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FINITE ELEMENT ANALYSES OF CELLULAR COFFERDAMS
by
Yash Pal Singh
Dissertation submitted to the Faculty of the
Virginia Polytechnic Institute and State University
in partial fulfillment of the requirements for the degree of
Doctor of Philosophy
T. Kuppusamy
T. L. Brandon
in
Civil Engineering
APPROVED:
G. W. cl>ugh, Chairman
October, 1987
Blacksburg, Virginia
. . "'n. Duncan
R. A. Heller
ae=- ..
FINITE ELEMENT ANALYSES OF CELLULAR COFFERDAMS
by
Yash Pal Singh
G. W. Clough, Chairman
Civil Engineering
(ABSTRACT)
Cellular cofferdams have primarily been used as temporary systems which serve to allow
construction of facilities in open bodies of water. Applications for these structures have been
increasing and today they may serve as permanent retaining walls or as navigation or
waterfront structures. Conventional design methods for cellular cofferdams are based on
semi-empirical approaches largely developed in the 1940s and 1950s. None of the available
traditional procedures are capable of predicting cofferdam deformations, a parameter of key
importance to the cofferdam performance, and which is often observed during construction for
purposes of safety monitoring. Also, there is evidence that much of the conventional design
technology is conservative, in some cases predicting loading by more than twice that which
actually occurs. Recently, the finite element method has shown promise as a tool which can
be used to help resolve some of the outstanding problems with cofferdam design.
There are three primary objectives of this work: (1) enhance existing finite element pro-
gram to allow for more accurate and refined analysis of cellular cofferdams, (2) use the en-
hanced finite element programs to assess the degree of conservatism in conventional design
methods for cofferdams founded on sandy soils, and (3) use the results of parametric studies
of cofferdams founded on sandy soils to develop a simplified procedure to predict cofferdam
movements and determine potential for internal failure. The first of the objectives involves
adding better bending elements to the program SOILSTRUCT to represent the sheet pile sys-
tem In axisymmetric and plane strain analyses. Also, in the case of the plane strain program,
a new method is developed to allow shear transfer through the sheet pile system. Through
case history and theoretical analyses, the enhanced programs are demonstrated to yield ac-
curate and realistic results.
Parametric studies using the axisymmetric program show that conventional design meth-
ods overpredict, in some areas strongly, the interlock forces which develop during filling of the
cofferdam. Parametric studies using the plane strain program suggest that there is also
considerable conservatism in design methods to predict internal stability of the cofferdam. A
new, simplified method is proposed for this type of analysis. In addition, it is shown that the
deformations of cofferdams on sand follow consistent trends and can be set into a non-
dimensionalized context which can be used to predict future cofferdam movements.
Acknowledgements
The author wishes to express his deep gratitude to his advisor, Dr. G. W. Clough, for his
guidance during the course of this research. I am extremely grateful to Dr. Clough for his
constant encouragement, tremendous patience, and very sincere personal considerations
without which the completion of this work could not have been possible. Special thanks are
due to Dr. T. Kuppusamy for his encouragement and reviewing of the research work from time
to time and soliciting advice. Much appreciation is extended to my other committee members,
Dr. J. M. Duncan, Dr. T. L. Brandon and Dr. R. A. Heller, for their interest in my studies and
research. Thanks are due to Dr. J. N. Reddy for his advice on some part of the research and
for his time.
I express gratitude to U.S.Army Corps of Engineers, Waterways Experiment Station for
funding this research project under contract No. DACW 39-86-K-0007. Support from personnel
of the St.Louis District of Corps of Engineers was provided at various times during the course
of the work. In particular, valuable instrumentation data for the Lock and Dam 26(R) cofferdam
were made available for this research. Thanks are extended to Mr. Reed Mosher, Dr. N.
Radhakrishnan, Mr. Donald Dressler and Mr. Tom Mudd for their help during the course of the
work.
Acknowledgements iv
I am indebted to my wife, for her continuous encouragement, moral sup-
port, facing all the hardships with lot of courage and assuming complete responsibility of the
family during all these years. Without her support, I could not have accomplished this task.
I have a lot of appreciation for my two children, : md who have shown
unbelievable cooperation, great understanding, and a lot of patience. Thanks and appreci-
ation are due to Or. M.P. Singh and Mrs. Kusum Singh for their encouragement and moral
support during these years. Thanks to all the friends and relatives who helped me in this
endeavour. Last but not feast, I tha.nk Miss Cathy Barker for her expert and efficient typing
of the dissertation and meeting all the deadlines without exception.
Acknowledgements y
Table of Contents
INTRODUCTION • . • • . • • • . . . • . • • • . . . . • • • . . . • . . . • • • . . • . . . • • • • • • • • • . . • . . . • • • 1
BACKGROUND • • • • • • . . . . . . • • • . • . . • • • • • . • • . . • . • . . . . • • . . . . . . . • • . . • • • • . . • • 6
2.1 Historical Background . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
2.2 Construction of Cellular Cofferdams .....................................• 7
2.3 Failure of Cellular Cofferdams . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10
2.4 Existing Design Theories . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12
2.4.1 Interlock Tension . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13
2.4.2 Shear in Cell Fill . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17
2.5 Finite Element Analysis Capabilities . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22
2.5.1 Early Investigations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23
2.5.2 Lock and Dam 26 (R) Cofferdam Studies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25
2.6 Summary and Recommendations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32
AXISYMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) . • • . • • • • • • • 36
3.1 Modification in Axisymmetric Finite Element Program: Provision of Shell Element . . 37
3.2 Test Problems to Check Shell Element . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44
Table of Contents vi
3.2.1 Test Problem 1 ................................................. 44
3.2.2 Test Problem 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 46
3.3 Problem of Interaction of Shell Element with Two-Dimensional Elements in Program
SOILSTRUCT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49
3.4 Case History Analysis Using One-Foot Thick Solid Element and New Shell Element for
Sheet Piles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49
3.4.1 Case History . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49
3.4.2 Previous Predictions and Observed Behavior . . . . . . . . . . . . . . . . . . . . . . . . . . 53
3.4.3 Predictions Using New Shell Element . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 53
3.5 Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 55
PARAMETRIC ANALYSES WITH THE AXISYMMETRIC FINITE ELEMENT PROGRAM 60
4.1 Effect of Depth of Embedment on Sheet Pile Deflections and Interlock Forces 61
4.2 Effect of Free Cell Height on Sheet Pile Deflection and Interlock Forces . . . . . . . . . . 71
4.3 Effect of Foundation Soil And Cell Fill Parameters on Sheet Pile Deflection and Inter-
lock Force . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 4
4.4 Discussion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 79
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) • • • • • • . • • • • 81
5.1 Modifications in Plane Strain Finite Element Program. . . . . . . . . . . . . . . . . . . . . . . . 83
5.2 Provision of Beam Element . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 84
5.2.1 Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 84
5.2.2 Test Problems to Check Beam Element . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 86
5.2.3 Problem of Interaction of Beam Element with Two-Dimensional Elements in Pro-
gram SOILSTRUCT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 90
5.2.4 Comparison With Previous Results - Cell Filling Case . . . . . . . . . . . . . . . . . . . . 90
5.3 Provision of Shear Transfer Element . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 92
5.3.1 Method of Computing Modulus (E) of Shear Transfer Elements for Use in Analyses 95
Table of Contents vii
CASE HISTORY STUDIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 104
6.1 Second Modulus Reduction Factor and General Analyses Procedures . . . . . . . . . . 105
6.2 Willow-Island Second Stage Cofferdam - Cell 27 . . . . . . . . . . . . . . . . . . . . . . . . . . 107
6.2.1 Project Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 107
6.2.2 Site Conditions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 110
6.2.3 Finite Element Analyses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 111
6.3 Willow Island Second-Stage Cofferdam Cloverleaf Cell 33 . . . . . . . . . . . . . . . . 119
6.3.1 Project Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 119
6.3.2 Finite Element Analyses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 119
6.4 Lock and Dam No. 26 (Replacement), First-Stage Cofferdam . . . . . . . . . . . . . . . . . 124
6.4.1 Project Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 124
6.4.2 Finite Element Analyses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 125
6.5 Summary of Case Histories . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 128
6.6 Stress Transfer Mechanism From Outboard to Inboard Sheet Pile . . . . . . . . . . . . . 130
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING ••••••••• 133
7.1 Analysis Procedures and Assumptions Therein . . . . . . . . . . . . . . . . . . . . . . . . . . . 134
7.2 Cell Filling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 136
7.3 Predicted Response for Flood-Type Load . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 139
7.3.1 Deflection of Sheet Piles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 139
7.3.2 Lateral Earth Pressure Coefficients . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 142
7.3.3 Base Pressure Distribution 146
7.3.4 Change of Vertical Stress in Cell Fill and Foundation . . . . . . . . . . . . . . . . . . . . 150
7.4 Predicted Response for High Lateral Loads . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 153
7.4.1 Deflection of Cell . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 153
7.4.2 Load-Deflection Response . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 154
7.4.3 Lateral Earth Pressure Coefficient . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 158
7.4.4 Possible Failure Mechanisms . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 159
Table of Contents viii
7.4.5 Vertical Displacement of Cell Fill and Slippage of Sheet Piles During Lateral
Loading . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 166
7.5 Summary and Conclusions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 173
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAIL·
URE UNDER LATERAL LOADINGS ..••...•..••••••.•.....•••....•••... , ... 176
8.1 Parametric Studies 178
8.1.1 Deflected Shapes of Cell . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 179
8.1.2 Effect of Depth of Embedment on Sheet Pile Deflections Due to Lateral Loading 184
8.1.3 Load Deflection Response of Cell . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 186
8.1.4 Vertical Displacement of Cell Fill and Slippage of Sheet Piles . . . . . . . . . . . . . 190
8.1.5 Failure Mechanisms Under Extreme Lateral Loadings . . . . . . . . . . . . . . . . . . . 190
8.2 Proposed New Method For Determination of Lateral Capacity of Cellular Cofferdams 192
8.2.1 An Example Problem to Compute Failure Load . . . . . . . . . . . . . . . . . . . . . . . . 202
8.3 Comparison of Shear Failure Analyses Methods . . . . . . . . . . . . . . . . . . . . . . . . . . 206
SUMMARY AND CONCLUSIONS • . • • . . . • • • • . . • . • . • • . • • • • • • • • • . • • • . • . . • • . . • 210
9.1 Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 210
9.2 Conclusions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 212
9.2.1 Modifications in SOILSTRUCT Programs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 213
9.2.2 Cell Filling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 213
9.2.3 Differential Loading . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 214
APPENDIX A • • • • . • . . • • • . • • • • • . . . • • . • • • • . • . • . . • . . . • . . • • . • • • . • • • • • • . . • • 216
APPENDIX B • • • . • • • • • • • • • • • • . . • • . . • • • . • . . • • • . . • . • • . . • • • • • . • • • • • • • . . • . 227
REFERENCES ...... I ••• I I •• I •••• I ••••••• I • I ••••••••• I I I • I • I ••••••• I • • • 238
Table of Contents Ix
VITA ............................................................... 242
Table of Contents x
LIST OF ILLUSTRATIONS
page
Figure 2.1. Common cell configurations (Lacroix, et al. 1970). 8
Figure 2.2. Conventional analyses methods for interlock force (from Shannon and Wilson, 1982). • . • • • • • . • 14
Figure 2.3. Interlock force, comparison of different conventional methods. . . . . . . . . . . . . . . . . . . . . 16
Figure 2.4. Terzaghi's vertical shear method •••• 18
Figure 2.5. Failure surfaces suggested by different authors. . • • 21
Figure 2.6. Finite element models (from Shannon and Wilson, 1982). 24
Figure 2.7. Non-linear stress strain behavior of soils •••
Figure 2.8. Comparison of results from axisymmetric and vertical slice analyses for cell filling (from Shannon and
28
Wilson, 1982). . • • . • • • • • • • • • • • . • • • • 30
Figure 2.9. Comparison of interlock forces predicted by various methods at the end of cell filling (from Clough and Kuppusamy, 1985) •.••••••.•
Figure 2.10. Vertical slice analysis, sheet pile deflections for different construction stages (from Shannon and
31
Wilson, 1982). • . • • . • • • . • • • • • • • . • • . 33
Figure 3.1. A thin cylindrical shell ••• 38
Figure 3.2. Test Problem 1, long cylinder subjected to internal pressure. . . . . . . . . . . . . . . . . . . . . 45
Figure 3.3. Test Problem 2, cylindrical tank with hydrostatic pressure. • • • 47
Figure 3.4. Lock and Dam 26 (R) cofferdam, basic conditions. • • • 51
Figure 3.5. Axisymmetric analysis, using one-foot thick element, sheet pile deflections and interlock forces at the end of cell filling. • • • • • • • • • • • • • • • • • • • 54
Figure 3.6. Finite element mesh for axisymmetric analyses of Lock and Dam 26 (R) cofferdam.. • • • • • • • • • • • • • • 56
List of Illustrations xi
Figure 3.7. Lock and Dam 26 (R)' sheet pile deflections at the end of cell filling. . . . . . . . . . . . . . . . . 57
Figure 3.8. Lock and Dam 26 (R)' interlock forces at the end of cell filling. . . . . . . . . . . 58
Figure 4.1. Deflected shapes of cofferdam cell at the end of cell filling. . . . . . . . . . . . . . . . . 62
Figure 4.2. Maximum sheet pile deflections at the end of cell filling. . . . . . . . . . . . . . . . . . . 64
Figure 4.3. Lateral earth pressures against sheet pile at the end of cell filling. . • • • • • . • . • • . • • • • • 65
Figure 4.4. Maximum interlock forces at the end of cell filling. • 66
Figure 4.5. Cell deflections below dredge line at the end of cell filling. . . . . . . . . . . . . . . . . . . . . . . . 68
Figure 4.6. Effect of depth of embedment on location of maximum cell deflection and interlock force at the end of cell filling. . . . . . . . . . . . . . . . . . . . . . 69
Figure 4.7. Lock and Dam 26 (R), interlock forces at the end of cell filling. Comparison of FE analysis and conventional design methods. • • • • • • . • . • • • 70
Figure 4.8. Effect of cell fill material on maximum sheet pile deflections at the end of cell filling. 72
Figure 4.9. Effect of cell fill material on maximum interlock forces at the end of cell filling. • • • • • • • • • • • 73
Figure 4.10. Effect of free cell material on maximum interlock force (FEM and Schroeder and Maitland method) at the end of cell filling. . . . . . . . . . . . . . . . . . . . . . 75
Figure 4.11. Effect of free cell height on location of maximum cell deflection and interlock force at the end of cell filling. . . . . . . . . . . . . . . . . 76
Figure 4.12. Effect of foundation material on maximum sheet pile deflections at the end of cell filling. • • • • • • • 77
Figure 4.13. Effect of foundation material on maximum interlock forces at the end of cell filling. • • 78
Figure 5.1. Planar representation of cofferdam cell for FEM analysis (from Hansen and Clough, 1982). • • • • • ••• 82
List of Illustrations xi\
Figure S.2. A beam element. . . . . . . . . . . . . . . . . . . . . 8S
Figure S.3. Test problem l, beam with transverse load. . . . . . . 87
Figure S.4. Test Problem 2, beam on elastic foundation. . . . . . . 89
Figure S.S. Test Problem 2, deflection of beam on elastic foundation. . . . . . . 91
Figure S.6. Finite element mesh for Lock and Dam 26 (R) first stage cofferdam. . . . . . . . . . . . . . . . . . . 93
Figure S.7. Deflection of sheet pile at the end of cell filling, Lock and Dam 26 cofferdam. • • • • • • • • • • • • . • 94
Figure S.8. Isometric view of cell fill elements and overlapping shear transfer elements. • • . • . • • • • • • • . • • 96
Figure S.9. Schematic details of thin cylinder and finite element mesh. . . . . . . . . . . . . . . . . . . . . 98
Figure S.10. Deflection ratio versus modulus ratio for Lock and Dam 26 (R). . • • . • • . • • • • • . 101
Figure S.11. H/B versus modulus ratio. 103
Figure 6.1. Deflection of sheet piles due to lateral load. 106
Figure 6.2. Willow Island second-stage cofferdam location plan ••• 109
Figure 6.3. Finite element mesh for Willow Island cofferdam, cell no. 27. . . . . . . . . . . . . . . . . . 112
Figure 6.4. Willow Island Cofferdam, Cell 27, construction sequence modeled. • • • • • • • • 114
Figure 6.S. Willow Island Cofferdam, Cell 27, inboard sheet pile deflections due to initial dewatering. • • • • • • • • 116
Figure 6.6. Willow Island Cofferdam, Cell 27, inboard sheet pile deflections due to initial dewatering and equipment surcharge load. . • • • . . • • . • • • 11 7
Figure 6.7. Willow Island Cofferdam, Cell 27, inboard sheet pile deflections due to initial dewatering, using springs and shear transfer elements. • • • • • • • • . • 118
Figure 6.8. Finite element mesh for Willow Island cofferdam, cloverleaf cell no. 33 ••••••••••••••••• 120
Figure 6.9. Willow Island Cofferdam, cloverleaf cell 33, deflections
List of Illustrations xiii
of inboard sheet pile due to initial dewatering. . • • 122
Figure 6.10. Finite element mesh for Lock and Dam 26 (R) first stage cofferdam. . • . • • . . . • • . • • • • . • . 123
Figure 6.11. Lock and Dam (R) cofferdam, construction sequence modeled. . . . . . . . . . . . . . . 126
Figure 6.12. Lock and Dam 26 (R) cofferdam, deflection of sheet piles due to berm placement. . . • • • . • • 127
Figure 6.13. Lock and Dam 26 (R) cofferdam, deflection of inboard sheet pile due to initial dewatering. • • . • 129
Figure 6.14. Lock and Dam 26 (R) cofferdam load transfer from outboard to inboard sheet pile at El. 105 for hydros ta tic load 1 lwh. • . • • • • • • • • • 131
Figure 7.1. Schematic representation of a cofferdam cell subjected to lateral load. • • • • • • • • • 135
Figure 7.2. Lateral earth pressure coefficient (K) for cell filling. . . . . . . . . . . . 138
Figure 7.3. Deflected shape of a cofferdam cell due to lateral load. . . . . . . . . . . . . . . . . 140
Figure 7.4. Deflection of sheet piles due to lateral load. • • • • 141
Figure 7.5. Lock and Dam 26 (R), observed cell deflection for flood load (from Martin, 1987). • • • • . • 143
Figure 7.6. Lock and Dam 26 (R), average response of 11 typical cells to lateral loading (from Martin, 1987). • • • 144
Figure 7.7. Lateral earth pressure coefficients (K) for hydrostatic load 3 lwh. • • • • • • • • • • • • • • • 145
Figure 7.8. Base pressure at end of cell filling, Lock and Dam 26 (R) cofferdam. • • • • • • • • . • • . . • • 147
Figure 7.9. Base pressures at dredge line due to lateral load, Lock and Dam 26 (R) cofferdam. . . • • • • • • • • • 148
Figure 7.10. Change of vertical stress in cell fill due to lateral load, Lock and Dam 26 (R) cofferdam. • • • • • 151
Figure 7.11. Change of vertical stress in foundation due to lateral load, Lock and Dam 26 (R) cofferdam. • • • • • • 152
Figure 7.12. Lock and Dam 26, deflected shape of cell for lateral
List of Illustrations xiv
loads. • . • 155
Figure 7.13. Lock and Dam 26, deflected shape of cell for collapse lateral load 7lwh. • • • . 156
Figure 7.14. Lock and Dam 26, lateral load versus deflection of sheet pile top. . • • • . • • . . • • • • • • • 157
Figure 7.15. Lateral earth pressure coefficient (K) for hydrostatic lateral load 3lwh. • • . . . • . • • . • . 160
Figure 7.16. Lateral earth pressure coefficient (K) for hydrostatic lateral load 5lwh. • • . . • . . • • . 161
Figure 7.17. Determination of direction of failure planes. • . 163
Figure 7.18. Lock and Dam 26, failed soil elements and failure loads. • . • • . . • • • . • • • • • • • • 164
Figure 7.19. Lock and Dam 26, failure plane directions and failure surfaces due to lateral loads. . • • • • • • . • . 165
Figure 7.20. Lock and Dam 26, vertical displacements at top of cell fill without and with soil interfaces. • • • • • . 167
Figure 7.21. Lock and Dam 26, effect of soil interfaces on sheet pile deflections during lateral loading. • • • • • • • 169
Figure 7.22. Schematic representation of slippage of sheet piles due to lateral loads. • • • • • • • • • • • • • • 171
Figure 7.23. Lock and Dam 26, axial pull and interlock resistance in inboard sheet pile due to lateral load. • 172
Figure 8.1. Deflected shapes of 63 feet and 40 feet wide cells for load llwh. • • • • • • • • • 181
Figure 8.2. Deflected shapes of cofferdam cell for collapse lateral load. . . . . . . . . . . . . . . . . . . . . . . . 182
Figure 8.3. Deflected shapes of cofferdam cell with and without scour. 183
Figure 8.4. Effect of depth of embedment on sheet pile deflection during lateral loading. • • • • • ••••••••• 185
Figure 8.5. Sheet pile deflection as percentage of cell height for different depths of embedment and cell width. • • • . • 187
Figure 8.6. Lateral load versus deflection of sheet pile top for cell width of 63 feet. • • • • • • . • • • • • • • • • • • • 188
Figure 8.7. Lateral load versus deflection of sheet pile top for cell
List of Illustrations xv
width of 40 feet .•.• . • 1a9
Figure a.a. Radius versus center of rotation of curved failure surface . ...... . 191
Figure a.9. Shear failure analysis with curved failure surface •.. 195
Figure 8.10. Shear failure analysis with vertical failure surface .• 197
Figure a.11. Cofferdam circular cell, location of vertical shear failure surface •. 200
Figure a.12. Schematic representation of failure surfaces and free body diagram showing forces. • • • • • . • . 205
Figure a.13. Comparison of shear failure analyses methods, load-deflection curves for cell width 63 feet • • • . . • • 207
Figure a.14. Comparison of shear failure analyses methods, load-deformation curves for cell width 63 feet • • • . • • 2oa
List of Illustrations xvi
LIST OF TABLES
page Table 3.1. Predicted deflections and hoop stresses in a hollow
cylinder. . • • • • • • • . • • 48
Table 3.2 Soil parameters for finite element analysis of Lock
Table 5.1
Table 6.1
Table 8.1.
and Dam 26 (R). • • . . . . . • • • • • . • 52
Dimensions of cylinders used in parametric studies to evaluate response of shear transfer elements ••••.• 100
Soil or rock properties for Willow Island cofferdam ••• 113
Circular Failure Surfaces ••••• . .193
List of Tables xvii
Chapter I
INTRODUCTION
Cellular cofferdams are used to retain soil or water or both. Initially, they were generally
built only as temporary structures to exclude water from an excavation to ensure construction
in dry conditions, but today they are also used as permanent structures such as piers,
wharves and jetties. They are constructed of interlocking sheet piles forming adjacent cells
and are usually filled with free draining cohesionless material. Shapes of cofferdam cells are
circular, diaphragm, and cloverleaf. However, circular cells are most commonly used.
Conventional design methods for cellular cofferdams consider sliding, overturning, inter-
lock tension and vertical shear failure of cell fill. The most frequent cause of cell failure has
been related to the interlock tension issue. Even though these problems were largely attri-
buted to structural failure of fabricated tees and wyes due to inadequately designed con-
nections or faulty fabrication, the nature and magnitude of interlock tension per se, and the
use of proper factor of safety remains a matter of concern. There are a number of different
design methods for determining interlock tensions, and each assumes different lateral earth
pressure magnitudes and distributions in the calculation technique. As a result, significantly
INTRODUCTION 1
different predictions can be made for interlock tension. Comparison with observed data sug-
gests that predictions of most of the conventional methods are conservative. Similar prob-
lems exist concerning the possibility of shear failure of cell fill during lateral loading. The
conventional theories for analyzing this failure differ in both the assumption of failure surface
as well as lateral earth pressure coefficient, and these as well have been shown to largely
yield overly conservative results.
Although some modifications have been proposed in the last decade for cofferdam design,
most of the design methods were developed more than 30 years ago, and the alternatives lead
to considerable differences in predicted behavior. These methods are also lacking in that:
• There is no means to predict cell wall movements and deflections.
• Explicit procedures to consider soil-structure interaction effects are not provided.
• The effect of alternative construction sequences cannot be predicted.
The first deficiency is particularly important because safety instrumentation for cofferdams is
mainly directed at measurement of cell movement.
In the past decade, a number of investigators have begun to apply the finite element
method to the cofferdam problem. This method offers the possibility to predict cofferdam be-
havior while analyzing the cofferdam as a unit, and accounting for many of the aspects of the
system that elude conventional procedures. Both two and three dimensional models have
been proposed for analysis of cofferdams. The three-dimensional model provides the means
for accurately accounting for the complex geometry of the cellular cofferdam, but it is expen-
sive to use, and remains beyond the reach of most applications. Two-dimensional models
offer utility in the study of cofferdams through parametric studies; however, the models used
to date have mainly been designed for specific applications.
INTRODUCTION 2
In one of the most extensive studies of a specific project, Clough and Kuppusamy (1985)
undertook analyses for the Lock and Dam 26 Replacement (R) cofferdam. This cofferdam was
one of the largest projects of its type in the world, and its first stage was well instrumented.
In the course of this study, the program SOILSTRUCT was modified to be used in three ver-
sions, with each version designed to address some important aspect of the cofferdam re-
sponse. To model orthotropic behavior of sheet piles, an E-ratio concept was introduced.
Reasonable predictions of the behavior of the cofferdam were made, and verified through the
instrumentation results from the first stage of the cofferdam. However, it was apparent that
improvements in the modeling techniques could be made, and that this was advisable before
any general parametric studies were conducted with the programs.
This particular investigation was undertaken with the general objective of adding needed
enhancements to the SOILSTRUCT cofferdam programs, as discussed in following para-
graphs, and conducting parametric studies to aid in developing improvements to the existing
design technology for cofferdams. At about the same time as this work began, a comple-
mentary effort was undertaken at the U.S. Army Corps of Engineers Waterways Experiment
Station by R. Mosher to develop a three-dimensional finite element program for analysis of
cofferdams. It was decided that where possible, the programs for the three-dimensional
analysis and two-dimensional analysis would be made compatible. Thus, the objective of the
present effort was expanded with this goal in mind.
In Chapter 2, a review of the literature on cofferdams is presented. This includes historical
background, techniques for construction, examples of failures of cofferdams, existing design
approaches, and available finite element techniques. Areas where improvements are needed
in finite element analysis procedures are noted.
Chapter 3 presents the documentation for inclusion of a shell element in the axisymmetric
version of SOILSTRUCT finite element program. The shell element is provided to make it
INTRODUCTION 3
possible to model sheet pile thickness exactly, to account for their bending characteristics,
and to make this program compatible with three-dimensional version being developed at
Waterways Experiment Station. Predicted results using the new program are verified against
closed form solutions and compared to predictions for the Lock and Dam 26 (R) cofferdam,
made previously using two and three dimensional finite element models.
Parametric studies of the cell filling case using the modified axisymmetric program are
outlined in Chapter 4. Effects of depth of cell embedment, free cell height, and the strength
of soil in the cell fill and foundation on the maximum sheet pile deflections and maximum
interlock forces are investigated.
In Chapter 5, modifications to the plane strain version of SOILSTRUCT are described. The
plane strain model is used to examine the response of a vertical slice cut through the
cofferdam. This model allows one to study the response of the cofferdam to differential load-
ing as a result of berm placement, dewatering, and river flooding. The first of the modifica-
tions involves the addition of a beam element to the program to allow for improved modeling
of the structural system used for the cells, as actual thickness and bending behavior of sheet
piles could be modeled. The beam element serves to represent the "front and back walls" of
the cell in the vertical slice analysis. The second modification is the formulation of a new
method for the system used to connect the front and back walls of the cell. The connection
system in essence serves as the means to realize the effects of the "missing" part of the cells
that exists between the front and back walls. In the new approach, a set of special shear
transfer elements are used which overlay the soil elements representing the cell fill. Also
included in Chapter 5 are theoretical analyses designed to determine one of the two modulus
reduction factors for the shear transfer elements.
Chapter 6 is devoted to a series of case history studies using the modified plane strain
program. These studies are designed to test the ability of the new program to predict actual
INTRODUCTION 4
behavior of cofferdams where instrumentation results are available to check the response.
A secondary purpose of the case history analyses is to compute the second modulus re-
duction factor to arrive at stiffness that is needed for the shear transfer elements.
Chapters 7 and 8 are devoted to use of the modified plane strain program for studying the
behavior of Lock and Dam 26 (R) cofferdam during differential loading and conducting
parametric studies. The results are applied to evaluation of conventional analyses of internal
failure of cofferdam cells. Particular attention is given to deformations of the cells to provide
the designer with useful information that can guide decisions about how much deformation
will occur in future cofferdams. Finally, a new method for the analysis of internal failure of
cofferdams is proposed. This method is less conservative than those now existing.
The last chapter presents a summary of the information in this document. Also, conclu-
sions that can be drawn from the results of the study are made.
INTRODUCTION 5
Chapter II
BACKGROUND
2.1 Historical Background
The cellular cofferdam was first used as a temporary structure to exclude water from an
excavation so that construction could proceed in the dry condition. Today, cofferdams are
used to retain both soil and water and may be permanent structures, such as piers, wharves
and jetties. Cellular cofferdams are used in lieu of earth or rockfill dams when the width of
the structure must be small, when a vertical face is required, or when stability against scour
is required. The first cellular cofferdam was built in 1908 at Black Rock Harbor, Buffalo, N.Y.
with a height of 30 feet and using square cells. Top of cell movements were as large as 3.5
feet between crosswalls (Stevens, 1980). Circular cells were used two years later in a
cofferdam built to raise the battleship Maine in Havana Harbor. An internal earth berm was
used to stabilize the cofferdam because of excessive movements during dewatering.
Diaphragm cells, consisting of curved cell faces and straight crosswalls, were used by the U.S.
Army Corps of Engineers in 1915 at Troy, N.Y.
BACKGROUND 6
2.2 Construction of Cellular Cofferdams
Cellular cofferdams are constructed using interlocking steel sheet piles forming adjacent
cells which are usually filled with free-draining cohesionless material. The combination of
steel cells and fill, which individually are unstable, make cofferdams a unique type of structure
which is capable of withstanding lateral loads. They are usually temporary, may have a low
factor of safety, can resist large lateral loads that may cause noticeable cell movements
without hindering their performance, and are often constructed where difficult site conditions
exist.
Cells are commonly of circular, cloverleaf and diaphragm configurations, as shown in Fig-
ure 2.1. Circular cells are constructed using a template, or frame, having the same plan area
as the cell. Connection sheet piles are set first against the outer perimeter of the template,
and are held in place by spot welding and guy lines. Closure is made by sticking the re-
maining sheet piles, usually in groups of three or four to minimize interlock tension. For cells
on a rock foundation, sheet piles are driven individually into or to refusal on rock to increase
the resistance to sliding, decrease the interlock tension at the toe of the cell, and minimize the
possibility of cell fill loss. Penetration is usually limited to about five feet in hard clay and ten
feet in dense sand so pre-excavation may be required. Higher penetrations are sometimes
used depending upon project requirements. Hard driving is avoided to decrease the chance
of driving out of interlock. Splices are staggered to limit deformation, and the piling should
be long enough to extend above the water level.
