses the focus was on the near-bed downstream velocity profile,
consisting of 10 measurement points at 3, 4, 5, 6, 8, 10, 20, 30, 40 and 50 mm above the bottom
of the tank. For some experiments additional measurements at 60, 80, 100 and 120 mm above the
bottom were added. The depth of the gravity currents within the sampling interval of 30 s was h
= 0.12 m which was determined using the integral definition of depth from Ellison and Turner
[1959] where 0 0
( ) ( ) h u z z dz u z dz∞ ∞
= ∫ ∫ . Hence, the measurements represent the bottom 1/3-1/2
of the gravity current. To obtain one velocity profile required that 10 equivalent runs be made,
and that the ADV was raised between each run. The u-velocity reflects the streamwise, the v-
velocity the across stream and the w-velocity the vertical velocity component. Turbulent
properties were then extracted by defining the turbulent fluctuations from the mean flow, as
described in more detail in section 4.2.
42
After the experiments we observed only very thin deposits from the sediment-laden flows
on the tank floor near the measuring location with most of the sediment being deposited in the
sump. In the discussion section we show that within the main body of the current, where our
measurements were focused, velocities and velocity fluctuations remained large enough to keep
particles in suspension. We therefore assume that the main deposits on the tank floor must have
settled out in the tail section of the current where velocities decreased significantly. As this
sedimentation occurs outside of the measuring interval this had no affect on our results.
2.4.1 General flow properties
Figure 2.3a depicts experimentally determined velocity profiles of the saline and
particulate gravity currents. The level of umax occurs between z/h = 0.25-0.35 for both saline and
the sediment-laden flows. The velocity maxima can be considered as the top of the inner region
[Kneller et al., 1999] whereby the BBL only occupies a fraction of this depth [e.g. Dallimore et
al., 2001] at z/h < 0.1 (Figure 2.3a).
Fig. 2.3: Vertical distribution of the downstream velocity component. The horizontal bars indicate the standard deviation of the ADV data. a) Velocity distribution over the entire thickness of the current. b) Various curves added to the velocity data using the law of the wall approach in the BBL. R2 represents a least-squares fit of the data. Note that the graph in b) is plotted with a semilog axis.
43
Both the saline and particulate laden gravity currents had similar downstream velocity profiles.
Our analysis focuses hereafter on the inner region between the bottom z/h = 0 - 0.4 as shown in
Figure 2.3a. Figure 2.3b shows the velocity measurements at a higher resolution within the BBL
between z/h = 0 - 0.1. The dotted lines describe a possible fit of the logarithmic velocity profile
of Eq. [2.2] to the experimental data for the saline (R2 = 0.84) and turbidity current (R2 = 0.82)
obtained by a least squares fit of the data.
Lock-release gravity currents usually have Fr of order one [Shin et al., 2009], which is
defined as / 'Fr U g h= where g’ is the reduced gravity ′g = g (ρu-ρa) / ρa with ρu the density
of the underflow, ρa the density of the ambient water. The mean downstream velocity in our
experiments was U = 0.05 ± 0.001 m s –1, giving Fr ~ 0.43 for both the saline and particulate
gravity flows. We note that this estimation is based on the initial density contrast. Due to mixing
processes and entrainment of water the density difference g’ decreases as the flow evolves so
that the actual Fr will be slightly higher. However, such a small increase will not affect the flow
properties significantly so that this value of Fr should be treated as a lower limit. Such a value of
Fr is broadly similar to many previous experimental observations of gravity currents where 0.2 <
Fr < 1.3 [Garcia and Parker, 1993; Simpson, 1997; Kneller et al., 1999; Gray et al., 2006; Islam
and Imran, 2010] and in good agreement to the theoretical model introduced by Benjamin
[1968]. For the velocity profiles shown in Figure 2.3a, the bulk Reynolds number is
approximately Re = 6000 where Re= U h/ν, with ν is the kinematic viscosity. This value of Re
implies that the flow was fully turbulent and comparable to other experimental turbulent gravity
currents, e.g. Re = 2.7 × 103 Kneller et al. [1999], Re = 2 - 6 × 103 Gray et al. [2006], Re = 7.2 ×
103 Monaghan et al. [2009] or Re = 1.4 × 104 Islam and Imran [2010]. A detailed description of
all our relevant experimental parameters is given in Table 1.
44
Tab. 2.1: Summary of parameters for experimental gravity currents
45
2.4.2 Velocity fluctuations
We characterize the distribution of shear stress and turbulent kinetic energy (TKE) by
analyzing the velocity fluctuations in the body of the gravity current, i.e. after the passage of the
flow front and before the tail arrives at the measuring location. For our experiment the body of
the gravity current lasted over 30 s. The data shown in Figure 2.4a and 2.4c are time series of
downstream velocity (u) measured approximately 4 cm (z/h = 0.33) above the tank floor for a
saline and sediment-laden gravity currents. Generally, the downstream velocity is one order of
magnitude larger than the across-stream and bed-normal velocities. Saline gravity currents
showed similar velocity time series data compared to the sediment-laden gravity currents, with
the velocity fluctuations at the same order of magnitude as in similar experimental flows
described by Kneller et al. [1999], Gray et al. [2006] or Islam and Imran [2010].
Fig. 2.4: Time series of downstream velocity components (u) for saline and sediment-laden gravity current taken approximately z/h = 0.33 a,c) raw data reflecting the instantaneous velocities and b,d) averaged velocity ū over a 100 ms time window and turbulent velocity fluctuations u’ after subtracting u- ū.
Velocity fluctuations were obtained by subtracting a smoothed time series from the
measured data set, e.g. as u’ = u – ū, where u indicates the raw data obtained by the ADV
measurement at a sampling rate of 100 Hz and ū the smoothed local velocity component. The
smoothing of the data was done by filtering the raw data with a 100-point moving average to
46
determine ū, as in Kneller et al. [1999]. Hence, the temporal length of the filter used for the
calculation was 1 s and yielded comparable turbulent fluctuations obtained in previous studies
[Kneller et al., 1999; Islam and Imran, 2010]. This decomposition of time series data into a mean
ū and a fluctuating component u’ for the downstream velocity u(z) is plotted in Figure 2.4b and
2.4d. Usually the turbulent fluctuations are at least one order of magnitude smaller than the mean
(smoothed) values.
The sampling volume of the ADV was chosen to be large enough that potential bias due
to noise was kept at a minimum which resulted in a signal data quality for each flow with a
correlation of > 95 %. In addition, the time series data were analyzed and filtered with a spike
detection routine so that any corrupted data larger than 2.5 times of the standard deviation was
removed from the time series.
47
2.4.3 Reynolds stresses
The bed normal Reynolds stresses are obtained from the turbulent fluctuations of
downstream u’ and bed-normal velocity w’ components according to
τ R=-ρ u'w' [2.7]
[Tennekes and Lumley, 1972]. The mean Reynolds stress distribution using Eq. [2.7] for z/h <
0.4 is shown in Figure 2.5a for turbulent saline gravity currents, and in Figure 2.5b for sediment-
laden gravity currents.
Fig. 2.5: Profiles of Reynolds stress and viscous stress in the BBL for saline (a) and sediment-laden (b) gravity currents. All profiles are normalized by ρρρρU2. The horizontal bars indicate the standard deviation. The horizontal dashed line indicates the viscous boundary layer.
In both cases the Reynolds stresses are normalized by ρU2. Both the experimental saline and
particulate gravity currents have the highest positive Reynolds stresses near the bottom (z/h ~
0.1). The saline gravity current has a maximum normalized Reynolds stress of 1.5 ± 0.5 ×10-3,
which is significantly larger than the maximum of sediment-laden gravity current with 0.8 ± 0.45
×10-3. Below the maxima at z/h < 0.1 the Reynolds stresses decrease significantly towards the
bottom. Around and above umax at z/h = 0.25-0.35 (Figure 2.3a) the Reynolds stresses are close to
zero, and stresses become negative in the interfacial region where the velocity gradient is
48
negative. Those values are consistent with Reynolds stresses reported by Gray et al. [2006] and
Islam and Imran [2010]. A new experimental observation is the distinct decrease in Reynolds
stresses for z/h < 0.1, which has not been described in any previous gravity current experiments.
The viscous stress τ
v= µ ∂u
∂z is normalized by ρU2 and is also shown in Figure 2.5a and 2.5b
using the measured velocity gradient and µ = 1.17 ×10-3 N s m-2. Maximum velocity gradients
occur near the base, but away from the viscous boundary layer (VBL) there is a dramatic
decrease in vτ between z/h = 0.025-0.1 with increasing height. We can determine the thickness
of the VBL (δVBL) with the empirical formula δVBL = 8 µ/(ρ u*) [Tritton, 1989] where u* is
calculated using Eq. [2.3] with a depth averaged τB = 2 × 10-3 for saline and τB = 2.5 × 10-3 for
sediment-laden flows (from Figure 2.5a and 2.5b). This yields δVBL = 0.0042 m and δVBL =
0.0037 m (see Figure 2.5a and 2.5b) indicating that VBL occupies only a small region of the
entire BBL. According to Eq. [2.1] the total stress is obtained by addition of the two stress
components as R vτ τ τ= + . The largest positive total stresses are found close to the bottom,
where with increasing height Reynolds stresses show a significant increase which balances
decreasing viscous stresses so that the total stress is roughly constant. Above the Reynolds stress
maxima (at z/h > 0.1) the total stress gets significantly smaller.
The strong dependence of the Reynolds stress upon the velocity gradient is depicted in
Figure 2.6 where Reynolds stresses and velocity gradient are related to each other. Only around
umax, where du/dz is almost zero, are small stresses prevalent. The observed Reynolds stress
changes sign from the positive (below umax) to negative (above umax) corresponding to changes in
the velocity gradient du/dz. The largest positive Reynolds stresses coincide with the large
positive velocity gradient which is close to the bottom (Figure 2.5). Generally, we find a
49
favourable linear correlation between the Reynolds stress and the velocity gradient between -2 s-1
< du/dz < 3 s-1 for the particle-laden flow while there is a larger variance for the saline flows. For
du/dz > 3 s-1 a few stress values deviate from the linear correlation (depicted by gray squares and
dots in Figure 2.6) which we attribute to the close proximity to the bottom where du/dz has
maximum values and where viscous stresses dominate over Reynolds stresses (Figure 2.5).
Fig. 2.6: Relation between the velocity gradient du/dz and the normalized Reynolds stress ττττR/ρρρρU2 across the flow thickness. The error bars indicate the standard deviation.
The relationship between stress and velocity gradient was also investigated by Odier et al.
[2009]. They conducted supercritical (Fr >1) experimental saline density currents along an
inclined plane to investigate mixing processes outside the BBL. Their flow thickness was h = 6
cm and U = 6 cm/s, so that Re ~ 3000 and their flow was similarly turbulent (but supercritical) to
our experimental gravity currents. They found the Prandtl mixing length model to be a good
approximation to describe mixing processes in stratified gravity currents by relating Reynolds
50
stresses to the mean velocity gradient with:
z
u
z
uLwu m ∂
∂×∂∂= 2'' [2.8a],
z
u
z
uwu
Lm
∂∂×
∂∂
= ''2 [2.8b].
The Prandtl mixing length model implies that the eddy viscosity coefficient νE in Eq. [2.1] is a
linear function of the velocity gradient, so that νE = Lm2×∂u/∂z [2.8a] where Lm is the mixing
length. Lm can then be calculated using Eq. [2.8b] and resulting length scales are plotted
in Figure 2.7.
Fig. 2.7: Mixing length Lm of saline and sediment-laden gravity currents using Eq. [2.8b]. The error bars indicate the standard deviation.
In the BBL (z/h < 0.1) and in the upper part of the flow (z/h > 0.5) the mixing length is
significantly smaller than in the interface region previously studied by Odier et al. [2009] who
observed a fairly constant Lm = 0.45 ± 0.1 cm throughout the entire flow outside the boundary
regions. In the BBL the inferred mixing lengths were Lm = 0.01-0.15 cm, i.e. of a comparable
order of magnitude to the viscous boundary layer. Only between 0.1 < z/h < 0.5 is Lm = 0.05-0.35
cm, i.e. similar to measurements by Odier et al. [2009]. As Lm is not constant in the BBL, but
51
rather increases with height the mixing length model would not lead to a constant eddy
diffusivity in the BBL layer, unlike in the interfacial region studied by Odier et al. [2009]. The
higher values of Lm in the interfacial region in the saline flow of Odier et al. [2009] might be due
to the larger slope of 10o along which the current flowed leading to a higher Fr than in our
experiments. Due to the larger Fr in their supercritical flow, their density current would have had
more interfacial entrainment [Wells et al., 2010] due to the higher turbulence levels at the upper
interface associated with Kelvin-Helmholtz billows.
2.4.4 Turbulent kinetic energy profiles
The turbulent kinetic energy (TKE) in the gravity current represents the intensity of the
turbulence associated with velocity fluctuations from the turbulent eddies [e.g. Tritton, 1989].
The total TKE per unit volume is calculated from time averages of the velocity fluctuations
according to
TKE =
1
2ρ(u'2 + v'2+w'2) [2.9]
[Gray et al., 2006]. Experimental observations of TKE normalized by ρU2 for saline and
sediment-laden flows are plotted in Figure 2.8. Both flow types show a strong normalized TKE
increase in the BBL whereby the saline gravity current has a maximum normalized TKE value of
0.018 ± 0.001 at z/h = 0.08, which is approximately 30% larger than the normalized TKE value
of 0.013 ± 0.0005 for the particle gravity current at z/h = 0.08. Above and below their maxima
the normalized TKE decreases constantly and reaches minimum values of 0.004 at z/h = 0.35
which correlates with the flow velocity maximum at z/h ~ 0.3-0.35. Above this minimum the
normalized TKE tends to increase again. The TKE distribution of both flow types is
quantitatively comparable with the distribution described by Gray et al. [2006] and Islam and
52
Imran [2010]. Both previous studies report normalized TKE maxima of 0.02 at z/h = 0.1 as in
our study and a distinct normalized TKE minimum of 0.004 ± 0.0005 around umax. In addition,
our data show a continuous decrease of the TKE in the BBL for z/h < 0.1.
Fig. 2.8: Vertical profiles of TKE for saline and sediment-laden gravity currents. All values are normalized by ρU2. The horizontal bars indicate the standard deviation.
53
2.4.5 Drag coefficients
Figure 2.9 compares the calculated values of CD obtained from the three different
methods introduced in section 2 for saline and sediment-laden gravity currents. Generally both
flow types show similar CD values but each method yields a different order of magnitude. The
log-fit method gives the largest CD at O(10-2) with CD = 0.02 ± 0.002 for saline and 0.048 ±
0.005 for turbidity currents. Drag coefficients derived from the maximum total stress in the BBL
in Figure 2.5 is 3.65 ± 0.4 × 10-3 for saline and 2.95 ± 0.3 × 10-3 for turbidity currents and hence
one order of magnitude smaller than values obtained with the log-fit method. The direct
measurements of the averaged turbulent velocity ût using Eq. [2.5] lead to the smaller value of
CD = 4 ± 3 × 10-4 and CD = 0.95 ± 3 ×10-4 for turbidity and saline gravity currents respectively.
Fig. 2.9: Calculated drag coefficients using Eq. [2.2] (light gray), Eq. [2.3] (dark gray) and Eq. [2.5] (black) for saline and sediment-laden gravity currents. To treat the drag coefficient determined by using Eq. [2.5] as a bulk drag coefficient the data of the single measurements of ût were averaged between z/h = 0.025 - 0.085. The horizontal bars indicate the standard deviation.
54
The estimates of the CD obtained from the maximum total stress in the BBL and by using
a log-fit are consistent with the range of data found in the literature where CD values range from
10-2 [Garcia and Parker, 1993; Kneller et al., 1999; Straub et al., 2008] to CD = 10-3 [Bowen et
al., 1984; Pope et al., 2006]. However, we note that only the estimate of CD using the maximum
bottom stress approach gives values at the same order of magnitude as the observed CD values in
oceanographic gravity currents that range in thickness from 5 m to 150 m [e.g. Dallimore et al.,
2001; Peters and Johns, 2006; Umlauf and Arneborg, 2009a]. The range of reported values could
be attributed to a variety of reasons, most importantly differences in the calculation method used
to estimate u* and CD respectively.
