86
Bengt H. Fellenius, Dr.Tech., P.Eng. 2475 Rothesay Avenue, Sidney, British Columbia, V8L 2B9 TEL: (778) 426-0775 e-address: <[email protected]> Web site: [www.Fellenius.net] Basics of Design of Piled Foundations A Course and Seminar Santa Cruz, Bolivia April 25, 2013 The primary intent of the course is to demonstrate that deep foundation design is a good deal more than finding some value of capacity. The course aims to show what data one must pull together and present processes of analysis and calculations necessary for a design of a specific project. Aspects of negative skin friction and associated drag load and downdrag are emphasized. The presentation includes both broad generalities and in-depth details. Aspects of where to install instrumentation, perform a test, and analyze the test data are addressed. Settlement analysis is of vital importance to the design of piled foundations, and the course addresses principles of settlement analysis and provides some of the mechanics of calculating settlement. A few aspects are included of construction aspects as well as of Limit States Design, LSD (Ultimate Limit States, ULS, and Serviceability Limit States, SLS, by Canadian terminology and Load and Resistance Factor Design, LRFD, by US terminology). To simplify following along the flow of the presentation and taking notes, hand-out course notes are provided, consisting of black-and-white copies of all Power Points slides, six to a page. Full-size color copies of the slides are also available on my web site [www.Fellenius.net ]. These can be downloaded from the link [/Bolivia]. Note, the link is hidden and has to be typed into the command line ("command ribbon"). The slides contain only a minimum of text. For a background and explanation to much of the presentations, I refer you to my text book "Basics of Foundation Design" also available for downloading from my web site (the file is called “313 The Red Book_Basics of Foundation Design.pdf”. After downloading, the book can be viewed and read on-screen or be printed (color or black & white) without any restriction. The book contains a list of references pertinent to the material presented in the course. Copies of the referenced papers where I am the author or co-author are available for downloading at my web site (click on the link "Download Papers"). I will be glad to respond to any e-mail with a question you might wish to put to me. Sidney April 2013 Bengt H. Fellenius

Fellenius bases de diseño de pilotes de fundación

Embed Size (px)

Citation preview

Page 1: Fellenius   bases de diseño de pilotes de fundación

Bengt H. Fellenius, Dr.Tech., P.Eng.2475 Rothesay Avenue, Sidney, British Columbia, V8L 2B9

TEL: (778) 426-0775 e-address: <[email protected]>Web site: [www.Fellenius.net]

Basics of Design of Piled FoundationsA Course and Seminar

Santa Cruz, BoliviaApril 25, 2013

The primary intent of the course is to demonstrate that deep foundation design is a good deal more thanfinding some value of capacity. The course aims to show what data one must pull together and presentprocesses of analysis and calculations necessary for a design of a specific project. Aspects of negativeskin friction and associated drag load and downdrag are emphasized.

The presentation includes both broad generalities and in-depth details. Aspects of where to installinstrumentation, perform a test, and analyze the test data are addressed. Settlement analysis is of vitalimportance to the design of piled foundations, and the course addresses principles of settlement analysisand provides some of the mechanics of calculating settlement. A few aspects are included ofconstruction aspects as well as of Limit States Design, LSD (Ultimate Limit States, ULS, andServiceability Limit States, SLS, by Canadian terminology and Load and Resistance Factor Design,LRFD, by US terminology).

To simplify following along the flow of the presentation and taking notes, hand-out course notes areprovided, consisting of black-and-white copies of all Power Points slides, six to a page. Full-size colorcopies of the slides are also available on my web site [www.Fellenius.net]. These can be downloadedfrom the link [/Bolivia]. Note, the link is hidden and has to be typed into the command line ("commandribbon").

The slides contain only a minimum of text. For a background and explanation to much of thepresentations, I refer you to my text book "Basics of Foundation Design" also available for downloadingfrom my web site (the file is called “313 The Red Book_Basics of Foundation Design.pdf”. Afterdownloading, the book can be viewed and read on-screen or be printed (color or black & white) withoutany restriction. The book contains a list of references pertinent to the material presented in the course.Copies of the referenced papers where I am the author or co-author are available for downloading at myweb site (click on the link "Download Papers").

I will be glad to respond to any e-mail with a question you might wish to put to me.

Sidney April 2013

Bengt H. Fellenius

Page 2: Fellenius   bases de diseño de pilotes de fundación

Basics of Design of Piled FoundationsA Course and Seminar

Bengt H. Fellenius, Dr.Tech., P.Eng.

The course comprises four main lectures leading up to and presenting the essentials of the Unified Method of deepfoundations design for capacity, drag load, settlement, and downdrag for single piles, pile groups, and piledfoundations. The presentations are illustrated with case histories of testing and design analysis including how toevaluate strain-gage measurements from instrumented pile loading tests and to assess residual load. Settlementanalysis is of vital importance to the design of piled foundations, and the course addresses principles of settlementanalysis and how to calculate settlement of piles and piled foundations. Pertinent aspects of constructionprocedures and Load and Resistance Factor Design, LRFD are discussed.

08:00h Brief Background to Basic Principles Applicable to Piled Foundations

Stress distribution and interaction between adjacent foundations; Settlement analysis; Applications ofwick drains to piled foundations.

09:30h Coffee Break

09:45h Analysis of Load Transfer, Capacity, and Response to LoadLoad-movement response of foundations; Bearing capacity and load-transfer by beta, alpha, and lambdamethods, and by CPT and CPTu methods; Set-up and relaxation; Residual load; Results of predictionevents.

11:30h The Static Loading Test: Performance, Analysis, and Instrumentation

Methods of testing and basic interpretation of the results. How to analyze results from strain-gageinstrumented piles to arrive at resistance distribution along the pile shaft and the pile toe response.

12.00h LUNCH

13:00h The Static Loading Test: Resumed

Determining pile elastic modulus. The importance of residual load and how to include its effect in theanalysis. Principles of the bi-directional test (the O-cell test) and how to analyze the results of an O-celltest. Case histories of analyses on results of static loading tests on driven and bored piles.

14:30h Coffee Break

14:50h 4. Piles and Pile Groups — Long-Term Behavior and how we know what we know; The Unified Design Method.

Important case histories presenting studies that demonstrated the actual long-term response of piles toload and observed settlement of piles and pile groups. The lessons learnt will be referenced to aspects ofdesign applying the Unified Method for Design of Piled Foundations considering Capacity, Drag Load,Settlement, and Downdrag for single piles, pile groups, and piled foundations.

1. Capacity (choice of factor of safety, and rules of LRFD and Limit States Design) and design forstructural strength (including drag load)

2. Settlement of single piles and pile groups due to load directly on the piles and due to influence fromadjacent activity (downdrag)

3. How to combine the various aspects for the design of an actual case with emphasis on foundationsettlement illustrated with examples

17:00h Questions and Discussions; End of Day

Page 3: Fellenius   bases de diseño de pilotes de fundación

1

BASICS OF DESIGN OF PILED

FOUNDATIONSFOUNDATIONS

Bengt H. Fellenius

1

A short course

Santa Cruz, Bolivia, April 25, 2013

08:00h Brief Background to Basic PrinciplesApplicable to Piled Foundations

SCHEDULE

09:30h Break

09:45h Analysis of Load Transfer, Capacity and Response to Load

11.30h The Static Loading Test: Head-down and O-cell Tests

12.00h LUNCH

13.00h The Static Loading Test: Continued

14 00h Case Histories on Pile Analysis Drag Load Downdrag

2

14.00h Case Histories on Pile Analysis, Drag Load, Downdrag,Pile Groups, Piled Raft, Piled Pad

14.30h Break

14.50h The Unified Method of Design

17:00h Questions and Discussions and End of Day

Page 4: Fellenius   bases de diseño de pilotes de fundación

2

www.Fellenius.net

Bolivia

To Download All COURSE SLIDES

Power Point Slides1 - Background Lecture 1.pdf2 - Analysis Methods Lecture 2.pdf3 - Static Loading Test Lectures 3a and 3b.pdf4 - Case Histories and Lectures 4a and 4b.pdf

Design Methods

4

Page 5: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

1

BASICS OF DESIGN OF PILED

FOUNDATIONS

Bengt H FelleniusBengt H. Fellenius

Background and Basic Principles

Bolivia, April 25, 2013

Some Fundamental Principles

22

Determining the effective stress is the key to geotechnical analysis

• The not-so-good method:

hΔ=Δ '' γσ γ’ = buoyant unit weight

33

)'(' hz Δ∑= γσ

)1(' iwt −−= γγγ

It is much better to determine, separately, the total stress and the pore pressure. The effective stress is then the total stress minus the pore pressure.

)( hΔ∑

44

)( hz Δ∑= γσ

uz −= σσ '

Determining pore pressure

u = γw hThe height of the column of water (h; the head representing the water pressure)is usually not the distance to the ground surface nor, even, the distance to thegroundwater table. For this reason, the height is usually referred to as the“phreatic height” or the “piezometric height” to separate it from the depth below

PRESSURE

55

the groundwater table or depth below the ground surface.

The pore pressure distribution is determined by applying the facts that

(1) in stationary conditions, the pore pressure distribution can be assumed to be linear in each individual soil layer

(2) in pervious soil layers that are “sandwiched” between less pervious layers, the pore pressure is hydrostatic (that is, the vertical gradient is unity)

SAND Hydrostatic distribution

CLAY Non-hydrostatic distribution, but linear

SAND Hydrostatic distribution Artesian phreatic head

GW

DEPTH

Distribution of stress below a a small load area

0LBqqz

××=

The 2:1 method

66

)()(0 zLzBqqz +×+

The 2:1-method can only be used for distributions directly under the centerof the footprint of the loaded area. It cannot be used to combine (add)stresses from adjacent load areas unless they all have the same center. it isthen only applicable under the area with the smallest footprint.

Page 6: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

2

The Boussinesq Method Derived from calculation of stress from

a point load on the surface of an elastic medium

33z

77

2/522 )(23

zrzQqz +

Newmark’s method for stress from a loaded area

Newmark (1935) integrated the Boussinesq equation over a finite area and obtained a relation for the stress under the corner of a uniformly loaded rectangular area, for example, a footing

CBAI +×

88

π40CIqqz =×=

2222

22

112nmnm

nmmnA+++

++=

12

22

22

++++

=nmnmB

⎥⎥⎦

⎢⎢⎣

−++++

= 2222

22

112arctannmnm

nmmnC

m = x/zn = y/zx = length of the loaded areay = width of the loaded areaz = depth to the point under the corner

where the stress is calculated

(1)

• Eq. 1 does not result in correct stress values near the ground surface. To represent the stress near the ground surface, Newmark’s integration applies an additional equation:

π CBA −+×

99

ππ

40CBAIqqz

+×=×=

For where: m2 + n2 + 1 ≤ m2 n2

(2)

Stress distribution below the center of a square 3 m wide footing

-2

0

) 0 15

0.20

0.25

CTO

R,

IEq. (1)

Eq. (2) Eq. (2)

1010

0 20 40 60 80 100-6

-4

STRESS (KPa)

DE

PTH

(m

0.01 0.10 1.00 10.000.00

0.05

0.10

0.15

m and n (m = n)

INFL

UE

NC

E F

AC

Eq. (1)

0

1

2

0 25 50 75 100

STRESS (%)

met

ers)

Boussinesq

Westergaard

0

1

2

0 25 50 75 100

SETTLEMENT (%)

met

ers)

Boussinesq

Westergaard

1111Comparison between Boussinesq, Westergaard, and 2:1 distributions

3

4

5

DEP

TH (

dia

2:13

4

5

DEP

TH (

dia

2:1

0

1

2

0 25 50 75 100

STRESS (%)

eter

s)

Westergaard

Boussinesq

0

1

2

0 25 50 75 100

SETTLEMENT (%)

met

ers)

Boussinesq

Westergaard

1212

2

3

4

5

DEP

TH (

diam

2:1

2

3

4

5

DEP

TH (

diam

2:1

Page 7: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

3

0

1

2

0 25 50 75 100

STRESS (%)

amet

ers)

Westergaard

Boussinesq

0

1

2

0 25 50 75 100

SETTLEMENT (%)

amet

ers)

Boussinesq

Westergaard

1313

3

4

5

DE

PTH

(di

a

2:1 Characteristic Point; 0.37b from center

3

4

5

DEP

TH (

dia

2:1 Characteristic Point; 0.37b from center

Below the characteristic point, stresses for flexible and stiff footings are equal

Now, if the settlement distributions are so similar, why would we persist in using

Boussinesq stress distribution instead of the much simpler 2:1 distribution?

1414

Because a footing is not alone in this world; near by, there are other footings, and fills,

and excavation, etc., for example:

The settlement imposed outside the loaded

foundation is often critical

0

1

2

0 25 50 75 100

SETTLEMENT (%)

met

ers)

BoussinesqOutside Point Boussinesq

Center Point

1515

2

3

4

5

DEP

TH (

diam

Loaded area

The end result of a geotechnical design analysis

is

1616

Settlement

Stress-Strain

σ' (

KPa

)

Δσ

 

εσΔΔ

=tM

1717

STRAIN (%)

STR

ESS,

σ

Δσ Δε

Δε

Plotted as Strain-Stress

N (

%)

N (

%)

TIO

, e

Plotted as Void Ratio vs. Stress

1818

STRESS, σ' (KPa)

STR

AIN

STRESS, σ' (KPa)

STR

AIN

STRESS (KPa)

VOID

RA

T

Page 8: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

4

Stress-strain behavior is non-linear for most soils. The non-linearity cannot be disregarded when analyzing compressible soils, such as silts and clays, that is, the elastic modulus approach is not appropriate for these soils.

Non-linear stress-strain behavior of compressible soils, is conventionally modeled as follows.

11 'l'l σσC

1919

where ε = strain induced by increase of effective stress from σ‘0 to σ‘1Cc = compression indexe0 = void ratioσ‘0 = original (or initial) effective stressσ‘1 = final effective stress

CR = Compression Ratio = (MIT)

0

1

0

1

0 'lg

'lg

1 σσ

σσ

ε CRe

Cc =+

=

01 eC

CR c

+=

Some use the term "Ccε" for the "CR", creating quite a bit of confusion thereby

In overconsolidated soils (most soils are)

)''lg

''

lg(1

1 1

00 pc

pcr CC

e σσ

σσ

ε ++

=

2020

where σ‘p = preconsolidation stressCcr = re-compression index

The Janbu Method

The Janbu tangent modulus approach, proposed by Janbu (1963; 1965; 1967; 1998), and referenced by the Canadian Foundation Engineering Manual, CFEM (1985; 1992), applies the same basic principles of linear and non-linear stress-strain behavior. The method applies to all soils, clays as well as sand. By this method, the relation between stress and strain is a function of two non-dimensional parameters which are unique for a soil: a stress exponent, j, and a modulus number, m.

2121

Janbu’s general relation is

])''()

''[(1 01 j

r

j

rmj σσ

σσε −=

where: σ‘r = a “reference stress = 100 KPaj = a stress exponent

m = the modulus number

The Janbu Method

Dense Coarse-Grained Soil j = 1

Cohesive Soil j = 0 1'ln1 σε =

'1)''(101 σσσε Δ=−=

mm

'21)''(

21

01 σσσε Δ=−=mm

σ’ in KPa

σ’ in ksf

2222

Cohesive Soil j = 0

Sandy or Silty Soils j = 0.5

0'lnσ

εm

=

)''(51

01 σσε −=m

pm''(2

1 σσε −=

σ’ in KPa

σ’ in ksf

There are direct mathematical conversions

between m and the E and Cc-e0

For E given in units of KPa (and ksf), the relation between the modulus number and the E-modulus is

2323

m = E/100 (KPa)m = E/2 (ksf)

For Cc-e0, the relation to the modulus number is

cc Ce

Cem 00 13.2110ln +

=+

= And m = 2.3/CR

Typical and Normally Conservative Modulus Numbers

SOIL TYPE MODULUS NUMBER STRESS EXP.

Till, very dense to dense 1,000 — 300 (j=1)

Gravel 400 — 40 (j=0.5)

Sand dense 400 — 250 (j=0.5compact 250 — 150 _ " _loose 150 — 100 _ " _

Silt dense 200 — 80 (j=0.5)compact 80 — 60 _ " _loose 60 — 40 _ " _

This is where the greater value of the Janbu approach versus the MIT CR-approach comes in.

ClaysSilty clay hard, stiff 60 — 20 (j=0)

stiff, firm 20 — 10 _ " _Clayey silt soft 10 — 5 _ " _

Soft marine claysand organic clays 20 — 5 (j=0)

Peat 5 — 1 (j=0)

For clays and silts, the recompression modulus, mr, is often five to twelve times greater than the virgin modulus, m.

This is where the Janbu approach and the MIT CR-approach are equal in practicality.

Reference: Fellenius, B.H., 2012. Basics of foundation design, a text book.Revised Electronic Edition, [www.Fellenius.net], 385 p.

Page 9: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

5

0.80

1.00

1.20

Voi

d R

atio

(- -

)

m = 12(CR = 0 18)

p'c

10

15

20

25

Stra

in (

%)

C

1/m

Slope = m = 12

Evaluation of compressibility from oedometer results

2525

0.40

0.60

10 100 1,000 10,000

Stress (KPa) log scale

V (CR = 0.18)

0

5

10 100 1,000 10,000

Stress (KPa) log scale

p 10p

Cc

Cc = 0.37

e0 = 1.01 p'c

p 2.718p

Void-Ratio vs. Stress and Strain vs. Stress — Same test data

Note, if the "zero"-value -- the e0 -- is off, the Cc-e0 is off (and so is the CR) even ifthe Cc is correctly determined. Not so the "m" (if determined from the test results).

Comparison between the Cc/e0 approachand the Janbu method

0 10

0.15

0.20

0.25

0.30

0.35

PRES

SIO

N IN

DEX

, Cc

Do these values indicate a

compressible soil, a medium compressible

soil, a moderately ibl il

15

20

25

30

35

MO

DU

LUS

NU

MB

ER, m

2626

Data from a 20 m thick sedimentary deposit

0.00

0.05

0.10

0.40 0.60 0.80 1.00 1.20

VOID RATIO, e0

CO

MP compressible soil, or a

non-compressible soil?0

5

10

0.400.600.801.001.20

VOID RATIO, e0

VIR

GIN

The Cc-e0 approach (based on Cc) implies that the compressibility varies by 30± %.

However, the Janbu methods shows it to vary only by 10± %. The modulus number, m, ranges from 18 through 22; It would be unusual to find a clay with less variation.

Conventional Cc/e0

How many of these oedometer results indicate

(o) highly compressible clay

(o) compressible clay

( ) di ibl l20

30

40

50

OD

ULUS

NU

MB

ER, m

0 20 40 60 80 100WATER CONTENT, wn (%)

Janbu Modulus Number m

The Cc-values converted via the associated e0-values to modulus

numbers.

2

3

4

5

MPR

ESSI

ON

IND

EX, C

c

2727

(o) medium compressible clay

(o) non-compressible clay?

0

10

0.00 0.50 1.00 1.50 2.00 2.50 3.00

VOID RATIO, e0

VIRG

IN M

m < 10 ==> Highly compressible Oedometer test data from Leroueil et al., 1983

0

1

0.00 1.00 2.00 3.00

VOID RATIO, e0

CO

M

Stress produces strainLinear Elastic Deformation (Hooke’s Law)

ε = induced strain in a soil layer

= imposed change of effective stress in the soil layer 'σΔ

E'σε Δ

=

2828

p g y

E = elastic modulus of the soil layer (Young’s Modulus)

Young’s modulus is the modulus for when lateral expansion is allowed, which may be the case for soil loaded by a small footing, but not when the load is applied over a large area. In the latter case, the lateral expansion is constrained (or confined). The constrained modulus, D, is larger than the E-modulus. The constrained modulus is also called the “oedometer modulus”. For ideally elastic soils, the ratio between D and E is:

ν = Poisson’s ratio

)21()1()1(νν

ν−+

−=

ED

Settlement is due to Immediate Compression, Consolidation Settlement, and Secondary Compression

Immediate Compression is the compression of the soil grains (soil skeleton) and of any free gaspresent in the voids. It is usually assumed to be linearly proportional to the change of stress Theimmediate compression is therefore often called 'elastic' compression. It occurs quickly and isnormally small (it is not associated with expulsion of water).

Consolidation (also Primary Consolidation) is volume reduction during the increase ineffective stress occurring from the dissipation of pore pressures (expelling water from the soilbody). In the process, the imposed stress, initially carried by the pore water, is transferred to the

il t t C lid ti i kl i i d il b t l l i fi i d

2929

soil structure. Consolidation occurs quickly in coarse-grained soils, but slowly in fine-grainedsoils.

Secondary Compression is a term for compression occurring without an increase of effectivestress. It is triggered by changes of effective stress. It does not usually involve expulsion ofwater, but is mainly associated with slow long-term compression of the soil skeleton. Somecompression of the soil structure occurs and it is then associated with some expulsion of water,but this is so gradual and small that pore pressure change is too small to be noticed. Sometimes,the term "creep" is used to mean secondary compression, but "creep" should be restricted toconditions of shear. Secondary compression is usually small, approximately similar in magnitudeto the immediate compression, but may over time add significantly to the total deformation of thesoil over time. Secondary compression can be very large in highly organic soils, such as peat.Theoretically, seconday compression occurs from the start of the consolidation (effective stresschange), but in practice, it is considered as starting at the end of the consolidation.

On applying load, the soil skeleton compresses and the soil grainsare forced closer to each other reducing the void ratio. Thecompression of the soil skeleton occurs more or less immediately incontrast to the reduction of the void volume which requiresexpulsion of water ("consolidation") and can take a long time.However, in soils containing gas bubbles, the load applicationcauses the bubbles to compress (and partially to go into solution in

Immediate Compression and Consolidation Settlement

3030

the pore water), which also occurs immediately. Then, as the porepressure dissipates during the consolidation process, the gasbubbles expand which slows down the settlement process. The"slow-down" is often mistaken for approaching the end ofconsolidation. The thereafter observed settlement is theninterpreted as a large secondary compression (addressed later on).

Page 10: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

6

2H

Drainage Layer

Clay Layer (consolidating)

Drainage Layer

0

1uu

SS

U t

f

tAVG −==

where UAVG = average degree of consolidation (U)St = settlement at Time tSf = final settlement at full consolidationut = average pore pressure at Time tu0 = initial average pore pressure (on application of the load at Time t = 0)

Basic Relations

UAVG

Consolidation Settlement

3131

vv c

HTt2

=

where t = time to obtain a certain degree of consolidationTv = a dimensionless time coefficient: cv = coefficient of consolidationH = length of the longest drainage path

UAVG (%) 25 50 70 80 90 “100”

Tv 0.05 0.20 0.40 0.57 0.85 ≤1.00

)1(lg1.0 UTv −−−=

HOW TO HANDLE A MULTILAYERED PROFILE?

c/c

d

"Square" spacing: D = √4/π c/c = 1.13 c/c

"Triangular" spacing: D = √(2√3)/π c/c = 1.05 c/c

Vertical Drains

3232

c/cBasic principle of consolidation process in the presence of vertical drains

hh Ud

DT−

−=1

1ln]75.0[ln81

hh UdD

cDt

−−=

11ln]75.0[ln

8

2

and

hh c

DTt2

=

The Kjellman-Barron Formula

Walter Kjellman, inventor of the very first wick drain, the Kjellman Wick, a 100 mm wide, 3 mm thick, cardboard drain that became the prototype for

33

p ypall subsequent wick drains.

Walter Kjellman, 1950

Important Points

Build-up of Back Pressure

The consolidation process can be halted if back-pressure is let to build-up below the embankment, falsely implying that the process is completed

3434

Flow in a soil containing pervious lenses, bands, or layers Theoretically, vertical drains operate by facilitating horizontal drainage. However, where pervious lenses and/or horizontal seams or bands exist, the water will drain vertically to the pervious soil and then to the drain. When this is at hand, the drain spacing can be increased significantly.

Pervious seams (silt or sand) will dry faster than the main body of clay. The pervious seams can be observed in a Shelby sample during the drying process, as indicated in the photos.

3535

p

CPTU soundings with readings every 10 mm can also disclose the presence of sand and silt seams (if they are thicker than about 10 mm; which the illustrated small seams are not).

How deep do the wick drains have to be installed?

In theory, the drains do not need to go deeper than to where the applied stress is equal to the preconsolidation stress.

However in practice it is a good rule to always go down to a

3636

However, in practice, it is a good rule to always go down to a pervious soil layer (aquifer) to ensure downward drainage. But, if the surcharge is by vacuum treatment or combined with vacuum treatment, it is better to avoid having the drains in an aquifer, or they would "suck".

Page 11: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

7

3737

The Kjellman wick, 1942 The Geodrain, 1972

3838

The Geodrain, 1976

Wick drain types

The Burcan Drain, 1978

The Mebra Drain 1984 (a development of the

Castleboard Drain 1979)

3939

0

5

10

15

20

25

30

35

40

0 100 200 300Pore Pressure (KPa)

Dep

th (

m)

Wick Drains Installed

m)

Settlement at center of a 3.6 m high embankment BangkokAirport. Wick drains at c/c 1.5 m were installed to 10 m depth.

PORE PRESSUREEnlarged

40

AVERAGE MEASURED SETTLEMENT

DESIGN CURVE FOR THISSURCHARGE (75 KPa)

1.0 m

FINAL HEIGHTOF FILL

SET

TLEM

ENT

(mm

)

≈200 days

FILL

HEI

GH

T (m

CalculatedTotalSettlements

Settlement and Horizontal Displacement for the 3.6 m Embankment

WICK DRAINS TO 10 m DEPTHWICK DRAINS TO 10 m DEPTH

Settlement was monitored in center and at embankment sides and horizontal displacement was monitored near sides of embankment

Note the steep slopes

4141

Time from start to end of surcharge placement = 9 monthsObservation time after end of surcharge placement = 11 months

1.0 m

2.0 m

WICK DRAIN

Moh and Lin 2006

Horizontal Displacement versus Settlement at Different Test Locations

OVE

MEN

T (c

m)

4242

HOR

IZO

NTA

L M

O

SETTLEMENT (cm)

Page 12: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

8

Secondary Compression

1000

log1 t

te

C ααε+

=

The value of the Coefficient of Secondary Compression, Cα, is usually expressed as aratio to the consolidation coefficient, Cc, ranging from 0.02 through 0.07 with an averageof about 0.05 (Holtz and Kovacs 1981). For example, in a soft clay with Cc of about 0.3

d f b t it (i d l b f 15) C ld b b t 0 01

4343

and e0 of about unity (i.e., a modulus number of 15), Cα, would be about 0.01.

The key parameter, however, it the t100 value, the time it takes for 100 % of consolidation (or 90 %, more realistically) to develop. Also when using wick drains, the 100-% should be the time for vertical drainage, not horizontal.

It is commonly assumed that secondary compression does not start until primary consolidation is completed; U = 100 %. However, the consensus amongst the experts is that secondary compression starts as soon as a change of effective stress has been triggered, i.e., it starts at at 0 % consolidation.

The purpose of calculating stresses is to calculate settlement. The following showssettlements calculated from the Boussinesq distribution. how stress applied to thesoil from one building affect the settlement of an adjacent existing 'identical'building loaded the same constructed about 5 years before.

EXISTING ADJACENT BUILDING

NEW BUILDING

WITH SAME LOAD OVER FOOTPRINT

AREA

The 2nd building was constructed five years after the 1st building. The 1st building had then settled about 80 mm (≈3 inches), which was OK albeit close to what was felt to be

4444The soils consist of preconsolidated (OCR = 2) compressible silt and clay

6.5 m6.5 m 4 m m

1st Building

2nd Building

was OK, albeit close to what was felt to be acceptable. Did the construction of the 2nd building add settlement to the 1st, and what was the settlement of the 2nd building?

(Because the buildings are on raft foundation, the characteristic point is the most representative point for the settlement calculations).

