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UFL/COEL-99/016
LOCAL SEDIMENT SCOUR AT LARGE CIRCULAR
PILES
By
ATHANASIOS PRITSIVELIS
Thesis
1999
LOCAL SEDIMENT SCOUR AT LARGE CIRCULAR PILES
By
ATHANASIOS PRITSIVELIS
A THESIS PRESENTED TO THE GRADUATE SCHOOL
OF THE UNIVERSITY OF FLORIDA IN PARTIAL FULFILLMENT
OF THE REQUIREMENTS FOR THE DEGREE OF
MASTER OF SCIENCE
UNIVERSITY OF FLORIDA
1999
ACKNOWLEDGMENTS
I would like to express my deepest gratitude to my advisor and committee
chairman Dr. D. Max Sheppard. His continuous support and his insight have permitted
this study to become a reality. I would like also to thank Dr. Mufeed Odeh, P.E., head of
the Engineering Section at the USGS Laboratory part of my committee, for his support
during my 14-month stay in Massachusetts. My thanks also go out toward Dr. Robert
Dean and Dr. Robert Thieke for serving on my supervisory committee.
John Noreika, Stephen Walk, Phil Rokasah and the other members at the USGS-
BRD Laboratory in Massachusetts also deserve my thanks for putting up with me and
helping me on the practical parts of the experiments. Also deserving my deepest
appreciation are Tom Glasser and Edward Albada for helping me, sometimes working 15
hours, with the experiments.
Sidney Schofield, Jim Joiner, Vernon Sparkman, Chuck Broward, and the other
members of the Coastal and Oceanographic Engineering Laboratory also deserve my
thanks for their assistance, as well as Chris Jette for answering all my questions about
transducers fast and efficient.
I am also grateful to J.S. Jones, P.E. with the Federal Highway Administration and
Shawn McLemore, P.E., and Rick Renna, P.E., with the Florida Department of
Transportation for their financial support for this research and their interest and helpful
suggestions.
Many others deserve a hearty thank you. My fellow students, including Ed, Roberto,
Guillermo, Hugo, Tom, Bill, and Erika, for the help on classes. Additional gratitude goes
to Becky, Helen, Laura, and so many other people at the department.
Finally, I want to express my deepest gratitude to my parents, George and Vasiliki,
and my sister Helen for their patience and lifelong support.
TABLE OF CONTENTS
page
ACKNOWLEDGMENTS ........................................................ ... ......................... ii
LIST OF TABLES ....................................................................................................... vi
LIST OF FIGURES..................................................................................................... vii
KEY TO SYMBOLS ........................................................................................................ xii
A B STR A C T ...................................................................................................................... xv
CHAPTERS
1 INTRODUCTION.................................................................................................... 1
2 BACKGROUND AND LITERATURE REVIEW.................................. .......... .7
Description of the Flow Field Around a Pier.......................................... ...............7
Scour Formulation for Steady Flow....................................................................... 9
Effect of the Various Parameters .............................................................................11
Effect of Aspect Ratio yo/b .............................................. ................................ 11
Effect of Velocity Ratio U/Uc .................................................................. 13
Effect of Sediment to Pier Size Dso/b................................................................17
Effect of Sediment Gradation ............................................................................ 19
Effect of Pier Properties (Shape and Alignment) ....................................... ...21
3 EXPERIMENTAL APPROACH.........................................................................24
Facilities and Instrumentation....................................................................................24
Facilities...........................................................................................................24
Instrum entation ................................................................................................28
Velocity measurement..............................................................................28
Water level measurement.............................................................. ...........29
Temperature measurement.............................................................................29
Acoustic transducers ................................................................................30
Video measurements ..................................................................... ...........32
Measurement setup ..................................................................................35
Point gauging ...................................................................................................36
M odels....................................................................................................................36
Sedim ent ................................................................................................................38
4 EXPERIMENTAL DATA REDUCTION AND ANALYSIS...................................41
Experim mental Pprocedure.............................................................................................41
Data Reduction.......................................................................................................43
Processed Data Results .......................................................................................... 44
Discussion of Results...................................................................................................56
5 COMPARISON OF LOCAL SCOUR PREDICTION EQUATIONS ........................ 58
Scour Prediction Equations..........................................................................................58
Com pilation of Local Scour Data ................................... .........................................65
Com parative Analysis ..................................................................................................67
Field Data Example................................................................................................85
6 SCALING MODEL SCOUR DEPTHS TO PROTOTYPE CONDITIONS ...............89
7 SUM M ARY AND CON CLU SION S .................................................................96
Sum m ary ................................................................................................................96
Conclusions..................................................................................................................98
Recom m endations for Future W ork............................... .......................... ..........99
APPENDICES
A EFFECTS OF THE W EIR ........................................................................................100
B FLOW UNIFORM ITY ..............................................................................................103
C EXPERIM EN TAL DATA ........................................................................................105
D COMPARISON OF METHODS CALCULATING CRITICAL DEPTH
AVERAGE VELOCITY .................................. ................. ................................109
REFEREN CES .......................................................................................................... 14
BIOGRAPHICAL SKETCH ........................................ ................ ........................... 118
LIST OF TABLES
Table page
2.1 Shape factor for pier nose, taken from HEC-18 (1995).........................................22
2.2 Other factors for pier shapes ............................................................................... 22
2.3 Correction factor K2 for angle of attack 0 of flow, where L is the length of the pier
and b the width, taken from HEC-18 (1995) ................................... ........... 23
3.1 Table with values of (-log (D50/b)) before sand availability..................................37
3.2 Table with values of (-log (D5o/b)) for the piles and sediment used in the tests......38
4.1 Parameters for the experiments conducted .........................................................41
6.1 Cases for model and prototype..............................................................................93
A.1 Prototype and model dimensions ......................................................................100
C .1 Experim ental data............................................................................................. 105
LIST OF FIGURES
Figure page
1.1 Effects of local scour on a bridge pier
(taken from University of Louisville web site) .....................................................
2.1 Schematics of the vortices around a cylinder..................................... .............. 8
2.2 General relationship between equilibrium scour depth and
water depth when other parameters are held constant .......................................12
2.3 General relationship between equilibrium scour depth and velocity
when other parameters are held constant......... ............................. ........... 14
2.4 Dependence of scour depth on mean velocity for two types of sediment ..............16
2.5 Dependence of equilibrium scour depth on ratio of sediment diameter
to structure diameter for 1 > U/Uc > 0.9 and yo/b > 2.5 .....................................18
2.6 Influence of a on scour depth, taken from Melville and Sutherland (1988)............19
2.7 Graphic relationship between a and KI, taken from Chiew (1984) .......................20
2.8 Alignment factor K2 for rectangular piers, taken from Laursen (1958)...................21
3.1 Aerial photograph of the S.O. Conte Laboratory........................................... ..25
3.2 Schematic figure of the setup for the experiments..............................................26
3.3 A test pile with the instrumentation......................................................................31
3.4 Detailed view of the arrays for the small structures...........................................31
3.5 Detailed view of the arrays for the large structures ....................................... ..32
3.6 Picture of the cameras for the 0.114 m (4.5 in) pile..............................................33
3.7 Picture of the cameras for the 0.305 m (12 in) pile............................... ........... 34
3.8 Picture of the cameras for the 0.92 m (36 in) pile..............................................34
3.9 Diagram of the measurement system ....................................................................35
3.10 Cross-Section of the 0.92m (36 in) pier............................... .................................37
3.11 Gradation Curve for Sand No. 1 (Dso = 0.22 mm)...........................................39
3.12 Gradation Curve for Sand No. 2 (D50 = 0.80 mm)..............................................40
4.1 Elevation contour plot of the equilibrium scour hole for Experiment No.1
(b = 0.114 m, D50 = 0.22 mm, yo = 0.186 m and U = 0.290 m/s) ........................45
4.2 Elevation contour plot of the equilibrium scour hole for Experiment No.2
(b = 0.305 m, Ds0 = 0.22 mm, yo = 0.190 m and U = 0.305 m/s) ......................45
4.3 Elevation contour plot of the equilibrium scour hole for Experiment No.3
(b = 0.920 m, D50 = 0.22 mm, yo = 2.268 m and U = 0.325 m/s) ......................46
4.4 Elevation contour plot of the equilibrium scour hole for Experiment No.4
(b = 0.920 m, D50 = 0.80 mm, yo = 2.402 m and U = 0.454 m/s) ........................46
4.5 Elevation contour plot of the equilibrium scour hole for Experiment No.5
(b = 0.920 m, D50 = 0.80 mm, yo = 0.866 m and U = 0.335 m/s) ......................47
4.6 Elevation contour plot of the equilibrium scour hole for Experiment No.6
(b = 0.305 m, D50 = 0.80 mm, yo = 1.305 m and U = 0.381 m/s) ......................47
4.7 Elevation contour plot of the equilibrium scour hole for Experiment No.7
(b = 0.114 m, D50 = 0.80 mm, yo = 1.280 m and U = 0.388 m/s) ......................48
4.8 Equilibrium profiles of scour hole for Experiment No.1
(b = 0.114 m, D50 = 0.22 mm, yo = 0.186 m and U = 0.290 m/s)
a) Inline profile, and b) Normal profile.............................................................49
4.9 Equilibrium profiles of scour hole for Experiment No.2
(b = 0.305 m, Dso = 0.22 mm, yo = 0.190 m and U = 0.305 m/s)
a) Inline profile, and b) Normal profile.............................................................50
4.10 Equilibrium profiles of scour hole for Experiment No.3
(b = 0.920 m, D50 = 0.22 mm, yo = 2.268 m and U = 0.325 m/s)
a) Inline profile, and b) Normal profile..............................................................51
4.11 Equilibrium profiles of scour hole for Experiment No.4
(b = 0.920 m, D50 = 0.80 mm, Yo = 2.402 m and U = 0.454 m/s)
a) Inline profile, and b) Normal profile ............................................................52
4.12 Equilibrium profiles of scour hole for Experiment No.5
(b = 0.920 m, D50 = 0.80 mm, yo = 0.866 m and U = 0.335 m/s)
a) Inline profile, and b) Normal profile................................................ ............53
4.13 Equilibrium profiles of scour hole for Experiment No.6
(b = 0.305 m, D50 = 0.80 mm, yo = 1.305 m and U = 0.381 m/s)
a) Inline profile, and b) Normal profile................................................ ............54
4.14 Equilibrium profiles of scour hole for Experiment No.7
(b = 0.114 m, D50 = 0.80 mm, yo = 1.280 m and U = 0.388 m/s)
a) Inline profile, and b) Normal profile................................................ ............55
5.1 Local scour depth dependence on velocity, as proposed by Sheppard (1997).........65
5.2 Comparison of equations for clearwater data ...........................................................69
5.3 Comparison of equations for live-bed data....................................................70
5.4 Comparison of measured and calculated scour for clearwater data for
(A) Garde et al. (1993), and (B) Ahmad (1953) equations................................71
5.5 Comparison of measured and calculated scour for clearwater data for
(A) Breusers et al. (1977), and (B) Chitale (1962) equations ............................72