55
2.5 Discussion
Our new observations of shear stresses within the BBL now complement the previous
Reynolds stress profiles measured outside the BBL [e.g. Buckee et al., 2001; Gray et al., 2006;
Islam and Imran, 2010]. Our observations have focused on the Reynolds stresses below umax and
especially below z/h < 0.1. Largest positive Reynolds shear stresses occur at z/h ~ 0.1 and
decrease rapidly in the region dominated by viscous stresses (Figure 2.5). A similar decrease of
the near bed Reynolds stresses close to the bottom boundary was also observed with high
frequency ADCP measurements of the turbulence structure in the bottom layer of the Red Sea
outflow plume [Peters and Johns, 2006]. As shown in Figure 2.5, we find that the Reynolds shear
stress (at a distance of z/h = 0.1) is the main contributor to the total stress budget outside the
viscous boundary layer [Tritton, 1989].
There has been a considerable discussion on the potential difference in turbulence
dynamics between saline and turbidity currents, as well as the influence of particle size [Stacey
and Bowen, 1988; Kneller and Buckee, 2000; Gray et al., 2006]. Using the Rouse number Z of
,max
1'
p
rms
wZ
w= < [2.10]
[Bagnold, 1962; Leeder et al., 2005], where w’rms, max is the root mean square of vertical turbulent
velocity and wp = 9.1 × 10-4 m s-1 the settling velocity defined by Eq. [2.6], we found that the
experimental turbidity currents (with an average value of w’rms = 1.4×10-3 m s-1) had Z=0.638 < 1
so were sufficiently turbulent to keep the particles in suspension. This calculation of the
suspension criterion is also consistent with observations of negligible deposition near the
measuring location (see section 3), so that our turbidity flows can be classified as non-
depositional or weakly depositional. This explains our observation that we find a similar
Reynolds stress (Figure 2.5) and TKE distribution (Figure 2.8) for both flow types. Beyond the
56
broad similarity, there are minor differences in that saline flows exhibits larger Reynolds stresses
and TKE values outside the BBL, as was also found by Islam and Imran [2010]. This suggests
that the presence of particles has some influence, as sediment-laden flows are often described as
having significant density stratification near the lower boundary compared to saline currents
[Garcia and Parker, 1993; Peakall et al., 2000]. For instance, Sequeiros et al. [2010a,b] observed
regions near the bed in subcritical flows where excess densities varied relatively little, while
supercritical flows exhibited density profiles that declined exponentially. Particles can
accumulate near the base of the current and exhibit a Rouse-type density profile where coarse
material is concentrated towards the lower part of the flow whereas fine-grained material is more
evenly distributed throughout the depth of the flow [Kneller and Buckee, 2000]. This could
account for an attenuation of turbulence in the BBL represented by smaller TKE and shear
stresses at z/h < 0.1. Despite these minor differences we conclude that the saline flows are a good
analogue to non-sedimenting turbidity currents. Our experimental observations of velocity and
turbulence structure give more weight to this implicit assumption in the numerous analogue
experiments where saline density currents are used to model the dynamics of turbidity currents
[e.g. Keevil et al., 2006; Islam and Imran, 2008; Sequeiros et al., 2009; Cossu et al., 2010].
57
Figure 2.10 depicts normalized velocity profiles of several field measurements of large
scale gravity currents and our experimental gravity currents. The comparison reveals that the
basic features of the velocity profile of these field gravity currents are in accordance to our
laboratory currents.
Fig. 2.10: Comparison of downstream velocity profiles between natural and experimental saline and sediment - laden gravity currents. Data are normalized by umax and the height of umax (hu)
Based on our results it seems reasonable to compare the observations from laboratory
gravity currents in section 4.5 with the direct measurements of field scale gravity currents. The
CD values found in natural density currents are of O(10-3), e.g. CD = 2 × 10-3 to 8 × 10-3 in the
150 m deep Red Sea outflow [Peters and Johns, 2006], CD = 5 × 10-3 in a 5 m deep underflow in
an estuary in Japan [Dallimore et al., 2001] and CD = 3 × 10-3 from ADV measurements in a
20 m deep density current in the Baltic sea [Umlauf and Arneborg, 2009a]. In all these cases
direct observations using turbulence microstructure profiles of the turbulent friction velocity lead
to estimates of order CD = 10-3. The CD values in Figure 2.9 stem from three different approaches
and differ by almost two orders of magnitudes between O(10-4) and O(10-2). The largest values at
58
O(10-2) in Figure 2.9 and in the literature were obtained based on a log-fit method. To have
confidence in this technique requires a good fit of the velocity profile to the logarithmic curve,
which needs a very high and accurate spatial resolution of the velocity profile to obtain a reliable
fit [Biron et al., 1998; Pope et al., 2006; Baas et al., 2009]. However, even with several
measuring points in the BBL estimates of u* based on the velocity profile in Figure 2.3b vary
between 2.5 - 5 × 10-2 and lead to values that are significantly larger than field observations.
Similarly, CD values derived from the turbulent velocity ût using Eq. [2.5] yield a significantly
smaller value with CD = 4 - 9.5 × 10-4 that are also not consistent with field data. On the other
hand, the Reynolds stress distribution (Figure 2.5) is in good agreement with other recent
experimental studies [Gray et al., 2006; Islam and Imran, 2010] so that we can say with
confidence that the estimates of u* using Eq. [2.3] with the maximum total bottom stress should
also be correct. Drag coefficients obtained with this method are of O(10-3) which agrees well
with observations from natural gravity currents. It can be concluded that while it is possible to
estimate u* reliably with a log-fit at field scale [Johnson et al., 1994], it is difficult to obtain a
reliable estimate at a laboratory scale. Hence, using only 2 or 3 vertical measurements of the
velocity within the BBL [Kneller et al., 1999; Straub et al., 2008] could lead to an overestimate
of CD while we found the maximum bottom stress to be the most robust method to calculate the
bottom drag coefficient.
Apart from the calculation method, the range of reported values in the literature could be
attributed to a variety of other reasons, e.g. different flow properties in experiments (different
Reynolds or bulk Richardson numbers), different bed surfaces (bed form structures like ripples
or dunes, width of the channel etc.) and different measurement techniques. Hand [1974, 1975]
and Komar [1975] discussed the importance of these factors in terms of their different estimates
for CD which deviated by 800 %, e.g. CD = 0.04 Komar [1975] and CD = 0.005 [Hand, 1975].
59
Providing conditions of a hydraulically smooth bed CD values in the range of O(10-3) seem to be
a reasonable estimate [Hand, 1975] and collapse well with our data and various field
observations. The variation of CD and values at O(10-2) for gravity currents can further be
attributed to the parameterization of the overall drag, consisting of the bottom drag described
above and the interfacial entrainment of overlying water.
The momentum budget for a steady gravity current that is subject to bottom stress and
entrainment of ambient fluid can be written as a balance between buoyancy forces and the sum
of the bottom drag and interfacial entrainment as:
′g S= (CD
+ E)U 2
d [2.11]
where S is the bottom slope and E is the entrainment coefficient [Ellison and Turner, 1959;
Stacey and Bowen, 1988; Price and Baringer, 2009]. E is a strong function of Fr, varying
between 0.1 for very high Fr values, down to values as low as 10-4 for Fr of 0.5. For the typical
Fr of gravity currents that are in the range of 0.4 to 1.2 [e.g. Simpson, 1997; Kneller et al., 1999;
Gray et al., 2006] the entrainment ratio E varies between 5 × 10-4 to 5 × 10-2 [Wells and
Wettlaufer, 2005; Wells et al., 2010]. These values of E are almost the same range as the values
of CD presented here and in the literature, which leads to the conclusion that in at least some
cases the influence of interfacial entrainment has been implicitly included into the estimation of
CD, which is then used to estimate the bottom drag and shear stresses at the bed. For instance,
Garcia and Parker [1993] determined CD in the range of CD = 2 - 9 × 10-2 by back-calculation
from experimental velocity profiles and density concentrations with a layer-integrated
momentum equation. The use of such an approach implicitly considers the drag over the whole
thickness of the current including the interfacial drag at the upper boundary of the density flow.
60
Including these high values of E may then lead to an overestimate of CD, and hence overestimate
the shear stress at the bed.
The rate of entrainment of bottom sediment by gravity currents is often calculated based
upon the empirical formulae of Garcia and Parker [1993], as in the numerical models of
Blanchette et al. [2005], Huang et al. [2005] and Hu and Cao [2009]. This empirical relation for
bed entrainment requires a definition of u* which can be estimated if U and CD are known. Even
numerical models [e.g. Huang et al., 2007] that derive their shear stress from the simulated flow
field (which does not require the specification of CD) use a calculation of entrainment of
sediment to suspension, following a relation of Smith and McLean [1977], which in turn has
been tested against data by Garcia and Parker [1991]. In their calculation of the erosion rate
Garcia and Parker [1993] used a CD of O(10-2). Their empirical formulae has a very strong
dependence of erosion rate on the CD value, so if bed erosion is modelled using bottom stresses
estimated with a CD that is an order of magnitude too high, then this method can overestimate the
entrainment rate and erosion at the bed by a factor of O(101-102). The solution would be to
assume simply that the shear stress at the bottom of their gravity current was lower and then
recalculate the empirical constants in their equation that predicted the observed erosion in their
original experiments.
2.6 Summary and Conclusions
Our experiments show that saline and weakly-depositional sediment-laden gravity
currents have a generally similar turbulence structure in the BBL, with both flow types revealing
very similar Reynolds stresses and TKE distribution. Outside of the BBL we find maxima in
both Reynolds stresses and TKE at z/h ~ 0.1 and minima around umax. These results support
findings in previous works [e.g. Gray et al., 2006; Islam and Imran, 2010] which focused on data
61
outside of the BBL. A new result of our measurements is that Reynolds stresses decrease rapidly
below their maximum and that Reynolds stresses balance viscous forces at the bottom and lead
to large positive stress maxima near the base of gravity currents (Figure 2.5).
The velocity, Reynolds stress and TKE distribution of saline and sediment-laden currents
suggests that both flow types are dynamically similar when turbulent velocities near the bed are
so large that the turbidity current is only weakly depositional. Figure 2.10 demonstrates that we
find a very good agreement between velocity profiles of field gravity currents and our laboratory
gravity currents. The useful implication of this is that much of the recent work by
oceanographers on the interior dynamics of density overflows [Johnson et al., 1994; Dallimore et
al., 2001; Peters and Johns, 2006; Umlauf and Arneborg, 2009a] could also be applied to
understanding non-depositional large-scale turbidity currents.
Three different methods to determine CD values for gravity currents were tested against
our experimental data. While the log-fit method and measurements of turbulent velocities at the
bottom yield either very large or small values of CD respectively, we find the most reasonable
results of O(10-3) by using the maximum total bottom stress for both flow types. This data range
is similar to that of oceanographic studies, but lower than previous indirect estimates from
laboratory studies. When a log-fit approach is used to estimate the bulk friction velocity near the
bed, we note that there must be a very high resolution of the velocity profile to avoid a potential
overestimate of CD if the whole velocity profile below the velocity maxima is assumed to be well
represented by a logarithmic velocity profile.
62
Acknowledgements
Funding for this work was provided by NSERC, the Canadian Foundation for Innovation and the Ontario
Research fund. We thank Brian Greenwood and Joe Desloges for help with the laboratory work.
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66
Chapter 3 Influence of the Coriolis force on the velocity structure of gravity currents in straight submarine channel systems Remo Cossu, Mathew G. Wells and A. K. Wåhlin Abstract
Large-scale turbidity currents in submarine channels often show a significant asymmetry in the
heights of their levee banks. In the Northern Hemisphere there are many observations of the
right-hand channel levee being noticeably higher than the left-hand levee, a phenomenon that is
usually attributed to the effect of Coriolis forces upon turbidity currents. This chapter presents
results from an analogue model that documents the influence of Coriolis forces on the dynamics
of gravity currents flowing in straight submarine channels. The observations of the transverse
velocity structure, downstream velocity and interface slope show good agreement with a theory
that incorporates Ekman boundary layer dynamics. Coriolis forces will be important for most
large-scale turbidity currents and need to be explicitly modeled when the Rossby number of
these flows (defined as RoW = U/Wf where U is the mean downstream velocity, W the channel
width and f the Coriolis parameter defined as f=2Ω sin(φ), with Ω being the Earth’s rotation rate
and φ the latitude), is less than order 1. When |RoW| << 1 the flow is substantially slower than a
non-rotating flow with the same density contrast. The secondary flow field consists of
frictionally induced Ekman transports across the channel in the benthic and interfacial boundary
layers, and a return flow in the interior. The cross-channel velocities are at the order of 10% of
67
the along-channel velocities. The sediment transport associated with such transverse flow
patterns should influence the evolution of submarine channel levee systems.
3.1 Introduction
Submarine channels are the most significant morphologic features of the submarine
landscape on the continental slope and are known to be the main conduits for turbidity currents
to transport sediments to the deep ocean basins [Meiburg and Kneller, 2010]. There are still very
few direct observations of turbidity currents moving through submarine channels [Hay, 1987;
Khripounoff et al., 2003; Xu et al., 2004] since their occurrence in great water depths and high
current velocities make measurements difficult to obtain. Due to the spatial extent of submarine
channel systems and the associated long travel time, the flow properties and environments of
those currents are likely to be deflected by Coriolis forces that arise due to the Earth’s rotation
[Menard, 1955; Komar, 1969; Wells, 2009] for mid- and high latitude systems. While the
influence of Coriolis forces upon turbidity currents is acknowledged in several reviews
[Middleton, 1993; Huppert, 1998; Imran et al., 1999; Kneller and Buckee, 2000] and theoretical
studies [Komar, 1969; Bowen et al., 1984; Nof, 1996; Emms, 1999; Ungarish and Huppert,
1999; Kampf and Fohrmann, 2000], there have been very few previous experimental studies
specifically focusing on turbidity currents on a rotating platform [Wells, 2009].
One of the most noted effects of the Coriolis force upon well-developed levee systems is
that the deflection of the turbidity current by Coriolis forces leads to an asymmetry between
levee bank heights [Menard, 1955]. The right-hand-side channel levee (looking downstream) is
consistently higher in the Northern Hemisphere [Chough and Hesse, 1976; Klaucke et al., 1997,
1998; Wood and Mize-Spansky, 2009] and the left-hand-side channel levee is higher in the
Southern Hemisphere [Droz and Mougenot, 1987; Carter and Carter, 1988; Bruhn and Walker,
68
1997]. These differences in levee height can be large, for instance, in the NAMOC, there is a
difference in levee height that can reach more than 100 m and has an average difference of 65 m
along a 950 km long section [Klaucke et al., 1997]. Such observations of levee asymmetry are
usually described in the context of the theory of Komar [1969], although this theory has never
been tested in laboratory scale experiments on a rotating platform. In this paper the first rigorous
test of this theory is presented as well as a complementary theory that quantifies the downstream
and cross-stream velocity components.
The basic description of rotationally influenced turbidity currents that is most widely
used was presented by Komar [1969]. This theory is based upon a simple momentum balance
across the channel, whereby the pressure gradient forces that result from the surface slope of the
turbidity current are balanced by the Coriolis and centrifugal forces. Turbidity currents are often
constrained to flow in channelized systems, and it is usually assumed that the maximum levee
heights are a good indication of the maximum thickness of the turbidity currents that formed the
levee systems. If the difference in levee heights is a good measure of the maximum slope of the
interface of the turbidity current, then the theory of Komar [1969] can be used to infer the
magnitude of the mean current speeds of the typical turbidity currents that would have originally
formed the channel levee system. There are several important simplifications made in the theory
of Komar [1969] to describe the influence of Coriolis forces upon turbidity currents. Firstly, it is
assumed that the Froude number Fr = U / g 'h (where U is the mean downstream velocity, g’
the reduced gravity and h the thickness of the current), remains constant at a value of one. The
use of a constant Froude number implicitly assumes that the rotation rate has no control on the
velocity of the current, counter to the observations of Cenedese et al. [2004] and Cenedese and
Adduce [2008] where laboratory experiments clearly show a large reduction in velocity when the
69
Coriolis parameter is high. Another significant assumption in the theory of Komar [1969] is the
neglect of boundary friction, which means that the Ekman boundary layers are ignored even
though the Coriolis forces are assumed to be high. In a series of theoretical and experimental
papers by Wåhlin [2002, 2004], Davies et al. [2006] and Darelius [2008] these boundary layers
were shown to play a critical role in determining the sense of the secondary circulation in
rotationally controlled gravity currents. Even in cases where Coriolis forces are not dominant,
frictional effects have been shown to be important in determining the slope of a density interface
flowing in a channel in estuaries [Ott et al., 2002; Chant and Wilson, 1997; Fugate et al., 2007;
Nidzieko et al., 2009].