The settlement of the first building calculated using UniSettle Version 4

0 2 4 6 8 10YEARS

SETTLEMENT OVER TIME

4545

020406080

100120

0 2 4 6 8 10

SETT

LEM

ENT

(mm

)

2nd Building constructed

Calculations using Boussinesq distribution can be used to determine how stressapplied to the soil from one building may affect an adjacent existing building(having the same loading as the new building).

0

5

0 20 40 60 80 100

STRESS (%)

STRESSES UNDER AREA

BETWEEN THE TWO BUILDINGS

EXISTING ADJACENT BUILDING

NEW BUILDING

WITH SAME LOAD OVER FOOTPRINT

AREA

4646

10

15

20

25

30

DEP

TH (

m)

STRESSES ADDED TO THOSE UNDER THE FOOTPRINT OF THE ADJACENT BUILDING

STRESSES UNDER THE FOOTPRINT OT THE LOADED BUILDING

TWO BUILDINGS

Calculations by means of UniSettleThe soils consist of preconsolidated

moderately compressible silt and clay

6.5 m6.5 m 4 m m

Calculations using Boussinesq stress distribution can be used to determine howstress applied to the soil from one building may affect an adjacent existing building(having the same loading as the new building).

EXISTING ADJACENT BUILDING

NEW BUILDING

WITH SAME LOAD OVER FOOTPRINT

AREA

0

5

10

0 20 40 60 80 100

STRESS (%)

STRESSES UNDER THE AREA

BETWEEN THE TWO BUILDINGS

PRECONSOLIDATION MARGIN (Reducingwith depth)

4747The soils consist of preconsolidated moderately compressible silt and clay. The preconsolidation margin reduces with depth.

6.5 m6.5 m 4 m m

10

15

20

25

30

DEP

TH (

m)

CENTER STRESSES COMBINED

STRESSES UNDER THE FOOTPRINT OF THE LOADED BUILDING

STRESSES FROM LOADED BUILDING CALCULATED UNDER THE FOOTPRINT OF THE ADJACENT BUILDING

Settlement distributions (UniSettle Version 4)

0

5

10

0 20 40 60 80 100 120

SETTLEMENT (mm)

1st ONLY

Increase due to 2nd Bldng BOTHSand &

Gravel

Silty Clay

0

5

10

0 20 40 60 80 100 120

SETTLEMENT (mm)

Of ground due to 1st Bldng only

Due to 2nd Bldng

4848

15

20

25

30

35

DEP

TH (

m)

1st BUILDING

Soft Clay 15

20

25

30

35

DEP

TH (

m)

2nd BUILDING

Page 13: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

9

-83 KPa

105 KPa

34 KPa

85 KPa

105 + 34 + 85 = 224 - 83 141 KPa

110 m

38 m74 m

MORE ON SETTLEMENT

YEARYEAR

49

Briaud et al. 2007; Fellenius and Ochoa 2008

0

50

100

150

200

250

300

350

4001936 1946 1956 1966 1976 1986 1996 2006

YEAR

SETT

LEM

ENT

(m

m)

.

0

50

100

150

200

250

300

350

400

1 10 100

SETT

LEM

ENT

(mm

)

1936 1937 1940 1945 1950 1960 1975 2000

LINEAR PLOTLOWER SCALE

LOGARITHMIC PLOTUPPER SCALE

1936 1946 1956 1966 1976 1986 1996 2006

0

20

40

60

80

100

120

140

YEAR

WA

TER

DEP

TH (

m)

132a- 14m217 - 26m216a- 39m115 -153m209 -159m111 -161m501a-180m912 -206m114a-261m618 -267m606 -301m501b-365m132b-442m114b-480m

1925 1935 1945 1955 1965 1975 1985 1995 2005 2015

SHALLOW WELLS

DEEP WELLS

Water Depths Measured in Deep Wells

50

Monument and Well Locations

Well head at Burnett School, Baytown, Texas

YEAR

51

0

50

100

150

200

250

300

350

400

1 10 100

YEAR

SE

TTLE

ME

NT

(mm

)

1936 1937 1940 1945 1950 1960 1975 2000

DEPTH TO WATER TABLE

SETTLEMENT

0

25

50

75

100

125

DEP

TH T

O W

ATE

R T

AB

LE (

m)

San Jacinto MonumentSettlement and Measured Depths to Water in the Wells Plotted Together

1925

The lowering of the pore pressures due to mining of water and subsequent regionalsettlement is not unique for Texas. Another such area is Mexico City, for example.Here is a spectacular 1977 photo from San Joaquin, California.

52

1977

1955

Subsidence at San Joaqu in Valley, California

0.0

0.5

1.0

1920 1930 1940 1950 1960 1970 1980 1990 2000 2010

YEAR

ent

(m)

I II III IV

5353

1.5

2.0

2.5

Settl

eme

NEW ORLEANS 1924 - 1978

I. Initial Period of Pumping II. Increased Pumping III. Further Increased IV. Reduced Pumping

Data from Kolb, C.R. and Saucier, RT., 1982

Site Investigation Techniques

The SPT and the CPT/CPTu

Page 14: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

10

The SPTExample from Atlantic coast of

South USA

0

5

10

15

0 20 40 60 80 100

SPT N-Indices (bl/0.3m)

0

5

0 10 20 30 40 50

SPT N-Indices (bl/0.3m)

5555

20

25

30

35

40

45

50

DEP

TH (

m)

East Abutment

10

15

20

25

DEP

TH (

m)

DETAIL

0

10

20

30

40

0 20 40 60 80 100

N-Index (bl/0.3m)

H (

m)

0

10

20

30

40

0 20 40 60 80 100

N-Index (bl/0.3m)

H (

m)

0

10

20

30

40

0 20 40 60 80 100

N-Index (bl/0.3m)

H (

m)

Example from Atlantic coast of

Canada

5656

40

50

60

70

80

DE

PT 40

50

60

70

80

DE

PT 40

50

60

70

80

DE

PT

SPT for design After problems arose

Forensics

0

10

20

30

0 20 40 60 80 100

N-Index (bl/0.3m)

m)

With all data points

5757

30

40

50

60

70

80

DE

PTH

(m

0.010

0.100

1.000

mv (

1/M

Pa)

30405060708090

100

Mod

ulus

(M

Pa)

Direct numerical use of the SPT N-index

5858

0.0011 10 100

N60-Index (bl/0.3m)

01020

0 10 20 30 40 50N60-Index (bl/0.3m)

(after Terzaghi, Peck, and Mesri 1996 from Burland and Burbidge 1985)

Determining pile Capacity from SPT-indices

0

5

10

15

0 10 20 30 40

SPT N-Index (bl/0.3m)

(m)

0

5

10

15

0 10 20 30 40

SPT N-Index (bl/0.3m)

(m)

0

5

10

15

0 10 20 30 40Cone Stress, qt (MPa)

(m)

5959

20

25

30

35

DEP

TH (

Estimated required depth

20

25

30

35

DEP

TH (

Potentially possible depth

Estimated required depth1

2

Pile 1 had a much smaller capacity than Pile 2!

20

25

30

35

DEP

TH (

N (bl/ft)

Pile 1 had a much smaller capacity than Pile 2!

2

1

Principles of the CPT and CPTU

The Cone Penetrometer

606060

Sleeve friction, fs

Pore PressureU2 position

Cone Stress, qc

“U2 Position” = pore pressure measured on the cone “shoulder”cone shoulder

Page 15: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

11

616161 626262

6363 6464

Continuous cores samples obtained by pushing down a pipe having an inside plastic tube. On withdrawal and cutting the tube open, the soil sample is available in a better condition than a sample in a SPT-spoon.

Courtesy of Pinter and Associates, Saskatoon, SK.

0

10

0 10 20 30

INCLINATION ANGLE (°)

(m)

0

10

0 2 4 6 8

RADIAL DEVIATION (m)

(m)

0

10

0.0 0.3 0.5 0.8 1.0

DEPTH DEVIATION (m)

(m)

The CPT sounding rod is never truly vertical, of course.

How much can it be off?

6565

20

30

40

50

AC

TUA

L D

EPTH

20

30

40

50

AC

TUA

L D

EPTH

20

30

40

50

AC

TUA

L D

EPTH

5

10

15

20

25

Y-D

irect

ion

(m)

20.6 m

PLAN VIEW

"Unfolded"

0

10

20

30

40

50

0 1 2 3 4

DEPTH DEVIATION (m)

EPTH

(m

)

0

10

20

30

40

50

0 5 10 15 20 25

RADIAL DEVIATION (m)

EPTH

(m

)

6666

-5

0

-5 0 5 10 15 20 25

X-Direction (m)

Example 2

60

70

80

90

100

DE

60

70

80

90

100

DE

Inclination plane

X-plane Y-plane

Page 16: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

12

0

5

10

15

0 10 20 30Cone Stress, qt (MPa)

TH (

m)

0

5

10

15

0 100 200

Sleeve Friction (KPa)TH

(m

)

0

5

10

15

0 100 200 300 400

Pore Pressure (KPa)

TH (

m)

0

5

10

15

0.0 1.0 2.0 3.0 4.0

Friction Ratio (%)

TH (

m)

CLAY CLAYCLAY

6767

20

25

30

DEP

T 15

20

25

30

DEP

T 15

20

25

30

DEP

T

20

25

30

DEP

T

SILT SILT SILT

SAND SAND SAND

Results of a CPTU sounding

Soil profilingApplications

6868The Begemann original profiling chart (Begemann, 1965)

1

10

100

Con

e St

ress

, qt

(MPa

)

4

56

7

8

9

10

11

12

Friction Ratio from 0.1 % through 25 %

6969

Profiling chart per Robertson et al. (1986)

01 10 100 1,000

Sleeve Friction (KPa)

C

12

3 25 %

7070Profiling chart per Robertson (1990)

1

10

100

Con

e St

ress

, qE

(MPa

) 5 1 = Very Soft Clays, or Sensitive or Collapsible Soils 2 = Clay and/or Silt 3 = Clayey Silt and/or Silty Clay 4a = Sandy Silt 4b = Silty Sand 5 = Sand to Sandy Gravel

3

4

7171

0.11 10 100 1,000

Sleeve Friction (KPa)

1 2

The Eslami-Fellenius profiling chart (Eslami 1996; Eslami and Fellenius, 1997)

Example of a CPTU sounding from a river estuary delta (Nakdong River, Pusan, Korea)

0

10

20

30

0 10 20 30Cone Stress, qt (MPa)

DEP

TH (

m)

0

10

20

30

0 200 400

Sleeve Friction (KPa)

DEP

TH (

m)

0

10

20

30

0 250 500 750 1,000

Pore Pressure (KPa)

DEP

TH (

m)

0

10

20

30

0 1 2 3 4 5

Friction Ratio (%)

DEP

TH (

m)

Profile

Mixed

CLAY

7272

The sand layer between 6 m and 8 m depth is potentially liquefiable.

The clay layer is very soft.

The sand below 34 m depth is very dense and dilative, i.e., overconsolidated and providing sudden large penetration resistance to driven piles and relaxation problems.

30

40

50

30

40

50

30

40

50

30

40

50

SAN

Reduced pore pressure (“dilation”)

SAND

Page 17: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

13

1

10

100

one

Stre

ss, q

E (M

Pa)

5

3

4

7373

0.11 10 100 1,000

Sleeve Friction (KPa)

Co

1 2

The CPTU data of the Preceding Slide plotted in an Eslami-Fellenius Chart

The CPTU is an excellent and reliable tool for soil identification, but there is more to geotechnical site

investigation than just establishing the soil type.

And, the CPTU can deliver much more than soil profiling

7474

Liquefaction7.4 Magnitude Earthquake of August 17, 1999

Kocaeli, Adapazari, Turkey

7575

Photos courtesy of Noel J. Gardner, Ottawa

7676

Photo courtesy of Noel J. Gardner, Ottawa

dv

v rg

aCSR 'max65.0

σσ

=

CSR = Cyclic Stress Ratio

For earthquakemagnitude of 7.5

An earthquake generates a Cyclic Stress Ratio, CSR

Assessment of liquefaction risk fromresults of a CPTU sounding

7777

amax = maximum horizontal acceleration at ground surface (m/s2)

g = gravity constant (m/s2)

σv = total overburden stress (Pa)

σ'v = effective overburden stress (Pa)

rd = stress reduction coefficient for depth (dimensionless)

z = depth below ground surface (m)

CRR

The safety against liquefaction depends on the Cyclic Resistance Ratio, CRR, determined from the CPTU data

7878

CSRCRRFs = For earthquake magnitude of 7.5

Page 18: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

14

KPaqforqCRR cc 5005.0

100833.0 1

1 <+⎟⎠⎞

⎜⎝⎛=

)(045.0 114.0 cqeCRR =

The following fitted equation represents both equations above

The Cyclic Resistance Ratio, CRR, is expressed in two equations

KPaqKPaforq

CRR cc 1605008.0

10093 1

31 <<+⎟⎠

⎞⎜⎝

⎛=

7979

qc1 = cone stress normalized to depth (i.e., overburden stress)

CNc1 = normalization factor

σr = reference stress = 100 KPa (= atmospheric pressure)

σ'v = effective overburden stress at the depth of the conestress considered (KPa)

'11v

rccNcc qCqq

σσ

==where

CSRCRRFs =

Determining seismic risk from CPTU soundingEvery plotted point represents an earthquake observation (CSR)

with either no liquefaction of with liquefaction observed

Correlations between CRR-valuescalculated from actual earthquakesversus qc1 values for cases ofliquefaction (solid symbols) and noliquefaction (open symbols), andboundary curve (solid line) accordingto Robertson and Wride (1998) andYoud et al. (2001).

The boundary line is the CyclicR i t R ti C CRR hi h

All Data; 0 m through 16.0 m

0.4

0.5

0.6

0.7

SR

Robertson and Wride (1998)

Fines: 35 % 15 %

8080

Resistance Ratio Curve, CRR, whichis also shown as a linear regressioncurve for the boundary values. Thetwo dashed curves show theboundary curves for sand with finescontents of 15% and 35%,respectively (Stark and Olsen 1995).The original diagram has the conestress, qc, divided by atmosphericpressure to make the number non-dimensional.

Note, the effect of fines contents haslately become challenged.

0.0

0.1

0.2

0.3

0 5 10 15 20

Adjusted and Normalized Cone Stress, qc1 (MPa)

CS

0 m through 6.0 m

0.4

0.5

0.6

0.7

max

/g

All Data; 0 m through 16.0 m

0.4

0.5

0.6

0.7

CSR

Separating on two depths and looking at relative seismic force versus not-normalized cone stress.

Re-analysis of data from Moss et al. (2006)

8181

0.0

0.1

0.2

0.3

0 5 10 15 20

Not Normalized Cone Stress, qc (MPa)

a m

A

0.0

0.1

0.2

0.3

0 5 10 15 20

Not Normalized Cone Stress, qc (MPa)

C

BThe 'old' rule that liquefaction risk is small for shallow depth wherethe cone stress is ≥5 MPa appears to hold for quake ratio < 0.25.

In the past, liquefaction risk was based on values of the SPTN-index. Correlations between the CPTU, qc, and the N-indexindicate a ratio between qc and N of about 5. However, thatratio has a very large range between low and high. It isquestionable how relevant and useful a conversion from an

8282

qSPT Index value to a cone stress would be for an actual site.One would be better served pushing a cone in the first place.

Example of determining liquefaction susceptibility before and after vibratory compaction

0

1

2

3

4

0 5 10 15 20Cone Stress (MPa)

(m)

0

1

2

3

4

0 50 100 150 200Pore Pressure (KPa)

H (

m)

0

1

2

3

4

0 20 40 60 80Sleeve Friction (KPa)

H (

m)

0

1

2

3

4

0.0 0.5 1.0Friction Ratio (%)

H (

m)

Sand

PROFILE

Fine sand to Silty Sand

8383

5

6

7

8

9

10

DEP

TH

5

6

7

8

9

10

DEP

TH5

6

7

8

9

10

DEP

TH 5

6

7

8

9

10

DEP

TH

Sand

Silty Clayand Clay

Four CPTU initial (before compaction) soundings at Chek Lap Kok Airport. The heavy lines in the cone stress, sleeve friction, and friction ratio diagrams are the geometric averages for each depth of the four soundings.

10

15

ss, q

E (M

Pa)

1 = Very Soft Clays, Sensitive and/or Collapsible Soils 2 = Clay and/or Silt 3 = Clayey Silt and/or Silty Clay 4a = Sandy Silt and/or Silt

5

Soil chart

8484

0

5

0 20 40 60 80 100

Sleeve Friction (KPa)

Con

e St

res 4b = Fine Sand and/or

Silty Sand 5 = Sand to Sandy Gravel

4b

4a

3

21

Page 19: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

15

0

1

2

3

4

5

0 5 10 15Cone Stress (MPa)

TH (

m)

0

1

2

3

4

5

0 10 20 30 40 50Sleeve Friction (KPa)

TH (

m)

0

1

2

3

4

5

0 50 100 150 200Pore Pressure (KPa)

TH (

m)

0

1

2

3

4

5

0.0 0.1 0.2 0.3 0.4 0.5Friction Ratio (%)

TH (

m)

7 Days7 Days

Before

8585

6

7

8

9

10

DE

PT

6

7

8

9

10

DE

P

6

7

8

9

10

DE

PT

6

7

8

9

10

DE

PT

7 DaysBeforeBefore

Geometric average values of cone stress, sleeve friction, and friction ratios andmeasured pore pressures from CPTU soundings at Chek Lap Kok Airport beforeand seven days after the vibratory compaction.

Fs versus depth0

1

2

3

4

5

0.00 1.00 2.00 3.00 4.00 5.00

Factor of Safety, Fs (--)

PTH

(m

)

Before Compaction

7 Days after

CSRCRRFs =

8686

Factor of safety against liquefaction before and after vibratory compaction

6

7

8

9

10

DEP compaction

CPT and CPTU Methods

for Calculating the Ultimate

Resistance (Capacity) of a Pile

Schmertmann and Nottingham (1975 and 1978)

8787

Meyerhof (1976)

deRuiter and Beringen (1979)

LCPC, Bustamante and Gianeselli (1982 )

Eslami and Fellenius (1997 )

ICP, Jardine, Chow, Overy, and Standing (2005)

But we will save those methods for later

Vibrations from Pile Driving

v = 433 Eh

Z P

M g hr

= 433 Eh

Z P

M g hx2 + z2

V = vertical component of the ground vibration, m/sEh = hammer efficiency coefficientZP il i d N /

88

ZP = pile impedance, Ns/mM = hammer (ram) mass, NG = acceleration, m/s2

H = hammer height-of-fall, m, taken as the equivalentheight-of-fall that corresponds to the kinetic energyat impact

z = pile penetration depth, mx = horizontal distance at the ground surface from pile

to observation point, m

Most ground vibrations are generated from the pile toe

6

8

10

12

14

16

18

20

bration Velocity, v

0  (m

m/s)

89

0

2

4

0 5 10 15 20 25 30 35 40 45 50

Distance to pile toe, r  (m)

Vi

Vibrations from driving a long toe bearing pile: measured compared to calculated

Page 20: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

1

BASICS OF DESIGN OF PILED

FOUNDATIONS

Bengt H Fellenius

1

Bengt H. Fellenius

Load Transfer and Capacity of Piles

Bolivia, April 25, 2013 22Driving closed-toe pipe piles into fine sand about 2.5 m above the groundwater table

33Driving 12-inch precast concrete pile into clay for Sidbec in 1974

Head measured in aquifer below the clay layer

44Svärta River 1969

GW

What really is Capacity?

For piles, capacity is

what we determine in

55

— define from —

a loading test

?

e.g.: The Offset Limit Load (Davisson, 1972)

Do you agree that this pointon the curve represents thecapacity of the pile?

Qu

Qu

66

Rs

Rt

Page 21: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

2

γγ NbNqNcr qcu '5.0'' ++=

and for Footings?The Bearing Capacity Formula

where ru = ultimate unit resistance of the footingc’ = effective cohesion interceptB = footing width’ b d ff ti t t th f d ti l l

77

q’ = overburden effective stress at the foundation levelγ‘ = average effective unit weight of the soil below the foundation

Nc, Nq, Nγ = non-dimensional bearing capacity factors

The main factor is the

“Nq”

Nq

88

Nq

But what is the reality?

φ

Results of static loading tests on 0.25 m to 0.75 m square footings in well graded sand (Data from Ismael, 1985)

400

500

600

700

D

( KN

)

1.00 m

0.75 m

0.50 m

0.25 m

1,000

1,200

1,400

1,600

1,800

2,000

S S

( K

Pa

)

Normalized

99

0

100

200

300

0 10 20 30 40 50

SETTLEMENT (mm)

L O

A D

MOVEMENT

0

200

400

600

800

,

0 5 10 15 20

MOVEMENT/WIDTH (%)

S T

R E

S

1.00 m

0.75 m

0.50 m

0.25 m

Normalized

0

2

4

0 5 10 15 20Cone Stress, qt (MPa)

0

2

4

0 100 200 300 400

Sleeve Friction, fs (KPa)

0

2

4

0 20 40 60 80

Pore Pressure (KPa)

0

2

4

0 1 2 3 4 5

Friction Ratio, fR (%)

SAND

CPTU PROFILE

Load-Movement for Five Footings on Sandat Texas A&M University Experimental Site.

J-L. Briaud and R.M. Gibbens, 1994, ASCE GSP 41,

10

6

8

10

12

14

16

DEPT

H (

m)

6

8

10

12

14

16

DEPT

H (m

)

6

8

10

12

14

16

DEP

TH (

m)

6

8

10

12

14

16

DEPT

H (m

)

SANDY CLAYEY SILT

Eslami- RobertsonFellenius

As before the data will tell usmore, if we divide the load withthe footing area (to get stress)and divide the movement withthe footing width, as follows.

Load-Movement of Four Footings on SandTexas A&M University Experimental Site

ASCE GSP 41, J-L Briaud and R.M. Gibbens 1994

8,000

10,000

12,000

N )

3.0 m

3.0 m 1,400

1,600

1,800

2,000

KPa

)

Texas A&MSettlement Prediction Seminar

11

0

2,000

4,000

6,000

,

0 50 100 150 200

MOVEMENT ( mm )

L O

A D

(

KN

1.5 m

1.0 m

2.5 m

0

200

400

600

800

1,000

1,200

0 5 10 15 20

MOVEMENT / WIDTH (%)

S T

R E

S S

(

Load-Movement of Four Footings on SandTexas A&M University Experimental Site

ASCE GSP 41, J-L Briaud and R.M. Gibbens 1994

8,000

10,000

12,000

N )

3.0 m

3.0 m1,600

2,000

)

e

QQ

⎟⎟⎠

⎞⎜⎜⎝

⎛=

2

1

2

1

δδ

e = 0.4

q-z curve:

We can also borrow from pileanalysis (Pile toe response) andapply a q-z function to the stress-movement data. The "Ratio" functionis applied here.

Texas A&MSettlement Prediction Seminar

12

0

2,000

4,000

6,000

,

0 50 100 150 200

MOVEMENT ( mm )

L O

A D

(

KN

1.5 m

1.0 m

2.5 m

0

400

800

1,200

0 5 10 15 20MOVEMENT/WIDTH, δ (%)

STR

ESS,

σ

(KPa

)

Page 22: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

3

Lehane et al. 2008Settlement Prediction Seminar

200

250

300

350

400

450

500

OA

D (

KN

)

1.0 m 1.5 m

1.0 m

200

300

400

500

RES

S (K

Pa)

1.0 m

13

Lehane, B.M., Doherty, J.P., and Schneider, J.A., 2008. Settlement prediction for footings on sand. Conference on Deformational Characteristics of Geomaterials. S.E. Burns, P.W. Mayne, and J.C. Santamarina (Editors), Atlanta, September 22-24, 2008, Vol. 1, pp.133-150.

0

50

100

150

0 10 20 30 40 50

MOVEMENT (mm)

L

0

100

0 1 2 3 4 5 6 7 8

MOVEMENT / WIDTH (%)

STR

Footing, 1.5 mFooting 1.0 mFooting 1.0 m

Six footings on gravel

Caisson under air pressure to control water level.

GW//\\//\\//\//\\//\\ //\\//\\//\//\\//\\

14 m16 m

6,000

8,000

10,000

12,000

14,000

TRES

S (K

Pa)

0.3 x 0.3

14Kusakabe, O., Maeda, Y., and Ohuchi, M., 1992. Large-scale loading tests of shallow footings in pneumatic caisson. ASCE Journal of Geotechnical Engineering, 118(11) 1681-1695.

"SCORIA" = Sandy GRAVEL, trace fines. An "interlocked" and highly overconsolidated volcanic soil.

e0 = 1.2, wn = 40 %, ρ = 1,800 kg/m3

``W

Footing test

!?

0

2,000

4,000

0 5 10 15 20 25 30 35 40

NORMALIZED MOVEMENT (%)

ST

0.3 x 0.30.4 x 0.40.7 X 0.71.3 X 1.30.4 X 1.20.4 X 2.0

8,000

10,000

12,000

14,000

ESS

(KPa

)

Considering the "Preloading"/"Reloading"/"Prestress" Effect

15

0

2,000

4,000

6,000

0 5 10 15 20 25 30 35 40

NORMALIZED MOVEMENT (%)

STR

E

0.3 x 0.30.4 x 0.40.7 X 0.71.3 X 1.30.4 X 1.20.4 X 2.0

Data from Kusabe et al. 1992

Plate loading tests on 0.55 m x 0.65 m and 1.10 m x 1.30 m rectangular slabs in silty sand at Kolbyttemon, Sweden

1,500

2,000

(KPa

)

TREND1 1m x 1 3m

16Fellenius (2011). Data from Bergdahl, U., Hult, G., and Ottosson, E. (1984)

0

500

1,000

0 1 2 3 4 5 6 7 8 9 10MOVEMENT (%)

STR

ESS

0.55m x 0.65m

1.1m x 1.3m

Ultimate Shaft Resistance

rs, RsUltimate Shaft Resistance

is a reality

1717

Ultimate Toe Resistance does not exist other than as a definition of load at a certain movement

rt, Rt

Ultimate Toe Resistance does not exist other than as a definition of load at a certain movement

Ultimate Toe Resistance is not

50

100

150

200

AG

E S

HA

FT S

HEA

R(K

Pa)

O-cell to GL3

GL3 to GL1Pile D2000

2,000

3,000

4,000

RA

GE

STR

ESS

AN

DSH

EAR

(K

Pa)

Toe Resistance

Pile D2000

Shaft and toe resistances from full-scale static loading tests on a 2,000 m diameter, 85 m long bored pile in silty clay

Shaft Resistance Toe Resistance

1818

0

50

0 20 40 60 80 100

MOVEMENT (mm)

AVE

R

0

1,000

0 20 40 60 80 100MOVEMENT (mm)

AVE

R S

Shaft resistances(repeated for reference)

The above curve shows the shape of theload-movement every toe resistance."Ultimate Toe Resistance" does not exist!

A pile toe reacts to load by a stiffnessresponse and failure does not occurhowever much the pile toe is moveddown.

Page 23: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

4

• Pile capacity is the combined effect of shaft resistance and toe resistance.

• Shaft resistance is governed by shear strength, which has an ultimate value. That is, shaft capacity is reality.

• In contrast, toe resistance is governed by

1919

In contrast, toe resistance is governed by compression, which does not have an ultimate value. As the load is increased, a larger and larger soil volume is stressed to a level that produces significant compression, but no specific failure or peak value: Toe capacity is a delusion.

Analysis Methods for Determining Shaft Resistance, rs

The Total Stress Method

The Lambda Method

Th SPT M th d

2020

The SPT Method

The CPT and CPTU Methods

The Pressuremeter Method

The Beta Method

where rs = unit shaft resistance

τu = undrained shear strength

α = reduction coefficient for τu > ≈100 KPa

[ ]uusr αττ ==

Piles in Clay

Total Stress Method

"Alpha analysis"

2121

The undrained shear strength can be obtained from unconfined compression tests, field vane shear tests, or, to be fancy, from consolidated, undrained triaxial tests. Or, better, back-calculated from the results of instrumented static loading tests. However, if those tests indicate that the unit shaft resistance is constant with depth in a homogeneous soil, don’t trust the analysis!

