Chapter111 AbutmentsA11y
Chapter111 AbutmentsA11y
1 • October 2022
11.1.1 INTRODUCTION
Abutments are the substructure components at the ends of a bridge used to transfer the
loads from the superstructure to foundations, support approach slabs, and retain the
approach embankment. In the first part of this chapter, common types of abutments and
basic aspects of abutment design according to AASHTO LRFD Bridge Design
Specifications, 8th Edition with California Amendments, referred to herein as AASHTO-
CA BDS-8 (AASHTO, 2017; Caltrans, 2019a) are discussed. Subsequently, a design
example of the short seat (non-integral) abutment is presented to illustrate the typical
design procedure.
Diaphragm Seat
Bin Closure
The general detailing of abutments is covered in Bridge Design Details (BDD) Chapter 6.
wingwall
shear key
backwall
footing
stem
Furthermore, sacrificial components of abutments such as backwalls and shear keys shall
be designed in accordance with SDC and AASHTO-CA BDS-8 requirements. Refer to
Article 3.4.5.2 for height limitations associated with this provision. The dynamic allowance
(IM) of the live load is disregarded for non-integral abutments refer to Article 3.6.2.1
(AASHTO-CA BDS-8).
including shear keys, is assumed to be uniformly distributed along the abutment width. In
the case of non-integral abutments, only reaction forces (vertical and horizontal) are
applied to the abutments. However, moments are also transferred from the superstructure
to the abutment for integral abutments. Figure 11.1.3-1 shows typical forces acting on a
seat-type abutment.
LS
DCsup
DW
LL
PS
BR
CE
PS
CR Total Bearing
SH Pad Shear
TU
11.1.3.3 Horizontal Loads from Superstructure (BR, CE, WS, WL, TU,
PS, CR, SH)
For the seat type abutments with elastomeric bearing pads, the total amount of horizontal
load that may be transmitted through the bearings before slippage occurs is limited to 0.2
(DCSup + DW) according to Article 3.4.5 (AASHTO-CA BDS-8). This force should be
applied in both directions (toward and away from the backwall) horizontally.
The passive earth pressure resistance exerted by the fill in front of the abutment is usually
neglected in the design due to the potential for erosion, scour, or future excavation in front
of the abutment. Furthermore, a larger relative movement is needed to activate the
passive pressure. The vertical load from the toe backfill should be included in the analysis
for overturning if it increases overturning. Figure 11.1.3-2 shows earth pressure
components acting on a typical abutment.
EV
EH
Technical Policies. According to SDC 6.3.4, the shear key is limited by shear capacity of
the foundation. Therefore, the shear capacity of piles under the Extreme (Earthquake)
Event load combination needs to be calculated.
For abutments in the S2 (non-competent) soil, special design provisions are required.
Such provisions should be discussed in the Type Selection meeting.
60 degrees and for horizontally curved bridges with an abutment skew exceeding 45
degrees, A refined analysis should be performed to capture live load distributions more
accurately.
The factored shear resistance of the pile foundation shall be compared to the factored
shear force (Strength and Construction) applied to the foundation. The shear resistance
of the foundation system is developed by the resistance of all the piles considering group
and batter effects. The shear resistance of a single pile is the smaller of the structural
shear resistance of the pile and the shear force applied at the cut-off elevation when the
maximum moment in a pile reaches its factored nominal flexural resistance.
Plan view and typical section of the abutment are shown in Figure 11.1.6-3.
The shear resistance of the pile group under the Extreme (Earthquake Event) = 64 kip
Concrete:
= fc' 3.6 ksi,
= γ c 150 pcf
Reinforcing steel: fy = 60 ksi
W (nl ) ( MPF )
N= (11.1.6-1)
bn
where:
W = abutment length along the skew (62.6 ft in this example)
nl = number of whole lanes that are under consideration
bn = effective live load distribution width at the top of the footing
MPF = multiple presence factor
Per Article 3.6.1.1.1, the maximum number of design lanes that can be placed on the
bridge is determined by taking the integer part of the ratio of the clear roadway width in
feet between curbs and/or barriers then divided by 12. Furthermore, roadway widths from
20 to 24 ft should have two design lanes, each equal to one-half the roadway width.
Therefore
The edge distance is the width of the barrier; however, it can be assumed to be zero as
the designer may need to consider future widening per Article 2.3.2.1 and use the edge
of the deck (EOD) to EOD.
The effective live load distribution width at the top of the footing can be written as:
where, an is the effective live load distribution width at the deck elevation (ft):
8 + ( edge distance ) + 12 ( n − 1)
an = (11.1.6-4)
cos θsk
Since MPF depends on the number of lanes, the designer needs to calculate the
equivalent number of lanes for each case (one, two, three,…n lanes) from Equation
11.1.6-4
For example, for two live load lanes (n = 2)
8 + (1) + 12 ( 2 − 1)
=a2 = 22.35 ft
( )
cos 20°
The effective width at the top of the footing is calculated by Equation 11.1.6-3 as follows:
W ( nl )( MPF ) (=
62.6 )( 2 )(1.0 )
=N2 = 3.42 lanes
bn 36.6
Table 11.1.6-5 summarizes calculated values of an and bn for different values of n, as well
as the equivalent number of lanes, N, for HL-93 live load:
In this example, two lanes result in the largest number of equivalent lanes. Therefore, an
equivalent number of live load lanes for HL-93 truck, N, is taken as 3.42 lanes.
The same method is used for permit trucks; however, the designer should consider only
one or two lanes of P truck with MPF of one used for both cases.
Table 11.1.6-6 provides a summary of calculations for the number of Permit Truck live
load lanes.
The equivalent number of live load lanes for permit truck is 3.42 lanes which is calculated
by placing two lanes side by side.