In contrast to the rarely observed turbidity currents, there are many direct observations of
large-scale oceanographic density currents [Ivanov et al., 2004] that can inform our
understanding of the circulation patterns in turbidity currents. In the oceanographic literature
there a number of previous experimental studies on how Coriolis forces deflect cold or salty
currents of dense water as they flow down the continental margins of oceans [Griffiths, 1986;
Price and Baringer 1994; Etling et al., 2000; Hallworth et al., 2001; Cenedese et al., 2004;
Davies et al., 2006; Cenedese and Adduce, 2008]. These experimental studies found that rotating
gravity currents rapidly come into a geostrophic balance, where the trajectory of the density
current is determined by a balance between buoyancy forces, friction and Coriolis forces. Both
density currents and turbidity currents are examples of gravity currents, in that the flows are
primarily driven by density differences [Huppert, 1998]. Low concentration and weakly
depositional turbidity currents exhibit concentration and velocity profiles that are very similar to
saline currents [Kneller and Buckee, 2010]. For this reason many laboratory measurements using
saline currents [e.g. Keevil et al., 2006; Islam et al., 2008; Darelius, 2008] have made important
contributions to defining both the structure of the flow field and the turbulence intensities
70
associated with these gravity currents and therefore helped to develop a general understanding of
the fluid dynamics also for turbidity currents. In this context we use experimental density
currents for this study to understand the first order effects of how Coriolis forces influence the
circulation of channelized gravity currents, which will be also relevant to geologists wishing to
comprehend the interaction of turbidity currents and channels they build. Nonetheless we note
that further experimental work considering how sediment dynamics influence transport in Ekman
boundary layers, will be needed to gain more insight into evolution of submarine channel
systems subjected to Coriolis forces.
Many submarine fan channels are confined by prominent levees, which form by
deposition of suspended sediment on the slower moving margins of a turbidity current. These
levees can grow rapidly, for instance, the average sedimentation rates during the active growth
phases of the levees of the Amazon channel during the Pleistocene were 1 to 2.5 cm year-1
[Shipboard Scientific Party, 1995]. The rapid growth has been attributed to deposition of
suspended load as successive turbidity currents transit the channel and spill over the channel
margins along their entire length [Hiscott et al., 1997; Peakall et al., 2000; Straub et al., 2008]. In
addition, recent non-rotating experiments on channelized turbidity currents have shown that the
morphological evolution and associated depositional histories of submarine channel systems are
highly influenced by the secondary flow structures within the channel, which determine where
erosion and deposition will occur [Corney et al., 2006; Keevil et al., 2006; Straub et al., 2008;
Islam et al., 2008; Islam and Imran, 2008]. The main focus in these non-rotating experiments has
been to investigate the secondary circulation due to an imbalance of centrifugal and pressure
gradient forces in channel bends, which plays a major role in the formation of super-elevation of
levee systems at the outer bend [e.g. Straub et al., 2008]. Coriolis forces can also give rise to
secondary flows within turbidity currents through the generation of Ekman boundary layers at
71
the upper interface and the base of the flow. In the Northern Hemisphere these boundary layer
flows will be directed to the left when looking downstream. To conserve volume there is return
flow directed to the right in the interior of the flow. The basic features of such Ekman boundary
layers in channelized current have been seen in several laboratory experiments [Benton and
Boyer, 1966; Hart, 1971; Johnson and Ohlsen, 1994; Davies et al., 2006; Darelius, 2008; Wåhlin
et al., 2008]. Qualitatively similar secondary flows driven by Ekman boundary layer dynamics
have been seen in oceanic gravity currents, such as reported in the Vema channel [Johnson et al.,
1976], in the Faroe Bank Channel [Johnson and Sanford, 1992; Fer et al., 2010], in the Ellet
Gully [Sherwin, 2010] and in the Baltic Sea [Umlauf and Arneborg, 2009 a,b]. Turbidity currents
should also experience similar secondary flow patterns, when the flows are at large enough
scales that the Coriolis force becomes important.
Though the theory of Komar [1969] has been cited almost one hundred times in the
geological literature [i.e., Bowen et al., 1984; Klaucke et al., 1997; Imran et al., 1999], no
experiment has ever tested its validity. The goal of this study is to look at the flow structure in
experimental rotating gravity currents and to relate it to a general geological context. Of primary
importance for geologic applications is to infer the speed of the turbidity current that would have
formed the asymmetric levees in a submarine channel, as this information can be used to
determine the likely evolution of sediment deposition in turbidite beds that may be rich in
hydrocarbons [Weimer et al., 2000]. Using an analogue experiment mounted on a rotating
platform we are able to determine the dependence of the secondary flow structure, downstream
velocity and interface tilt upon rotation rate. These observations are compared with the theory
initially developed by Wåhlin [2002, 2004].
72
3.2 Theory
The most widely used description of how Coriolis forces influence the dynamics of
turbidity currents was proposed by Komar [1969], in which a force balance between the Coriolis
force, the centrifugal force induced by flow curvature, and the pressure gradient force is
assumed. Assuming that the upper interface has a constant slope and that friction is negligible,
the momentum balance across the channel can then be written as:
−g '
dh
dy= fU +
U 2
R, [3.1]
where U is the mean downstream velocity, R is the radius of curvature of the channel and f the
Coriolis parameter (defined as f =2Ω sin(φ), with Ω being the Earth’s rotation rate and φ the
latitude). The reduced gravity is g ' = g ρ
2− ρ
1( ) ρ1, where the gravity current has the density ρ2
and ρ1 is the ambient density of the seawater. Equation [3.1] can be rewritten in terms of a
Froude number ( Fr = U / g 'h ), as:
−
dh
dy= Fr 2 fh
U+
h
R
. [3.2]
This momentum budget does not include any turbulence drag from the boundary and so
implicitly assumes that stratification suppresses turbulent motions [e.g. Chant and Wilson, 1997].
Based upon the force balance shown in Eq. [3.2] and assuming that Fr = 1, Bowen et al. [1984]
expressed the difference in levee height due to the Coriolis-effect in a straight channel as:
∆h = Wh f / U , [3.3]
where ∆h= W dh/dy, with W being the channel width and h being the depth of the main body of
the flow. This equation can also be written as / 1/Wh h Ro∆ = where RoW = U/Wf. Equation
[3.3] is valid only for the straight sections of channels, where centrifugal effects are absent.
73
Equation [3.3] has been used to describe observed channel height asymmetries, such as in the
Amazon channel [Imran et al., 1999], the Navy fan in California [Bowen et al., 1984] or the
NAMOC described by Klaucke et al. [1997, 1998].
In a rotating system, the inclusion of friction into the momentum equation means that the
Ekman boundary layers must be properly described. The resulting flow structure of a gravity
current in a rotating system has been studied previously in the oceanographic literature [Wåhlin,
2002] and is illustrated in Figure 3.1.
Fig. 3.1: Schematic sketch of a density current flowing down a submarine channel with the gradient s, the channel height D and the channel width W, looking upstream. The density of the ambient fluid and the gravity are ρρρρ1 and ρρρρ2 respectively, with ρρρρ2 > ρρρρ1. The main downstream flow is uG while there is also a significant transverse motion consisting of the interior flow vG and bottom and interfacial currents ve. The thickness δ δ δ δ of the Ekman boundary is small in comparison to the entire thickness of the flow h(y).
In the Northern Hemisphere the currents are deflected to the right side of the channel
(looking downstream) until the flow reaches a geostrophic balance. Friction at the upper and
lower boundaries leads to the formation of Ekman boundary layers, which drive a transverse,
secondary circulation within the flow [i.e. Darelius, 2008]. Figure 3.1 shows a sketch of the flow
74
structure. The secondary circulation consists of an across-channel flow in the Ekman boundary
layers next to the bottom and next to the interface, and an oppositely directed across-channel
flow in the interior away from the Ekman boundary layers. The thickness of the Ekman layers is
δ , and the velocity there is ve. In the interior the across-channel velocity is vG. Similar secondary
flows have been described in previous rotating laboratory experiments by Hart [1971], Johnson
and Ohlsen [1994], Davies et al. [2006], Wåhlin et al. [2008] and Darelius [2008] and were also
reported in oceanic gravity currents, [e.g. Johnson and Sanford, 1992; Sherwin, 2010; Fer et al.,
2010]. In Umlauf and Arneborg [2009a,b] a different secondary flow structure was observed,
with a thin jet in the interfacial layer and no clear Ekman layer at the bottom. This may be due to
the fact that the Ekman boundary layer was comparable in thickness to the flow itself.
The Ekman boundary layer dynamics of a gravity current have been previously examined
for V-shaped [see e.g. Davies et al., 2006; Darelius and Wåhlin, 2007; Darelius, 2008], cosine-
shaped [Wåhlin, 2002; Darelius and Wåhlin, 2007] and parabolic shaped [Darelius and Wåhlin,
2007] canyons and ridges. In this paper a square channel is investigated for the first time, which
permits analytical expressions for the across and along channel components of the velocity and
the transverse slope of the interface, as a function of the rotation rate and mean slope of the
channel.
Consider a rectangular channel of width W, which slopes downward at angle s to the
horizontal (Figure 3.1). Assuming a force balance between Coriolis, bottom friction, and
pressure gradient, and a 1.5 layer system, the momentum equations can be written as:
2
2' E
ufv g s
zν ∂− = − +
∂ [3.4]
2
2' E
h vfu g
y zν∂ ∂= − +
∂ ∂, [3.5]
75
where f is the Coriolis parameter, v the velocity in the across-channel (i.e. y) direction, g' the
reduced gravity, νE the molecular viscosity, u the velocity along the channel and h(y) the
thickness of the dense layer. Note that Eq. [3.5] in similarity with Eq. [3.1] expresses the
interface slope as a function of the along-channel velocity. The difference is that Eq. [3.5]
includes the viscous term (last term on right-hand-side) but does not include the centrifugal term
which is absent in straight sections. Away from the Ekman boundary layers the viscous terms
can be neglected and Eq. [3.4] and Eq. [3.5] reduce to the geostrophic velocities, i.e.:
v → v
G= g 's
f , [3.6]
u → u
G= − g '
f
∂h
∂y. [3.7]
The Eq. [3.4] and Eq. [3.5] can be solved using Ekman theory [see e.g. Cushman-Roisin, 1994,
p. 66; Darelius, 2008], for which the velocity in the directions along- (u) and across- (v) the
channel are given by:
ue(z) = u
G(1− e
−z
2δ cos(z 2δ )) − vGe
−z
2δ sin(z 2δ ) [3.8a]
ve(z) = u
Ge
− z
2δ sin(z 2δ ) + vG(1− e
− z
2δ cos(z 2δ )) [3.8b]
where δ = υ 2 f is the Ekman layer thickness, uG and vG are the geostrophic velocities given
by Eq. [3.6] and Eq. [3.7] in the interior and it has been assumed that h>> δ (we note that often a
different definition of δ = 2υ f can be found in the literature, e.g. Cushman-Roisin [1994]).
Expression [3.8a,b] has been plotted in Figure 3.2 for uG = 0.07 m s-1, vG = -0.01 m s-1 and three
different values of f. As can be seen, far above the boundary layer the velocity approaches the
geostrophic velocities, and in the boundary layer the velocity rotates and decreases exponentially
76
to zero. For vG<<u G the maximum value of v(z) is v
MAX=
uG
2e
−π4 ≈ 0.3u
G, approached at
z ≈ πδ
2. The mean velocity in the Ekman boundary layer is 0.1 M EAN Gv u≈ . The boundary
layer thickness δ is indicated by thin horizontal lines in Figure 3.2.
Fig. 3.2: Dependence of the flow velocity u and ve in the Ekman boundary layer on the Coriolis parameter f. Note that also the thickness δδδδ of the Ekman boundary layer varies with f and is indicated by the horizontal lines. The net transport across the channel is found by vertical integration of Eq. [3.8b] from the
bottom (z = 0) to the top of the dense layer (z=h), to give:
`
v(z)dz=0
h
∫ hvG
+ δ (uG
− vG
) , [3.9]
where we have used a standard result from Ekman theory, namely that the transport in the
Ekman boundary layer is given by δ(uG – vG) when h>> δ (which will be used for the rest of the
theory). Classical Ekman theory pertains to the flow over a solid boundary, but there are many
examples of observations of interfacial Ekman layers, [e.g. Darelius, 2008; Sherwin, 2010]. The
77
basic dynamics are the same, although the thickness of the layer may be greater than in the
bottom boundary layer. The interfacial stress gives rise to an Ekman layer next to the interface,
with the Ekman transport directed to the left of the main flow direction in the Northern
Hemisphere (looking downstream). By vertical integration across the interfacial Ekman layer an
expression similar to Eq. [3.9] is obtained. The net across-channel transport in the presence of
both an interfacial and a benthic Ekman layer is hence given by:
v(z)dz=
0
h
∫ hvG
+ 2δ (uG
− vG
) [3.10]
where the factor 2 comes from the effect of including both boundary layers. We note that the δ
here is still the viscous Ekman boundary layer, and will discuss the possible influence of a
turbulent boundary layer later. When the Ekman boundary layers meet the vertical side walls the
horizontal flow will be transported vertically within Stewartson boundary layers [Duck and
Foster, 2001] and then returned to the interior flow. Provided there is no net transport across the
channel the horizontal flow in the geostrophic interior balances the flow in the Ekman boundary
layer, so that:
hvG
+ 2δ (uG
− vG
) = 0. [3.11]
Using Eq. [3.6] and Eq. [3.7], Eq.[3.11] can be rewritten as:
∂h
∂y− s
h
2δ= −s, [3.12]
which gives a solution for the position of the interface across the width of the channel as:
h( y) = Cesy
2δ + 2δ . [3.13]
78
In Eq. [3.13] C is a constant of integration with units of length that must be determined by a
boundary condition. If we use the along-channel transport Q as the boundary condition
(assuming that the dense layer is thick compared to the Ekman layer and vG<<u G) we get:
Q = hu
G0
W
∫ dy = hg 'f
∂h
∂y0
W
∫ dy , [3.14]
or using Eq. [3.13]:
Q = 1
2
g '
f
∂∂y
(h2)0
W
∫ dy
= 1
2
g '
fh2(W) − h2(0)
= 1
2
g '
fC2(e
sW
δ − 1) + 4δC(esW
2δ −1)
.
[3.15]
From Eq. [3.15] we can express C in terms of Q. For most cases, in particular for high rotation
rates, δ << h and the relationship between C and the volume flux Q is given by:
C = 2 fQ
g '1
(esW
δ − 1)
. [3.16]
79
Figure 3.3 shows the interface for various rotation rates, looking downstream. In order to
compare this expression for h with Eq. [3.3] we can determine ∆h = h(W) -h(0) using Eq. [3.13].
Fig. 3.3: Calculated position of the interface in the channel after Eq. [3.13] for varying Coriolis parameter f.
The mean along-channel velocity U is given by the volume flux divided by the cross-sectional
area A of the flow:
U = Q / A, [3.17]
where the area is calculated using Eq. [3.13]:
0
2
0
2
( )
( 2 )
2 ( 1) 2'( 1)
2
W
W sy
sW
sW
A h y dy
Ce dy
Qe W
s ge
f
δ
δ
δ
δ
δ δ
= ⋅
= + ⋅
= − +−
∫
∫ [3.18]
80
and Eq. [3.16] has been used to define C. The mean downstream geostrophic velocity uG will be
referred to as U in the rest of the manuscript so that meaningful comparison can be made with
the non-rotating environment.
3.3 Method
The physical experiments were carried out on a computer-controlled rotating platform
with a diameter of 1 m. The rotation rate was varied from f = -1 rad s-1 to f = 1 rad s-1 (including
f = 0) to represent a range of different latitude systems. All experiments were conducted in a
1.85 m × 1.0 m × 0.35 m rectangular tank that was placed on the rotating platform (Figure 3.4).
Fig. 3.4: a) Layout of the experimental setup. The velocity of the density currents was measured approximately 50 cm from the inflow at the upstream end of the channel model. b) Position of the UDVP and ADV used for the measurements.
81
Inside this tank a channel model was placed and the tank was filled with tap water up to a level
of approximately 0.30 m, so that the entire channel system was submerged by approximately 0.1
m at the inflow point. The channel model had a constant, rectangular cross-sectional shape with a
width of 0.1 m and a height of 0.08 m. The length of the straight channel was 0.6 m and was
elevated 0.12 m above the tank floor. When the density current leaves the channel the dense
water flows into the sump region below the channel, which restricts the influence of gravity
current reflections from the sides of the tank. In order to have a constant velocity of the inflow
the saline water passed through a 0.10 m thick diffuser made of drinking straws and foam to
damp any irregularities in the inflow velocity. The slope of the channel axis s was 1:50.