Circular cells are often filled hydraulically with sand and gravel dredged near the site. This
eliminates the need for compaction and actually pretests the interlocks because the maximum
interlock stresses may occur during filling if the water inside the cell is high and the water
elevation outside is low. The template is removed after partial filling has given the cell
BACKGROUND 7
8 "
B b
a. Circvl<Y CoFkrrlom
J. -
' ' c,.,, . ..,.~,""
b 8 .
- -b. Dlophrom Col/~rtlom
c. Clovtrleal C"llerr:bm l~9~nd
IJ 'V"'°"'k"I wid'lh or c1Bu/o,. col'l'1rdom; wio'flJ of /'.c/i,,ew• sl'fll~l-wr1// ""°/"""'°"7 IY ~ "'"" au11 o,. s~clio,, A'loo'u/11, 9~"~r411}' o•a8/J lo a9/J
b lolol """" o' i:'I/,.. ~""°" (. o.-~ra91 di.s/oM>~ '4/,tt11 uon woQ r r"o'i'vs ~ circubr all lfOll. d.O~ "1011, or clowr/MI" w"ll
tn U>Own
Figure 2.1. Common cell configurations (Lacroix, et al. 1970).
BACKGROUND 8
enough stability to prevent racking. Circular cells are filled before the connecting arcs. An
alternative to the use of dredging the fill is placement by clamshell process. This leads to
lower interlock stresses during cell filling. Diaphragm cells are filled progressively, so that the
difference in elevation of the fill does not exceed three to five feet on opposite sides of each
crosswall.
In response to cell filling, the cell walls barrel out as the piling is laterally loaded and the
slack in the interlocks is taken up. The maximum bulging, and the maximum interlock tension,
occurs at a point usually located one-third to one-quarter of the cell height above the dredge
line (Stevens, 1980).
The cell fill settles as the cofferdam is dewatered. During subsequent fluctuations of the
phreatic surface, additional settlement occurs, particularly on the unloaded side of the
cofferdam. Extensive movement of heavy construction equipment over the top of the cells also
contributes to the compaction of the fill. Lacroix et al. (1970) report total cell fill settlement
may be as much as six inches for high cofferdams with heights greater than 50 feet. Cells
founded on sandy or silty soils may experience total settlements as large as fifteen inches
(Stevens, 1980).
In response to dewatering, top of cell movements in the horizontal direction of three to six
inches are normally experienced for high cofferdams with good foundation conditions. One
exception was the New Cumberland cofferdam which consisted of fifty-four foot diameter cells
sixty feet high founded on rock. This is the smallest width to height ratio attempted in the
series of Ohio River cofferdams. Swatek (1966) reported that the cofferdam "performed ad-
mirably" despite eighteen inches of horizontal movement at the top of the cell. Schroeder,
Marker and Khyujerernpanishk (1977) also reported nine inches of movement at the top of a
56-foot high cellular bulkhead founded on sand without impairment of performance. Lacroix
BACKGROUND 9
et al. (1970) have concluded that top of cell movements would have to be several feet before
interlock rupture would occur.
2.3 Failure of Cellular Cofferdams
Lacroix et al. (1970) reported that the most frequent cause of cell failure in the cases they
reviewed was excessive interlock tension, which may have resulted from inadequately de-
signed connection of sheet piles or excessive cell deformation. In a later report by the U.S.
Army Corps of Engineers (1974), it was concluded that structural failure of fabricated tees and
wyes has been a common cause of cell rupture. The Corps (1974) reported ten failures of 90°
welded tees and four failures of 78° welded wyes. Failure of welded connectors usually oc-
curred in the web of the main sheet pile, or through web rupture on both sides of the stem,
separating the connector into three pieces. The inherent weakness of welded fabrications
prompted the Corps to require riveted connectors in 1965 (Stevens, 1980).
Failures of connectors were noted to usually occur during cell filling, although one failure
took place during dewatering and another as overburden inside the cofferdam was removed.
It is recommended that to decrease the pull exerted by the stem of a connector, the radius
of the connecting arc should be as small as possible, never exceeding one-half the cell radius.
Because the component of the stem force normal to the sheet pile for a 30° wye is one-half
that for a tee, Lacroix et al. (1970) recommended that riveted tees only be used for cell heights
of less than 40 feet.
During easy driving, piling may not seat in rock when uneven pile lengths are driven in
pairs or the rock surface is very irregular. During hard driving, piling can be driven out of
interlock. High velocity flow will scour the overburden and weathered rock, exposing windows
BACKGROUND 10
at the base of the cell. The current pulls the cell fill out, forming a pipe to the top of the cell
along the sheet pile wall. Cell collapse may be prevented by dumping in coarse rock or baled
hay, but must not be delayed because a cell can empty and collapse in a few hours. The
windows can also be sealed from outside the cell. The Corps (1974) reported the collapse of
three cells at Webbers Falls Locks and Dam and one at Holt Lock and Dam by removal of fill
by scour. At Keystone Dam, 2.5 feet of the shale foundation was eroded during a long period
of high spillway discharge, but cell rupture was averted.
The catastrophic failure of the second stage cofferdam at Cannelton was attributed to pip-
ing. The failure occurred during high water at a tie-in arc connecting the downstream arm of
the cofferdam to the sloping face of the river lock wall. The seals provided were not adequate
to limit seepage along the fill-concrete interface. As the cell unloaded, the piling moved away
from the lock wall, and water rushed in, flooding the cofferdam.
Driving piling out of interlock is a common occurrence. Although split interlocks usually
do not lead to cell rupture, loss of cell fill due to piping may occur when overburden is re-
moved by scour or excavation. Only three cases of total interlock failure were reported by the
Corps of Engineers (1974), all occurring during cell filling. Splits discovered after dewatering
are repaired by welding steel plates across the gap. To avoid split interlocks, piling should
not be driven through overburden containing boulders or other obstructions. To ensure that
used sheet piles interlock properly, the amount of spread between thumb and finger as well
as the overall distortion needs careful inspection. Sheets at splices must be dimensionally
compatible to prevent high localized stresses in the interlocks and webs.
When divers inspected the 12 cells forming the river arm of the first stage cofferdam at
Cannelton, of the 14 splits discovered, 12 occurred in connecting areas. A preponderance of
splits occurs in connecting arcs when the arcs are driven after the adjacent main cells have
been filled. The sheet piles of the arc must conform to the curvature of the connectors. Some
BACKGROUND 11
adjustment is possible within the interlocks, but the main cell barrels out so much that driving
out of interlock occurs frequently. This is prevented by driving at least the first two sheets of
the connecting arc prior to filling the main cell.
The first stage cofferdam at Uniontown Locks and Dams failed by deep-seated sliding
during a rising river ten days after dewatering was completed. Seven downstream arm cells
slid with the shale and limestone foundation on an underlying coal and clay seam. Four cells
remained essentially intact, sliding 37 to 72 feet into the cofferdam interior. The two adjacent
cells ruptured, and the cofferdam was flooded in less than ten minutes after movement was
first noticed. The failure plane was located at a maximum depth of 16 feet below the top of
rock, but daylighted at a normal fault near the center of the cofferdam (Stevens, 1980).
The sub-cofferdam located inside the first stage cofferdam at Cannelton Locks and Dam
failed when seven cells slid eleven feet toward the nearly completed pier excavations, with
one cell rupturing at 90° riveted tee (Stevens, 1980). Failure resulted because the cells were
too near the excavation and the rock surface was of poor quality.
2.4 Existing Design Theories
The present basis for design of cellular cofferdams is essentially semi-empirical. Design
methods were originally suggested by Pennoyer (1934) and were later modified and extended
by Terzaghi (1945). Alternative design concepts and modifications have been proposed by
Cummings (1957), Krynine (1945), Hansen (1953, 1957), Department of Navy (1977), and
Schroeder and Maitland (1979).
BACKGROUND 12
The usual design approach for cellular structures involves consideration of both internal
and external stability. External stability requires adequate factor of safety against (i) sliding
and (ii) overturning. The internal stability considers safety against (i) bursting of interlocks
and (ii) shear distortion of cell fill. The methods for design have been discussed by Terzaghi
(1945), Lacroix et al. (1970), Dismuke (1975), Schroeder and Maitland (1979) and U.S. Army
Engineer Waterways Experiment Station (1986).
Based on experimental evidence, Schroeder and Maitland (1979) have indicated that nei-
ther sliding nor overturning can occur before a typical cell embedded in deep sand will fail
because of loss of internal stability. Therefore, in designing such cellular structures, it be-
comes important to provide an adequate design for internal stability.
2.4.1 Interlock Tension
Design for interlock tension has been discussed by Terzaghi (1945), Lacroix et al. (1970)
and Schroeder and Maitland (1979). Four recommended design pressure diagrams for cal-
culating interlock forces are presented in Figure 2.2. These differ in the distribution and
magnitude of lateral earth pressure applied to cell walls. The computed maximum lateral
earth pressure is converted to an interlock force using following formulae:
Main cell piles:
T = Px R
where:
T = Interlock force
P = Lateral earth pressure
R = Radius of cell
BACKGROUND 13
TERZAGHI METHOD ---------------I
·' , I
I I
I I - I -
I I
I I p I
K = 0.4
TVA METHOD ----------I
I I
I I , - I
I
' ' '
P =Ka ' at 0.75H av K • tan2 (45-! )
a 2
·iP H
U.S. ARMY CORPS OF ENGRS METHOD SCHROEDER '& MAITLAND METHOD -----------------------~----- ---------------------------
-
p
K
/ /
I I
I I
I p I
Kcr ' at H v 0.5
/ /
/
H I I I
/ ,'
/ /
/
I p
' ' ' ~:r ', d' '
P = Kcr ' at 2 H' v -3-
H' = H+d' d'= 5 ft.
T
K=l.2 to 1.6 tan2 (45-! ) 2
NOTE: crv' is vertical effective stress
Figure 2.2. Conventional analyses methods for Interlock force (from Shannon and Wilson, 1982).
BACKGROUND
H'
14
Common wall piles:
T = P x L x Seca
where:
L = center line distance between main and arc cells
a = angle between center line of main cell and Y-connection point
In computing maximum interlock force, the Terzaghi and Corps of Engineers methods
consider lateral earth pressure increasing up to dredge line, assuming a lateral earth pres-
sure coefficient as 0.4 and 0.5, respectively. The lateral earth pressure in the TVA method
increases up to one-fourth of free cell height from dredge line, and then decreases to zero at
dredge line, with the lateral earth pressure coefficient being taken as active earth pressure
coefficient. Schroeder and Maitland method considers the plane of fixity below dredge line
and assumes maximum lateral earth pressure at a distance of one-third of the height from
point of fixity to top of cell measured from point of fixity.
For a direct comparison of these methods, consider a cofferdam cell with cell diameter of
63 feet, free cell height of 60 feet, depth of embedment 20 feet, a cell fill total unit weight and
friction angle of 123 pcf and 30 degrees, respectively, and water level at 30 feet from top of the
cell. The predictions of interlock forces using these design methods are shown in Figure 2.3.
The TVA method predicts the smallest interlock force, and the Schroeder and Maitland
method, Terzaghi method and Corps of Engineers method yield maximum interlock force val-
ues which are higher by 36%, 47% and 83%, respectively, as compared with TVA values.
BACKGROUND 15
-., QJ QJ ~ '-'
i::: 0 ~ ., cu > QJ
..-t f%l
70
60
50
40
30
20
10
.,,.
Engineers & Maitland
Terzaghi
Interlock Force (Kip/inch)
Figure 2.3. Interlock force, comparison of different conventional methods.
BACKGROUND 16
2.4.2 Shear in Cell Fill
Terzaghi (1945) suggested that before failure due to overturning occurs, the cofferdam is
likely to fail due to shearing of soil along vertical line gh (Figure 2.4) at center of cell during
application of lateral loads. He developed the design approach for vertical shear for
cofferdams founded on rock. However, he indicated that results of such an analysis were not
greatly different for structures on rock or on sands and proposed that the rules developed for
analysis of cofferdams on rock would apply to all cases.
In his vertical shear analysis, Terzaghi (1945) assumed a straight line distribution of pres-
sure on the base of cofferdam (Figure 2.4).
Q = Total force represented by each triangle of base pressure diagram
M = Overturning moment
M = 2bQ 3
or Q = 3M 2 b
(2.1)
The shearing resistance S' on vertical plane gh = PcTan<p .
where: Pc = Earth pressure on gh per unit length of cofferdam
q> = Coefficient of internal friction of cell fill
Pc = 1/2yKH2 •
where: y = unit weight of cell fill
H = height of cell
K = coefficient of lateral earth pressure at center line of cell
BACKGROUND 17
BACKGROUND
J• b
~rrM g
I oJllo
I
m Rock
.. ,
I H
~ Pressure diagram at base n
! +Q I-- 2b/3--f
Figure 2.4. Terzaghi's vertical shear method.
18
Therefore, S' = 1/2 y K H2 tan q>. Total tension in a interlock with length H is:
T = 1/2 KyH 2r
where: r = radius of cell
Total resistance against slippage in interlock is:
T f = 1/2 yKH 2r f
where: f = coefficient of interlock friction.
Circular cells contain two cross walls per cell and length of each cell is 2L.; those of the
diaphragm type contain one cross wall per cell and the length of each cell is L. Hence, the
resistance to shearing along gh contributed by interlock per unit length.
S" = rL = .1.yKH2L.r L 2 L
[2.2]
Total average shearing resistance S is given by:
S = S' + S" = .1.yKH2( tan q> + L.r, 2 L
[2.3]
the ratio r/L is close to or equal to unity. Hence, approximately:
S = 1/2 y K H2 (tanq> + f).
The corresponding factor of safety:
2 Gs= ~ = y~~ K(tanq> + f) [2.4]
Terzaghi proposed that the lateral earth pressure coefficient K within the cell should re-
main at its initial value of something less than 0.5. The factor of safety G, is taken as equal
to or greater than 1.25 and 1.5 for temporary and permanent structures, respectively.
BACKGROUND 19
Since its proposal by Terzaghi, the vertical shear concept has been the subject of consid-
erable criticism, in part directed towards the assumption of the vertical shear mechanism, and
in part towards the use of 0.5 for the lateral earth pressure coefficient. Concern about the use
of the vertical shear surface was first voiced by Pennoyer (1945), who analyzed a number of
cofferdams that had performed well, and found that only 60% of them were predicted to be
stable using the Terzaghi mechanism. Notably, all of the cofferdams had a large width relative
to their height, and Pennoyer felt that the shear surface should be a function of cell width.
Subsequently, three authors suggested alternative methods of analysis based on different
assumptions for the internal failure surface as shown in Figure 2.5. Krynine (1945) proposed
that the failure surface should be curved, and follow a path from the bottom of the outboard
sheet up to the top of the inboard sheet. This mechanism then allows for increased resistance
as the cell width gets larger. Hansen (1953, 1957) followed a different track, and suggested
that the failure surface would be located near the bottom of the cell and have a shape of log-
arithmic spiral passing from outboard to inboard sheet piles. In a simplified version of this
approach, Cummings (1957) proposed a method of analysis based on horizontal shear con-
cept. He suggested that the failure surfaces could be taken as a straight horizontal shear
planes through the cell fill. Schroeder and Maitland (1979) reported that Cummings' approach
overestimates moment resisting capacity of cofferdam cells.
In an effort to sort out the controversy about the type of failure surface which should be
used to analyze for failure under lateral loading, Schroeder and Maitland (1979) performed a
series of large scale model tests of cellular cofferdams. In the tests, the cells were loaded to
complete failure, and it was found that sharply defined terraces formed at the surface of the
cell fill. In addition, slippage was observed along the sheet pile interlocks in the middle and
inboard portions of the cell. The observed slippages in the fill and the sheet pile interlocks
were considered to support the original Terzaghi vertical shear mechanism. Notably, at the
stage of the tests where the failure mechanism was clearly visible, the deformations of the
cells were very large, with lateral movements of the tops of the sheet piles reaching up to 50%
BACKGROUND 20
Load Failure I Surface / >·/·
KRYNINE (1945)
Load
Load
- - - -- - - - - ---t'11n'l~
(~~~!._ ~~~:~e . '·
HANSEN (1953 ,1957)
CUMMINGS ( 195 7)
Figure 2.5. Failure surlaces suggested by different authors.
BACKGROUND 21
of the cell height. This suggests the need for the application of a significant factor of safety
against this failure mode if deformations are to be kept to reasonable levels.
While Schroeder and Maitland (1979) generally supported the failure mode of Terzaghi,
they disagreed with his proposed lateral earth pressure coefficient to be used in the vertical
shear calculation. Earlier, Krynine (1945) had noted that there was reason to believe that the
coefficient of lateral earth pressure during lateral loading should be higher than 0.5, and could
be slightly higher than the at-rest coefficient. Schroeder and Maitland (1979) found that if the
Terzaghi vertical shear mechanism is used, then a coefficient of earth pressure of one should
be used in the calculations. This leads to an automatic doubling of the predicted lateral load
capacity relative to that originally proposed by Terzaghi.
Considering all of the proposed methods, one point is clear. The end result is not simply
a product of using one of the assumptions about failure surface or coefficient of lateral earth
pressure. The final result reflects a combination of the type of failure surface, the lateral earth
pressure coefficient, and the factor of safety applied. Debate about one or the other of the
factors on an independent basis is somewhat artificial since all of them are linked.
2.5 Finite Element Analysis Capabilities
Conventional design methods for cellular cofferdams typically consider analyses for inter-
lock tension, vertical shear and overall stability independently, and none of the existing pro-
cedures predict cell movements and deflections. Although Schroeder and Maitland (1979)
modified design procedures few years ago, most of the design techniques were developed
more than 30 years ago, and the different methods often lead to considerable differences in
results.
BACKGROUND 22
2.5.1 Early Investigations
In the late 1960s, the finite element method was finding application to problems involving
soil-structure interaction because it could be used to consider the soil and the structure as a
single unit, and predict deformations as well as structural loads and behavior. It was not until
the mid 1970s that investigators began to experiment with the finite element method for
cofferdams. Kittisatra (1976) proposed to analyze the problem of cell filling using an
axisymmetric model {Figure 2.6). His results were interesting, but did not appear to be real-
istic, a finding which probably results from the fact that his model was limited. Kittisatra as-
sumed that the cell was a perfect pressure vessel, the soil was a linear elastic medium, and
that no deformations occurred between the fill and the cell walls as the backfill was placed.
Clough and Hansen (1977) and Hansen and Clough (1982) proposed the use of "vertical
slice" plane strain type of analysis to approximately model the effects of cell filling, dewatering
and interior excavation at the Willow Island cofferdam located on the Ohio River. Circular and
cloverleaf cells were considered in the analyses. Internal springs were used to connect the
front and back wall of cofferdam {Figure 2.6). Spring stiffnesses were designed to represent
the connecting effect exerted by circular cell shape. The soil in the cell fill and foundation was
assumed to behave as a nonlinear medium and slippage between the cell walls and the soil
was allowed by the use of special interface elements. Stevens (1980) extended the vertical
slice model idea of spring elements by his proposal to reduce the internal spring stiffnesses
from those of the of the perfect pressure vessel to allow for interlock yielding and slack.
While the analyses using the vertical slice model gave reasonable predictions of general
cell deformation and overall behavior, they provided no rigorous accounting for any form of
three-dimensional interaction between the cell. Thus, the interactions at common walls be-
tween cells and at critical connection points could not be checked.
BACKGROUND 23
AXISYMMETRIC MODEL
VERTICAL SLICE MODEL
HORIZONTAL SLICE MODEL
[QuiPOl•ftti•I lines (typ;"''
Figure 2.6. Finite element models (from Shannon and Wilson, 1982).
BACKGROUND 24
2.5.2 Lock and Dam 26 (R) Cofferdam Studies
In the early 1980s, the U.S. Corps of Engineers proposed to apply the finite element method
to the analysis of the Lock and Dam 26 (Replacement) cofferdam. This cofferdam was signif-
icant because it was to be one of the largest in the world, and it was to be instrumented, al-
lowing for evaluation of the observed behavior against that predicted. The location for the
cofferdam is on the Mississippi River at a site about 20 miles upstream from St. Louis,
Missouri. The cofferdam is described in the publications by Shannon and Wilson (1982),
Moore and Kleber (1985), and Clough and Kuppusamy (1985). Details of the cofferdam will
be given later in this document as it is used in a number of test analyses herein. For purposes
of introduction, the cofferdam was conceived of as consisting of three stages. The first stage
was built in 1982, and work with it was completed in 1985. The second stage was built in 1986
and is presently in place. The third stage is to be built in 1989. In stage one, the cells were
approximately 63 ft. in diameter, and stood 60 ft. above the mudline of the river. Stage two
cells have the same diameter as the first stage, but on the average, the cells are 80 ft. above
the dredge line for stage two. The sheet piles for the cells consisted of U.S. Steel Designations
PS-32 for the main and arc cells, and PSX-32 for the common walls. In the stage one
cofferdam, the sheet pile penetrated some 35 ft. into the riverbed. Foundation soils consisted
of medium-dense to dense sands. The cell fill was obtained from the riverbed sands, and was
clamshelled into place in the cell.
The instrumentation effort was primarily focused on the stage one cofferdam. Many types
of measurements were made, and the monitoring was done frequently. Stage two behavior
was monitored mainly through the use of a survey net aimed at measuring top of cell move-
ments.
BACKGROUND 25
The initial finite element analyses of the cofferdam consisted of two-dimensional models,
and these were unique in that three different approaches were used in an attempt to gain an
insight to all of the important facets of the cofferdam behavior. Details are given by Shannon
and Wilson (1982), Clough and Kuppusamy (1985). and Kuppusamy et al. (1985). Of the three
approaches, two were the previously described axisymmetric and vertical slice analyses. The
third was a new analysis which is termed the horizontal slice, or the generalized plane strain
model. Schematically, this is shown in the right-hand portion of Figure 2.6 as consisting of a
horizontal slice cut through the cofferdam. It will be described subsequently. All of the
models, schematically shown in Figure 2.6, were handled using three different versions of the
program SOILSTRUCT, developed by Professor G. W. Clough and his co-workers to analyze
soil-structure interaction problems. In all three analysis types, allowances were made for
sequential staging of the loading, non-linear soil behavior, slip of the soil on the interface be-
tween the soil and the sheet piles, and yielding in the interlocks of the sheet piles.
The vertical slice model used for the initial studies of Lock and Dam 26 (R) was similar to
that first proposed by Clough and Hansen (1977), except that provisions were made for sheet
pile interlock yielding. Stevens (1980) first recognized that there was a need for extra flexi-
bility in sheet pile systems due to slack and yielding in interlocks and made reductions in
connector spring stiffness. To represent this behavior, Clough and his co-workers proposed
an E-ratio concept for Lock and Dam 26 (R) studies, where the E-ratio is the ratio of the re-
duced horizontal modulus to that of steel. In the axisymmetric analysis, the sheet pile system
was treated as an orthotropic shell with reduced modulus in radial direction. In the vertical
direction, the steel modulus was used. This will be discussed in more detail later. In the
vertical slice analyses, the stiffnesses of the connecting springs were reduced by amounts
based on the E-ratio concept for case of cell filling. Based on case history analyses, it was
concluded that the appropriate E-ratio for a typical cofferdam lies between 0.1 and 0.03 for cell
filling. It was also observed that predictions using an E-ratio of 0.03 reasonably modeled the
average observed behavior for the Lock and Dam 26 (R) stage one cofferdam. Subsequently,
BACKGROUND 26
interlock connection testing of PS32 and PSX32 sheet piles was performed by Barker et al.
(1985), substantiating that the average E-ratio was 0.03 during filling.
It was judged by Clough and Kuppusamy (1985) that after cell filling, much of the interlock
deformation and sheet pile re-alignment should have occurred. Thus, they proposed that an
E-ratio of one was appropriate for loading after filling for the vertical slice analysis.
The new horizontal slice model was proposed to provide a means of analyzing the inter-
action between main and arc cells. A horizontal slice is cut through the cofferdam system at
some level above dredge line {Figure 2.6). This approach assumes that a constant strain ex-
ists in the out of plane direction. generated by the vertical gravity loads above the plane.
Horizontal load effects are generated automatically as a part of the analysis. The analysis
provides results on interlock tensions and cell deformations for the main and arc cells, the
common wall, and the critical wye section where the two cells are joined. This model cannot
account for the lateral support of foundation soils, and thus is applicable only for the upper
two-thirds or so of the cells where the dredge line effects have little influence. In this ap-
proach, only the horizontal response of the cells is considered, and the modulus of the sheet
piles was reduced to accommodate the E-ratio effect.
In all the Lock and Dam 26 (R) analyses. the soil behavior was simulated by a nonlinear.
elastic stress-strain response (Figure 2.7). The model followed similar lines of response to
that described by Duncan et al. (1980). The modulus at any point on the nonlinear loading
portion of the stress-strain curve is defined as the tangent of a hyperbola which fits the curve.
The shear and bulk modulus values of the soil were varied to accommodate the changes in
shear and confining stresses, which occur during the step-by-step simulation of construction
loading process (Clough and Kuppusamy, 1985). The modulus of each element in the mesh
was modified after each step of loading, and the entire stiffness matrix reformulated.
BACKGROUND 27
f O"' C\J
L&J (.) z L&J a:: w u. u. 0 (/) (/) L&J a:: ..... (/)
...J
ci: (.) z a:: a.
BACKGROUND
PRIMARY LOADING
UNLOAD-RELOAD
STRAIN
Figure 2.7. Non-linear stress strain behavior of soils.
28
The predicted behavior for Lock and Dam 26 (R) cofferdam stage one allowed comparisons
of the different models and of the models to the observed behavior. In the model to model
comparison, the case of cell filling was used since all three were applied for this stage.
Comparison of the axisymmetric and vertical slice results for cell filling is given in Figure 2.8,
where interlock forces and cell denections are given for the final filling stage of the cofferdam.
It can be seen that the two different analyses produce very comparable results. The cell wall
denections show the cofferdam to exhibit a bulging profile with the maximum radial denection
occurring at a position above the mudline. The interlock forces follow this same general trend
as they should since the interlock forces are proportional to the cell deflections in the filling
stage. Similar comparisons between the horizontal slice model results and those of the other
two are given by Kuppusamy et al. (1985), where it is shown that for the main cell, the three
different models yield similar results. No comparisons are made for the predictions of hori-
zontal slice model for the arc cells and the common wall, since only the horizontal slice model
is capable of analyzing for these conditions.
The Shannon and Wilson (1982) report gives comparisons of the various finite element
model predictions for interlock forces for cell filling and those obtained from conventional
interlock force procedures (Figure 2.9). Of the conventional methods, those of Schroeder and
Maitland (1979) and TVA yield a distribution similar to that predicted by the finite element an-
alyses. In this case, the interlock forces first increase with depth below the cell top, and then
break and decrease in the area near the mudline. The other conventional analysis procedures
predict interlock forces increasing continuously to the mudline. In terms of magnitudes of the
interlock forces, the finite element predictions of the E-ratios of 0.03 and 0.1 fall between those
of Schroeder and Maitland (1979) and the TVA procedure.
Comparisons of the interlock forces from the finite element predictions to those observed
showed a reasonable agreement. There was considerable scatter in the observed data, and
BACKGROUND 29
QI )> n ,.. Ci') ::u 0 c z c
w 0
Interlock Force(Kip/in) Horiz.Deflections(ln.)
430° 2 4 6 430° 1 2 3 4
420 420
~ 410 ~ 410 (.!) (.!)
\ z W.T. ~ 400 I W.T.
- 400 + µ I µ C1I \
C1I C1I C1I
t. 390 I t. 390 c: \ c: 0 I 0
-r-l j •.-4
~ 380 µ
I Ill 380 :> /
:> C1I C1I
...... r-1
w 370 w 370
I Axisymmetric t
360 rr /•rt ical slice 360 11 r-Vertical slice1 350 ~ I 350 f
I I
340 11 J j 340 I
I I I I I I I J L I
Figure 2.8. Comparison of results from axlsymmetrlc and vertical slice analyses for cell filling (from Shannon and Wilson, 1982).
Interlock Force Kips/inch
420
410
~ 402 SJ.-cu 400 cu
......... ...... '
fa.
c: 390 E-Ratio= 0 • 03
~
c: 0 380 ~
~
co > cu 370 ..-4
fzl
360
350
340
Legend
--- Schroeder ----~Axisymrnetric FE Analysis --- Terzaghi ------TVA - --Corps of Engineers -·-·-DM-7
Figure 2.9. Comparison of Interlock forces predicted by various methods at the end of cell filling (from Clough and Kuppusamy, 1985).
BACKGROUND . 31
the finite element models tended to give interlock forces that agreed well with the average
results.
Of the two-dimensional models used in the initial studies of the Lock and Dam 26 (R)
cofferdam, only the vertical slice is able to predict behavior for loadings beyond filling. Figure
2.10 gives predicted wall displacements for a series of loading stages after cell filling. Com-
parisons to observed behavior showed that there was general agreement with the predictions
in qualitative response, but that magnitudes of movements were only approximately modeled.
Clough and Kuppusamy (1985) suggested that better predictions could be made if the shear
transfer mechanisms from one side of the vertical slice model to the other could be improved.
Following the initial finite element investigation for Lock and Dam 26 (R), additional studies
have been performed aimed at this project. One of these involved two-dimensional analyses
to determine the effect of depth of penetration of the sheet piles. This led eventually to the
use of lessened penetrations of the second stage cofferdam. In addition, an effort was
undertaken to develop a three-dimensional finite element model for the cofferdam by R.
Mosher at the Waterways Experiment Station. Results from this study are in the process of
being published and will be covered later in this document as a basis for comparison to the
new two-dimensional models used herein (Clough et al., 1987).
2.6 Summary and Recommendations
The conventional design methods for cellular cofferdams were largely developed over 30
years ago. Recently, Schroeder and his co-workers have proposed significant modifications
to the conventional methods that lead to less conservative results than those of the older
technology.
BACKGROUND 32
GI
~ ~ a ::0 0 c z g
w w
0 > (!) z • t;j
L&J ..... z z 0 ~ ~ ~ L&J
Lateral Deflection of Inboard SldeWall,ln. Lateral Deflectlon of Outboard Side Woll, in. 430 4 3 2 I . I I ' I
I I
4201- I ,, I
I I
410 I I
I I
I 400 I
I I \
390 \ \ \ I ~d Sldt \
\ \ 380 ,, \~ ....... .... ' 370
........ '
380~ Outboard Side
I
Inboard~
3!10
340
0 0 I 2 3 ~ 1430 ------'T"'----,1 WI R M I I
\
' ' 420
410
400
390
380
Drtde• Lint II / _,,,,, I 310
I If( I~~/ - Complttlon of cell flll
///J -· Completion of btrn fl II
I - Dtwoterln9 - Eacovotlon - Flood W.T. El 428
360
3!10
340
Figure 2.10. Vertical slice analysis, sheet pile deflections for different construction stages (from Shannon and Wilson, 1982).