5.6 Comparison of measured and calculated scour for clearwater data for
(A) Froehlich (1988), and (B) Gao et al. (1992) equations................................73
5.7 Comparison of measured and calculated scour for clearwater data for
(A) Hancu (1971), and (B) HEC-18 (1995) equations.......................................74
5.8 Comparison of measured and calculated scour for clearwater data for
(A) Inglis-Blench (1962), and (B) Jain and Fischer (1979) equations.................75
5.9 Comparison of measured and calculated scour for clearwater data for
(A) Laursen and Toch (1956), and (B) Melville (1997) equations....................76
5.10 Comparison of measured and calculated scour for clearwater data for
(A) Shen et al. (1969), and (B) Sheppard et al. (1995) equations......................77
5.11 Comparison of measured and calculated scour for live-bed data for
(A) Ahmad (1953), and (B) Breusers et al. (1977) equations............................78
5.12 Comparison of measured and calculated scour for live-bed data for
(A) Chitale (1962), and (B) Froehlich (1988) equations............................ ..79
5.13 Comparison of measured and calculated scour for live-bed data for
(A) Gao et al. (1992), and (B) Hancu (1971) equations............................. ..80
5.14 Comparison of measured and calculated scour for live-bed data for
(A) HEC-18 (1995), and (B) Inglis-Blench (1962) equations ...........................81
5.15 Comparison of measured and calculated scour for live-bed data for
(A) Jain and Fischer (1979), and (B) Laursen and Toch (1956) equations..........82
5.16 Comparison of measured and calculated scour for live-bed data for
(A) Melville (1997), and (B) Shen et al. (1969) equations................................83
5.17 Comparison of measured and calculated scour for live-bed data
for Sheppard et al. (1995) equation........................... ........................................84
5.18 Comparison of equations for Experiment No. 3
(b = 0.920 m, Dso = 0.22 mm, yo = 2.268 m and U = 0.325 m/s) ......................86
5.19 Comparison of equations for example of field conditions............................. ..87
6.1 Fitting curves for the scale factor using equation (6.1).................................. ..91
6.2 Regions for the model and prototype cases........................................................92
6.3 Data fitting curves for the scale factor .................................................................94
A.1 Positions of velocity profile collection ................................................................ 101
A.2 Flow profiles of the model at certain distances from the entrance of the flume ....101
B.1 Contour plots of velocity for the 1.22 m (4 ft) water depth .................................104
B.2 Contour plots of velocity for the 2.44 m (8 ft) water depth ...................................104
C.1 Scour history for Experim ent 1 ................................... ........................................105
C.2 Scour history for Experim ent 2 ................................... ........................................106
C.3 Scour history for Experim ent 3 ............................................................ ................106
C.4 Scour history for Experim ent 4 ................................... ........................................107
C.5 Scour history for Experim ent 5 ................................... ........................................107
C.6 Scour history for Experim ent 6 ............................................................................108
C.7 Scour history for Experiment 7 ............................................................................108
D.1 Relationship between critical shear velocity and median grain diameter .............109
D.2 Comparison of the methods for calculating Ue in respect to
(A) Grain Median Diameter, (B) Temperature, and (C) Relative Roughness ...111
KEY TO SYMBOLS
b pile width (diameter)
bm model pile width
bp prototype pile width
B channel width
c exponent related to bed load
Cwr rectangular weir coefficient
D16 sediment size for which 16 percent of bed material is finer
Dso median sediment diameter
D5o m model median sediment diameter
D84 sediment size for which 84 percent of bed material is finer
D50 p prototype median sediment diameter
dse equilibrium scour depth
dse(c) equilibrium scour depth for a sediment with a given a
dse m model equilibrium scour depth
dse p prototype equilibrium scour depth
Fr Froude number
Frc critical Froude number
g acceleration of gravity
H head over the weir
K pier shape factor
K1 factor for shape of pier nose
K2 factor for angle of attack of flow
Kd sediment-size factor
KI flow intensity factor
Ks pier-shape factor
KyD flow depth-pier width factor
K, pier-alignment factor
K, factor for the gradation of sediment
L length of pier
Lm model scale length
Lp prototype scale length
Pw weir height
q discharge per unit width
Q discharge
R ratio of model to prototype Dso/b
Rep pier Reynolds number
Rew wall Reynolds number
s relative sediment density
S scale factor
SG geometric scale factor
U mean depth average velocity
Ue critical depth average velocity
U' velocity for the initialization of sediment movement around the
structure
u* bed shear velocity
u*e critical bed shear velocity
Vc velocity for the initialization of sediment movement around the
structure
yo depth of flow
Ca, Ca2 coefficients of scale factor, SF, related to b/Dso of prototype
0 angle of attack of flow
It dynamic viscosity of water
v kinematic viscosity of water
p density of water
Ps density of sediment
C gradation of sediment
T bed shear stress
A factor for pier shape
Abstract of Thesis Presented to the Graduate School
of the University of Florida in Partial Fulfillment of the
Requirements for the Degree of Master of Science
LOCAL SEDIMENT SCOUR AT LARGE CIRCULAR PILES
By
Athanasios Pritsivelis
August 1999
Chairman: Dr. D. Max Sheppard
Major Department: Coastal and Oceanographic Engineering
Local sediment scour experiments were performed with three circular pile diameter
(0.114 m, 0.305 m, and 0.920 m) and two sediment grain sizes (D50 = 0.22 mm and 0.80
mm) under clearwater scour conditions. The results were analyzed and combined with
data from other researchers to form two data sets, one for clearwater and one for live-bed
conditions. These data sets were used to evaluate and compare 14 different scour
prediction equations. The 0.92 m diameter pile was then considered to be a prototype pile
and the other, smaller piles models of the prototype. The model and prototype data were
then used to obtain the proper model to prototype scale factor for computing the
equilibrium scour depth for the prototype from the model results. The scale factors are
represented in plots of scale factor versus D50 (model)/ D50 (prototype) for various values of
sediment to pile diameter ratio for the prototype.
CHAPTER 1
INTRODUCTION
When designing hydraulic structures, one must consider many aspects, which are
important for the functionality and mostly for their safety and the safety of the people
depending on them.
Some of the aspects considered are (Pilarczyk, 1995):
1. Function of the structure; erosion is not always the problem as long as the
structure can fulfill its function,
2. Physical environment; the structure should offer the required degree of
protection against hydraulic loading, with an acceptable risk and, when possible,
meet the requirements resulting from landscape, recreational and ecological
viewpoints,
3. Construction method; the construction costs should be minimized to an
acceptable level and legal constrictions must be adhered to,
4. Operation and maintenance; it must be possible to manage and maintain the
hydraulic structure.
From all these aspects, the cost of construction and maintenance is generally the
controlling factor. In the case of bridge design, local scour around the piles of the bridge
is one of the factors that contribute to the total construction and maintenance cost and is
important in the estimation of stability of the structure. Underprediction can result in
costly bridge failure and possibly in the loss of lives, while overprediction can result in
millions of dollars wasted on a single bridge.
Scour in general is caused by changes in the characteristics of flow, which lead to
changes in the sediment transport in the area of interest. There is an equilibrium scour
depth associated with a given set of environmental conditions (water depth, sediment
density and size, flow velocity, etc.). When the environmental conditions change (e.g. a
change in flow velocity), the scour depth progresses toward the new equilibrium depth. If
the new conditions are maintained for a sufficiently long period of time the new
equilibrium scour depth is reached. Scour caused by a structure (e.g. a pile) can be
divided into two categories: general (or contraction) and local. As a first approximation,
the scour caused by each process can be added to obtain the total scour. Of the two types
of scour, local scour is the least understood.
General scour happens when the cross sectional area of the flow at a particular
location is reduced due in most cases to the presence of a new structure. This results in an
increase in flow velocity and bed shear stress and increases the potential for erosion of the
area. This type of scour is well understood and there are a number of methods for
predicting these scour depths.
Local or structure induced scour is caused by the structure itself. A picture of local
scour around a structure (bridge pier) is shown on Figure 1.1. The main causes of local
scour are
1) an increase in mean flow velocities in the vicinity of the structure,
2) the creation of secondary flows in the form of vortices and
3) the increased turbulence in the local flow field.
Two kinds of vortices are observed: Wake vortices, downstream of the points of flow
separation on the structure and horizontal vorticies at the bed and free surface, due to
pressure variations along the face of the structure. Those phenomena, although relatively
easy to observe, are difficult to quantify mathematically. Some researchers (Shen et al.,
1969) have attempted to describe this complex flow field mathematically but with little
success. A number of numerical solutions have also been attempted but with limited
success.
Figure 1.1 Effects of local scour on a bridge pier
(taken from a Bridge Scour Site, 1998)
Historically, scientists and engineers have used scale models in order to predict
complex prototype phenomena. This requires a knowledge and understanding of the
modeling laws for the particular situation (i.e. a knowledge of the pertinent dimensionless
groups for the processes involved), in order to extrapolate the measured values for the
model to prototype conditions. Ideally, the values of the salient dimensionless groups are
made the same in the model as they are in the prototype. This, however, is not always
possible and when it is not the extrapolation process becomes more difficult. For local
structure induced scour, the processes are characterized by three dimensionless groups,
Y U and Ds- where b is the diameter of the pile, yo is the water depth, U in the
b Uc b
mean depth average velocity, Uc is the critical depth average velocity and Ds0 is the
median sediment diameter. It is normally easy to configure the model so as to make the
first two groups the same for the model and prototype but due to lower limits on the
sediment diameter (before the sediment becomes cohesive) the third group usually cannot
be properly scaled. In many locations, such as Florida, the sediment is sand with a
prototype Ds0 between 0.1 and 0.4 mm and the structures can be large (on the order of 10
to 20 m in width). For a geometric scale of 40, the model sediment Ds0 would have to be
as small as 0.0025 mm, which is in the cohesive range, where the scour properties are
significantly different (and less understood). The problem is then, how to predict the
prototype scour depth from the scour depth measured in the model study. The most
common procedure used to date has been to simply use the prototype-to-model geometric
5
scale (i.e. dse = dsem ). Note that this ignores the differences in D0 for the model
me L b
and prototype and the impact of this difference on the scour depth.
Most scour prediction relationships, such as the Colorado State University (CSU)
relation, (currently used in the FHWA Hydraulic Engineering Circular No. 18) and the
University of Florida (UF) equation (Sheppard et al., 1995) are empirical. Many of these
equations are relatively accurate in predicting local scour for laboratory scale structures
but are very conservative in their estimates of scour depths for prototype structures. There
is a significant amount of scour data in the literature for small structures but very little for
prototype size structures in a controlled environment.
One of the objectives of the work reported in this thesis is to provide local scour data
for large circular piles. Laboratory experiments were conducted for three pile diameters,
two different sediment sizes and a range of water depths. The results of those experiments
along with other data from various researchers were then used to compare 14 different
scour prediction equations. This data set was also used to obtain the scale factor for
estimating prototype scour depths from measured model scour depths.
To better understand the problem of local scour, Chapter 2 reviews the current state
of knowledge of local scour. The primary mechanisms are reviewed first followed by the
formulation of the most important dimensionless groups for local scour.
Chapter 3 gives a detailed description of the experiments performed and the
procedures used. Seven experiments were conducted with three pile diameters and two
sediment sizes. The experiments were run for approximately 24 hours beyond the point at
which the scour depth ceased to increase.
Chapter 4 presents the experimental results and the data processing procedures. In
line and normal scour hole profiles are presented along with contour plots of the scour
holes.
Chapter 5 presents a comparison of a number of scour prediction equations using
clearwater, live-bed and a typical example of field data. The equations are compared on
their ability to predict those data and the results are shown with line and scatter plots.