In the experiments the turbidity current was modelled by a dense saline mixture as in
previous studies [e.g. Keevil et al., 2006; Imran et al., 2007; Islam et al., 2008] that have used
saline gravity currents to gain insight into the flow field and secondary circulations in turbidity
currents. The justification for this is that the dynamics of large-scale non-depositional turbidity
currents are similar to density currents. The density contrast was generated with salt, and 30 L of
the saline mixture was pumped in at the upstream end of the straight channel section using a
pump with a constant discharge of Q = 16 L/min, so that each flow lasted for about 120 s after
the pump was turned on and the current entered the channel model. The excess density was 1%,
giving a density for the saline current of 1010 kg m-3. The tank was spun up for at least 30 min in
order to achieve solid body rotation of the water, after which the experiment was initiated. In
order to visualize the density current and the slope of the density interface blue food dye was
added to the mixture in some experiments.
The across-stream and along-stream velocities were measured at a distance of 0.5 m from
the flow diffuser at the start of the channel. Two different acoustic velocity instruments were
used: a Metflow Ultrasonic Doppler Velocity Profiler (UDVP) and a Nortek Acoustic Doppler
82
Velocimeter (ADV). Arrays of UDVPs have been frequently used in geometrically similar non-
rotating experiments [e.g. Best et al., 2001; Corney et al., 2006; Peakall et al., 2007a]. An array
of UDVP probes is ideal for making transverse measurements of the flow. Each UDVP probe
can record single-component velocity data along a profile of 128 points along the axis of the
ultrasound beam at a frequency of 4 Hz. Vertical velocity profiles were obtained from an array of
6 transducers to monitor the velocity at heights of 0.5, 1.5, 2.5, 3.5, 4.5 and 5.5 cm above the
bottom (Figure 3.4b). Representative values were obtained by averaging the velocities over 30-
35 s, starting immediately after the head of the current had passed the instrument (Figure 3.5).
Fig. 3.5: The time averaged horizontal velocity is plotted at different heights above the bed for three different rotation rates. These velocities were measured using the UDVP. The error bars depict the standard deviation over the 30 second measurement period. Most of the volume flux of the density current is between 0.5 cm and 4 cm above the bottom. Hence, the point measurements with the ADV were taken at 2.5 cm above the bottom, to represent the significant velocities between 0.5 and 4 cm. This region of the flow best represents the geostrophically adjusted velocity ug used in the theory section, e.g. Eq. [3.7] to Eq. [3.14]. The open markers showing the ADV data are taken at the same rotation rates as the closed markers for the UDVP data, e.g. diamonds reflect a Coriolis parameter f=0 rad s-1.
83
The second instrument was a Nortek ADV. This can sample simultaneously 3
components of velocity at frequencies up to 200 Hz, but only measures at a single point, so is a
good complement to the UDVP. The ADV consists of one transmitter and three receivers which
are slanted at 30o from the axis of the transducer and focus on a common sample volume of 80
mm3 that is 50 mm away from the probes [Voulgaris and Throwbridge, 1998]. This ensures
nearly non-intrusive flow measurements within the flow field of the current. The velocity
components measured by the ADV were recorded in the centre of the channel, 2.5 cm above the
bottom at a frequency of 50 Hz (Figure 3.4b). The data were taken over the same sampling
interval over which the UDVP data was averaged.
In order to measure the interface position, a digital camera was used. In those
experiments blue food dye was added to the salt water. The camera was mounted on the table
looking upstream so that the thickness of the current and slope of the interface could be
measured (Figure 3.4b).
3.4.1 General observations
The aspects of the flow that have been analyzed are the flow velocity U of the interior
bulk flow (measured with the ADV), the secondary flow cells (measured with the UDVP) and
the deflection of the density interface (photographs).
In the absence of rotation (f=0 rad s-1) the front of the dense current formed a head with
the typical overhanging nose that covered the whole cross section of the channel. Behind the
head the density current was significantly thinner, but the flow still occupied the whole channel
width. After the passage of the head the flow conditions remained fairly constant. A small
amount of mixing of ambient water into the current was noticed through the more transparent
color at the upper interface. Vertical velocity profiles from several experiments with different
84
values of the Coriolis parameter are shown in Figure 3.5 together with the point ADV
measurements. The velocity profiles show the typical “bullet nose” profile [Middleton, 1993;
Kneller and Buckee, 2000] with the maximum velocity close to 0.5-1 cm above the bottom.
Within the bottom boundary layer the velocity increases non-linearly between the base and the
velocity maximum Umax as also observed in Kneller et al. [1999]. Above the velocity maximum
the velocity decreases continuously to U < 0.02 m s-1 at 5.5 cm above bottom. Based on these
profiles the point measurements using the ADV were positioned 2.5 cm above the bottom,
approximately representative of the mean downstream velocity. As can be seen in Figure 3.5
there is a favorable agreement between the UDVP measurements and the ADV measurements,
which later were used to determine U.
In the experiments with rotation the formation of the head and its transition to the body
with a distinct thinning of the flow was less obvious, as the gravity current was pushed towards
the wall after it had entered the channel. With positive f the currents were deflected to the right-
hand-side of the channel (looking downstream) and for negative Coriolis parameter (-f) to the
left-hand-side. This deflection became greater as the rotation rate increased. The propagation
speed of the gravity currents was also observed to decrease significantly as the rotation rate
increased. In the non-rotating experimental gravity currents shown in Figure 3.5, the mean
velocity averaged over the entire thickness was approximately Umean= 0.04 m s –1. This flow had
a thickness of approximately h = 0.06 m so that the Froude number was / 'meanFr U g h= =
0.52. Such a Froude number is broadly similar to many previous experimental observations of
gravity currents where 0.2 < Fr < 1.3 [Garcia and Parker, 1993; Kneller et al., 1999; Baas et al.,
2005; Gray et al., 2006]. Flows with such small Froude numbers are also expected to have very
low interfacial entrainment rates [Wells and Wettlaufer, 2007; Wells and Nadarajah, 2009; Wells
et al., 2010]. The flow had a Reynolds number of Re = 2400 where Re = U h/ν, where ν is the
85
molecular viscosity. The value of Re indicates that the flow was turbulent and can be compared
to other experimental gravity currents such as Kneller et al. [1999], Amy et al. [2005] or Davies
et al. [2006] with similar Reynolds numbers where the flow was turbulent.
The distance over which the flow is expected to adjust geostrophically is in the order of
the internal Rossby radius of deformation defined as Rdef = (g’h)1/2/f [e.g. Darelius, 2008; Wells,
2009]. For the rotating gravity currents used in our experiments the value of Rdef is about 0.4 m
for low rotation rates of f = 0.1 rad s-1. The Coriolis force gets larger for higher rotation rates
(e.g. f > 0.1 rad s-1) so that these flows come more quickly into a geostrophic balance which
means that the radius of deformation decreases. As all of the velocity measurements were
obtained 0.5 m from the inflow point we expect that all flows will have reached geostrophic
conditions and reproduce sufficiently characteristics associated with rotating gravity currents.
3.4.2 Observations of downstream velocity U
The downstream velocities measured with the ADV for different rotation rates are plotted
in Figure 3.6 and compared to the mean velocity based on the theory incorporating Ekman
dynamics (using Eq. [3.17] and Eq. [3.18]) which predicts a significant decrease of the
downstream velocity between small and large Coriolis parameters f. The error bars indicate the
standard deviation in the averaging period. The experiments reveal that for f < 0.2 rad s-1 the
velocity is not significantly influenced by rotation as the velocity remains relatively constant at U
~0.07 m s-1, which is close to the velocity computed based on the density difference and a
constant Froude number. As f increases the measured downstream velocity decreases. At large f
the downstream velocities are up to 40% smaller than for the non-rotating case (f=0 rad s-1). The
experimental data show good agreement with the theory using Ekman boundary layer dynamics
(Eq. [3.17] and Eq. [3.18]).
86
In Figure 3.6 there is a slight offset in the downstream velocity between small positive
and negative Coriolis parameter (e.g. between f = 0.1 – 0.25 rad s-1). We can attribute this
velocity difference mainly to two reasons: the alignment of the measuring device might not have
been exactly at the centerline so that the maximum speed of current was not captured perfectly
during those experiments. Secondly, due to the experimental set-up at the inflow point those
currents were not entirely uniform and more pronounced at either the right-hand or left-hand side
of the channel so that the maximum flow velocity was off-set to the position of the measuring
device. However, we can consider those differences as negligible as the overall data set reveals a
distinct and consistent trend, with symmetry at large f (small RoW).
Fig. 3.6: Dependence of the mean downstream velocity U with varying Coriolis parameter f. The graph shows the mean velocity U based on the initial Froude number, and U calculated using Eq. [3.17] and Eq.[3.18] with a turbulent and a laminar boundary layer and direct ADV measurements. The ADV data were taken at a height of 2.5 cm above the base and in the middle of the channel approximately 0.5 m away from the injection point.
87
The analytical expressions (Eq. [3.10] and Eq. [3.18]) are based on purely laminar flow
conditions [Wåhlin, 2002; Darelius, 2008]. However, a large Reynolds number of Re = 2400
suggests that the currents are turbulent rather than laminar. In both the turbulent and laminar
flows, the thickness of the boundary layers represents the length scale over which friction is
important. These equations can be estimated by rearrangement of the Ekman number, which is
defined as Ek = ν ΩH 2 [Cushman-Roisin, 1994], where H is a characteristic vertical length
scale. If the Ekman number is of order 1, then frictional influences are important so that
H ~ ν Ω . The expression for the turbulent boundary layer thickness comes from a
consideration of the turbulent viscosity. For instance, in Figure 3.2 the theory ( δ = υ 2 f )
predicts thicknesses of the laminar boundary layer of order 0.1 cm. As will be demonstrated in
section 4.3 and 4.4 the observations of the experimental currents suggest that there are larger
boundary layers, in particular turbulent mixing with the ambient water at the upper boundary
layer led to a thick interfacial boundary layer (Figure 3.10b). When comparing our theory using
Ekman dynamics (Eq. [3.17] and Eq. [3.18]) with the observations of velocities and interface
slope, we make the simple assumption that the turbulent Ekman boundary layers are thicker than
the laminar Ekman boundary layers. This is consistent with the scaling of a turbulent boundary
layer, which can be defined in terms of the turbulent velocity scale as *
* 0.4u
fδ = [Weatherly
and Martin, 1978], where u* represents the friction velocity. The friction velocity can be defined
in terms of the mean velocity as u* = C
DU . Thus with f = 0.25 rad s-1, where the velocity U is
0.06 ± 0.005 m s-1 (Figure 3.6), a drag coefficient of CD = 0.003 [Umlauf and Arneborg, 2009a]
implies u* = 0.0032 m s-1 so that the turbulent Ekman boundary layer is δ* ~ 0.4 cm, which is
approximately 2.5-3 times larger than the thickest theoretical laminar boundary layer thickness
88
of δ = 0.14 cm (black dashed line Figure 3.2). Empirically we find the best fit to our
experimental data where we use * 1.7 1.7 / 2fδ δ ν= = . This is a reasonable value as it is larger
than the laminar model and smaller than turbulent scaling which can overpredict the thickness in
strongly stratified fluids [Weatherly and Martin, 1978]. Using a thicker turbulent Ekman
boundary layer thickness yielded velocities that were significantly smaller than with a laminar
boundary layer. and are in much better agreement with the experimental data in Figure 3.6. We
use this estimated turbulent boundary layer thickness in Eq. [3.18] and in the rest of the
manuscript so that more meaningful comparison can be made with the experimental density
currents.
The experimental velocity data can be expressed in a more general way by the use of a
dimensionless Rossby number RoW and the Froude number Fr, which are plotted in Figure 3.7.
Fig. 3.7: Relation between Rossby number RoW and the Froude number Fr for the channel model with varying Coriolis parameter f. RoW and Fr (using h=0.06 m from Figure 3.5) are based on the measured mean velocity U (in the interior of the flow), the calculated mean velocity U using Eq. [3.17] and Eq. [3.18] (solid line) and U based upon the assumption of a constant velocity with Fr = 1 (dashed line).
89
We note that we now use the averaged geostrophic velocity of the interior of the current (from
Figure 3.6) to define Fr. For |RoW| < 2 there is generally a good agreement between the theory
using Ekman boundary layer dynamics (Eq. [3.17] and Eq. [3.18]) and the measured velocities.
The poorer agreement for |RoW| > 2 suggests that Eq. [3.17] and Eq. [3.18] are less applicable for
large |RoW|. This is expected as we assumed that f >> 0 rad s-1, in order for the flow to be
geostrophically adjusted, and for the Ekman boundary layers to be fully developed. Due to the
small velocity differences between small positive and negative Coriolis parameter f (Figure 3.6)
we observe a slight asymmetry in the Froude numbers (the normalized velocity) when the flow is
not strongly rotationally controlled, i.e. for |RoW| > 2 . Based on the experimental results in
Figure 3.6 and 3.7 we conclude that only for |RoW| < 2 does the Coriolis-effect become
significant for our experimental gravity currents. Such a threshold is consistent with
oceanographic literature where RoW of order 1 is usually the criterion when currents start to feel
the effect of rotation [e.g. Nof, 1996; Wells, 2009].
3.4.3 Slope of the interface with changing f
The strong influence of the Coriolis force on the lateral density interface can be seen in
Figure 3.8. The photographs show the shape of the across-stream interface for RoW ~ ∞ (f = 0)
and RoW = 0.83 (f =±0.6 rad s-1) looking upstream. For the case without rotation (f = 0 rad s-1,
Figure 3.8b) the density interface is horizontal. Those conditions, where f is almost zero, would
be relevant to large-scale turbidity-currents that occur in areas close to the equator, or for which
the scales are such that |RoW| > O(1). With smaller Ro, illustrated in Figure 3.8a (for f = +0.6 rad
s-1) and Figure 3.8c for (f = -0.6 rad s-1), a significant deflection of the slope of the across-stream
interface can be observed. For a positive Coriolis parameter (Northern Hemisphere), a deflection
of the current to the right-hand-side (looking downstream) can be seen. For a negative f
90
(Southern Hemisphere), the flow is deflected to the left-hand-side of the channel. The height
difference of the interface between the left and the right channel wall is negligible for an infinite
RoW, but for RoW = ±0.83 the difference is about 4 cm, which accounts for more than half of the
depth of the non-rotating gravity current. This tilt of the interface due to the rotation was also
observed in the low Reynolds number experiments by Darelius [2008] and with a numerical
model by Imran et al. [1999].
Fig. 3.8: Deflection of the interface of the density currents for a) RoW = 0.83 (with f=+0.6 rad s-1) b) RoW = ∞ (with f=0 rad s-1) and c) RoW = -0.83 (with f= -0.6 rad s-1). Note that the perspective is upstream and hence a deflection to the left-hand-side means a deflection to the right-hand-side from the downstream perspective.
Figure 3.9 shows the relation between RoW and the observed deflection ∆h of the
interface, normalized by the current thickness h. The deflection of the interface is defined as the
height difference between the left- and right-hand-side of the interface at the channel walls. The
experimental results demonstrate that with decreasing |RoW| the deflection increases. In addition,
Figure 3.9 compares the experimental results with the theoretical approaches to define the
deflection according to the theory of Komar [1969] expressed in Eq. [3.3] (where
/ 1/ Wh h Ro∆ = ) and the theory involving Ekman boundary layers of Eq. [3.13], respectively.
For small |RoW| the measured height difference is approximately 50% smaller than predicted by
Eq. [3.3] and there is generally a better agreement with the theory that used turbulent Ekman
boundary layer dynamics. The lack of viscous effects and Ekman boundary layers in Eq. [3.3]
91
tends to overestimate the slope of the interface when rotation is important as the velocity is also
overestimated (Figure 3.6 and Figure 3.7).
Fig. 3.9: Comparison of the deflection ∆∆∆∆h and RoW for various values of f after Eq. [3.3], Ekman boundary layer dynamics following Eq. [3.13] and the measured height differences. ∆∆∆∆h is normalized by the current thickness h (Figure 3.5). Error bars of the experimental data depict a variance of 10%.