The basic design procedures for cofferdams assume that the problem is to be divided in
two parts which are analyzed independently of each other. Thus, cell filling is treated as one
case, and differential lateral loading as another. In each situations, earth and water loadings
are assumed, and applied to the structure without a formal consideration for the effects of
soil-structure interaction. None of the existing methods have a technique for predicting def-
ormations and deflections of the cells. This latter deficiency is important in that safety
instrumentation for cofferdams is largely directed at measurement of movements.
Finite element procedures offer the possibility of dealing with the cofferdam system as a
soil-structure unit, and providing the means to predict cofferdam movements and cell de-
flections. To date, three two-dimensional finite element models have been proposed for
analysis of cofferdam structures - axisymmetric, vertical slice and horizontal slice. Also, a
new three-dimensional model is being developed at the U.S. Army Engineers Waterways Ex-
periment Station.
The two-dimensional models will remain the primary analysis tool, however, because of
their relative simplicity and ease of application. The two-dimensional finite element analysis
methods were developed primarily to meet certain job-specific needs. As such, they are in
need of improvement. This review of the previous work suggests that the following refine-
ments in the two-dimensional model are needed:
1. Provision of a shell element in the existing axisymmetric finite element program to model
the sheet pile thickness exactly and avoiding the need for reducing modulus value as is
presently done using one-foot thick two-dimensional elements.
2. Inclusion of a beam element in the existing vertical slice finite element program to model
the sheet pile thickness exactly and avoiding the need for reducing modulus value as is
presently done using two-dimensional bending elements.
BACKGROUND 34
3. Incorporation of a continuous load transfer element to represent the "missing" part of the
cell in the vertical slice analysis as opposed to the use of discrete springs.
The review of the literature also shows that there is a need for studies which can be used
to test proposed conventional methods of analysis of cofferdams, and to possibly provide in-
formation that can be used to predict deflections and movements of cofferdams. Areas which
appear to be useful to study through finite element parametric study include:
1. Effects of depth of sheet pile embedment, cell height, and properties of the cell fill and
foundation soils on movements and interlock forces.
2. Simplified methods to predict movements of cell walls during cell filling and differential
loadings.
3. Potential failure mechanisms in the cell fill during lateral loading.
4. Lateral earth pressure conditions in the cell fill during lateral loading.
BACKGROUND 35
Chapter Ill
AXISYMMETRIC VERSION OF FINITE ELEMENT
PROGRAM {SOILSTRUCT)
The program SOILSTRUCT was originally developed by Clough (1969) for plane strain
analysis of soil-structure interaction problems. In the early 1980's, it was modified by Clough
and his co-workers for axisymmetric analysis so that it could be used to study the effects of
filling of an isolated cofferdam cell (Clough and Kuppusamy, 1985). Radial, tangential and
vertical sheet pile deflections and stresses can be predicted along with profiles of sheet pile
deflections and stresses of the cell fill and foundation soils. In this version of the program, the
sheet piles are modelled by one-foot thick, four-node solid element having two degrees of
freedom at each node. A thickness of one foot was chosen from the aspect ratio point of view
to avoid numerical problems. The modulus value for the sheet pile is reduced in certain
proportion of the ratio of area of one-foot thick element and that of actual sheet pile. The
four-node solid element used for steel sheet piles, however, cannot take into account the true
bending characteristics of the sheet piles, and has thickness greater than that of the actual
sheet pile.
AXISYMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 36
To circumvent these problems, the existing axisymmetric version of SOILSTRUCT was
modified in this work to incorporate a shell element for modelling the behavior of sheet piles.
This allows the thickness of shell element to be taken the same as that of sheet piles. Three
degrees of freedom (i.e., axial and radial displacements and rotation) are considered at each
shell element node to account for the bending characteristics of sheet piles. The modification
of the program to include a shell element also provides compatibility with a three dimensional
code developed by Mosher (1987).
3.1 Modification in Axisymmetric Finite Element Program:
Provision of Shell Element
The existing axisymmetric version of SOILSTRUCT finite element program was modified to
incorporate the two-node shell element described by Zienkiewicz (1977). Each node has three
degrees of freedom.
For a thin cylindrical shell (Figure 3.1), the three strain components are given the following
expression:
AXISYMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 37
(a) Displacements and Stresses
( b) A Shell Element
Figure 3.1. A thin cylindrical shell.
AXISYMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 38
where: E, = Axial strain
E9 = Hoop strain
x, = Rotation
v = Axial deformation
w = Radial deformation
r = Radius of cylinderical shell.
The corresponding stress resultants are:
{cr} -[ ~ ]- (D]{t}
where [DJ is elasticity matrix.
For isotropic shell:
1 v 0
[DJ= E.t v 1 0 1 - v2 t2
0 0 12
where: E = Modulus of elasticity
t = Thickness of shell
v = Poissons ratio .
For an orthotropic shell consider:
E1 = Value of modulus of elasticity in axial direction
E2 = Value of modulus of elasticity in circumferencial direction.
According to Goodman (1980):
AXISYMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 39
V12 = Vz1 or, E1 Ez
where: v11 determines normal strain in symmetry direction j when stress is added in symmetry
direction i.
For an orthotropic shell, the matrix D becomes:
E1t V12E2t 0
1 - V12V21 1 - V12V21
[DJ= V21E1t E2t 0
1 - V12V21 1 - V12V21
0 0 E1t3
12(1 - V12V21)
and
E - Ration = Ez!E1
1 nv12 0
[DJ = E1t nv12 n 0
(1 - V12V21) t2 0 0
12
if V12 = V21 = v I
AXISYMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 40
1 nv 0
[O] = E1t nv n 0
(1 - v2) t2 0 0
12
The shell element with two nodes, i j, possesses six degrees of freedom determined by the
element displacements:
where a,= [;]
The displacements within the element have to be uniquely determined by nodal displace-
ments a• and the position s, and maintain slope and displacement continuity.
In local coordinates, we have:
If v is taken as varying linearly with s and w as a cubic in s:
v = <11 + <1zS
r.t.=(dw). and r.t,=(dw). ,.,, ds ' ,., ds 1
AXISVMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 41
w,
~j
Where, S' = SIL
or {u} = [NJ {q}.
The strain components are:
Where,
0 -1/L 0 0 1/L 0
[8] = 1 - 3S'2 + 2S,a J:..(S' - 2S'2 + S'3) (3S'2 - 2S'3) .!;-( -S'2 + S'3) r 0 r 0 r r (6 - 12S')
0 (4 - 6S') ( -6 + 12S')
0 (2 - 6S')
L2 L L2 L
The stiffness matrix K becomes:
dA = 2nrds = 2nrLds'
AXISVMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 42
Where: S' = SIL
S' varies from 0 to 1
K = 2nrjJ(BTDBL) ds' n
or, K = 2nr I, H/(a) 1-1
For numerical integration of the above equations, the following formulae has been used to
change integration limits from a to b to -1 to 1:
b b - a n Z;(b - a) + b + a faf(x)dx = 2 _L W; f( 2 ) J, 1=0
In our case a=O and b=1.
The two-point integration has been used. For two-point integration:
f1f(x)dx = j_[1 x f{ (0.577350269189626 x 1) + 1} + 1 x f{ ( -0.577350269189626 x 1) + 1 }] JO 2 2 2
= ~ [f(0.788675124594813) + f(0.211324865405187)]
The above values are used in the finite element program to compute the shell element
stiffness matrix K.
AXISYMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 43
3.2 Test Problems to Check Shell Element
Two test problems were solved using the modified finite element program to check the
accuracy of implementation techniques for the shell element in the program.
3.2.1 Test Problem 1
Consider long cylindrical shell subjected to uniform internal pressure (Figure 3.2). Ac-
cording to Timoshenko and Krieger (1970), the closed form solution for deflection and hoop
stress at center are:
w = pr2/Eh
O'r = pr/h
where: w = Radial deflection at center
O'r = Hoop stress at center
We assume for an example:
p = Internal pressure = 1000 psf
r = Radius of shell = 4.0 ft.
E = Modulus of elasticity for shell = 4.32 x 109 psf
h = Thickness of shell = 0.042 ft. (0.5 inch)
Based on closed form solution, the radial deflection and hoop stress at center are:
w = (1000 x 16)/(4.32 x 109 x 0.042) = 0.88 x 10-4 ft.
and O'r = (1000 x 4)/0.042 = 0.95 x 105 psf.
AXISVMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 44
i I - 10 . I 9 -I
8 . -- 7
- 6 9 she 11 elements 1000 ~ 5 @ 4.0 ft each
- 4
- 3
- 2
-'"' 4.0 ft,,
Figure 3.2. Test Problem 1, long cylinder subjected to Internal pressure.
AXISYMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 45
Using finite element program, the predicted radial deflection and hoop stress at center of
the cylindrical shell are 0.85 x 10-4 and 0.96 x 105 psf, respectively, which match the closed
form solution very well.
3.2.2 Test Problem 2
Consider a cylindrical tank with hydrostatic pressure inside (Figure 3.3). According to
Timoshenko and Krieger (1970), the closed form solution is:
w" = y(d - x)r2/Eh
<rt" = y(d - x)rlh
where: w" = Radial deflection at distance x from bottom
<rt = Hoop stress at distance x from bottom )(
We assume for an example that:
y = Unit weight of fluid = 100 psf
d = Height of tank = 36 ft.
r = Radius of tank = 4.0 ft.
E = Modulus of elasticity = 4.32 x 109 psf
h = Thickness of the wall of the tank = 0.042 ft. ( = 0.5 inch)
The deflections and hoop stresses using the closed form solution and predicted by the ti-
nite element program are given in Table 3.1. These results indicate that the finite element
predictions are consistent with the closed form solutions.
AXISYMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 46
~ ,-' I I I I I I i i 4.0 ft -i I•
10
9
8
7
6
5
4
3
2
9 shell elements @ 4.0 ft each
Figure 3.3. Test Problem 2, cylindrical tank with hydrostatic pressure.
AXISYMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 47
Table 3.1
Predicted Deflections and Hoop Stresses in a Hollow Cylinder
Distance from Radial Deflection Wx Hoop Stress at Bottom (x) (ft.) (ft.) (psf)
Closed Form FEM Closed Form FEM
6.0 0.2857 x 1011 0.259 x 1()6
8.0 0.2469 x 10-3 0.2541 x 10-s
10.0 0.247 x 1D6 0.244 x 1D6
22.0 0.1333 x 108 0.133 x 1()6
28.0 0.706 x 10-• 0.704 x 10-•
30.0 0.5714 x 1D6 0.576 x 1a5
32.0 0.3528 x 10-• 0.350 x 10-•
AXISVMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 48
3.3 Problem of Interaction of Shell Element with
Two-Dimensional Elements in Program SOILSTRUCT
As shell element nodes have three degrees of freedom and two-dimensional soil element
nodes have two degrees of freedom, this results in incompatibility between two elements.
This incompatibility will have insignificant effect on deflections. However, the rotation and
bending moments obtained from the results of analyses are incorrect. To check the deflection
results using shell elements along with two-dimensional solid elements, a case history is an-
alyzed in the following section.
3.4 Case History Analysis Using One-Foot Thick Solid
Element and New Shell Element for Sheet Piles
3.4.1 Case History
Lock and Dam 26 (R) stage one cofferdam was considered for analysis because this re-
presents a typical size cofferdam and was well instrumented. Details describing this
cofferdam are given in Shannon and Wilson (1982) and Moore and Kleber (1985). Figure 3.4
depicts the basic conditions for Lock and Dam 26 (R) stage one cofferdam. The cofferdam
cells are approximately 63 feet in diameter and 60 feet high above dredge line. The
embedment depth of sheet piles is about 35 feet. The cells were filled by dumping riverbed
sands with a clamshell. The foundation soil is medium to dense sand. Same soil parameters
AXJSYMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 49
as used in previous analyses and described in Shannon and Wilson (1982) were considered.
These are given in Table 3.2. The water level during cell filling was 32 feet above dredge line.
The sheet piles for main cell consisted of U.S. Steel designation PS-32.
As per previous analyses, the soil was modelled as nonlinear material following a
hyperbolic elastic model as described by Duncan et al. (1980). The modulus at any point of
nonlinear curve is defined as:
where: Er = stress dependent tangent modulus
E; = initial tangent modulus
R, = curve fitting parameter
SL = stress level or ratio of the present value of principal stress difference to that at failure
For most soils, R, is in the range of 0.8 to 0.9.
where: Km = modulus number
P. = atmospheric pressure
n = modulus exponent
crc = confining stress .
If unloading or reloading occurs, then the response is assumed to be linear and defined
AXJSYMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 50
,.. 63 ftr--+f
' . 60ft. Cell fill
. . . . T T 28ft. 1
. . •' Alluvial Outwash ..l_ ~~-..P':r.l~:ir.'11:1- :..: :_: ~ -~ -~~-~ _· .. ·"""'*""'-'"'""-~,..,,.,,..,< .... s ....... an .... a...-· • .... r ..... >__,,.....,..-
12 ft. T -------1---------2a ft.
t 30 ft.
35ft. l_
Wisconsin Outwash (Sand II)
Illinoisan Ice Contact (Sand III) J_
... >::>:> >>.» >:?7~/,?.??77 4/,,..,,,-,,,,.;» ./,/,,,,.;r,..,.;?/ff /,//7.//////.,?.///,//////,/7//77.¢
ROCK
Figure 3.4. Lock and Dam 26 {R) cofferdam, basic conditions.
AXISYMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 51
~ (I) -< 3: 3: m ~ n < m :u (It
0 z 0 "" ::!! z =i m m r m 3: m z -I "V :u 0 C') :u ,,. 3: (ii Q r (It -I :u c (') .:j
"' N
Table 3.2
Soil Parameters for Finite Element Analyses of Lock and Dam 26 (R)
SOIL PROPERTIES
Total Unit Friction
Weight Poisson Angle y Ratio cp Cohesion
Material (pcf) v (degrees) c
Cell Fill 123 0.45 35.0 0.0
Foundation 133 0.45 41.0 0.0 (alluvial outwash)
Foundation 133 0.45 41.0 0.0 (Wisconsin outwash)
Foundation 133 0.45 41.0 0.0 (lllinoisian ice contact)
NOTE: For foundation soil profile, see Figure 3.4.
•km = coefficient in the initial tangent modulus expression E; = P.Km<.!!!.r P.
•Kur = coefficient in unload-reload modulus expression Eu, = P.Ku,( ~3 )n •
·n = exponent in modulus expression
Earth Pressure
Coefficient Ko
0.4
0.6
0.5
0.5
•Rf = strength factor: ratio of measured strength at failure to ultimate hyperbolic stength.
HYBERBOLIC PARAMETERS
Km•
800
1600
1700
1700
Kur•
800
1600
1700
1700
n·
0.65
0.5
0.5
0.5
Rf*
0.82
0.85
0.85
0.85
by the modulus value Eur , which is calculated as:
where: Kur = unload-reload modulus number .
3.4.2 Previous Predictions and Observed Behavior
The previous axisymmetric analyses for cell filling for Lock and Dam 26 (R) cofferdam
performed by Clough and Kuppusamy (1985) used one-foot thick solid element to model sheet
piles. To take into account the slack and yielding of interlocks, the sheet pile system was
modeled as orthotropic shell with reduced modulus in radial direction using E-ratio concept.
E-ratio is defined as ratio of modulus in radial direction to steel modulus, and values of 1, 0.1
and 0.03 were used in analyses. The predicted radial denections and interlock forces at the
end of main cell filling using E-ratio of 0.03 are shown in Figure 3.5. The results show that the
denection and interlock force increase to a depth of about one fourth the height of the cell
above dredge line, whereupon they decrease. The maximum denection and maximum inter-
lock force for E-ratio of 0.03 are approximately 3 inches, and 3.5 kip/inch, respectively.
3.4.3 Predictions Using New Shell Element
The finite element mesh used for axisymmetric analyses using the new shell element is
shown in Figure 3.6. As an E-ratio of 0.03 predicted results more consistent with observed
data during previous analyses, this was also used for analyses using shell element. As sheet
piles are modeled using shell elements, the E-ratio in this case is defined as ratio of
circumferential modulus to steel modulus. The predicted radial denections at the end of main
AXISVMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 53
~ (I) -< ii: s: m n < m :u (I)
0 z 0 "'II
::!! z =t m m r m ii: m z ~ .,, :u 0 () :u )> ii: (ii 0 ;::: (/) ~ :u c (') .d
UI •
Interlock Force(Kip/in) Radial Deflection(inches)
4309 2 4 6 430° 1 2 3 4 I I I I I I I
420 L \ J 420
410 0 410
~ ::> W.T. W.T. (.!)
:z:. 400 + ~ 400 I \ + -4-1 QI QI ~ ......,,
i:: 0 ..... 4-1 co > QI ~ f..t.l
-4-1 QI
390 QI 390 ~ ......,,
i:: 0 380 ..... 380 4-1 co :> QI rl 370 f..t.l 370 . . '
360 u J 360
350 ~ -/ 350
340 ... -l 340
Figure 3.5. Axlsymmetrlc analysis using one-foot thick element, sheet pile deflections and Interlock forces at the end of cell filling.
cell filling with the shell element and those obtained in three-dimensional analyses by Mosher
(1987) for an E-ratio of0.03 are given in Figure 3.7, along with the range ofthe observed values
for the two instrumented cells of Lock and Dam 26 (R) cofferdam - Stage I. The results of the
original analysis using the one-foot thick, solid element and E-ratio of 0.03 are also presented
in Figure 3.7 for comparison. All the analyses give qualitatively similar predictions. The new
analyses with shell elements match well with those obtained during previous axisymmetric
analyses using one-foot thick, solid element, and the observed radial deflections bound the
predicted values. The results of three-dimensional analysis show similar trend but yield lower
values as compared to those obtained from axisymmetric analyses. This discrepency is be-
cause three-dimensional analysis uses modified hyperbolic model for non-linear soil behavior,
taking into consideration the effect of intermediate principal stress. Also, the three-
dimensional finite element mesh includes the sheet pile system for arc cell also which will
have restraining effect on deflections of main cell during main cell filling.
The interlock forces for case of cell filling obtained from axisymmetric analyses (using
one-foot thick element and shell element). and three-dimensional analyses and those obtained
from instrumentation data (Moore et al., 1985) are shown in Figure 3.8. The results show that
the predictions of both axisymmetric analyses and three-dimensional analyses have similar
trends, and that they fall within the bands of observed data at almost all elevations. However,
three-dimensional analysis predicts lower interlock forces as compared to axisymmetric ana-
lyses for the same reason as explained above in case of radial deflections.
3.5 Summary
A shell element is incorporated in the program SOILSTRUCT to model sheet pile thickness
exactly for analyzing behavior of cofferdam cell during filling. Comparison of predicted results
AXISYMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 55
~ en ~ s:: ~ n :ii ::u en 0 z 0 "Tl
:!! z ~ m J;; s:: m z -f -a ::u g ::u )> s:: c;; 0 ;::
~ c 2
C.11 Ol
<t, CIRCULAR CELL 160 ft
i--31.5 ft ---t - El 430 ~ 7'.: ~ 1---shell Element 7" -I"." 7-r
7-
r- lnterf oce Elements on either side - of Shell Elements ., -;--::-~ ,... ;-, r-
·~ ~ -;-
hi ) ~ ) • h.t .. ,.~~ht h: )-,> h: ),;t hJ
l l
-=---~
-,..
--
). >
-El. 370 ( Ored~e I ine)
El. 300
Figure 3.6. Finite element mesh for axlsymmetric analyses of Lock and Dam 26 (R) cofferdam.
-t-w w lL.
z 0 t-~ w _J w
410.0
400.0
390.0
380.0
370.0
360.0
0 Axisymmetric Analysis With I ft thick element (£-ratio =0.03}
• Axisymmetric Analysis With Shell Element (£-Ratio= 0.03)
0 Three- Dimensional Analysis (E-Rotio=0.03}
Range of Observed Values
350.0 ... J----.L-----.......... --_ _._ ___ __.._ __ __. 0.0 2.0 4.0 6.0 8.0 I 0.0
RADIAL DEFLECTION (INCHES)
Figure 3.7. Lock and Dam 26 (R), sheet pile deflections at the end of cell filling.
AXISYMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 57
430.0
0 Axisymmetric Analysis With One Foot thick element
420.0 (E-Ratio=0.03)
• Axisymmetric Analysis With Shell Element (E-Ratio =0.03)
410.0 a Three-Dimensional Analysis ( E-Ratio•0.03)
1---i Observed Values
400.0 -..... I.LI I.LI u..
z 390.0 0 t-<t > I.LI ....J I.LI 380.0
360.0
350.0-----+--.&--------'---------"-----------------" 0.0 2.0 4.0 6.0 8.0 I 0.0
INTERLOCK FORCE (KIPS/INCH}
Figure 3.8. Lock and Dam 26 (R), Interlock forces at the end of cell filling.
AXISYMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 58
with closed form solution indicates that inclusion of shell element in the axisymmetric pro-
gram has been done properly. The predictions using new shell element to model sheet piles
generally match well with the results of previous axisymmetric analyses and three-
dimensional analyses.
AXISYMMETRIC VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 59
Chapter IV
PARAMETRIC ANALYSES WITH THE
AXISYMMETRIC FINITE ELEMENT PROGRAM
The new version of the finite element program which incorporates the shell element to
represent the sheet piles is used in this chapter to conduct parametric studies of the case of
filling of the cofferdam cell. The results of the analyses are compared to the predictions of
conventional methods for analyzing cofferdam response. The parameters considered in this
chapter are depth of cell embedment, free cell height above the mudline, and strength of cell
fill and foundation soils.
Lock and Dam 26 (R) stage one cofferdam is used as the base case for the analyses in-
asmuch as it represents a typical cofferdam designed to handle significant loads. An E-ratio
of 0.03 is assumed for the cell. It may be remembered that the cell embedment of the stage
one cofferdam for Lock and Dam 26 (R) was 35 feet, a relatively large value. For the
parametric studies, embedments of 0, 10, 20, 25 and 45 feet are also considered. Where the
free cell height for Lock and Dam 26 (R) was 60 feet, in the parametric studies, problems with
PARAMETRIC ANALYSES WITH THE AXISVMMETRIC FINITE ELEMENT PROGRAM 60
free cell heights of 40, 50, 60, 70, and 80 feet are analyzed. Finally, the effects of cell fill and
foundation sand strengths are considered in the use of friction angles of 35 and 41 degrees
at various times for both materials. The 35 degree case is representative of a medium sand,
while the 41 degree case is consistent with a dense sand.
4.1 Effect of Depth of Embedment on Sheet Pile
Deflections and Interlock Forces
The deflected cell shapes at the completion of cell filling for the three depths of
embedment, 10, 20, and 35 feet, are presented in Figure 4.1. As expected, in all cases there
is a bulging shape imparted to the cell, with the maximum lateral deflection of 3.03, 2.93, and
3.16 inches for depths of embedment of 10, 20 and 35 feet, respectively. Because of different
scales for cell geometry and cell deflection, it appears from Figure 4.1 that maximum lateral
deflections are occurring below dredge line, but it is not true. For depths of embedment of
10 and 20 feet, the maximum deflections occur at a point about one-fourth the height of the
cell from the mudline, and for the 35 feet embedment, at a point about one-sixth the height of
the cell above the mudline. Although there are similarities in the cell deflection patterns, it
can be seen in Figure 4.1 that there are differences. The lowest embedment case shows the
largest stretching of the cell bottom, a situation not unexpected in view of the fact that this
case should have the highest lateral stress imparted to the bottom of the cell. The highest
embedment case shows the sharpest reversal in cell curvature as the deflections penetrate
into the ground. This reflects the stiffening effect of the embedment, and the fact that little
movement penetrates to the bottom of the cell in this case.
PARAMETRIC ANALYSES WITH THE AXISYMMETRIC FINITE ELEMENT PROGRAM 61
.35 ft.
•
Hd is Depth of embedment.
-- lid
Hd _._,._ Hd
10 feet 20 feet
35 feet
Original sha?e of cell
11-.111-,,.-11-ir-11-k-x-x-x-JC. ·~·--·--·--·~·~·~·~-~·
Cofferddm Cell
l I
20.0ft. Scale :or cell geometry
2.0 inch Scale for cell de:lections
Figure 4.1. Deflected shapes of cofferdam cell at the end of cell filling.
PARAMETRIC ANALYSES WITH THE AXISYMMETRIC FINITE ELEMENT PROGRAM 62
The relative influences of cell embedment, and the presence of the open end of the cell
at full embedment lead to the maximum lateral cell deflections of the 20 foot embedment case
to fall in between those of the shallower and deeper embedment cases. In Figure 4.2, the
maximum radial deflection is plotted against depth of embedment, and it can be seen that the
smallest value occurs at 20 feet of embedment, although there are no great differences in any
case.
Due to the lateral cell deflection and the weight of the cell fill, the cell walls also undergo
a vertical movement. The vertical movement of the sheet piles are 1.1, 0. 7, and 0.4 inch for
the embedments of 10, 20 and 35 feet, respectively, as shown in Figure 4.1. Vertical movement
is higher for lesser embedments depth because of lower frictional resistance.
The lateral pressures acting on the interior of the cell walls for embedments of 10, 20 and
35 feet are shown in Figure 4.3. The pressures are very similar for all cases, and this is not
unexpected in view of the similarity in cell deflections for the different embedments. The
magnitude of Rankine's active earth pressure are also plotted in Figure 4.3 for comparison.
The lateral earth pressures acting on cell wall at the end of cell filling are approximately the
same as active earth pressures up to a distance of about H/5 above dredge line and there-
after, lateral earth pressure values are lower than active earth pressure values because of
embedment effects. Below dredge line, lateral earth pressures become higher because of
resistance of foundation soil against cell movement.
The maximum interlock forces are plotted versus depth of cell embedment in Figure 4.4.
As expected, there is not a large difference in the interlock forces, given that, as noted previ-
ously, there is not a large difference in lateral deflections or the earth pressures acting on the
cell walls. The lack of influence of cell embedment on interlock forces reinforces the idea that
cell embedment is provided for reasons other than for reducing interlock forces.
PARAMETRIC ANALYSES WITH THE AXISYMMETRIC FINITE ELEMENT PROGRAM 63
-Cll QJ .c 3.0 CJ c H .._,, c 0 ...... .i.J CJ 2.0 CJ
..-1 ...... E-Ratio 0.03 CJ 0 ..-1
C1l 1.0 ...... 'O
C1l ~
e :I e ...... x C1l ~ 0.0 10.0 20.0 30.0 40.0 50.0
Depth of Embedment (Feet)
Figure 4.2. Maximum sheet pile deflections at the end of cell filling.
PARAMETRIC ANALYSES WITH THE AXISYMMETRIC FINITE ELEMENT PROGRAM 64
....... ~ cu cu
130
120
110
100
e 90 i:: 0
-M ~ co > ~ 80 t>:l
70
60
50
40
0.0
W.T. -+
1.0 Lateral Earth Pressure
2.0
H is Free cell
Hd is Depth of
Hd 10
Hd 20 Hd 35
H/4 H/6
',~~' '-·~·, ...............
") ,.."'> ).- ...... , . " I.
I J I I I I . I I I I \
,,
(Ksf)
3.0
height
Embedment
feet
feet
feet
line
Figure 4.3. Lateral earth pressures against sheet pile at the end of cell filling.
PARAMETRIC ANALYSES WITH THE AXISYMMETRIC FINITE ELEMENT PROGRAM
4.0
65
E-Ratio 0.03 5.0 -..c:
(.) c:
H -0. 4.0 "" ::iG -(I) (.) M 0 ~
~ 3.0 (.) 0
.-l M (I) ~
c: H
e 2.0 § "" ~ co ~
1.0
0.0 l-~~~~L-~~~----11:---~~~--L~~~~--'-~~~~--' o.o 10.0 20.0 30.0 40.0 50.0
Depth of Embedment (Feet)
Figure 4.4. Maximum interlock forces at the end of cell filling.
PARAMETRIC ANALYSES WITH THE AXISYMMETRIC FINITE ELEMENT PROGRAM 66
There is one interesting issue related to the effect of embedment. Namely, is there a point
of fixity for the cell walls. As can be seen in the deflected cell shapes, the greater the
embedment, the less the bottom of the cell is deflected. In Figure 4.5, the lateral cell move-
ments below the dredge line are plotted against depth of embedment. There is an obvious
difference in the curvature of the embedded portion of the cell, depending upon the amount
of cell embedment. However, even for the case of 45 feet embedment, the bottom of the cell
is being deflected. Thus, for these cases, there is no point of absolute fixity for the cell.
The location of the point of maximum deflection and that for the maximum interlock force
is identical. As noted, this typically occurs slightly above the level of the mudline. In Figure
4.6, the location of the maximum deflection and interlock force above the mudline is plotted
against depth of embedment for the analyses performed in this study. The position of the
maximum of either parameter occurs at one-sixth to one-fourth of the free cell height above
the mudline. This location is similar to that reported for instrumented cofferdams with similar
conditions to those included in these analyses (Martin, 1987).
The interlock forces predicted by the finite element analyses can be compared to those
that are calculated by conventional design methods. This is done in Figure 4.7, where the
interlock forces calculated using the Corps of Engineers and the Schroeder and Maitland
procedures are plotted for Lock and Dam 26 (R) dimensions along with those determined us-
ing the finite element program. As has been shown in previous work by Clough and
Kuppusamy (1985), the finite element method typically predicts lower interlock forces than the
two conventional methods shown in Figure 4. 7.
PARAMETRIC ANALYSES WITH THE AXISYMMETRIC FINITE ELEMENT PROGRAM 67
.,, ,.. ::a ,.. 3:: m if c; ,.. z ,.. r-~ m en ;; ;! ;! m
~ c;; -< 3:: 3::
m c; .,, z =i m m r-m 3:: m z .... .,, ::a 8 ::a ,.. 3::
°' OJ
,-... ~ QJ QJ
i:z.. ._, ~
~ QJ a
'O QJ
.0 a ~
~ 0
..c ~
0.. QJ
Q
Sheetpile Deflections (Inches) line o.o 0.2 0.4 0.6 0.8 1.0 1. 6
0 ~ ;;;J;: ' --~..i-•.d-:1:-=,_...:!!..::-~1--..:= 'l: ......._.;;:;:c;:ll=-_ - - :=J_ - - - __ , __ - --
10
20
30
40
45
Hd is Depth of Embedment.
~ Hd = 10 feet
-·-·- Hd = 20 feet
---- Hd 35 feet
--·-Hd = 45 feet
Figure 4.5. Cell deflections below dredge line at the end of cell filling.
c:: 0 ~ ~ (J ...... <U ::i::
.-1 -..... <U x 0
~
E CO =' E <U ~ (J x ,... ca o L.,,. ..... ...:.:: 0 (J
0 c:: .-1 0 ,... ~ <U ~ ~
ca !:: (J H 0
....i""'
0.2
0.1
0.0 o.o 10.0
Free cell height H 60 ft
20.0 30.0 40.0 50.0 Depth of Embedment (Feet)
figure 4.6. Effect of depth of embedment on location of maximum cell deflection and Interlock force at the end of cell filling.
PARAMETRIC ANALYSES WITH THE AXISYMMETRIC FINITE ELEMENT PROGRAM 69
1-L&J La.I L&..