In Chapter 6 the problem of scaling model scour depths to prototype conditions is
examined. A scaling factor that depends on D50 and D50 is presented.
D50-p b ) prototype
Finally, a summary of the work conducted for this thesis, along with some
conclusions and recommendations for future work is given in Chapter 7.
CHAPTER 2
BACKGROUND AND LITERATURE REVIEW
Bridge scour has received a lot more attention this past decade and a number of
advances have been made. Many researchers have conducted laboratory experiments in
order to improve the accuracy of equilibrium scour depth prediction. Most of these tests
were done with simple structures, like a single pile, in a horizontal sand bed subjected to
a steady flow. These experiments succeeded in identifying the physics of the local scour
processes. Recently, there has been an increase in the research on local scour at more
complex piers.
2.1 Description of the Flow Field Around a Pier
This section discusses the flow field near a cylindrical pile in a steady flow, as seen
from various researchers. The flow field in the immediate vicinity of a structure is quite
complex, even for simple structures such as circular piles. The dominant feature of the
flow is the large-scale eddy structure, or system of vortices that develop about the pier.
That system is the basic mechanism of local scour, and has been recognized by many
investigators (e.g. Shen et al., 1966, Melville, 1975).
It has been found that depending on the type of pier and flow conditions, the eddy
structure can be composed of one or more of the basic systems, which comprise the
horseshoe vortex and the wake vortex systems. It has also been identified that the
acceleration of the flow around the pier is a factor in the early stages of local scour.
8
The horseshoe vortex system is developed at the base of the structure. The term
"horseshoe" is derived from the shape that the system takes as viewed from above. It
wraps around the structure and tails downstream, as shown in Figure 2.1. Shen et al.
(1966) describe the horseshoe vortex system very accurately. The main cause of this
system is the stagnation pressure difference developed at the nose of the structure. If the
difference is large enough, there is a downward flow, which rolls up ahead of the toe of
the structure to form the horseshoe vortex system. The system in its simplest form is
composed of two vortices, a large one, adjacent to the structure, with a small counter
vortex. A more complicate system consists of multiple small counter vortices, which are
unsteady and periodically shed and are swept downstream. Clearly, the geometry of the
structure is important in determining the strength of the system, although it is not steady
for all kinds of structures. Blunt nosed structures create the most energetic vortex system.
Wake Reaion
'.TOP VIEW..
T P Vo .W *- -. '
SJ.OE VIWM
Figure 2.1 Schematics of the vortices around a cylinder
Melville (1975) measured mean flow directions, mean flow magnitude, turbulent
flow fluctuations, and computed turbulent power spectra around a circular pier for
flatbed, intermediate and equilibrium scour holes. He found that a strong vertical
downward flow developed ahead of the cylinder, as the scour hole enlarged. The size and
circulation of the horseshoe vortex increased rapidly and the velocity near the bottom of
the hole decreased as the scour hole was enlarged. As the scour hole develops, the
intensity of the vortex decreases and reaches a constant value at the equilibrium stage.
Although the horseshoe vortex is considered the most important scouring
mechanism for steady flows, the wake vortex system is also important. Wake vortices are
created by flow separation on the structure. Large scour holes may also develop
downstream from piers, when the horseshoe vortex system does not form, as
demonstrated by the experiments of Shen et al. (1966). With their vertical component of
flow, wake vortices act somewhat like a tornado in removing the bed material, which is
then carried downstream by the mean flow.
2.2 Scour Formulation for Steady Flow
In order to formulate quantitative relationships to predict local scour, there has to be
a distinction between clearwater and live-bed scour. Clearwater scour is the local scour
that occurs when the flow velocity is below the value needed to initiate sediment motion
on the flat bed upstream from the structure. Live-bed scour occurs when the flow velocity
exceeds the value needed to initiate sediment motion upstream of the structure. The
sediment is assumed to be cohesionless and the term local scour is assumed to be the
depth of the deepest point around the structure.
The equilibrium scour depth depends on the fluid and sediment properties, the flow
parameters, and characteristics of the structure, e.g.
dse = f [, p, g, D50, u, p,, yo, U, b, h(pier)], (2.1)
where
dse is the equilibrium scour depth,
p and ps are the density of water and sediment respectively,
g is the dynamic viscosity of water (depends on temperature),
g is the acceleration of gravity,
Ds5 is the median diameter of the sediment,
a is the gradation of sediment,
yo is the depth of flow upstream of the structure,
U is the depth average velocity,
b is the pier diameter/width normal to the flow,
h(pier) is a function that depends on the shape and the alignment of the pier in the
flow.
The most important dimensionless groups for local scour can be obtained from the
quantities given in Equation 2.1. These eleven quantities can be expressed in terms of
three fundamental dimensions: force, length and time. According to the Backingham I
theorem, 11 3 = 8 independent dimensionless groups exist for this situation. An example
of these eight groups is shown in Equation 2.2.
d U p, Ub U D50, h(pier) (2.2)
b bt *4 p v U b
Of these eight groups, the following six are considered the most important as shown in
Equation (2.3)
dse o b,U o-, h(pier)J, (2.3)
b b 'Ub b
where Uc is the critical depth averaged velocity (the velocity required to initiate sediment
motion on a flat bed).
2.3 Effect of the Various Parameters
The aspects of scour processes described by the various dimensionless groups are
understood as a result of numerous laboratory experiments. These groups are described in
the following paragraphs.
2.3.1 Effect of Aspect Ratio yv/b
The effect of flow depth on scour depth is significant. Observations (Ettema 1980,
Chiew 1984) have shown that, for shallow flows, the scour depth increases with
increasing depth of flow up to a point beyond which no effect is observed. The above is
generally accepted by many researchers e.g. Laursen and Toch (1956), Neill (1973),
Cunha (1970). As Ettema (1980) states, the effect of the flow is due to the impact it has
on the formulation of the surface and bottom vortices located at the upstream side of the
pier. The pressure differences along the nose of the pier cause a surface roller at the top
and the horseshoe vortex at the bottom. The two rollers rotate to opposite directions. In
principle, as long as they do not interfere, the local scour depth is independent of the
depth of the flow. With decreasing depth, the surface roller interferes with the downflow,
making it weaker. Other reasons are the influence of the sediment bar behind the structure
for small values of yo/b and the fact that the portion of the flow that is diverted into the
hole, diminishes for low values of yob (Ettema, 1980).
Another researcher, Bonasoundas (1973) concluded that the effects of the flow depth
were insignificant for yo/b > 1 to 3. However, his experiments were only run for two
hours and thus equilibrium depths could not have been achieved. Basak (1975), Hancu
(1971), White (1973), Chabert and Engeldinger (1956) and Jain and Fischer (1979)
observed the same general behavior for live-bed conditions.
Laboratory data (Ettema 1980, Chiew 1984, etc.) indicate that, if the other two
parameters (U/Uc and Dso/b) are held constant, the equilibrium scour depth increases
rapidly with yo/b until a value of 2.5 to 3 and then remains constant. This is shown
schematically in Figure 2.2.
2.5-
2-
1.5-
1-
0.5-
0---------------
0 1 2 3 4
yo/b
Figure 2.2 General relationship between equilibrium scour depth and water depth
when other parameters are held constant
2.3.2 Effect of Velocity Ratio U/U_
The critical depth average velocity, Uc, is important since it is the velocity at which
sediment movement is initiated on a flat bed upstream of the structure. A better
understanding of critical velocity can be achieved, by examining the forces acting on a
sediment particle subjected to a steady flow (Shields, 1936). Shields states that a critical
bed shear stress exists, above which there is movement of the sediment at the bottom.
Comparing the drag force on a grain with its submerged weight, Shields developed an
empirical formula for the critical shear stress. From the shear stress, the shear velocity,
u = can be computed. For a fully developed velocity profile, the Prandtl-Von
Karman formula can be used to compute the depth averaged velocity as a function of the
shear velocity and bed roughness (Sleath, 1984). From the above, the critical depth
averaged velocity, Uc, can be calculated. For flow velocities higher than this value, the
local scour is defined as "live-bed scour." "Clearwater scour" is defined as the local scour
that occurs for velocities less than the critical value.
Several different methods have been used by researchers to estimate the value of
critical depth averaged velocity and their results can differ significantly. Note that in
comparing data from different researchers, it is important that the same method be used
for all the data. A brief description of the more common methods for computing Uc is
given in Appendix D along with a comparison of their predicted values.
The depth of equilibrium local scour is closely related to the mean depth average
velocity. It is evident from published literature that under clearwater conditions, the local
scour increases almost linearly with the approach velocity. Breusers et al. (1977)
developed the relationship between scour depth and the ratio of U/Uc by dimensional
analysis, but applied no detailed analysis into the nature of the dependency. Hanna (1978)
found out that scour is initiated around u*/u*, = 0.5, where u* is the bed shear velocity and
u*, is the critical bed shear velocity and reaches a maximum value for u*/u*c equal to
unity. Other data, that show that the initiation of scour depth starts at around 0.4-0.5Uc,
for circular piles, come from Chabert and Engeldinger (1956) and Ettema (1980). Most of
the laboratory data seem to follow Figure 2.3.
Clearwater Live-bed
Conditions Conditions
<--- --->
-0.4-0.5
1
U/UC
Figure 2.3 General relationship between equilibrium scour depth and velocity
when other parameters are held constant
As for live bed conditions (U/Ue > 1.0); the results are even more difficult to obtain.
The difficulty resides in the fact that the experiments are difficult to perform and the
results hard to interpret. Early researchers related the relative scour depth dse/b to the
Froude number. Most of the conclusions drawn state that for a given flow depth, the
scour depth increases with increasing velocity. Later researchers e.g. Chabert and
Engeldinger (1956), Laursen (1962) etc. found that as the velocity increased beyond the
critical velocity, Uc, the scour depth decreases by about 10%. Further increases in
velocity increase the scour depth until a second peak is reached. The decrease of scour
depth after the initiation of live-bed conditions was believed to be caused by infill of the
scour hole due to movement of the bed. Hancu (1971) conducted a series of live-bed
scour experiments and concluded that the local scour depth is independent of the flow
velocity for live-bed conditions. This conclusion is similar to that of Breusers et al.
(1977).
Ettema (1980) stated though that there is a dependence of both clearwater and live-
bed equilibrium local scour depth on velocity. He concluded that the maximum value for
live-bed local scour can be lower or higher than the one for the clearwater depending on
the type of sediment (Figure 2.5). He thought that for ripple-forming sediments (D50 < 0.6
mm), the deepest scour hole is for live-bed conditions, while for non ripple-forming
sediments, the deepest scour depth occurs at transition from clearwater to live-bed
conditions. His explanation for the above distinction is that "shallower maximum depths
of local scour generally occur for ripple-forming than for non ripple-forming bed
materials, because the formation of ripples on the approach bed alters the roughness of
the bed, creates a low level of sediment transport into the scour hole, affects the boundary
layer separation at the pier and consequently changes the strength of the horseshoe
vortex". Sheppard (1997) concluded that the condition that defines which peak
(clearwater or live-bed) is higher depends on the ratio of median diameter of the sediment
and pier diameter, D50/b, and not on whether the sediment was ripple-forming.