2222

Clay adhering to extracted piles

Photo courtesy of K.R. Massarsch

The Lambda MethodVijayvergia and Focht (1972)

)2'( mms cr += σλ

where rm = mean shaft resistance along the pileλ = the ‘lambda’ correlation coefficientσ’m = mean overburden effective stresscm = mean undrained shear strength

Piles in Clay

2323

Approximate Values of λ

Embedment λ(Feet) (m) (-)

0 0 0.5010 3 0.3625 7 0.2750 15 0.2275 23 0.17

100 30 0.15200 60 0.12

The Lambda method was developed for long piles in clay deposits (offshore conditions)

{ } 'tan')/2()()(lg87.0)(016.02.28.0 2.042.0 δσ zts bhOCRSOCRr −−+=

where rs = unit shaft resistance

OCR = overconsolidation ratioSt = sensitivity

Piles in Clay

A method from fitting a variety of parameters to results from static loading tests

2424ICP (Imperial College Pile method)

Jardine, Chow, Overy, and Standing (2005 )

h = height of point above pile toe ; h ≤ 4bb = pile diameterδ’ = interface friction angle

Page 24: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

5

The SPT MethodMeyerhof (1976)

Rs = n N As D

where Rs = ultimate shaft resistance

n = a coefficient

N = average N-index along the pile shaft (taken as a pure number)

Piles in Sand

2525

g g p ( p )

As = unit shaft area; circumferential area

D = embedment depth

n = 2·103 for driven piles and 1·103 for bored piles (N/m3)[English units: 0.02 for driven piles and 0.01 for bored piles (t/ft3)]

For unit toe resistance, Meyerhof's method applies the N-index at the pile toe times a toe coefficient = 400·103 for driven piles and 120·103 for bored piles (N/m3)

[English units: 4 for driven piles and 1 for bored piles (t/ft3)]

CPT and CPTU Methods

for Calculating the Ultimate

Resistance (Capacity) of a Pile

Schmertmann and Nottingham (1975 and 1978)

2626

deRuiter and Beringen (1979)

Meyerhof (1976)

LCPC, Bustamante and Gianeselli (1982 )

ICP, Jardine, Chow, Overy, and Standing (2005)

Eslami and Fellenius (1997 )

caOCRt qCr =The CPT and CPTU Methods

where rt = pile unit toe resistance (<15 MPa)COCR = correlation coefficient governed by the

Schmertmann and Nottingham(1975 and 1978)

CLAY and SAND

SAND (alternative)ccs qKr =sfs fKr =

2727

overconsolidation ratio, OCR, of the soil qca = arithmetic average of qc in an influence zone*)

Kf = a coefficient depends on pile shape and material, cone type, and embedment ratio. In sand, the coefficient ranges from 0.8 through 2.0, and, in clay, it ranges from 0.2 through 1.25.

Kc = a dimensionless coefficient; a function of the pile type, ranging from 0.8 % through 1.8 %

qc = cone resistance (total; uncorrected for pore pressure on cone shoulder)

*) The Influence zone is 8b above and 4b below pile toe2828

Filtering of qc-values and determining pile toe resistance (Schmertmann method)

deRuiter and Beringen(1979)

uct SNr =

us Sr α=Means turning the CPT-

method into the Total St th d

2929

where rt = pile unit toe resistanceNc = conventional bearing capacity factor

Su = undrained shear strength — — — — —>

NK = a dimensionless coefficient, ranging from 15 through 20, reflecting local experience

α = adhesion factor equal to 1.0 and 0.5 for normally consolidated and overconsolidatedclays, respectively

An upper limit of 15 MPa is imposed for rt

k

cu N

qS =

Stress method

LCPC Bustamante and Gianeselli (1982 )

cs qKr =

cat qCr =

3030

C = toe coefficient ranging from 0.40 through 0.55qca = cone stress averaged in a zone 1.5 b above and

1.5 b below the pile toe plus filtering

rt = pile unit toe resistance < 15 KPa, <35 KPa, or <120 KPa, depending on soil type, pile type, and pile installation method

K = a dimensionless coefficient; a function of pile type, rangingfrom 0.5 % through 3.0 % (Compare: Schmertmann proposes 0.8 %

through 1.8 %)

Page 25: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

6

Soil Type Cone Stress Bored Piles Driven Piles Maximum rt

CLCPC CLCPC

(MPa) (- - -) (- - -) (MPa)

CLAY - - qc < 1 0.04 0.50 15

Coefficients and Limits of Unit Toe Resistance in the LCPC Method Quoted from the CFEM (1992)

3131

c

1 < qc < 5 0.35 0.45 15

5 < qc - - - 0.45 0.55 15

SAND - - - qc < 15 0.40 0.50 15

12 < qc - - - 0.30 0.40 15

Soil Type Cone Stress Concrete Piles Steel Piles Maximum rs(MPa) & Bored Piles

KLCPC KLCPC J

(- - -) (- - -) (KPa)

CLAY - - qc < 1 0.011 (1/90) 0.033 (=1/30) 15

1 5 0 025 (1/40) 0 011 ( 1/80) 35

Coefficients and Limits of Unit Shaft Resistance in the LCPC Method Quoted from the CFEM (1992)

3232

1 < qc < 5 0.025 (1/40) 0.011 (=1/80) 35

5 < qc - - - 0.017 (1/60) 0.008 (=1/120) 35

SAND - - - qc < 5 0.017 (1/60) 0.008 (=1/120) 35

5 < qc < 12 0.010 (1/100) 0.005 (=1/200) 80

12 < qc - - - 0.007 (1/150) 0.005 (=1/200) 120

The values in the parentheses are the inverse of the KLCPC-coefficient

cac

t qdbr )5.01( −=

cJs qKr =

σ ' b

ICP (Imperial College Pile method)Jardine, Chow, Overy, and Standing (2005 )

3333

δσσσ tan)')()'(0145.0( 38.013.0

mtr

zcJ h

bqK Δ+=

bq

qqrz

rzccmc 01.0)]

'(10216.1)'(00125.00203.0(2[' 1

265.0 −−− ∗−+=Δ

σσσσσ

Egtt qCr =Eslami and Fellenius

(1997 )

Ess qCr =

rt = pile unit toe resistance

Ct = toe correlation coefficient (toe adjustment factor)—equal to unity in most cases

Shaft Correlation Coefficient

Soil Type*) Cs

Soft sensitive soils 8 0 %

bCt 3

1=

bCt

12=

b in metre

b in inch

3434

qEg = geometric average of the cone point resistance over the influence*) zone after correction for pore

pressure on shoulder and adjustment to “effective” stress rs = pile unit shaft resistanceCs = shaft correlation coefficient, which is a function of soil

type determined from the soil profiling chartqE = cone point resistance after correction for pore pressure

on the cone shoulder and adjustment to “effective” stress

*) The Influence zone is 8b above and 4b below pile toe

Soft sensitive soils 8.0 %Clay 5.0 %Stiff clay andClay and silt mixture 2.5 %Sandy silt and silt 1.5 %Fine Sand and silty Sand 1.0 %Sand to sandy gravel 0.4 %

*) determined directly from the CPTU soil profiling

Unit shaft resistance as a function of cone stress, qc in Sandaccording to the LCPC method and compared to the Eslami-Fellenius method

100

120

140

ce, r

s (K

Pa)

Sandy Silt to silty Sand to sandy Gravel

Concrete

Range for the Eslami Fellenius method

3535

0

20

40

60

80

0 5 10 15 20 25 30 35 40

Cone Stress, qc (MPa)

Uni

t Sha

ft R

esis

tan piles

Steel piles

PILES IN SAND

Cone Stress, qc and qt (MPa)

Pile Capacity or, rather, Load-Transfer follows

principles of effective stress

3636

principles of effective stress and is best analyzed using the

Beta method

Page 26: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

7

the Beta method

Unit Shaft Resistance, rs

zsr 'βσ=

where c‘ = effective cohesion interceptβ = Bjerrum-Burland coefficientσ'z = effective overburden stress

Effective Stress Analysis (Beta-analysis as opposed to Alpha analysis)

3737

dzcAdzrAR zssss )''( βσ+∫=∫=Total Shaft Resistance, Rs

where As = circumferential area of the pile at Depth z(surface area over a unit length of the pile)

Shaft Resistance — in Sand and in Clay

KMr ''tan σφ=

vsr 'σβ=

3838

where rs = unit shaft resistance

M = tan δ’ / tan φ’

Ks = earth stress ratio = σ’h / σ’vσ‘v = effective overburden stress

vss KMr tan σφ=

Approximate Range of Beta-coefficients

SOIL TYPE Phi Beta

Clay 25 - 30 0.20 - 0.35

Silt 28 - 34 0.25 - 0.50

Sand 32 - 40 0.30 - 0.90

Gravel 35 - 45 0.35 - 0.80

0.05 - 0.80 !

3939

Gravel 35 45 0.35 0.80

These ranges are typical values found in some cases. In any given case,actual values may deviate considerably from those in the table.

Practice is to apply different values to driven as opposed to bored piles, but ....

2.0

3.0

4.0

5.0

6.0

coef

ficie

nt i

n s

and

G

Trend line

4040

0.0

1.0

0 5 10 15 20 25 30

LENGTH IN SOIL (m)

ß-c

HK GEO (2005)CFEM (1992)

Gregersen et al. 1973

Beta-coefficient versus embedment length for piles in sand (Data from Rollins et al. 2005). Ranges suggested by CFEM (1993), Gregersen et al 1973, and Hong Kong Geo (2005) have been added.

1.00

1.50

2.00

2.50

OEF

FIC

IEN

T IN

SA

ND

Concrete piles

Open-toe pipe piles

Closed-toe pipe piles

Gregersen

4141

0.00

0.50

0 50 100 150 200 250 300 350

AVERAGE EFFECTIVE STRESS, σ'z (KPa)

ß-C

O et al. 1973

Beta-coefficient versus average σ’ for piles in sand. (Data from Clausen et al. 2005).

1.00

1.50

2.00

2.50

FIC

IEN

T IN

SA

ND

Concrete piles

Open-toe pipe piles

Closed-toe pipe piles

4242

0.00

0.50

0.0 0.2 0.4 0.6 0.8 1.0 1.2

AVERAGE DENSITY INDEX, I D

ß-C

OEF

Beta-coefficient versus average ID for piles in sand. (Data from Karlsrud et al. 2005).

Page 27: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

8

0.20

0.30

0.40

0.50

0.60co

effic

ient

in

cla

y

Norway Japan Thailand Vancouver Alberta

4343

0.00

0.10

0 20 40 60 80

PLASTICITY INDEX, I P

ß-c

Beta-coefficient versus average IP for piles in clay. (Data from Karlsrud et al. 2005 with values added from five case histories).

c

CCI

CKr

vD

C eCe

K φβ σσ

tan'

ln100

10

24

302

⎟⎟⎠

⎞⎜⎜⎝

⎛−

−=

Where K = coefficient of earth stress at restI = density index (“relative density”)

The Beta-coefficient has a certain appeal to the academia it seems. This is what is proposed in a recent issue of the ASCE Journal.

44

ID = density index ( relative density )σ’v = effective overburden stressσr = reference stress = 100 KPaΦ = triaxial-compression critical-state

friction angleC1 = a coefficient: 0.6< C1 <0.7C2 = a constant = 0.2C3 = a constant = 0.4C4 = a constant = 1.3

Unit Toe Resistance, rt

where Nt = toe “bearing capacity” coefficient

D = depth to pile toeσ'z=D = effective overburden stress at the pile toe

Dztt Nr == 'σ

Toe Resistance

4545

Total Toe Resistance, Rt

where At = toe area (normally, the cross sectional area of the pile)

Dzttttt NArAR === 'σ

Approximate Range of Nt-coefficients

SOIL TYPE Phi Nt

Clay 25 - 30 3 - 30Silt 28 - 34 20 - 40Sand 32 - 40 30 - 150Gravel 35 - 45 60 - 300

4646

The Toe Resistance, Rt, while not really an “ultimate” resistance, isusually considered as such in design. However, toe resistance should bethought of as that mobilized in a static loading test at the maximumacceptable movement usually considered applicable to a piled foundation.

Also the toe resistance appears to have certain qualitiesintriguing to the academia. This is what is proposed inthe same recent issue of the ASCE Journal.

DDccD ICC

r

hICCCr

ICtoeu eCeCr 876542 )'()(

21,−−+−=

σσσ φφ

Where ru, toe = ultimate toe resistance for a pile head movementequal to 10 % of the pile diameter

ID = density index (“relative density”)

!!!

47

D y ( y )σ’h = effective horizontal stress (= σ’v/K0?)Φ = triaxial-compression critical-state friction angleC1 = a constant = 0.23C2 = a constant = 1.64C3 = a constant = 0.0066C4 = a constant = 0.10414C5 = a constant = 0.0264C6 = a constant = 0.0002C7 = a constant = 0.841C8 = a constant = 0.0047

Total Resistance (“Capacity”)

tsult RRQ +=

suzsuz RQdzAQQ −=∫−= 'σβ

0

5

10

0 500 1000 1500 2000

LOAD

H

Qult/ Rult

4848

15

20

25

DEP

TH

Rt Rs

Effective stress — Beta — analysis is the method closest to the real response of a pile to an imposed load

Page 28: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

9

0

1

2

0 50 100 150

UNIT SHAFT RESISTANCE (KPa)

0

1

2

0 100 200 300 400 500 600 700 800

TOTAL SHAFT RESISTANCE (KN)

Pile CCPT-3

Calculations of unit and total shaft resistances for a pile driven into asaprolite (residual soil) in Porto, Portugal. The soil can be classified bothas a clay type and sand type.

Shaft resistance by CPT-methods

4949

3

4

5

6

DEP

TH (

m)

DutchSand

MeyerhofSand

LCPCSand

LCPCClay Schmertmann

Clay

Eslami-Fellenius

SchmertmannSand

DutchClay

TumayClaya

3

4

5

6

DEPT

H (

m)

Effective StressBeta = 1.00

DutchSand

MeyerhofSand

LCPCClay &Sand

SchmertmannClay

Eslami-Fellenius

SchmertmannSand

DutchClay

TumayClayb

0

1

2

0 200 400 600 800 1,000 1,200 1,400 1,600 1,800 2,000

CALCULATED PILE RESISTANCE (KN)

TumayClay

Eslami-Fellenius

SchmertmannClayDutch

Clay

LCPC

DutchSand

MeyerhofSand

Pile CCPT-3

Total resistance by CPT-methods

5050

3

4

5

6

DEP

TH (

m) Schmertmann

Sand

LCPCSand

LCPCClay

a

Let’s look at a few case studies

Annacis/Lulu Island Tests, Vancouver,

BC

by UBC 1985

5151

Static loading tests on three 324 mm diameter pipe piles driven to depths of 14 m, 17 m, and 31 m into the Fraser River deltaic soils

0

5

10

15

20

0 5 10 15Cone Stress, qt (MPa)

PTH

(m

)

0

5

10

15

20

0 100 200

Sleeve Friction (KPa)

TH (

m)

0

5

10

15

20

0 500 1,000

Pore Pressure (KPa)

PTH

(m

)

0

5

10

15

20

0 1 2 3 4 5

Friction Ratio (%)

PTH

(m

)

PILES1 2 3 4

PROFILE

Eslami-Fellenius Robertson

CLAY CLAY

SANDSAND

SANDGRAVEL & SAND

CPT and CPTU analysis for capacity

5252

25

30

35

40

DEP

25

30

35

40

DEP

25

30

35

40D

EP

25

30

35

40

DEP

CLAY andSilty

CLAY

CLAY andSilty

CLAY

Annacis/Lulu Island Tests by UBC 1985

The results of the load-movement curves from all three tests combined in

600

800

1,000

1,200

OA

D (K

N)

Depth 16.8 mSet-up Time

85 days

Depth 31.1 mSet-up Time

38 days

5353Data from Lulu Island Tests

by UBC 1985

tests combined in one graph. (With offset limit lines and maximum load in the tests).

0

200

400

0 10 20 30 40

MOVEMENT (mm)

LO

Depth 13.7 mSet-up Time

197 days

Results of CPT and CPTU analysis compared tocapacity from the static loading tests

0

5

10

0 500 1,000 1,500 2,000

SHAFT RESISTANCE (KN)

Eslami-Fellenius

DutchLCPC

SchmertmannUniPile eff.stress

ß = 0 15

0

5

10

0 500 1,000 1,500 2,000

SHAFT and TOE RESISTANCEs (KN)

Eslami-FelleniusDutchLCPCSchmertmannUniPile eff. stressPile static tests

ß = 0.15

5454“UniPile eff.stress” is effective stress analysis matched to results of static tests

15

20

25

30

35

DEP

TH (

m)

ß = 0.15

ß = 0.20

ß = 0.15

15

20

25

30

35

DEP

TH (

m)

ß 0.15 Nt = 7

ß = 0.20 Nt = 25

ß = 0.15 Nt = 3

Test too soon after EOID

Page 29: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

10

150

a)

O-cell to GL3 GL3 to GL2 GL2 to GL1O-cell to GL2 O-cell to GL1

Sunrise City Project, HoChiMinh City, Vietnam1,800 mm diameter bored piles constructed to 70 m depthUnit shaft resistances versus measured downward movement at depths of ≈50 m

150

Pa)

O-cell to GL4 GL4 to GL3 GL3 to GL2O-cell to GL3 O-cell to GL2 O-cell to GL1

SHAFT RESISTANCE

HoChiMinh

Ha Noi

Cai Mep Port

55

0

25

50

75

100

125

0 1 2 3 4 5 6 7 8 9 10

MOVEMENT (mm)

UN

IT S

HA

FT R

ESIS

TAN

CE

(KPa

TBP-1

Next reading was at 56 mm

ß = 0.14

0

25

50

75

100

125

0 1 2 3 4 5 6 7 8 9 10

MOVEMENT (mm)

UN

IT S

HA

FT R

ESI

STA

NC

E (K

P

TBP-2

ß = 0.13

Next reading was at 35 mm

No records were obtained during the sudden movement occurring at about 5 mm

0

500

1,000

1,500

2,000

2,500

0 50 100 150 200

MOVEMENT (mm)

UN

IT R

ESIS

TAN

CE

(KPa

)

TBP-1

Unit Toe Resistance

Unit Shaft Resistances

10% of diameter

TOE RESISTANCE

56

0

500

1,000

1,500

2,000

2,500

0 50 100 150 200

MOVEMENT (mm)

UN

IT R

ESIS

TAN

CE

(K

Pa)

TBP-2

TBP-1Unit Toe Resistance

Unit Shaft Resistances

The stiffness of the toe stress-movement is unusually soft for adense sand and typical of a pilehaving a layer of debris at the bottomof the shaft when the concrete wasplaced. A pile a few metre to the sidewas constructed using the samemethod and equipped with a coringtube. Coring through this pile toe intothe soil two weeks after constructionrevealed presence of about 30 mm ofsoft material between the pile and thesoil.

Core from the pile toe and into the soil below

57

Bridge over Panama Canal, Paraiso Reach, Republic of PanamaO-cell test on a 2.0 m (80 inches) diameter, 30 m (100 ft) deep shaft

drilled into the Pedro Miguel and Cucaracha formations, February 2003.

0

5

0 5,000 10,000 15,000 20,000 25,000 30,000

LOAD (KN) ß

0.30

0.45

5858

10

15

20

25

30

DEP

TH (

m) 0.30

___

1.20

O-cell Tests on an 11 m long, 460 mm square precast concrete pile driven in silica sand in

North-East Florida(Data from McVay et al 1999)

0

2

4

6

8

0 500 1,000 1,500 2,000 2,500 3,000

Shaft Resistance, Rs (KN)

(m

)

E-FLCPCSchmertmannDutchMeyerhofBetaTests

5959

(Data from McVay et al. 1999)

A study of Toe and Shaft Resistance

Response to Loading

10

12

14

16

18

20

DEP

TH

The foregoing analysis results are quite good predictions

They were performed after the test results were known

Such “predictions” are always the best!

So, what about true predictions?

6060

Let’s see the results of a couple ofPrediction Events

p

Page 30: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

11

ULTIMATE R

Prediction Event at Deep Foundations Institute Conference in Raleigh, 1988

6161

44 ft embedment, 12.5 inch square precast concrete driven through compact silt and into dense sand

Capacity in Static Loading Test = 200 tonsRESISTANCE

TonsPREDICTORS (60 individuals)

1,500

2,000

2,500

ity (

KN

)

Orlando 2002 Predictions

Max LoadAvailable

6262

0

500

1,000

Predictors

Cap

ac

500

600

700

KN

)

0 20 40 60 80MOVEMENT (mm)

FHWA Washington, DC, 1986

273 mm diam. closed-toe pipe pile driven 9.1 m into hydraulic sand fill

6363

0

100

200

300

400

1 2 3 4 5 6 7 8 9 10PREDICTIONS

CA

PAC

ITY

( 800

1,000

1,200K

N)

0 2 4 6 8 10 12 14 16 18MOVEMENT (mm)

FHWA Baltimore, MD, 1980

Two 273 mm diam. closed-toe pipe piles driven 13.1 m into Beaumont clay

6464

0

200

400

600

800

PARTICIPANTS

CA

PAC

ITY

(K

1,500

2,000

2,500

3,000

3,500

OA

D (

KN

)

Singapore 2002

1,400

1,600

1,800

2,000

65

0

500

1,000

1 3 5 7 9 11 13 15 17 19 21 23 25 27 29 31 33

L

400 mm H-Pile (168 kg/m) driven through sandy clay to a 15 m embedment

0

200

400

600

800

1,000

1,200

0 10 20 30 40 50MOVEMENT (mm)

LOA

D (

KN

)

Brazil 2004: Bored pile (Omega screw pile) 23 m long, 310 mm diameter

0

2

4

6

8

0 20 40 60 80

Water Content (%)

(m)

0

5

10

0 5 10 15 20 25N-Index (blows/0.3)

(m)

SPT 18at 23 m Pile

0

2

4

6

8

0 25 50 75 100

Grain Size (%)

(m)

SILT

SAND CLAY

Sandy SiltyCLAY (Laterite)

Sandy SILT

6666

10

12

14

16

18

20

DEP

TH

wnwP wLGW

15

20

25

DEP

TH

10

12

14

16

18

20

DEP

TH Sandy SILT

and CLAY

Sandy ClayeySILTGW

Page 31: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

12

Brazil 2004

Static Loading Test

on a 23 m 310 mm bored pile

Load-Movement Response

1,500

2,000

2,500

KN

)

Prediction Compilation

2,000

2,500PUSH L= 23m

0 5 10 15 20 25 30

MOVEMENT (mm)

6767

0

500

1,000

0 10 20 30 40

MOVEMENT (mm)

LOA

D (

K

0

500

1,000

1,500

PARTICIPANTS

LOA

D (

KN

)

Portugal 2004. Precast 350 mm diameter pile driven to 6 m depthin a saprolite, a residual soil consisting of silty clayey sand.

0

1

2

3

0 10 20Cone Stress, qt (MPa)

) 1 500

2,000

2,500

3,000

PAC

ITY

(KN

)

CAPACITY FROM STATIC LOADING TEST

Pile C1

6868

4

5

6

7

8

DEP

TH (

m

0

500

1,000

1,500

1PREDICTIONS

TOTA

L C

AP

0

OFFSET LIMIT LOAD

1,200

1,400

1,600

1,800

KN

)

Pipe-Pile

0 10 20 30 40MOVEMENT (mm)

Northwestern University, Evanston, Illinois, 1989.15 m embedment, 457 mm diameter closed-toe pipe piles driven in sand on clay.

6969

0

200

400

600

800

1,000

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24

CA

PAC

ITY

(K

PREDICTIONS

Finno 1989

Edmonton, Alberta, 2011

Prediction of load-movement and capacity of a 400-mm diameter, 18 mlong, augercast pile constructed in transported and re-deposited glacial till.

2 000

3,000

4,000D

(KN

)E = 20 GPaE = 35 GPa

70

0

1,000

2,000

0 5 10 15 20 25 30 35 40 45 50

MOVEMENT (mm)

LOA

D

10 capacity predictions are at movements > 50 mm

7 mm (4 mm + b/120 mm)TEST RESULTS

Values

Rea

ltive

Fre

quen

cy

σ = Standard Deviation, σ = 833 µ = Mean, 1,923 σ/µ = Coefficient of Variation, COV = 0.43

Mean, µ

NORMAL DISTRIBUTIONEdmonton 2011

71

CAPACITY PREDICTIONS

T he area between -σ and +σ f ro m the mean value is 68% o f to tal areaT he area between -2σ and +2σ f ro m the mean value is 95% o f to tal areaT he area between -3σ and +3σ f ro m the mean value is 99% o f to tal area

0

100

200

0 10 20 30 40 50 60 70 80 90 100

PRED

ICTE

D L

OA

D =

100

MOVEMENT (mm)

NORMALIZED TO LOAD

Forthcoming Prediction Event in Bolivia April 2013

Four bored instrumented piles in sand tested in compression

0

5

2.9 m GW1.0 m

4.5 m

1.0 m

4.5 m

Groundsurface

TP1 TP2 TP3 TP4 "Std" FDP FDP "Std" +EB +O-cell +EB BH1 BH3 BH 4 BH2

0.0 m 400 mm 440 mm 400 mm 400 mm

72

5

10

15

20

25

DE

PTH

(m

)

1.2 m17.5 m 2.5 m

15.0 m

O-cell

EB EB

600 mm

5

7.5 m

10.5 m

13.5 m

16.5 m 15.8 m

4.5 m

7.5 m

10.5 m

13.5 m

Test Pile Configurations and Strain-Gage Levels

440 mm400 mm 600 mm

Page 32: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

13

0

2

4

6

8

10

0 10 20 30 40 50N (blows/0.3m)

PTH

(m

)

SPT1SPT2SPT3

0

2

4

6

8

10

0 5 10 15 20 25 30

WATER CONTENT (%)

TH (

m)

0

2

4

6

8

10

0 20 40 60 80 100

GRAIN SIZE (%)

TH (

m)

Fine to Medium Sand

Medium to Coarse SandFines

BH-1

Soil Profile

73

12

14

16

18

20

DEP

10

12

14

16

18

20

DEP

T 10

12

14

16

18

20

DEP

T Gravel

Zone of Clay and Clayey Sand (no samples)

Deadline for submitting a prediction is April 1I will be glad to email the details for how to submit one.

Pore Pressure Dissipation

0

5

10

0 100 200 300 400 500 600

PORE PRESSURE (KPa)

(m)

0

5

10

0 100 200 300 400 500 600

PORE PRESSURE (KPa)

(m)

0

5

10

0 100 200 300 400 500 600

PORE PRESSURE (KPa)

(m)

7474Paddle River, Alberta, Canada (Fellenius 2008)

15

20

25

DEP

TH

Before Driving

EOID

Total Stress

15

20

25

DEP

TH

30 Days after EOID 15 Days

after EOID

Before Driving

EOID

Total Stress

15

20

25

DEP

TH

4 Years after Driving

30 Days after EOID 15 Days

after EOID

Before Driving

EOID

Total Stress

800

1,000

1,200

1,400

1,600

D (

KN

)

Effective Stress Analysis

0

5

10

0 500 1,000 1,500 2,000

LOAD (KN)

(m)

4 Years after EOID

7575

0

200

400

600

0 10 20 30 40 50

MOVEMENT (mm)

LOA

Paddle River, Alberta, Canada

15

20

25

DEP

TH (

15 Days after EOID

30 Days after EOID

All three analyses apply the same coefficients coupled with the actual

pore pressure distribution

If we want to know the load distribution, we can measure it. But, what we measure is the increase of load in the pile due to the load applied to the pile head. What about the load in the pile that was there before

76

pwe started the test?