420.0
410.0
400.0
z 390.0 0
~ > La.I _J La.I 380.0
370.0
360.0
• Axisymmetric Analysis With Shell Element (E-Rotio s0.03)
~ Observed Values -- Corps of Engineers Method -Schroeder and Maitland
Method
350.09-~-+-~.._~~~..L-~~~...L-~~~-l-~~~.....J
0.0 2.0 4.0 6.0 8.0 I 0.0
INTERLOCK FORCE (KIPS/INCH)
Figure 4.7. Lock and Dam 26 (R), Interlock forces at the end of cell filling. Comparison of FE analysis and conventional design methods.
PARAMETRIC ANALYSES WITH THE AXISYMMETRIC FINITE ELEMENT PROGRAM 70
4.2 Effect of Free Cell Height on Sheet Pile Deflection and
Interlock Forces
Parametric studies were also performed for main cell filling using a problem following the
Lock and Dam 26 (R) history and soil conditions, to investigate effect of free cell height on
maximum sheet pile deflection and interlock force. The free cell heights used were 20, 30, 40,
50, 60, 70 and 80 feet. An E-ratio of 0.03 was used. The water level was considered at mid-
height of the cell above mudline. Maximum predicted radial deflection and maximum interlock
force values from the finite element analyses are plotted against free cell height in Figures
4.8 and 4.9. Values are shown for cell fill conditions with a friction angle of 35° (the base Lock
and Dam 26 (R) condition), and a cell fill with a friction angle of 41°. The effects of the cell fill
friction angle are covered in subsequent section.
These results show that maximum radial cell deflections and interlock forces show an in-
crease as free cell height increases. The relationship is approximately linear. Interlock forces
computed using Schroeder and Maitland method are plotted in Figure 4.10 against free cell
height along with those from the finite element method. In all instances, the Schroeder and
Maitland method yields higher values than those from the finite element analyses. For ex-
ample, for a cell height of 60 feet, the maximum interlock force computed based on Schroeder
and Maitland method is about 34% higher than that predicted by finite element method. No-
tably, the difference between the Schroeder and Maitland predictions and those of the finite
element method grow larger as the free cell height increases. The reason for this is that the
Schroeder and Maitland method does not consider the true nature of the soil-structure inter-
action process, and also the assumed location of maximum interlock force based on the
Schroeder and Maitland method is different than predicted by finite element analyses. The
PARAMETRIC ANALYSES WITH THE AXISYMMETRIC FINITE ELEMENT PROGRAM 71
-en G> ~ u c -c 0 ·.;: u .!?
4.0
3.0
':; 2.0 0
0 :0 0 a:: E 1.0 ::s E ·;c 0 ~
20.0 30.0 40.0 50.0
0 Cell fill cf> = 350
0 Cell fill "' = 41° Foundation material cf> =41°
60.0 70.0 80.0 Free Cell Height (Feet)
Figure 4.8. Effect of cell fill material on maximum sheet pile deflections at the end of cell filling.
PARAMETRIC ANALYSES WITH THE AXISYMMETRIC FINITE ELEMENT PROGRAM 72
-..c u c ........ a. ~
Q) u '-& ~ u 0 1: Q) -c
E ~
E )( 0 ~
0 Cell fill cp = 350
6.0 0 Cell fill cp = 410
Foundation material c/J =41°
5.0
0.0 --~~--~~~--~~~--~~~...__~~___,,~~~~ 20.0 30.0 40.0 50.0 60.0 70.0 80.0
Free Cel I Height (Feet)
Figure 4.9. Effect of cell fill material on maximum Interlock forces at the end of cell filling.
PARAMETRIC ANALYSES WITH THE AXISYMMETRIC FINITE ELEMENT PROGRAM 73
effect of maximum interlock force location becomes more pronounced as the cell height in-
creases.
Location of maximum cell deflection and maximum interlock force, as predicted by finite
element analyses, is plotted for different free cell heights in Figure 4.11 for a cell embedment
of 35 feet. This location remains constant at about 0.15 H from mud line for all values of cell
heights for depth of embedment of 35 feet.
4.3 Effect of Foundation Soil And Cell Fill Parameters on
Sheet Pile Deflection and Interlock Force
Parametric studies were also performed using the axisymmetric program varying the
foundation and cell fill soil strengths. The soil characteristics used were those given in Table
3.2, using friction angle <p = 35 and 41 degrees for both cell fill and foundation for different
analyses. The free cell heights used were 20, 30, 40, 50, 60, 70 and 80 feet. The E-ratio and
cell diameter were fixed at 0.03 and 63.0 feet, respectively. The water level in the cell was
assumed to be at mid-height from dredge line. The embedment depth of cell was 35.0 feet.
Maximum radial deflection and maximum interlock force values are plotted against free
cell height in Figures 4.8, 4.9, 4.12 and 4.13. Maximum interlock forces computed based on
Schroeder and Maitland method are also plotted for cell fill friction angles of 35 and 41 de-
gre~s in Figure 4.10. The following observations are made from these results:
1. The friction angle of cell fill has a significant effect on predicted deflections and
interlock forces (Figures 4.8 and 4.9). Increasing the fill friction angle from 35 to 41
PARAMETRIC ANALYSES WITH THE AXISYMMETRIC FINITE ELEMENT PROGRAM 74
-..c u c ........ Q. ~
Q) u '-if ..¥ u 0 '-Q) -c
E :l E )( 0 ~
6.0
5.0
4.0
3.0
0 Cell fill 4' = 35o
0 Cell fill cp = 41°
- FEM Predictions
-·-Schroeder and Maitland method
O.OL-~~~.&.-~~--1r.......~~---'~~~---'-~~~-'-~~~~
20.0 30.0 40.0 50.0 60.0 70.0 80.0 Free Cell Height (Feet)
Figure 4.10. Effect of cell fill material on maximum interlock force (FEM and Schroeder and Maitland method) at the end of cell filling.
PARAMETRIC ANALYSES WITH THE AXISVMMETRIC FINITE ELEMENT PROGRAM 75
c .Q -0 Q) --Q) :I: O-E >< ::J -eo ·- Cl) )( 0 0 ... :?if
0.3
0.2
Depth of embedment Hd=35 ft
H is Free cell height
-..:.:: 0 0 0.1 c.2 .2 ~ --oc o-
.3 ~ 0·~0L.o--3-o.1...o---4-10.-o--5.....JoL-.o--s-o..1....-o-----1~0-=.o:----a~o.o Free Cel I Height (Feet l
Figure 4.11. Effect of free cell height on location of maximum cell deflection and Interlock force at the end of cell filling.
PARAMETRIC ANALYSES WITH THE AXISYMMETRIC FINITE ELEMENT PROGRAM 76
-.,, CD .s= u c -c .2 -u .!! -... CD 0
.2 "O 0 a: E :I E ·;c 0 :E
4.0
3.0
2.0
0 Foundation cp = 35°
1.0 0 Foundation cf:>= 41°
Cell fill cp = 350
20.0 30.0 40.0 50.0 60.0 70.0 80.0 Free Cell Height {Feet)
Figure 4.12. Effect of foundation material on maximum sheet pile deflections at the end of cell filling.
PARAMETRIC ANALYSES WITH THE AXISYMMETRIC FINITE ELEMENT PROGRAM 77
-.J:: (J c
' a. ~
G) (J ... & ~ (J 0 ... G) -c
E :J E )( c ~
0 Foundation <j> = 35°
6.0 0 Foundation </> = 41°
Cel I Fi 11 </> = 35°
5.0
1.0
o.o--~~--~~~---~~~--~~~---~~~.__~~----
20.0 30.0 40.0 50.0 60.0 70.0 80.0 Free Cell Height ( Feet)
Figure 4.13. Effect of foundation material on maximum interlock forces at the end of cell filling.
PARAMETRIC ANALYSES WITH THE AXISYMMETRIC FINITE ELEMENT PROGRAM 78
degrees results in reductions of about 30% in maximum radial deflection and 35%
in maximum interlock force for all free cell heights.
2. The values of maximum interlock force from Schroeder and Maitland method are
higher than those predicted by finite element method for cell fill friction angles of
both 35 and 41 degress. The reduction in values from Schroeder and Maitland
method, using a cell fill friction angle of 41 degrees instead of 35 degrees is about
25% for all values of free cell height.
3. Changing the friction angle of the foundation soil type from 35 to 41 degrees has an
insignificant effect on maximum radial cell deflections and maximum interlock
forces (Figures 4.12 and 4.13.).
4.4 Discussion
The parametric studies presented in this chapter concern foundation and cell fill conditions
that are favorable for cofferdam performance. The soils are taken to be sands with high
strengths, and the cofferdam dimensions are within usual limits. For these circumstances, tile
analyses show that the most important parameters are free cell height and cell fill strength.
Within the limits of the parameters assumed, no unusual behavior trends are determined.
As has been observed in previous finite element studies, the depth of cell embedment is
not important to the maximum cell deflection or interlock force for the case of cell filling. Cell
embedment is governed by other considerations for cofferdam design. Also expected in the
analysis results is the finding that the finite element analyses predict lower interlock forces
than those obtained by conventional design methods. A new observation is that the conven-
tional design methods become more conservative relative to the finite element predictions as
PARAMETRIC ANALYSES WITH THE AXISYMMETRIC FINITE ELEMENT PROGRAM 79
the free cell height becomes larger. This could be significant in the design of future
cofferdams, and should be studied further.
PARAMETRIC ANALYSES WITH THE AXISYMMETRIC FINITE ELEMENT PROGRAM 80
Chapter V
PLANE STRAIN VERSION OF FINITE ELEMENT
PROGRAM {SOILSTRUCT)
The program SOILSTRUCT has been used to model response of a cofferdam due to cell
filling, berm placement, dewatering, excavation within the cofferdam, and flooding (Shannon
and Wilson, September 1982), in terms of a vertical slice analysis. In this case, the cofferdam
is visualized as a planar system. The cofferdam cells are depicted as if they consisted of two
walls separated by the main cell diameter with soil between the walls. To represent the effect
of the HmissingH part of the cells, Hansen and Clough (1982) proposed that the walls be con-
nected with one-dimensional spring elements (Figure 5.1). The springs can transmit only
tensile forces from the front to the back wall, thus they exert no restraint on the vertical
movement of the cell fill.
Stiffnesses of the spring elements were proposed to be determined from the response of
a cylindrical vessel subjected to an internal pressure (Hansen and Clough, 1982). In this ap-
proach, the sheet piles are modelled by one-foot thick, four-node solid element having two
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 81
Connection spring
Cell wall Cell wall
Cell fill
Foundation
Figure 5.1. Planar representation of cofferdam cell for FEM analysis (from Hansen and Clough, 1982).
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 82
degrees of freedom at each node. A thickness of one-foot was chosen from an aspect ratio
point of view to avoid numerical problems. The modulus value for the sheet pile is reduced
in certain proportion of the ratio of moment of inertia of one-foot thick element and that of
actual sheet pile. To model the effects of an orthotropic cell, the stiffness of the spring ele-
ments are varied in proportion to the ratio of radial modulus due to presence of interlocks to
the modulus of sheet piles.
5.1 Modifications in Plane Strain Finite Element Program.
The existing finite element program has been shown to reasonably predict many aspects
of cofferdam behavior. However, there are several factors which can be improved. These
relate to the representations for the cell walls and the structural connections for the front and
back walls. In the case of the quadrilateral, one-foot thick solid element used for the sheet
piles, there are questions about the equivalent modulus for sheet piles. The spring elements
which serve as the front and back wall connections also suffer from the following drawbacks:
• The spring stiffnesses are computed based on assumption of pressure vessel sub-
jected to uniform internal pressure, a situation not applicable during differential
loading.
• The springs take only longitudinal force and no transverse force. During differential
loading, however, both longitudinal and transverse forces are generated.
• With springs, the connection is only from outboard to inboard sheet pile. However,
in actual case, the stresses in the cell sheet piles would vary from outboard to in-
board side under differential loading.
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 83
To obviate these problems, the existing plane strain version of SOILSTRUCT was modified
to incorporate a new beam element and shear transfer element. The beam element is used
for modelling the behavior of sheet piles, and it allows the thickness of beam element to be
taken the same as that of sheet piles. Three degrees of freedom (i.e., longitudinal and trans-
verse displacements and rotation) are considered at each beam element node to account for
bending characteristics of sheet piles.
The shear transfer element used is a plane stress element to model load transfer during
differential loading. These elements are placed overlapping all the soil elements within the
cell for outboard to inboard side, and provide continuous connection from outboard to inboard
sheet piles independent of the soil elements and their nodes. The beam and shear elements
are described in more detail in following sections.
5.2 Provision of Beam Element
5.2.1 Description
The beam element used is a two-node element as described by Desai (1979). Each node
has three degrees of freedom. A beam element and nodal degrees of freedom are shown in
Figure 5.2.
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 84
Figure 5.2. A beam element.
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 85
5.2.2 Test Problems to Check Beam Element
Two test problems were solved using the modified finite element program to check the
accuracy of implementation techniques for the beam element in the program.
Test Problem 1
Consider a beam with three nodes, fixed at both exterior nodes and subjected to concen-
trated transverse load at central node (Figure 5.3).
The closed form solution for maximum deflection and maximum moment are:
w/3 8 max= 192E/
Mmax = ~ 8
where:
W = transverse concentrated load ( = 1000 lb)
I = length of beam ( = 8.0 feet)
E = modulus of elasticity for beam ( = 4.32 x 109 psf)
I = moment of inertia of beam ( = 0.667 ft~)
Using the above values, 8 max and Mmax are computed as 0.139 x 10-3 feet and 1000 lb.
ft, respectively. The predicted values of 8 max and Mmax using modified finite element pro-
gram are 0.09255 x 10- 3 and 1000 lb. ft., respectively, which match the closed form solution
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 86
4.0 ft.
1000 lb.
4.0 ft.
Width of beam = 2.0 ft.
Height of beam = 1.0 ft.
Figure 5.3. Test problem 1, beam with transverse load.
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCl) 87
very well.
Test Problem 2
A problem of beam on elastic foundation was considered. Length, width and thickness of
the beam was 60 feet, 1 foot and 6 inches, respectively, and a uniformly distributed load was
applied in central 8.0 feet length of the beam. A Winkler type foundation having support
springs with spring constant K as 10,000 lb/ft was assumed. The model used for finite element
analysis is shown in Figure 5.4.
The closed form solutions (Boresi et al., 1978) for deflections at distance 'x' from center
of load are:
(i) for 'x' lying within loaded portion
(ii) for 'x' on right hand side of loaded portion
where:
Yx = deflection of beam at x
q = uniformly distributed load (1000 lb/ft)
k = spring constant (10,000 lb/ft)
a = distance of point of deflection from left end of the load
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 88
"V
~ z m
~ > z ;!ii ::a en 0 z 0 "" ::!! z ~ m r m 3: m z .... "V ::a 8 ::a > 3: (ii 0
~ c ~
Oii co
!4:of I I I
Beam
4.0 ft . ...j I•
Load q~lOOO lb/ft.
Sprngs, K=lOOOO lb/ft
30.0 ft.
Figure 5.4. Test Problem 2, beam on elastic foundation.
b = distance of point of deflection from right end of the load
E = Young's modulus of elasticity of beam (0.432 x 109 psf)
I = moment of inertia of beam
The results (Figure 5.5) show that the predicted deflections match well with those obtained
from closed form solution.
5.2.3 Problem of Interaction of Beam Element with Two-Dimensional
Elements in Program SOILSTRUCT
As in case of shell element discussed in Chapter 3, the inclusion of beam element in
SOILSTRUCT program results in incompatibility between beam element nodes having three
degress of freedom and adjoining two-dimensional element nodes with two degrees of free-
dom. This incompatibility means that the resulting rotations and bending moments from the
analyses would be incorrect, but it will have insignificant effect on deflections. To check de-
flections using beam elements along with two-dimensional solid elements, results of analyses
are compared with previous analyses using one-foot thick solid element for Lock and Dam 26
(R) in the following section.
5.2.4 Comparison With Previous Results - Cell Filling Case
To test the accuracy of the beam element for a cofferdam problem, an analysis was per-
formed for main cell filling of Lock and Dam 26 (R) cofferdam. The results were compared
with those obtained from earlier analyses.
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 90
-0
~ z m
~ )lo z < m :u en 0 z 0 "'II
::!! z ~ m r m 3: m z -t -0 :u 0 C'> :u ,,. 3: en 0 ;:: ~ :u c (') d
co ....
-Ill Q) .c u i::
1-t ._..
13 <ll Q) al
~ 0
i:: 0
•r-1 ~
u Q)
...... ~ Q)
Cl
-0.1
o.o
0.1
0.2
0.3
0.4
0.5
0.8 I
Closed form solution
FEM Predictions
Original position of beam
I _____ L__ _ __ l__ _____J o.o 5.0 10.0 15.0 20.0 25.0 30.0
Distance From Center of Beam (Feet)
Figure 5.5. Test Problem 2, deflection of beam on elastic foundation.
The original plane strain analyses performed for main cell filling of Lock and Dam 26 used
a one-foot thick solid element to model sheet piles (Shannon and Wilson, 1982). The equiv-
alent modulus value used for PSX32 sheet piles was 7.0Sx1a6 psf for steel. The reduction
factor used was about 613 computed on the basis of El values of one-foot thick element and
actual sheet pile, where E and I are modulus and moment of inertia, respectively.
The finite element mesh using beam elements to model sheet piles is shown in Figure 5.6.
The mesh, as shown, is not symmetrical because the same mesh was used for analyses of
cofferdam behavior due to different types of lateral loading. The soil parameters used in both
cases are given in Table 3.2. The dimensions and details of cofferdam are as described under
Section 3.4.
The predicted sheet pile displacements from the previous analyses and those using beam
element to model sheet pile behavior for an E-ratio of 0.03 are shown in Figure 5.7 for com-
pletion of cell filling. The results of the two different approaches agree very well. It is im-
portant to note that Clough and Kuppusamy (1985) indicated that the sheet pile deflections for
cell filling using one-foot thick solid elements for sheet pile and E-ratio of 0.03 were in general
agreement with the observed behavior. This indicates, therefore, that the beam element op-
tion included in the finite element program yields results which are in conformity with the re-
sults of observed behavior for Lock and Dam 26 (R).
5.3 Provision of Shear Transfer Element
In this investigation, provisions are made to provide a connection of front and back
cofferdam wall in the vertical slice analysis, using a plane stress shear transfer element. A
four-node plane stress element as described by Zienkiewicz (1977) is used. This element has
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 92
I
I J
I
(l(I • OS I 00·001
0 0 0 U'I
"' 0 0 0 0 "' 0 0 0 Ill ::I'
0 0 0 0 ::I'
0 0 0 U'I
.... 0 0 0 0 .., 0 0 0 U'I
"' 0 0 0 C'
"' c r c~
• 0 Cl
c CJ
I ·' C.·
c' V
'
.... c.:
PLA
NE
STR
AIN
VERSIO
N O
F FINITE
ELE
ME
NT P
RO
GR
AM
(SO
ILSTR
UC
T)
-- c CP E
CP u IV a. CP ~
co N
E
IV 0 i::J c IV
.lJlf. u 0
..J .. 0 -.c Ill CP E
- c CP E
.
CP E -
IV CP i::J .! ; c=
_
o
u.. u
93
130
120
110
100
90 t-w w LL
z 80 0 t-
~ w _, w 70
60
50
40
E- Ratio= 0.03
o One fod thick solid e~me
a Beam element ( 1/i'thick)
Dredge line ......... aazxaw•W
1.0 2.0 3.0 4.0 5.0 DEFLECTION (INCHES )
6.0
Figure 5.7. Deflection of sheet pile at the end of cell filling, Lock and Dam 26 cofferdam.
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCl) 94
a thickness of unity in the plane strain analyses. The shear transfer elements are provided
as superimposed on to the cell fill elements and connecting outboard and inboard sheet piles
over the entire height of cell as shown in Figure 5.8.
5.3.1 Method of Computing Modulus (E) of Shear Transfer Elements for
Use in Analyses
For the plane stress shear transfer element introduced in plane strain analyses to repre-
sent the cofferdam behavior under lateral loading, it is necessary to determine the appropriate
modulus (E) value of this element based on some factor applied to the modulus value of steel.
Two modulus reduction factors were considered for this purpose:
1. First modulus reduction factor computed based on comparison of theoretical solutions
and results of linear elastic finite element analyses using different set of parameters.
2. Second modulus reduction factor derived from testing the program against case history
data, taking into account the non-linear behavior of cell fill and foundation soils and the
soil-structure interaction effects. This reduction factor would include the effects of inter-
lock slack and yielding and the three-dimensional effects during lateral loading.
In this chapter, the technique for determining first modulus reduction factor is discussed. In
Chapter 6, the case history studies are done to compute the second modulus reduction factor.
A case of thin, hollow cylinder having height as equal to free cell height of cofferdam and
diameter as equal to width of cofferdam cell in plane strain analysis was considered appro-
priate for comparing results of finite element analyses with closed form solutions. The bottom
of the cylinder is fixed, and a uniform lateral load is applied on full height of cylinder. To ob-
tain closed form solution, cantilever beam theory is used for cylinder. In finite element ana-
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 95
F"ront wa// of Cofferdam
Shear ,,., · Ot7 ansfer elem
lo Ctlf/ fit/ , en1s su/Je, . e1emen1s r'"'Posea ,,----
'( )'\. I ff 5ection
Figure 5.8. Isometric view of cell fill elements and overlapping shear transfer elements.
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 96
lyses, beam elements were used to model front and back sheet piles of hollow cofferdam, and
shear transfer elements used connecting outboard and inboard sheet piles. No soil or inter-
face elements were used in these analyses, and only linear elastic analyses were done. The
sheet piles were fixed at dredge line, and uniform lateral loading was applied in entire height
of cofferdam. The schematic representation of the cylinder and the cofferdam is shown in
Figure 5.9.
The horizontal deflections of the sheet piles at top, mid-height and one-fourth height (near
dredge line) from bottom were compared with closed form solutions using cantilever beam
theory for the cylinder. The deflections for the cylinder are computed as:
8 max= wh" BE/
and
Sx = ~(x" - 4h 3x + 3h4) 24EI
where:
8 max = maximum deflection at top
w = uniform distributed load over height h
I = moment of inertia of thin cylinder
E = modulus of elasticity
ox = deflection at distance x from top
r = outside radius of cylinder
r0 = inside radius of cylinder
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 97
"'D s;: _z m
~ ~ z ~ ::u (/I
0 z 0 'Tl 'Tl z ~ m r-m
== m z -t "'D ::u 8 ::u ,.. :!: en 0 ~ ;i c n
..::I
co 00
Loadw
B
Thin Cylinder H
(a) Thin Cylindrical Shell ( Closed form solution )
B ,. .,
Loadw
Sheet pile (Beam elements)
Load Transfer Shear clements
(b) Schematic Mesh for Finite Element Analysis
Figure 5.9. Schematic details of thin cylinder and finite element mesh.
The ratios of deflections from finite element analyses o,em and deflections obtained from
closed form theory Ot1reoty were computed at top, mid-height and near dredge line for particular
value of height (H) and width (B) of cofferdam cell and for different ratio of modulus of steel
(Es) and modulus of shear elements (Eshear) used in analyses. The values of H and B used
for this parametric study are given in Table 5.1.
The results of the finite element analyses are compared to those of the closed form theory
in terms of the deflections predicted for the top, mid-height and near dredge line portion of the
cylinder on the side opposite of the loading. The deflection ratio is termed as o,,,,,,Jot1reoty . In
Figure 5.10, this ratio is plotted versus the ratio of modulus of steel (Es) to modulus of shear
transfer elements (Eshear) for a cylinder with dimensions like those of Lock and Dam 26 (R)
cells, free cell height (H) of 60 feet and cell width (B) of 63 feet. For other values of H/B ratio,
similar plots are presented in Appendix A. The factor by which the modulus of steel should
be reduced to compute the modulus for shear transfer element so that the predicted cell dis-
placements from finite element analyses equal the closed form solution, is obtained from
intersection of the curve at o,,,,,,Jot1r•oty equal to unity. In case of Lock and Dam 26 (R), these
values are 268, 235 and 100 for top, mid-height and lower part of cell, respectively (Figure 5.9).
Results of all of the analyses show that:
1. The value of the first modulus reduction factor Es/Eshear corresponding to o,,,m!Ot11eoty
equal to unity increases as cell height to cell width ratio H/B increases.
2. Reduction factor Es/Eshear for o,.,,,/ot1r•oty equal to unity is more for top of cell than for
mid-height of cell, indicating that higher reduction factor should be applied to steel
modulus for computing modulus for shear transfer elements for top portion of cell than for
middle portion.
3. The modulus of shear transfer elements has to become very much smaller than that of
steel to yield a deflection ratio o,.,,,/ot1r.oty of one.
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 99
Table 5.1.
Dimensions of Cylinders Used in Parametric Studies to Evaluate Response of Shear Transfer Elements
H B H/B (feet) (feet)
84.0 63.0 1.33 60.0 63.0 0.952 48.8 63.0 0.775 37.6 63.0 0.597 25.0 63.0 0.397 12.5 63.0 0.198 50.0 40.0 1.25 40.0 40.0 1.0 30.0 40.0 0.75 20.0 40.0 0.5 10.0 40.0 0.25
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 100
>-'-0 Q) .c -"° ........ ~ w LL
"° II
0.1
l
0.01
E5 /Eshr=235
H = 60 ft 8 = 63 ft H/8=0.952
.OOl'-----4~0-----8~0----~1720=----716~0:----:2~0~0:-----;2~4~0~-;:;;:280
Figure 5.10. Deflection ratio v/s modulus ratio for Lock and Dam 26 (R).
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 101
The first modulus reduction factors are computed for different values of H/B ratio and
presented in Figure 5.11. For the case of Lock and Dam 26 (R), the first modulus reduction
factors based on these curves are approximately 270 and 235 for top and mid-height of cell,
respectively. Values are plotted for cell width (B) of 63 and 40 feet for top and mid-height of
cell. As most of the cofferdams fall within B = 40 to 60 feet, it would be reasonable to use
these curves for computing first modulus reduction factor for shear transfer elements.
The curves discussed above, thus, yield the first modulus reduction factor for shear trans-
fer elements computed based on the comparison of theoretical solution and finite element
analyses. The second modulus reduction factor, based on case history evaluation, is dis-
cussed in Chapter 6.
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 102
.... 0 41 .s::. Ill
IJJ --Ill IJJ
100
10.0
Top of cell
For.lock & Dam 26 -- - - - - - - - - - - - - - - - - - -- -
Es= Young's modulus of steel
Eshear =Young's rrodulus of shear element
H = Free height of cell
B = Width of cell
--8 = 63.0Ft
-- --- B = 40.0 Ft
1.0--~~--i~~~--L~~~-L~~~-'-~~...._,,__~~--i~~~.....1 o.o 0.2 0.4 0.6 0.8 1.0 1. 2 1.4
H/B
Figure 5.11. H/B versus modulus ratio.
PLANE STRAIN VERSION OF FINITE ELEMENT PROGRAM (SOILSTRUCT) 103
Chapter VI
CASE HISTORY STUDIES USING MODIFIED PLANE
STRAIN FINITE ELEMENT PROGRAM
To verify the predictions of the modified plane strain finite element program and to help
determine the second modulus reduction factor (RF2), it was considered necessary to analyze
case histories documented through instrumentation. The second modulus reduction factor
(RF2) is applied along with the first modulus reduction factor (RF1) to arrive at appropriate
stiffnesses for the shear transfer elements during lateral loading.
In Chapter 5, it was shown that the modulus of load transfer shear elements should be
reduced by first modulus reduction factor (RF1), depending on the ratio of the free height (H)
to width (B) for the cofferdam. However, the basis for the first modulus reduction is theore-
tical, and the case history analyses allow practical factors to be considered.
Three case histories are studied: (i) Willow Island second-stage cofferdam - cell 27, (ii)
Willow Island second-stage cofferdam - cloverleaf cell 33, and (iii) Lock and Dam 26 (replace-
CASE HISTORY STUDIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 104
ment) first-stage cofferdam. These case histories were selected firstly because they were well
instrumented and secondly because the cofferdam in these cases were founded on sandstone,
clay and deep sands, respectively, representing three different types of foundations.
6.1 Second Modulus Reduction Factor and General
Analyses Procedures
Before lateral loads are applied to cofferdam due to berm placement, dewatering or
flooding, the spring elements are removed and shear elements are installed instead. Al-
though during cell filling most of the interlock slacks and slippages must have been com-
pleted, there would still be some slack and slippage left. Also, there would be some rotation
or local yielding and imperfect alignment of interlocks which would result in further reductions
in modulus value of shear transfer elements during lateral loading after cell filling. Therefore,
analyses for lateral loading have to incorporate a second modulus reduction factor (RF2) to
be applied to steel modulus in addition to first modulus reduction factor (RF1) to compute
modulus of shear transfer elements. Moreover, it was observed for the case of Lock and Dam
26 (R) that both outboard and inboard sheet piles behave more or less like a cantilever beam
during lateral loading (Figure 6.1). During lateral loading, the horizontal distance between
outboard and inboard sheet piles decreases indicating general compression in the cell in
horizontal direction. Therefore, there should be a bulging force in other horizontal direction
towards the cross wall represented by shear elements. Thus, the modulus in circumferential
direction for shear transfer elements would become predominant and important during lateral
loading. The second modulus reduction factor determined based on case history analyses
would, therefore, also include the impact of reduced circumferential modulus of shear transfer
elements along with the three-dimensional behavior effects.
CASE HISTORY STUDIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 105
130.0
I
120.0 I Inboard I I ------ Out board I
110.0 I I I I
100.0 I - I I- I UJ I UJ lL. 90.0 I
I
z I 0 I
I I- 80.0 I <{ > I UJ I _, I UJ I Dredge line I 10.0 ~ '/ 1U\" <.;4,;
1.0.0
o.o o.s 1.0 1.5 2.0 2.s 3.0 3.5 DEFLECTION ( INCHES)
Figure 6.1. Deflection of sheet piles due to lateral load.
CASE HISTORIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 106
Case history analyses were conducted in two stages. First stage of analysis was limited
to the cell filling operation which was done in a number of steps. Connecting springs with an
E-ratio of 0.03 were used between outboard and inboard sheet piles during cell filling. The
second stage of analysis considered berm placement, dewatering and application of equip-
ment load on top of cell fill as the case may be. Spring elements were replaced by shear
transfer elements between outboard and inboard sheet piles during second stage of analyses.
Results of first stage analysis were used as initial state of deflections and stresses for second
stage analyses. Results of these analyses are compared with the observed data to arrive at
an appropriate value of second modulus reduction factor (RF2) for shear transfer elements.
6.2 Willow-Island Second Stage Cofferdam - Cell 27
6.2.1 Project Description
The Willow Island Locks and Dam are located on the Ohio River 162 miles downstream of
Pittsburgh, Pennsylvania, at Willow Island, West Virginia. The project includes two parallel
locks, a high-lift gated dam, and a fixed overflow weir. The locks are located on the Ohio side
of the river and consist of a main lock 1200 feet long by 110 feet wide and an auxiliary lock 600
feet long by 110 feet wide. The dam has an overall length of 1,017 feet and consists of eight
tainter gates each 110 feet long by 34 feet high supported between nine reinforced concrete
piers. The weir is located on the West Virginia side and is 110 feet long. Normal upper and
lower pool elevations are 602.0 feet and 582.0 feet, respectively.