Non ripple-forming sediment
\
Ripple-forming sediment
-0.4- 0.5
1
U/UC
Figure 2.4 Dependence of scour depth on mean velocity for two types of sediment
2.3.3 Effect of Sediment to Pier Size D5o/b
The effect of this parameter was not recognized until recently. Laursen and Toch
(1956) stated "exactly the same depth of scour should result in the model, no matter what
velocity or sediment is used, as long as there is general bed load movement and the
Froude number is everywhere less than unity". However they added "because secondary
effects of velocity and sediment size which could not be detected in the limited range of
the laboratory data may become important at large scale, the validity of this conclusion
can only be tested by model-prototype conformity studies". The results of the model study
by Chitale (1962), Ahmad (1962) support the conclusions drawn by Laursen and Toch
(1956) concerning the effect of sediment on scour depth. Krishnamurthy (1970) also
stated that the effect of sediment size is negligible for high Froude number and large pile
sizes.
The data from Chabert and Engeldinger (1956) show a small effect of sediment size
on scour depth. Nicollet and Ramette (1971) extended the experiments of Chabert and
Engeldinger (1956) and showed that the sediment size has a considerable effect. Raudkivi
and Ettema (1977) decided to hold U/Ue and yo/b constant and change D50/b. Even though
their data showed effects of sediment size, they attributed the changes to ripple formation
and it was not given further thought. Baker (1986) correlated scour depth with b/D50
using the data from Raudkivi and Ettema (1977) and found that there is a correlation
between the two values. Ettema's (1980) clearwater data showed that the influence of
sediment size is significant, if the ratio of b/D50 is less than 20-25 and that for higher
values the scour depth is independent of sediment size. A similar study to determine the
scour depth dependence on D50/b was conducted by Sheppard and Ontowirjo (1994).
Using their data and that due to Ettema (1980) and Chiew (1984), they found that the
effect of sediment size is as shown in Figure 2.5. The value of dse/b increases and then
decreases with increasing values of D50/b. Sheppard (1997) assumed that one possible
explanation for why the laboratory data correlate so well with the parameter D50/b is that
it is actually the ratio of two different Reynolds numbers, one based on the sediment grain
diameter (and the associated near bed shear velocity) and one on the structure diameter
and the depth average velocity. Both Reynolds numbers are important in characterizing
the flow and sediment transport in the vicinity of the structure.
3-
2.5 +
+ +
+t
S(E + ttema (
2 + '
0 +A
0.5 -
0 + Ettema (1980)
0 UF/USGS
0-
-4 -3 -2 -1
log(Ds0/b)
Figure 2.5 Dependence of equilibrium scour depth on ratio of
sediment diameter to structure diameter for 1 > U/Uc > 0.9 and yo/b > 2.5
2.3.4 Effect of Sediment Gradation a
For a given structure and flow, the equilibrium scour depth is very dependent on the
sediment gradation. Experiments carried out by Nicollet and Ramette (1971) and a more
extensive study by Ettema (1976) showed that the equilibrium scour depth decreases as
the standard deviation of the particle size distribution increases for clearwater scour
conditions. For live-bed tests conducted by Baker (1986) and plotted by Melville and
Sutherland (1988), there was a reduction as well but not as much as for clearwater and for
values of U/Uc > 4, the effect was almost independent of the gradation of the sediment
(Figure 2.6). It is believed that the main effect of a is in the formation of an armor layer
around the upstream perimeter of the pier reducing the scour hole depth.
2.0
dse/h b
0 1.O
U/Uc
Figure 2.6 Influence of a on scour depth, taken from Melville and Sutherland (1988)
20
Ettema (1980) replotted his previous data as K, versus a, where KI is the coefficient
in the equation
= K dse (2.9)
b b
where a- = 8
D16
de ( is the equilibrium clearwater scour depth for a sediment with a given a,
b
dse is the equilibrium scour depth for uniform sediment (a < 1.6).
b
The graph is reproduced in Figure 2.7. The data is grouped by sediment type (ripple-
forming, D50 < 0.6 mm or non ripple-forming, D50 > 0.6 mm). KI varies from 1.0 for
uniform sediments to less than 0.25 for sediments with a large gradation.
3
0-g
Figure 2.7 Graphic relationship between o and IK, taken from Chiew (1984)
2.3.5 Effect of Pier Properties (Shape and Alignment)
The shape of the pier and its orientation to the flow can have a significant effect on
the equilibrium scour depth. The shape and orientation effect can be accounted for with
coefficients multiplied times the equation for a circular cross-section pier.
db
dse KK2( dse (2.10)
b b circular pier
Values for K1 for common geometric pier cross-sections are given in Tables 2.1 and
2.2. The effect of flow skew angle (pier orientation) can be seen in Table 2.3 and Figure
2.8, taken from HEC-18 (1995) and Laursen (1958) respectively.
7 I 1 I II 1 I I i I a s
5 r10
0 15 30 45 60 75 90
ANGLE OF ATTACK 0 (Degrees)
Figure 2.8 Alignment factor K2 for rectangular piers, taken from Laursen (1956)
Table 2.1 Other factors for pier shapes
Laursen Chabert
And And
Tison Toch Engeldinger Neill Venkatadri
Shape in plan L/a (1940) (1956) (1956) (1973) (1965)
Lenticular
Parabolic nose
Triangular nose, 600
Triangular nose, 900
Elliptic
Ogival
Joukowski
Rectangular
Circular
0.67
0.41
0.86
0.76
1.40
1.00
0.56
0.75
1.25
Table 2.2 Shape factor for pier nose, taken from HEC-18 (1995)
Shape of pier nose KI
Square Nose 1.1
Round Nose 1.0
Circular Cylinder 1.0
Group of cylinders 1.0
Sharp Nose 0.9
1.00
0.97
0.76
0.91
0.83
1.11
1.11
0.73
0.92
0.86
1.11
1.00
1.00
23
Table 2.3 Correction factor K2 for angle of attack 0 of flow,
where L is the length of the pier and b the width, taken from HEC-18 (1995)
Angle L/b = 4 L/b = 8 L/b = 12
0 1.0 1.0 1.0
15 1.5 2.0 2.5
30 2.0 2.75 3.5
45 2.3 3.3 4.3
90 2.5 3.9 5.0
CHAPTER 3
EXPERIMENTAL APPROACH
This chapter includes a detailed description of the experiments performed as part of
this work, as well as a description of the equipment and instrumentation used.
3.1 Facilities and Instrumentation
The equipment used in the experiments is divided in four categories. The first is the
facilities, which includes the flume and the equipment used to place and remove the
sediment. The second is the instrumentation used to measure the water properties, flow
conditions and scour depth. The third category is a description of model piers and the last
category is a description of the sediment used in the experiments.
3.1.1 Facilities
All experiments were conducted in a flume located at the U.S. Geological Survey
Biological Research Division, S.O. Conte Anadromous Fish Research Laboratory
(referred to here as USGS-BRD Laboratory) in Turners' Falls, Massachusetts. The
primary purpose of this laboratory is to study the behavior and biology of anadromous
fish and to conduct research on fish passages. This is the first time the flume has been
used for sediment scour research. An aerial view of the laboratory is shown on Figure 3.1.
The flume area of the laboratory has three parallel open channels. The main channel,
located in the middle, has a width of 6.1 m (20 ft). The two side channels have widths of
3.05 m (10 ft). All three channels have a length of 38.6 m (126.5 ft) and a depth of 6.4 m
(21 ft). A not-to-scale, schematic drawing of the flume area in the Engineering Building is
shown in Figure 3.2. Only the 6.1 m wide main channel was used for the work reported
here.
Figure 3.1 Aerial photograph of the S.O. Conte Laboratory
The laboratory is located between a hydropower stationcanal and the Connecticut
River. The flow in the flume is generated by the head difference between the canal and
the Connecticut River. There is an intake pipe connecting the flume and the canal. The
flow passes through grates to filter the water entering the flume. The flow is controlled by
four sluice gates with dimensions of 1.22 m x 1.22 m (4 ft x 4 ft). Two of the gates are
located at the north wall and one on either side at the north end. The gates are controlled
with electric motors that raise or lower them individually. Discharge as large as 350 cfs
Flow Intake from Reservoir
126 I
NOT TO SCALE
All dimensions in feet
Flow Discharge
To Connecticut
River
Clearwater Scour Test Setup
NOT TO SCALE
All dimensions in feet
TestSediment 6
Section A-A
1- 126 1
I I 1
Filter Material
Base Sediment
Test Sediment
Base Sediment
Section B-B
Figure 3.2 Schematic figure of the setup for the experiments
i 4
can be achieved with the two main sluice gates with an additional 50 cfs from the other
two gates (depending on the canal and river elevations).
For the purpose of the work reported in this thesis, a weir was placed at the
downstream end of the flume to control the water level and volumetric discharge. Model
tests were performed to determine how far upstream of the weir, the velocity profiles
were affected (see Appendix A). It was determined that the weir has minimal effect on the
velocity profiles in the test section.
The discharge, Q, over a rectangular weir occupying the entire width of the flow B
can be computed using the equation
Q= Cwr 2 BH3, (3.1)
3
where Cwr is the rectangular weir coefficient. From dimensional analysis arguments, it is
expected that Cw is a function of Reynolds number (viscous effects), Weber number
(surface tension effects) and the ratio of water head over the weir to the weir height,
H/Pw. In most practical situations, the Reynolds and Weber numbers effects are
negligible, and the following expression can be used (Rouse 1946, Blevins 1984)
Cw, = 0.611+0.075-. (3.2)
Pw
More precise values of C,, can be found in the literature (Henderson, 1966).
At the upstream entrance of the flume, a 5.5 m (18 ft) high flow straightener was
installed to maintain uniformity of the flow over the width of the flume. The flow
straightener consists of vertical wood slats with a 25% opening. The setup was successful
in that it produced near uniform flow across the flume for the range of water depths and
velocities used in the experiments (see Appendix B for details).
In order to reduce the volume of the relatively expensive, uniform diameter sand,
gravel with a D50 of approximately 0.48 cm (3/8 in) was used as a filler away from the
test area (Figure 3.2). A filter cloth with a mean diameter opening of 0.1 mm was placed
over the drains in the floor of the flume and between the sand and the gravel. An
additional advantage of the gravel was the reduction of the drain time for the flume. A
total of 360 m3 of gravel and 205 m3 of test sediment were used. In order to prevent
sediment transport near the entrance of the flume, where the water was jetting from the
openings in the flow straightener, gravel was placed on the bed for the first 8.5 m (28 ft).
This hastened the development of a fully developed velocity profile and prevented the
formation of sand dunes that would have occurred due to the increased velocities near the
flow straightener.
3.1.2 Instrumentation
The instrumentation for the data collection is composed of the instruments, for the
measurement of the water temperature and elevation, flow velocity and scour depth. The
instruments are described below.
3.1.2.1 Velocity measurement
Two commercially available electromagnetic current meters were used to measure
the velocity during the tests [Marsh-McBimey Models 523 (0.5 in sensor) and 511 (1.5 in
sensor)]. The water velocity was measured at the same two horizontal locations upstream
of the test structure for all the experiments. The meters were located a distance of 1.52 m
(5 ft) from the sides of the flume and approximately 5 meters upstream from the center of
the test structures. The vertical position of the velocity sensors were such that they were
at the point of depth averaged velocity for a fully developed velocity profile, which is
approximately yo3 from the bed. The time over which the velocity was averaged was
increased until the measurement was steady. This value was found to be one minute.
Velocities at the same elevation of the sensors were also measured using an impeller type
current meter (Ott-meter). This instrument was also used during the experiments to check
the electromagnetic meters. The duration of the measurement at each location was one
minute. The accuracy of the electromagnetic and impeller meter measurements was
estimated to be 1 cm/s and 0.5 cm/s respectively.