That is, the Residual load.

Normalized Applied Load

Load distributions in

static loading tests on

four instrumented

77

D E P T H

piles in clayS d

Example from Gregersen et al., 1973

0

2

4

6

8

0 50 100 150 200 250 300

LOAD (KN)

(m)

0

2

4

6

8

0 100 200 300 400 500 600

LOAD (KN)

(m) True

Residual

True minus Residual

78

B. Load and resistance in DA

for the ultimate load applied

Sand8

10

12

14

16

18

DE

PTH

(

Pile DA

Pile BC, Tapered

8

10

12

14

16

18

DE

PTH

(

A. Distribution of residual load in DA and BC

before start of the loading test

Page 33: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

14

FHWA tests on 0.9 m diameter bored pilesOne in sand and one in clay

(Baker et al., 1990 and Briaud et al., 2000)

0

2

4

0 10 20 30 40

Cone Stress and SPT N-Index(MPa and bl/0.3 m)

Silty Sand

0

2

4

0 10 20 30 40

Cone Stress (MPa)

ClaySilty

Sand Clay

79

6

8

10

12

DEPT

H (m

)

Sand

Pile 4

6

8

10

12

DEPT

H (m

)

Pile 7

N

qc Sand Clay

ANALYSIS RESULTS: Load-transfer curves

0.0

2.0

4.0

0 1,000 2,000 3,000 4,000 5,000

LOAD (KN)

m)

0.0

2.0

4.0

0 1,000 2,000 3,000 4,000 5,000

LOAD (KN)

)

True Distribution

0.0

2.0

4.0

0 1,000 2,000 3,000 4,000 5,000

LOAD (KN)

m)

Measured Distribution

0.0

2.0

4.0

0 1,000 2,000 3,000 4,000 5,000

LOAD (KN)

m)

True Distribution

Residual Load

80

6.0

8.0

10.0

12.0

DEP

TH (

m

PILE 4SAND

Measured Distribution6.0

8.0

10.0

12.0

DEP

TH (

m)

PILE 4SAND

Residual Load

Measured Distribution

6.0

8.0

10.0

12.0

DEP

TH (

m

PILE 7CLAY

6.0

8.0

10.0

12.0

DEP

TH (

m

PILE 7CLAY

Results of analysis of a Monotube pile in sand(Fellenius et al., 2000)

0

5

0 1,000 2,000 3,000

LOAD (KN)

Measured Resistance

Residual Load

81

10

15

20

25

DE

PTH

(m

)

True Resistance

Method for evaluating the residual load distribution

0

2

4

0 500 1,000 1,500 2,000

RESISTANCE (KN)

Measured Load

Shaft

82

6

8

10

12

14

16

DE

PTH

(m

)

Measured Shaft ResistanceDivided by 2

Residual Load

True Resistance

ExtrapolatedTrue Resistance

Resistance

0

5

10

15

20

0 500 1,000 1,500 2,000 2,500LOAD (KN)

(m)

Static Loading Testat Pend Oreille, Sandpoint, Idaho, for

the realignment of US95

406 m diameter,45 m long, closed-toe pipe pile

driven in soft clay

Determining True Resistancefrom Measured Resistance (“False Resistance”)

Cl

83

25

30

35

40

45

50

DEP

TH (

Fellenius et al. (2004)

driven in soft clay

200+ m

Clay

0

5

10

15

20

-500 0 500 1,000 1,500 2,000

LOAD (KN)

(m)

ß = 0.60

ß = 0.06

AS MEASURED,i.e. "FALSE RES."

A

ß = 0.09

0

5

10

15

20

-500 0 500 1,000 1,500 2,000

LOAD (KN)

(m)

ß = 0.60

ß = 0.09

ß = 0.09

AS MEASURED,i.e. "FALSE RES."

CPTu Eslami-Fellenius

B

84

Test on a strain-gage instrumented, 406 mm diameter,45 m long pile driven in soft clay in Sandpoint, Idaho

25

30

35

40

45

50

DE

PTH

ß = 0.06

"TRUE RES." RESIDUAL LOAD

AFTER 1st UNLOADING

25

30

35

40

45

50

DE

PTH

ß = 0.10

"TRUE RES." per CPTu

RESIDUAL LOAD

AFTER 1st UNLOADING

ß = 0.10

Extrapolated

Page 34: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

15

0

5

10

15

0 500 1,000 1,500 2,000 2,500 3,000 3,500

LOAD (KN)

PTH

(m

)

True Resistance

HEAD-DOWN AND FULL RESIDUAL LOAD

Residual Load

True Resistance

False Resistance

Silty Sand

Silty Clay

0

5

10

15

0 500 1,000 1,500 2,000 2,500 3,000 3,500

LOAD (KN)

PTH

(m

)

HEAD-DOWN AND PARTIAL RESIDUAL LOAD

True

False Resistance

Shaft Resistance

Typical Example: Table 7.3 in the Red Book

85

20

25

30

35

DE

P Resistance

Residual and TrueToe Resistance

Transition Zone

Silty Sand

Glacial Till

20

25

30

35

DEP

Residual Load

Resistance

Residual and TrueToe Resistance

Transition Zone

Resistance

The effect of residual load on an uplift test

0

5

10

-2,000 -1,500 -1,000 -500 0 500 1,000

LOAD (KN)

m)

True Resistance

TENSION TESTAND FULL RESIDUAL LOAD

Residual Load

0

5

10

-2,000 -1,500 -1,000 -500 0 500 1,000

LOAD (KN)

m)

Residual Load

True Resistance

TENSION TESTAND PARTIAL RESIDUAL LOAD

8686

15

20

25

30

35

DE

PTH

(m

False Resistance

Toe Resistancein an Uplift Test?!

15

20

25

30

35

DEP

TH (

m

False Resistance

Toe Resistancein an Uplift Test?

Combining the results of a head-down test with those of a tensions test will help determining the true resistance

0

5

10

15

0 500 1,000 1,500 2,000 2,500 3,000 3,500

LOAD (KN)

H (

m)

HEAD-DOWN AND PARTIAL RESIDUAL LOAD

FalseHead-down

True Shaft

False TensionTest

8787

20

25

30

35

DEP

TH

Residual Load

True Resistance

Residual and TrueToe Resistance

Transition Zone

True Shaft Resistance

Not directly useful below this level

Now you know why some claim that resistance in tension is smaller than that in compression

400

600

800

1,000

LOA

D (

KN

)

No Residual Load

Residual Load present

No Strain Softening

Presence of residual load is not just of academic interest

400

600

800

1,000

LOA

D (

KN

)

With Strain Softening

Residual Load present

No Residual Load

8888

0

200

400

0 5 10 15 20 25 30

MOVEMENT (mm)

L

OFFSET LIMIT LOAD

0

200

400

0 5 10 15 20 25 30

MOVEMENT (mm)

L

OFFSET LIMIT LOAD

• "Residual Load " follows the same principle and mechanism as "Drag Load". The distinction made is that by residual load we mean the locked-in load present in the pile immediately before we start a static loading test. By drag load we mean the load present in the pile in the long-term.

Additional Comments on Residual load

8989

• Residual load as well as drag load can develop in coarse-grained soil just as it does in clay soil.

• Both residual load and drag load develop at very small movements between the pile and the

soil.

600

800

1,000

1,200

D (

KN

)

HEADTOE TELLTALE

A

Does not this shape of

Residual Load Affects Toe Resistance Response

9090

0

200

400

600

0 5 10 15 20 25

MOVEMENT (mm)

LOAD TOE

Does not this shape of measured toe movement

suggest that there is a distinct toe capacity?

Page 35: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

16

400

600

800

1,000

1,200

LOAD

(K

N)

HEAD

TOE

TOE TELLTALEA

400

600

800

1,000

1,200

LOAD

(K

N)

HEAD

TOE

B

9191

0

200

0 5 10 15 20 25

MOVEMENT (mm)

0

200

0 5 10 15 20 25

MOVEMENT (mm)"Virgin" Toe Curve

No, it only appears that way when we forget to consider the residual toe load (also called the initial, or “virgin” toe movement)

Miscellaneous DetailsOpen vs. Closed Toe

Tapered sectionH section

9292

H-section. . . . . . .

Special Conditions

Step-tapered pile

9393

"Add-on" toe resistance acting on a donut-shaped area

Special Conditions

Step-tapered pileSmooth-tapered pile

Conical pile (wood pile)

Calculate in elements

(increments) at t

9494

"Add-on" toe resistance acting on a donut-shaped area

every metre or so the shaft resistance acting along the pile and toe resistance for the “donut” of

each element

Just because the design assumes that the pile shaft issmooth and straight with parallel sides does not mean it is.

9595

A A

B B

A-A and B-B

The "donut" area A minus B projection acting like an extra Pile Toe

An unintentional effect for many bored piles and intentional for “multi-underreamed” piles

9696

Page 36: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

17

9797 9898

PILES FOR AN EXPANSION OF A LOADING DOCK

9999

CALCULATION OF PILE CAPACITY and

LOAD-TRANSFER CURVES

355 mm diameter closed-toe pipe pile to 32 m embedment

Area, As = 1.115 m2/m Live Load, Ql = 200 KN

Area, At = 0.099 m2 Dead Load, Qd = 800 KN

SILT

CLAY

4 m

W

5 m

100100

, t , d

LAYER 1 Sandy Silt ρ = 2,000 kg/m β = 0.40

LAYER 2 Soft Clay ρ = 1,700 kg/m3 β = 0.30

LAYER 3 Silty sand ρ = 2,100 kg/m3 β = 0.50With artesian head of 5 m

LAYER 4 Ablation Till ρ = 2,200 kg/m3 β = 0.55Nt = 50 TILL

SAND

27 m

21 m

32 m

CALCULATION OF LOAD TRANSFERArea, As = 1.115 m2/m Live Load, Ql = 200 KN Shaft Resistance, Rs = 1,817 KNArea, At = 0.099 m2 Dead Load, Qd = 800 KN Toe Resistance, Rt = 1,205 KN

Total Load, Qa = 1,000 KN Total Resistance, Ru = 3,021 KNF.S. = 3.02 Depth to N. P. = 26.51 m Load at N. P., Qmax = 1,911 KN

DEPTH TOTAL PORE EFFECTIVE INCR. Qd+Qn Qu-RsSTRESS PRES. STRESS Rs

(m) (KPa) (KPa) (KPa) (KN) (KN) (KN)

LAYER 1 Sandy Silt ρ = 2,000 kg/m3 β = 0.400.00 30.00 0.00 30.00 0.0 800 3,0211.00(GWT) 48.40 0.00 48.40 17.5 817 3,0044.00 104.30 30.00 74.30 82.1 900 2,922

LAYER 2 Soft Clay ρ = 1,700 kg/m3 β = 0.304.00 104.30 30.00 74.30 900 2,9226.00 136.04 57.06 78.98 26.0 951 2,8708.00 168.08 84.12 83.96 27.7 1,005 2,816

10 00 200 37 111 18 89 20 29 4 1 063 2 758

101101

10.00 200.37 111.18 89.20 29.4 1,063 2,75812.00 232.88 138.24 94.64 31.2 1,125 2,69714.00 265.55 165.29 100.26 33.1 1,190 2,63116.00 298.38 192.35 106.03 35.0 1,259 2,56218.00 331.33 219.41 111.92 37.0 1,332 2,48920.00 364.40 246.47 117.93 39.0 1,409 2,41321.00 380.97 260.00 120.97 40.0 1,449 2,373

LAYER 3 Silty sand = 2,100 kg/m3 β = 0.5021.00 380.97 260.00 120.97 1,449 2,37323.00 422.17 280.00 142.17 76.3 1,596 2,22625.00 463.45 300.00 163.45 88.2 1,766 2,05527.00 504.80 320.00 184.80 100.1 1,960 1,861

LAYER 4 Ablation Till = 2,200 kg/m3 β = 0.5527.00 504.80 320.00 184.80 1,960 1,86130.00 569.93 350.00 219.93 372.4 2,332 1,48932.00 613.41 370.00 243.41 285.1 2,617 1,205 for Nt = 50

0

5

10

0 1,000 2,000 3,000 4,000

LOAD and RESISTANCE (KN)

Qd + qn

Qd

QallowQlive Qu

Plot of the Calculated Values

zs cr '' βσ+=

Dztt Nr == 'σ

Calculation of shaft and toe resistance per the

effective stress method

102102

15

20

25

30

35

DEP

TH (

m)

Qu - rs

Rt

dzcAdzrAR zssss )''( βσ+∫=∫=

Dzttttt NArAR === 'σ

Mother Nature no like no kinkie stuff

Page 37: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

18

0

5

10

15

0 1,000 2,000 3,000 4,000

LOAD and RESISTANCE (KN)

H (

m)

103103

20

25

30

35

DEP

TH

Transition Zone

Qn

Note, just because we carried the static loading test to acertain toe movement does not mean that Nature willimpose the same toe load and toe movement for thelong-term condition.

0

5

10

0 500 1000 1500 2000

LOADQult/ RultQdead

0

5

10

0 500 1000 1500 2000

LOADQult/ RultQdead

104104

A) Small settlement only in the surrounding soils B) Large settlement in the surrounding soils

15

20

25

DEP

TH

Rs

Qn

(Rt)

15

20

25

DEP

TH

(Rt) Rs

Qn

RESIDUAL LOAD

0

5

0 500 1000 1500 2000

LOADQult/ Rult

A test pile.

Before the start of the test there is no

105105

10

15

20

25

DEP

TH

Residual Toe Load

load on the pile head

A Case history of evaluation of static and dynamic tests on a 300 mm, 12 m long pile driven in sand. Data from Axelsson (2000).

GW

Silty CLAY

SAND with lenses of clay and silty clay

Uniform SAND (80% sand size)

with occasional

9.25"235 mm

0 m

2.5

m

T E S T S

Static loading test 5 days after driving at Depth 12.8 m

Restrike after static test to final depth 13.0 m with PDA/CAPWAP

106106

with occasional lens of Silty CLAY13

.0

Redrive to 13.0 m depth

Static loading test 1 day after redrive

Static loading test 8 days after redrive

Static loading test 120 days (4 months) after redrive

Static loading test 670 days (22 months) after redrive

Total unit weight 0 m - 2.5 m = 18 KN/m3

Total unit weight 2.5 m - 13.0 m = 19 KN/m3

Hydrostatic pore pressure distribution

cnt.

107107

0123

0.00 0.20 0.40 0.60 0.80 1.00

Equivalent ß (- - -)

0123

0 25 50 75 100

Unit Shaft Resistance (KPa)

0123

0 25 50 75 100

Unit Shaft Resistance (KPa)

ß-Method E-F Method

Equivalent ß-coefficient from CPTU sounding and Eslami-Fellenius Method

Unit Shaft Resistance from Equivalent ß-coefficient and CPTU Method plus LCPC-Method

cnt.

108108

456789

10111213

DEP

TH (

m)

E-F Method

456789

10111213

DEP

TH (

m) 4

56789

10111213

DEP

TH (

m)

LCPC Method

Page 38: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

19

250

300

350

400

450

500

(KN

)

Static test 8 days after driving

PDA/CAPWAP after static test

Load-movement curves from a static loading test andthe CAPWAP-determined load-movement curve from asubsequent same-day dynamic test.

cnt.

109109

0

50

100

150

200

250

0 5 10 15 20 25 30 35 40 45 50

MOVEMENT (mm)

LOAD

Load-Movement Curves for static tests after the redrive

cnt.

250

300

350

400

450

500

OAD

(KN

)

1 Day

8 Days

4 Months

4 Months(Reloading)22 Months

110

0

50

100

150

200

0 10 20 30 40 50 60 70

MOVEMENT (mm)

LO

An obvious example of set-up in sand — Right?

300

350

400

450

500

KN)

1 Day

8 Days

cnt.

When plotting the data in sequence as the testsprogressed from unloadings to reloadings, notime-dependent increase can be discerned.

111

0

50

100

150

200

250

0 25 50 75 100 125 150 175 200

MOVEMENT (mm)

LOAD

(K 8 Days

4 Months

4 Months(Reloading)

22 Months

100

150

200

OE

LOA

D (

KN

)

1 Day

8 Days

4 Months

22 Months

Toe load from earth stress cell at pile toe

cnt.

112

0

50

0 50 100 150

MOVEMENT OF PILE HEAD (mm)

TO

This indicates an ultimate toe resistance, i.e., no increase of toe resistance for increasing toe movement — Right?

Toe load from earth stress cell at pile toe

cnt.

100

150

200

INC

REA

SE

(KN

)

1 Day8 Days4 Months22 Months

113

Residual Toe Load

The entire history of the toe response needs to be considered. A plot of entire history does not show an ultimate value. Residual load can be determined from instrumented tests.

0

50

0 25 50 75 100 125 150MOVEMENT (mm)

LOA

D

Redundancy is nothing to look down on

114

Page 39: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

1

BASICS OF DESIGN OF PILED

FOUNDATIONS

B t H F ll iBengt H. Fellenius

The Static Loading TestPerformance, Instrumentation, Interpretation

Bolivia, April 25, 2013

33

Candidates for Darwin Award, First Class

44

! ! !Testing piles is a risky business.

55

! ! ! 2 SPACER

1. SWIVEL PLATE

What do you think could happen to the stack of four pieces on the pile head when

66

4. JACK

3. LOAD CELL

2. SPACER the load is applied? And, therefore, to the three oblivious persons next to the pile?

Page 40: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

2

77This is how experience taught the three, and others, to arrange the units on the pile head 88

99 1010

1111 12

Page 41: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

3

1313 14

Fellenius 1984

250

300

350

d (K

N)

Head-down O-cell Pile

August 2006

The error can be small or it can be large. Here are resultsfrom two tests at the same site using the same equipmenttesting two adjacent piles, one after the other.

1,500

2,000

) 15% Error

Shinho-Pile August 2006

15

0

50

100

150

200

0 2,000 4,000 6,000 8,000 10,000Loadcell (KN)

Erro

r in

Jack

Loa

d

2.5% Error

0

500

1,000

0 5,000 10,000 15,000Loadcell load (KN)

Erro

r (K

N)

2.5% Error

Note, the test on the pile called "O-cell pile" is a head-down test after a preceding O-cell test.

A routine static loading test provides the load-movement of the pile head...

and the pile capacity?

16

The Offset Limit MethodDavisson (1972)

LLEAQ Δ=

Q

17

OFFSET (inches) = 0.15 + b/120

OFFSET (SI-units—mm) = 4 + b/120

b = pile diameter (inch or mm)

The Decourt ExtrapolationDecourt (1999)

1,000,000

1,500,000

2,000,000

-- Q

/s (

inch

/kip

s)

1

2

CC

Qu =C1 = Slope

C2 = Y-intercept

δQ

18

0 100 200 300 400 5000

500,000

, ,

LOAD (kips)

LOAD

/MVM

NT

-

Ult.Res = 474 k ips

Linear Regression Line

Q

Page 42: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

4

Other methods are:

The Load at Maximum Curvature

Mazurkiewicz Extrapolation

Chin-Kondner Extrapolation

19

DeBeer double-log intersection

Fuller-Hoy Curve Slope

The Creep Method

Yield limit in a cyclic test

For details, see Fellenius (1975, 1980)

DECOURT 235

20

1,500

2,000

2,500

N)

Definition of capacity (ultimate resistance) is only needed when the actual value is not obvious from the load-

movement curve

21

0

500

1,000

0 5 10 15 20 25 30 35 40

MOVEMENT (mm)

LOAD

(KN

Offset-LimitLine

The capacity is not a constant, but changes with time

1,500

2,000

2,500

3,000A

CIT

Y (

KN

)8 years

BOR

16 h BOR

48 days Static Test

CASE 14 years20 m

22

0

500

1,000

0.01 0.10 1.00 10.00 100.00 1,000.00 10,000.00

DAYS AFTER EOID

CA

PA

1 h BOREOIDs CASE 2

16 m

Pile Toe Movement

3,000

4,000

AD

(K

N) HEAD

HEAD LOAD vs. TOE MOVEMENT 65 ft long, 14 inch pipe pile.

With a telltale to the toe arranged to

23

0 5 10 15 20 25 300

1,000

2,000

MOVEMENT (mm)

LOA

D A

T P

ILE

HE

A

determine pileshortening. Don’t arrange it to measure toe movement directly.

Analysis of toe resistance

An adjacent pull test on a similar pile established that the pile shaft resistance (2,000 KN) was approximately fully

3,000

4,000

D (

KN

)

HEAD

HEAD LOAD vs. TOE MOVEMENT

PILE SHORTENING

24

was approximately fully mobilized just short of a 5-mm upward movement at the pile toe. Therefore the load applied in the push test beyond a toe movement of 5 mm goes to toe resistance, only.0 5 10 15 20 25 30

0

1,000

2,000

MOVEMENT (mm)

LOA

D A

T P

ILE

HE

AD

ESTIMATED T OE LOAD vs.

TOE MOVEMENT(Based on the assumption thatshaf t resistance is 2,000 KN)

+10 %

-10 %

Page 43: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

5

20 inch square diameter, prestressed concrete pile driven to 58 ft embedment, through about 45 ft of soft silt and clay, 5

ft of sand, and to bearing 6 ft into hard clay

PUSH and

PULLTo separate

f

Unloading-reloading once or a couple of times “on the way up”

400

500

600

)

Push test

Offset LimitTOEHEAD

25Data from AATech Scientific Inc.

shaft and toe resistances. The pile is

equipped with a toe telltale.

y pserves no purpose and may result in distorted analysis results

0

100

200

300

0.0 0.2 0.4 0.6 0.8 1.0 1.2

MOVEMENT (in)

LOA

D (

kips

Pull test

Combining the push and pull test results with the telltale measurements to determine the load-movement for the pile toe

400

500

600

ps)

PUSH TEST

TOE

"Toe Telltale "

26Data from AATech Scientific Inc.

0

100

200

300

0.0 0.2 0.4 0.6 0.8 1.0 1.2

MOVEMENT (in)

LOA

D (

ki

PULL TESTSHAFT

From pull test with the head movement adjusted to the toe movement

Instrumentation

a d

27

and

Interpretation

T e l l t a l e s• A telltale measures shortening of a pile and must never be arranged to

measure movement.• Let toe movement be the pile head movement minus the pile shortening.• For a single telltale, the shortening divided by the distance between

the pile head and the telltale toe is the average strain over that length.• For two telltales, the distance to use is that between the telltale tips.

28

, p• The strain times the cross section area of the pile times the pile material

E-modulus is the average load in the pile.

• To plot a load distribution, where should the load value be plotted? Midway of the length or above or below?

Load distribution for constant unit shaft resistance

00 100 LOAD, Q

A1

Average Load 0

PILE HEAD

29

50

100h A2

MidheightLoad

Distribution Q = az

DEPTH, zPILE TOE

ars =

21 AA =

Linearly increasing unit shaft resistanceand its load distribution

00 Unit Shaft

Resistance

az 31

3axA =

)23( 323 xhxha +

00 Average

LoadLOAD, Q0

A1x

30

h DEPTH, z

21 AA =

hhX 58.03==“X” is where the average load should be plotted

6)23(2 xhxhaA +−

=

A2

LoadDistribution

Q = az2/2 h

Page 44: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

6

• Today, telltales are not used for determining strain (load) in a pile because using strain gages is a more assured, more accurate, and cheaper means of instrumentation.

• However, it is good policy to include a toe-telltale to measure toe movement. If arranged to measure shortening of the pile, it can also be used as an approximate back-up for the average load in the pile.

Th f ib ti i t i ( ti l t i l

31

• The use of vibrating-wire strain gages (sometimes, electrical resistance gages) is a well-established, accurate, and reliable means for determining loads imposed in the test pile.

• It is very unwise to cut corners by field-attaching single strain gages to the re-bar cage. Always install factory assembled “sister bar” gages.

32

Rebar Strain Meter — “Sister Bar”

Instrument Cable

Three bars?!

Reinforcing Rebaror Strand

Instrument Cables

33

Reinforcing Rebar

Rebar Strain Meter

Wire Tie

or Strand

Tied to Reinforcing Rebar

Hayes 2002

Wire Tie

Tied to Reinforcing Rings

(2 places)

Rebar Strain Meter(3 places, 120° apart)

8

10

12

14

16

18

20

LOA

D (

MN

)Load-strain of individual gages and of averages

4

6

8

10

12

14

16

18

LOA

D (

MN

)

LEVEL 1 D CA B

A&C B&D

34

0

2

4

6

0 50 100 150 200STRAIN (µε)

Level 1A+1C

Level 1B+1D

Level 1 avg 0

2

4

0 100 200 300 400 500 600 700

STRAIN (µε)

The curves are well together and no bending is discernable

Both pair of curves indicate bending; averages are very close; essentially the same for the two pairs

If one gage “dies”, the data of surviving single gage should be discarded. It must not be combined with the data of another intact pair.Data from two surviving single gages must not be combined.

12

14

16

18

20

N)

A&C+D

Means: A&C, B&D, AND A&B&C&D

A&C+BB+CA+D

LEVEL 1

35

0

2

4

6

8

10

0 100 200 300 400 500 600 700

STRAIN (µε)

LOA

D (

MN

Error when including the single third gage, when either Gage B or Gage D data are discarded due to damage.

Glostrext Retrievable Extensometer (Geokon 1300 & A9)

36

Lee Sieng Kai, 2010. Recent development in pile instrumentationtechnology for driven, jacked-in and bored cast-in-place piles.Lecture notes. [www.glostrext.com.my]

Anchor arrangement display Anchors installed

Page 45: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

7

Gage for measuring displacement, i.e., distance change between upper and lower extensometers. Accuracy is about 0.02mm/5m

37

corresponding to about 5 µε.

That the shape of a pile sometimes can be quite different from the straight-sided cylinder can be noticed in a retaining wall built as a pile-in-pile wall

38

0

5

10

0.00 0.50 1.00 1.50 2.00 2.50

DIAMETER RATIO AND AREA RATIO

(m)

Nominal Ratio

Determining actual shape of the bored hole before concreting

39

15

20

25

DEP

TH

Gage Depth

DiameterRatio

Area Ratio

O-cell

Page 46: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

1

We have got the strain.How do we get the load?

• Load is stress times area

1

• Stress is Modulus (E) times strain

• The modulus is the key

εσ E=

For a concrete pile or a concrete-filled bored pile, the modulus to use is the combined modulus of concrete,

reinforcement, and steel casing

cs

ccsscomb AA

AEAEE

++

=

2

Ecomb = combined modulus Es = modulus for steelAs = area of steelEc = modulus for concreteAc = area of concrete

• The modulus of steel is 200 GPa (207 GPa for those weak at heart)

• The modulus of concrete is. . . . ?

Hard to answer. There is a sort of relation to the cylinder strength and the modulus usually appears as a value around 30 GPa, or perhaps 20 GPa or so, perhaps more.

This is not good enough answer but being vague is not necessary.

The modulus can be determined from the strain measurements.

3

Calculate first the change of strain for a change of load and plot the values against the strain.

Values are knownεσΔΔ

=tE

50

60

70

80

90

100

DU

LUS

(G

Pa)

Level 1

Level 2

Level 3

Level 4

Level 5

Example of “Tangent Modulus Plot”

4

0 200 400 600 8000

10

20

30

40

50

MICROSTRAIN

TAN

GE

NT

MO

Best Fit Line

baddEt +=⎟

⎠⎞

⎜⎝⎛= ε

εσ

εεσ ba+⎟

⎞⎜⎛= 2

Which can be integrated to:

B t stress is also a f nction of

In the stress range of the static loading test, modulus of concrete is not constant, but a more or less linear relation to the strain

5

εεσ b+⎟⎠

⎜⎝

=2

εσ sE=

But stress is also a function of secant modulus and strain:

Combined, we get a useful relation:

baEs += ε5.0 and Q = A Es ε

50

60

70

80

90

100

DU

LUS

(G

Pa)

Level 1

Level 2

Level 3

Level 4

Level 5

Example of “Tangent Modulus Plot”

6

0 200 400 600 8000

10

20

30

40

50

MICROSTRAIN

TAN

GE

NT

MO

Best Fit Line

Intercept is

”b”

Slope is “a”

Page 47: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

2

Note, just because a strain-gage has registered some strain values during a test does not guarantee that the data are useful. Strains unrelated to force can develop due to variations in the pile material and temperature and amount to as much as about 50±microstrain. Therefore, the test must be designed to achieve strains due to imposed force of ideally about 500 microstrain and

7

beyond. If the imposed strains are smaller, the relative errors and imprecision will be large, and interpretation of the test data becomes uncertain, causing the investment in instrumentation to be less than meaningful. The test should engage the pile material up to at least half the strength. Preferably, aim for reaching close to the strength.