In order to construct the dam, a two-stage cofferdam was designed and built in the early
1970s. The first-stage cofferdam tied into the West Virginia bank and was used for the con-
CASE HISTORY STUDIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 107
struction of Piers 5 through 9. The second-stage cofferdam tied into Pier 5 and the river lock
wall and was used for the construction of Piers 1 through 4. Both cofferdams were instru-
mented to monitor movement, pore pressure and phreatic surface, but the second stage
instrumentation was more closely monitored than the first.
The second-stage cofferdam consisted of fourteen circular cells and five cloverleaf cells
interconnected by arcs as shown in Figure 6.2. Cells 14, 15 and 35 were part of the first-stage
cofferdam. Cloverleaf cells 31, 32 and 33 were constructed in the dry inside the dewatered
first-stage cofferdam and filled by clam shell. The remaining circular cells were filled hy-
draulically with well-graded, free-draining sand and gravel dredged from the river channel.
The water level was about 18 to 20 feet below top of cells.
The cells and connectors were constructed of type MP-102 steel sheet piling. The arcs
were joined to the cell by 30° wyes, and 120 ° wyes and cross-pieces were used to construct
the cross walls of the cloverleaf cells. These riveted connector piles were fabricated from type
MP-102 piling. The piling was driven to top of sandstone or six to eighteen inches into the
indurated clay layer where it was present. Weep holes were cut in the piling on the dry side
of all cells and connectors.
The cells in the upstream arm of the cofferdam were 58 to 61 feet high. The cells in the
downstream arm were approximately four feet lower, ranging from 54 to 57 feet high. The
circular cells were 64 feet in diameter. The cloverleaf cells had a maximum diameter of 90
feet, and were capped with an eighteen inch layer of stone to prevent scour in the event of
overtopping. Timber seals were installed between the four tie-in cells and the existing river
lock wall or Pier 5. Cell 27 was 54 feet high and 64 feet in diameter and was founded on
sandstone caprock.
CASE HISTORY STUDIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 108
PIER 2 PIER I , ... , I I
I I I
r·· • ' • '
0 SO 100 ISO ZOO kxd I I
5CAU I• IHI
RIVER LOCK WALL
Figure 6.2. Willow Island second-stage cofferdam location plan.
CASE HISTORIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 109
6.2.2 Site Conditions
The bedrock at the Willow Island site consists of thick, marine, shallow water deposits
which consolidated to indurated clays, claystones, shales, siltstones and sandstones. These
deposits were uplifted and folded by the same intense tectonic forces acting from the south-
east which formed the Appalachian Mountains.
Erosion has exposed members of the Conemaugh Series of the Pennsylvanian Age. These
beds are variable in composition and thickness with frequent facies changes and limited lat-
eral extent. The top of rock within the second-stage cofferdam has an average elevation of
557 feet and consists of a moderately hard, fine to medium grained, gray, micaeous sandstone
which is ten feet thick under Cell 24 but pinches out in the area of Cell 33 (Figure 6.2). The
sandstone caprock is underlain by a massive fifteen foot formation of soft, red and gray, highly
slickensided indurated clay with siltstone phases. The top two to twelve inches of this mem-
ber had decomposed to a soft clay. Beneath the indurated clay is a second strata of moder-
ately hard, fine grained, gray silty sandstone interbedded with moderately hard, red and gray
siltstone. This fifteen foot bed is interrupted by a three foot finger of indurated clay, and Piers
1 through 4 are founded below this clay zone. The sandstone-siltstone member is underlain
by a ten-foot zone of soft, red and gray, highly slickensided indurated clay with silty zones and
twelve feet of moderately hard, red and gray, silty shale with sandy zones.
The instrumentation for the second-stage cofferdam consisted of five inclinometer wells,
five in-place deflectometer wells with four sensors per well, twelve pneumatic piezometers,
twenty phreatic piezometers and a survey control net.
CASE HISTORY STUDIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 110
The instrumentation was installed after cell filling, but before dewatering. It generally
performed well, but on Cell 27, the inclinometer casing was hit by a crane and top of cell
movement had to be estimated thereafter.
6.2.3 Finite Element Analyses
The finite element mesh used for plane strain analysis is shown in Figure 6.3. The soil and
rock properties used were derived from the work by Clough and Hansen (1977), and are given
in Table 6.1. The water level was 18 feet below top of cell.
The analysis procedures allowed for a step-by-step simulation of construction sequence
as shown in Figure 6.4. Initial stage consisted of installation of cofferdam cell sheet piles in
place with river water level at about 18 feet below top of cell. This was followed by cell filling
which was completed in nine steps. After cell filling, the initial dewatering was modeled as
the third stage of construction.
An E-ratio of 0.03 was used for cell filling. After cell filling, analyses were conducted for
initial dewatering using the second modulus reduction factors (RF2) of 33, 25, and 20 for shear
transfer elements. The H/B ratio for Cell 27 was 0.843 and for this value of H/B the first
modulus reduction factor (RF1) for shear transfer element was computed from Figure 5.11 as
250 for top half and 190 for bottom half of the cell height. Both modulus reduction factors, RF1
and RF2, were applied to steel modulus to determine the modulus of shear transfer elements
used in the analyses.
The sheet pile deflection for initial dewatering from these analyses and those observed in
field using inclinometers are shown in Figure 6.5. The finite element predictions for all the
values of RF2 show similar trends. Maximum deflections occur at about one-third of cell
CASE HISTORY STUDIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 111
0 •:J
·.:.> ._., '" 0 0
CJ 0
t") «' _____ ....... C\.I
CJ ------0 0 ':r'
1--t-+-+-+-+--i C\.I
0 t-+++-t-+-+-1-+-+-+--+-+-+-+-~ 0
IJ ................. ~ ............. -+-+--+-+-+-+--'"~
0 C."l
Ht-+-+-+-+~ 0 C\.I
-------=> co
u 0
H~-+--+--+-_.,.o ~
0 0
.-~~~--~~~~-.-~~~"-i.,...a...&....&....L--L
oo·cf GC 0 091 00·021 oo·oe OO"Oh
CASE HISTORIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM
....: N
ci c "i u e ftl -e ~ u ,, c ftl iii
.. .2 .c en
CD E -c CD E CD "i .! c Li: cw; cO 2! :I Q
Li:
112
n )lo> en m ::i:: iii a ::u < en 2 2 m en c en z C') ;: 0 2 'Tl iii c .,, ~ z m en -4 ::u )lo> z :!! z ~ m r-m s: m z -4 .,, ::u 0 C') ::u )lo> :s:
.... .... w
Cell Soil No. or
Rock Type
SS-1
Circular SS-2 Cell SS-3 27 SS-4
SS-5 rial
SS-6
Clover- SS-7 leaf SS-8 33 SS-9
SS-10 rial
Table 6.1 Soil or Rock Properties for Willow Island Cofferdam
Soil or Rock Properties Hyperbolic Parameters
Unit Modulus Friction Cohe- Pois- Earth weight E angle sion son pressure Remarks 'Y q> c ratio coefficient (pcf) {psf) {degrees) v Ko Km Kur n Rf
97.6 2.5x101 0.0 0.0 0.2 1.0 - - 0.0 - Up to 7.6 ft. depth in foundation
97.6 - 0.0 5760.0 0.2 1.0 2000.0 2000.0 0.3 0.9 7.6 to 21.3 ft. 97.6 6.51x107 0.0 0.0 0.2 1.0 - - 0.0 - 21.3 to 39.7 ft. 97.6 3.9x107 0.0 0.0 0.2 1.0 - - 0.0 - 39.7 to 50.0 ft. 110.0 - 30.0 144.0 0.2 0.7 500.0 1000.0 0.5 0.9 cell fill mate-
97.6 - 0.0 5760.0 0.2 1.0 2000.0 2000.0 0.3 0.9 Upto11.8ft. depth in foundation
97.6 2.5x101 0.0 0.0 0.2 1.0 - - 0.0 -- 11.8 to 28.8 ft. 97.6 -- 0.0 5760.0 0.2 1.0 2000.0 2000.0 0.3 0.9 28.8 to 34 ft. 97.6 3.9x107 0.0 0.0 0.2 1.0 - - 0.0 -- 34 to 54 ft. 110.0 -- 30.0 144.0 0.2 0.7 500.0 1000.0 0.5 0.9 cell fill mate-
n l:; m :J: iii d ::u iii fn c fn z a s:: 0 0 :!! m 0 "Q
~ z m en ~ > z :!! z ~ m r m s:: m ~ "Q ::u g ::u > s::
... ... ..
T 18ft
1--64£ t ,____
,,... T 60 ft.
~~'0-~~~~~~"~~~"' 1
(A) Cell In Place
· .. -: ~":..: .. ..: .... I • •
:"·' .'• ~ .. ·. . . . " ~ . . · ... '.
, ...... ·. , ·.... . ..
(B) Cell Filling (C) Initial Dewatering
Figure 6.4. Willow Island Cofferdam, Cell 27, construction sequence modeled.
height from dredge line. The results show that maximum deflection is more closely matched
with observed value if second modulus factor (RF2) of 25 is used for shear transfer elements.
The maximum deflections were of the order of 0.6 inch. However, observed deflections of
sheet pile top are higher by 0.15 inches than those predicted. This probably could be because
the inclinometer casing was hit by a crane. Also, movement of heavy equipment on top of cell
fill could also cause this. The load of the construction equipment was estimated to range from
500 to 1500 psf. To examine the effect of heavy machinery movement on top of cell fill, a load
of 500 psf was applied in this case as surcharge on top of cell fill over one-half of cell width
from center line of cell to cell wall. With this loading, the predicted sheet pile deflections
match well with those observed (Figure 6.6). Thus, a second modulus reduction factor of 25
is considered appropriate for shear transfer elements during lateral loading for this case.
It was considered useful to compare the response of Willow Island cofferdam cells using
connector springs with that using shear transfer elements between outboard and inboard
sheet piles during lateral loading. The sheet pile deflection results obtained using springs
with E-ratio of 1.0 and as reported by Hansen and Clough (1982) are plotted in Figure 6.7 along
with the predictions of present analyses using shear transfer element (with RF2 = 25) without
any surcharge equipment load. The observed data is also presented on this figure. These
results show that models using spring elements with E-ratio of 1.0 and shear transfer elements
with second modulus reduction factor (RF2) of 25 yield similar predictions.
CASE HISTORY STUDIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 115
110
9~ I •
100 9~ I •
¢~ I •
90 9 ~ • • RF2 is Second - ~~ Modulus Reduction ..... Factor for Shear L&J ' . Transfer Elements. L&J 80 ~\ IL.
z 0 ..... ~ 70 > UJ . ..J L&J
60
Dredge tine
• Observed (Inclinometer)
~ RF2=33 40
-·<>-· RF2 = 25 ---0--- RF2 = 20
0.2 0.4 0.6 0.8 1.0
DEFLECTION (INCHES)
Figure 6.5. Willow Island Cofferdam, cell 27, Inboard sheet pile deflections due to Initial dewatering.
CASE HISTORIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 116
100 • Observed
RF2=25
90 ---- With load on to
500 PSF ...... RF2 =25 LLJ LLJ u..
z 0 ...... < > RF2 is Second LLJ 70 Modulus Reduction ...J LLJ Foctor for Shear
Transfer Elements.
60
50
40 ........ ~~---''--~~-L.~~~-'-~~~--~~---' 0,0 o.s 1.0 1.5 2 .o 2 .5
DEFLEC110N (INCHES)
Figure 6.6. Willow Island Cofferdam, cell 27, inboard sheet pile deflections due to initial dewaterlng, and equipment surcharge load.
CASE HISTORIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 117
110
I 100 I
I I
90 -t-w w LL
80 z 0 t-< > l.JJ 70 ...J l.JJ
so
• Observed
With shear transfer elements (RF2=25)
----- With spring elements (E-ratio=LO)
RF2 is Second Modulus Reduction Factor for Shear Transfer Elements.
DEFLEC110N (INCHES)
Figure 6.7. Willow Island Cofferdam, cell 27, inboard sheet pile deflections due to initial dewatering, using springs and shear transfer elements.
CASE HISTORIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 118
6.3 Willow Island Second-Stage Cofferdam Cloverleaf
Cell 33
6.3.1 Project Description
The general project description and site conditions at Willow Island cofferdam are given
in Section 6.2.1. The cloverleaf Cell 33 was founded directly in indurated clay (Figure 6.2).
Sheet pile penetration varied from 6 to 18 inches. The diameter of cell was about 90 feet and
the height 62 feet. The water level during cell filling was about 20 feet below top of cell.
6.3.2 Finite Element Analyses
The finite element mesh used for the analyses of Cell 33 is shown in Figure 6.8. One row
of sheet pile elements was used in the center of the cell to model crosswall in cloverleaf cell.
The soil properties used are given in Table 6.1. The sequence of construction followed in the
analyses was same as mentioned for Cell 27 in Section 6.2.3.
An E-ratio of 0.03 was assumed for cell filling, which was completed in nine steps. After
cell filling, analyses were done for initial dewatering using second modulus reduction factor
(RF2) of 25 for shear transfer elements. The H/B ratio for Cell 33 was approximately 0.62 and
the corresponding first modulus reduction factors (RF1) for shear transfer elements computed
from Figure 5.11 were 120 and 95 for top half and bottom half of the cell height, respectively.
Both modulus reduction factors RF1 and RF2 were applied to steel modulus to compute
modulus of shear transfer elements used in the analyses.
CASE HISTORY STUDIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 119
Cll 4-' i:: Q
) s Q
) r-4 tzl
r-4 r-4 cu !:l Cl) Cll 0 ,... u oo·oz1
oo·oe
. ' OO
"Oh
... 0 0 0 '° ...... 0 0 0 C\J (T
l
0 0 0 CD C
\I
0 0 . 0 =r C\J
0 a 0 0 C\J
0 0 . 0 •.J:)
0 0 0 C\J
0 0 0 (0
0 0 0 ::r
0 0 . oo·(f
CA
SE
HIS
TOR
IES
US
ING
MO
DIFIE
D P
LAN
E S
TRA
IN FIN
ITE ELE
ME
NT P
RO
GR
AM
C"> C">
0 c -8 'ti G> 'C
: 0 u .. .2 .c
= E
120
The predicted and observed sheet pile deflections due to initial dewatering are shown in
Figure 6.9. As the inclinometer casing was placed in cell fill at some distance from inboard
sheet pile, the predicted deflections are also ploted in Figure 6.10 for soil elements in cell fill
at about 12 feet distance from inboard sheet pile. The predicted soil deflections match well
with those observed up to about 15 feet from dredge line. Thereafter, the observed deflections
are greater than predicted, reaching a difference of about 0. 75 inches at top of the cell. As
indicated earlier in Section 6.2.3 for Cell 27, this discrepancy in deflections could probably be
due to movement of heavy machinery such as crane and loaders. As indicated earlier, the
load of this equipment was approximated to be about 500 to 1500 psf. In this analysis appli-
cation of a load of 1500 psf as surcharge on the cell fill over half of cell width resulted in rea-
sonable match of finite element predictions with the observed deflections.
As can be observed from the predicted pattern of deflections, use of RF2 of 25 for shear
transfer elements appears appropriate to match with observed values in the vicinity of dredge
line where deflections are not much affected due to equipment loading and other disturbances
on top of the cell. In case of Cell 27 also, discussed in Section 6.2, it was observed that a
second modulus reduction factor of 25 for shear transfer elements yields results which rea-
sonably represent the observed behavior.
CASE HISTORY STUDIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 121
120.0
110.0
100.0
-~
~ 90.0 LL
z 0 80.0 ~ < > LLJ 70.0 ...J LLJ
60.0
40.00.0 0.5
I I I I I
I I
• Observed RF2=25
----- RF2 = 25 for soil at 12Ft away
--- With load on top 1500psf
1 oredge line
RF2 is Second Modulus Reduction Factor for Shear Transfer Elements.
1.0 1.5 2.0. 2 .s 3.0 DEFLECTION (INCHES)
3.5
Figure 6.9. Willow Island cofferdam, cloverleaf 33, deflections of inboard sheet pile due to Initial dewatering.
CASE HISTORIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 122
I
J
' I
oo·os1 0
0'0
01
oo·os
0 0 0 "' "' 0 0 0 0 .... ~ "' 0 0 0 Ill ':3'
0 0 0 0 ':3'
0 0 0 "' M 0 0 0 0 M
... 0 0 0 "' "' 0 0 0 0 "' 0 0 C)
, .... -0 0 0 0 -[l
c.• 0 II'
0 0
oo·cf
CASE H
ISTO
RIE
S U
SIN
G M
OD
IFIED
PLA
NE
STR
AIN
FINITE E
LEM
EN
T PR
OG
RA
M
;:-c CD E
3 ftl Ci. CD a: -
123
6.4 Lock and Dam No. 26 (Replacement), First-Stage
Cofferdam
6.4.1 Project Description
General description of Lock and Dam 26 (R), stage one cofferdam is given in Chapters 2
and 3. The cofferdam cells are approximately 63 feet in diameter and 60 feet high above the
dredge line. The sheet piles penetrated into the riverbed soils a distance of 35 feet. The cells
under study were filled by dumping riverbed sands with a clamshell. The water level was at
28 feet below top of cell.
Foundation materials at the replacement site consist of about 70 feet of granular alluvium
overlying bedrock (Figure 3.4). The alluvium increases in grain size with depth. At the river
bottom, it is a medium sand and at greater depths, the alluvium contains lenses of cobbles
and boulders.
Two circular cells and one arc cell of the downstream leg of the cofferdam were instru-
mented through a cooperative effort between the Corps of Engineers, St. Louis District and
Shannon & Wilson, Inc. The instrumentation program and results obtained through the cell
filling operations and early dewatering efforts are described in Shannon & Wilson (1983).
Instrumentation included eight inclinometers, 410 strain gage bridges, and 24 earth pressure
cells. In addition, pneumatic and open piezometers were installed on the piles, trilateration
monuments were placed along the perimeter of the cell walls, and settlement points were
placed in the top of the cell fill.
CASE HISTORY STUDIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 124
6.4.2 Finite Element Analyses
The finite element mesh used for plane strain analyses of Lock and Dam 26 (R) first-stage
cofferdam is shown in Figure 6.10. The water level during cell filling was 28 feet below top of
cell. The soil parameters used are given in Table 3.2.
The construction sequence (Figure 6.11) modeled in the analyses considered cofferdam
cell placement with river water level at 28 feet below top of cell, followed by cell filling in ten
steps. Thereafter, berm placement on inboard side and initial dewatering were simulated as
separate construction stages representing application of lateral loads to cofferdam cell.
The cell filling was simulated in ten steps and E-ratio of 0.03 was used for the spring ele-
ments. After cell filling, analyses were performed for berm placement and dewatering using
second modulus reduction factor (RF2) of 25 for shear transfer elements. The H/B ratio was
0.95 and corresponding first modulus reduction factors (RF1), computed using Figure 5.11, are
270 and 230 for top half and bottom half of cell, respectively. Both modulus reduction factors,
RF1 and RF2, were applied to the modulus of steel to computed modulus of shear transfer
elements.
The predicted and observed sheet pile deflections due to berm placement are shown in
Figure 6.12. The results show general consistency with the observed behavior.
For dewatering, predicted and observed behavior of inboard sheet pile are shown in Figure
6.13. With the application of 1500 psf surcharge load due to construction equipment on top of
cell fill over half of cell width, the predicted sheet pile deflections match well with those ob-
served. These results confirm the observations from Willow Island cofferdam Cell 27 and Cell
33 analyses, discussed in Sections 6.2 and 6.3, that using the second modulus reduction factor
CASE HISTORY STUDIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 125
~63ft.--t Cell fill
T . ., . . . T 28 ft. . . . . . ..
. , .. ·." ... . -~ ·... . . : 60 ft.
Foundation
(A) Cell in Place (B) Cell Filling
, ....... _ ... · ....... .. . .. . ·· ... :-: ':: ,' ..... : .. _ .. : -: · ....
·. . .. ~ :' ~ ........ , .· . . ·. .. .. · .. ·. ' .. :. '..:. , : .. : : -===-,. .I~. .. • •• :· • •
. . . . • :· . • . . ·. . . . . . . . r-:----,'"'
.. ·. · .... <.": .= ..... · ... :;.·:: . ... : .. · .. ·. : : · ... · .. _ .· ........ . . : ....... ·. · .. · ...... : .. ~:
-~--I.. ....•
(C) Berm Placement (D) Initial Dewatering
Figure 6.11. Lock and Dam 26 (R) cofferdam, construction sequence modeled.
CASE HISTORIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 126
120 --+- Observed ( Inboard)
~ Observed (Out board)
110 --<>-- Predicted (In board) RF2.=25
-100 ---er.-- Predicted (out board) t- RF2=25 w w I LL ' 90 t> RF2 is Second z ' Modulus Reduction 0 Foctor for Shear t- Transfer Elements. < > w _, w
70
60
so
40
o.o 1.0 2.0 3.0 4.0 s.o 6.0 DEFLECTION ( INCHES )
Figure 6.12. Lock and Dam 26 (R) cofferdam, deflection of sheet piles due to berm placement.
CASE HISTORIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 127
of 25 for shear transfer elements yields results which reasonably match the observed behav-
ior.
6.5 Summary of Case Histories
As indicated in the earlier chapter, the appropriate modulus value of shear transfer ele-
ment should be determined on the basis of (i) comparison of finite element results with the-
oretical solutions and (ii) analyses of case histories. The first modulus reduction factor (RF1)
based on (i), discussed in Chapter 5, is obtained using the curve (Figure 5.11) for a particular
cell height and cell width ratio H/B. The second modulus reduction factor (RF2), based on
case histories discussed in this chapter, considers three-dimensional effects, and interlock
slack and yielding. during lateral loading.
Although the three case histories indicate that during lateral loading, the second modulus
reduction factor (RF2) of 25 for shear transfer elements yields results which agree most with
the general observed behavior, it is difficult to arrive at this conclusion for definite. The rea-
sons for this are 1) small amount of sheet pile deflections, 2) reliability of the instrumentation
data, and 3) expected disturbances due to construction equipment over the cell fill.
Nevertheless, RF2 of 25 could be used for shear transfer elements during lateral loading
to obtain reasonable results.
Both the above modulus reduction factors, RF1 and RF2, should be applied to the modulus
value of steel to compute the modulus of shear transfer elements for use in analyses.
CASE HISTORY STUDIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 128
120
100
-~
ttl 90 LL
z 80 0
t:= ~ w ...J 70 w
60
50
40
0.0
---o--- Observed
- - - --- Predicted (RF2
-....._..
=~5) with differential load
Predicted (RF2 = 25) with load on top =1500psf
Dredge line
RF2 is Second Modulus Reduction Factor for Shear Transfer Elements.
1.0 2.0 3.0 4.0 5.0
DEFLECTION { INCHES }
6.0
figure 6.13. Lock and Dam 26 (R) cofferdam, deflection of inboard sheet pile due to initial dewatering.
CASE HISTORIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 129
6.6 Stress Transfer Mechanism From Outboard to Inboard
Sheet Pile
Analyses were done to study the effects of alternative methods for providing shear transfer
through cell fill during application of lateral loads. Lock and Dam 26 (R) dimension and soil
conditions were considered and hydrostatic loading was applied on full free cell height, as
discussed in detail in Chapter 7. Cases using shear transfer elements with second modulus
reduction factor RF2 of 25, springs with E-ratio of 1.0 and using no connectors between out-
board and inboard sheet piles were analyzed. Model using no connectors was considered to
compare and study the effect of presence of shear transfer mechanism.
The results of incremental horizontal stress (~ crx) over the cell width at El. 105 (25 feet
from top and 35 feet from dredge line) for hydrostatic load of 1ywh are shown in Figure 6.14
for cases with load transfer shear elements; with spring elements, and with no connectors
between outboard and inboard sheet piles.
The results with load transfer shear elements show a smoother transfer of lateral load
through cell fill as well as through shear elements. The maximum incremental horizontal
stress is near outboard sheet pile, and it is reduced to almost zero near inboard sheet pile.
In case of spring elements, the ~ crx near outboard sheet pile is very high and suddenly
drops near the center of cell fill. Similarly, with no connectors, there is very high ~ crx near
outboard sheet pile and drops to zero at 8/6 from center towards inboard sheet pile (Figure
6.14). The soil near inboard sheet pile beyond 8/6 from center experiences tensile stresses.
CASE HISTORY STUDIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 130
1.5 In cell fill with 1.4 ' shear elements
' With springs u. ' -·-Vl ' ~ 1.2 ' No connectors ' -----
~ \ In shear elements <J ' --·-9\ \ Vl 1.0 \ Dredge line El.= 70.0 Vl
L&J \ a:: \ ~ \ Vl \
...J 0.8 \ ~ \ ~ z \ 0 \ N 0.6 \ a:: \ . 0 \I :c z
0.4 \° w c.!) z ~ 0.2 :c u
0.0
l cell1 .... ____ -0.2 -0.3
0.0 10.0 20.0 30.0 40.0 50.0 60.0 Outboard DISTANCE {FEET) Inboard
side side
Figure 6.14. Lock and Dam 26 (R) cofferdam load transfer from outboard to inboard sheet pile at El. 105 for hydrostatic load 1ywh.
CASE HISTORY STUDIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 131
As the spring elements connect outboard and inboard sheet piles at some distance inter-
vals, while the shear transfer elements connect the sheet piles in full height. the shear ele-
ments are, therefore, expected to result in the load transfer mechanism which could be
somewhat closer to the realistic behavior.
CASE HISTORY STUDIES USING MODIFIED PLANE STRAIN FINITE ELEMENT PROGRAM 132
Chapter VII
PREDICTED RESPONSE OF LOCK AND DAM 26 {R)
TO LATERAL LOADING
An important aspect considered in the design of cofferdams, other than interlock tension
issue discussed in Chapter 4, is the failure of cell fill during lateral loading. As noted before,
such failures have been rare, and it is believed that the conventional design methods for
vertical shear failure in cell fill are conservative. As an example, for Lock and Dam 26 (R)
stage one cofferdam, the factors of safety against vertical shear for the case of normal pool
are computed as 6 and 12 based on Terzaghi and Schroeder and Maitland method, respec-
tively. These values are 1.5 and 3.0 for normal flood case. At normal pool and flood loadings,
this cofferdam has been functioning as a safe structure, as borne out by its behavior observed
in the field. Considering the observed maximum sheet pile deflections of only 1to1.4 inch for
flood loading on Lock and Dam 26 (R), it could be deduced that both Terzaghi and Schroeder
and Maitland method yield conservative predictions as the cofferdam cell would need to un-
dergo substantial deformation before vertical shear failure could occur.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 133
Following sections discuss the response of Lock and Dam 26 (R) cofferdam for normal flood
and higher lateral loads. Lock and Dam 26 (R) is considered for analyses as this represents
a typical large cofferdam. Analyses for normal flood load after cell filling are intended to ap-
proximately model the actual flood condition and study the behavior in respect of cell de-
flection, lateral earth pressure coefficients and base pressure distributions. Although
application of higher lateral loads to failure represents a condition not achievable in the field,
it is considered important to investigate what the nature of response will be. Also, the results
of analyses for loads to failure will give better idea of real factor of safety against failure and
help assess the degree of conservatism in the design. Development of failure surfaces during
high lateral loads is also discussed. The failure mechanism investigated would be helpful in
development of new design method of shear failure in cell fill presented in Chapter 8.
7.1 Analysis Procedures and Assumptions Therein
Using plane strain SOILSTRUCT program, vertical slice analyses were done for Lock and
Dam 26 (R) in two stages. First stage simulated cell filling in ten steps, using an E-ratio of 0.03
for springs. Following cell filling, lateral loads in steps of one hydrostatic pressure (1y.jJ) were
applied on entire free height of outboard sheet pile. The schematic representation of
cofferdam cell subjected to lateral loading is shown in Figure 7.1. Shear transfer elements
with RF2 of 25 were used during lateral loading. The finite element mesh used for analyses
is shown in Figure 6.10. The hydrostatic loading was considered because of following:
• As a base case, it represents the normal flood condition.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 134
side -i r Inboard side
T .or-----~ Outboard
h
Cofferdam Cell H
y h w
Dredge line
Foundation
figure 7.1. Schematic representation of a cofferdam cell subjected to lateral load.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING . 135
• Moment being the most important factor, any particular loading would be translated into
the aplied moment on the cell. Hydrostatic loading offers a general case and could be
related to any kind of specific load in terms of moment.
• Offers a simplified tool to allow comparison between conventional and finite element
methods.
• Failure of "safe" cofferdam could be reached by application of load increased by unit
hydrostatic load in each step.
It may be noted that the verification of shear transfer elements in SOILSTRUCT program
and computation of modulus reduction factors is based on analyses for working conditions
only. It could be possible that at higher lateral loads, local dislocations and relative dis-
placements in cell fill or slippage between sheet piles may occur that could affect the behavior
and failure mechanism of the cofferdam. The basic model does not consider the effects of
these factors, but they are examined later in the chapter.
Vertical slice analyses were conducted considering Lock and Dam 26 (R) dimensions and
soils. Cell width, free cell height and depth of embedment were taken as 63, 60 and 35 feet,
respectively. The soil parameters used were as given in Table 3.2. The water level was 28
feet below top of cell.
7.2 Cell Filling
Behavior of cofferdams during cell filling was studied in detail in Chapter 4 using
axisymmetric SOILSTRUCT program. In this section, the development of lateral earth pres-
PREDICTED RESPONSE OF LOCK ANO DAM 26 (R) TO LATERAL LOADING 136
sure coefficient in cell fill is discussed to compare with the values used in conventional de-
signs for interlock force.
As discussed in Chapter 2, various conventional design theories assume different values
of lateral earth pressure coefficient (Figure 2.2) to compute maximum lateral earth pressures
and maximum interlock force on sheet pile walls. As lateral earth pressure coefficient value
would affect the maximum interlock force in direct proportion, it is important to use the lateral
earth pressure coefficient value as close to reality as possible. The lateral earth pressure
coefficients (K) for cell fill and foundation soil within and just outside the cell in foundation at
the end of cell filling are shown in Figure 7.2.
Consider cell fill material having friction angle <P = 35°, the earth pressure coefficient at
rest, Ko, is defined as 1 - sin <p, and it equals 0.42. The active earth pressure coefficient is:
Ka = tan2(45 - <p/2)
or, = 0.27 for <P = 35°
The passive earth pressure coefficient is:
Kp = tan2(45 + q>/2)
or, = 3.69 for <P = 35°
The results for cell filling (Figure 7.2) show that lateral earth pressure coefficient values in
cell fill are between active and at rest coefficients and closer to at rest value Ko. The average
values near sheet piles are approximately 0.42. The range of values in cell fill is 0.37 to 0.49.