3.4.4 Secondary flow cells and across-stream velocities
The secondary circulation patterns in the channel are illustrated in Figure 3.10 for various
Rossby numbers. Without rotation there are two adjacent flow cells in the channel that spin in
opposite directions, with a flow convergence at the surface and divergent flow at the bottom of
the density current (Figure 3.10a). This is essentially the same as the classic “helicoidal flow”
that was first observed in rivers at the end of the 19th century, and reported in open channel
flows [e.g. Rhoads and Welford, 1991; Colombini, 1993]. In a rotating density current the
secondary circulation changes dramatically, as demonstrated in Figure 3.10b and Figure 3.10c
for RoW = ± 2.4 (f= ± 0.25 rad s-1). The positive rotation leads to a deflection of the current to the
right-hand side (Figure 3.10b) and a corresponding interior flow vG with maximum velocities up
92
to 0.005 m s-1 towards the right-hand wall (looking downstream). This interior flow is bordered
by two return flows ve at the upper interface and the bottom of the density current, which are the
Ekman boundary layers. The maximum velocities of these return flows are approximately ve =
0.015 ± 0.005 m s-1 and hence larger than the interior flow towards the wall. Using Eq. [3.8a]
and Eq. [3.8b] the magnitude of the velocities in the Ekman boundary layer can also be
estimated. As the mean downstream velocity for f = 0.25 rad s-1 is U = 0.06 m s-1 we predict that
the mean velocity in the Ekman boundary layer is ve = 0.017 m s-1. This theoretical velocity
conforms to the observed velocity in Figure 3.10b where the transverse velocities have a
magnitude ve = 0.015 ± 0.005 m s-1 and are approximately 25 % of the downstream velocity U.
Fig. 3.10: Across-stream velocities for the experimental flows in the submarine channel (looking upstream) measured with the UDVP. a) RoW = 2.4 (with f = 0.6 rad s-1) b) RoW = ∞ ( with f = 0 rad s-1) and c) RoW = -2.4 (with f = -0.6 rad s-1). The sense of the rotation is sketched on the right hand panels. Note the upwelling mechanism denoted by the upward directed arrow in the right hand panels in b and c.
93
As the bulk flow vG in the interior towards the right wall of the channel (looking
downstream) occupies about 60 % of the depth of the current (near the right wall of the channel),
the return flows ve that occur in the thinner Ekman boundary layers have a higher velocity than in
the interior bulk flow (Figure 3.2 and Figure 3.10) in order for the integral of the cross-stream
velocity to be zero. When our experimental measurements of the transverse velocity were
integrated over the whole depth of the density current, we found an almost balanced relation
between the interior flow and the opposite velocities in the boundary layers. For larger f this
balance between vG and ve is even more prominent as the Ekman boundary layers tend to get
thinner (see section 2) while the interior flow expands further over the whole thickness. This is
accompanied by smaller bulk velocities vG in the interior and faster return flows ve in the
boundary layers. Figure 3.10c illustrates basically the same flow field as in Figure 3.10b, but for
negative f and hence mirrors the flow field of Figure 3.10b. Similar flow fields to those shown in
Figure 3.10 have been described by Johnson and Ohlsen [1994], Davies et al. [2006] and
Darelius [2008] from experiments in rotating fluids. Analogueous secondary flow patterns have
also been reported in several natural gravity currents, e.g. in the Faroe Bank Channel [Johnson
and Sanford, 1992; Fer et al., 2010], in the Ellet Gully [Sherwin, 2010] and in the Baltic Sea
[Umlauf and Arneborg, 2009a,b].
The magnitude of the secondary flows can be estimated from the geostrophic velocities
by rearranging Eq. [3.6] and Eq. [3.7]. Division of Eq. [3.6] by Eq. [3.7] gives an estimate of the
ratio of the interior transverse velocity vG to the mean downstream velocity U as vG/U =
s/(dh/dy). In our experiments the downstream slope of the channel s was constant, whereas the
cross-channel slope of the interface dh/dy increases for decreasing |RoW| (Figure 3.9), so that
vG/U should also decrease with |RoW|. Figure 3.7 showed that the theory incorporating Ekman
boundary dynamics appeared to be particularly suitable for |RoW| < 2.
94
Figure 3.11 depicts the measured values of the observed relation s/(dh/dy) for |RoW| < 4. With an
increasing deflection, the geostrophic interior of the flow becomes proportionally thicker, while
the Ekman boundary layers decrease in thickness, which results in a reduction in the velocity vG
and consequently a reduction of the ratio vG/U. For large rotation rates or |RoW| < 0.5 the ratio
vG/U is approximately 0.3. Figure 3.11 shows a partial regression line from which the
relationship U=0.5 sW2f/∆h can be derived. This simple empirical relationship could be used as a
first order approximation to determine the mean downstream velocity U of a turbidity current if
the levee height difference (or vice versa) and the slope of the submarine channel system is
known.
Fig. 3.11: Relation between s/(dh/dy) and RoW for varying Coriolis parameter f. The graph compares experimental data and the Ekman boundary layer dynamics calculated after Eq. [3.13].
There has been a considerable effort recently to look at the secondary circulations in
turbidity currents flowing in submarine channels, in particular in the bends of sinuous channels
[Keevil et al., 2006; Islam et al., 2008; Islam and Imran, 2008; Straub et al., 2008]. In channel
95
bends, the curvature-induced centrifugal acceleration of the flow balances an inwardly directed
radial pressure gradient leading to secondary flows that are of the order of 10% of the mean flow.
It is worth noting that the secondary flows driven by Coriolis-effects have a similar magnitude to
these previously studied flows but quite a different internal structure.
3.5 Discussion
An understanding of flow dynamics and sediment transport processes in submarine
channels is essential to interpret and analyze their morphology and architecture and to develop
process models, e.g. Peakall et al. [2000] or Pirmez and Imran [2003]. The growth of channel
levee systems is thought to arise from extensive overbank flow and over-spill, based upon direct
observations of overbank flow [Normark and Dickson, 1976b; Normark, 1989], and from
observations of the grain size distribution taken from silt and fine-sand beds on levee crests
[Hesse et al., 1987; Hiscott et al., 1997]. The height of turbidity currents can extend vertically
beyond the channel depth up to a factor of 4 [Normark, 1989] and fine grained sediment in this
upper part residing above the channel can spread laterally and be deposited on the overbank
surface [Straub et al., 2008]. Hence, in straight channel sections finer sediments are usually
found along channel levees rather than inside the channel and this continuous overspill accounts
for levee growth along submarine channels, e.g. in the NAMOC [Klaucke et al., 1998] or the
Amazon channel [Pirmez and Imran, 2003]. In channel bends however, the levee deposits can
also consist of coarse-grained sediments that are upwelled by centrifugal forces. These flow
dynamics in channel bends have been studied extensively in non-rotating sinuous submarine
channels [e.g. Corney et al., 2006; Keevil et al., 2006; Peakall et al., 2007; Straub et al., 2008].
Channel bend levees at the outer bank result predominantly from overspill deposition caused by
centrifugal forces, and the secondary flow cells. The deflection of the interface and the
96
movement of sediment by the secondary circulation, leads to an outer bank upwelling towards
the overbank region and promotes subsequent growth of high outer bank channel levees [Corney
et al., 2006; Straub et al., 2008].
Our results show that strong secondary circulations are present in straight channel
sections for |RoW| < 2 (f > 0.25 rad s-1) due to the interaction of Coriolis force and pressure
gradient force. A continuous deposition of sediments that are carried by these secondary
circulations in turbidity currents could lead to the asymmetry between right-hand and left-hand
levee banks, which has been described for several submarine channel systems in the Northern
and Southern Hemisphere [Menard, 1955; Carter and Carter, 1988; Klaucke et al., 1997]. These
secondary flows could contribute to overbanking in straight channel section where the
centrifugal force is absent. The secondary circulation consists of an interior flow towards the
right-hand-side of the channel (looking downstream) in the Northern Hemisphere and a return
flow along the density interface (Figure 3.10b). Hence this secondary flow cell could lead to an
upwelling of sediment at the right-hand-side of the channel and promote the growth of the right-
hand levee by continuous deposition (denoted by the vertical arrow in Figure 3.10b). This
upwelling is a similar mechanism that has been reported in channel bends without rotation,
where there was pronounced levee formation on the outer bends of submarine channels [Corney
et al., 2006; Keevil et al., 2006]. In a rotating system, we hypothesize that similar upwelling of
sediment, driven by the observed secondary flows, causes a constantly larger sediment flux
towards the right-hand-side of straight channel sections, leading to a consistent increase in levee
heights on the right-hand-side of submarine channels. This upwelling might also lead to
deposition of coarser sediment which is usually transported at the base of the current onto the
right-hand levee. Such deposition patterns and grain size distributions have been observed by
Straub et al. [2008] driven by a similar mechanism with superelevation and upwelling at an outer
97
channel bend. In the Southern Hemisphere the negative Coriolis parameter forces this upwelling
of sediments onto the left-hand-side of the channel (looking downstream), leading to greater
levee heights on the left-hand-side of the channel (Figure 3.10c).
In addition, the experiments showed good agreement with our theory (Eq. [3.13], Eq.
[3.17] and Eq. [3.18]) that incorporated Ekman boundary layer dynamics. In particular there was
good agreement with the predicted reduction in downstream velocity, U, and for the magnitude
of the cross-channel interface difference, ∆∆∆∆h. Our theory agreed with our observations better than
the theory of Komar [1969] in straight submarine channels. This is an important result, as the
new theory can now be used as an analytical method to derive flow properties from field data of
submarine channel systems.
The experiments indicate that the transition between the regimes when the two different
models should be used can be expressed in terms of the Rossby number so that the transition
occurs approximately for |RoW| = O(1). For example, in the NAMOC the right levee bank
exceeds the left levee bank up to 100 m, so that the ratio between ∆ ∆ ∆ ∆h to the entire depth D of the
channel is often large with ∆∆∆∆h /D > 0.5. The use of Eq. [3.3] for the NAMOC channel predicts
downhill velocities between 0.1-1.06 m s-1 [see table 1 in Klaucke et al., 1997]. The
corresponding Rossby numbers for these velocities at a latitude 53° N are small ranging from 0.2
- 0.5. These small values of RoW indicate the Ekman boundary layer dynamics cannot be
neglected in this system. At the equivalent Rossby number for our experimental analogue in
Figure 3.6, we found that the effective downhill velocity is over 30% smaller than obtained
following Eq. [3.3]. Hence, we conclude that the actual velocities in the NAMOC in straight
channel sections are generally smaller than proposed in Klaucke et al. [1997] by a factor of 0.7.
For smaller submarine channel systems such as the Navy fan in California, where the
estimated downstream velocities in the narrow upper fan are of order 0.75 m s-1 [Bowen et al.,
98
1984] there would be large Rossby numbers of about 10-18, for a latitude 33.5° N and a width W
= 0.5-1 km. Consequently rotation appears to be less important in this channel and no significant
asymmetry of the channel banks has been reported in the upper fan valley. However, when the
system widens towards the mid and lower fan system to 3 km to 8 km the velocities drop
significantly to 0.12-0.3 m s-1 and |RoW| < 1 is obtained. In this region Bowen et al. [1984]
observed an asymmetry on the mid-fan with the right-hand-side levee of the fan-system (looking
downstream) being up to 30 m higher than the left-hand-side.
Another example of a gravity current flowing in a submarine channel is the
Mediterranean inflow into the Black Sea [Flood et al., 2009]. Here a density current bearing a
small amount of sediment, continuously flows through a submarine channel system. When the
channel is on the inner shelf it has a width between 0.5–1 km and a depth of 10- 35 m [Flood et
al., 2009]. For the velocity range of about 0.2-0.4 m s-1 [Özsoy et al., 2001], the predicted
Rossby numbers are in the range RoW =2-5 suggesting that Coriolis forces will likely influence
the secondary circulation of any gravity currents in this channel system. Specifically we would
expect that the density interface tilts to the right-hand-side, and any sediment will be deposited
dominantly on the right-hand levee. However, due to the lack of significant sediment load in the
density current this system shows no prominent levee systems. Based on our results we predict
that the density interface would exhibit a tilt resulting in the interface being up to 5 m higher at
the right-hand-side (looking downstream). With a downstream velocity of 0.2–0.4 m s-1 we
expect that the mean velocity of the Ekman boundary layers will be of order 0.05–0.1 m s-1 and
will be directed to the left-hand-side of the channel looking downstream. At high discharge rates
this might also lead to intensive overspill of dense saline water, which could build features like
antidunes outside of the channel that have been observed and linked to overbank flow [Flood et
al., 2009].
99
Near the equator the Coriolis parameter is small and any asymmetry in levee heights is
expected to be less prominent compared to high latitudes. Nonetheless, the deep sea submarine
channel system offshore of Trinidad and Tobago at latitude 10.5° displays a consistently higher
right levee system, with cross channel differences of up to 20 m. This asymmetry in the
approximately 600 m wide and 200 m deep channel is attributed to the regional southward dip of
the northeastern South American basin [Wood and Mize-Spansky, 2009]. Nonetheless, we note
that for small downstream velocities, that are likely to occur in the upper portion of the velocity
profile of a gravity current (as in Figure 3.5) Rossby numbers of order 1 can be obtained. Fine
sediments transported as suspended load in the upper profile of a turbidity current [Peakall et al.,
2000] would predominantly be deflected to the right-hand-side of the channel system. In this
light, the observed asymmetry of up to 10% of the whole channel depth could also be attributed
to Coriolis forces. It follows that thicker, slower and finer-grained turbidity currents could give
rise to levees with more prominent asymmetry than thinner and faster, coarser-grained turbidity
currents, even at low latitudes.
100
3.6 Conclusions
This work demonstrated that the Coriolis force plays an important role in determining the
velocity structure in gravity currents running through straight submarine channels. The
frequently observed asymmetry in depositional elements in large-scale submarine channels,
where the right-hand (left-hand) levee banks tend to be higher in the Northern Hemisphere
(Southern Hemisphere), can be linked to the Earth’s rotation and arising rotational effects on
large-scale turbidity currents. In geological applications the theory of Komar [1969] as expressed
by Eq. [3.3] has been used to derive flow parameters from submarine channel systems. In
contrast, oceanographic studies mostly include Ekman boundary layer dynamics to describe the
characteristics of gravity currents in the ocean.
The major findings were that the theoretical model using Ekman boundary layer
dynamics is more accurate in describing the downstream velocity U and the interface tilt ∆∆∆∆h for
channels that have scales with Rossby numbers smaller than 2. In addition, it can be used to
describe the secondary across-stream velocities vG and ve. The downstream velocity decreases
significantly as the rotation rate increases, so that the theory after Eq. [3.3] overestimates the
velocity by more than 30% for large rotation rates. Similarly, the theory Komar [1969]
overestimates the tilt of the interface by as much as 50%.
Significant secondary circulations develop that are driven by Ekman boundary layer
dynamics. Those flow cells promote an upwelling at the right-hand-side of the channel (looking
downstream) in the Northern Hemisphere and an upwelling at the left-hand-side of the channel in
the Southern Hemisphere which governs most likely sedimentation transport processes and the
evolution of submarine channels.
The Rossby number RoW = U/Wf , where U is the mean downstream velocity, W the
channel width and f the Coriolis parameter, can be used to determine whether the rotational
101
effects are significant. The results show that particularly for |RoW| < 2 the flow properties are
better reflected by the theory incorporating the Ekman boundary layers dynamics.
Acknowledgements
We gratefully acknowledge the support of Jeff Peakall who loaned a Metflow UDVP system of the NERC
supported Sorby Environmental Fluid Dynamics Laboratory at the University of Leeds for the use in these
experiments. The rotating table was built on a design generously provided by Karl Helfrich. Helpful conversations
with Ilker Fer and Lars Umlauf are acknowledged. Mathew Wells received financial support from NSERC, the
Canadian Foundation for Innovation and the Ontario Innovation Trust. Remo Cossu was partially supported in this
work by a travel grant from the Centre for Global Change Science at the University of Toronto.
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Chapter 4 Coriolis forces influence the secondary circulation of gravity currents flowing in large-scale sinuous submarine channel systems Remo Cossu and Mathew G. Wells Abstract
A combination of centrifugal and Coriolis forces drive the secondary circulation of turbidity
currents in sinuous channels, and hence determine where erosion and deposition of sediment
occur. Using laboratory experiments we show that when centrifugal forces dominate, the density
interface shows a superelevation at the outside of a channel bend. However when Coriolis forces
dominate, the interface is always deflected to the right (in the Northern Hemisphere) for both left
and right turning bends. The relative importance of either centrifugal or Coriolis forces can be
described in terms of a Rossby number defined as RoR = U/Rf, where U is the mean downstream
velocity, f the Coriolis parameter and R the radius of curvature of the channel bend. Channels
with larger bends at high latitudes have |RoR| < 1 and are dominated by Coriolis forces, whereas
smaller, tighter bends at low latitudes have |RoR| >> 1 and are dominated by centrifugal forces.