Unlike steel, the modulus of concrete varies and depends on curing, proportioning,mineral, etc. and it is strain dependent. However, the cross sectional area of steel in aninstrumented steel pile is sometimes not that well known.

y = -0.0013x + 46.79145

50

55

60

STIF

FNES

S, E

A (

GN

)

45

50

55

60

STIF

FNES

S, E

A (

GN

)

EAsecant (GN) = 46.5 from tangent stiffnessEAsecant (GN) = 46.8 - 0.001µε from secant stiffness

8

30

35

40

0 100 200 300 400 500 600

STRAIN, με

SEC

AN

T S

30

35

40

0 100 200 300 400 500 600

STRAIN, με

TAN

GEN

T

y = 0.000x + 46.451

TANGENT STIFFNESS, EA = ∆Q/∆εSECANT STIFFNESS, EA = Q/ε

(Data from Bradshaw et al. 2012)

Pile stiffness for a 1.83 m diameter steel pile: open-toe pipe pile. Strain-gage pair placed 1.8 m below the pile head.

Field Testing and Foundation Report, Interstate H-1, Keehi Interchange, Hawaii, Project I-H1-1(85), PBHA 1979.

4

5

Q/∆ε

(G

N)

TANGENT STIFFNESS, ∆Q/∆ε

4

5

ε (

GN

)

SECANT STIFFNESS, Q/ε

Strain-gage instrumented, 16.5-inch octagonal prestressedconcrete pile driven to 60 m depth through coral clay andsand. Modulus relations as obtained from uppermost gage(1.5 m below head, i.e., 3.6b).

9Data from PBHA 1979

y = -0.0014x + 4.082

0

1

2

3

0 500 1,000 1,500 2,000

STRAIN (µε)

TAN

GEN

T S

TIFF

NE

SS, ∆Q

y = -0.0007x + 4.0553

0

1

2

3

0 500 1,000 1,500 2,000

STRAIN (µε)

SEC

AN

T S

TIFF

NES

S, Q

Secant DataSecant from Tangent DataTrend Line

10

15

TIFF

NES

S, E

A (

GN

)

10

15

STIF

FNES

S, E

A (

GN

)

y = -0.003x + 7.41

TANGENT STIFFNESS, EA = ∆Q/∆εSECANT STIFFNESS, EA = Q/ε

For the "calibrating" uppermost gage level, the secantmethod appears to be the better one to use, right?

10

Pile stiffness for a 600 mm diameter concreted pipepile. The gage level was 1.6 m (3.2b) below pile head

Data from Fellenius et al. 2003

0

5

0 50 100 150 200 250 300

STRAIN, µε

SEC

AN

T S

T

0

5

0 50 100 150 200 250 300

STRAIN, µε

TAN

GEN

T S

y = -0.004x + 7.21

EAsecant (GN) = 7.2 - 0.002µε from tangent stiffnessEAsecant (GN) = 7.4 - 0.003µε from secant stiffness

y = -0.0053x + 11.231

20

30

40

50

NT

STI

FFN

ESS,

EA

(G

N)

20

30

40

50

ENT

STI

FFN

ESS

, EA

(G

N)

EAsecant (GN) = 10.0 - 0.003µε from tangent stiffnessEAsecant (GN) = 11.2 - 0.005µε from secant stiffness

TANGENT STIFFNESS, EA = ∆Q/∆εSECANT STIFFNESS, EA = ∆Q/∆ε

Or this case? Here, that initial "hyperbolic" trend canbe removed by adding a mere 20 µε to the strain data,"correcting the zero" reading, it seems.

11

0

10

0 100 200 300 400 500

STRAIN (µε)

SEC

AN

y = -0.0055x + 9.9950

10

0 100 200 300 400 500

STRAIN (µε)

TAN

GE

Secant stiffness after adding 20µε to each strain value

Secant stiffness from tangent stiffness

Pile stiffness for a 600-mm diameter prestressed pile.The gage level was 1.5 m (2.5b) below pile the head.

Data from CH2M Hill 1995

Or the adding of a mere8 µε for this case?

40

50

S, E

A (

GN

)

40

50

SS, E

A (

GN

)

Secant for Virgin Loading

Trend Line from Tangent Stiffness

TANGENT STIFFNESS, EA = ∆Q/∆εSECANT STIFFNESS, EA = ∆Q/∆ε

0

2,000

4,000

6,000

8,000

10,000

12,000

14,000

0 1 2 3 4 5 6MOVEMENT (mm)

LOA

D (

KN

)

12

y = -0.008x + 30.295

10

20

30

0 100 200 300 400 500STRAIN (με)

SEC

AN

T S

TIFF

NES

y = -0.0115x + 29.234

10

20

30

0 100 200 300 400 500

STRAIN (με)

TAN

GE

NT

STI

FFN

ES

EAsecant (GN) = 29.2 - 0.006µε from tangent stiffness

EAsecant (GN) = 30.2 - 0.008µε from secant stiffness

gRelation

Secant Stiffness after adding 8µε to each strain value

Pile stiffness for a 900-mm bored pile constructed in Indonesia. The gage level was 2.0 m (2.2b) below pile the head.

Page 48: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

3

After completion of the test, the pilewas reloaded. Below, the 2nd cycle datahave been added to the first cycle plot.

0

2,000

4,000

6,000

8,000

10,000

12,000

14,000

0 1 2 3 4 5 6MOVEMENT (mm)

LOA

D (

KN

)

40

50

SS, E

A (

GN

)

40

50

ESS,

EA

(G

N)

Secant for Reloading(1st cycle strains removed)

TANGENT STIFFNESS, EA = ∆Q/∆εSECANT STIFFNESS, EA = ∆Q/∆ε

13Data from Geo Optima Pt. 2011

10

20

30

0 100 200 300 400 500STRAIN (με)

SEC

AN

T S

TIFF

NE

S

10

20

30

0 100 200 300 400 500STRAIN (με)

TAN

GE

NT

STI

FFN

E

Secant for Reloading

Tangent for Reloading

Illustration of the adverse effect of unloading/reloading.

What really do we learn fromunloading/reloading and what

14

unloading/reloading and whatdoes unloading/reloading do tothe gage records?

The Testing Schedule

150

200

250

300

ERC

EN

T"

A much superior test schedule. It presents a large number of values (≈20 increments), has no destructive unloading/reload cycles, and has constant load-hold duration. Such tests can be used in analysis for load distribution and settlement and will provide value to a project, as opposed to the long-duration, unloading/reloading, variable load-hold duration, which is a next to useless test.

Plan for 200 %, but make use of the opportunity to go higher if this becomes feasible

0

50

100

0 6 12 18 24 30 36 42 48 54 60 66 72

TIME (hours)

"PE

The schedule in blue is typical for many standards. However, it is costly, time-consuming,and, most important, it is diminishes or eliminates reliable analysis of the test results.

XXXXX

What about keeping the load on the pile until "zero" movement?

(Long-duration load-holding)

30

40

50

60

D (

MN

)

Pile TP-1 Pile TP 1

30

40

50

60

(MN

)

16

0

10

20

30

0 5 10 15 20 25 30

DAYS

LOA

D

Lakhta Center, St Petersburg, Russia2.0 m diameter, 84 m long, bored pile

0

10

20

30

0 20 40 60 80 100

MOVEMENT (mm)

LOA

D

Pile TP 1

0

10

20

30

40

50

0 50 100 150 200 250 300

TIME (hours)

MO

VEM

ENT

(mm

)

2L-13

2L-112L-10

2L-12

2L-14

Pile TP 1

0

5

10

15

20

25

30

35

0 5,000 10,000 15,000 20,000

TIME (minutes)

LOA

D B

ETEE

N G

Ls (

MN

)

GL6 to GL7 GL5 to GL6 GL5 to GL7

2L-142L-13

2L-122L-11

2L-142L-132L-12

2L-10

2L-122L-112L-10

2L-14

2L-10

2L-11

2L-13

17

Lakhta Center, St Petersburg, Russia2.0 m diameter, 84 m long, bored pile

The long-duration load-holding and variations of load increments have obviously hadconsiderable costs consequence for the project. Yet, nothing was "bought" by thosecosts. On the contrary, the uneven load-holding durations and the differing load incrementmagnitudes messed up the data and reduced the usefulness of the detailed analysis ofthe test records.

( ) TIME (minutes)

The occasional unloading/reloading and varying load-holding durationsprovide no information of any value for assessing pile response to load. Itis nothing but a vestigial practice, i.e., remnant of old, now obsolete, partof the practice, much like our tailbone.

Figuratively speaking, it is strange that so many still appear to believe thatthey have a tail at their rear end to wag despite the fact that the vestigial

On unloading/reloading

18

they have a tail at their rear end to wag, despite the fact that the vestigialtailbone is not connected to the head. Indeed, to schedule a test toinclude unloading/reloading and varying load-holds duration is nothing butakin to a insisting on that there is a tail to wag, disregarding all evidenceto the contrary. Those who argue for the wag seem to be too busycontemplating their navel to realize that nothing useful happens.

Page 49: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

4

The strain-gage measurement is supposed to be the change of strain due to the applied load relative the “no-load” situation (i.e., when no external load acts t th l ti )

Determining load from strain-gage measurements in the pile

1919

But, is the “no-load” situation really the reading taken at the beginning of the test? What is the true “zero-reading” to use?

at the gage location).

• We often assume – somewhat optimistically or naively – that the reading before the start of the test represents the “no-load” condition.

• However, at the time of the start of the loading test, loads do exist in the pile and they are often large.

• For a grouted pipe pile or a concrete cylinder pile,

2020

these loads are to a part the effect of the temperature generated during the curing of the grout.

• Then, the re-consolidation (set-up) of the soil after the driving or construction of the pile will impose additional loads on the pile.

Concrete hydration temperature measured in a grouted concrete cylinder pile

40

50

60

70

RA

TUR

E (°

C)

Temperature at various depths in the grout of a 0.4 m center hole in a 56 m long, 0.6 m diameter, cylinder pile.

2121

0

10

20

30

0 24 48 72 96 120 144 168 192 216 240

HOURS AFTER GROUTING

TEM

PER

Pusan Case

20

30

40

50

60

70

TEM

PER

ATU

RE

(°C

)

Start of Static Loading Test

Temperatures measured in a 74.5 m long, 2.6 m diameter bored pile

20

30

40

50

60

70

TEM

PER

ATU

RE

(°C

)

Temperatures measured in a 74.5 m long, 2.6 m diameter bored pile

2222

100 5 10 15 20 25 30 35

DAY AFTER GROUTING

100 1 2 3 4 5

DAY AFTER GROUTING

Temperature records during curing of grout in the Golden Ears Bridge test pile, Vancouver, BC. Data courtesy of Trow Engineering Inc. and Amec Inc.

-200

-100

0

100

NG

E O

F ST

RA

IN (

µε) Change of strain measured in a 74.5 m

long, 2.6 m diameter bored pile

2323

-400

-300

0 5 10 15 20 25 30 35

DAY AFTER GROUTING

CH

AN

Rebar ShorteningSlight Recovery of Shortening

Change of strain during the hydration of the grout in the Golden Ears Bridge test pile

The strain gages themselves are not are temperature sensitive, but the records may be!

The vibrating wire and the rebar have almost the same temperaturecoefficient. However, the coefficients of steel and concrete are slightlydifferent. This will influence the strains during the cooling of the grout.

2424

g g gMore important, the rise of temperature in the grout could affect the zeroreading of the wire and its strain calibration. It is necessary to “heat-cycle” (anneal) the gage before calibration. (A routine measure ofGeokon, US manufacturer of vibrating wire gages).

Page 50: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

5

0

5

10

15

20

25

-300 -200 -100 0 100 200 300 400

STRAIN (µε)

m)

Zero Reading. Does it mean

l d?

Immediately before the test, all gages must be checked and "Zero Readings" must be taken.

2525

25

30

35

40

45

50

55

60

DEP

TH (

m

Shinho Pile

zero load?

Answer to the question in the graph:

No, there's always residual load in a test pile.

0

5

10

15

20

25

-300 -200 -100 0 100 200 300 400

STRAIN (µε)

H (

m)

9d

15d

23d

30d

39d

49d

Strain measured during the 218-day wait-period between driving (grouting) and testing.

Do these strains really represent

2626

30

35

40

45

50

55

60

DEP

TH

59d

82d

99d

122d

218d Day ofTest

At an E- modulus of 30 GPa, this strain change corresponds to a load change of 3,200 KN

really represent load in the pile, as present before the start of the static loading test?

• Readings should be taken immediately before (and after) every event of the piling work and not just during the actual loading test

• The No-Load Readings will tell what happened to the gage before the start of the test and will be helpful in assessing the possibility of a shift in the reading value representing the no load condition

2727

reading value representing the no-load condition

• If the importance of the No-Load Readings is recognized, and if those readings are reviewed and evaluated, then, we are ready to consider the actual readings during the test

Of course,

we must consider also other aspects:

2828

Also the best field work can get messed up if the analysis and

conclusion effort loses sight of the history of the data

1,000

1,500

2,000

D (

KN) STATIC TEST

DYNAMIC TEST

1,000

1,500

2,000

D (

KN)

DYNAMIC TEST

1,000

1,500

2,000

D (

KN)

DYNAMIC TEST in a series of blows

Repeated STATIC TEST

2929The dynamic test (CAPWAP) was performed after the static test.

The redriving (ten blows) forced the pile down additionally about 45 mm.

0

500

0 100 200 300

MOVEMENT (mm)

LOA

0

500

,

0 100 200 300

MOVEMENT (mm)

LOAD

0

500

,

0 100 200 300

MOVEMENT (mm)

LOAD

Result on a test on a 2.5 m diameter, 80 m long bored pile

Does unloading/reloading add anything of value to a test?

20

25

30

)

Acceptance Criterion

20

25

30

)

Acceptance CriterionRepeat test

30

0

5

10

15

0 25 50 75 100 125 150 175 200

MOVEMENT (mm)

LOA

D (

MN

)

0

5

10

15

0 25 50 75 100 125 150 175 200

MOVEMENT (mm)

LOA

D (

MN

)

Page 51: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

6

Plotting the repeat test in proper sequence

15

20

25

30

AD

(M

N)

Acceptance Criterion Repeat test plotted in sequence of testing

31

0

5

10

0 25 50 75 100 125 150 175 200

MOVEMENT (mm)

LOA 500

1,000

1,500

2,000

LOA

D (

KN

)

3232

The above series of unloading/reloading has added nothing but they have cost the client a lot of money.

0

500

0 1 2 3 4

MOVEMENT (mm)

Good measurements do not guarantee good conclusions!

A good deal of good thinking is necessary, too

Results of static loading tests on a 40 m long, jacked-in,

instrumented steel pile in a saprolite soil

0

5

10

15

0 2,000 4,000 6,000 8,000 10,000

LOAD (KN)

0

5

10

0 50 100 150 200 250

UNIT SHAFT SHEAR (KPa)

3333

A good deal of good thinking is necessary, too15

20

25

30

35

40

45

DEP

TH (

m) 15

20

25

30

35

40

DEP

TH (

m) ?

0

5

10

0 2,000 4,000 6,000 8,000 10,000

LOAD (KN)

ß = 0.3

A more thoughtful analysis of the data

0

5

10

0 50 100 150 200 250

UNIT SHAFT SHEAR (KPa)

ß = 0.3

3434

15

20

25

30

35

40

45

DEP

TH (

m)

ß = 0.4

15

20

25

30

35

40

45

DEP

TH (

m)

ß = 0.4

And a second pile:

0

5

10

15

0 50 100 150 200 250 300 350 400 450

UNIT SHAFT SHEAR (KPa)

ß = 0.3

0

5

10

15

0 2,000 4,000 6,000 8,000 10,000

LOAD (KN)

ß = 0.3

3535

15

20

25

30

35

40

45

DEP

TH (

m)

ß = 0.5

15

20

25

30

35

40

45

DEP

TH (

m)

ß = 0.5

400

600

800

ER P

ILE

(KN

) Single PileAverage of 4 Piles

Average of 9 Piles

Group Effect and Interaction

36

0

200

0 2 4 6 8 10

PILE HEAD MOVEMENT (mm)

LOA

D P

E

O’Neill et al. (1982)

20 m

Page 52: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

7

800

mm

800 mm

60 mm

#1

#2 #3

#4 #5

Loading tests on a single pile and a group of 5 piles in loose, clean sand at Gråby, Sweden.

37Data from Phung, D.L (1993)

2.30

m

Pile numbers indicate order of driving. Pile #1 wasdriven first and tested as a single pile. Piles #2 - #5were then driven and tested in sequence as singlepiles. Finally, the full five-pile group was tested withpile cap not in contact with the ground.

8

10

12

14

16

AD

/PIL

E (K

N) Average

#2

#5

#4

#3

#1

#1 as single

38Data from Phung, D.L (1993)

0

2

4

6

0 5 10 15 20 25 30 35 40 45 50

MOVEMENT OF PILE HEAD (mm)

LOA

#12,3 m

340 mm

#2

#3 #4

#5

680 mmc/c = 5.7 b

sq60 mm

Pile #1: Effect of compaction caused by driving Piles #2 — #5 and re-testing

8

10

12

14

16

PILE

(K

N) Pile #1 reloaded as

part of the group after Piles #2 - #5 were driven

#1

#1

Data from Phung, D.L (1993)39

0

2

4

6

0 10 20 30 40 50 60 70 80

MOVEMENT OF PILE HEAD (mm)

LOA

D/P

#1

#2

#3 #4

#5

8

10

12

14

PILE

(K

N)

Head average

Head single

Toe single

Toe average

The main change occurred along the shaft

The toe resistance showed little change, only

40Data from Phung, D.L (1993)

0

2

4

6

0 5 10 15 20 25 30 35 40 45 50

MOVEMENT (mm)

LOA

D/P

Shaft single

Shaft average

The Bi-Directional Static Loading Test

The Osterberg

“O-cell Test”

4141

Jorj Osterberg

2001

Schematics of the Osterberg O-Cell Test(Meyer and Schade 1995)

Telltales

andPile Head

4242

Upward Load

Downward Load

THE O-CELL

Grout Pipe

Page 53: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

8

4343

Three O-Cells inside the reinforcing cage(My Thuan Bridge, Vietnam) 4444

The O-cell can also be installed in a driven pile (after the driving). Here in a 600 mm cylinder pile with a 400 mm central void.

4545 46O-cell in a pipe pile inserted in a augercast pile after grouting.

4747Inchon, Korea

-60-50-40-30

0 5,000 10,000 15,000 20,00

Load (KN)

Results of an O-cell test on a 2.8 m by 0.8 m, 40 m deep barrette in Manila, Philippines

4848

30-20-10

010203040506070

Mov

emen

t (m

m)

Upward

Downward

Upward

Approximate extrapolation of toe movement back to starting conditions

Page 54: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

9

O-Cell test on a 1,250 mm

diameter, 40 m long, bored pile at US82 Bridge 20

40

60

80

100

120

MEN

T (m

m)

UPPER PLATE UPWARD MVMNT

Shaft

4949

across Mississippi

Riverinstalled into dense sand

-80

-60

-40

-20

0

0 2,000 4,000 6,000 8,000 10,000

LOAD (KN)

MO

VEM

LOWER PLATE DOWNWARD MVMNT

Weightof

Shaft

Residual Load

Toe

From the O-Cell results, one can produce the equivalenthead-down load-movement curve that one would haveobtained in a routine “Head-Down Test”

“Head –down”

cnt.

5050

cnt.

5151

O-Cell Results Shown Two Ways

40

60

80

100

120

(mm

)

6,000

7,000

8,000

9,000

N)

Shaft Movement

Toe Movement

cnt.

5252

-80

-60

-40

-20

0

20

40

0 2,000 4,000 6,000 8,000 10,000

LOAD (KN)

MO

VEM

ENT

0

1,000

2,000

3,000

4,000

5,000

0 20 40 60 80 100 120

MOVEMENT (mm)

LOA

D (

KN

Weight of Shaft

Residual Load

38 m

Equivalent Head-down Curve

10

15

20

25

OA

D (

MN

)

Acceptance ReferenceLoad 25 mm Movement

O-cell Load-Movement Curves

-40

-20

0

20

MEN

T (m

m)

UPWARD

DOWNWARD

Evaluation of Proof Test Results from an O-cell Test

10

15

20

25

OA

D (

MN

)

Offset Limit

Acceptance ReferenceLoad 25 mm Movement

53

O-cell0

5

10

0 20 40 60 80

MOVEMENT (mm)

LO

-100

-80

-60

0 5 10 15LOAD (MN)

MO

VEM

Fellenius and Tan, 2010

0

5

10

0 20 40 60 80

MOVEMENT (mm)

LO

Kahuku Bridge across Kamehameha Highway, Hawaii

Test on a 16-inch (600 mm), 75 ft (23 m) long, bored pile in hard clay and

weathered rockDesired allowable load = 340 kips

7

O cell is

5454

-1

0

1

2

3

4

5

6

0 50 100 150 200 250 300 350 400

O-cell Load (kips)

MO

VEM

ENT

(inc

hes)

UPWARD

DOWNWARD

O-cell is placed at

46 ft (14 m) depth

Page 55: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

10

0

10

20

0 100 200 300 400 500 600 700 800

LOAD (kips)

Silty stiff clay

The load distribution after tangent-modulus evaluation of pile stiffness

The equivalent "head-down load distribution"and speculative fully mobilized resistance

0

10

20

0 100 200 300 400 500 600 700 800

LOAD (kips)

SPECULATIVE, FULLY MOBILIZEDDISTRIBUTION

1,100

cnt.

55

30

40

50

60

70

80

DEP

TH (

ft)

DATA FROM O-CELL TEST

O-cell

Shaft and toe resistances are not fully mobilized below the O-cell

Silty hard clay

Weathered rock

Buoyant Weight

Project rules: Qallow. = RULT (=600)/2.0 for test results ===> = 300 kips

Qallow. = RULT(=1,100)/3.0 for calculations ===> = 365 kips

30

40

50

60

70

80

DEP

TH (

ft)

CONVERTED TO HEAD-DOWN "TEST"

APPROXIMATED

O-cell

Orchard Center SingaporeFellenius and Tan (2010)

Combining O-cell and Head-down Tests

56Photo of scale model Photo of building

Head-down Test

Bored Pile, Singapore, 2007

#13

#12

#11

ft)

1,000 mm (39 i )

Stiff

mar

ine

clay

1,030 mm

cnt.

5757

#1

#8

#7

#6

#5

#4

#3

#2

#9

37.5

m (1

23 f

Sapr

olite

Sand

, Silt

, and

cla

y as

mat

rix in

w

eath

ered

gra

nitic

bed

rock

O-cell

Head-down Tangent Modulus

30

40

50∆σ

/∆ε

(GPa

)

SG-13

SG-12

SG-11

SG-9

SG-8

UTP-3, Stage 1b

cnt.

5858

10

20

0 200 400 600 800 1,000 1,200

STRAIN (µε)

SG-7

SG-6

0

5

10

15

20

0 5 10 15 20 25

LOAD (MN)

H (

m)

Now, having determined the

relation between strain and

secant modulus (directly or from

the tangent-modulus), we are

ready to convert measured

strain to ”measured” load in the

Marine clay

cnt.

5959

20

25

30

35

40

DEP

T

UTP-3

Shaft Resistance is not fully mobilized below 20 m depth.

pile: The load distribution. Saprolitic soil

Note

Stage 1 Head-down Test (Stages 1a and 1b)

Stage 2 O-cell test. O-cell is left open

The tests were repeated: Stage 3 head-down and Stage 4: O-cell

5

10

15

20

25-60-50-40-30-20-100

MOVEMENT (mm)

LOA

D (

MN

)

Stage 1

Acceptance Criterion

0 2 4 6 8 10 12 14 16LOAD (MN)

cnt.

60

0

UTP-3 Head-down

-60

-40

-20

0

200 2 4 6 8 10 12 14 16

MO

VEM

ENT

(mm

)

UTP-3 O-cell test

Downward

Stage 4

Stage 2

Max toe movement in Stage 1

Upward

Page 56: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

11

Head-down Test

LOAD DISTRIBUTIONS STAGES 3 AND 4O-cell Test

0

5

10

0 5 10 15 20 25

LOAD (MN)

Max LoadSt 1b

Before Start

After Unload

0

5

10

-5 0 5 10 15 20

LOAD (MN)

cnt.

61

15

20

25

30

35

40

DEP

TH (

m)

UTP-3, Stage 3

Unload

O-cell

C

15

20

25

30

35

40

DEP

TH (

m)

UTP-3, Stage 4

O-cell

Before Start

D

0

5

10

15

0 10 20 30 40 50 60

LOAD (MN)

"Flipped" UTP-3O-cell Curve

Maximum ResistanceHead-down Test (1b)

Head-down curves movedto connect ith

0

5

10

15

0.0 0.5 1.0 1.5 2.0

BETA COEFFICIENT (--)

)

ß

rs, avg. = 100 KPa

Combining the results of the head-down and O-cell tests

cnt.

6262

20

25

30

35

40

DEP

TH (

m) to connect with

load in O-cell test

Effective stress analysis fitted to tests

15

20

25

30

35

40

DEP

TH (

m)

O-cell

Head-downPILE UTP-4

A B

rs, avg. = 450 KPa

rs, avg. = 550 KPa

Head-downPILE UTP-3

The effect of residual load on an uplift test ("Head-up")

0

5

10

-2,000 -1,500 -1,000 -500 0 500 1,000

LOAD (KN)

m)

True Resistance

TENSION TESTAND FULL RESIDUAL LOAD

Residual Load

0

5

10

-2,000 -1,500 -1,000 -500 0 500 1,000

LOAD (KN)

m)

Residual Load

True Resistance

TENSION TESTAND PARTIAL RESIDUAL LOAD

63

15

20

25

30

35

DE

PTH

(m

False Resistance

Toe Resistancein an Uplift Test?!

15

20

25

30

35

DEP

TH (

m

False Resistance

Toe Resistancein an Uplift Test?

Combining the results of a head-down test with those of a tension test will help determining the true resistance

0

5

10

15

0 500 1,000 1,500 2,000 2,500 3,000 3,500

LOAD (KN)

H (

m)

HEAD-DOWN AND PARTIAL RESIDUAL LOAD

FalseHead-down

True Shaft

False TensionTest

6464

20

25

30

35

DEP

TH

Residual Load

True Resistance

Residual and TrueToe Resistance

Transition Zone

True Shaft Resistance

Not directly useful below this level

Now you know why some claim that resistance in tension is smaller than that in compression

0

5

10

15

0 500 1,000 1,500 2,000 2,500 3,000 3,500

LOAD (KN)

(m)

O-CELLAND FULL RESIDUAL LOAD

Residual Load

The effect of residual load on an O-cell test

0

5

10

15

0 500 1,000 1,500 2,000 2,500 3,000 3,500

LOAD (KN)

(m)

O-CELLAND PARTIAL RESIDUAL LOAD

True Shaft

65

20

25

30

35

DEP

TH Load

False Resistance

True Resistance

Residual and TrueToe Resistance

EquivalentHead-down

False Resistance

The O-cell

The O-cell load includes the residual load whereas the load evaluated from the strain-gages does not.