Terzaghi (1945) specified lateral earth pressure coefficient values of 0.3 to 0.5 for cellular
cofferdams. Both field and laboratory studies (Maitland and Schroeder, 1979) indicate that the
lateral earth pressure coefficient within the cell fill for cell filling condition lies between the
active and at rest coefficients. Schroeder and Maitland (1979) suggested that the lateral earth
pressure coefficient value ranges from 1.2 to 1.6 times Rankine active earth pressure coeffi-
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 137
... 1·------63. 0 Ft
--0.4 0.4 0.4 0.4 0.4
0.39 0.49 0.47 0.49 0.39
0.4 0.38 0.4 0.38 0.4
0.43 0.36 0.36 0.37 0.42
0.45 0.42 0.42 0.43 0.45 60.0A
Lo 0.43 0.38 0.37 0.38 0.43
aded side~ 0.42 0.38 0.37 0.38 0.42
0.41 0.39 0.39 0.39 0.41
0.41 0.41 0.41 0.41 0.41
Dredge line~ 0.49 0.44 0.44 0.44 0.49 "{'" _ .....
2.58 0.4 0.34 0.32 0.33 0.4 ~~ 2.57
1.67 0.43 0.35 0.32 0.35 0.43 1.65
JS.Of 1.33 0.43 0.37 0.34 0.37 0.43 1.31
1.05 0.43 0.4 0.39 0.4 0.42 1.0 -
t 0.97 0.42 0.44 0.43 0.44 0.42 0.95
// '///////////// / /'/ '//// / // / / / / / //
Figure 7.2. Lateral earth pressure coefficient (K) for cell filling.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 138
cient KA . This gives a range of .32 to 0.43 for cell fill friction angle of 35 degrees. Schroeder
and Maitland (1979) suggested an average value of lateral earth pressure coefficient as 1.38
times active earth pressure coefficient. The average value of lateral earth pressure coefficient
based on this and cell fill friction of 35 degrees is 0.37.
7.3 Predicted Response for Flood-Type Load
This section deals with the response of Lock and Dam 26 (R) cofferdam for flood type
loading conditions represented by hydrostatic load 1 y..,)1 . The discussion is related to cell
deflection, lateral earth pressure coefficient, base pressures and vertical stress in cell fill.
7.3.1 Deflection of Sheet Piles
For purposes of understanding the general effect of the lateral loading, it is useful to first
examine the effects of the application of the hydrostatic load of 1 y..,)1 . The deflected shape
of cell due to application of flood load is shown in Figure 7.3, and the horizontal deflections
of the inboard and outboard sheet pile are shown in Figure 7.4. The following observations
are made from the results:
• The deflections of both outboard and inboard sheet piles under lateral loading resemble
cantilever behavior. Maximum deflections occur at top of sheet piles. Similar type of
behavior was observed for Willow Island cofferdam cells 27 and 33 for dewatering (Fig-
ures 6.5, 6.6 and 6.9) and for Lock and Dam 26 (R) for berm placement and dewatering
(Figures 6.12 and 6.13) as discussed in Chapter 6.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 139
Loaded Side Original shape of cell
,.--.:_ ____ ~Deflected shape of cell
I -------1 I I I I I I I I f I
60ft. : Cofferdam Cell / I I I
I I / I
I I I I
,' I I I
I
I I I I I I
35ft. ! / l _:__'_-~---~---~-~-=------=--~~~ f ..-~~~~~63 ft·~--~---~-~~-_J
20.0ft. i--~~~- Scale for cell geometry.
1.0 inch .,__~~~~Scale for deflections.
Figure 7.3. Deflected shape of a cofferdam cell due to lateral load.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 140
130.0
I
120.0 I Inboard I I
Out board I ------110.0 I
I I I
100.0 I I .... I I.LI
I.LI I IJ.. 90.0 I
I
z I 0 I .... ao.o I ~ I > I I.LI I ~ I I.LI I Dredge line 10.0 I
~'I QS;t\ cow
60.0
50.0.
40.0
o.o o.s 1.0 1.5 2.0 2.5 3.0 3.5 DEFLECTION ( INCHES)
Figure 7.4. Deflection of sheet piles due to lateral load.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 141
• Outboard sheet pile deflections are more than inboard sheet pile above dredge line and
less below dredge line. Thus, soil in cell fill experiences some compression and foun-
dation soil is under slight tension.
The maximum deflections due to hydrostatic load are predicted as about 1.3 inches. The
observed deflections of a particular cell for flood load are shown in Figure 7.5 (from Martin,
1987). The maximum sheet pile deflection observed is 0.7 inch and according to these results,
outboard sheet pile moves only 0.4 inch which is less than inboard sheet pile deflection. This
is contrary to logical behavior. This, therefore, suggests that there could be some problem
with instrumentation data. However, based on optical survey, the observed average maxi-
mum sheet pile deflections for 11 cells for flood loading from point "B" to "D", ignoring fluctu-
ations, is about 1.4 inches as shown in Figure 7.6 for December, 1982 flood (Martin, 1987),
which compares well with the finite element predictions.
7.3.2 Lateral Earth Pressure Coefficients
The values of lateral earth pressure coefficients for lateral loading of 1 y.)7 are shown in
Figure 7.7. These results show that K increases substantially in cell fill near outboard sheet
pile and center of cell fill. The increase of K in soil near inboard sheet pile is only limited to
about 20 feet from top of cell. The maximum values of K within cell fill are about 0. 7 near
outboard sheet pile, the range being 0.4 to 0.71. The sheet pile deflections (Figure 7.4) also
show maximum compression near center and lower portion of cell. The K values are, there-
fore, higher near outboard sheet pile as the cell fill soil near outboard sheet pile shares more
lateral load compared to soil near inboard sheet pile.
In foundation soil within the cell, the K values do not change significantly during flood
loading. In foundation outside outboard sheet pile, the K value decreases substantially from
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 142
"O ::u m c
~ c ::u m (I) "O 0 z (I) m 0 "l'I
g " ,.. z c c ,.. 3: N
°' ~ ~
§ ::u ,.. r
g S! z a
.... t
-1ouTBOARO)
Ored9eline ") . /,/4\\fl// ----- ----;- - \"\'WT~·,
..
LOCK ANO DAM NO. 26 ( R) C e 11 on Sand Foundot ion
~4~
Sand Cell Fi IL
. .
I in
..
.. ·.
I I Displacement Scale
30 fl 1-------l Structure Scale
(INBOARD)--.
. . . . . .. '''"'''''' ... . . .....
...
Figure 7.5. Lock and Dam 26 (R), observed cell deflection for flood load (from Martin, 1987) .
--c <t w :c ~ <t .... z w a: w "-"-c
LOCK AND DAM NO. 26 ( R)
Cell on Sand Foundation (STAGE I)
II Typical cells
t 4.8 Hioh Water
/ 3.6
2.4
1.2
I Normal Oewatered Pool
l ®
PT to PT ACTIVITY
A II DEWATERING II C NORMAL FLUCTUATIONS C D DEC 1982 FLOOD D E FLOOD INTERIOR E F DEWATER INTERIOR F G APRIL t98l FLOOD G H FLOOD INTERIOR
• AveraQe of tnboord and Outboard Deflections
0 t.O 2.0 30 4.0
TOP DEFLECTION TOWARD INTERIOR 50
( in)
Figure 7.6. Lock and Dam 26 (R), average response of 11 typical cells to lateral loading (from Martin, 1987).
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 144
I """·------63.o Ft
- -0.4 0.42 0.55 0.63 0.57
0.43 0.65 0.62 0.62 0.47 0.5 0.49 0.51 0.46 0.46
0.55 0.48 0.47 0.43 0.46 0.58 0.56 0.54 0.49 0.48 60.0Ft
Lo 0.59 0.51 0.46 0.42 0.43 aded side~ 0.64 0.52 0.43 0.37 0.44
0.63 0.57 0.44 0.39 0.43 0. 71 0.56 0.49 0.42 0.41
Dredge line"-\ 0.69 0.57 0.49 0.46 0.5 ' ~'"'" 0.7 0.43 0.38 0.36 0.38 0.42 2.78
o. 76. 0.36 0.34 0.35 0.41 0.47 1. 76
35.0ft 0.76 0.46 0.38 0.36 0.39 0.46 1.42
o. 77 0.53 0.42 0.39 0.4 0.42 1.11
0.81 0.54 0.46 0.42 0.43 0.4 1.01
//nVa///////////////////////////
Figure 7.7. Lateral earth pressure coefficients (K) for hydrostatic load 1ywh.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 145
average 1.4 to 0.78, indicating decrease in horizontal stress (ox) during flood loading. Outside
inboard sheet pile there is slight increase in K value, indicating some increase in ox.
7.3.3 Base Pressure Distribution
As discussed in Chapter 2, Terzaghi's method (1945) for vertical shear analysis considers
the rotation of cofferdam cell about the center of base line (dredge line) and assumes linear
pressure distribution about the center line of the base (Figure 2.4) during application of lateral
loads. Vertical slice analyses were done to study the rotation of cell and base pressure dis-
tributions and compare results with Terzaghi's assumptions.
The analyses were done for flood loading cases of 1 y.)> acting on entire free height of
outboard sheet pile and load 1 y.)> acting on upper half of outboard sheet pile height. A
hydrostatic load of 2 y.)> was also applied to confirm the pattern of base pressure distribution.
These analyses were performed after cell filling. The incremental base pressures (change in
vertical stresses) for cell filling and for hydrostatic loads at dredge line are plotted over the
cell width in Figures 7.8 and 7.9, respectively.
For cell filling, the base pressures are nearly uniform over the cell width, the average value
being about 5.0 ksf. For hydrostatic load of 1 y.)> and 2 y.)> acting on full height of outboard
sheet pile, the incremented base pressures are zero at a distance of about 8/8 (8 = width
of cofferdam cell) from center of cell towards outboard sheet pile. For 1 y.)> load in upper half
of outboard sheet pile height, incremental base pressures are zero at approximately 8/5 from
center of cell towards outboard sheet pile.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 146
63 ft. I
t of cclli
<ti' 2.0 ~ -"' "' e -r.n ; Ci! ! <.J'
"€ > I 6.0
Figure 7.8. Base pressures at end of cell filling, Lock and Dam 26 (R) cofferdam.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 147
-~000
----~~h¥SI~ 5 Rei~R£ - 2xh¥d£~sfi. lo~~ on u eig -· -·-i xh~d ros tli. l~rd on pp er a
-1200 t of cell
I - , .. BI 5. !,.I .... -860 co 0.
I I ..._,
QJ I
1 .. B/ s .. j,. ""' -400 B/S ~I ::I (I) "''' I I (I) I QJ ....
""' "-~,I p... 0 •I
QJ (I) 200 ca
l:Q
i: ~
QJ 660
00 i: ca
..c:: u HIOO
1400
1800
0.0 10.0 20.0 30.0 40.0 50.0 60.0 Distance from Outboard Side
Figure 7.9. Base pressures at dredge line due to lateral load, Lock and Dam 26 (R) cofferdam.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 148
This means that under lateral loading the cofferdam cell tends to rotate along some point
on the dredge line which may be at a distance of 8/5 to 8/8 from center of cell towards out-
board sheet pile.
This result is in contradiction with the theory developed by Terzaghi suggesting that the
cofferdam tends to rotate along the center line of the base under lateral loading. The pre-
dieted behavior is probably because of the interaction between sheet piles and soil and also
stress transfer mechanism in cell fill. Terzaghi theory does not consider this effect.
Figure 7.9 also shows that maximum incremental compressive stresses occur at a distance
of about 8/5 from cell center towards inboard sheet pile and maximum incremental tensile
stresses occur at about 8/10 from cell center towards outboard sheet pile. Near inboard and
outboard sheet piles, the incremental stresses are reduced to almost negligible because of
slippage between sheet pile and the soil.
Due to interaction between sheet piles and soil, the incremental base pressures are re-
duced compared to the linear pressure distribution assumed in conventional design sug-
gested by Terzaghi (1945). As an example for Lock and Dam 26 (R), for normal flood load the
maximum incremental base pressure is computed as 9340 psf as compared to 4665 psf, pre-
dieted by finite element analysis (Figure 7.9). Thus, the maximum incremental pressures
could be about 50% of those computed using conventional design theories using simple laws
of mechanics. Terzaghi's (1945) vertical shear concept used to evaluate the failure due to
shear distortion in cell fill soil (as discussed in Chapters 2 and 8) suggests the computation
of vertical shear using following equation:
Q =3M 2b
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 149
This relationship is obtained assuming linear variation of base pressure due to lateral load.
The reduction in base pressures and their distribution pattern would result in substantial re-
duction in vertical shear (Q) values and thus higher factor of safety against vertical shear
failure compared to Terzaghi values. For 50% reduction in base pressure, the factor of safety
will be twice of that obtained using linear variation of incremental pressure on base.
7.3.4 Change of Vertical Stress in Cell Fill and Foundation
In addition to the study of development of base pressures at dredge line during lateral
loading as discussed under Section 7.3.3, an investigation was made of the change of vertical
stress in cell fill as well as in foundation soil to have an idea about the vertical stress transfer
through the height of the cell.
The results of changes in vertical stress (~ cry) at different elevations in cell fill and in
foundation soil within the cell for flood load of 1 y.jl on full outboard height are shown in Fig-
ures 7.10 and 7.11, respectively.
In cell fill (Figure 7.10), the maximum incremental vertical stresses near dredge line and
10 feet above dredge line (El. 73 and El. 80) occur at about 8/5 from center of cell. For El. 90
(20 feet above dredge line) maximum incremental compressive stresses occur near both
sheet piles and maximum incremental negative stress occurs at center of cell. This probably
is due to more prominent effect of interfaces between sheet pile and soil at this level. For El.
116 (14 feet from top) and El. 122 (8 feet from top) the maximum incremental compressive and
tensile stresses occur near outboard and inboard sheet pile, respectively. The stresses are
comparatively quite low at these elevations probably because of less unrestricted movement
of soil elements.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 150
-0.4 -·-- EL-122.0
EL-116.0 EL-92.0 EL- 80.0 EL- 73.0
- -0.3 u. Vl ~ -~-0.2
I_, Dredge line EL '70.0
,.1 ' <l ... Vl Vl w 0:: ..... Vl
...J <{ u ..... 0:: w > z w I,!) z <{ :I: u
-0.1
0.0
0.1
0.2
0.3
0.4
. ' ' ' ' ' ~--
.>·?
¢.. ceu--l I
\ \ \ \ \ \ \
O.SL----l....--L-----'-----11---~--:-:--':""'""" 0 0 10.0 20.0 30.0 40.0 50.0 60.0
ou;ii:r~rd DISTANCE (FEET) ln5~~rd
Figure 7.10. Change of vertical stress in cell fill due to lateral load, Lock and Dam 26 (R) cofferdam.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 151
2.0
-·-- EL-67. 0
1. 6 -·- EL-61.0
----- EL-45.0
u. 1.2 EL-33.0 Vl Dredge I ine EL = 70.0 ~
~ 0.8 <J
<t cell1 9' Vl 0.4 Vl w
I ~ I-Vl _J 0.0 <{ u I-~ w 0.4 > z w 0.8 ~ z <{ :I: u 1.2
1.6
2.0L-~~~~--1-~~.l.-~--L~~--'-~~-'-~ 0 10.0
Cfotboard side
20.0 30.0 40.0 50.0 DISTANCE (FEET)
60.0 Inboard
side
Figure 7.11. Change of vertical stress In foundation due to lateral load, Lock and Dam 26 (R) cofferdam.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 152
For foundation soil within the cell (Figure 7.11), the change in vertical stress follows more
or less similar trend at different elevations. Maximum incremental tensile stresses occur near
outboard sheet pile, while maximum incremental compressive stresses occur at about 8/5
from cell center towards inboard sheet pile, as was observed in case of development of base
pressures. In this case also, rotation of cell takes place about the axis passing through points
at about 8/8 from center of cell towards outboard sheet pile.
7.4 Predicted Response for High Lateral Loads
To study the response and failure mechanism of cofferdam cell during application of high
lateral loads, vertical slice analyses were conducted for Lock and Dam 26 (R). The behavior
of cofferdam was studied in relation to cell deflection, load-deformation response, lateral earth
pressure coefficients and possible failure mechanisms.
7.4.1 Deflection of Cell
The deflected shapes for cofferdam cell for loads 1 y.)J, 2 y.)J, and 4 y.)J are shown in Figure
7.12 and for collapse of load of 7 y.)J in Figure 7.13. The deflected shapes at collapse load are
unrealistic as they represent the configuration of cell just before complete collapse due to
overturning, which normally would not happen because cofferdam would fail due to other
causes prior to collapse. Nevertheless. the deflected shapes give some information about the
deflection pattern of the cell during lateral loading. Results presented in Figures 7.12 and 7.13
indicate that there is a general tendency of lifting up of outboard sheet piles during application
of lateral loads. For load 4 y.)J the outboard sheet pile moves up by 3 inches and for 7 y.)J it
moves up by 6 feet, the maximum lateral deflection for these loads being 11 inches and 9.4
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 153
feet, respectively. The maximum lateral deflections for loads 1 y.jl and 2 y.jl are 2 inches and
3.2 inches, respectively.
The point of rotation (Figure 7.12) during successive application of lateral loads moves from
outboard side to inboard side from center of cell as the load increases. The inboard sheet
pile deflects as cantilever with restraint due to foundation.
7.4.2 Load-Deflection Response
The deflections of inboard sheet pile for different values of lateral loads are plotted in
Figure 7.14. The deflection for a normal flood load which is equal to 1 y.jl is approximately 2
inches. For lateral load of 1 y.jl representing the flood condition, sheet pile deflection is about
1.5 inches. Those for load of 4 to 5 y.jl at which the cell starts to show substantial defor-
mations are 11 to 23 inches. At collapse load of 7 y.jl, the sheet pile deflection, as predicted,
is 112 inches (approximately 9.4 feet). Failure loads predicted based on Terzaghi (1945) and
Schroeder and Maitland (1979) method of vertical shear analysis are also presented in Figure
7.14. These loads are 1.1 y.jl and 2.2 y.jl, the failure load from Schroeder and Maitland
method being twice that from Terzaghi method. The sheet pile deflections at failure loads are
2 and 3.3 inches, as predicted by Terzaghi and Schroeder and Maitland methods, respectively.
The fact that these deflections are much less compared to those corresponding to near failure
loads confirms the idea that conventional design methods are conservative.
The effects of relative movements in cell fill on load-deformation response are discussed
later in the chapter.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 154
.,, ::u m c
~ c ::u m (I)
i (I) m 0 "II
g " > z c c > 3::: N
"' ~ a ~ ~ r-g 2 z C')
... UI UI
130
IU
.... t:i 98 u.. -z Q 82 .... ~ 1£1 jj 66
50
JS
Deflected shape of cell
------------1rr---7 =t·\\ l I
I
:'I t, l
\ . ~\
Original shape of cell
Drtdgt lint
\ \ : \ . I ', I : )i ,/ 1/ ,
\ I I I ,
//---;/-{ /" 1/ I • . ll ~ .. -------;... ". °=·---.-:..- .::::;~-?.}
~ 63.0 Ft j t ln~rd Outboard sidt sidt
Sc alt: 8.0 ft Gt0mtlry
~ Dtfltclions
Figure 7.12. Lock and Dam 26, deflected shape of cell for lateral loads .
1 x Hydrost. load
2 x Hydrost. load
4 x Hydrost .load
130
111.
.... 98 I.LI I.LI lJ..
z 82 0 .... <{ > I.LI _, 66 I.LI
so
JS Inboard
I ·
Depth of Embedment H0 = 35.0 ft.
Original shape of cell
63-0Ft
Deflective shape of cell
Scale
SD Ft Geometry
20A Deflections
Figure 7.13. Lock and Dam 26, deflected shape of cell for collapse lateral load 7ywh.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 156
.,, ::u m g
~ g ::u m (I) .,, 0 z (I) m 0 '"" r-~ " > z g g > ~ N
°' -~ -t 0
E m ::u > r-r-0 > S? z a
... en .....
"'O 111 0 -l
(J •.-i ~
111 ~
C/l 0 S..
"'O >-::c
~-----,~-.--.~.---r~-r--r~i-:~---i 7.0
6.0
s.o
4.0
3.0
2.0
1.0
o.o 0
Cell Width B = 63 ft. Hd = Depth of Embedment
_ .. _____ (.Schroeder, F.S.=l.O )
------ ( Terzaghi, F.S.=l.O)
10 20 30 40 50 60 70 80 90 100 Horizontal Deflections, Ux (Inches)
Figure 7.14. Lock and Dam 26, lateral load versus deflection of sheet plle top
110
7.4.3 Lateral Earth Pressure Coefficient
Investigation of lateral earth pressure coefficients (K) at high lateral loads is considered
important to estimate the failure loads against shear failure in cell fill during lateral loading.
As indicated in Chapter 2, there have been controversies about K value to be used in the
anlyses for vertical shear failure.
Terzaghi (1945) estimated lateral earth pressure coefficient (K) value for lateral loads as
0.4 to 0.6 for cellular cofferdams and recommended the use of 0.4 for analyses. Field obser-
vations (Schroeder et al., 1977) have shown that K may be as high as 0.7 during construction
of cofferdams.
Model studies (Schroeder and Maitland, 1979) on large and small cells indicated that back
filling increased the hoop stress, a function of K, at front sheet piles from 13% to 25% and
decreased hoop stress in back sheet piles by up to 50% over cell filling values. There was
no consistent correlation between depth of embedment and increase in hoop stresses. Con-
sidering an average value of K as 0.42 would mean a range of K as 0.47 to 0.53 for 13% to 25%
increase.
Maitland and Schroeder (1979) indicated the increase in earth pressure coefficient K is
most likely greater near center and lower portion of cell where compression of fill is larger
during application of lateral load.
For lateral loads up to failure due to vertical shear, Schroeder and Maitland (1979) indi-
cated that K values are above both at rest coefficient Ko and Krynine (1945) value. They
suggested that K during overturning and shear distortion can be approximated by unity.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 158
Predicted K-values for hydrostatic load of 3 y.)7 (Figure 7.15) have a range of .44 to 2.2.
Maximum values occur near outboard sheet pile. The values at center of cell range from 0.58
to 0.93. For load 5 y.)7 , the predicted values of lateral earth pressure coefficient are shown
in Figure 7.16. The values near center of cell range from 0.5 to 1.8, the average value being
more than 1.0. Near inboard sheet pile, the values range from 0.26 to 1.7, the average being
approximately 0.75. It could be fairly concluded that near failure load, K values in center of
cell could reach approximately unity or even more than that, and near inboard sheet pile the
average K value could be considered as 0. 75.
Thus, the predicted results of lateral earth pressure coefficients during cell filling and
during lateral loads confirm the field and laboratory observations in general.
7.4.4 Possible Failure Mechanisms
To investigate the pattern of development of failure mechanism in cell fill, stress ratios
(ratio of shear stress to shear strength) for each soil element within cell fill and foundation
were studied at the end of each load step of 1 y.)7 . Elements having stress ratio equal to or
more than 1 (which represents the failure of the element) were marked for a particular loading
stage.
Possible Failure Surfaces
Based on angle e (the angle of major principal plane measured counterclockwise from the
positive Y-axis), obtained from finite element analyses results for soil elements failed in shear,
failure planes directions are determined using details given on Figure 7.17. The direction of
failure planes are then plotted for each failed element. Pattern and sequence of failure sur-
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 159
l ..... ..._ _____ 63.0 Ft
--0.41 0.66 0.93 0.94 0.75
0.6 0.94 0.89 0.81 0.56
0.73 o. 77 0.73 0.58 0.53
0.82 0.76 0.68 0.51 0.5
0.84 0.88 0.77 0.58 0.52 60.0Ft 0.9 0.86 0.63 0.47 0.56
L oaded side~ l.04 0.92 0.61 0.44 0.49
l. l l.09 0.58 0.48 0.46
1.5 0.96 0.62 0.47 0.44
Dredge line-, 2.2 0.92 0.64 0.52 0.5 ,. __ T
2.45 0.87 0.63 0.5 0.43 ~r
l.11 0.41 0.49 0.51 0.53 2.23
35 .. Oft 7.6 0.45 0.38 0.43 0.49 1.8
11. 5 0.41 0.37 0.38 0.39 l. 35
17.1 0.41 0.39 0.41 0.35 1.2
//////777////////777///// //77 /////
Figure 7.15. Lateral earth pressure coefficients (K) for hydrostatic load 3 y wh.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 160
I .... ·------63-0 Ft - r-
0.25 0.9 1. 74 3.2 1. 7 I
0.41 1.14 1.64 1.97 0.92
0.61 1.02 1.53 1.68 0.82
0.91 1.14 1.69 1.17 0.95
1.08 1.42 1.84 1.09 0.79 60.0Ft
L 1.28 1. 71 1. 79 0.69 0.62
oaded side~ 1.6 2.34 1.11 0.58 0.76
1.82 2.59 1.83 0.41 0.31
1. 72 2.88 0.7 0.76 0.26
Dredge Ii ne """\ 4.56 1.6 0.48 0.42 0.34
'~-· 27.8 15.0 1.44 0.43 0.13 ,_,.._
3.94 High 1.6 0.56 0.46
35.0ft High High OL86 1.56 0.52
High High 0.66 0.27 0.42
High High 0.29 0.23 0.31 I
///////////////// // '//////////// //
Figure 7.16. Lateral earth pressure coefficients (K) for hydrostatic load 5 y wh.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 161
faces in cell fill and foundation is then determined based on direction of failure planes of dif-
ferent failed soil elements and also the loading stage causing failure in particular soil element.
The multiple of hydrostatic load causing failure in soil elements is shown in Figure 7.18.
The direction of failure planes and resulting possible failure surfaces are presented in Figure
7.19.
The results show that active and passive failure conditions occur in foundation outside
outboard sheet pile and inboard sheet pile, respectively, for a load of 1 to 2 yjl acting on
outboard side before any failure surface develops in cell fill. The foundation soil within cell
is also subjected to failure near outboard sheet pile, initially.
On further application of lateral load, a curved (convex upward) failure surface develops
in cell fill near dredge line at a load of 4 to 5 yjl . The shape of failure surface could be
considered as nearly circular. This confirms the concept as suggested by Hansen (1953, 1957).
The soil in foundation within cell and in cell fill near dredge line in the vicinity of inboard sheet
pile also starts failing in shear at loads of 4 to 5 yjl , the failure planes being almost vertical.
However, till the failure load of 7 yjl causing tilt of the cell, the vertical shear develops only
up to approximately mid-cell height from dredge line. Thus, at any section, the soil in cell fill
does not fail in shear in full height until collapse. The tendency of vertical shear failure oc-
curring first at center of cell, as suggested by Terzaghi (1945) and confirmed by Schroeder and
Maitland (1979) was not observed as the failure takes place near inboard sheet pile first.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 162
~
Major Principal Plane
.L. Failure Plane 11A11
/ ./
y =45°+:
Inclination of Failure Plane "A"
"' From X-Axis a= (90+9-y) =90+9-45-2
=(45+9-:)
Inclination of Failure Plane 11 8 11
From X-Axis {3 = -(90-9-y)
13: -(45-9- : )
Figure 7.17. Determination of direction of failure planes.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 163
FAlLURE
lxy H w
3xy H w
7xywH.
Loaded side
LOAD
~ ~
- ji--•----63.Q Ft
~
60.0Ft
Figure 7.18. Lock and Dam 26, failed soil elements and failure loads
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 164
Outboard side
LOAD
Dredge line
I ... ·------63. 0 Ft EL 130.0
Inboard side
60.0Ft
otat ion t----"'-+----
ELO.O
Figure 7.19. Lock and Dam 26, failure plane directions and failure surfaces due to lateral loads.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 165
7.4.5 Vertical Displacement of Cell Fill and Slippage of Sheet Piles
During Lateral Loading
As discussed in Section 7.4.4, vertical shear failure planes start developing in cell fill near
inboard sheet pile under high lateral loads, but the cell fill does not seem to fail in shear in
complete height before collapse. Some cases of vertical shear failure in cofferdams have,
however, been noticed. Model studies (Schroeder and Maitland, 1979) have also indicated
development of such failure at high loads. To explain the occurrence of such failures, the
other causes of failures such as vertical displacements of cell fill and possibilities of slippage
of sheet piles during application of lateral loads were studied.
Vertical Displacement of Cell Fiii
During large scale model tests (Schroeder and Maitland, 1979), some terraces were ob-
served at the surface of cell fill near inboard sheet pile and middle of cell during lateral
loading until failure. Vertical displacements of top of cell fill as predicted by finite element
analysis using no soil to soil interfaces in cell fill for lateral load of 3 y..)l are presented in
Figure 7.20. These results show general bodily tilt of cell fill without terrace formation, as
would be obviously expected from this model. To investigate the relative vertical displace-
ments of soil in cell fill, soil to soil interfaces having same angle of internal friction as cell fill
(i.e., 35 degrees) were provided throughout the cell height at a distance of 13 feet and 25 feet
from inboard sheet pile, and finite element analyses were done using different steps of lateral
loading. The intention to provide soil to soil interfaces was to model the vertical displace-
ments of soil more realistically. The results of vertical displacements of top of cell fill for lat-
eral load 3 y..)l from these analyses are also plotted in Figure 7.20. The results show that there
is a relative movement of the order of 0.6 to 0.7 inch in top of cell fill at the location of soil
interfaces and as a result, terraces are formed in cell fill.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 166
~
c 0 .....
6.0
4.
2 .
Depth of embedment Hd=35 ft.
Load = 3y h w
Location of Soil Interfaces~, I I
Without soil y ~
I .u CJ QJ
.-4
...... Q)
Q
l--12 f~l3ft
I .-4 ~ O.q-"~~~~~~~~~_::::.....-~::::::~~:--~~~~~~-l
~ !' ...... : ......... . ,... '"(!) ...... ...... • QJ ' I > ...... ~
-2.0 With soil interfaces
-4.0
OUTBOARD SIDE Distance (Feet)
60 t INBOARD SIDE
Figure 7.20. Lock and Dam 26, vertical displacements at top of cell fill without and with soil interfaces.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 167
To study the impact of providing soil interfaces on sheet pile deflections, the lateral de-
flections of inboard sheet pile top from analyses without and with soil interfaces are shown in
Figure 7.21 for different steps of lateral loadings until collapse. The results show that the trend
of deflection curve is similar in both cases and analyses with soil interfaces obviously yield a
more flexible response. At normal flood load equivalent to 1 y.)J , the deflections of sheet pile
top are within 2 to 3 inches range without and with soil interfaces. However, close to collapse
load, say 6 y.)1 , the deflections in case of model with soil interfaces are 106 inches (8.82 feet)
as compared to 48 inches (4.0 feet) without soil interfaces.
Thus, the finite element model without soil interfaces underestimates the sheet pile de-
flections substantially at high lateral loads. The use of load transfer shear elements as a
connection between outboard and inboard sheet piles may also contribute to some underes-
timation of sheet pile deflections. To represent cell fill soil more realistically, more soil
interfaces should be provided in cell fill to assess the sheet pile deflections at high loads.
However, at working loads of 1 to 3 y.)1, the effect of providing soil interfaces does not signif-
icantly affect the sheet pile deflections. Therefore, the finite element model could be consid-
ered to result in reasonably realistic predictions of sheet pile deflections during application
of normal working lateral loads on cofferdam. Based on deflection data shown in Figure 7.21,
it is recommended that a factor of 1.75 may, however, be used in estimating deflections due
to working lateral loads using the model to account for soil to soil interaction.