4.1 Introduction
Recent non-rotating experiments on channelized turbidity currents have shown that the
morphological evolution and associated depositional histories of submarine channel systems are
highly influenced by the secondary flow structures within the channel, which determine where
erosion and deposition will occur [Corney et al., 2006; Keevil et al., 2006; Straub et al., 2008;
Islam et al., 2008]. The main focus in these non-rotating experiments has been to investigate the
107
secondary circulation due to an imbalance of centrifugal and pressure gradient forces in channel
bends, which plays a major role in the formation of superelevation of levee systems at the outer
bend [e.g. Straub et al., 2008; Kane et al., 2010]. The circulation in such a curved channel is
shown in Figure 4.1a. At the level of the downstream velocity maximum the centrifugal forces
are at maximum. The velocity maximum usually occurs relatively close to the base of the gravity
current due to drag induced by mixing processes at the upper interface [Turner, 1973; Meiburg
and Kneller 2010]. For such velocity profiles [e.g. Corney et al., 2006; Keevil et al., 2006;
Corney et al., 2008] the secondary flow near the base is directed towards the outer bend and
return flow is near the surface, in contrast to river flows. However, in some experiments using
square channels there is an additional secondary flow directed towards the outside bend below
the velocity maximum [Imran et al., 2007; Islam et al., 2008a,b].
Coriolis forces deflect the bulk of the gravity currents to the right (in the Northern
Hemisphere) [Hacker and Linden, 2002; Davies et al., 2006; Wells 2009], which causes a lateral
tilt of the interface in a confined, straight channel. This tilt (and any secondary circulation)
means that overbanking sediment flows are more likely to occur on the right-hand-side of the
channel (looking downstream) for mid- and high latitude systems in the Northern Hemisphere,
leading to an asymmetry between levee bank heights [Menard, 1955; Komar, 1969].
Observations at higher latitudes have found that the right-hand-side channel levee is consistently
higher in the Northern Hemisphere [Klaucke et al., 1997] while the left-hand-side channel levee
is higher in the Southern Hemisphere [Carter and Carter, 1988; Bruhn and Walker, 1997]. In
addition, Coriolis forces generate Ekman boundary layers in gravity currents [Wahlin, 2002] as
illustrated in Figures 4.1b and 4.1c, for the case of the Northern and Southern Hemisphere
respectively. In previous theoretical and experimental studies by Wahlin [2004] these boundary
layers were shown to play a critical role in determining the sense of the rotationally controlled
108
secondary circulation in gravity currents flowing down straight channels. These secondary
circulations dominated by Ekman boundary layer dynamics are also observed in oceanic gravity
currents [Johnson and Sanford, 1992].
Fig. 4.1:a) In a curved channel the velocity maximum of the gravity current is close to the base of the flow, the secondary circulation consists of a basal flow towards the outer bend and a return flow near the surface and sometimes below the velocity maxima [Keevil et al., 2006; Islam et al. 2008]. b) In a straight channel Coriolis forces deflect the upper density interface and drive secondary circulations due to the presence of Ekman boundary layers. In the Northern Hemisphere (f > 0) the interface is deflected to the left-hand-side of the channel, when looking downstream, whereas c) in the Southern Hemisphere (f < 0) the interface is deflected to the right-hand-side and the secondary circulation is in the opposite sense.
There are few direct observations of the velocity structure within turbidity currents
because their occurrence in great water depths and high current velocities make measurements
difficult to obtain [Xu et al., 2004, Meiburg and Kneller, 2010]. The dynamics of large-scale
non-depositional turbidity currents are often assumed to be similar to gravity currents, so that
previous experiments in sinuous channels [e.g. Keevil et al. 2006; Imran et al., 2007; Islam et al.,
2008] have used studies of saline gravity currents to gain insight into the secondary circulation in
turbidity currents. An open question is whether the secondary circulation in large-scale turbidity
currents flowing down a sinuous channel will be dominated by centrifugal forces or by Coriolis
forces. We will address this question through the use of analogue laboratory experiments
mounted on a rotating platform that can produce Coriolis forces. In particular we will investigate
how the interface slope and secondary circulation cells in a saline gravity current change in terms
109
of a dimensionless Rossby number RoR, and so determine when the flows are dominated by
Coriolis or centrifugal forces.
4.2 Theory
The geological observations of levee height asymmetry are usually described in terms of
the cross-channel tilt (dh/dy) of the upper interface of the turbidity current, using the theory of
Komar [1969]. Assuming that tangential friction is small and turbulence is absent, the
momentum balance across the channel can then be written as:
g '
dh
dy= fU +
U 2
R, [4.1]
where U is the mean downstream velocity, R is the radius of curvature of the channel and f the
Coriolis parameter, defined as f = 2Ω sin φ with Ω the Earth’s rotation rate and φ the latitude. R
is defined as positive when the bend is to the left (looking downstream), so that the force is in the
same direction as the Coriolis force in the Northern Hemisphere, while turns to the right will
have negative R. The Coriolis parameter f is positive in the Northern Hemisphere and negative in
the Southern Hemisphere, so that the sign of dh/dy depends upon both the latitude and the
curvature of the channel. The reduced gravity is g ' = g ρ
2− ρ
1( ) ρ1, where the gravity current
has the density ρ2 and ρ1 is the ambient density of the seawater. Equation [4.1] can be re-
arranged to give an equation for the interface slope whereby:
dh
dy= Fr 2 fh
U+
h
R
, where Fr 2 =
U 2
g 'h. [4.2]
Hence if the flow velocity remains constant, the interface deflection due to the Coriolis forces
increases with latitude. We note that Eq. [4.2] has never been previously tested in a rotating
experiment with a channel bend. The interface of the gravity current will be flat (dh/dy = 0) when
110
Coriolis forces and centrifugal forces balance, which occurs when fh/U = -h/R for a bend to the
right in the Northern Hemisphere. This condition can be re-written in terms of a Rossby number
defined as:
1R
URo
Rf≡ = − . [4.3]
We hypothesize that in sinuous flows with |RoR| >> 1, the interface always slopes in towards the
inner bend, while flows with |RoR| << 1 the interface will always slope to the right-hand-side
(left-hand-side) in the Northern Hemisphere (Southern Hemisphere). We note that a complete
description of the flow dynamics around a bend would require a full momentum budget
including cross-stream frictional influences and non-local adjustment terms as discussed in
Nidzieko et al. [2009]. However, we focus on Eq. [4.1] to Eq. [4.3] and point to future work that
has to incorporate these features in a more thorough mathematical model.
4.3 Experiments
All experiments were conducted in a channel placed within a 1.85 m × 1.0 m × 0.35 m
rectangular tank. This tank was rotated at a constant rate, with Coriolis parameters from
f = 0 to ± 0.5 rad s-1. Before the experiment began, the tank had to be spun up for at least 30 min
in order to achieve solid body rotation of the water. The channel had a constant, rectangular
cross-section with a width of 10 cm and a height of 8 cm (similar in dimensions to Keevil et al.
[2006]) and was submerged by 0.1 m of water at the inflow point. As shown in Figure 4.2a, the
channel consisted of a straight section of length 0.64 m, joined to a single channel bend of length
of 0.9 m and with mean radius of R = +0.36 m (representing a sinuosity of 1.09).
111
Fig. 4.2: Our experiment consists of a curved channel that can be rotated in either the Northern or Southern Hemisphere sense.
A constant velocity of the inflow was achieved by using a 0.10 m thick diffuser. We used
a saline gravity current as an analogue to a turbidity current. To visualize the slope of the gravity
current interface at the bend apex, fluorescein dye was added to the saline mixture and the flow
was illuminated by a thin sheet of light. The down-stream (u), across-stream (v), and vertical (w)
velocity data were recorded in the apex of the left-turning channel bend (Figure 4.2b) using a
Metflow Ultrasonic Doppler Velocity Profiler (UDVP), as used in Keevil et al. [2006]. Each
UDVP probe records simultaneous single component velocity data along a profile of 128 points
along the beam axis at a frequency of 4 Hz. Measurement time per profile was 11 ms, with a 15
ms delay between the recording of each profile. Vertical velocity profiles were obtained from an
array of 6 transducers at heights of 0.5, 1.5, 2.5, 3.5, 4.5 and 5.5 cm above the bottom. The
velocities were averaged over an interval of approximately 30 s after the head of the current had
passed the instrument. Experimental conditions are summarized in Table 1.
112
Tab. 4.1: Experimental conditions. The flow thickness h was estimated visually at the point upstream of the channel bend, and is a good estimate of the centre line channel depth as shown in Figure 4.2.
4.4 Results and Discussion
The strong dependence of the cross-stream slope of the density interface in the channel
bend to changes in the Coriolis force is shown in a series of photographs in Figure 4.3 for
various values of the Coriolis parameter f. For f = 0 rad s-1, the Rossby number is infinite and the
density interface slopes up towards the outer bend due to the centrifugal acceleration (Figure
4.3a). Such a superelevation is characteristic for non-rotating density currents in channel bends
as described by Corney et al. [2006], Keevil et al. [2006] and Straub et al. [2008]. For a positive
Coriolis parameter f = +0.25 rad s-1, the Rossby number is +0.55 and the tilt of the interface
towards the outer bend increases as now the Coriolis and centrifugal forces act in the same
direction (Figure 4.3b). The experiment shown in Figure 4.3c has a negative Coriolis parameter f
= -0.25 rad s-1 so that the Rossby number is -0.42, so that the Coriolis force acts in opposition to
the centrifugal force and the superelevation at the outer bend of the interface is largely reduced.
As the Rossby number is close to RoR = -1 there is an almost horizontal interface in the bend
apex. For a larger negative Coriolis parameter f = -0.5 rad s-1 with RoR = -0.2, the current shown
113
in Figure 4.3d now ramps up towards the inner bend and is completely reversed compared Figure
4.3a. The observations in Figure 4.3 are typical of the 100 experiments conducted using a range
of g’ and f. In particular the horizontal interface observed in Figure 4.3c is always seen when
0.35 < |RoR| < 0.45 in other experiments using different g’ and f.
Fig. 4.3: The photographs of the tilting interface of the gravity current are taken looking upstream at the apex of the bend. The inner and outer bends are marked as IB and OB respectively and the channel is 10 cm wide. In a) f = 0 rad s-1 and the Rossby number is infinite, in b) f = +0.25 rad s-1 giving RoR = +0.55, in c) f = -0.25 rad s-1 giving RoR = -0.42 and in d) f = -0.5 rad s-1 giving RoR = -0.2.
114
The resulting secondary circulation patterns are presented in Figure 4.4 for different
values of the Coriolis parameter f. In the non-rotating experiment with f =0 rad s-1 the cross-
stream velocity structure is broadly similar to experiments of Corney et al. [2006] or Keevil et al.
[2006]. Near the base of the gravity current (between 1 and 2.5 cm) the flow is directed from the
inside to the outside of the bend (in the region near the inside bend) while above this flow the
fluid moves from the outside towards the inside bend which causes an upwelling close to the
outside. The downstream flow velocity maximum occurs at depths between hu = 1-2 cm. The
total depth of the gravity current is h = 6 cm, so that the ratio of hu /h = 0.16-0.33. In non-rotating
gravity currents, the secondary circulation pattern is determined by the position of the velocity
maxima [Corney et al., 2008], so that when the velocity maximum is near the base (i.e. hu/h <
0.4), there is a flow towards the outer bend at intermediate depths, as seen in Figure 4.4a. Very
close to the bottom at 0.5 cm there is another flow directed toward the inner bend. This thin
bottom boundary flow occurred below the downstream flow maximum and is essentially the
same feature observed by Imran et al. [2007] using a similar rectangular channel cross section.
For a positive Coriolis parameter f = +0.25 rad s-1 (Figure 4.4b) the corresponding flow field has
a similar structure to the non-rotating experiment. However, as the centrifugal and Coriolis
forces act together the tangential and upwelling velocities are intensified as is the superelevation
(Figure 4.3b) at the outer bend.
115
Fig. 4.4: (left) The centre line downstream velocity profiles (u). (right) The cross-stream velocity field V is shown by the contoured colours, while the vectors show both V (cross stream) and W (vertical) velocities measured in two sets of identical experiments at the bend apex. The dashed boundary represents the spatial extent of the UDVP measurements, and the dark straight line represents the interface profiles from Figure 4.3. In a) the Coriolis parameter is f = 0 rad s-1, b) f = +0.25 rad s-1, c) f = -0.25 rad s-1 and d) f = -0.5 rad s-1.
The flow pattern changes dramatically if the Coriolis parameter is negative and hence the
Coriolis force counteracts the centrifugal force, as seen in Figures 4.4c and 4d for f = -0.25 and
f =-0.5 rad s-1 (RoR = 0.42 and RoR = -0.2 respectively). In both cases, the flow towards the
outside bend at mid-depth has decreased significantly compared to Figure 4.4a, but there is still a
flow between heights of 3 to 5 cm directed toward the inner bend. The vertical flows are now
almost absent in the current, suggesting that there is non-local adjustment of the velocity
116
occurring in the downstream direction. In both Figures 4.4c and 4.4d the basal flow towards the
outer bend is almost absent, suggesting that the opposition of Coriolis and centrifugal forces
suppresses this feature in rotating currents in left-turning channel bends in the Northern
Hemisphere. This is in contrast to the case when the Coriolis forces act in concert with
centrifugal force, and the basal flow is increased (Figure 4.4b). Thus, when |RoR| >> 1, in a
sinuous channel there would be a strong asymmetry in secondary circulation patterns between
successive left and right turning channel bends.
In addition, Figure 4.4 shows the mean downstream velocity profiles measured at the
centerline in the bend apex. Maximum velocities range from 0.075 m s-1 for f = 0 rad s-1 to 0. 05
m s-1 for f = - 0.5 rad s-1 which indicates that an increase of the rotation rate gradually decreases
the velocity. This is consistent with our observations in the straight channel in Chapter 3.
However, the influence of rotation on the downstream velocity core is discussed in more detail in
the following chapter. In previous studies [Keevil et al., 2006; Imran et al., 2007; Straub et al.,
2008] secondary flows were reported to be at the order of 10% of the mean flow. For our rotating
experiments we find similar values with the secondary flows being 5-15 mm s-1, which is about
10-20% of the mean downstream velocity. As sketched in Figure 4.1c the currents in Figure 4.4
will have Ekman boundary layer flows directed towards the inner bend for positive f. For a value
of f = +0.25 rad s-1 the Ekman number (Ek = υ / fH 2 ) is one for a thickness of H = 0.2 cm,
suggesting the Ekman boundary layer is much less than 1 cm in our experiments and hence may
not be detectable with the UDVP in Figure 4.4. Despite being unable to resolve explicitly these
thin boundary layers at large f, these Ekman flows are central to driving the significant cross-
stream flows as shown in the previous chapter for straight channels.
The importance of the Coriolis force on gravity current dynamics becomes evident when
we compare the Amazon submarine channel, located at latitudes between 3°-7° North, with the
117
NAMOC located at latitudes of 53°-59° North. The low latitude Amazon submarine channel
system exhibits a strong sinuosity over several hundred kilometers and consistently has the
highest levee banks on the outside of channel bends. Pirmez and Imram [2003] reported a mean
radius of curvature of between 1-2 km and estimated mean streamwise velocities of turbidity
currents between 1-3 m s-1. The Coriolis parameter for this range of latitudes is between f =
0.076 - 0.177 × 10-4 rad s-1 so that the magnitude of the Rossby number for the submarine
channel system is approximately between 30-130, i.e. |RoR| >> 1. These large Rossby numbers
indicate that Coriolis forces are negligible and the flow dynamics in the channel bends are
dominated by centrifugal forces. Hence, the superelevation is on the outside bend and the
resulting secondary flow field promotes upwelling at the outside (like in Figure 4.4a), leading to
the levee asymmetry between inner and outer bends.
By way of contrast the NAMOC channel has low sinuosity with observations [Klaucke et
al., 1997] suggesting that the mean radius of curvature of the channel is mostly 10-20 km and the
predicted mean velocity is in the range 0.2-1 m s-1. At latitudes between 53°-59°N the Coriolis
parameter is an order of magnitude larger at f = 1.16 - 1.2 × 10-4 rad s-1 so that the resulting
Rossby number is between 0.05-0.5, with an average value of 0.2, i.e. RRo << 1. The NAMOC
channel system shows a continuous higher right levee system irrespective of left or right turning
bends [Klaucke et al., 1997] consistent with Coriolis forces rather than centrifugal forces
dominating the secondary circulation and movement of sediment within the channel. Figure 4.3
and Figure 4.4 clearly demonstrate that the Coriolis forces are important for high latitude
submarine channel systems and give rise to flow patterns that explain the observations of levee
height asymmetry in these channel systems.