20

25

30

35

DEP

TH

Residual Load

False Resistance

True Resistance

True Shaft Resistance

EquivalentHead-down

False Resistance

The O-cell

0

5

10

0 500 1,000 1,500 2,000 2,500 3,000 3,500

LOAD (KN)

True Shaft Resistance

False Head-down Resistance

Combining an O-cell test with a subsequent head-down test to determine the distribution of residual load

66

15

20

25

30

35

DEP

TH (

m) Resistance

False O-cell Resistance

True Resistance

O-cell Equivalent Head-down False

Resistance

Residual Load

Page 57: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

12

Measured load-movements can besimulated (fitting) to t-z and q-z relations

Pile shaft by t-z relation; Pile toe by q-z relation ("Ratio function")

80

100R = MVMNT^Exp

TOE

SHAFT

exp

2

1

2

1 )(δδ

=RR

Ratio function

cnt.

6767

0 20 40 60 80 1000

20

40

60

Movement (%)

Res

ista

nce

(%)

Exp. = 0.75

Exp. = 0.05

Exp. = 0.50

Exp. = 0.33

Exp. = 0.20

Exp. = 0.10

t-z and q-z (and p-y) functionsHypothetical case of load-movement curves modeling a test on a pile with a capacity of 100 % at a pile head movement of 4 mm

b

uurr ⎜⎜⎝

⎛⎟⎟⎠

⎞=

δδ

21 CCr

+=

δδ

RATIO

HYPERBOLIC

80

100

120

140

AR

(%

of r

ult)

Ratio (b = 0.25)

Hyperbolic (C2 = 0.006)

Exponential (b = 0.75)rU

80 % (strain-hardening)

Zhanga = 0.0083r∞/ru = 50 %

δb

6868

EXPONENTIAL

80 %

Zhang0

20

40

60

0 5 10 15 20 25

RELATIVE MOVEMENT BETWEEN PILE AND SOIL ELEMENT (mm)

SH

AFT

SH

EA

80 % (strain-softening)δU

2)()(

δδδ

bacar

++

=

21 CCr

+=

δδ

uu

ar

−=21

2bc

rru =∝

)1( δbu err −−=

uu

ar

−=41

The ratio function applies also a toe response and, some of the functions can also be used as p-y curves which is the term applied to horizontally loaded piles.

Pensacola, Florida410 mm diameter, 22 m long, precast concrete pile driven into silty sand

6969

Pensacola, Florida, USA

1

2

3

4

(mm

)

10

20

30

40

50

60

MO

VEM

ENT

(mm

)

O-cell equipped, 16-inch, 72-ft, prestressed pile driven into sand.

cnt.

7070

-4

-3

-2

-1

0

0 500 1,000 1,500 2,000 2,500

LOAD (KN)M

OVE

MEN

T (

-10

0

0 500 1,000 1,500 2,000 2,500

LOAD (KN)

O-cell

After the push test, the pile toe is located higher up than when the test started!

Test at Bangkok Airport

7171

Stage 1Lower Cell activatedUpper cell closed

Stage 2Lower Cell openUpper Cell activated

Stage 2

cnt.

7272

Stage 2Lower Cell closedUpper Cell activated

Data fromFox, I., Du, M. and Buttling,S. (2004)Buttling, S. (2006)

Page 58: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

13

Downward movements during test phases 1, 2, and 3

0

25

50

75

100

0 2,000 4,000 6,000 8,000 10,000

LOAD (KN)

EMEN

T (m

m) P1 P2

P3

1 2 3

cnt.

7373

Concern was expressed (Buttling 2006) that the toe resistance (Phase 1) was ≈3,000 KN and the shaft resistance for the lower segment was ≈5,000 KN (Phase 2), while in Phase 3 the combined shaft and toe resistances were only ≈6,000 KN. Should not the Phase 3 resistance be ≈8,000 KN rather than ≈6,000 KN (i.e., the sum of the values ≈5,000 KN and ≈3,000)?

125

150

175

MO

VE

Active CellInactive, Open CellInactive, Closed Cell

0

25

0 2,000 4,000 6,000 8,000 10,000

LOAD (KN)

P3

1 2 30

25

0 2,000 4,000 6,000 8,000 10,000

LOAD (KN)

(mm

)

1 2 3

The downward toe movements. However, the movements are best plottedper sequence of testing. Particularly when considering the example toeresistance, one must evaluate the load-movement response in comparingPhase 1 + Phase 2 to Phase 3 (i.e., P2 shaft below cell plus P1 toe).

cnt.

7474

50

75

100

125

150

175

MO

VEM

ENT

(mm

)

Active CellInactive, Open CellInactive, Closed Cell

P1 P2P3

50

75

100

125

150

175DO

WN

WA

RD

MO

VEM

ENT

Active CellInactive, Open CellInactive, Closed Cell

P2

P1 and P2 data combined

P3

O-cell Tests on a 1.4 m diameter

bored pile in North-West Calgary

constructed in silty glacial clay till

7575

glacial clay till

A study of Toe and Shaft Resistance Response to Loading and correlation to CPTU

calculation of capacity

0

5

10

0 10 20 30Cone Stress, qt (MPa)

0

5

10

0 200 400 600 8001,00

0

Sleeve Friction, fs (KPa)

0

5

10

-100 0 100 200 300 400 500

Pore Pressure (KPa)

0

5

10

0 1 2 3 4 5

Friction Ratio, fR (%)PROFILE

The upper 8 m will be removed for basement

uneutral

GW

Cone Penetration Test with Location of Test Pile

cnt.

7676

15

20

25

30

DEP

TH (

m)

10

15

20

25

30

DEP

TH (

m)

10

15

20

25

30D

EPTH

(m

)

10

15

20

25

30

DEP

TH (

m)14 m

net pile length

30

40

50

60

70

80

ENT

(mm

)

Pile Profile and O-cell Location O-cell Load-movement Up and Down

ELEV.(m)

cnt.

7777

-30

-20

-10

0

10

20

0 1,000 2,000 3,000 4,000 5,000 6,000

LOAD (KN)

MO

VEM

E

#5

#4

#3

#2 #1

Load Distribution

0

5

0 5 10 15 20LOAD (MN)

0

5

0 5 10 15 20LOAD (MN)

cnt.

7878

10

15

20

25

DEP

TH (

m)

O-cell

10

15

20

25

DEP

TH (

m)

ß = 0.75

ß = 0.35

Page 59: Fellenius   bases de diseño de pilotes de fundación

3/24/2013

14

 

0

5

0 5 10 15 20LOAD (MN)

After consideration of potential presence of residual load and applying judgment

Load Distribution

cnt.

7979

10

15

20

25

DEP

TH (

m)

ß = 0.75

ß = 0.35

ß = 0.65

0

5

0 5 10 15 20LOAD (MN)

Schmertmann

LCPC withoutmax. limitsTEST

LCPC withmax. limits

Load Measured Distribution Compared to Distributions Calculated from the CPTU Soundings

cnt.

8080

10

15

20

25

DEP

TH (

m)

E-F

8,000

10,000

12,000

14,000

(KN

) Loadtest's Curvefor the Pile Head

Pile Head

Pile Shaft

The Test Data for Shaft and Toe and Evaluation of Head-down Movement Using t-z and q-z evaluations

cnt.

8181

0

2,000

4,000

6,000

0 20 40 60 80 100 120

MOVEMENT (mm)

LOA

D Pile Shaft

Pile Toe

Test range

Los Angeles Coliseum, 1994Case Record

82

The Northridge earthquake in Los Angeles, California,in January 1994 was a "strong" moment magnitudeof 6.7 with one of the highest ground accelerationever recorded in an urban area in North America.

The piles had been designed using the usual design approachwith adequate factors of safety to guard against the unknowns.Moreover, the acceptable maximum movement was morestringent than usual.

The earthquake caused an estimated $20 billion inproperty damage. Amongst the severely damagedbuildings was the Los Angeles Memorial Coliseum,which repairs and reconstruction cost about $93million. The remediation work included constructionof twenty-eight, 1,300 mm diameter, about 30 m long,bored piles, each with a working load of almost9,000 KN (2,000 kips), founded in a sand and graveldeposit.

It was imperative that all construction work was finished in sixmonths (September 1994, the start of the football season).However, after constructing the first two piles, which took sixweeks, it became obvious that constructing the remainingtwenty-six piles would take much longer than six months.Drilling deeper than 20 m was particularly time-consuming.The design was therefore changed to about 18 m length,combined with equipping every pile with an O cell at the piletoe. — Note, the O-cell was now used as a construction tool.

Los Angeles Coliseum, 1994

-100

-90

-80

-70

-60

-50

-40

-30

-20

-10

0

10

20

30

40

0 2,000 4,000 6,000 8,000 10,000

LOAD (KN)

MO

VEM

ENT

(mm

)

100

-90

-80

-70

-60

-50

-40

-30

-20

-10

0

10

20

30

40

MO

VEM

ENT

(mm

)

20

30

40

ONE OF THE PILES

cnt.

83

-1000 2,000 4,000 6,000 8,000 10,000

LOAD (KN)

Schmertmann (2009, 2012), Fellenius (2011)

-100

-90

-80

-70

-60

-50

-40

-30

-20

-10

0

10

0 2,000 4,000 6,000 8,000 10,000

LOAD (KN)

MO

VEM

ENT

(mm

)

THE O-CELL AS A CONSTRUCTION TOOL

TESTS ON EVERY PILE

ONE OF THE PILES

THREE OF THE PILES

ALL PILES

2,000

4,000

6,000

8,000

10,000

LOA

D (

KN

)

Downward, First Loading

2,000

4,000

6,000

8,000

10,000

LOA

D (

KN

)

Downward, Second Loading

cnt.

84

FIRST STAGE LOADING; "VIRGIN" TESTSWITH LINE SHOWING AVERAGE SLOPE

RELOADING STAGE. DOWNWARD DATA ONLY

The first stage loading is of interest in the context of general evaluation of test results and applying them to design

00 25 50 75 100 125 150

MOVEMENT (mm)A0

0 25 50 75 100 125 150MOVEMENT (mm)B

Page 60: Fellenius   bases de diseño de pilotes de fundación

1

BASICS OF DESIGN OF PILED

FOUNDATIONS

Bengt H Fellenius

1

Bengt H. Fellenius

Case Histories of Results from Instrumented Piles and Soil

Leading up to the Unified MethodBolivia, April 25, 2013 22

• Design of piles requires understanding of how load is transferred from pile to soil and, less obvious but equally important, from soil to pile.

Th t t t f th t h l d f f

33

• The current state-of-the-art has evolved from a few ground-breaking case histories that appeared in the late 1960s and early 1970s.

Bjerrum et. al., (1965; 1969)

presented case histories of 300-mm diameter steel piles

CASE #1

44

driven through marine clay

deposited directly on bedrock in Oslo Harbor, Norway.

Heröya

55

Profile of test site and piles. Heröya site.

(Bjerrum et al., 1969)

0

5

10

15

20

0 100 200 300 400

EFFECTIVE STRESSAND PORE PRESSURE (KPa)

DEP

TH (

m)

σ'z after full dissipation of excess pore

pressure

σ'zΔu

Marine Clay

FILL

0

5

10

15

20

0 300 600 900 1,200 1,500

PILE LOAD (KN)

DEPT

H (m

)

uncoated

Distribution calculated from

ß=0.3 times σ'z for actual excess u

Measured distribution

0

5

10

15

20

0 5 10 15

PILE SHORTENING (mm)

DEP

TH (

m)

Bitumen coated uncoated

66

Distribution of soil stress, excess pore pressure, pile shortening, and load distributions. Heröya site. (Data from Bjerrum et al., 1969).

25

30

35

Start of Bedrock

Gravel

25

30

35

Bitumen coated

Notice the distinct Force Equilibrium, the Neutral Plane

25

30

35

Page 61: Fellenius   bases de diseño de pilotes de fundación

2

Compilation of Norwegian results

cm cm β

Drag load

77

0

Endo et al. 1969, presented a very

ambitious study in Japan on drag load on four

i t t d t l il

CASE #2

88

instrumented steel piles during a period of three

years. The soils consist of silt and clay on sand. The case history is one of the few that actually also

measured settlement.

99

Profile of test site and piles

Closed-toe, Open-toe, Inclined, and Short Pile

(Endo et al., 1969)

Neutral plane = Force Equilibrium = Settlement Equilibrium

0

5

10

15

20

25

0 500 1,000 1,500 2,000 2,500 3,000 3,500

LOAD (KN)

H (

m)

SandySilt

Clay

0

5

10

15

20

25

0 50 100 150 200

SETTLEMENT (mm)

Soil

Pile

1010

Load distribution in the three long piles together and settlement of soil and piles measured March 1967 672 days after start. (Data from Endo et al., 1969).

25

30

35

40

45

50

DEP

TH

Closed-toePiles: Inclined and Vertical

Open-toePile

Sand

Silt

( ) ?

25

30

35

40

45

50Closed-toe PilesToe

Penetration

- NEUTRAL PLANE -

Toe forces and toe penetrations extracted from the graphs of Endo et al.

1,500

2,000

D (

KN

)

Approximation

11

0

500

1,000

0 10 20 30

TOE PENETRATION (mm)

TOE

LOA

D

From data in paper

0

5

10

15

20

25

0 2,000 4,000 6,000 8,000

LOAD (KN)

PTH

(m

) Measured load

Calculated Curve

ß = 0.40

ß = 0.35

1212

30

35

40

45

50

DE

P

ß = 0.30

ß = 0.25

Measured load distribution and distribution matched to measured values in effective stress analysis. (Data from Endo et al., 1969).

Page 62: Fellenius   bases de diseño de pilotes de fundación

3

Fellenius (1972) presented a study

of two instrumented,

precast concrete

CASE #3

1313

piles driven through marine clay and

into sandat Bäckebol,

Göteborg, Sweden

1414

M# = Pile Force gages

0

5

10

15

20

25

0 25 50 75 100

PL, LL, and wn (%)

DEP

TH (

m)

LAYER 2

LAYER 3 wn LAY

1515

30

35

40

LAYER 4

LAYER 5

SAN

DC

Pile II segments with Gage M4 at pile toe

1616

First load (360 KN) placed on the piles

1717

Piles with loads applied but before fill was placed over the site

1818

Page 63: Fellenius   bases de diseño de pilotes de fundación

4

800

1000

1200

1400

1600

1800

E A

T G

AG

E (K

N)

First load placed on piles

Second load placed on piles

2 m thick fill placed over site M1 & M5

M2 & M6

M3 & M7

M2 & M6

M3 & M7

1919Measured loads in piles versus time after driving

0

200

400

600

0 500 1,000 1,500 2,000 2,500 3,000 3,500

DAYS AFTER END OF DRIVING

FOR

CE

M4

M4

M1 & M5

0

10

20

30

0 500 1000 1500 2000FORCE AT GAGE (KN)

= “LIVE LOADS”

Placing the fill

2020

40

50

60

2,650

19881923

Distribution of load in Piles I and II

Note, the dragload was eliminated by the “live load” Neutral

Plane

That the toe resistance is small is

due to that the movements are not

large enough to mobilize any larger toe

resistance

Distribution of measured and calculated consolidation settlement due to the fill

The settlement measured at depth

0

5

10

15

0 50 100 150 200 250

STRESS (KPa)

(m)

(σ'Z)f

0

5

10

15

0 100 200 300 400 500

SETTLEMENT (mm)

(m

)

MEASURED

CALCULATED FINAL (after 80

years)

2121

pamounted to only a few millimeters,

but this was enough to fully

mobilize the negative skin

friction

20

25

30

35

40

DEP

TH

(σ'Z)i PRECONSOLIDATION

STRESS, σ'c

20

25

30

35

40

DEP

TH

Force gage locations

FHWA Project, Keehi Interchange, Honolulu,Hawaii 1977

CASE #5

2222

Test piles, embankment fill, and soil profile

OLD FILL

EMBANKMENT

SOFT CLAY

27 m

SLEEVE

PLAN VIEW

PILE #8PILE #6

PILE #7

18 m

6 m

CASE #5

2323

Data from Clemente, 1981

SOFT CLAY w = 70 %

LL = 80PL = 45

SILTY CLAY

MIXED STRATACORAL SANDCORAL CLAY

0

10

20

30

0 500 1,000 1,500 2,000 2,500

LOAD (KN)

TH (

m)

450 mm

10 mmEND OF

SETTLEMENT

0

10

20

30

0 500 1,000 1,500 2,000 2,500

LOAD (KN)

TH (

m)

ß = 0.25

450 mm

10 mmEND OF

SETTLEMENT

Total stress evaluation Effective stress evaluation

24243/16 inch = 4 mm

30

40

50

60

DEP

T

0 mm

END OF COAT

ß = 0.25

#7 #6

#8

30

40

50

60

DEP

T

ß = 0.25

0 mm

35 m uncoated pile ==> 1,770 KN35 m bitumen coated pile ==> 375 KN for less than 1/16-inch (1.5 mm) coat = Reduction to 20 % of uncoated load 3/16 coat + stiff outer skin ==> elimination of drag load

END OF COAT

ß = 0.25

#7 #6

#8

Page 64: Fellenius   bases de diseño de pilotes de fundación

5

2525

Bitumen coating of piles

Laboratory tests on bitumen coats at different

2626

at different rates of shear

A study in Australia of two 760 mm, strain-gage instrumented, open-toe pipe piles driven through a 6 m sand layer over a 15.5 m thick overconsolidated silty clay deposited on silt and sand. Ground surface settlement was induced by placing a 3 m high surcharge over 200m x 100m area around the test piles, causing drag load.

CASE #6

2727Data from Walker et al. (1973

0

5

10

15

0 50 100 150 200 250 300

DAYS AFTER START

T (m

m)

1,500

2,000

KN)

Fill completed

Load in pile at 20m depth

CASE #6

0

5

10

15

20

0 500 1,000 1,500 2,000 2,500

LOAD (KN)

DEP

TH (

m)

FILL

FineSand

StiffSiltyClay

Tran

sfer

Zon

e

Bitumen coated

pile

2828

Load distribution on two pipe piles, one bitumen-coated and one uncoated

20

25

30

35

40

SE

TTLE

ME

NT

0

500

1,000

LOAD

(K

Settlement

Ground surface settlement due to a 3 m high surcharge placed over 200m x 100m area around the test piles.

Data from Walker et al. (1973

25

30

35

SandySilt

Sandand

Gravel

Leung, C.F, Radhakrishnan, R., and Tan Siew Ann (1991) presented a case history on

instrumented 280 mm square precast concrete piles driven in marine clay in Singapore

Note, the distribution of negative skin friction is linear (down to the beginning of the transition zone) indicating the proportionality to the effective overburden stress

CASE #7

2929

Neutral PlaneTRANSITION

ZONE

0

5

10

0 200 400 600

LOAD (KN)

(m)

OldSilt&

ClayFill

Marine

ß = 0.5

Two months

after start(57 days)

Two years later

(745 days)

Variable load i.e., Live Load

3030Data from Leung, Radhakrishnan, and Tan (1991)

15

20

25

30

DEP

TH

Clay

Weak Shale

Bedrockand

Residual Soil

Clay

Page 65: Fellenius   bases de diseño de pilotes de fundación

6

• Indraratna et al. (1992) reported results from full-scale field tests on instrumented 400 mm diameter, 25 m long cylinder piles driven into Bangkok clay

CASE #8

3131

piles driven into Bangkok clay. Tests were made in push and pull on bitumen-coated and uncoated piles.

-10

-5

0

5

-15 -10 -5 0 5 10 15

Distance (m)

Dist

ance

(m

)

Coated Uncoated

3232Indraratna et al. 1992

10

-5

0

5

10

15

20

25

30

-15

DEPT

H (

m)

PiezometersLoad Cells

Coa

ted

Leng

th

Weathered

Soft

Stiff

2 m high embankment Fill

Installation was made one 4 m long segment at a time. Beforesplicing on the next segment and continuing, pull tests were carriedout. The diagrams below show the measured load-movementcurves.

300

400

500

AD

(K

N)

8 m Length

12 m Length

16 m Length

20 m Length300

400

500

AD

(K

N)

8 m Length

12 m Length

16 m Length

20 m Length

Uncoated Pile Bitumen Coated Pile

00 200 400 600 800

3333

0

100

200

0 10 20 30 40 50

MOVEMENT (mm)

LOA

0

100

200

0 10 20 30 40 50

MOVEMENT (mm)

LOA

Data from Indraratna et al. 1992

Pull Test Results

5

10

15

20

25

30

0

5

0 100 200 300 400 500 600 700 800

Axial Load (KN)

Ground Surface

Loads from pull tests

The measurements compiled and put into

the context of the basic soil response.

0

5

0 100 200 300

SETTLEMENT (mm)

PILE

0 5 10 15 20

3434Data from Indraratna et al. 1992

10

15

20

25

30

DE

PTH

(m

)

β = 0.2

β = 0.3 β = 0.3

Loads at 265 days

p

Settlement distributionMeasured and calculated load distribution

10

15

20

25

30D

EPTH

(m

)

3 Days

25 Days

53 Days

81 Days

141 Days

209 Days

265 Days

10

15

20

25

35

CASE #9

36

Okabe, T., 1977. Large negative skin friction and friction-free methods.

Proc. 9th ICSMFE, Tokyo, Vol.1, pp. 679 – 683.

Page 66: Fellenius   bases de diseño de pilotes de fundación

7

Strain-gage instrumented, 600mmdiameter, pipe piles driven throughsilty clay and silt with silty sand.

A fill was placed on the ground (no

CASE #9

0

5

10

15

20

0 10 20 30 40 50 60 70 80

wn, wP, and wL (%)

(m)

37Data from Okabe (1977)

A fill was placed on the ground (noinformation of fill height) over a vastarea of the site and pumping ofwater at depth lowered the porepressures at depth (no informationon pore pressure distribution).

25

30

35

40

45

50

DEP

TH (

0

10

0 2,000 4,000 6,000 8,000

LOAD (KN)

83 days

131 days

277 days

944 days

Test Pile #1 — Single Pile

Load distribution with time after driving

Test Pile #2 — Single Pile

Load distributions as loads (700 KN and 1,000 KN have been placed on the pile head

0

10

0 1,000 2,000 3,000 4,000 5,000

LOAD (KN)

550 days

+1 day

+5 days

+28 days

38

20

30

40

50

DEP

TH (

m)

1,663 days20

30

40

50

DEP

TH (

m) +63 days

++1 day

++5 days

++19 days

++43 days

++59 days

++194 days

?

Data from Okabe 1977

0

10

-2,000 0 2,000 4,000 6,000 8,000

LOAD (KN)

-

Note: Tension

Average of sleeved piles

Group of piles connected to a common cap

Four piles are “sleeved” one pile is not

0

10

-1,000 0 1,000 2,000 3,000 4,000

LOAD (KN)

?

-

Sacrificial

Group of piles connected to a common cap surrounded by “sacrificial” piles supposedly(?)

not connected to cap

39

20

30

40

50

DEP

TH (

m)

Depth of sleeve

No-sleeve pile

20

30

40

50

DEP

TH (

m)

Sac c apiles

Foundation piles

Sacrificial pile

Data from Okabe 1977

Case historieson

Damaging Drag Load

4040

g g gand

Damaging Downdrag

Inoue, Y., Tamaoki, K., and Ogai, T., 1977. Settlement of building due to pile downdrag. Proc. 9th ICSMFE, Tokyo, July 10-15, Vol. 1, pp. 561– 564.

CASE #10

41

A three-storey building with a foot print of 15 m by 100 m founded on500 mm diameter open-toe pipe piles driven through sand and siltyclay to bearing in a sand layer at about 35 m depth. The piles hadmore than adequate capacity to carry the building. Two years afterconstruction, the building was noticed to have settled some 150 mm.Measurements during the following two years showed about 200 mmadditional settlement. The building was demolished at that time.

A Downdrag Case

< 102 m >

SAND FILL

42

FINE SAND

SILTY CLAY: w = wL = 40% - 60%; τu = 40 KP

SILTY CLAY: w = wL = 40% - 60%; τu = 80

FINE SAND

SAND FILL

FINE SAND

SILT & SAND

Pile Toe Depth Inoue 1977

Page 67: Fellenius   bases de diseño de pilotes de fundación

8

FINE SAND

SILTY CLAY: w = wL = 40% - 60%; τu = 40 KP

SILTY CLAY: w = wL = 40% - 60%; τu = 80

FINE SAND

SAND FILL

FINE SAND

SILT & SAND

43Settlement between piles in Row 6 and Row 10 from Sep. 1967 through May 1969 = 150 mm.

Slope ≅ 1 : 100 (Sep 67 Apr 71)

Inoue 1977

LOAD — SETTLEMENT

m)

Soil settlement

Load in Pile

Building

-5

0

5

10

15

0 200 400 600 800

m)

Stress and Pressure (KPa)

SAND

SAND

CLAY

Settling Layer

44

Dep

th (

Speculative distribution

Data from Inoue et al. 1977

20

25

30

35

40

45

Dep

th (m

SAND

CLAY

SANDsilt"Current"

Ef fective Stress

Pore Pressure

30 m long piles driven to bedrock 50 m long

piles driven to shaft bearring

Province A Province B

Marine l

XXXX ≈NEUTRAL PLANE

Highly loaded (max allowed by code)

Lightly loaded

≈NEUTRAL PLANE

4545One Bridge — Two foundations

?

clay on bedrock

A CASE HISTORY OF A STRIP-MALL FOUNDED ON PILES

GROUND SURFACE

4646Limestone bedrock providing good bearing

The soils investigation revealed 54 ft (16m) of no-strength "muck".

Design called for 54 ft long piles. Designer discounted all shaft resistance contribution.

54 ft(16 m)

54 ft (16m) f " k'

GROUND SURFACE

4747

of "muck'

Limestone bedrock providing good bearing

Strip-Mall as designed

A real DOWNDRAG case

ORIGINALGROUND SURFACE

5 ft (1.5m) of fill added before the piles were

4848

X x X x X x X x X x X x X x X

54 ft (16m) of "muck"

Limestone bedrock providing good bearing

pdriven

5 ft (1.5m) of "muck"

Page 68: Fellenius   bases de diseño de pilotes de fundación

9

Office Building placed on longtoe-bearing piles in Brisbane,Australia. A later built, lightextension was placed on shortwood piles.

5 m

0 m

FILL

Soft CLAY

49

10 m

15 m

0 1 2 3 MPaqc :

Stiff CLAY

SANDSTONE

Data Courtesy (2007) of Wagstaff Piling Pty. Ltd., Queensland, Australia.

View toward the roof

5050

Foundations and underpinning

5151

The original piles had a capacityabout three times the applied load,but downdrag got the better of them.Luckily, new piles could be installed(driven to the sandstone; for somecolumns to a“four-for-one” ratio).

$ $ $ $

A downdrag Case

52Courtesy of Joram M. Amir, Amir Geotechnical Engineering Ltd.

The photo shows a building placed on piled foundations made up of 14 m longbored piles through loose non-engineered coarse-grained fill into soft rock.Once the building was occupied and the lawn and garden established andwatered, the fill lost volume and ground settled. The pile capacity was morethan adequate to support the building loads.

Under one wing of the building, the fill layer was thicker, in fact, approachingthe length of the piles. The reduced pile length in the rock plus the pile toeresistance under the wing was not sufficient to prevent a neutral plane —settlement equilibrium — from developing in the fill. Therefore, considerabledowndrag developed and the building wing suffered extensive damage.

Monitoring deformations and settlement in Uppsala, Sweden (1965)

70

53530

10

20

30

40

50

60

70

0 10 20 30 40 50 60

EAST-WEST (m)

NO

RTH

- SO

UTH

(m

)

Stand-pipe Piezometers, ZHouse Bench MarksGround Benchmark, STest Piles, PBorehole, B+

+

N

P88

P52

P2P1

Z1

Z2

Z3

B1

S3 S1

S2

0

5

10

0 10 20 30 40 50UNDRAINED SHEAR STRENGTH (KPa)

m)

0

5

10

0 10 20 30 40 50 60 70 80WATER CONTENT (%)

m)

CLAYCLAY

(mean level) GW GW

Basement Excavation

+11.00 m

Clay crust

Soil Profile After construction, a one metre thick fill was placed over the site around all buildings.