Slippage of Sheet Piles
Based on large scale model tests, Schroeder and Maitland (1979) indicated that the slip-
page of sheet pile interlocks occurred in front portion (unloaded side) along with shear dis-
tortion in cell fill under high lateral loads. The picture in the paper (Schroeder and Maitland,
1979) shows that at least 5-6 sheet piles had slipped together.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 168
.,, ::0 m 0 n ;;l 0 ::0 m Cl> .,, 0 z Cl> m 0 "Tl
5 n " > z 0 0 > iii: N
°' ~ a ~ ::0 > r r 0 > 2 z a
.... °' co
"'Cl co 0
..J
u ..... ~
co ~ Ul 0
"' "'Cl >.
::i:
1.0~~--~~..--~-r-~-,~~-,-~-,~~-r~-,.~~,.-~-.~---,
6.0
s.o
4.0
3.0
2.0
1.0
0.0 0
. .,........- ------0------- -- ---.... ...- ...-c With soil interfaces .,..
Without soil interfaces Depth of ernbedrnent Hd = 35 ft
Cell Width B = 63 ft.
10 20 30 40 so 60 70 80 . 90 Horizontal Deflections, Ux (Inches)
Figure 7.21. Lock and Dam 26, effect of soil Interfaces on sheet pile deflections during lateral loading .
100 110
Analyses were therefore conducted to investigate the possibility of slippage of inboard
sheet piles due to lateral load, which could in turn result into failures of cell fill. The cofferdam
dimensions and soil properties used were same as that of Lock and Dam 26.
Axial pull in sheet pile was computed based on average axial forces in beam elements.
The results are multiplied by 1.33 to compute axial pull in one sheet pile which is 16 inches
(1.33 feet) wide. Axial pull for a number of sheet pile together is computed by multiplying this
number to the axial pull for one sheet pile.
Interlock resistance was calculated based on lateral stresses in cell fill near inboard sheet
pile. A friction factor of 0.3 was used between sheet pile interlocks. Total interlock resistance
against slippage was computed using entire height of sheet pile and considering two resisting
interlock surfaces as any slippage would involve at least two resisting surfaces. The sche-
matic representation of slippage of sheet piles on inboard side is shown in Figure 7.22.
Axial pull for different number of sheet piles and total interlock resistance considering two
slipping surfaces were plotted for different number of hydrostatic loads. The results are
shown in Figure 7.23.
When axial pull equals interlock resistance, slippage could occur. The results show that
for any stage of loading the interlock resistance is always much higher than axial pull for one
sheet pile. This suggests that if we consider individual sheet pile, the slippage shall not occur
unless there are interlock misalignment or other sheet pile installation defects. However, just
as an academic exercise, it was assumed that a group of sheet piles could act as one unit as
if there were no intermediate interlocks present. This would mean that although the total
interlock resistance (for two extreme interlocks) does not increase for a group of sheet piles,
the total axial pull is proportionately increased. Thus, based on this assumption, slippage of
the group of sheet piles could occur. The possible number of sheet piles that could be in-
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 170
Vl
ell
0..
- ell ell ..s:: V
l
{-----~-rr---------,---.
\ \ \ \ \ \ \
I I
I I
I
;----
c 0
0 c·-
·-- 0'1'-·-
Vl
1.... 0
oc..
1.... ell
--(1.1
0 O
'l c
0 0
c.. -
c.. ·v; ·;;; 0 a..
"0
1....
0 ell
O-o
-g . i;i
r\_---_i (1.1
O'l
tr
(1.1 1....
0
I I
--:::;,
PR
ED
ICT
ED
RE
SP
ON
SE
OF
LO
CK
AN
D D
AM
26 (R) T
O L
AT
ER
AL
LO
AD
ING
Vl
-c .X
u
ltJ
0 £
1.... «i
ell ...
-c Q
) ... ~ 0
-Q)
::I 'tJ Ill ~
a. ... Q
)
w
Q)
0 ~
Ill
Vl
- 0 0
Q)
Cl
0::: ltJ
~
a. 0
.e-CD
iii z
- 0 c 0 ; ltJ
- c Q)
Ill Q
) ... a. Q
) ... ()
; ltJ E
Q
) ~
()
Cl)
c:"i N
.....: Q
) ... ::I C
l u:
171
...J
...J ::::> a.. ...J < x <
700
600
500
" 1.00 w u z ;:! Vl Vl w a:: :x:: u 0 ...J a:: w .,_ z
300
Ho= 3 5.0 teet
• Interlock resistance
AXIAL PULL
One sheet pile Five sheet piles Eight sheet piles Ten sheet piles
3 " 5 HYDROSTATIC LOAD
6 7
Figure 7.23. Lock and Dam 26, axial pull and interlock resistance in inboard sheet pile due to lateral load.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 172
volved in slip and the hydrostatic load that could cause slip are 10 and 1.7 y.ji . respectively.
For a load of 1 y.ji equivalent to nood load, the number of sheet pile required to act as a unit
for slippage is eleven.
The slippage of sheet piles could be possible during application of normal lateral load, only
if the group of sheet piles could act as one unit. However, this possibility appears to be un-
realistic because during loading, each interlock would start offering resistance to axial pull.
The number of sheet piles required for slippage increases with increase of depth of
embedment, which is quite logical. sheet piles will not slip due to the causes other than
misalignment and other structural defects.
7.5 Summary and Conclusions
Vertical slice analyses using spring elements with an E-ratio of 0.03 up to cell filling and
using shear transfer elements with second modulus reduction factor RF2 of 25 for lateral
loading suggest following:
Deflection pattern of sheet pile resembles cantilever behavior, outboard sheet pile de-
flections being slightly more than those of inboard sheet pile above dredge line and less
below dredge line.
Lateral earth pressure coefficient values in cell fill at the end of cell filling are between
active and at rest earth pressure coefficients and closer to at rest value. The average
value for cell fill soil having friction angle of 35 degrees is approximately 0.42, the range
being 0.37 to 0.49. The range of values suggested by Terzaghi (1945) and Schroeder and
Maitland (1979) are 0.3 to 0.5 and 0.32 to 0.43, respectively.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 173
For lateral loads, Terzaghi (1945) estimated lateral earth pressure coefficient as 0.4 to 0.6.
Schroeder and Maitland (1979) indicated that for lateral loads up to failure due to vertical
shear, lateral earth pressure coefficient value at center of cell fill could be considered as unity.
The predicted lateral earth pressure coefficient values for lateral load 1 y.)1 and 3 y.)1 have a
range of 0.4 to 0.71, and 0.44 to 2.2. respectively. The values at center of cell for load 3 y.)1
range from 0.58 to 0.93. For load 5 y.)1 . the values of lateral earth pressure coefficient at
center of cell reaches more than unity and average value near the inboard sheet pile is ap-
proximately 0. 75.
Under lateral loading, cofferdam cell tends to rotate along some point on the dredge line
which may be at a distance of B/5 to B/8 from center of cell towards outboard sheet pile in-
stead of centerline as suggested by Terzaghi (1945). The pressure distribution at base
(dredge line) is curved instead of linear as assumed by Terzaghi. Interaction between sheet
piles and soil results is substantial reduction of base pressures as compared to those com-
puted based on Terzaghi theory.
Vertical stress distribution in cell fill due to lateral loading show no particular trend. In
foundation, however, the change in vertical stress follows more or less similar trend at dif-
ferent elevation, the zero stress change point being at about B/8 from center of cell towards
outboard sheet pile.
Study of deflected shapes of cofferdam cell, load-deflection curves, failure mechanism and
failure surfaces, and vertical displacements of cell fill without and with soil interfaces and
possibility of slippage of sheet piles due to high lateral loading suggest following.
Although, even at collapse load of 7 y.)1 , the vertical shear failure surface does not de-
velop in full height of the cell fill near inboard sheet pile, it does not necessarily mean that the
cell fill will not fail in vertical shear. The results obtained by inclusion of soil interfaces indi-
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 174
cate relative displacement of soil and formation of terraces. Some soil interfaces show shear
failure. Looking at the impact of both the results of vertical shear failure of soil elements and
the relative vertical slip of soil along soil interfaces, it may be fairly concluded that the cell fill
will fail in vertical shear also at a load of about 5 y..,/1 at which the curved failure surface de-
velops fully.
Slippage of sheet piles could only occur either due to some misalignment and other
structural defects or if a group of at least eleven sheet piles acts as a unit with no resistance
from intermediate interlock. The former problem cannot be accounted for in design. The later
cause seems to be a rare possibility.
Thus, assuming 5 y..,/1 as failure load for shear distortion in cell fill, the deflections of sheet
pile top at this load are 23 inches. Considering a factor of safety of 1.5, the allowable load
would become 3.3 y..,/1 and corresponding sheet pile deflections would be 7.5 inches for Lock
and Dam 26 (R).
Failure loads based on Terzaghi (1945) and Schroeder and Maitland (1979) method for Lock
and Dam 26 are 1.1 y..,/1 and 2.2 y..,/1 and the corresponding sheet pile deflections are 2 inches
and 3.3 inches for Terzaghi and Schroeder and Maitland method, respectively, as compared
to 23 inches from finite element analyses for failure load of 5 y..,/1 . Considering a factor of
safety of 1.5, the allowable loads are 0.75 y..,/1 and 1.5 y..,/1 and corresponding sheet pile de-
flections are 1.5 inches and 2.6 inches, for Terzaghi and Schroeder and Maitland method, re-
spectively; while they are 3.3 y..,/1 and 7.5 inches based on finite element analyses. The
conventional design methods, therefore, yield conservative predictions.
PREDICTED RESPONSE OF LOCK AND DAM 26 (R) TO LATERAL LOADING 175
Chapter VIII
PARAMETRIC STUDIES AND METHODS TO
PREDICT CELL DEFORMATIONS AND FAILURE
UNDER LATERAL LOADINGS
One of the main design conditions for cofferdams occurs when they are subjected to the
lateral loads caused by dewatering and flooding. There is a tendency of shear distortion in
a cofferdam cell fill when lateral load is applied. Failure of cofferdams under these conditions,
however, is rare, and in most cases there is more concern about the magnitude of the defor-
mations that will occur than collapse. Deformation control for the cofferdam system is indi-
rectly insured in conventional design of cofferdams, as it is for many geotechnical problems,
by using what is perceived as an adequate factor of safety against failure. It would be of sig-
nificant importance to estimate the cell deflection at failure and arrive at allowable value
based on appropriate factor of safety. The performance of the cofferdam could then be mon-
itored in the field effectively as the instrumentation is generally done to measure cell de-
flections.
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 176
The methods for calculating the factor of safety against collapse for a cofferdam under
lateral loading are described in Chapter 2. The most widely accepted technique for deter-
mining the factor of safety against collapse during lateral loading of a cofferdam was proposed
by Terzaghi (1945). There are two key aspects to the Terzaghi technique: (1) the cell fill is
assumed to fail along a vertical shear plane that passes through the center of the cell; and (2)
the lateral stresses acting on the vertical shear plane are assumed to be defined as the ver-
tical gravity stress in the cell fill multiplied by the lateral earth pressure coefficient of the cell
fill (usually taken to be 0.5). As noted in Chapter 2, a number of investigators have questioned
one or both of Terzaghi's assumptions, with most noting that they lead to overly conservative
answers for design.
Hansen (1953, 1957) suggested curved failure surfaces near dredge line and foundation
during application of lateral loads. Esrig (1970) had indicated that vertical shear concept is
invalid. Cummings (1957), working from observations on very small model cells with very rigid
sheet piles, proposed a method of analysis based on horizontal shear concept. Maitland and
Schroeder (1979) indicated that Cummings' method overestimates moment resisting capacity
of cells with embedded sheet piles.
Large scale model tests (Schroeder and Maitland, 1979) indicate that Terzaghi's vertical
shear concept is valid. There was no evidence in either the large or small scale model fail-
ures indicating a convex or concave circular or logarithmic spiral slip plane, as has been re-
ported in previous model studies. Therefore, to investigate further the response and failure
mechanism in cellular cofferdams due to high lateral loads, parametric analyses were done
using modified plane strain program SOILSTRUCT.
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 177
8.1 Parametric Studies
The study of response and failure mechanism under lateral load for Lock and Dam 26 (R),
discussed in Chapter 7, demonstrated the need for conducting some parametric studies to
investigate the effect of depths of embedment and cell width on sheet pile deflection and to
study the failure mechanism due to lateral loading for different size cofferdams and different
depths of embedment.
Including analyses done for Lock and Dam 26, presented in Chapter 7, finite element ana-
lyses were done using following set of parameters:
Cell Free Cell Depth of Hydrostatic Width Height Embedment Loads (8) Feet (H) Feet (Hd) Feet Applied
63 60 10 1 to 5 ywh 63 60 21 1 to 7 ywh 63 60 35 1 to 7 ywh 40 50 10 1 to 3 ywh 40 50 20 1 to 5 ywh 40 50 35 1 to 5 ywh
Separate analyses were also conducted for cell width of 60 feet and depths of embedment
of 21 and 35 feet providing soil to soil interfaces in cell fill. The soil types used were as given
in Table 3.2 for Lock and Dam 26 (R). The water level was 28 feet below top of cell for B = 63
feet and 25 feet below top of cell for B = 40 feet. Cell width B = 63 feet, free cell height H = 60
feet and depth of embedment Hd = 35 feet represents Lock and Dam 26 (R), stage one
cofferdam.
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 178
E-ratio of 0.03 was used up to cell filling. During application of lateral loads, second
modulus reduction factor (RF2) of 25 was used for shear transfer elements. The first modulus
reduction factor (RF1) was computed based on H/B ratio.
Lateral loads mentioned above were applied in full free height of outboard sheet pile in
steps of 1 y.jl . The stresses in soil of cell fill and foundation were studied for each step of
load.
The model tests conducted by Schroeder and Maitland (1979) had indicated that sheet piles
had undergone large amount of deflections under lateral loads before failure due to shear
distortion of cell fill occurred. The above mentioned hydrostatic loads were, therefore, applied
in finite element analyses to obtain maximum possible sheet pile deflections before tilting of
the cell.
8.1.1 Deflected Shapes of Cell
The deflected shapes of cells of cofferdam having cell widths of 63 feet and 40 feet and
depth of embedment of 35 feet are shown in Figure 8.1 for flood load of 1 y.jl. These results
show that trend of deflection in both cases is similar. Maximum lateral deflection for cell
widths 63 and 40 feet are 1.3 and 1.5 inches, respectively. Thus, for similar type of loading 40
feet cell deflects more than 63 feet cell. This is because the slenderness ratio H/B for 40 feet
cell is 1.25 as compared to 0.94 for 63 feet cell. However, below mudline, the deflections in
both cases are of the same order.
Analyses were done for a cofferdam having cell width B = 63 feet and free cell height H = 60
feet (same as Lock and Dam 26 (R)) and depths of embedment, Hd of 10, 21 and 35 feet to study
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 179
the deflected shape of cell before collapse under application of lateral loads. Results for depth
of embedment of 35 feet are already discussed in Chapter 7. The soil properties used and
water level were same as described in Chapter 7. The deflected shapes just before collapse
are shown in Figure 8.2.
During lateral loads, outboard sheet piles moved up substantially and inboard sheet pile
moves down very little except for depth of embedment of 10 feet in which case it moves down
by 6 inches (Figure 8.2). The sheet piles on inboard side deflect as cantilever. The outboard
sheet piles move up by approximately 1, 7.8 and 6 feet for depths of embedment of 10, 21 and
35 feet, respectively, before collapse. The horizontal deflection of sheet pile tops are 2.4, 10.8
and 9.4 feet for Hd = 10, 21 and 35 feet, respectively. The movements of sheet piles for Hd
= 21 feet are more than those for Hd = 35 feet. This is because same hydrostatic loading of
7 y,)I was applied before collapse. In fact, for same deflections, the lateral load for Hd = 21
feet would be lesser. Because the loading was applied in steps of 1 y,)I , the load of 7 y,)I
was considered for both cases as a condition before collapse.
Thus, there is a general tendency of lifting up of outboard sheet piles during overturning.
For Hd = 10 feet, the cell can withstand much less deformations before collapse as compared
to Hd = 21 feet and 35 feet.
For loads just before collapse, the cell with Hd = 10 feet has rotating tendency about some
point near center at dredge line. The applied load before collapse is 5 y,)I as compared to 7
y,)I applied for Hd = 21 and 35 feet. For Hd = 21 and 35 feet, the cell rotates about a point very
near to inboard sheet pile just before collapse.
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 180
60ft. l 50ft.
35ft.
l
Original shape of 63ft wide cell
Original shape of 40ft wide cell
r-----L--r---if-----=--.., _ - - --, . I
I I
I I I I L_
I
I I
I I I I
I I
/ I
/ I .
r-·-·-1 ·-. . I .
I I
1· JJl'C:-// .. \\C:li·b
l I I I -:..::::.-:_- -
I I
I I
·-·-·; I . I J I / / i I
. I I I
/~•fleeted shape · , of 40ft wide cell
I I / I »""';>1AJ Dredge line
I I
I ~Deflected I 63ft wide I I
shape of cell
·-- ...... :- -....J
I..,.•....---- 40f t. Scale:
._., _____ 63ft.-----~ _z_o_._o_f_t_. _Cell geometry
l.Oinch Cell deflection
Figure 8.1. Deflected shapes of 63 feet and 40 feet wide cells for load 1 ywh
Parametric Studies and Methods to Predict Cell Deformations and Failure Under Lateral Loadingir 181
130
114
.... 98 LLJ LLJ LL
z 82 0 .... < > LLJ _, 66 LLJ
so
35
Ho = 35.0Ft ( 7 x hydrostatic load)
Ho = 21. 0 Ft ( 7 x hydrostatic load)
Ho = 10. 0 Ft ( 5 x hydrostatic load )
Original shape of cell
Inboard 1~·-------6~0Ft--------~
Deflected· shapes ·~of cell
-~-~ ---, I I I I I I I I I I I I I I I I I I
J.
I I/
Scale
8.0 Ft
2 OFl Geometry
Deflections
Figure 8.2. Deflected shapes of cofferdam cell for collapse lateral load.
Parametric Studies and Methods to Predict Cell Deformations and Failure Under Lateral Loadings 182
: iii 3 ID .. .. n en .. c CL ii Ill II
&. ;: !l ':r'
8. Ill
~ "'O Cil CL ~ n == 0 ~ .. 3 ! 0 :i Ill • :i CL
~ c Cil c :i CL ID .. i !. b g_ ;-~
.... OI w
Deflected of cell
130
114
.....
~ 981 I (/ z 2 82 .... ~
~ 661 ........
so
35
I. 63.0 Ft
t Outboard
sidt
Original shq>t of cell
t ln~rd
Stdt
Out board 1hcct ~Ile
1111111111
I 12>9 ,~· Hft j_
Sea It:
Element 237 to 239 eacovoted to model seour
4 • Hydrost. load wilhout scour
-tt- t, !I Hydrost.load with scour
8.0 fl Gtomttry
2.0 in Otfltctions
Figure 8.3. Deflected shapes of cofferdam cell with and without scour.
Effect of Scour:
To study the impact of scouring on sheet pile deflections and failure, analysis was also
done with excavation of foundation soil up to failure, 20 ft, outside outboard sheet pile and
application of lateral loads. The deflected shape for load 4 y.,jl before collapse is presented
in Figure 8.3. Also shown is the deflected shape for 4 y.,jl without scour effects.
Due to scouring the load before collapse is reduced from 7 y.,jl to only 4 y.,jl for Hd = 35
feet. Outboard sheet pile moves up by 5.0 inch for scouring and 2.8 inches for no scouring for
a load of 4 y.,jl . Inboard sheet piles move down about 2.5 and 2 inches, respectively. The
maximum horizontal deflection of sheet pile top are 16 inches and 11 inches for scouring and
no scouring, respectively.
Thus, scouring substantially reduces the capability of the cell to withstand the overturning
load and to undergo deflections before collapse.
8.1.2 Effect of Depth of Embedment on Sheet Pile Deflections Due to
Lateral Loading
Maximum sheet pile deflections for cell widths of 63 feet and 40 feet and various loading
levels are plotted in Figure 8.4 against depth of sheet pile embedment. The deflections as a
percentage of free cell height are presented in Figure 8.5 for both cell widths of 63 feet and
40 feet. These results indicate the following:
• For both cell widths, the sheet pile deflections for depth of embedment Hd of 10 feet are
slightly higher than those for Hd of 20 feet and 35 feet. At normal flood load of y.,h , these
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 184
-.c u c:
25
!j 20 c: 0 ..... µ u QI
..-1 ~ 15 A QI
r-1 ...... c:i. µ QI
~ 10 Ul
H/B=0.94 , load 3Ywh
0 \
\ \ \ \ \ \ \
\
H = Free cell height B
H/B = Cell Width Slenderness ratio of cell
= Hydrostatic load
\(H/B=l.25,load 3yw11
\ \ \ \ \ \ \
Go--- -- -------e--
H/B=l.25,load lYwh ~ H/B=0.94,load lYwh
---.4-13------L=@ - ---~ 0 ~~~~~~~""-~~~~~~-'-~~~~~~-£--~~~~~~~ o.o 10.0 20.0 30.0 40.0
Depth of Embedment (Feet)
Figure 8.4. Effect of depth of embedment on sheet pile deflection during lateral loading.
Parametric Studies and Methods to Predict Cell Deformations and Failure Under Lateral Loadings 185
values range from 2 to 2.5 inches. The difference becomes substantially more at high
lateral loads. For example, for load of 3 y.)J , the deflections for cell width of 63 feet are
8.6, 6.2 and 6 inches and for cell width of 40 feet. they are 26.5, 9.3 and 8.4 inches for
embedment depths of 10, 20 and 35 feet, respectively.
• Increase in depth of embedment from 20 feet to 35 feet has insignificant change in sheet
pile deflections.
• At normal flood load of y.)J , the deflection of sheet pile top could be estimated as 0.35%
to 0.28% of free cell height (Figure 8.5) for cell width ranging from 40 feet to 63 feet for
depths of embedment values from 10 to 35 feet. At working flood load, thus, the per-
centage of deflection to cell height is not much influenced either by depth of embedment
or by cell width for usual size of cofferdams. At higher lateral loads, however, the influ-
ence of depth of embedment below 20 feet and the cell width becomes more significant.
8.1.3 Load Deflection Response of Cell
The sheet pile top deflections due to lateral loads for cell widths of 63 feet and 40 feet and
for different depths of embedment are presented in Figures 8.6 and 8. 7, respectively. The
load-deflection curve for Lock and Dam 26 with depth of embedment of 35 feet was discussed
in Chapter 7. These results show that the deflections for depths of embedment of 20 feet and
35 feet are not significantly different, even at high lateral loads. Failure load for depth of
embedment of 10 feet is about 60 percent lower than those for depths of embedment of 20 and
35 feet for cell widths of 64 feet as well as 40 feet.
For working flood load of 1 y.)J , the sheet pile top deflections range from 2 to 2.5 inches
for depths of embedment of 10, 20 and 35 feet for cell widths of 63 and 40 feet.
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 186
0 0 -
5.0
~ 4.0 ~ .c: 00 ~ Q)
:::::: ..-4
~ 3.0 u -c: 0
..-4 ~
CJ
~ 2.0 ..... Q) 0 ..-4 ..-4 Q)
~ 1.0
\ \ \ \
B = Cell Width Hydrostatic load
\~ B=40ft.,load
\ \
\ \
\ \
\
' '0----- - - "7-----e---B=6Jft., load 3Ywh
B=40ft.,load lYwh ~B=63ft.,load lYwh ::.::$"----~~----------~
Depth of Embedment (Feet)
Figure 8.5. Sheet pile deflection as percentage of cell height for different depths of embedment and cell width.
Parametric Studies and Methods to Predict Cell Deformations and Failure Under Lateral Loadings 187
: D1 3 ! .. n ~ c ICI. ii' II DI ~ ICI. 3:: CD ... -:r 0 ICI. II
S' ,. iiJ ICI. !l n ~ 0 CD O' .. 3 a 0 ~ II 1111 ~ ICI.
"" !. c iiJ c ~ ICI. CD .. r-i !. b DI ICI. :r
IQ II
.... m m
7~0r-~-,~~-,.~~-,-~~-,-~~.-~~.-~~r-~--ir--~---i-~~-.-~~-
6.0
'"Cl s.o CIJ 0
...l
CJ
'" "" 4.0 CIJ
"" Cll I .
0 i... yl ~ 3.0
::c:
2.0
1.0
o.o 0 10
/
.>?/' /
20
--- --- -- -..... ~ -- ·~---Hd=35 ft.
/
-· _.0-. - .r- Hdc:lO ft --· . L-. - . ~ -· -· -·-· -·-·-·-·-·0
30
Cell Width B = 63 ft. Hd = Depth of Embedment
40 50 60 70 80 . 90 100 Horizontal Deflections, Ux (Inches)
Figure 8.6. Lateral load vis deflection of sheet pile top for cell width of 63 feet.
110
.,, DI .. DI 3 CD ... .. n (II ... c a. i" • • :I a. i: CD ... -:r 0 a. • ... 0 .,, ; a. fl (")
~ g CD O' .. 3 a 0 :I • DI :I a. "Tl !!. c .. • c: :I a. CD .. ! CD .. !. b DI a. ;-
u:i •
... m co
"C Ill 0
...:i CJ
•r-4 ~
Ill ~ (/) 0 ....
"C >. =
7.0r-~~r-~-y-----,i----.----,,---,~--,~--,.---.----.-~--
6.0
s.o
4.0
3.0
2.0
1.0
Hd=35 ft. _... .... -0"-
// //
// <: :J"r.v',.. Hd=20 ft /p •
Cell Width B ~ 40 ft.
Hd • Depth of embedment
L " =10 f !':\.-. d t. --~ -· _/' ·-/ ·--· yr/ -·-·-·-
o.o~---1----L----L.----'----'----l----'---........ --_._--_._--__. 0 10 20 30 40 50 60 70 80 90 100 110
Horizontal Deflections, Ux (Inches)
figure 8.7. Lateral load v/s deflection of sheet pile top for cell width of 40 feet .
8.1.4 Vertical Displacement of Cell Fill and Slippage of Sheet Piles
As discussed in Chapter 7 for Lock and Dam 26 case with depth of embedment of 35 feet,
vertical displacement of cell fill and possibility of slippage of sheet piles were also investi-
gated for different depths of embedment to study their impact on failure of cell fill.
The results of vertical displacements of cell fill top without and with soil to soil interfaces
for depth of embedment of 21 feet show similar results as for the case of 35 feet. Inclusion
of soil interfaces results into relative soil displacements of about 1.3 inches and formation of
terraces. The load-deflection curve for 21 feet embedment also shows similar behavior as
noticed in case of 35 feet embedment.
The slippage of sheet piles was also investigated for sheet pile embedments of 10 and 21
feet. These results lead to similar observations as noticed in case of 35 feet embedment,
discussed in Chapter 7. As per results, the slippage of sheet piles could only be possible if
a number of sheet piles acts as one unit together, and there is no resistance from intermediate
interlocks.
8.1.5 Failure Mechanisms Under Extreme Lateral Loadings
Possible failure surface and mechanism during lateral loading for Lock and Dam 26 (R)
was discussed in detail in Chapter 7. The lateral loads, failure of different soil elements, the
failure planes and failure surfaces for cell width of 63 feet and depth of embedment of 10 and
21 feet and for cell width of 40 feet and depths of embedment of 10, 20 and 35 feet are given
in Appendix B.
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 190
~ 60.0 cu u.. -• ..... cu ~ 'g 40.0
VJ
~ ;:I
~ u.. "lj 20.0
~ 'O ~
B = Cell width
B = 63 fit=> --e--·-----0--- ~--~-8-~·L-------8----- ~ B =· 40 ft.
... o.o· L--~--------r--------,----, ~
-~ 40.0 ........ cu .s
...:l ~
~ 30.0
~ 0 v
c:Q i:: -~ 20.0 cu -0 0:: ..... 0 .... cu
~ ..... 0
10.0
s.o 10.0 20.0
Depth of Embedment Hd (Feet) (A)
3o.o.
B = Cell width
35.0
0.0.L--,---------,-------.-----, s.o 10.0 20.0 30.0 35.0
Depth of Embedment Hd (Feet)
(B)
Figure 8.8. Radius and center of rotation of curved failure surface.
Parametric Studies and Methods to Predict Cell Deformations and Failure Under Lateral Loadings 191
As noticed for Lock and Dam 26 (R) case in Chapter 7, at certain lateral load, the curved
failure surface develops in cell fill near dredge line and vertical shear failure starts near in-
board sheet pile in all the cases studied. The curved failure surfaces are approximated by a
circular surface for simplicity. Although the rotation of cell generally occurs along an axis
passing through points at approximately 8/8 (i.e., 8 feet for 8 = 63 feet) from center of cell to-
wards outboard sheet pile as discussed in Chapter 7, it can be assumed to simplify the ana-
lyses that the center of rotation lies along center line of cell.
The details of circular failure surfaces for different values of cell width, cell height and
depths of embedment are given in Table 8.1. The radius of the curved surface increases as
depth of embedment increases. The center of rotations is lower for higher depth of
embedment. Figures 8.8(A) and 8.8(8) show relationship between depth of embedment Hd to
radius of curved failure surface "r" and distance of center of rotation from dredge line, re-
spectively, for cell width 8 = 63 feet and 40 feet. The relationship is approximately linear.
8.2 Proposed New Method For Determination of Lateral
Capacity of Cellular Cofferdams
Conventional theories devised by Terzaghi (1945) and Schroeder and Maitland (1979) for
vertical shear analyses were discussed in Chapter 2. These methods assume vertical shear
failure plane at center of cell fill. As discussed in Chapter 7 and previous section, the results
of finite element analyses indicate that a curved failure surface develops in cell fill near
dredge line and vertical shear failure surface starts developing in soil near inboard sheet pile
at high lateral loads. A new method is, therefore, proposed in this section for analyses of
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 192
Table 8.1
Circular Failure Surfaces
Curved Failure Surface Details Cell Free Depth of Hydrostatic Center of Width Cell Embedment Radius Failure Rotation B H Hd r Load Below Dredge Line (feet) (feet) (feet) (feet) (xywh) (feet)
63 60 10 35 4 to 5 25.0 63 60 21 39 5 to 6 30.0 63 60 35 46 5 to 7 35.0 40 50 10 28 3 20.0 40 50 20 32 4 to 5 25.0 40 50 35 38 4 to 5 33.0
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 193
shear distortion failures in cell fill due to lateral loads, accounting for both curved failure sur-
face as well as vertical failure surface.
As indicated in Chapter 7, active and passive failure conditions develop first in foundation
soil outside outboard and inboard sheet piles during lateral loading. The resistance of these
surfaces is, however, neglected in this proposed analysis.
Development of curved failure surface near dredge line generally starts with the develop-
ment of vertical shear planes in the soil near inboard sheet pile. However, the curved failure
surface normally gets formed completely before the vertical shear failure progresses up to
mid-height of the cell (Figure 7.18 and Appendix 8). The resistance due to the curved surface
is computed using Figure 8.9. The center of rotation is assumed to lie on the center line of
cell.
The resultant load P is acting at a distance H1 from dredge line . The computation of
overturning moment Mo due to this load is discussed later.