118
4.5 Conclusions
The influence of Coriolis forces upon the flow dynamics that we have reported in this
paper will have implications for the nature of depositional units such as the “outer-bank bars” or
“point bars”, as the orientation of secondary flows affects the position and geometry of these
deposits [Peakall et al., 2007; Amos et al. 2010]. The outer-bank bars are depositional units that
are likely to be sand prone and hence of high porosity which has significant implications for
prediction of hydrocarbon reservoirs [Nakajima et al., 2010]. Based upon the data in Figures 4.3
and 4.4 we predict that Coriolis forces will affect the secondary circulation in successive bends
of a sinuous channel differently; directing flow first towards the outer bank and then the inner
bank then back to the outer, as the channel turns to the left then right then left in the Northern
Hemisphere. Thus the relative position and geometry of inner (point-bar) and outer (OBB)
accumulations would vary between successive bends. We expect that this asymmetry in
deposition patterns between left and right bends will increase as a function of latitude, changing
from a symmetric distribution at low latitudes to a highly asymmetric distribution at high-
latitudes.
Acknowledgements
RC was partially supported by the CGCS at the University of Toronto. MGW acknowledges support from NSERC,
CFI and the Ontario MRI. The Metflow UDVP system was borrowed from Jeff Peakall of the NERC supported
Sorby Environmental Fluid Dynamics Laboratory at the University of Leeds.
119
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Chapter 5 Flow structures and sedimentation processes in submarine channels under the influence of Coriolis forces: experimental observations in rotating gravity currents Remo Cossu and Mathew G. Wells
Abstract
Submarine channels are the main conduits by which turbidity currents transport sediments from
the continental shelf to deep ocean basins. Many of these channels extend over thousands of
kilometers so that Coriolis forces can become important at higher latitudes and influence the
processes by which submarine channels evolve. Submarine channels at low latitudes often show
sinuous planform geometries similar to meandering rivers, whilst at high latitudes they are less
sinuous. The Coriolis-effect can strongly influence where erosion and deposition occur within
submarine channels by deflecting gravity currents and changing their flow properties, leading to
significant asymmetries between left and right channel levee heights at higher latitudes. We
present results from experimental gravity currents to show that the density interface and position
of the downstream velocity core shift for high values of the Coriolis parameter representative of
high latitudes. We combine our new observations of the velocity structure with an existing
conceptual model for sedimentation and erosion in sinuous channels to elucidate potentially
different sedimentation patterns at different latitudes. Based upon the internal velocity structure,
we predict that high latitude channel systems will exhibit depositional patterns that oppose a
strong lateral growth in channel bends, in contrast to low latitude systems.
122
5.1 Introduction
There has been considerable effort to explain the architecture of sinuous submarine
channels and to reconstruct their evolution as their depositional units have significant
implications as hydrocarbon reservoirs [Abreu et al., 2003]. Highly sinuous submarine channels
are found in modern equatorial regions, e.g. off the coast of West Africa and Brazil [Clark and
Pickering, 1996; Abreu et al., 2003]. For instance, the Amazon fan reveals a maximum sinuosity
of 2.6 in its mid-fan region at 3°- 7° North [Pirmez and Imran, 2003]. In contrast, high latitude
systems reveal generally only small sinuosity [Peakall et al., 2011] and can show distinct levee
asymmetries [Menard, 1955]. Examples of low sinuosity channels are the NAMOC with a
sinuosity of 1.01-1.05 at 59° North [Klaucke et al., 1997] and the Bering Sea channels that have
a mean sinuosity of 1.05 at 55° North [Clark and Pickering, 1996].
Due to the large dimensions of submarine channel systems and the associated long travel
time, turbidity currents are deflected and slowed by Coriolis forces at higher latitudes [Wells,
2009]. The Coriolis parameter f = 2Ω sinφ (with Ω being the Earth’s rotation rate and
φ being the latitude) represents the magnitude of the Coriolis force and is defined positive in the
Northern Hemisphere (+f) and negative in the Southern Hemisphere (-f). The Rossby number
RoW = U/Wf (where U is the mean downstream velocity, W the channel width) can then be used
to determine whether a submarine channel system is influenced by Coriolis forces [Cossu et al.,
2010]. Komar [1969] introduced a momentum balance for gravity currents flowing in a channel
bend as:
2 dh hf h
Frdy U R
= +
[5.1a], 2 1
W
h WFr
h Ro R
∆ = +
[5.1b]
123
where dh/dy is the interface slope across the channel, Fr is the Froude number (defined
as Fr = U / g 'h with g’ being the reduced gravity of the density interface), h is the mean height
of the current and R is the radius defined as positive if it turns left in the Northern Hemisphere.
Equation [5.1a] can be expressed in terms of RoW with ∆h representing the height difference of
the left and right channel levee (Eq. [5.1b]). This height difference can be observed in many
cross channel asymmetries and is attributed to the deflection of turbidity currents to one side so
that sediment is also predominantly deposited at one side of the channel levee system due to
overbanking [Menard, 1955; Klaucke et al., 1997]. For a given channel geometry where the ratio
W/R is fixed, the cross channel slope dh/dy depends on the magnitude of RoW. In high latitude
systems with /WRo R W< turbidity currents are more strongly deflected, resulting in larger
levee asymmetries [Komar, 1969]. It follows that less sinuous channels at high latitudes are
dominated by Coriolis forces, whereas sinuous submarine channels at low latitudes often have
/WRo R W>> and hence are dominated by centrifugal forces [Cossu and Wells, 2010]. The
motivation of this study is to investigate how the deflection of the velocity core in gravity
currents affects the growth of channels and their sinuosity due to depositional processes inside
the channel.
Recent laboratory studies [Amos et al, 2010 and references therein] have analyzed how
the internal flow structure of gravity currents determines the locations of erosion and deposition
in sinuous submarine channels. Amos et al. [2010] introduced a conceptual model that explains
the morphological evolution and associated depositional histories of submarine channel systems
at low latitudes (RoW ~∞). In this study we extend the process model of Amos et al. [2010] to
systems where /WRo R W< using new observations of the dependence of the position of the
downstream velocity core on RoW. We discuss how Coriolis forces could influence the evolution
124
and architecture of submarine channels. Our updated process model predicts that sediment
transport processes will change with latitude so that channel sinuosity, as well as levee
deposition, could differ significantly between the equator and the poles.
5.2 Method
The experiments were conducted in a sinuous channel model placed within a 1.85 m ×
1.0 m × 0.35 m rectangular tank. This tank was rotated at a constant rate, with Coriolis
parameters ranging from f = 0 to ± 0.5 rad s-1. The tank was spun up for at least 30 min in order
to achieve solid body rotation of the water. The channel had a constant, rectangular cross-section
with a width of W = 0.1 m and a height of H = 0.08 m (similar in dimensions to Amos et al.,
2010) and was submerged under 0.1 m of water at the inflow point. The channel consisted of a
0.64 m long straight section, joined to a 0.9 m long single left turning channel bend with a mean
radius of R = 0.36 m and sinuosity of 1.09 (Figure 5.1). The slope was either 1:50 or 1:25. A
constant velocity of the inflow was achieved by using a 0.10 m thick diffuser. We used saline
gravity currents which are a good surrogate for fine mud turbidity currents [e.g. Keevil et al.,
2006; Amos et al., 2010; Sequeiros et al., 2010]. To visualize the slope of the gravity current
interface at the bend apex, fluorescein dye was added. Photographs were taken looking upstream
into the channel bend. Downstream and cross stream velocity data in the channel bend were
recorded using a Metflow Ultrasonic Doppler Velocity Profiler (UDVP, as in Keevil et al., 2006)
and additional downstream data were taken along the channel with a Nortek Acoustic Doppler
Velocimeter (ADV, as in Cossu et al., 2010). The UDVP probe records simultaneous single
component velocity data along a profile of 128 points along the beam axis at a frequency of 4
Hz. Vertical velocity profiles were obtained from an array of 6 transducers at heights of 0.5, 1.5,
2.5, 3.5, 4.5 and 5.5 cm above the bottom. The ADV consists of one transmitter and three
125
receivers and measures the 3 components of velocity at a frequency of 50 Hz in a sample volume
of 80 mm3 that is 50 mm away from the probes [Cossu et al., 2010]. The velocity components
measured by the ADV were recorded 0.5, 1, 2, 3, 4 and 5 cm above the bottom (Figure 5.1). The
ADV and UDVP velocities data were averaged over an interval of 30 s after the head of the
current had passed the instrument.
Fig. 5.1: Schematic diagram of the laboratory channel showing location of velocity measurements.
5.3 Results
In the non-rotating flow (f = 0 rad s-1, RoW = ∞) the vertically averaged velocity at the
centre line was U = 0.052 m s–1. This flow had a mean thickness of h = 0.06 ± 0.005 m and a
reduced gravity of g’= 0.098 m s-2, giving a subcritical Froude number Fr = 0.68 ± 0.15, similar
to comparable experiments [Straub et al., 2008; Amos et. al., 2010]. The Reynolds number of the
flow was Re = 3100 (where Re= U h/ν, with ν being the molecular viscosity) again of a
comparable magnitude as in similar non-rotating experiments [Kane et al., 2008; Amos et al.,
2010].
126
Our observations of the interface slopes from 20 experiments in the sinuous channel and
11 experiments in a straight channel (data taken from Cossu et al., 2010) are summarized in
Figure 5.2. There is good qualitative agreement with Eq. [5.1b] in that for the straight channel
(where W/R = 0) we find ∆h / h ∝ Fr 2 / RoW
.
Fig. 5.2: Relationship between Fr 2 / RoW
and the lateral tilt of the interface ∆h / h for different rotation
rates, channel slopes and for sinuous and straight channel sections. In the straight channel the data collapses
to the dashed line where ∆h / h = 1.5 × Fr 2 / RoW
. The experiments in the sinuous channel collapse to the
solid line that has the same slope.
In the sinuous channel (with W/R ~ 0.28), the interface is flat at a negative value of Fr2/RoW = -
0.4 ± 0.1 indicating that in left-turning bends Coriolis forces and centrifugal forces counteract
and for ∆h / h = 0 balance each other in the Southern Hemisphere (f < 0). Without rotation
(Fr2/RoW = 0) we observe a height difference ∆h / h = 0.5 ± 0.1 which reflects the dominance of
the centrifugal force in the momentum balance at the equator and low latitudes. The data for
observed ∆h h for all 31 experiments collapses well to the dashed and solid lines which have a
slope of 1.5, which is in favorable agreement to the predicted slope of 1 from Eq. [5.1b].
127
The main experimental results for the internal flow structure are shown in Figure 5.3a-d,
where we compare the slope of the interface (Figure 5.3a), the position of umax (Figure 5.3b) and
across-stream velocities (Figure 5.3c) in the bend apex, for various Coriolis parameters f. The
spatial variations of the measuring locations of umax are shown in Figure 5.3d. The changes in the
position of the density interface clearly correspond to changes in the position of the location of
umax, so when the interface is deflected to the right, so is the location of umax (Figure 5.3b). For f
= 0 rad s-1 (RoW ~∞) the velocity core is predominantly close to the centre line whilst for f = -0.5
rad s-1 (RoW = -0.65) a significant deflection of the velocity core towards the inner bend can be
seen. For f = +0.25 rad s-1 (RoW = +1.5) the velocity core is shifted towards the outer bank, and at
the base of the current at the outer bend the downstream velocity has increased to 0.085 m s-1,
while there is almost no downstream flow (< 0.01 m s-1) near the inner bend. In Figure 5.3c we
observe a basal outward helical circulation for f = 0 rad s-1 (RoW ~∞) but the velocity field
changes significantly for f = ±0.5 rad s-1 (RoW = ±0.65) as velocities at the base decrease by a
factor of 4 and the entire helical flow cell is lifted up. For f = -0.5 rad s-1 the flow cell is reversed
compared to f = 0 rad s-1 with an inward directed flow and a return flow above it [see Cossu and
Wells, 2010]. The locus of umax is marked by a dashed line in Figure 5.3d. For f = 0 rad s-1 it
alternates between left and right turning bends, similar to patterns described in Keevil et al.
[2006] or Straub et al. [2008]. However, with f = -0.5 rad s-1 we observe that the location of the
downstream velocity maximum is also pushed to the left-hand-side in the channel upstream and
downstream of the bend apex (Figure 5.3d). Similarly for f = +0.5 rad s-1 both the velocity core
and the location of the velocity maximum are shifted to the right-hand-side along the channel
pathway.
128
Fig. 5.3: a) Lateral tilt of the density interface in the bend apex for various f. b) Corresponding distribution of the velocity core in the bend apex for various f. c) Across stream velocities in the bend apex for various f. d) Distribution of the bottom downstream component in a sinuous submarine channel for f = 0 rad s-1 and f = ± 0.5 rad s-1. The locus of the highest velocity is indicated by the dashed line.
129
5.4 Discussion
In submarine channels at high latitudes |RoW|< |R/W|, where Coriolis forces control the
internal flow structure of turbidity currents, it seems likely that the spatial distribution of
sedimentation and erosion could be different than in low latitude systems. As outlined by Amos
et al. [2010] sedimentation regimes can be classified as bed-load (Figure 5.4a-c) or suspension
fall-out dominated (Figure 5.4d-f). In non-rotating bed-load dominated turbidity currents with
/WRo R W>> (Figure 5.4a) sediment is eroded from the left-hand-side upstream of a bend and
accumulates on the inner bank downstream of the bend as inner lateral accretion packages [LAP,
e.g. Peakall et al., 2007a; Amos et al., 2010]. A similar growth of LAPs in channel bends is also
seen in river bends and attributed to perturbations of the primary flow field by the centrifugal
force [e.g. Johannesson and Parker, 1989]. Subsequent growth of LAPs continuously increases
the sinuosity of these channels [Abreu et al., 2003; Babonneau et al., 2010]. However, in high
latitude systems in the Southern Hemisphere ( /WRo R W< , Figure 5.4b) centrifugal forces are
outbalanced by Coriolis forces and the location of the velocity maximum is always on the left-
hand-side promoting erosion rather than deposition on the inside bank in the bend apex. This
effect would be even more pronounced in right turning bends where Coriolis force and
centrifugal force magnify the erosion on the outside bend. This is also evident as across stream
velocities near the base (Figure 5.3c) have reduced significantly, so that we expect a less
pronounced sediment transport across the channel. It can be concluded that this shift leads to an
overall lateral migration of the channel system to the left (dashed line). In the Northern
Hemisphere ( /WRo R W< , Figure 5.4c) we observe highest velocities always on the right-
hand-side suggesting a mirrored erosion depositional pattern as in Figure 5.4b.
130
Fig. 5.4: Predicted sedimentation pattern in bed-load and suspension fall-out dominated turbidity currents in a left- turning submarine channel for a,d] RoW = ∞, b,e] |RoW| < |R/W| in the Southern Hemisphere and c,f) for |RoW|< |R/W| in the Northern Hemisphere. The dashed lines delineate a possible channel plan form evolution with time.
131
Hence, in high latitude systems we predict that the formation of LAPs on both sides of
the channel will be suppressed and that deposition generally will occur in regions of minimum
downstream velocities, which are continuously on the same side upstream and downstream of a
bend apex as sketched in Figure 5.4b and 5.4c. This will minimize the potential for increases in
channel sinuosity and promote a lateral migration of the entire channel system, e.g. to the right-
hand side in the Northern Hemisphere.
In contrast, in suspension fall-out dominated regimes (Figure 5.4d-f) there is a vertical
accretion of the submarine channel [Nakajima et al., 2009; Amos et al., 2010]. Without rotation
(RoW = ∞) the deposition occurs predominantly along the outside bend where the downstream
velocity and suspended sediment concentration is largest [Amos et al., 2010]. Continuous
deposition in outer bends leads to vertical aggradation of the channel and little change in the
channel planform geometry [Straub et al., 2008; Kane et al., 2008]. In the Southern Hemisphere
(for /WRo R W< ) we found that the location of umax and the largest flow thickness and hence
the maximum sediment concentration will always be on the left-hand-side (Figure 5.4e), so that
in fine grained turbidity currents suspension fall-out would occur also on the left side along the
channel pathway. Particularly in right-turning bends in the Southern Hemisphere, when Coriolis
and centrifugal forces work in the same direction and amplify the inertial run-up, more sediment
will be deposited on the outside bend. Over time a continuous deposition on the left-hand-side
could decrease the sinuosity as sketched in Figure 5.4e. In the Northern Hemisphere where (for
/WRo R W< , Figure 5.4f) the sedimentation pattern will mirror that in the Southern
Hemisphere as the flow velocity maximum and maximum sediment concentration are shifted to
the right-hand-side of the channel (Figure 5.3d).