54

15

20

25

DEP

TH (

m

15

20

25

DEP

TH (

m

SILT SILT

SAND & GRAVEL SAND & GRAVELPilePile

Drop-hammer driven, 250 mm diameter, ordinary reinforced, precast concrete pile.

Page 69: Fellenius   bases de diseño de pilotes de fundación

10

LID

LID

BASEMENTWALL

BASEMENTFLOOR

PILE

CENTERTUBE

3

21

CLAY

+ 11.00 m

+ 10.30 m

ORIGINALGROUNDSURFACE CONSOL

+ 12.00 m

Fill

50 mm 'SETTLEMENT' PIPE

4 7

8

9

10

0 200 400 600 800 1000 1200

DAYS

PHRE

ATI

C E

LEVA

TIO

N (

m)

WINTER -67/68 WINTER -68/69 WINTER -69/70

+

+

+

+

Z1 & Z2

Z3

0 200 400 600 800 1 000 1 200

DAYS

Phreatic elevation measured in Piezometers Z1 - Z3

55

UPPERTELLTALE

LOWERTELLTALE

PILE TOE

19.5 mm SOUNDINGROD

25 mm PROTECTION PIPE

SILTSAND

GRAVEL

- ≈ 5.0 m

- ≈ 10.5 m

0

5

10

15

20

25

30

0 200 400 600 800 1,000 1,200G

RO

UN

D S

UR

FAC

E SE

TTLE

MEN

T (m

m)

S1S2P1P2P52P88

WINTER -67/68 WINTER -68/69 WINTER -69/70

Settlement of ground surface at benchmarks close to building and at test piles

Measurement arrangement at the test pilesfor measuring pile shortening and settlementof building and soil

-3

-2

-1

0

1

0 200 400 600 800 1 000 1 200

SETT

LEM

ENT

(mm

)

From Survey At Pile 1 At Pile 2

At Pile 52 At Pile 88

WINTER -67/68 WINTER -68/69 WINTER -69/70

-2

-1

0

OVE

MEN

T (m

m)

F ll L th Sh t i

56

0 200 400 600 800 1,000 1,200

DAYS

-30 200 400 600 800 1,000 1,200

DAYS

MO Full Length Shortening

Upper Length ShorteningLower Length ShorteningWall SettlementPile Toe Penetration

Pile 1Pile P1 shortening and building settlement measured after completion of building. The shortening of the upper and lower lengths of pile were about 1.5 mm and 0.5 mm, respectively, which corresponds to an average strain of 100 µε for both lengths

Settlement of pile-supported basement wall measured near the test piles and according to survey

0

5

10

0 200 400 600 800 1,000

LOAD (KN)

EPTH

(m

)

Increase of load after three years

0

5

10

0 200 400 600 800 1,000

LOAD (KN)

EPTH

(m

)

Load distribution after three years

Load distribution at end of construction

Drag load after three years

57

15

20

25

DE

Average Load in Upper, Lower,and Full Lengths of Pile

BA. Typical distribution of load in a pile at end of construction and three years later

B. Increase of load in the pile during three years

15

20

25

DE

Neutral plane

Assumed short and long term mobilized toe resistances

A

Page 70: Fellenius   bases de diseño de pilotes de fundación

1

BASICS OF DESIGN OF PILED

FOUNDATIONS

Bengt H Fellenius

1

Bengt H. Fellenius

The Unified Method for Design of Piled FoundationsCapacity, Drag Load, Settlement, and Downdrag

Bolivia, April 25, 2013

A foundation design is carried out by a team of professionals

2

3

Distribution of load at the pile cap

The case histories have made us realize how piles and piled foundations will respond to load and settling soil. Here are a few applications of the knowledge gained.

00 500 1,000 1,500 2,000 2,500 3,000

LOAD and RESISTANCE (KN)

DEAD LOAD LIVE LOAD CAPACITY

44

5

10

15

20

DEP

TH (

m)

CLAY

SAND Neutral PlaneTransition Zone

Static Loading Test Distribution

The effect of different pile length and/or different toe resistance response

0

5

0 500 1,000 1,500 2,000 2,500 3,000

LOAD and RESISTANCE (KN)

m)

CLAY

55

10

15

20

DEP

TH (

m

SAND

This pile happens to have more (about 50%) toe resistance or is longer.

0

5

10

-500 0 500 1,000 1,500 2,000 2,500

LOAD and RESISTANCE (KN)

EPTH

(m

)

CLAY

66

15

20

DE

SAND Neutral PlaneTransition Zone

Now, let’s assume that this pile is damaged at the pile toe, or that debris collected at the toe, eliminating the toe resistance.

So, what is the effect of this?

Page 71: Fellenius   bases de diseño de pilotes de fundación

2

0

5

-500 0 500 1,000 1,500 2,000 2,500

LOAD and RESISTANCE (KN)

(m)

CLAY

77

10

15

20

DEP

TH

SAND Neutral PlaneTransition Zone

AVERAGE"AVERAGE" or Design Pile

The analysis of the capacity and resistance distribution detailed in the foregoing deals withanalysis of a single pile or small groups of piles, where interaction between the piles doesnot occur or is negligible. However, for larger groups, the group effect is substantial. Thereis a difference between a single pile and a pile in a group of piles, as well as between pilesinside a pile group as opposed to at the perimeter of the group.

Most of our knowledge comes from studies of the response of single piles. Yet, piles are rarely single. So, what about the response of a group of piles?

8

A moderate size pile group (36 piles), two small groups (4 and 2 piles), and a single pile.

Pile Group: b = 0.32 m, c/c = 1.0 m (1.4 m) = 3.1b (4.4 b) Pile area to footprint area = 8 %

0

5

10

15

20

25

0 50 100 150

Neg. Skin. Friction (KPa)

DEP

TH (

m)

0

5

10

15

20

25

0 1,000 2,000 3,000

Drag Load (KN)

DEP

TH (

m)

0

5

10

15

20

25

0 50 100 150

Neg. Skin. Friction (KPa)

DEP

TH (

m)

9

30

35

40

45

D

CENTER SINGLE

Distributions of unit negative skin friction and of accumulated drag load for a single pile and for a fully shielded pile in the center of the group.

30

35

40

45

D

30

35

40

45

D

CENTER SINGLE SINGLECENTER

0

5

10

15

20

25

0 500 1,000 1,500 2,000 2,500 3,000

LOAD (KN)

DEP

TH (

m)

SINGLE

CENTER

SIDE

CORNER

10

30

35

40

45

Load distribution in the pile group piles ("Center", "Side", and "Corner") and single pile ("Single), assuming the Center piles fully shielded, and the Center and Corner piles partially shielded from the negative skin friction effect.

Let's assume that conditions at depth > 40 m are such that the neutral plane lies at a depth of 40 m

0

5

10

15

20

25

0 500 1,000 1,500 2,000 2,500 3,000

LOAD (KN)

EPTH

(m

)

SINGLE

CENTER

OUTER

11

Load distribution in the pile group piles ("Outer" and "Corner") and single pile("Single"), assuming that the center piles ("Center") are fully shielded, andthat the outer piles are not shielded from the negative skin friction effect.Note, the effect of pile cap stiffness is not included in the foregoing.

30

35

40

45

DE

We can use our understanding to critically review design recommendations in current text books and standards. For example:

12

text books and standards. For example:

Page 72: Fellenius   bases de diseño de pilotes de fundación

3

A quote from a textbook *)

“The net effect negative skin friction is that the pile load capacity is reducedand pile settlement increases. The 'allowable load capacity' (sic!) is given as:”

negnegult

allow QF

QQQ −

−=

It could have been worse. Logically, the drag load should here been increased by a factor of safety. But so what there is little logic in

13

If you think this ghastly recommendation is correct, you have not been paying attention!

*) Compassion—perhaps misdirected—compels me not to identify the author

SF But so what, there is little logic in the approach anyway.

Do not include the drag load when determining the allowable load!

0

5

10

0 500 1,000 1,500 2,000 2,500

LOAD (KN)

TH (

m)

ALLOWABLE

LOAD - (Fs = 2.5)CAPACITY

Drag load must neither subtracted from the pile capacity nor from the allowable load

0

5

10

0 500 1,000 1,500 2,000 2,500

LOAD (KN)

TH (

m)

ALLOWABLE LOAD minus DRAGLOAD*1.0

CAPACITY

Effect of subtracting the drag load

14

10

15

20

DEP

T

DRAG LOAD

10

15

20

DEP

T

DRAG LOAD

INCREASE!If the pile capacity had been reduced with the amountof the drag load before subtracting the drag load, therewould have been no room left for the working load!

Similarly for the LRFD:

Do not include the drag load when determining the factored resistance!

Drag load not subtracted from the factored resistance Drag load factored and subtracted!

0

5

0 500 1,000 1,500 2,000 2,500

LOAD (KN)FACTORED RESISTANCE

CAPACITY

0

5

0 500 1,000 1,500 2,000 2,500LOAD (KN)

FACTORED RESISTANCEminus FACTORED DRAGLOADFactors = 0.6 and 1.5, respectively

FACTORED RESISTANCE CAPACITY

1515

10

15

20

DEP

TH (

m)

DRAG LOAD

10

15

20

DEPT

H (

m)

DRAG LOAD

If a factor of safety of 2.0 is applied and the drag load is subtracted from the allowable load . . . , then ?

The allowable load becomes zero!

Imagine a shaft-bearing pile (no toe resistance) with a certain capacity and an allowable load for a factor of safety of 2.0. In a settling soil, the drag load amounts to half the capacity value.

1616

Imagine that same pile designed for uplift: Logically, if one subtracts the drag load for the push case, should one not add it for the pull case ??!!??

Do you think that there is a difference in bearing capacity between an

ordinary precast and a prestressed pile? — Be the pile prestressed or not

prestressed, the prestress has nothing to do with the pile bearing capacity.

Load placed on a pile causes downward movements of the pile head due to:

1. 'Elastic' compression of the pile.

2. Load transfer movement -- the movement response of the soil.

3. Settlement below the pile toe due to the increase of stress in the soil. This isonly of importance for large pile groups, and where the soil layers below the pilesare compressible.

SETTLEMENT

1717

A drag load will only directly cause movement due to Point 1, the'elastic' compression. While it could be argued that Point 2 also is atplay, because the stiffness of the soil at the pile toe is an importantfactor here, it is mostly the downdrag that governs (a) the pile toemovement, (b) the pile toe load, and (c) the location of the neutralplane in an interactive — "unified" — process.The drag load cannot cause settlement due to Point 3, because there has been no stress change in the soil below the pile toe.

Negative-skin-friction/drag-load does not diminish

capacity. Drag load (and dead load) is a matter

for the pile structural strength, and the main

question is "will settlement that can cause

1818

downdrag occur around the pile(s)"? The

approach is expressed in “The Unified Design

Method”, which is a method based on the

interaction between forces and movements.

Page 73: Fellenius   bases de diseño de pilotes de fundación

4

The Unified Design Method is a three-step approach

1. The dead plus live load must be smaller than the pile capacitydivided by an appropriate factor of safety. The drag load is not included when designing against the bearing capacity.

1919

2. The dead load plus the drag load must be smaller than the structural strength divided with a appropriate factor of safety. The live load is not included because live load and drag load cannot coexist.

3. The settlement of the pile (pile group) must be smaller than a limiting value. The live load and drag load are not included in this analysis. (The load from the structure supported by the piles does not normally cause much settlement, but the settlement due to other causes can be large. The latter is called downdrag).

"

2020

Construing the Neutral Plane and Determining the Allowable Load

The distribution of load at the pile cap is governed by the load-transfer behavior of the piles. The “design pile” can be said to be the average pile. However, the loads can differ considerably between the piles depending on toe resistance, length of piles, spacing, etc.

2121

The location of the neutral plane is the result of Nature’s iterations to find the force equilibrium. If the end result — by design or by mistake — is that the neutral plane lies in or above a compressible soil layer, the pile(s) will settle even if the total factor of safety appears to be acceptable.

The principles of the mechanism are illustratedin the following three diagrams

2222

The mobilized toe resistance, Rt, is a function of the Net Pile Toe Movement

Pile toe response for where the settlement is small (1) and where it is large (2)

00 1,500LOAD and RESISTANCE

00

SETTLEMENT

21

NEUTRAL PLANE 1

Utimate Resistance

2323

DEP

TH

1 2

NEUTRAL PLANE 2

Toe Penetrations

Note, the magnitude of settlement affects not only the magnitude of toe resistance but also the length of the Transition Zone

= Movement into the soil

Pile toe response for where the settlement is small (1) and where it is large (2)

00 1,500LOAD and RESISTANCE

00

SETTLEMENT

21

NEUTRAL PLANE 1

Utimate Resistance

2424

DEP

TH

1 2

NEUTRAL PLANE 2

Toe Penetrations

Note, the magnitude of settlement affects not only the magnitude of toe resistance but also the length of the Transition Zone

1 TOE PENETRATION

TOE

RES

ISTA

NC

E 1

2

3

a b c

Page 74: Fellenius   bases de diseño de pilotes de fundación

5

25

0

5

10

0 10 20 30 40 50

FILL

Silty SAND

SAND

N

N (bl/0.3m); qt (MPa); wP, wn, and wL (%);

GW

Example of the Unified Design Approach as Applied to a Refinery Structure

Design for a large refineryexpansion was undertaken at asite reclaimed from a lake inthe 1960s. The natural soilsconsist of sand deposited onnormally consolidated, com-pressible post glacial lacustrineclay followed by silty clay till onlimestone bedrock found atabout 25 m to 30 m depth

Soil Profile

26

15

20

25

30

DEP

TH (

m)

Silty SAND

CLAY TILL

LIMESTONE BEDROCK

wn

CLAY

m ≈ 100

mr ≈ 600 ∆σ' ≈ 9 MPa

m ≈ 20

mr ≈ 200 ∆σ' ≈ 20 KPaw LwP

qt

about 25 m to 30 m depthbelow existing grade. The sitewill be raised an additional1.5 m, which will cause long-term settlement. Some of thenew units are 30 m to 70 m inheight and will be supported onpiles—several thousand in all.

Fellenius and Ochoa (2010)

40

60

80

n)

Results of an O-cell test on a 575-mmdiameter test pile, a 26 m deep boredcylindrical pile. A 1.5 m thick fill willbe placed over the site beforeconstruction. Piles are single or insmall groups.

Results of analysis of test data:Load Distributions

0

5

10

0 1,000 2,000 3,000 4,000 5,000LOAD (KN)

m)

O-cell Test

Strain-gage Value

"FlippedSilt

Sand

27

-60

-40

-20

0

20

40

0 500 1,000 1,500 2,000 2,500LOAD (kips)

MO

VEM

ENT

(in

9 %

15

20

25

30

DEP

TH (m

O-cell

Long-term. (After Completed Consolidation due to the Fill).

Clay

Till

0

100

200

3000 1,000 2,000 3,000 4,000 5,000

LOAD (KN)

DO

WN

WA

RD

M

OVE

MEN

T (m

m)

O-cell Testq-z extrapolation

0

5

0 2,000 4,000 6,000LOAD (KN)

SiltSand

0

5

0 2,000 4,000 6,000LOAD (KN)

SiltSand

Qd

Distribution of residual load in the pile after installation, but before load is applied to the pile.

Distribution of load in the pile immediately after the pile starts to sustain the load from the structure.

28

10

15

20

25

30

DEP

TH (m

)

O-cell

Clay

Till

Residual Load Distribution Before Construction

10

15

20

25

30

DEP

TH (m

)O-cell

Clay

Till

Load Distribution Immediately After Construction

Long-term load distribution

The shaft shear isassumed to be fullymobilized. However, thetoe resistance value touse is a function of the

0

5

10

0 2,000 4,000 6,000

LOAD (KN)

(m)

SiltSand

Cl

Qd

29

toe penetration due todowndrag and can onlybe determined fromassessing the soilsettlement distribution.

15

20

25

30

DEP

TH

O-cell

Clay

Till

Long-term Load Distribution

0

5

10

15

0 2,000 4,000 6,000LOAD (KN)

PTH

(m)

SiltSand

Clay

Qd

0

5

10

15

0 50 100 150 200

SETTLEMENT (mm)

PTH

(m)

0

5

10

15

0 2,000 4,000 6,000LOAD (KN)

PTH

(m)

SiltSand

Clay

Qd Pile Cap Settlement

Soil Settlement

Force and settlement (downdrag) interactive design. The unified pile design for capacity, drag load, settlement, and downdrag

30

20

25

30

DEP

O-cell

Till

Pile toe load in the load distribution diagram must match the toe load induced by the toe movement (penetration), which match is achieved by a trial-and-error procedure.

20

25

30

DEP

20

25

30

DEP

O-cell

Till

0

1,000

2,000

3,000

4,0000 50 100

TOE

LOAD

(KN

)

Pile toe load in the load distribution diagram must match the toe load induced by the toe movement (penetration), which match is achieved by a trial-and-error procedure. PILE TOE PENETRATION (mm)

q-z relation

Page 75: Fellenius   bases de diseño de pilotes de fundación

6

0

5

10

15

0 50 100 150 200

SETTLEMENT (mm)

PTH

(m)

0

5

10

15

0 2,000 4,000 6,000LOAD (KN)

PTH

(m)

SiltSand

Clay

Qd Pile Cap Settlement

Soil Settlement

Force and settlement (downdrag) interactive design. The unified pile design for capacity, drag load, settlement, and downdrag

31

20

25

30

DEP

20

25

30

DEP

O-cell

Till

0

1,000

2,000

3,000

4,0000 50 100

TOE

LOAD

(KN

)

Pile toe load in the load distribution diagram must match the toe load induced by the toe movement (penetration), which match is achieved by a trial-and-error procedure. PILE TOE PENETRATION (mm)

q-z relation

0

5

10

15

0 50 100 150 200

SETTLEMENT (mm)

PTH

(m)

0

5

10

15

0 2,000 4,000 6,000LOAD (KN)

PTH

(m)

SiltSand

Clay

Qd Pile Cap Settlement

Soil Settlement

Force and settlement (downdrag) interactive design. The unified pile design for capacity, drag load, settlement, and downdrag

Summary

32

20

25

30

DE

P

20

25

30

DE

P

O-cell

Till

0

1,000

2,000

3,000

4,0000 50 100

TOE

LO

AD

(K

N)

Pile toe load in the load distribution diagram must match the toe load induced by the toe movement (penetration), which match is achieved by a trial-and-error procedure. PILE TOE PENETRATION (mm)

q-z relation

The final solution is based on three "knowns": The shaft resistance distribution, the toe load-movement response, and the overall settlement distribution. Which all comes from basic site and project knowledge.

The Unified Design Analysis for load-transfer and long-term downdrag involves an iterative procedure applied to single piles and small pile groups

2. Soil settlement due to sustained pile load and changes of effective stress around the pile(s)due to other causes: Calculate and plot the distribution of soil settlement developing after thesustained load has been placed on the pile. For single piles and small pile groups, the settlementbelow the pile toe due to the sustained pile loads will be small, usually negligible. However, settlementdistribution due to increase of effective stress from other causes, such as fills, groundwater (pore

1. Load-transfer response: Calculate and plot the distribution of the shaft resistance. Determine —make an assumption on — the magnitude of toe resistance and toe movement that developed beforethe sustained load was placed on the pile. This requires applying a pile-toe load-movement relation.You need either to have measurement results showing the relation, or assume a q-z relation to use.Maybe you have the results of an O-cell test available. This analysis produces a preliminary location ofthe Neutral Plane, N.P.

33

In a routine case, it is usually sufficient to just make sure that the neutral plane lies below a levelindicating settlement that can be accepted. Moreover, when analyzing not just single piles or a fewpiles clustered together, but pile groups, matters can become more complicated.

distribution due to increase of effective stress from other causes, such as fills, groundwater (porepressure) changes, etc. could be substantial and must be calculated. At the N.P., the settlement of thepile(s) and the soil are equal. Determine now what increase of toe resistance the enforced extra piletoe penetration has resulted in and let an iterative set of calculations determine agreement betweenN.P. as force equilibrium and settlement equilibrium. This is established once the toe load and net toemovement (difference between the total toe movement and the soil settlement at the pile toe) fits thetoe relation the downdrag (i.e., pile settlement).

The Unified Design Analysis for Pile Groups

A large pile group within a footprint made up of one raft or more adjoining rafts can be defined a collection of piles in more or less perpendicularly placed rows of piles or small piled footings where the smallest number of rows is at least three, usually five or more. The load applied to the footprint of such groups could significantly increase the effective stress below the pile toe level and cause the soil to compress (and the pile group to settle).

The transfer of the stress from the load on the raft, rafts, or pile footings over the particular footprint will start at the N.P. First by shaft resistance and, finally, as toe resistance. The settlement between the N.P. and the pile toe level can normally be disregarded because the presence of the piles have created a very stiff unit of "reinforced soil" that will not compress appreciably. The key question is how the pile

34

very stiff unit of reinforced soil that will not compress appreciably. The key question is how the pile load will distribute between the N.P. and the pile toe level. The shaft response can be considered as a series of individual elements between the N.P. and the pile toe, each spreading the load at 2(V):1(H) from the pile raft, rafts, or footings to the pile toe level. Progressively, however, each such element along the pile will have a shorter distance to the pile toe, and, therefore affect a smaller footprint. The pile toe resistance, of course, acts right a the pile toe. This series of stress footprints can be approximated to an equivalent raft at the N.P. with the footprint of the piled raft, rafts, or footings that spreads the total load at 5(V):1(H) to the pile toe level. From the pile toe level, the stress is distributed by either 2(V):1(H) for the average settlement of by Boussinesq distribution for calculation of the settlement at different locations within the pile group. Note, the drag load must not be included in the analysis of settlement.

Settlement Analysis of Large Pile Groups by the Equivalent Footing Method

0 300 600 900 1,200

LOAD (KN)

Qd+Qn alternatives

Qd0

5

10

0 300 600 900 1,200

LOAD (KN)

Qd60

80

AT

TOE

#7

Qd on Equiv. Raft Projected

35

DEP

TH (

m)

Ru-Rs

Rt

Neutral PlaneEquivalent Raft8m x 12 m

15

20

25

30

35

40

DEP

TH (

m)

Rt

Qd#1

#2#3

#4#5

#6#7

The Qd transferred to the soil in several steps along the pile from the neutral plane to the pile toe

0

20

40

-15 -10 -5 0 5 10 15 20

STR

ESS

A

AVERAGE WIDTH (m)

#2

#3

#4

#5

#6

#1

Qd on Equiv. Raft Projected 2(V):1(H)

5(V):1(H)

Pile Group F t i t

Settlement Analysis of Large Pile Groups by the Equivalent Footing Method

40

60

80

AT

TOE

#7

Qd on Equiv. Raft Projected 5(V):1(H)

36

5(V):1(H)

2(V):1(H) or Boussinesq

Neutral Plane

Footprint

Pile Toe Depth

Footprint Projected 5(V):1(H) to form an Equivalent Raft

Projection of Raft for Settlement Analysis

0

20

40

-15 -10 -5 0 5 10 15 20

STR

ESS

AVERAGE WIDTH (m)

#2

#3

#4

#5

#6

#1

Qd on Equiv. Raft Projected 2(V):1(H)

Page 76: Fellenius   bases de diseño de pilotes de fundación

7

Settlement Analysis of Large Pile Groups by the Equivalent Raft Method

soilsoilpilepile EAEA +The compressibility in this

Equivalent Footing placed at the Location of the Neutral Plane

G.W

FILLS, etc.

5:1 5:1

Start by placing an "Equivalent Raft" at the

depth of the Neutral Plane

37

soilpile

soilsoilpilepilecombined AA

E+

=The compressibility in this zone must be of soil and pile combined

2:1 distribution 2:1 distribution

Settlement of the piled foundation is caused by the compression of the soil due to increase of effective stress below the neutral plane from external load applied to the piles and, for example, from fills, embankments, loads on adjacent foundations, and lowering of groundwater table.

5:1 5:1

The approach is far beyond the 1948 Terzaghi and Peck approachof placing The Equivalent Raft at the lower third depth

Liquid storage tank in Tessaloniki, Greece (Savvaidis 2009)

38

-20

-15

-10

-5

0

5

10

15

20

-20 -15 -10 -5 0 5 10 15 20

East-West

Nor

ht-S

outh

Pile 11

Pile 16

Pile 7

112 1.0 m diameter, bored piles installed to 42 m depth

Dense, silty sand to 50+ m depth Settlement

No Settlement

0

10

0 5 10 15 20 25 30 35 40

ACROSS THE DIAMETER (m)

NT

(mm

)

Settlement measured across a diameter during a 30 Hydro Test

39

20

30

40

SETT

LEM

EN

Curve calculated for a flexible footing locatedat the pile toe level with parameters fitted tothe settlement measured at the tank mid-point

0

5

10

0 5 10 15 20 25 30 35 40

CONE STRESS, qc (MPa)

CLAYEY SAND

Ghent Grain Terminal — Settlement of a large pile group(Goossens and VanImpe, 1991)

85 m

34 m41 x 17 = 697 PILES

B

PILE GROUP CASE HISTORYFootprint ratio = 9 %

40

15

20

25

30

35

40

DEO

PTH

(m

)

CLAY

SAND

CLAY

Very dense SAND

0

500

1,000

1,500

2,000

2,500

0 2 4 6 8 10

MOVEMENT (mm)

LOA

D (

KN)

Pile #585

Pile #085

Can we use the results of the two static loading tests to estimate the settlement of the pile group?

0

50

NT

(mm

)

770 days

1 080 days

Footprint of Silo Foundation84 m by 34 m

BM 4 BM 2A BM 2 BM 1 BM 3

0

50

100

T (m

m) Measured and

calculated at the benchmarks

Footprint of Silo Foundation84 m by 34 m

BM 4 BM 2A BM 2 BM 1 BM 3

41Center to corner differential settlement is 0.25÷45 ≈ 1:200

100

150

200

SETT

LEM

EN

1,080 days1,245 days

1,960 days2,637 days3,471 days3,808 days

150

200

250

300

SETT

LEM

EN

benchmarks

Calculated value fitted to measured

Calculated for center line points

Calculated

42

Settlement of a Pile Group Supporting Five Furnaces at QIT Plant, Sorel, Quebec

Golder, H.Q. and Osler J.C., 1968.Settlement of a furnace foundation, Sorel, Quebec.Canadian Geotechnical Journal 5(1) 46-56.

Page 77: Fellenius   bases de diseño de pilotes de fundación

8

0

500

1,000

1,500

2,000

0 1 2 3 4

MOVEMENT (mm)

LOA

D (

KN

)

#1 #2 #3 #4 #5

54 m

16 m

NORTH SOUTH

Static loading test used to predict settlement of the five furnaces: 10 mm

v

v

v

vv v v v v v v v

v

v

10 m

16 m

6 m Pile Embedment Pile Toe at 8.5 m Depth

LAYOUT OF ONE FURNACE

Footprint ratio = 7 % (28 %?)