Radius r of the failure surface is computed using Figure 8.8 and angle 2a in degrees is
determined accordingly.
Approximate distance of top of curved surface from dredge line h = r(1-cosa). Due to
lateral loads, vertical stresses increase on inboard side and decrease on outboard side.
Vertical stress is considered at h/2 from dredge line due to cell fill to compute average re-
sistance of curved surface. Initial vertical stress after cell filling may be considered.
cm = vertical stress <JY at distance h/2 from dredge line
s = length of curved surface = 2ar x n/180 = nar/90
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 194
Sheet pile
Resultant Load P
HI
Hd he
B
~
I
Curved failure surface
I
' / './" / ' / ' / ' / ' 2a / ' . /
/
/ /
/
'~ '~/Center of rotation
H
Dredge line
Figure 8.9. Shear failure analysis with curved failure surface.
Parametric Studies and Methods to Predict Cell Deformations and Failure Under Lateral Loadings 195
Approximate shear resistance per unit length of curved surface = cm tan <P
where:
<p = friction angle of cell fill.
Total resistance of curved surface F,1 = crn tan <p x n9~ .
Resisting moment MR1 = F,1 x r,
2 MR1 = (crn tan <p) nar
90 [8.1]
Assuming that vertical shear planes could develop in full height of cell due to vertical shear
failure of soil near inboard sheet pile and due to relative displacement of soil in cell fill be-
cause of soil to soil interaction, a modified method of analysis for vertical shear is suggested
as an improvement over Terzaghi's method (1945) of analysis.
This method assumes the development of vertical shear plane near inboard sheet pile
based on the observations made in the analyses. The center of rotation based on analyses
results is considered at a distance of B/8 ( ~ 8 feet for B = 63 feet) from center of cell toward
outboard side. As vertical failure surface would develop at some distance near the inboard
sheet pile, the horizontal distance between this surface and center of rotation could be as-
sumed as B/2. For simplifying the analysis, it could be assumed that the vertical shear plane
would develop at the contact of sheet pile and soil and the center of rotation lies at center of
cell (Figure 8.10).
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 196
Resultant Load P
1-11
Hd I I I I I I I -----_;;'
Center of rotation I (Based on analyses)
1 ..
B
(t I
Vertical failure I surface
·I N
~ t ~ ~ ~
H
~ ~ ~
~ ~ ~ ~ ~
J..-Center of ro~tion I (Assumed at center line)
I• 8/2 •I
::::: B/2 • I
Inboard Shcetpile
Dredge line
Figure 8.10. Shear failure analysis with vertical failure surface.
Parametric Studies and Methods to Predict Cell Deformations and Failure Under Lateral Loadings 197
Mo = overturning moment
MRz = total resisting moment of soil and sheet pile interlocks = Q x 8/2
Q =Sc+ Sc'
where:
Q = total shear resistance of soil and sheet pile interlocks
Sc = shear resistance of soil in cell fill and foundation
Sc' = shear resistance of sheet pile interlocks.
Sc = Pc' tan <P'
where:
Pc' = total lateral pressure acting on failure surface N-N
<P' = friction angle of soil in particular reach
Total interlock force T = (Pd - Pu) x R
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 198
Total resistance of interlocks T x f = (Pd - Pu) x R x f
where:
Pd = total inside force on inboard side
Pu = total outside force on inboard side
R = radius of cell
f = friction factor = 0.3
This total resistance of interlocks is for one interlock. The failure of soil occurs near in-
board sheet piles, say at distances of about D/8 from inboard sheet pile, where D = cell di-
ameter. Considering an isolated circular cell the total length of chord on which failure is
assumed (Figure 8.11) will be approximately 4/3 R, where R = radius of cell, and since we
considered only one interlock, the applicable length of failure would be 2/3 R.
Thus, average resistance of interlock is Sc' = (Pd - Pu) x R x f x 2~
or Sc' = 3/2 (Pd - Pu) f.
Q = Sc + Sc' = Pc' tan <P + 3/2 (Pd - Pu) x f
MRZ = Q x B/2
= Bl2(Pc' tan <P' + 3/2(Pd - Pu)xf] [8.2]
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 199
Sheet piles
OUTBOARD SIDE
Cell fill
D
/ /
/ ol // . -- . _______ ;;:_. __ -· r- ~R
9 RZ mn = .JRz -15
~1-R -3
Failure surface
n INBOARD SIDE
Figure 8.11. Cofferdam circular cell, location of vertical shear failure surface.
Parametric Studies and Methods to Predict Cell Deformations and Failure Under Lateral Loadings 200
Coefficient K of lateral earth pressures used in analysis was 0.75 as during lateral load of
5 yjl average K value adjacent to inboard sheet pile were predicted as approximately 0.75
(Chapter 7).
Free body diagrams considering all forces for both curved and vertical failure surfaces is
shown in Figure 8.12. As cell fill weight "w" passes through center of rotation, it has no effect
on moments.
Considering the resistance due to both curved and vertical failure surfaces, total resisting
moment,
MR = MR1 + MR2 = (crn tan <P) ~~ r 2 + ~[Pc' tan q>' + 3/2(Pd - Pu)f] (8.3]
value off is usually taken as 0.3.
M Factor of safety = M~ .
Figure 8.8(8) can be used to determine depth of center of rotation below dredge line. The
overturning moment is computed about the center of rotation (Figures 8.9 and 8.10).
Overturning moment Mo = P(H1 + he)
P = resultant lateral load
H1 = distance of line of action of P from dredge line.
he = distance of center of rotation below dredge line.
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 201
8.2.1 An Example Problem to Compute Failure Load
As an example, consider Lock and Dam 26 (R) cofferdam with B = 63 feet, H = 60 feet,
Hd = 35 feet, water level at 28 feet below top. Cell fill and foundation soil friction angles are
35 and 41 degrees, respectively. The cofferdam is subjected to lateral load.
Curved Failure Surface:
From Figure 8.8, the radius of curved failure surface, r, is 46 feet and location of center of
rotation below dredge line , he, is 35 feet.
2a is angle of curved failure surface.
cosa = h; = ~~ = 0.76
a= 40.5°
h = r - he = 46 - 35 = 11 feet
CJn at 5.5 feet from dredge line
= 123 x 28 + 70.6(32 - 5.5)
= 5315 psf
Resistance of curved surface F,1 = CJn tan <p x ~~
= (5315 x tan 35 x 7t x 40.5 x 46)/90
F,1 = 242kips
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 202
Resisting Moment MR, = 242 x 46 = 11132 k. ft.
Vertical Failure Surface:
Using k = 0. 75,
Lateral earth pressures:
At 28 ft from top = 0. 75 x 123 x 28 = 2583 psf
At 60 ft from top = 2583 + (0. 75 x 70.6 x 32) = 4277.4 psf
(At dredge line)
At 35 ft below dredge line = 4277.4 + (0.75 x 70.6 x 35)
(Tip of sheet pile)
= 6130.7 psf
Resistance of cell fill along vertical failure plane:
Sc = (2583 x 14 x tan 35)
( 4277.4 + 6130. 7 x 35 x tan 41) 2
= 260.5 kips
Resistance of sheet pile interlocks:
Sc' = 1._ (Pd - Pu)f 2
+ ( 2583 + 4277.4 x 32 x tan 35) 2 +
Assuming maximum pressure at H/4 from dredge line, and K value near sheet pile as 0.4,
Pd = 0.4 x ~ x 123 x 45 x 95 = 105.2 kips
· Assuming dewatering completed before flooding, Pu = 0.0.
Sc' = ~ x 105.2 x 0.3 = 47.3 kips
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 203
Total resistance:
Q = sc + sc'
= 260.5 + 47.3 = 307.8 kips
Resisting moment MR 2 = Q x ~
= 307.8 x 623 = 9695.7 k. ft.
Total resisting moment MR = MR, + MR2
= 11132 + 9695.7
= 20827.7 k.ft.
Considering that there are n units of hydrostatic load required for failure:
Overturning moment M0 = n x ~ x 62.4 x 602 x (20 + 35)
= n x 6177.6 k.ft.
At failure, M0 = MR
n x 6177.6 = 20827.7
n = 3.4
Therefore, 3.4 times the normal flood load (3.4 y.jl) will result in shear failure in cell fill.
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 204
~~ -t:o m,.. :Os: )."' r- -t r-:o o-,..n 0(1) --1 Zc a o (I)-m
(I)
). z 0 s: ~ p 0 0 (I)
6 H, ,, :0
"' 0 ii -t n "' r- he r-0 m .,, 0 :0 s: ). ::! 0 z (II
). z 0 .,, ~ r-c :0
"' c z 0 m :0
~ "'
i r i B ·1 I I I I w
I · center of I rotation 14 ~s12 •I
(a) Failure surfaces and forces
p
(H1+hc)
~ I I
I I I I !w
( b) Free body diagram
Figure 8.12. Schematic representation of failure surfaces and free body diagram showing forces.
Q
8.3 Comparison of Shear Failure Analyses Methods
Load-deflection curves for cell widths of 63 and 40 feet and for different depths of
embedment were discussed in Chapter 7 and earlier in this chapter. On these curves are
plotted the predictions of failure loads based on Terzaghi (1945), Schroeder and Maitland
(1979) and proposed new method for analysis of shear distortion failure, and the results are
shown in Figures 8.13 and 8.14 for cell widths of 63 and 40 feet. respectively. These results
suggest following:
Terzaghi and Schroeder and Maitland methods give same failure load for all depths of
embedments because overturning moments are computed at the end of sheet pile or the point
of fixity, and the vertical shear resistance is calculated for cell fill and foundation up to same
depth. In case of new proposed method, the failure load is higher for higher depth of
embedment because the overturning moment is computed about center of rotation and shear
resistance is calculated up to depth of embedment. Logically also, the higher depth of
embedment should give higher failure load. For cell width of 63 feet, the predicted failure
loads (Figure 8.13) based on proposed new method are 2. 7 to 3.4 y.)1 which are about 23 to
52 percent higher for different depths of embedment than the failure load based on Schroeder
and Maitland method. The resulting deflections for depth of embedment of 21 or 35 feet are
2, and 3.3 inches based on Terzaghi, and Schroeder and Maitland method, respectively, and
are 5.5 and 8 inches for depth of embedment of 21 and 35 feet, based on proposed new
method.
In case of cell width of 40 feet, the predicted failure loads (Figure 8.14) based on new
method are 2.3 to 2.5 y.)1 , which are about 30 to 50 percent higher for different depth of
embedments than the failure load based on Schroeder and Maitland method. The corre-
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 206
!;:~ "1;u ;u )lo )lo s: ,..~ ,.. ::0 o-:Pn c en z~ "c en -'" en
)lo z c s: ~ 0 c en d '11 ::0
'" c r; ~ (") m ,.. ,.. c m "Tl 0 ::0 s: )lo ::I 0 z (I)
)> z CJ "Tl ~ r-c ::0 m c: z CJ m ::0
N 0 ...,
"'O C1I 0
..J
u ·~ ~
C1I ~
Cll 0 ...
"'O >. ::r:
7.0--~---,.--~--.~___, ........ ___,~--___,~--___,~--___,___,..,_~~.--~--.___,___,__.~~--
6.0
s.o
4.0
3.0
2.0
.~---- ______ ............ -,...~~-21 ft.
.,.. .,.. ~.,...,...
.,...,.. Hd•lO ft. __..0-·-·~-·-·-·-·-·-·--·-·--·0 ...-· ,,,..
/ /
~· /
_L_Hd•".lc:F .. _}
!f..'_~ H;;: _ (New Propo:ed Method) ------·- . F.S. 1.0
I Hd•lOft ·-----(Schroeder Method, F.S.=1.0)
Cell Width B • 93 ft.
Hd • Depth of Embedment
l.O ldi'l------(Terzaghi Method, F.S.=1.0)
o.o 0 10 20 30 40 50 60 70 80 90
Horizontal Deflections, Ux (Inches)
Figure 8.13. Comparison of shear failure analyses methods, load-deflection curves for cell width 63 feet.
100 l l 0
~~ ... :u '"» :u 3:
~m o-»n CHll zc! C>o en-m
(II
)> z CJ 3:
~ 0 0 (II
cj -0 :u m CJ n ... n m ,... ,... CJ m ,, 0 :u 3: ~ 0 z (II
)> z 0 .,.. )> ;= c :u '" c z CJ
'" :u
N 0 00
'tJ t'O 0 ~
u •.-1 4..1 t'O 4..1 (/) 0
'"' 'tJ >. :I:
7.0--~--..--~-.-~~---~~..,..-~~-.-~~--~~....-~--..--~--..~~-.....~~~
6.0
Cell Width B = 40 ft. 5.0 Hd•3~ ft.
Hd • Depth of embedment
4.0
Hd=lO ft.
.--G·-·-·L-·-·-·-·-·-'/ - . ,/' -~-===}New Proposed Method, F. S .•l. O -r----- ( Hd=l0,20 and 35 ft.)
~ fl --r----- Schroeder & Maitland, F. S .=1. O
3.0
2.0
1.0 Terzaghi, F.S.=1.0
o.00~---,1;~--;;;;---~::-----:-7-----::-!---~-----1-----L---__L ____ .L_ __ _J 10 20 30 40 50 60 70 80 100 90 110
Horizontal Deflections, Ux (Inches)
Figure 8.14. Comparison of shear failure analyses methods, load-deformation curves for cell width 40 feet.
spending deflections are 2, 3.3 and 7.3 inches based on Terzaghi, Schroeder and Maitland and
new method of analysis for depths of embedment of 20 and 35 feet. For embedment depth of
10 feet, the deflections are 3.5, 5.5 and 11 inches based on Terzaghi, Schroeder and Maitland
and new method, respectively.
Thus, the proposed new method yields substantially higher failure loads for shear dis-
tertian failure and larger deflections at failure in cofferdams as compared to conventional
methods.
PARAMETRIC STUDIES AND METHODS TO PREDICT CELL DEFORMATIONS AND FAILURE UNDER LATERAL LOADINGS 209
Chapter IX
SUMMARY AND CONCLUSIONS
9.1 Summary
Cellular cofferdams have primarily been used as temporary systems which serve to allow
construction of facilities in open bodies of water. Applications for these structures have been
increasing and today they may serve as permanent retaining walls or as navigation or
waterfront structures. Conventional design methods for cellular cofferdams are based on
semi-empirical approaches largely developed in the 1940s and 1950s. None of the available
traditional procedures are capable of predicting cofferdam deformations, a parameter of key
importance to the cofferdam performance, and which is often observed during construction for
purposes of safety monitoring. Also, there is evidence that much of the conventional design
technology is conservative, in some cases predicting loading by more than twice that which
actually occurs.
SUMMARY AND CONCLUSIONS 210
One method which has shown promise as a means to incorporate the process of soil-
structure interaction, and to reduce design conservatism is the finite element method. In
theory, this approach allows the cell, fill and foundation system to be considered in one
analysis, and incorporates the interaction between these key elements. Recent work has
shown that realistic results are only obtained if allowances are made for the nonlinear be-
havior of the soil and the local yielding of the sheet pile system at the interlocks between the
sheet piles. Finite element techniques with the appropriate characteristics have been devel-
oped to account for these behavioral aspects, and incorporated into the program
SOILSTRUCT. However, certain key elements of the structural system of the cofferdam remain
to be provided in this program. One of the major objectives of this work is directed at resol-
ution of this deficiency. In particular, this involved adding better bending elements to the
program to represent the sheet pile systems in axisymmetric and plane strain analyses. Also,
in the case of the plane strain program, a new method is developed to allow for stress transfer
through the sheet pile system. Through case history and theoretical analyses, the enhanced
programs are demonstrated to yield accurate and realistic results.
This investigation also included other objectives beyond that of simply improving the finite
element program. These related to using parametric studies of the filling, dewatering and
flooding stages to evaluate conventional design procedures and develop new, simplified
methods which could be used in design. All of the parametric studies focused on cofferdams
founded on sandy soils, and filled with free-draining sandy soil.
In the effort to improve the structural response of the axisymmetric version of the finite
element program, a shell element was added. This allows for modeling of the sheet piles
using their actual thicknesses, and accounts for their bending characteristics. The accuracy
of the shell element is tested by comparing predicted results to those from closed form and
finite element solutions. The plane strain version of the program was modified first by adding
a beam element to represent the front and back walls of the cofferdam. The beam element
SUMMARY AND CONCLUSIONS 211
allows the sheet pile response in the plane strain program to be consistent with that in the
axisymmetric program. Also, special shear transfer elements were added to the plane strain
program. These elements model the effects of the portion of the cofferdam which is not
physically present in the plane strain analysis of a cofferdam.
Design of the shear transfer elements to model the cofferdam response involved the de-
velopment of two modulus reduction factors. Application of these factors to the modulus of
steel and use of the resulting modulus for the shear transfer elements results in a structural
performance which models the larger cofferdam system. The first of the modulus reduction
factors accounts for the fact that the actual cofferdam cell is round as opposed to the planar
shape used in the analyses. The second modulus reduction factor incorporates the influence
of the nonlinear aspects of the cofferdam introduced by the cell fill and the sheet pile system
itself. Where the first modulus reduction factor is derived theoretically, the second is based
on case history analyses.
Using the modified finite element programs, parametric analyses were performed. Rela-
tive to the cell filling stage, the parametric analyses were directed to assess the effects of cell
embedment, cell dimensions, and cell fill and foundation properties on cell behavior. Effects
of differential water loading on the cofferdam were studied to evaluate the influence of the
same factors as for cell filling, but also including level of the differential loading.
9.2 Conclusions
The conclusions derived from this research on modification of finite element programs and
parametric analyses for cofferdams on sand are as follows.
SUMMARY AND CONCLUSIONS 212
9.2.1 Modifications in SOILSTRUCT Programs
1. The modifications to include better bending elements (shell and beam elements) in
axisymmetric and plane strain programs and shear transfer elements in plane strain
program make it possible to model cofferdams more realistically.
2. To determine appropriate value of modulus for shear transfer elements, two reduction
factors are applied to modulus of steel. First modulus reduction factor (RF1) is computed
based on a comparison of theoretical results to finite element analyses. Curves are de-
veloped to determine this factor for a particular value of cell height (H) to cell width (8)
ratio. A second modulus reduction factor (RF2) is needed to account for nonlinear be-
havior. A value of 25 is determined for RF2 based on case history studies.
3. Using shear transfer element results in smoother transfer of lateral load from outboard
sheet pile through cell fill as well as through shear transfer elements as compared to
when springs are used.
9.2.2 Cell Filling
1. Conventional design methods yield higher values of maximum interlock force than those
from finite element analyses. Interlock forces based on Schroeder and Maitland (1979)
method are higher by 36 percent as compared to finite element prediction for free cell
height of 60 feet. Conventional methods as well as finite element analyses for cell filling
show that maximum interlock forces increase as free cell height increases. The differ-
ence between conventional method and finite element predictions grows larger as the
free cell height increases.
SUMMARY AND CONCLUSIONS 213
2. The depth of embedment does not influence maximum cell deflection and maximum
interlock force significantly during cell filling. The cell embedment is, therefore, provided
for reasons other than for reducing interlock forces.
3. Location of maximum cell deflection and maximum interlock force for free cell height of
60 feet is at about one-fourth of free cell height from dredge line for depth of embedment
of 10 to 25 feet. For depth of embedment of 35 feet or more, they occur at about one-sixth
of free cell height from dredge line.
4. Location of maximum cell deflection and maximum interlock force remains constant at
about one-sixth of free cell height from dredge line for all cell heights, ranging from 20 to
80 feet for same depth of embedment of 35 feet.
5. Changing friction angle of the cell fill from 35 degrees to 41 degrees results in reductions
of about 30% in maximum radial deflection and 35% in maximum interlock force for all
free cell heights.
6. Changing the friction angle of the foundation soil from 41 degrees to 35 degrees has little
to no effect on maximum cell deflection and maximum interlock force. This confirms the
approach of conventional theories, which do not consider the effect of foundation material
on interlock forces.
9.2.3 Differential Loading
1. The conventional methods are conservative in predicting internal shear failure. For a
case of cofferdam with cell width of 63 feet, free cell height of 60 feet and depth of
embedment of 35 feet, the conservatism factors based on failure loads are 2.75 and 5.5
for Schroeder and Maitland (1979) and Terzaghi (1945) methods, respectively.
2. The load-deflection response of cofferdam is strongly nonlinear at high lateral loads. At
typical working loads, the factors of safety are large enough that the load-deflection re-
SUMMARY AND CONCLUSIONS 214
sponse is essentially linear. The load-deflection response is a function of cell width, cell
height, and depth of embedment for given cell fill and foundation soils.
3. Terzaghi (1945) recommended the use of 0.5 for lateral earth pressure coefficient (K) for
performing vertical shear analysis for cell fill. Based on finite element analyses, it is
concluded that at failure loads lateral earth pressure coefficient (K) values in center of
cell fill and near outboard sheet pile could reach unity, as suggested by Schroeder and
Maitland (1979) for vertical shear analysis.
4. Under lateral loading, cofferdam cell tends to rotate along axis passing through some
point on the dredge line which may be at a distance of B/5 to B/8 (B is cell width) from
center of cell towards outboard sheet pile.
5. At normal working lateral loads equivalent to flood loads on full height of cell, the lateral
deflections of sheet pile top are estimated as 0.35 to 0.28% of free cell height for cell width
of 40 feet to 63 feet and depth of embedment varying from 10 to 35 feet.
6. During high lateral loads, a curved (convex upward) failure surface develops in cell fill
near dredge line. Simultaneously, vertical shear failure also starts in cell fill and foun-
dation soil first near inboard sheet pile.
7. The possibility of slippage of sheet piles due to lateral loading is remote except if there
are interlock misalignment and other installation defects.
8. Proposed new method for analysis of shear distortion failure in cell fill results in allowable
loads which are 20 to 50 percent higher compared to those predicted by Schroeder and
Maitland (1979) method for different cell widths and embedment depths.
SUMMARY AND CONCLUSIONS 215
Appendix A
Appendix A 216
0.1
II
o. 01
Appendix A
B = 63. 0 Ft H = 81. .O Ft H/B =1.33
sFEM : Horizontal deflection of top of cell using finite element prog
Stheory = Horiz~tal deflection of top of cell using beam theory
Es/ Eshear
Deflection ratio versus modulus ratio for shear transfer elements.
217
1.0
>-.... 0 0.1 a.
.c:. -c.o '-... ~ UJ LL.
co II
~
0.01
Appendix A
B = 63.0 Ft H = 48.8 Ft H/B = 0.775
Deflection ratio versus modulus ratio for shear transfer elements.
218
>-L-0 Cl .c ...... ~
............. :E w u..
(/J
II
:E
1 o.o
1.0
H = 37. 6 Ft.
8 = 63.0 Ft.
H/B=0.597
------
0.01 __ ~~--~~~..._~~_._~~~-'--~~--1.~~~-L-~~~ 0 20 1.0 60 80 100 120
Es /Eshear
Deflection ratio versus modulus ratio for shear transfer elements.
Appendix A 219
>-... 0 Cll
..t::.
<.o --ai LL
tO
"
0.1
Appendix A
H = 25. 0 B = 6 3. 0 Ft H/B = 0.397
Es / E shear
---
Deflection ratio versus modulus ratio for shear transfer elements.
220
100.0
10.0
>-... 0 GI = co --~ UJ LL
t()
II
~
t. 0
Appendix A
H = 12. 5 Ft B = 6 3 Ft H/B = 0.198
0
a
Top of cell
Mid-height of cell
Deflection ratio versus modulus ratio for shear transfer elements.
221
>-'-0 Cll ~ -w --~ UJ lL.
co II
~
1. 0
0.1 I
I I
I
H : 50 Ft B : 40 Ft
H/8 = 1.25
, , /
~
, ,,
,. ,,, ,,, , ,. -
e.shr~l~ ~-..... e.s\ M .,.o
\ c.e\\ tor - --. ~\ o ------i,G
.. i·,"'-~e'~ -- -- \Esnr=~ ""' u e\\ --- Es "': ,.o ' c._-- tor "''
.,,,.. O'-,o~--.,,.
o. o10L---2...1.0 ___ 4l...o---6~0:------:::s:1=0---:,~o--o---:-:,2~0:-----;-:, 40
Es/ Eshear
Deflection ratio versus modulus ratio for shear transfer elements.
Appendix A . 222
>-... 0 • .c -co --~
lJ.. co II
0.1
Appendix A
H = 40 Ft B = 40 Ft H/B = 1.0
20 40 60 80 100 120
Deflection ratio versus modulus ratio for shear transfer elements.
140
223
1. 0
>-~
0 Cll
.s::. -<o ~
lJJ LL c.o
" :l:
I I
I 0.1
Appendix A
H : 30 Ft
B : 1.0 Ft H/8:0.75
~ --... .:,~"" (.~,--~· o\.,, \O~"" ,,-'
;'"' ;'
"' ~ , , /
/
-----
Es/ E shear
------------
Deflection ratio versus modulus ratio for shear transfer elements.
224
,,
0.1
Appendix A
H = 20 Ft B : 40 Ft
H/B = 0.5
Es/ E shear
Deflection ratio versus modulus ratio for shear transfer elements.
225
100.0r----.---r---,----,--__:__,-,--~
10.0
>-... 0 GI
.&; -co --. ::i: IJJ IJ..
co II
I
H : 10 Ft B : I. 0 Ft
H/B=0.25
"'~ (,~ --c} .,,.,,,.'
~ ~,,,"" ·~ (,fl,/ e '/ ~ o'/ .'b 7
.~ ~ ~~
I I
I I
1.oWZ'--------------------=1
0.1 0L----=2-'=-0 ----=,-k0--~5t;o:----~atro\--,1r1o;no--1:12ffiol--
Deflection ratio versus modulus ratio for shear transfer elements.
Appendix A 226
Appendix B
Appendix B . 227
FAILURE LOAD
lxywH [2ZJ
2xywH -
3xywH E
SxY H ~ w
Loaded side
i...1·-------63.Q Ft
=-- ..... -..... --_ __, -- -- -----:,......,--- -- _,,.,.. - - --- --::;... - ...,,,_
60.0Ft
Failed elements and failure loads, (B = 63 ft, Hd = 10 ft).
Appendix B 228
T 10.0 FT
..L
, ..... 1------63· 0 Ft EL 130.0 --
Outboard Inboard side side
LOAD 60.QFt
rFailure Surfaces\
\ ' v ........ ~ N ' - I ~ '
~ ~ \ ............... ~ r"....
-\-- -\- """' ""' i
Dredge Ii ne 4 // ~ ~ EL 70.0 ~T 'X / ~ ' ~ ~'\ ~ ">9 '
"!'... ... , ·~
""" ~ - ' K,,. ' -->< ......... ~
' .. ~~'- -\-. i'b ~ ~K"'" ~ 'Li~ ./
,~ ~·'o'.'.:·/ Center of Rotation
'//////////////// / ////////////////
Failure plane directions and failure surfaces (B = 63 ft, Hd = 10 ft).
Appendix B 229
FAILURE LOAD
6xy H "'
Loaded side
Appendix B
... 1-------63.Q Ft
60.0Ft
Failed elements and failure loads (B = 63 ft, Hd = 21 ft).
230
I l-l•------63.0 Ft EL 130.0
x -.--
~ Outboard lnboar d
side side
-LOAD 60.0Ft
~Failure Surfaces~
) ~ !""'-~~ ' ,,,, .......
f"'.. ~ ~
I ,, ~~~-- ...... ~· ~ JI'
T 21.0 FT
Dredge Ii ne ""'"'\ )R' -\- -\-- ........ ....... ~ EL 70.0 r--.... ~
l'\ x ?~ -\- ~ ....... ~ ~ rsy r--....
I~ ~ -\- -\-- - ........ ~ ' v~ t"""'- / ~
1 ~ "' ~~ -\- v
-\-::><"" - ,,' ......... " ~ p-;..
~---~w ,.,,
~ >< ~~~c:Y . , -\-['-.. -cen1er of Rotafion
ELO. 0 ///// '///////////// ///////////////
Failure plane directions and failure surfaces (B = 63 ft, Hd = 21 ft).
Appendix B 231
FAlLU~E LOAD
lxywH EZ:J 2xywH -
)xywH ~
Loaded side
Dredge tine\
i--r-----1.0.0Ft ---~1
--I
50.0Ft
I
Failed elements and failure loads (B = 40 ft, Hd = 10 ft).
Appendix B
.. :·::
}~¥!/
. 232
,._r----1.0.0Ft ----1 --
""" Outboard Inboard
side side
- 50.0Ft LOAD r Failure Surfaces'\
J ' ~ ~ --t< ' ~
-1- j~ ~ ........ .........
' I ' >< ~ ~ "-- ........ ~ l ' ~ ' ............
~ ~A- ~ ...... ~ Dredge line\ ..........
~ ' 1FT ~~ 'K I ,
......... ' '/ ~ >< ~~ .......... ~ .... ~ ~1' ~- '/......... ' ~ .""\ "'-...~ >< ........
\-/ ' \ I L__
20 ft >< ~ ~ >K ~ 6>~' " +J.-~./ .
Center of Rotation
Failure plane directions and failure surfaces (B = 40 ft, Hd = 10 ft).
Appendix B · 233
LOAD rt------1.0.0 Ft ---.-t1
50.0Ft
Loaded Side
-.,.... '"";:~ - ......... - - -~-==--............ -=-=..-
Failed elements and failure loads (B = 40 ft, Hd = 20 ft).
Appendix B 234
i-r----~O.OFt ----1 --
Outboard x Inboard side side
LOAD 50.0Ft ~
Failure Surfaces r ---r--. . . \ ,.
~ ~ ' >< ~ _J ........... ' ~ -:::-.. '
Dredge line\ x ~-\- ............ .......... ~ ......... .......... ' 'f..'- I"' ,, ~
_j ........... " I ~7 ~ ' r-- '-.. '
~ -~ ~ + -.l ........ /~ ,-~
~ ..... ~ !'--.. r--.. " 20 ft ~·~ ' ' / \' l
25ft "- // j\ ~~, II..
' '
-'-- VCenter of Rotation
.
Failure plane directions and failure surfaces (B = 40 ft, Hd = 20 ft).
Appendix B 235
lxy H 'W
Jxy H 'W
-1-----,0.0Ft ----~ LOAD I I
50.0Ft
Loaded Side
Failed elements and failure loads (B = 40 ft, Hd = 35 ft).
Appendix B 236
t--r----J..O.OFt-----1 --x I
Outboard -t- In boar side side
d
+ LOAD
50.0Ft Failure Surfaces ........
""' ~
~ ~ ~ ~
" :>< -+- J' ' ~ ' >< --\- -\-- It ......... ~ I~
' --\-- ~ ~ ~ I
Dredge line\ ~ ~ ~
" ~ - ~ ,, .
~ ~ ' rJ -~ ~ ........ \. ~
·~ ~ ~ ~ ~ I ,
' ~ "" i--
\~ ~ I --\--><."" '
~ ,I 35 ft 33ft ~
-1-~ ~ I
I I\ . I
-L ~ ~ ¥ Center of Rotation
I
Faiiure plane directions and failure surfaces (B = 40 ft, Hd = 35 ft).
Appendix B 237
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The vita has been removed from the scanned document