3.1.2.2 Water level measurement
A water pressure sensor was used to measure the water level during the tests. The
water level was measured at the same location for all the experiments downstream of the
test structure and approximately seven meters upstream of the weir. The time over which
the water level was averaged was one minute. The accuracy of the water level
measurement was estimated to be 0.5 cm.
3.1.2.3 Temperature measurement
A temperature sensor was used to measure the water temperature during the tests.
The temperature was measured at the same location for all the experiments, which was
close to the test structures. The meter was located a distance of approximately three
meters downstream from the test area and close to the wall of the flume. The time over
which the temperature was averaged was one minute. The accuracy of the temperature
measurement was estimated to be 0.050C.
3.1.2.4 Acoustic transducers
Two different transducer arrays were used for the temporal measurement of the
scour, one for the smaller structures and another one for the large structure. Both arrays
consisted of three elements, each of which contained four crystals. The transducers are
called Multiple Transducer Arrays or simply MTAs. They were positioned at the front of
the structure and at angles of 830 from the front. Their height from the sandy bottom
varied according to the water depth but they were always underwater and as close as
possible to the surface so as not to interfere with the scour process. For most of the
experiments, the transducers were located 10 cm (4 in) from the water surface. The
MTAs were custom built for this application by SeatekTM. For a more detailed description
of the system, see Jette and Hanes (1997).
The arrays for the small pile diameters consisted of four 2.25 MHz transducers with
4 cm separation between the elements. The transducers were 2.5 cm in diameter. The
footprint at a range of 0.9 m (3 ft) was 5 cm (which means a 1.5 degrees spread angle of
the acoustic beam). The arrays for the large pile diameters consisted of four 2.25 MHz
transducers with 8 cm separation between elements. The transducers were 4.0 cm in
diameter. The footprint at a range of 2.7 m (9 ft) was 8.7 cm. The arrays were made of
anodized aluminum.
The MTAs were mounted on each structure with an aluminum ring. The rings were
fastened at a certain height and each of the three arrays was positioned on the ring at
predetermined positions. Figure 3.3 shows the mounting of the transducers and cameras
and Figures 3.4 and 3.5 show the details of the transducers.
-I-
Camera
Traverse Mechanism--
Video Cameras
Test Sand
Acoustic Transdui
- Test Pile
I I
Figure 3.3 A test pile with the instrumentation
MTA for small pile diameters (0.5 to 1 ft. diameter)
side view (coss-section)
mounting ring
2.25 MHz transducers
front view (cross-section)
('27
0,375 l
(0,95 m)
j lSEATEK
u---eed i64In(e3 a n ----D- r raw by: Chris Jette' 3-24-97
Figure 3.4 Detailed view of the arrays for the small structures
FLOW
Plan View
1
MTA for large pile diameters (greater than 1 ft.) 1/2 scale
side view (cross-section) front view (cross-section)
mounting nng
0 5 In
top view
i..---0-- n(o.5, [ SEATEK
rawn by: Chris Jette' 3-25-97
Figure 3.5 Detailed view of the arrays for the large structures
3.1.2.5 Video measurements
The video measurement consisted of the video equipment, the mechanisms to
control them and the stepper motor for the movement of the cameras inside the piers.
Although it was used as a backup measurement, it proved to be very reliable. Two
cameras were used to monitor the rate of scour by moving vertically inside the piers. The
mechanism for support and moving of the cameras was the same for all the piers but the
carriage for the cameras changed according to the diameter of the pier (Figures 3.6 3.8).
The controller for the traverse mechanism was designed to allow traverse speeds from
10m/h to 1 mm/h. The mechanical part consisted of a threaded rod, which supported the
cameras, and was connected to a stepper motor, the speed of which could be set by the
controller. The rod had the appropriate length so the cameras could follow the sand-water
interface during the scour process.
The output from the video cameras was sent to the VCR. A second controller was
programmed to turn on the lights and record one minute of video at specified intervals
throughout the experiments. After the end of the recording time, the video and lights were
turned off and the system put in a stand-by mode until the next recording time. The
controller also switched between cameras during the recording session.
Figure 3.6 Picture of the cameras for the 0.114 m (4.5 in) pile
Figure 3.7 Picture of the cameras for the 0.305 m (12 in) pile
Figure 3.8 Picture of the cameras for the 0.92 m (36 in) pile
3.1.2.6 Measurement setup
Two personal computers with 486 processors were used for data acquisition. One
was used for velocity, water elevation and temperature and one for the acoustic transducer
measurements of the scour depth. The first computer was programmed to take one-minute
samples of velocity, water elevation and temperature every 30 minutes. The data were
written to a file on the hard drive. The second personal computer was connected to the
acoustic transducers through a control box (SeaTek Control Box). The purpose of this
box was to gather the signals from all 12 crystals and convert them to distances from the
transducer to the bed. The communication between the personal computer and the
acoustic control box was done with the software, CrosstalkTM, a serial/parallel/modem
communication package. The data was viewed on a computer screen and stored in files.
Data were sampled for ten seconds every ten minutes. A diagram of the measurement
system is shown in Figure 3.9.
PC Mechanical Monitor
#1 #2 Traverse
SSystem -
SeaTek VCR
Control Box
-Inside Camera/VCR
Cameras Control Box
Acoustic TieD
Water Digital Transducers Tme/D
Figure 3.9 Diagram of the measurement system
3.1.2.7 Point gauging
After every experiment, the scour hole was surveyed with a point gauge system. The
system was composed of a square array of steel beams that spanned the width of the
flume with a side length of 6.1 m (20 ft). The point gauge system was located on an
aluminum carriage that moved along tracks on the steel beams. The point gauge was
connected to a string potentiometer and voltage source so that the vertical position was
indicated by an electrical potential in mV. The horizontal and vertical accuracies of the
measurements were estimated to be 0.5 cm and 0.5 mm respectively.
3.1.3 Models
The models used in these experiments were piles with cylindrical cross-sections. The
pile diameters were 0.114 m (4.5 in), 0.305 m (12 in) and 0.92 m (36 in) with lengths that
exceeded the water depth. They were attached to the floor of the flume and given lateral
support near the top by a bridge that spanned the width of the flume above the water.
The 0.92 m (3 ft) diameter pile was 5.5 m (18 ft) high. It had two Plexiglas windows
fitted for scour visualization at angles of 450 from the front of the pile (Fig. 3.10). To
prevent the pile from distorting in shape, steel channels were attached to the walls inside
of the pier. Measuring tapes were glued to the inside faces of the piles at locations where
they could be seen by the inside video cameras. The 4.5 in and 12 in piles were
constructed of Plexiglas. Both were 3.35 m (11 ft) in length.
0.92 m (36 in)
diameter pipe
Aluminum
carrier
Waterproof case
with cameras
Figure 3.10 Cross-section of the 0.92m (36 in) pier
The rationale behind the pile diameter used in the experiments is as follows. The
0.92 m diameter was the largest standard diameter that could be used in the 6.1 m wide
flume without creating significant contraction scour. Even this diameter exceeded the
"rule of thumb" limit of 10% of the flume width. The second factor used in sizing the
piles was the need to maintain the same Dso/b ratio using different values of D50 and b. At
the time that the piles were being designed, the uniform diameter sand sizes that were
available were 0.20 mm and 0.65 mm. This would have produced Dso/b ratios as shown
in Table 3.1.
Table 3.1 Table with values of (-log (Dso/b)) before sand availability
Dso(mm)
b (m) 0.20 0.65
0.920 3.66 3.15
0.305 3.18 2.67
0.114 2.76 2.24
By the time the sand was purchased, the available uniform sand sizes changed to
0.22 mm and 0.80 mm. This resulted in Dso/b ratios as shown in Table 3.2. Even though
these ratios were not as close as planned, they were sufficient to test the dependence of
equilibrium local scour depth on the parameter Dso/b.
Table 3.2 Table with values of (-log (Dso0b)) for the piles and sediment
used in the tests
Dso (mm)
b (m) 0.22 0.80
0.920 3.62 3.06
0.305 3.14 2.58
0.114 2.71 2.15
3.1.4 Sediment
Two sand sizes, 0.22 mm and 0.8 mm, were used in these experiments. Experiments
with all three piles were performed with each of the two sediments. Near uniform
sediment diameters were used, since (under clearwater conditions) the greatest scour
depths occur in uniform diameter sediments. The sand was purchased from a vendor in
Rhode Island that had a system for producing near uniform diameter sand.
The grain size distributions for the two sand sizes are shown in Figures 3.11 and
3.12. Their properties are summarized as follows:
Sand No. 1
Ds0 = 0.22 mm
-= = 1.51
1A6
Mineral content = Quartz
Mass density = 2650 kg/m3
Sand No. 2
D5o = 0.80 mm
S 8= _= 1.29
6 D
Mineral content = Quartz
Mass density = 2650 kg/m3
100 -
80-
60-
40-
0.01
D4 = 0.32 mm
D50 = 0.22nim
20-[ D16=0.14nunm
S I I I 1 1I I
0.1
diameter (mm)
1
Figure 3.11 Gradation Curve for Sand No. 1 (Dso = 0.22 mm)
40
100-
D4= 1.07 mm
80-
60-
| D5o= 0.80 mm
40-
20 D6=0.64mm
0-1
0.1 1 10
diameter (mm)
Figure 3.12 Gradation Curve for Sand No. 2 (D50 = 0.80 mm)
CHAPTER 4
EXPERIMENTAL DATA REDUCTION AND ANALYSIS
This chapter contains the results from the experiments performed at the USGS-BRD
Laboratory in Turners' Falls, Massachusetts, as part of the work for this thesis. The
techniques and procedures used in performing these experiments and in reducing and
analyzing the data are also included.
4.1 Experimental Procedure
The sediment, flow and structure parameters used in the experiments are
summarized at Table 4.1 below.
Table 4.1 Parameters for the experiments conducted
Experiment No D50 (mm) b (m) yo (m) U (m/s) Uc (m/s) U/Uc
1 0.22 0.114 1.22 0.300 0.333 0.90
2 0.22 0.305 1.22 0.300 0.333 0.90
3 0.22 0.92 2.29 0.320 0.355 0.90
4 0.80 0.92 2.29 0.447 0.497 0.90
5 0.80 0.92 0.90 0.403 0.448 0.90
6 0.80 0.305 1.22 0.414 0.460 0.90
7 0.80 0.114 1.22 0.414 0.460 0.90
To assume consistent results, a series of procedural steps were developed for the
data collection. The procedures are divided into a) the pre-test, b) during test, and c) post-
test steps.
Before scour tests could be performed in the USGS-BRD flume, the bed had to be
prepared. First the gravel was put in place. Dividers in the flume made this task easier.
The next step was to place filter material on top of the gravel to separate it from the test
sediment. The following step was to install the structure. Next the test sediment was
placed on top of the gravel and in the test section. The sediment was compacted every 20
to 30 cm with a diesel driven mechanical compactor and hand tampers in the area near the
structure. The bed was then leveled. An observation platform that spanned the width of
the flume at the test section was mounted in the flume. The platform could be moved
vertically to accommodate the range of water depths used in the experiments. The next
step was to install and test the data collection equipment. The flume was then filled with
water up to the level of the weir. Care was taken so as not to disturb the bed or initiate
scour at the test structure. The water was then allowed to stand at this level, until the air
trapped in the sediment was released. This ranged from 4 to 10 hours.