43

0

20

40

60

80

SETT

LEM

TN (

mm

)

Apr. 1951 Nov. 1951

Aug. 1952

Jan. 1962

Furnace #1 Furnace #2 Furnace #3 Furnace #4 Furnace #5

Measured Settlement24 m of Compact SAND50 m Champlain CLAY

0.60

0.80

1.00

1.20

10 100 1,000 10,000

Stress (KPa)

Voi

d R

atio

(- -

)

CR = 0.026

mr = 90

CR = 0.257 m = 9

DEPTH = 14 mσ'0 = 230 KPaσ'c = 280 KPa

0

10

20

30

40

50

60

70

80

YEARS

SETT

LEM

ENT

(mm

)

1950 1955 1960 1965

North and South Side Furnaces

CenterFurnaces

0

10

20

30

0 25 50 75 100 125

SETTLEMENT (mm)

DEP

TH (

m)

Center of Furnace Row

Inside edge of Furnace #2

SANDCLAY+SAND

SAND

SANDY CLAY

CHAMPLAINCLAY

Outside edge of Furnaces #1 and #5

Between Furnaces#1 & #2 and #4 and #5

44

40

50

60

0

20

40

60

80

SETT

LEM

TN (

mm

)

Furnace #1 Furnace #2 Furnace #3 Furnace #4 Furnace #5

Nov. 1951

Aug. 1952

Jan. 1962

CALCULATED SETTLEMENT

SINCE APRIL 1951

Be the one of the pack to dareto design for settlement rather than "capacity"

45

Piled foundations in current codes

The Canadian Building Code and Highway Design Code (1992), as well as the Hong Kong Code (Geo Guide 2006) apply the Unified Design method. That is, the drag load is only of concern for the structural strength of the pile. Indeed, the Canadian Highway Code even states that for piles with an aspect ratio (embedment depth over diameter, D/b), smaller than 80, the design does not have to check for drag load. However, the design must always check for downdrag.

The Manual of US Corps of Engineers indicate a similar approach (but less explicit), stating that the drag load constitutes a settlement problem (as opposed to a bearing capacity problem).

4646

The ASCE “Practice for the Design and Installation on Pile Foundations (2007)” includes the following definitions:

DOWNDRAG: The settlement due to the pile being dragged down by the settling of surrounding soil;

DRAG LOAD: Load imposed on the pile by the surrounding soil as it tends to move downward relative to the pile shaft, due to soil consolidation, surcharges, or other causes.

and the following statement: . . . , the allowable load, as well as the pile embedment depth, is governed by concerns for settlement and downdrag, and by concern for structural strength for dead load plus drag load, rather than by bearing capacity.

The FHWA has produced one of the most extensive recent guidelines document. The full reference is: Report No. FHWA-NHI-05-042, Design and Construction of Driven Pile Foundations - Volume I and II. National Highway Institute, Federal Highway Administration, U.S. Department of Transportation, Washington, D.C., April 2006. 1,450 pages.

The current issue, drag load and downdrag, is covered in about 20 of the total number of pages. in all essential parts, the FHWA document adheres to the principles of the Unified Design Method.

The FHWA document indicates the following criteria for identifying a drag load and/or downdrag problem. If any one of these criteria is met, drag load or downdrag shall be considered in the design.

The criteria are:

4747

1. The settlement of the ground surface (after the piles are installed) will be larger than 10 mm (0.4 in) *).

2. The piles will be longer than 25 m (82 ft).

3. The compressible soil layer is thicker than 10 m (33 ft).

4. The water table will be lowered more than 4 m (13 ft).

5. The height of the embankment to be placed on the ground surface exceeds 2 m (6.5 ft).

*) This must not be taken to mean that negative skin friction would not develop unless the settlement is larger than 10 mm (0.5 inch)! On the contrary, both positive shaft resistance and negative skin friction are often mobilized at a movement between the pile and the soil as small as ≈2-3 mm.

The trend is toward Load and Resistance Factor Design(LRFD). The Canadian Highway Code has been based on LRFD for about 20 years. With regard to the drag load and downdrag issue, the Canadian Code follows the unified design method.

4848

Since 1995, the Australian Piling Standard is also a Limit States Design Code (LRFD), and, like the Canadian Code, the recommendation for the design of piled foundations is according to the Unified Method, as quoted in the following.

Page 78: Fellenius   bases de diseño de pilotes de fundación

9

The Australian Piling Standard, AS 2159—1995

3.3.2 Load combinations for strength design The load combinations for strengthdesign shall be as follows:

(a) The design load for ultimate strength design of piles shall be the combination of factored loads which produces the most adverse effect on the pile in accordancewith AS 1170.1

(b) If there are loads induced by soil movement (see Clause 3.3.1.2), they shall becomputed as follows:

49

(i) Design structural strength (see Clause 4.3.5)—determined as follows:(A) 1.2 Fnf — negative friction loads (i.e., drag load).(B) 1.5 Fes — compressive and tensile loads(C) 1.5 Fem— bending moments, shear forces, and axial loads.

(ii) Design geotechnical strength—loads induced by soil movement shall not be taken into account. (EDITORIALLY CORRECTED: axial loads

induced by soil movement shall not be included)

4.3.5 Negative friction In the absence of other information, the geotechnical strength in compression or uplift shall be assumed to be unaffected by negative frictionand shall be computed as set out in Clauses 4.3.1 and 4.3.2 for a single pile, andClause 4.3.3 for a pile group.

The additional axial forces induced in a pile by negative friction shall be considered inthe structural design of the pile.

4.5.3 Settlement Consideration shall be given to the settlement of both a pile and a pile group resulting from effects caused by settlement of the surrounding ground NOTE: In the absence of an analysis in

The Australian Piling Standard, AS 2159—1995

50

from effects caused by settlement of the surrounding ground. NOTE: In the absence of an analysis in which pile-soil interaction is allowed for, the settlement of a pile or pile group subjected to negative friction may be approximated as the greater of the following:(a) The settlement of the ground at the ‘neutral plane’ in the ground, that is the depth at whichthe shaft friction on the pile changes from negative (downward) to positive (upward). Applied compressive loading tends to raise the ‘neutral plane’ and increase the settlement of the pile or pile group.(b) The sum of the following three components:

(i) the compression of the pile shaft due to the design action;(ii) the compression of the pile shaft due to the computed forces arising from negative friction; (iii) the settlement of the portion of the pile shaft in the ‘stable’ soil (the part of the soil profile not

subjected to movement) under the sum of the design action and the maximum computed forcein the pile arising from negative friction.

As many other codes and standards, the Australian Standardcan go overboard with some details

TABLE 4.1RANGE OF VALUES FOR GEOTECHNICAL STRENGTH REDUCTION FACTOR

Method of assessment of ultimate geotechnical strength Range of vStatic load testing to failure 0.70Static proof (not to failure) load testing 0.70Dynamic load testing to failure supported by signal matching 0.65Dynamic load testing to failure not supported by signal matching 0.50Dynamic proof (not to failure) load testing supported by signal matching 0.65

Dynamic proof (not to failure) load testing not supported by signal matching (!) 0 50

51

Dynamic proof (not to failure) load testing not supported by signal matching (!) 0.50

Static analysis using CPT data 0.45

Static analysis using SPT data in cohesionless soils (!) 0.40Static analysis using laboratory data for cohesive soils 0.45

Dynamic analysis using wave equation method (!) 0.45

Dynamic analysis using driving formulae for piles in rock (!) 0.50

Dynamic analysis using driving formulae for piles in sand (!) 0.45

Dynamic analysis using driving formulae for piles in clay (!)

Measurement during installation of proprietary displacement piles,using well established in-house formulae 0.50

As many other codes and standards, the Australian Standardcan go overboard with some details

TABLE 4.1RANGE OF VALUES FOR GEOTECHNICAL STRENGTH REDUCTION FACTOR

Method of assessment of ultimate geotechnical strength Range of valuesStatic load testing to failure 0.70–0.90Static proof (not to failure) load testing 0.70–0.90Dynamic load testing to failure supported by signal matching 0.65–0.85Dynamic load testing to failure not supported by signal matching 0.50–0.70Dynamic proof (not to failure) load testing supported by signal matching 0.65–0.85

Dynamic proof (not to failure) load testing not supported by signal matching (!) 0 50 0 70

52

Dynamic proof (not to failure) load testing not supported by signal matching (!) 0.50–0.70Static analysis using CPT data 0.45–0.65

Static analysis using SPT data in cohesionless soils (!) 0.40–0.55Static analysis using laboratory data for cohesive soils 0.45–0.55

Dynamic analysis using wave equation method (!) 0.45–0.55

Dynamic analysis using driving formulae for piles in rock (!) 0.50–0.65

Dynamic analysis using driving formulae for piles in sand (!) 0.45–0.55

Dynamic analysis using driving formulae for piles in clay (!)

Measurement during installation of proprietary displacement piles,using well established in-house formulae 0.50–0.65

The Euro CodeThe European Community has recently completed EuroCode 7, which issupposed to be adopted by all member states. The EuroCode treats the dragload as a load acting similarly to the load from the structure, and requires it to beadded to that load (or subtracted from the pile capacity). Moreover, the shaftresistance in the soil layer that contributes to the drag load is disregarded whendetermining the pile resistance. That is, when a capacity has been determinedto, say, 1,000 and the drag load is expected to be, say, 400, the usable capacityis 1,600 and the usable unfactored resistance is a mere 1,600. This value isthen factored and reduced by the factored drag load. If resistance factor anddrag load factors are say 0 5 and 1 5 respectively the amount left is 200! What

5353

Unfortunately, the recently issued AASHTO LRFD Specs have adopted the EuroCode approach! A few US State DOTs, e.g., Utah, have wisely rejected the AASHTO Specs and apply the Unified Method.

drag load factors are, say, 0.5 and 1.5, respectively, the amount left is 200! What“salvages” the economy of some designs is that the EuroCode clausesadvocate that the designer maintain the faithful approach that “the drag loadcannot really be that large, can it, please?” to determining the magnitude of thedrag load. Incredibly, the EuroCode says little on how to calculate settlement ofpiled foundations and nothing is stated about downdrag!

5.0 m

SOFT CLAY

SILTY CLAY

11.5 m

FILL

Average unit shaft resistance, rs = 20 KPa

Rs = 94.2 KN; Rs = Qn

Average rs = 50 KPa

Rs = 543 KN fq*300 + fn*94 ≤ 543/fr

Q (unfactored) = 300 KN

Eurocode Guide , Example 7.4 (Bored 0.3 m diameter pile)

CALCULATIONS

and AASHTO Specs example

5454

"The settlement due to the fill is sufficient to develop maximum negative skin friction in the soft clay ".�

1.35*300 + 1.35*94 ≤ 543/1.0

532 ≤ 543

(Alternative: If fr = 1.1, the length in the silty clay becomes 12.4 m)

Rt = 0 KN ?!

The Guide states that the neutral plane lies at the interface of the two clay layers, which based on the information given in the example, cannot be correct. But there is a good deal more wrong with this “design” example.

The Guide states that the two rs-values are from effective stress calculation. The values correlate to soil unit weights of 18 KN/m3 and 19.6 KN/m3, ß-coefficients of 0.4 in both layers with groundwater table at ground surface, and a fill stress of 30 KPa.

Page 79: Fellenius   bases de diseño de pilotes de fundación

10

Analysis using the same numerical values for the pile shaft, but including the benefit of a small toe resistance

0

5

10

0 200 400 600 800 1,000LOAD (KN)

EPTH

(m

)

Fs = 2.50

5

10

SETTLEMENT (mm)

EPTH

(m

)

NeutralPlane

THE KEY QUESTION:

?

5555

If the settlement is acceptable, there may be room for shortening the pile or increasing the load. That would raise the location of the neutral plane. Would then the pile settlement still be acceptable?

15

20

DE Maximum

Load = 500 KNQn = 200 KN not 94 KN

Rf = 760/1.35 KN > 1.35*300 KN

Rf = 560 KN > 405 KN

Rt

125 KN

= Factored resistance

15

20

DE

Toe Movement

THE KEY QUESTION:is the settlement acceptable?

5656

TYPICAL EXAMPLEAn 84 m (275 ft) wide LNG tank is founded on 1,200 400 mm (16 in) driven piles at c/c 5.25b (footprint ratioof 3.5 %). The soil profile consists of 25 m of normally consolidated moderately compressible clay on 10 mof dense sand (with artesian pore pressure) followed by 25 m of moderately compressible, slightlypreconsolidated clay on very dense gravel at 60 m depth. A fill is placed under and around the tank to raisethe ground by one metre.

0

5

10

0 500 1,000 1,500 2,000 2,500 3,000 3,500 4,000

LOAD (KN)

CLAYQd

FILL

TestCondition

2,000

2,500

3,000

N)

Pile Head

Offset Limit2,300 KN

Pile Toe Mvmnt vs. Load at Head

Pile Shortening

57

15

20

25

30

35

40

DEP

TH (

m)

SAND

CLAY

Long-termCondition

0

500

1,000

1,500

0 5 10 15 20 25 30

MOVEMENT (mm)

LOA

D (

KN

Pile Shaft

Pile Toe unaffected by residual load

Pile Toe Mvmnt vs. Load at Toe

vs Mvmnt at Head

Load-movement curves from a static loading test Short and long term load distributions

SETTLEMENT OF A SINGLE PILE OR SMALL PILE GROUP OUTSIDE THE MAIN GROUP

0

10

20

0 1,000 2,000 3,000 4,000

LOAD (KN)

Long-termQd

0

10

20

0 25 50 75 100 125 150

SETTLEMENT (mm)

CLAY

FILL

Soil

Pile

Neutral Plane

58

30

40

50

60

70

DEP

TH (

m) 30

40

50

60

70

DEP

TH (

m) SAND

CLAY

GRAVEL

SETTLEMENT OF THE PILED FOUNDATION

05

10152025

0 5 10 15 20 25 30 35

DAYSWA

TER

HEI

GH

T (m

)

HYDRO TEST

0

100

200

0 10 20 30 40 50

TIME (years)

T (m

m)

LONG-TERM SETTLEMENTS OF THE PILED TANK FOUNDATION

Only Fill;Away from the tank

Tank Perimeter

59

DAYSW

0

2040

6080

0 5 10 15 20 25 30 35

SETT

LEM

ENT

(mm

)

200

300

400

500

SETT

LEM

ENT

Tank Center

A recent modern application of a piled pad foundation is the foundations for the Rion-Antirion bridge piers (Pecker 2004). Another is the foundations of the piers supporting the Golden Ears Bridge in Vancouver, BC (Sampaco et al.; Naesgaard et al. 2012), pictured below.

60

Page 80: Fellenius   bases de diseño de pilotes de fundación

11

Piled pad foundation piers supporting the Golden Ears Bridge in Vancouver, BC.

Bored piles (900 mm; 8 m) to provide lateral resistance

and

driven (300 mm; 30 m)piled-pad piles

BRIDGE DECK

FOOTING AND PILE CAP Sh t

61

over an about 100 m thick deposit of soft compressible clay

FOOTING AND PILE CAP

Longslenderpiles

Shortboredpile

Pad

ShinHo and MyeongJi Housing Project,in the estuary of the Nakdong River, Pusan, Korea

Project Managers: Drs. Song Gyo Chung and Sung Ryul Kim, Dong-A University, Busan

62

63 64

65

AIR VIEW(Shinho Site)

66

Page 81: Fellenius   bases de diseño de pilotes de fundación

12

SITE PLAN (SH Site)

67

Silty clay

0

10

20

30

0 10 20 30Cone Stress, qt (MPa)

EPTH

(m

)

0

10

20

30

0 25 50 75 100

Sleeve Friction, fs (KPa)

PTH

(m

)

0

10

20

30

0 500 1,000 1,500

Pore Pressure (KPa)

EPTH

(m

)

0

10

20

30

0 1 2 3 4 5

Friction Ratio, fR (%)

EPTH

(m

)

Profile

FILL

Silty CLAY(marine)

68

40

50

60

DE

40

50

60

DE

40

50

60

DE

40

50

60

DE

SILT&CLAY

Very dense SAND

SAND

CPTU sounding at the location of the O-cell

0

10

20

0 10 20 30Cone Stress, qt (MPa)

EPTH

(m

)

0

10

20

0 200 400

Sleeve Friction (KPa)

PTH

(m

)

0

10

20

0 250 500 750 1,000

Pore Pressure (KPa)

PTH

(m

)

0

10

20

0 1 2 3 4 5

Friction Ratio (%)

EPTH

(m

)

Profile

Mixed

CLAY

6905-08-08 Myeongji Site C-block

30

40

50

DE

30

40

50

DE

30

40

50

DE

30

40

50

DE

SAN

Reduced pore pressure (“dilation”)

SAND

The pile considered is a 600 mm diameter cylinder pile with a 100 mm wall driven closed-toe

The questions to resolve in the design are

1 What is the capacity in the different layers?

70

1. What is the capacity in the different layers?

2. What is the depth to the force equilibrium/settlement equilibrium, i.e., the neutral plane

3. What will be the maximum load in the pile? Is the structural strength adequate?

4. What is the settlement of the pile as a function of the location of the neutral plane.

0

5

10

15

0 500 1,000 1,500 2,000 2,500 3,000

LOAD and RESISTANCE (KN)

)

0

5

10

15

0 10 20 30 40 50 60 70 80

SETTLEMENT (mm)

)

SETTLEMENT OF PILE HEAD

PILE "CAPACITY"

DEAD LOAD

The Unified Method for Design of Piled Foundations(typical only)

7171

20

25

30

35

40

45

DEP

TH (

m)

20

25

30

35

40

45

DEP

TH (

m)

NEUTRAL PLANE

TOE MOVEMENT THAT MOBILIZES THE TOE

RESISTANCE

TOE RESISTANCE

DRAGLOAD

*) Portion of the toe resistance will have developed from the driving

*)

O-cell TestFor Pile Toe Response and to "Open up" the Pile Toe,i.e., remove pile Toe Resistance for the Subsequent Head-Down Test

20

25

30

T (m

m)

The pile head did not move

2nd Cycle

For Pile Toe Response and to "Open up" the Pile ToeSo that toe resistance is removed

72-90

-60

-30

0

30

0 1,000 2,000 3,000 4,000 5,000 6,000

LOAD (KN)

MO

VEM

ENT

(mm

)

Downward

Upward

1st Cycle

2nd Cycle

0

5

10

15

UPW

AR

D M

OVE

MEN

T did not move. A 16 mm pile compression of the shaft

for decreasing load is not realistic.

1st Cycle

Pile Toe Broke

So that toe resistance is removed from the subsequent head-down Test

Page 82: Fellenius   bases de diseño de pilotes de fundación

13

0

10

20

-5,000 0 5,000

LOAD 2nd TOE-UP (KN)

(m)

0

10

20

-5,000 0 5,000

LOAD 1st TOE-UP (KN)

(m)

73

30

40

50

60

DEP

TH (30

40

50

60

DEP

TH ( 5 000

6,000

7,000

8,000

9,000

10,000

OW

N T

ESTS

(K

N)

Now The Head-down Test

74

0

1,000

2,000

3,000

4,000

5,000

0 10 20 30 40 50 60 70 80 90

MOVEMENT (mm)

LOA

D H

EAD

-DO

First Head-down Test

40

50

60

ANG

E O

F ST

RAIN

, Mt

SG-12 CD

SG-12 AB

SG 11

SG-10

SG-9

SG-8

The Shinho test pile — head-down test

75

0

10

20

30

0 500 1,000 1,500

STRAIN (µε)

CHA

NGE

OF

STRE

SS/C

HA(G

Pa)

Q =A(-0.0035(µε)2 + 29µε)

0

10

20

0 2,000 4,000 6,000 8,000 10,000

LOAD, 2nd HEAD-DOWN (KN)

)

ß = 1.0

ß = 0.4 (0.25

ß = 0.1(0 1)

RESIDUAL (maximum)

76

30

40

50

60

DEP

TH (

m

ZERO LINE IS AT START OF 2ND HEAD-DOWN TEST

(0.1)

ß = 0.7(0.2)

ß = 0.3 (0.1)

TRUE RESISTANCE (for maximum residual load)

After Unloading

The shaded force area corresponds to a shortening of just about 3 mm

PRESUMED RESIDUAL LOAD AT START OF O-CELL TEST

Estimated Residual Load Distribution at Start of the O-cell Test

0

10

20

30

0 2,000 4,000 6,000 8,000 10,000 12,000 14,000

RESISTANCE and LOAD (KN)

TH (

m)

Qd ≈RULT

77

40

50

60

DEP

T

Qn

Shinho Pile

Long-term resistance and load distributions at the Shinho site

This has been a long day with lots of material and a sometimes heavy message I am afraid I just hope that I

78

message, I am afraid. I just hope that I have not overloaded you.

Page 83: Fellenius   bases de diseño de pilotes de fundación

14

79

The New International Airport, Bangkok Thailand

Data from: Fox, I., Due, M. and Buttling,S. (2004) and Buttling, S. (2006)

THAILAND

8080

Current and Future Pore Pressure Distribution

0

5

10

15

20

25

0 100 200 300 400 500

Pore Pressure (KPa)

pth

(m)

0

10

20

1975 1980 1985 1990 1995 2000 2005 2010

YEAR

er T

able

(m

)

DesignPhase

ConstructionPhase

Nearby Observations of Groundwater Table

81

30

35

40

45

50

Dep

Long-Term

Short-Term (Current)

30

40

50

60

70

Dep

th to

Gra

ounw

ate

Pumping (mining) of groundwater has reduced the pore pressures. At the start of the design process, pumping in the area was stopped.

82

The clay is soft and normally consolidated with a modulus number smaller than 10.

All foundations — the trellis roof, terminal buildings, concourse, walkways, etc. —are placed on piles. The stress-bulbs from the various foundations will overlap each other’s areas resulting in a complicated settlement analysis.

Several static loading tests on instrumented piles were performed to establish the load-transfer conditions at the site at the time of the testing, i.e., short-term conditions. Effective stress analysis of the test results for the current pore pressures established the coefficients applicable to the long-term conditions after water tables had stabilized.

83

A total of 25,000+ piles were installed.

The design employed the unified pile design method.

Example of resistance distribution for 600 mm diameter bored pile installed to a 30 m embedment depth.

0

10

LOAD (KN)

(m)

Qd = 1,040 KN RULT = 2,870 KNFs = 2.0

Short-Term

Fs = 2.0 on long-term capacity

0

10

LOAD (KN)

m)

Long-Term

Qd = 1,040 KN RULT = 2,160 KNFs = 2.0

84

The extensive testing and the conservative assumption on future pore pressures allowed an Fs of 2.0. The structural strength of the pile is more than adequate for the load at the neutral plane: Qd + Qn ≈ 1,500 KN.

20

30

DEPT

H (

Qn = 770 KN

20

30

DEPT

H (

m

Qn = 500 KN

Clay

Sand

Page 84: Fellenius   bases de diseño de pilotes de fundación

15

The settlements for the piled foundations were calculated to:

Construction Long-term TotalTrellis Roof Pylons 20 mm 90 mm 110 mm

Terminal Building 30 15 45

85

Concourse 35 20 55

* * *

0

5

10

15

0 20 40 60 80 100

Soft Clay, compressible

Sand and Gravel

Highway Viaduct over

Railroad

(m

)

Milford, Beaver County, Utah

12.75-inch Diameter 0.5-inch Wall

Pipe Piles

Driven closed-toe to52 ft (16 m) embedment

86

20

25

30

35

40

Sand

DEP

TH To be concrete-filled

Load at SLS = 240 kips 1,068 KN

Required Factored Resistance = 540 kips

2,400 KN

0

5

10

15

0 20 40 60 80 100Cone Stress, qt (MPa)

(m)

0

5

10

15

0 500 1,000

Sleeve Friction, fs (KPa)

m)

0

5

10

15

0 500 1,000

Pore Pressure (KPa)

(m)

0

5

10

15

0 1 2 3 4 5

Friction Ratio, fR (%)

(m)

Profile

CPTU Sounding Results

87

20

25

30

35

40

DEP

TH

20

25

30

35

40

DE

PTH

(

20

25

30

35

40

DE

PTH

(

20

25

30

35

40

DE

PTH

(

Profile0

5

10

15

0 2 4 6 8 10Cone Stress, qt (MPa)

Enlarged Cone Stress Scale Soil Profiling Chart

88

15

20

25

30

35

40

DE

PTH

(m

)

“Correlation” CPT - SPT

0

5

10

0 50 100

Cone Stress, qt (MPa)

1.5

2.0

2.5

Blow

s)

Utah case

Florida case

8989

10

15

20

25

30

35

DEP

TH (

m)

0.0

0.5

1.0

0.00 0.50 1.00 1.50 2.00

Mean Particle Size (mm)

q c/N

(M

Pa/B

S A N DFine Medium Coarse

0

2

4

6

0 100 200 300 400

Unit Shaft Resistance (KPa)

m)

ß= 1.2

ß= 0.5

0

2

4

6

0.00 0.50 1.00 1.50 2.00

Equivalent ß (- - -)

m)

90

8

10

12

14

16

18

20

DE

PTH

(m

LCPC and Schmertmann

ß= 1.2

ß= 0.80

E-F andß-Method

8

10

12

14

16

18

20

DEP

TH (

m

Page 85: Fellenius   bases de diseño de pilotes de fundación

16

0

2

4

6

8

0 500 1,000 1,500 2,000

Shaft Resistance (KN)

H (

m)

0

2

4

6

8

0 2,000 4,000 6,000Total Resistance (KN)

H (

m)

Required unfactored capacity

91

10

12

14

16

18

20

DEP

TH

E-F andß-Method

LCPC and Schmertmann

10

12

14

16

18

20

DEP

TH

LCPC E-F

0

5

10

15

0 10 20 30 40 50 60Cone Stress, qt (MPa)

(m)

qt filtered

qt

0

5

10

15

0 100 200 300 400 500 600 700 800Modulus Number, m)

(m)

LAB. TESTS, Oedometer

92

20

25

30

35

DEP

TH (

qt filtered and depth adjusted

20

25

30

35

DEP

TH

Filtered and unfiltered MODULUS NUMBER

0

5

10

15

0 100 200 300 400 500 600

Modulus Number, m Settlement (mm)

(m)

SETTLEMENT

93

20

25

30

35

DEP

TH (

MODULUS NUMBER

A repeat: Distribution of unit shaft shear and of load and resistance

SHAFT SHEAR LOAD

Settling Soil

Qd

9494

DEP

TH (–)

(+)

DEP

TH

Soil

Non-Settling

Soil

The shear force along the pile in a swelling soil is the opposite to that insettling soil, of course — "positive skin friction" as opposed to "negative skinfriction". But the same analysis method applies.

How would the distributions look for a pile in a swelling soil?

SHAFT SHEAR

Swelling Soil

NEGATIVE POSITIVE

PileLOAD

(+)

Qd

TENSION

0

95

Distributions of unit shaft shear

DEP

TH

(+)

(–)

Non-Swelling

Soil

A

and load for a pile in swelling soil

DEP

TH

(–)

(+)

COMPRESSION

BToe Load = 0

DEP

TH

Swelling Soil

Non-

(–)

Qd TENSION 0 COMPRESSION

Pile in swelling soil loaded in uplift Tension load

96

D

Swelling Soil, but Settling

Soil,perhaps

So, what does it mean that a pile loaded in tension in swelling soil can have a neutral plane in settling soil below the swelling soil?

Page 86: Fellenius   bases de diseño de pilotes de fundación

17

Conventional piled foundations with floor supported on the piles or as a ground slab

Piled Raft and Piled Pad Foundations

9797

Piled raft foundation with loads supported by contact stress and piles

Remaining load on raft evenly distributed as contact stress

Evenly distributed load on the raft supported by evenly distributed piles (Fs = 1.0)

Uneven load on raft supported by the piles

(Fs = 1.0)

9898

Piled pad foundation with loads supported by contact stress and piles

Engineered Backfill

Conventional raft or mat Geotextile

9999

The exception to this is in the case of a piled raft, which is a term referring to a piled foundation designed with a factor of safety for the piles of close to unity, or better expressed: The neutral plane is designed to be located close to or at the

At the level of the pile cap, there is no contact stress between the underside of the pile cap and the soil, because the soil will always settle more than the pile cap. Therefore, it is incorrect to allow any contribution from contact stress.

Comments on Contact Stress, Piled Raft, and Piled Pad

100100

better expressed: The neutral plane is designed to be located close to or at the underside of the raft. Only if the external loads on the pile cap are equal to or larger than the combined pile capacities will there be a contact stress.

The emphasis of the design for a piled raft is on ensuring that the contact stress is uniformly distributed across the raft. The piled-raft design intends for the piles to serve both as soil reinforcing (stiffening) elements reducing settlements and as units for receiving unavoidable concentrated loads on the raft. This condition governs the distribution across the raft of the number and spacing of the piles.