Between 53°- 59° North the NAMOC exhibits RoW < 0.5 [Cossu et al., 2010], and
132
/WRo R W>> [Klaucke et al., 1997] so that /WRo R W< . Using Figure 5.2 with Fr = 1 it
follows that the tilt of the interface is strongly dominated by Coriolis forces [Klaucke et al.,
1997; Cossu et al., 2010] so that the velocity core will also be strongly shifted to the right-hand-
side. The stratigraphy of the NAMOC shows fine sediments on its levees and coarser material
inside the channel [Klaucke et al., 1998; Skene et al., 2002] so we expect the depositional pattern
to be similar to the models in Figure 5.4c and 5.4f. The strong asymmetry between the right and
left levees, the low sinuosity and the minor lateral migration to the left in the NAMOC [Klaucke
et al., 1998] can be explained if suspension-fall out deposition predominantly takes place on
right-hand-side of the levee system and a deflection of the velocity core inside the channel to the
right inhibits a strong growth of sinuosity in channel bends. In contrast, for the Amazon fan we
obtain 30WRo > [Cossu and Wells, 2010] and / 1R W < [Pirmez and Imran, 2003], so that
/WRo R W>> and thus centrifugal forces will be dominant. The high sinuosity has been
attributed to the shift of umax due to centrifugal forces [e.g. Imran et al., 1999] leading to
formations of LAPs at inner banks behind bend apexes [Abreu et al., 2003].
Despite the significant role of Coriolis forces upon the flow properties in turbidity
currents, there are several other factors that may influence the evolution of sinuosity at high and
low latitude channel systems. Present day flows on continental margins are unlikely to be in
equilibrium with their channel morphology, as those channels were primarily formed during the
last glacial low-stand and subsequent sea-level rise [Imran et al., 1999; Parsons et al., 2010].
Particularly at times of rapid ice retreat glacially fed channels at high latitudes [Peakall et al.,
2011] may exhibit significant variations in flow and sediment type, and hence behave differently
to systems with direct inputs of large equatorial rivers such as the Amazon or Zaire fan.
However, as the morphology in submarine channel systems is mostly controlled by the
133
hydrodynamics of channelized flow [Clark and Pickering, 1996] our observations of the change
in hydrodynamics with latitude due to varying f and hence RoW might be the major control of
sinuosity in large-scale depositional channels in continental shelf and fan systems.
5.5 Summary and conclusions
We used a physical model to demonstrate the influence of Coriolis forces on flow
properties in gravity currents in order to explain the observed latitudinal dependence on sinuosity
in submarine channels [Peakall et al., 2011]. Based upon the locations of the velocity maxima
and the dependence of erosion and deposition on the velocity structure we suggest that Coriolis
forces will introduce a shift at high latitudes. When the width W, the radius R and the velocity U
of channel systems are known, the ratio RoW to R/W can be used to determine if depositional
patterns are influenced by Coriolis forces. In bed-load dominated flows at high latitudes we
predict that LAPs are built only on one side, thus inhibiting the growth of channel bends. In
suspension fall-out regimes sediment will mainly be deposited on the side to which the high
velocity core is shifted resulting in significant levee asymmetries due to overbanking. In both
sedimentation regimes, the shift of the velocity core to either the left- or right-hand-side of the
channel should lead to a gradual decrease in sinuosity in mid- and high latitude systems and a
lateral migration of the entire channel pathway. For channel systems at high-latitudes in the
Northern Hemisphere we predict /WRo R W< , so that channels exhibit a low sinuosity, have a
distinct higher right levee system and migrate predominantly to the left side. In channel systems
at low latitudes we usually find /WRo R W> implying that Coriolis forces are negligible. LAPs
are then formed on the inside of bends enabling an increase in sinuosity. Therefore equatorial
channel systems can become very sinuous, show a distinct lateral migration to both sides and
alternating levee asymmetry in subsequent channel bends.
134
Acknowledgements
RC was partially supported by the CGCS at the University of Toronto. MGW acknowledges support from NSERC,
CFI and the Ontario MRI. The Metflow UDVP system was borrowed from Jeff Peakall of the NERC supported
Sorby Environmental Fluid Dynamics Laboratory at the University of Leeds. We thank Nick Eyles, Brian
Greenwood and Joe Desloges for advice and discussions.
References
Abreu, V., Sullivan, M., Pirmez, C., and Mohrig, D., 2003, Lateral accretion packages (LAPs): an important
reservoir element in deep water sinuous channels. Mar. Pet. Geol., 20, 631-648.
Amos, K.J., Peakall, J., Bradbury, P.W., Roberts, M., Keevil, G., and Gupta, S., 2010, The influence of bend
amplitude and planform morphology on flow and sedimentation in submarine channels. Mar. Pet. Geol.,
27, 1431-1447.
Babonneau, N., Savoye, B., Cremer, M., and Bez, M., 2010, Sedimentary architecture of a submarine channel:
detailed study of the present Congo Turbidite Channel (Zaiango project). J. Sed. Res., 80, 852-866. doi:
10.2110/jsr.2010.078
Clark, J.D., and Pickering, K.T., 1996, Submarine channels: processes and architecture. Vallis Press, London, 231
pp.
Cossu, R., Wells, M.G. and Wahlin, A.K., 2010, Influence of the Coriolis force on the velocity structure of gravity
currents in straight submarine channel systems. J. Geophys. Res., 115, C11016 doi:10.1029/2010JC006208
Cossu, R., and Wells, M.G., 2010, Coriolis forces influence the secondary circulation of gravity currents flowing in
large-scale sinuous submarine channel systems. Geophys. Res. Letts., 37, L17603 doi:10.1029
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Imran, J., Parker, G., and Pirmez, C., 1999, A nonlinear model of flow in meandering submarine and subaerial
channels. J. Fluid Mech., 400, 295- 331.
Islam, M.A., Imran, J., Pirmez, C., and Cantelli, A., 2008, Flow splitting modifies the helical motion in submarine
channels. Geophys. Res. Letts., 35, L22603, doi:10.1029/2008GL034995.
Johannesson, H. and Parker, G., 1989, Linear theory of river meanders. In River Meandering (ed. S. Ikeda and G.
Parker), AGU, 181-213.
Kane, I.A., McCaffrey, W.D., and Peakall, J., 2008, Controls on sinuosity evolution within submarine channels.
Geology, 36, 287-290.
Keevil, G.M., Peakall, J., Best, J.L., and. Amos, K.J., 2006, Flow structure in sinuous submarine channels: Velocity
and turbulence structure of an experimental submarine channel. Mar. Geol., 241, 241-257.
Klaucke, I., Hesse, R., and Ryan, W.B.F., 1997, Flow parameters of turbidity currents in a low-sinuosity giant deep-
sea channel. Sedimentology, 44, 1093-1102.
Klaucke, I., Hesse, R., and Ryan, W.B.F., 1998, Seismic stratigraphy of the Northwest Atlantic Mid-Ocean Channel:
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Komar, P.D., 1969, The channelized flow of turbidity currents with application to Monterey deep-sea fan channel. J.
Geophys. Res., 74, 4544-4548.
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Nakajima, T., Peakall, J., McCaffrey, W.D., Paton, D.A., and Thompson, P.J.P., 2009, Outer-bank bars: a new intra-
channel architectural element within sinuous submarine slope channels. J. Sediment. Res., 79, 872–886.
Parsons, D.R., Peakall, J., Aksu, A.E., Flood, R.D., Hiscott, R.N., Besiktepe, S., and Mouland, D., 2010, Gravity-
driven flow in a submarine channel bend: Direct field evidence of helical flow reversal. Geology, 38, 1063–
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136
6 Final remarks
6.1 Summary and implication
In this thesis, the role of Coriolis forces on channelized large-scale turbidity currents
flowing through straight and sinuous submarine channels is investigated with physical
modelling. This is approached systematically: i) verification of the methodolog; ii) laboratory
experiments in a straight channel; and iii) laboratory experiments in a sinuous channel. The
results are summarized in a conceptual model contrasting the features and different growth
patterns of submarine channels at low and high latitudes due to the magnitude of Coriolis forces.
6.2.1 Density currents as an analogue for turbidity currents
Studies of the dynamics and characteristics of large-scale turbidity currents rely on
laboratory experiments, numerical techniques and field studies of turbidites. In particular, the
applicability and scalability of analogue experiments hinges on the constraints of the
experimental set-up, such as the spatial scale or the similarity of saline to sediment-laden flows.
Small-scale laboratory experiments of rotating density currents were conducted to simulate and
investigate the flow characteristics, which are most likely to be found in large-scale turbidity
currents. As discussed in Chapter 2, saline and weakly-depositional sediment-laden gravity
currents have generally a similar turbulence structure near the bottom with both flow types
revealing very similar vertical velocity, Reynolds stress and TKE distributions. Similar results
have been reported for the bulk and upper part of density and turbidity currents [Stacey and
Bowen, 1988; Islam and Imran, 2010 and partly by Gray et al., 2006]. These observations
suggest that saline and sediment-laden flows are dynamically similar when the settling velocity
is outbalanced by high turbulent velocities near the bed. In addition, a very good agreement
137
between velocity profiles of field gravity currents and laboratory gravity currents was observed.
This implies that findings of several recent studies [Johnson et al., 1994; Dallimore et al., 2001;
Peters and Johns, 2006; Umlauf and Arneborg, 2009a] on the interior dynamics of density
overflows could also be applied to understanding non-depositional large-scale turbidity currents.
However, not all turbidity currents are weakly-depositional or entirely fine-grained and might
show completely different behavior [Kneller and Buckee, 2000]. Hence, the outlined results
remain limited for the specific class of fine-grained and weakly-depositional turbidity currents.
6.2.2 Coriolis forces in straight submarine channels
Geological studies related to submarine channel systems usually refer to the theoretical
model of Komar [1969]. This model has been used predominantly to derive mean flow
parameters of turbidity currents flowing through submarine channels from channel geometries
and channel grain sizes [e.g. Bowen et al., 1984; Klaucke et al., 1997; Imran et al., 1999] using a
simple momentum balance between Coriolis, centrifugal and pressure gradient forces. However,
flow characteristics of channelized turbidity currents are far more complex as recent studies of
secondary flow fields in channel bends have demonstrated [i.e. Keevil, et al., 2006; Peakall et al.,
2007a; Islam and Imran 2008; Straub et al., 2008]. There is, however, a substantial analysis of
the importance of Coriolis forces on turbidity currents still missing as these earlier studies refer
to non-rotating environments, omitting potential influences from the Earth’s rotation. Therefore,
the experimental data discussed in this thesis contribute to a better understanding of turbidity
currents and turbidite systems. In Chapter 3 it was demonstrated that the downstream velocity
decreases significantly and the interface tilt increases with increasing Coriolis force. In addition,
secondary circulations develop throughout the whole thickness of the current that are driven by
Ekman boundary layer dynamics. These secondary flow cells promote an upwelling at the right-
138
hand-side of the channel in the Northern Hemisphere (Figure 3.10) which governs most likely
sedimentation transport processes and the evolution of levee systems. The Rossby number RoW =
U/Wf can be used to determine whether the rotational effects become important. As discussed in
Chapter 3 for systems with RoW ~ O(1) a theoretical model using Ekman boundary layer
dynamics [Wåhlin, 2004; Darelius, 2008] is more powerful in describing the flow field of
turbidity currents than the theory of Komar [1969]. Consequently, for geological applications
Ekman boundary layer dynamics should be used to describe the characteristics of gravity
currents rather than the theory of Komar [1969] for channel systems at high latitudes.
6.2.3 Coriolis forces in sinuous submarine channels and their implication for the evolution
of channel systems
Ultimately, the analysis of the internal flow structure in rotating density currents gives
rise to a conceptual model that helps to describe sedimentation patterns and evolution in straight
and sinuous submarine channels. The new results extend and improve an existing model [Amos
et al., 2010] by incorporating Coriolis forces so that it becomes more suitable to explain features
such as different asymmetries and sinuosity in channels at various latitudes.
Previous studies [Keevil et al., 2006; Peakall et al., 2007a; Islam and Imran 2008; Straub
et al.; 2008; Kane et al., 2008; Amos et al., 2010] observed secondary flow fields that are solely
driven by centrifugal and pressure gradient forces. The experiments in Chapter 4 showed that
Coriolis forces also have a significant effect on flow dynamics in sinuous channel systems which
will influence their evolution and growth at high latitudes. Depending on the magnitude of
curvature (magnitude of centrifugal forces), the latitude (magnitude and sense of rotation) and if
the channel bend turns to the left or the right, Coriolis forces can either balance, counteract or
magnify centrifugal forces. For small Rossby numbers RoR, where the radius of curvature is used
as a length scale, Coriolis forces significantly change secondary circulations in channel bends. In
139
Chapter 5 it was found that Coriolis forces can introduce a shift in the velocity core and the
superelevation of the interface and therefore change locations of erosion and deposition. At high
latitudes the results implied that LAPs [Abreu at al., 2003] are built only on one side, thus
inhibiting the growth of channel bends. Moreover, finer sediments from suspension fall-out
regimes will be deposited mainly where the high velocity core has shifted to result in significant
levee asymmetries due to overbanking. Hence, large Coriolis forces can lead to a decrease in
sinuosity in mid and high latitude systems and can cause a lateral migration of the entire channel
pathway which could explain the observed latitudinal dependence on sinuosity in submarine
channels [Peakall et al., 2011]. The ratio RoW to R/W can be used to determine if depositional
patterns are dominated by Coriolis forces. If |RoW|< |R/W|, high-latitudes systems will exhibit a
low sinuosity. In the Northern Hemisphere these channel systems have a distinctly higher right-
hand levee system and migrate predominantly to the left-hand side. In contrast, submarine
channels in low latitudes usually have |RoW| > |R/W| implying that Coriolis forces are negligible
so that centrifugal forces dominate the flow characteristics. Hence, equatorial channel systems
can become very sinuous, show a distinct lateral migration to both sides and alternating levee
asymmetry in subsequent channel bends [Abreu et al., 2003; Pirmez and Imran, 2003; Peakall et
al., 2011].
For geologic studies the conceptual model could be employed to further investigate and
characterize levee build-ups of channel systems. For instance, Klaucke et al. [1998] analyzed
core samples of the western and eastern levees of the NAMOC and found substantially thicker
Bouma divisions TC-TE on the western (right-hand-side) levee which was attributed to Coriolis
forces [Klaucke et al., 1997]. If similarly extensive and continuous asymmetries are found in
ancient channel levee deposits at low latitudes it could be concluded that the channel system had
been deposited in a high latitude setting and had been moved to its current location by plate
140
tectonics. Hence, the Coriolis force and resultant depositional pattern (e.g., Figure 5.4) could be
used as a key indicator to interpret and better understand facies models of modern or ancient
submarine channel deposits.
6.2.4 Future work
This thesis points towards interesting future research in submarine channels. Due to the
general difficulties in obtaining field data of large-scale channel systems, testing of the findings
against environmental data is desirable, but seems unlikely in the nearer future. Therefore, the
next step would be to repeat similar experiments at a larger scale which enables larger
experimental Reynolds numbers so that a larger dynamic similarity between experiment and
natural current can be achieved. One conceivable set-up would be the use of a deformable
bottom boundary similar to Peakall et al. [2007] or Amos et al. [2010]. Larger laboratory scales
would also allow the use of sediment-bearing currents as in Straub et al. [2008] or Islam and
Imran [2010] so that sediment properties as well as other types of turbidity currents (such as
erosional or strongly depositional flows) could be investigated. Furthermore, processes like flow
spilling and stripping and the related sediment delivery to areas adjacent to the channel could be
analyzed. As demonstrated in Chapter 3 to Chapter 5, Coriolis forces promote sediment transport
only to one side of the channel, but direct measurements of overspilling or density profiles could
lead to a more quantitative analysis of levee evolution. Another question that requires more
research relates to sediment processes inside the channel. Though there was a good agreement
between saline and sediment-laden flows (see Chapter 2), the analysis of Reynolds stresses in the
flow field of rotating experimental currents was not covered in this thesis. Hence, further work
that gives more insight into the turbulence structure of rotating turbidity currents to complement
findings of sediment-transport processes inside the channel as reported in Chapter 4 and V, is
141
necessary. Lastly, studies investigating channelized flow characteristics [i.e. Keevil et al., 2006;
Paekall et al., 2007; Imran et al., 2007; Islam and Imran, 2008; Straub et al., 2008; Kane et al.,
2008] used models that differ in size, aspect ratio and cross-sectional geometry. This might be an
important factor influencing flow processes [Islam et al., 2008; Straub et al., 2008] and it still
remains to be clarified to what extent the results in this thesis are affected by the rectangular
channel geometry and its aspect ratio. It is recommended therefore that future studies consider
using different channel geometries (aspect ratios) to shed light on the relevance of morphological
channel geometry for flow structures.
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