The experiment was started by opening the gates until the desired water level and
flow velocity were reached. The water level and velocity were checked throughout the
experiment and minor adjustments were made when necessary. The speed of the video
camera traversing mechanism was also adjusted during the experiment to account for the
changing rate of scour.
When no scour depth changes were observed for approximately 24 hours, the
experiment was terminated and the flume drained. The procedure took two to three hours.
Pictures of the scour hole were taken from six positions around the pile. The scour hole
was then point gauged and the structure was removed. At the end of the tests with the first
sediment, the test sand was loaded into 0.76 m3 (1.0 yd3) polypropylene bags and
removed from the flume. The second sand was then placed in the flume using the same
procedure as for the first sand.
4.2 Data Reduction
The quantities measured during these experiments were water temperature, water
elevation, flow velocity and scour depth. The scour depth was measured using two
different instruments during the test (acoustic and video) and a third method was used at
the end of each test after the water was drained from the flume (point gauge).
The data for temperature and water elevation were written to a file on the hard drive
of a personal computer (PC) used for data collection. At the end of each experiment, each
of the three data sets were averaged over the time span of the test.
The data from the two velocity meters were also written to the hard drive on the
same PC. The two data sets were averaged individually over the time duration of the tests.
The average from the individual gauges were then averaged to obtain the value associated
with that experiment. An impeller velocity meter (Ott meter) was used to check the
electromagnetic meters.
The video data were stored on one or more videocassettes for each experiment. After
each experiment, the video tapes were viewed and the scour depth versus time was
recorded.
The acoustic transducer data were written to a file on the hard drive on a second PC.
The data collected had to be filtered in order to remove those signals that did not
correspond to scour hole depth. These were caused by acoustic reflection from suspended
sediment and other particles in the flow and zero readings when the return signal was not
detected. The filtering was accomplished with the help of a computer program called
SMS, which allowed the data to be displayed and edited graphically. The acoustic
transducer ran continuously throughout the experiment and ten seconds of data was
sampled and recorded every ten minutes.
After the test was completed and the flume was drained, the entire scour hole was
surveyed with a point gauge. The (x, y) position of the tip was recorded along with the
voltage output from a string potentiometer, which was proportional to the vertical
positions of the gauge. The initial position of the bed was established by the initial tape
reading from the video cameras inside the pile. Then the voltage readings were converted
into distances from the undisturbed bed to the elevation of the scour hole at each
horizontal (x, y) position. The origin of the coordinate system was located at the center of
the pile and the initial, undisturbed bed. The survey extended to the flat portion of the bed
beyond the scour hole.
4.3 Processed Data Results
The processed data are presented in summary tables and graphs. A table in Appendix
C gives the summary of all the experiments conducted along with graphs showing the
scour depth versus time for both the video and acoustic transducers (when both are
available).
Contour plots of the equilibrium scour holes for all seven experiments are presented
on Figures 4.1 to 4.7. Equilibrium scour profiles inline and normal to the flow for all
seven experiments are given in Figures 4.8 to 4.14.
Z (in)
-1
-20 -10 0 10 20 30
X (in)
Figure 4.1 Elevation contour plot of the equilibrium scour hole for Experiment No.1
(b = 0.114 m, D50 = 0.22 mm, yo = 0.186 m and U = 0.290 m/s)
z (in) 0O o
330-
3 0 .. .a.
-3
-2
-6
-10
-1 0
-30 -20 -10 0 10 20 30 40 50 60 70
X (in)
Figure 4.2 Elevation contour plot of the equilibrium scour hole for Experiment No.2
(b = 0.305 m, D50 = 0.22 mm, yo = 0.190 m and U = 0.305 m/s)
Z (in)
5
3
1
0
-1
-3
-5
-7
-9
-11
-13
-14
-15
8N' , ~- -I
:I,4
S)0
x (in)
Figure 4.3 Elevation contour plot of the equilibrium scour hole for Experiment No.3
(b = 0.920 m, Dso = 0.22 mm, Yo = 2.268 m and U = 0.325 m/s)
60L
-18 2
-22
-26
-26 -20 40 40
-30
-34
-37 8
X (in)
Figure 4.4 Elevation contour plot of the equilibrium scour hole for Experiment No.4
(b = 0.920 m, D50 = 0.80 mm, Yo = 2.402 m and U = 0.454 m/s)
Z (in)
6
2
-2
--6
X(in)
Figure 4.5 Elevation contour plot of the equilibrium scour hole for Experiment No.5
(b = 0.920 m, D50 = 0.80 mm, yo = 0.866 m and U = 0.335 m/s)
z (in)
Q6
A
X(in)
Figure 4.6 Elevation contour plot of the equilibrium scour hole for Experiment No.6
(b = 0.305 m, D50 = 0.80 mm, yo = 1.305 m and U = 0.381 m/s)
48
Z(in) 3
2
0
-1 I0
-2 z .
-5 -2oL
-6
-30-
-7
1-8
X (in)
Figure 4.7 Elevation contour plot of the equilibrium scour hole for Experiment No.7
(b = 0.114 m, Dso = 0.80 mm, Yo = 1.280 m and U = 0.388 m/s)
10-
8-
6-
4-
-4 4 I _
I I
-30 -20
' I
-10
a) Inline profile
0 -
-30 -20 -10 0
Y (in)
10 20 30
b) Normal profile
Figure 4.8 Equilibrium profiles of scour hole for Experiment No. 1
(b = 0.114 m, Dso = 0.22 mm, yo = 0.186 m and U = 0.290 m/s)
a) Inline profile, and b) Normal profile
Flow
--------------
0-
-2 -
-4 -
10
X (in)
30
30
40
40
FloIv
0
I
Flow
-40 -30 -20 -10 0 10 20 30 40 50 60 70
X (in)
a) Inline profile
Flo\~
0
0 -4- -
-60 -40 -20 0
Y (in)
20 40 60
b) Normal profile
Figure 4.9 Equilibrium profiles of scour hole for Experiment No.2
(b = 0.305 m, D50 = 0.22 mm, yo = 0.190 m and U = 0.305 m/s)
a) Inline profile, and b) Normal profile
-70 -60 -50 -40 -30 -20 -10 0 10 20 30 40 50 60
X (in)
a) Inline profile
-80 -60 -40 -20 0
Y (in)
20 40 60 80
b) Normal profile
Figure 4.10 Equilibrium profiles of scour hole for Experiment No.3
(b = 0.920 m, D50 = 0.22 mm, yo = 2.268 m and U = 0.325 m/s)
a) Inline profile, and b) Normal profile
10-
0-
-10-
-20 -
-30 -
-40
a) Inline profile
-80 -60 -40 -20 0
Y (in)
20 40 60 80
b) Normal profile
Figure 4.11 Equilibrium profiles of scour hole for Experiment No.4
(b = 0.920 m, D5o = 0.80 mm, Yo = 2.402 m and U = 0.454 m/s)
a) Inline profile, and b) Normal profile
Flo\w
0
X (in)
- I
-80 -60
SI
-40
20
20
40
60
80
80
'
I *
\
\,
- - - - -
",z
' I
-80 -60 -40 -20 0 20 40 60 80
X (in)
a) Inline profile
-80 -60 -40 -20 0
Y (in)
20 40 60 80
b) Normal profile
Figure 4.12 Equilibrium profiles of scour hole for Experiment No.5
(b = 0.920 m, D50 = 0.80 mm, yo = 0.866 m and U = 0.335 m/s)
a) Inline profile, and b) Normal profile
-30 -20 -10 0 10 20 30 40
X(in)
50 60
a) Inline profile
-50 -40 -30 -20 -10 0
Y(in)
10 20 30 40 50
b) Normal profile
Figure 4.13 Equilibrium profiles of scour hole for Experiment No.6
(b = 0.305 m, D50 = 0.80 mm, yo = 1.305 m and U = 0.381 m/s)
a) Inline profile, and b) Normal profile
-20 0 20 40
X (in)
a) Inline profile
Flo\%
S
-50 -40 -30 -20 -10
0
Y (in)
10 20 30 40 50
b) Normal profile
Figure 4.14 Equilibrium profiles of scour hole for Experiment No.7
(b = 0.114 m, D50 = 0.80 mm, yo = 1.280 m and U = 0.388 m/s)
a) Inline profile, and b) Normal profile
- - - - -
4.4 Discussion of Results
The most unique aspects of the local scour experiments conducted during the work
of this thesis have to do with the size of the structure tested and the duration of the tests.
The 0.92 m (36 in) diameter pile is one of the largest, tested under controlled steady flow
conditions. Any questions regarding the equilibrium depths were eliminated by
continuing the tests until no measurable change in the scour hole was observed.
Several interesting observations were made regarding the scour hole at the large
diameter piles. The location of the deepest point in the hole was different from that for
the smaller piles. For the 0.114 m (4.5 in) and 0.305 m (12 in) diameter piles, the
equilibrium scour hole was more uniform in depth from the side to the front (upstream
edge) with the deepest point being directly in front of the pile. The deepest point in the
scour hole at the 0.92 m pile was between 450 and 600 from the front. There are several
possible explanations for this. One might be the fact that the slope of the pressure
distribution along the circumference of the pile is smaller for large diameter piles than for
small diameter piles. Another possible reason is that the effect of the horseshoe vortex
seems to be diminished for the large piles. The scour holes from the accelerated flow do
not extend to the front of the large structure, thus the horseshoe vortex is deprived of the
energy, caused by flow separation at the upstream edge of the scour hole.
Note that there was a slight asymmetry of the scour hole (see for example Figure
4.11). This is believed to be due to the slightly higher velocity on the west side of the
flume. Flow profiles for the 1.22 m (4 ft) and 2.44 m (8 ft) water depths that show this
asymmetry are given in Appendix B.
Ripples in the test section for the first two experiments can be also observed (Figures
4.1 and 4.2). The reasons for their formation are various. The sand, used in these
experiments, was very fine (0.22 mm), and ripples are common for sediments with D50 -
0.6 mm. Another reason is that those experiments were conducted at conditions very
close to live-bed conditions, so there may have been brief periods of time, when the flow
exceeded the critical value, Uc.
The other reason is the presence of a big sand dune, which did not affect the
formation of the scour holes, but helped initiate the ripples. This sand dune was formed
initially near the flow straightener due to velocities greater than Uc. The flow straightener
had an opening of 25% of the total cross section, so the velocities were up to four times
greater than the velocity downstream. Those conditions formed a sand dune that could
travel downstream but its speed was very small and it did not affect any of the results.
This problem was later corrected by substituting gravel for sand just downstream of the
flow straightener.
CHAPTER 5
COMPARISON OF LOCAL SCOUR PREDICTION EQUATIONS
5.1 Scour Prediction Equations
Over the past 40 years, numerous studies have been conducted and many equations
have been developed to predict local equilibrium scour depth. Most of these equations
were based on laboratory data. In some cases, limited field data was also used. Due to the
complexity of the processes involved in local scour and the large number of parameters
needed to describe these processes, the predictive equations differ dramatically. In some
cases, the data on which these empirical equations are based were not published. Fourteen
of the more commonly referred to equations are evaluated and compared in this chapter,
using two data sets, one for clearwater and one for live-bed scour conditions. The
clearwater data set includes the data obtained as part of the work for this thesis.
Perhaps the most commonly used scour prediction equation in the United States is
the so-called Colorado State University (CSU) equation. It is the recommended equation
in the U.S. Federal Highway Administration (FHWA) Hydraulic Engineering Circular
No. 18 (HEC-18) (1995). This equation is
( b 0.65
dse =2.0yK, K2 .Fr0.43, (5.1)
where
dse is the equilibrium scour depth,
Yo is the flow depth upstream of the structure,
K1 is a correction factor for pier nose shape,
K2 is a correction factor for angle of attack flow,
b is the pier width and
U
Fr = Froude number -
4g-o
Values from K1 and K2 can be obtained from HEC-18 and are discussed in Chapter 2.
This equation was developed by fitting laboratory data and is recommended for both live-
bed and clearwater conditions. In HEC-18, limiting values for the scour depth normalized
by the pier diameter, dse/b, are recommended as follows: dse/b = 2.4 for Fr < 0.8 and 3.0
for Fr > 0.8.
Melville (1997) developed a scour equation based on various laboratory experiments
of the form:
dse =I KdKyDKaKs, (5.2)
where
->1
1 u,
K, = flow intensity factor = for
U U
-<1
U, U,
b
-->25
1.0 D5
Kd = sediment-size factor = for
0.57 log 2.24 -- < 25
I D50 D50
b
< 0.7
2.4b Yo
KyD = flow depth-pier width factor = 2 y b for 0.7 < <5
yK
YO
4.5yo b
>5
Yo
K = pier-alignment factor, and
K, = pier-shape factor.
Values for K, and Ks can be obtained from tables given in Melville and Sutherland
(1988).
Hancu (1971) proposed the following scour prediction equation
dse = 2.42b 2- (5.3)
I Uc gb
U2
for 0.05 < _< 0.6 where Ue is calculated by the equation
gb
0.2
Uc = 1.2 (s-1)gD5o Yo .
D50
Equation (5.3) does not apply for values of less than 0.5.
UC
Laursen and Toch (1956) developed design scour depth curves that were later
described by Neill (1964) in equation form as
dse =1.35b07y03. (5.4)
Shen et al. (1966) used laboratory data and limited field data to develop the
following clearwater scour prediction equation,
dse= 0.000223 ReO619, (5.5)
Ub
where Rep = -. For live-bed conditions, Equation (5.5) was found to be too
v
conservative, so Shen (1971) recommended using the Larras (1963) equation,
dse =1.05b075. (5.6)
Breusers et al. (1977) developed the following equation (which is similar to
Equation (5.3) (Hancu, 1971))
dse = b f KK2 tanh ), (5.7)
where
U,
f =0 for -<0.5,
Uc
U U
f=2 -1 for 0.5<- <1.0,
U, Uc
U
Uc
and KI and K2 are the same as in Equation (5.1).
Jain and Fischer (1979) developed a set of equations based on their laboratory
experiments. For Fr Frc > 0.2
dse =2b(Fr Fr ).25 o (5.8)
(b
where Frc = critical Froude number = c
-gyo
For Fr-Frc <0
ds = 1.85bFr 025' (5.9)
For 0 < Fr Frc < 0.2, the larger of the two scour depths computed from Equations (5.8)
and (5.9) are to be used.
Garde et al. (1993) developed a clearwater scour equation based on various
laboratory experiments
,7 0.75(, 0.16 2 -0.4
ds =0.66 o u ,- (5.10)
Do Ds0) Ds0) (s-1)gDso
where Vc is the velocity for the initialization of sediment movement at the structure,
which is about 0.4-0.5 Uc, and s is the relative sediment density. The equation given to
calculate Vc is
V2 1, b -0. 11( Yo 0.16
(s-1)gD50 D50 D50)
Another scour prediction equation was developed by Chitale (1962), using very
limited laboratory data,
d = -0.51+ 6.65Fr 5.49Fr2. (5.11)
Yo
Based on data from previous investigations for local scour at spur dikes, Ahmad
(1953) concluded that scour does not depend on grain size for the range of his data (0.1 to
0.7 mm). He stated that this might not be accurate for the entire range of the sediment
sizes. Ahmad (1962) reanalyzed the work of Laursen (1962) with a special emphasis on
scour in sand beds in West Pakistan and developed the following equation:
dse = Kq2/3 Y, (5.12)
where K is assumed from model studies conducted by Ahmad (1962) to vary from 1.7 to
2.0 for piers and abutments. A value of 1.85 was used in the calculations made in this
thesis. Also q is the discharge per unit width of the channel and all units are in English.
Inglis (1949) performed experiments on model bridge piers and developed an
equation from his data. Blench (1962) reduced Inglis' (1949) formula to
- ,0.25
dse =1.80.25q 0.5 o -Yo, (5.13)
where all units are in English.
Gao et al. (1992) presented empirical equations for clearwater and live bed local
scour that were used by highway and railway engineers in China for more than 20 years.
The equations for clearwater and live-bed conditions are
dse = 0.78Kb0.6 015D07 U U (5.14)
U U
and dse = 0.65K b06 yo15D.07 U U (5.15)
respectively. Ks is a coefficient for pier shape and has the values of 1.0 for cylinders, 0.8
for round-nosed piers and 0.66 for sharp-nosed piers. The critical depth average velocity,
Uc, the velocity for initialization of scour at the pier, U' and the exponent c in Equation
(5.15) are calculated using
Uc= 0.14 [17.6(s-)D +6.05E 7 10 0.5
(D o0.0o53
', = 0.645-50 U ,,and
( b )
C= ( )9.35+2.23logD50
C= U\
Froehlich (1988) compiled field measurements of local scour at bridge piers from
reports of several investigations and developed the equation
dse = 0.320b Fr0.2 0.6 (5.16)
x.46 b o.08
where ) is a pier shape factor and has the value of 1.3 for square-nosed piers, 1.0 for
round-nosed piers, and 0.7 for sharp-nosed piers.
Sheppard et al. (1995) at the University of Florida developed a clearwater scour
prediction equation for cylindrical piers based on laboratory data,
b jb U, b
(5.17)
=4.81tanh [ 1-2.87 +1.43L ] 2log D exp -0.18[-log-( 2]2.9
b) t(_) I( b )
Based on his limited live-bed dataand data from other researchers, Sheppard (1997)
concluded that a second peak in the normalized scour depth (dse/b) versus normalized
velocity (U/Uc) plot occurred in the live-bed scour range and had a value of
approximately 2.1 (for yo/b > 2.5). The value of U/Uc, where the live-bed peak occurs, is
believed to coinside with the conditions, where the bed flattens. That condition has been
shown to be dependent on the Froude number and the velocity normalized by the
sediment fall velocity (Snamenskaya, 1969). For design purposes Sheppard (1997)
recommended connecting the clearwater peak to the live-bed peak with a straight line as
shown in Figure 5.1. For velocities greater than the value for the live-bed peak, the
equilibrium scour depth is assumed to be the value at the live-bed peak. For values of
yo/b < 2.5, the height of the live-bed peak is computed using the equation
e = 2.ltanh bo
db
independent of Do/b
2.1 ---- ----- -- -- -
depends on Dso/b
0.4- 0.5 1.0 (U/U),bp
U/U
Figure 5.1 Local scour depth dependence on velocity,
as proposed by Sheppard (1997)
5.2 Compilation of Local Scour Data
The clearwater and live-bed data sets used in this analysis were compiled from a
number of sources. These include Ettema (1980), Chiew (1984), Sheppard et al. (1995),
Chabert and Engeldinger (1956), Jones (1997), Melville and Chiew (1999), Graf (1995),
Shen et al. (1966), and the data obtained as part of the work for this thesis.
The data were divided into two categories, clearwater and live bed. This was done
for several reasons. The first reason is that the local scour processes are different for these
two categories. In the clearwater region, there is sediment movement only around the
structure, while in live-bed conditions there is movement over the entire bed. That may
result even at the reduction of the scour hole for velocities just over the critical value, Uc,
and is based on observations by Ettema (1980), Chiew (1984) and others. Another reason
is that many of the scour prediction equations were based on curve fits to just clearwater
data (Garde 1992, Sheppard et al. 1995), while others used both clearwater and live-bed
data.
The criteria used in selecting the data used in this analysis were as follows. The
author had to present sufficient information about the parameters of the experiment, so
that the equations used in this analysis could be evaluated. In addition the duration of the
experiments had to be sufficiently long that equilibrium (or near equilibrium) scour
depths were achieved. The time required to reach equilibrium is not well understood, but
it is known to increase with the size of the structure and (for clearwater scour) the
velocity. For the purpose of this analysis a minimum of 17 hours was chosen. Only scour
data for structures with a circular cross section were used, because the coefficients for
other shapes of structures vary for the different equations. Another criterion was that the
test sediment had to be relatively uniform in grain size. The data chosen had a gradation a
less than 1.6. Using these criteria, 215 clearwater and 244 live-bed data points were
compiled.
The scour depths were computed for the conditions of the test using Equations
(5.1) (5.17). The value for critical depth average velocity, Uc, was calculated using
Shields' diagram, except where stated otherwise, like for Hancu (1971), Melville (1984),
HEC-18 (1995) and Gao et al. (1992). For the data where temperature was not reported, a
value of 150C was assumed. Little or no data on bedforms was available for most of the
data. In the computation of Uc, a relative roughness r (ks/D5o) was assumed to be five. For
Breusers et al. (1977) and Hancu (1971), scour depths were assumed to be zero for U/Uc
< 0.5 and for U/Uc < 0.45 for Sheppard et al. (1995). Also for Hancu (1971), some data
points could not be considered due to limitations on the equation by the author.
5.3 Comparative Analysis
Predictions of the clearwater data will be discussed first. The Jain and Fischer
(1979), Laursen and Toch (1956), Gao et al. (1992) and Melville (1997) equations do a
good job of predicting clearwater scour depths for smaller diameter piles but overpredict
as the diameter increases. The Chitale (1962) and Ahmad (1953) equations, which depend
on a limited number of parameters, overpredict most of the data, as expected. The Hancu
(1971) equation underpredicts (as much as 95%) for the majority of the data points where
the equation can be applied. The Breusers et al. (1977), Froehlich (1988), Garde et al.
(1993), Inglis-Blench (1962) and Shen (1966) equations underpredict most of the data.
The best predictions were by the HEC-18 (1995) and Sheppard et al. (1995) equations
with an average overprediction of 31% and 16% respectively.
When the same equations (with the exception of Garde et al. (1992)) are used to
predict the 244 live-bed scour depths, some differences are observed. The Jain and
Fischer (1979), Gao et al. (1992) and Melville (1997) equations still overpredict as the
pier diameter increases. The Laursen and Toch (1956) equation gives better predictions
(53% as opposed to 104% for clearwater scour). The Chitale (1962) equation still
overpredicts (up to 690%) and the Ahmad (1953) equation underpredicts most of the
live-bed data. The Hancu (1971) equation, which cannot be applied to all the data, still
underpredicts by as much as 92%. The Froehlich (1988) and Inglis-Blench (1962)
equations underpredict for the live-bed data, as they did for clearwater conditions. The
Breusers et al. (1977) and Shen (1966) equations overpredict for most of the data. Again
the best predictive equations are the HEC-18 (1995) and Sheppard et al. (1995) equations
with mean overpredictions of 26% and 12% respectively. Both equations appear to be
more accurate for live-bed conditions.
The mean of the absolute values of the predictions and the range of the predictions
for all of the equations are shown in line plots of the ratio of measured to calculated scour
depths are given in Figures 5.2 and 5.3 for the clearwater, and live-bed data sets
respectively. The mean of the absolute value of the predictions for every equation is
represented with an asterisk along the range of the prediction line. The line of absolute
agreement is the dotted line passing from 1.0. The narrower the range and the closer the
mean of the absolute value is to the line of absolute agreement, the better is the equation.
Scatter plots of calculated versus measured scour depths for all the equations are given in
Figures 5.4 5.17.
C
Froelich (1988)-
Gao et al. (1992)-
Inglis-Blench (1962)-
Ahmad (1953)-
Melville (1997)-
Garde et al. (1993)-
Chitale (1962)-
HEC-18 (1995)-
Jain & Fisher (1979)-
Breusers et al. (1977)-
Hancu (1971)-
Laursen & Toch (1956)-
Shen et al. (1966)-
Sheppard et al. (1995)-
comparison of 14 equations
using 215 clearwater data
I
I I I I I I I
-4 -2 0 2 4 6 8
Ratio of calculated to measured scour
- Prediction Range
Mean of Absolute Value of Scour Predictions
- Absolute Agreement Line
Figure 5.2 Comparison of equations for clearwater data
I
10
I L1
w
I w
w
h\
I
iw
~---
I
I,
I
70
Comparison of 13 equations
using 244 live-bed data
Froelich (1988)
Gao et al. (1992)-
Inglis-Blench (1962)-
Ahmad (1953)-
Melville (1997)-
Chitale (1962)-
HEC-18 (1995)-
Jain & Fisher (1979)-
Breusers et al. (1977)-
Hancu (1971)-
Laursen & Toch (1956)-
Shen et al. (1966)-
Sheppard et al. (1995)-
Ke
-~t---
I,
-1~-
1,
~jc
-I. I
-6 -4 -2 0 2 4 6 8
Ratio of calculated to measured scour
Prediction Range
Mean of Absolute Value of Scour Predictions
- - Absolute Agreement Line
Figure 5.3 Comparison of equations for live-bed data
I
10
-
(A) Garde et al. (1993)
Ettema (1980)
Chiew (1984)
UF/USGS
Chabert & Engeldinger (1
Jones (1997)
Melville & Chiew (1999)
0 0.3 0.6 0.9
measured scour (m)
1.2 1.5
(B) Ahmad (1953)
++
++
++
++
Ettema (1980)
Chiew (1984)
UF/USGS
Chabert & Engeldinger (1956)
Jones (1997)
Melville & Chiew (1999)
0 0.3 0.6 0.9 1.2 1.5 1.8 2.1 2.4
measured scour (m)
Figure 5.4 Comparison of measured and calculated scour for clearwater data for
(A) Garde et al. (1993), and (B) Ahmad (1953) equations
1.5-
1.2-
- I
0 0.3
' I I
0.6 0.9
measured scour (m)
(B) Chitale (1962)
++
+ +
Ettema (1980)
Chiew (1984)
UF/USGS
Chabert & Engeldinger (1956)
Jones (1997)
Melville & Chiew (1999)
0 0.4 0.8 1.2 1.6 2 2.4
measured scour (m)
Figure 5.5 Comparison of measured and calculated scour for clearwater data for
(A) Breusers et al. (1977), and (B) Chitale (1962) equations
0.9-
0.6-
0.3 -
0-
1.2
I
1.5
(A) Breusers et al. (1977)
S + Ettema(1980)
0 Chiew (1984)
* UF/USGS
A Chabert & Engeldinger (1956)
E Jones (1997)
r Melville & Chiew (1999)
c**
2 + +
2L + +
(A) Froehlich (1988)
0 0.3 0.6 0.9
measured scour (m)
1.2 1.5
(B) Gao et al. (1992)
Ettema (1980)
Chiew (1984)
UF/USGS
Chabert & Engeldinger (1!
Jones (1997)
Melville & Chiew (1999)
0 0.3 0.6 0.9
measured scour (m)
1.2 1.5
Figure 5.6 Comparison of measured and calculated scour for clearwater data for
(A) Froehlich (1988), and (B) Gao et al. (1992) equations
(A) Hancu (1971)
Ettema (1980)
Chiew (1984)
UF/USGS
Chabert & Engeldinger (1956)
Jones (1997)
Melville & Chiew (1999)
0 0.3 0.6 0.9 1.2 1.5
measured scour (m)
(B)HEC-18(1995)
Ettema (1980)
Chiew (1984)
UF/USGS
Chabert & Engeldinger (1956)
Jones (1997)
Melville & Chiew (1999)
0 0.2 0.4 0.6
measured scour (m)
Figure 5.7 Comparison of measured and calculated scour for clearwater data for
(A) Hancu (1971), and (B) HEC-18 (1995) equations
(A) Inglis-Blench (1962)
Ettema (1980)
Chiew (1984)
UF/USGS
Chabert & Engeldinger (1956)
Jones (1997)
Melville & Chiew (1999)
0 0.3 0.6 0.
measured scour (m)
(B) Jain and Fischer (1979)
Ettema (1980)
Chiew (1984)
UF/USGS
Chabert & Engeldinger (1956)
Jones (1997)
Melville & Chiew (1999)
0 0.3 0.6 0.9 1.2 1.5 1.8
measured scour (m)
Figure 5.8 Comparison of measured and calculated scour for clearwater data for
(A) Inglis-Blench (1962), and (B) Jain and Fischer (1979) equations
(A) Laursen and Toch (1956)
2-
1.6 -
* *
I I I I I
+ Ettema (1980)
O Chiew(1984)
* UF/USGS
A Chabert & Engeldinger (1956)
Jones (1997)
r Melville & Chiew (1999)
I I I I I I
I I I I
0 0.4 0.8 1.2
measured scour (m)
(B) Melville (1997)
4 + Ettema (1980)
0 Chiew (1984)
S* UF/USGS
A Chabert & Engeldinger (1956)
ED Jones (1997)
F Melville & Chiew (1999)
0 0.3 0.6 0.9
0 0.3 0.6 0.9
1.2 1.5 1.8 2.1
1.2 1.5 1.8 2.1
measured scour (m)
Figure 5.9 Comparison of measured and calculated scour for clearwater data for
(A) Laursen and Toch (1956), and (B) Melville (1997) equations
*
*
1.2-
0.8-
0.4-
A-
2.1 -
1.8-
1.5-
1.2-
0.9-
0.6-
0.3-
A-
I
\f
t
v
(A) Shen et al. (1966)
+ Ettema (1980)
0 Chiew (1984)
* UF/USGS
A Chabert & Engeldinger (1956)
e Jones (1997)
] Melville & Chiew(1999)
*: *
++ *
a++
+- made ++ *
4gj
I 0.3
0 0.3
0.6 0.9
measured scour (m)
1.2
(B) Sheppard et al. (1995)
Ettema (1980)
Chiew (1984)
UF/USGS
Chabert & Engeldinger (1'
Jones (1997)
Melville & Chiew (1999)
1.5
0 0.2 0.4 0.6 0.8 1
measured scour (m)
Figure 5.10 Comparison of measured and calculated scour for clearwater data for
(A) Shen et al. (1966), and (B) Sheppard et al. (1995) equations
1.5 -
1.2-
0.9-
0.6-
0.3 -
0-
1 --
0.8-
F .........
V
(A) Ahmad (1953)
0 0.4 0.8 1.2
measured scour (m)
(B) Breusers et al. (1977)
A AL
+ +
+ +A,. *
+++ + +
AL
S + Shen et al. (1966)
Chiew (1984)
A Chabert & Engeldinger (1956)
Graf(1995)
/ Sheppard (1995)
'
0.1
0.1
0.2
0.2
0.4
0.4
measured scour (m)
Figure 5.11 Comparison of measured and calculated scour for live-bed data for
(A) Ahmad (1953), and (B) Breusers et al. (1977) equations
0.4-
0.3-
0.2-
0.1 -
0-
' I
(A) Chitale (1962)
0
A A A
A A A
*A A A
0 0.2 0.4 0.6 0.8
measured scour (m)
(B) Froehlich (1988)
+ Shen et al. (1966)
* Chiew(1984)
A Chabert & Engeldinger (1956)
* Graf(1995)
S Sheppard (1995)
9
0 0.2
measured scour (m)
Figure 5.12 Comparison of measured and calculated scour for live-bed data for
(A) Chitale (1962), and (B) Froehlich (1988) equations
80
(A) Gao et al. (1992)
0.8
0.6
E0
:J
0.4
C)
0.2
0
0 0.2 0.4 0.6 0.8
measured scour (m)
(B) Hancu (1971)
+ Shen et al. (1966)
Chiew (1984)
A Chabert & Engeldinger (1956)
Graf(1995)
9 Sheppard (1995)
AA A A AA
A A A
S A A *
uA A A A 4 AA
44 A& A A
AA* A A A
' I
0.1 0.2
measured scour (m)
0.3
0.3
Figure 5.13 Comparison of measured and calculated scour for live-bed data for
(A) Gao et al. (1992), and (B) Hancu (1971) equations
9 9
+
4 A
0.3 -
0.2-
0.1-
S I
81
0.4 (A) HEC-18 (1995)
0.3
+ A
o
0.2- +
4-+
o +A
0.1 4- + Shenetal.(1966)
4 0 Chiew (1984)
A Chabert & Engeldinger (1956)
Graf(1995)
e Sheppard (1995)
0 ---- I I I I
0 0.1 0.2 0.3 0.4
measured scour (m)
(B) Inglis-Blench (1962)
+ Shen et al. (1966)
Chiew (1984)
A Chabert & Engeldinger (1956)
Graf(1995)
Q Sheppard (1995)
0.2
U./ A AA
CA. / +
o +A* *
:: / +++ + +
0.1- A*
0
0 0.1 0.2 0.3
measured scour (m)
Figure 5.14 Comparison of measured and calculated scour for live-bed data for
(A) HEC-18 (1995), and (B) Inglis-Blench (1962) equations
(A) Jain and Fischer (1979)
0.1
0-
0.4
0.3
0
0
-o 0.2
0.1
0
0 0.1 0.2 0.3 0.4 0.5
measured scour (m)
(B) Laursen and Toch (1956)
A A&
+ +
+ -- Ai/ *
++t+ +,
+
At
AL .,/
0 0.1 0.2 0.3 0.4
measured scour (m)
Figure 5.15 Comparison of measured and calculated scour for live-bed data for
(A) Jain and Fischer (1979), and (B) Laursen and Toch (1956) equations
0.6
E 0.4
0
U
o
S0.2
o .
(A) Melville (1997)
A
+ A
A
-t? Q *
A A- A
A4t+ ++
AA
0 0.1 0.2 0.3 0.4 0.5
measured scour (m)
0.3
S0.2
0
0.1
0
(B) Shen et al. (1966)
+ +++ im+it k Q
AinA *
0 0.1 0.2 0.3
measured scour (m)
Figure 5.16 Comparison of measured and calculated scour for live-bed data for
(A) Melville (1997), and (B) Shen et al. (1966) equations
84
Sheppard et al. (1995)
0.4
0.3
0
S0.2
0.1
0
0 0.1 0.2 0.3 0.4
measured scour (m)
Figure 5.17 Comparison of measured and calculated scour
for live-bed data for Sheppard et al. (1995) equation
*
Ar
|