LLHL93 = ( equivalent number of lanes )(HL93 design vehicular load per lane )
(=
3.42 lanes )( 98.23 kip/lane ) 335.95 kip
(=
3.42 lanes )(184.01 kips/lane ) 629.31 kip
V=
1 (16.75 − 2.5 )(10 − 3.5 − 4.0 ) ( 62.6-2 (1) ) ( 0.12=
) 259.1 kip
Active soil pressure behind the abutment, H1:
(=
h + dftg ) WK a γ s (14.25 + 2.5 )2 ( 62.6 )( 0.3 )( 0.12 )
2
=
LS1 (
dLS h + dftg WK= )
a γs ( 2 )(14.25 + 2.5 )( 62.6 )( 0.3 )( 0.12
= ) 75.5 kip
The equivalent bearing pad shear, Vpad, is assumed as 20% of (DCSup + DW).
V=
pad (
0.2 DCsup + DW )
= 0.2 ( 772.2 + 93.9
=) 173.22 kip
W3 DC, DW, LL
LS3
H3
Pad Shear
LS2 V1
LS1 W2
H2
V2
H1
H4
W1
X
(0,0)
Vww2
Vww3
Vww1
Table 11.1.6-7 shows the summary of unfactored forces and coordinates of their
application points in the system of coordinates shown in Figure 11.1.6.5a. The moment
arm is calculated with respect to the point to be used in design calculations. For example,
for backwall design, the moment should be calculated about the center of the base of the
backwall. Therefore, the reference point will be the centerline of the backwall at the base,
and moment arms are calculated by subtracting the coordinates of the reference point
from the coordinates of the point of the application. To simplify dead load calculations of
the wingwall, it is divided into three parts, as shown in Figure 11.1.6-5b.
Note: LSVertical is the vertical force due to the live load surcharge acting on the heel side
of the footing. Vbarrier is the weight of the barrier acting at the top of the wingwall. H4 is
equal to zero because the passive pressure coefficient, Kp, is assumed to be zero in this
example. Historically, the passive pressure for a short seat abutment design is ignored in
Caltrans practice for several reasons. The first reason is that the quality of the backfill in
front of the abutment is unknown, and the soil in this area would be eroded during the life
of the bridge. The second reason is that a large movement is needed in order for passive
soil to engage. The designer should consult with GD for the value of Kp if passive soil
pressure needs to be considered.
The load factor for the bearing pad shear is either 0 or 1.25. The bearing pad shear should
be applied in both directions horizontally to capture the worst effect for each component.
Tables 11.1.3-1 and 11.1.3-2 summarize load factors to be used for abutment design.
Considering the large number of loads to be considered use of engineering judgement to
identify governing cases for the design of each component is not practical. CTAbut
examines all possible combinations and reports the governing cases that produce the
largest Demand-to-Capacity (D/C) ratio for each check. In this example, the governing
load cases have been extracted from CTAbut to show the design process.
The backwall can be easily analyzed as a cantilever beam to calculate factored load
effects for different load combinations:
There are two load factors for the substructure dead load, 0.9 and 1.25.
The horizontal earth pressure, EH (shown as H3), has two load factors, 0.75 and 1.5. The
factor for the horizontal live load surcharge, LS3, is 1.75. Design shear force for the
backwall is calculated based on the greatest effect, which is:
Similarly, the governing factored moment for the backwall design is calculated using the
upper limits of contributing loads (W3, H3, and LS3). However, W3 does not produce a
bending moment, therefore:
h hbw
=Mbw 1.5H3 bw + 1.75LS3 2
3
6.75 6.75
=(1.5 )( 51.3 ) + (1.75 )( 30.4 ) =352.7 kip-ft
3 2
The load factors are one for Service Limit State, and only a service moment is needed for
the crack control check:
hbw hbw
=Mservice (1.00)) H3 + (1.00 ) LS3 2
3
6.75 6.75
= (1.0 )( 51.3 ) + (1.0 )( 30.4 ) = 218.0 kip-ft
3 2
The backwall thickness of dbw = 12 in. is used to check the following factored
moments acting per unit length of the backwall
352.7
=
Mu = 5.63 kip-ft/ft
62.6
218.0
M=
service = 3.48 kip-ft/ft
62.6
Assume:
The factored flexural resistance is calculated in accordance with Articles 5.6.3.2 and
5.6.3.3 as follows:
=c =
As fy ( 0.60 )( 60
=
) 1.153 in.
0.85fc' β1b ( 0.85 )( 3.6 )( 0.85 )(12 )
Distance from the extreme compression fiber to the centroid of nonprestressed tensile
reinforcement:
d bd 1.0
de = d bw − (concrete cover) − = 12 − 2 − = 9.5 in.
2 2
The net tensile strain in the extreme tension steel reinforcement is calculated as follows:
Since the calculated strain εs is larger than 0.005, the section is considered as tension-
controlled, and a resistance factor φ is 0.9 (AASHTO-CA BDS 5.5.4.2). The factored
flexural resistance is calculated as:
a 0.98
Mr =
φMn = ( )( 0.9 )( 0.60 )( 60 ) 9.5 −
φ As fy de − =
2 2
= 291.92 =
kip-in. 24.33 kip-ft=
> Mu 5.63 kip-ft OK
Minimum Reinforcement
2
=
(12 )(12 )= 288 in.3
Gross section modulus: Sc S=
nc
6
Flexural cracking variability factor: γ1 = 1.6 for all concrete structures except precast
segmental structures per Article 5.6.3.3.
The ratio of specified minimum yield strength to ultimate tensile strength of the
reinforcement: γ3 = 0.75 for A706, Grade 60 reinforcement per Article 5.6.3.3. The
calculations are as follows:
Mcr =γ 3 γ1fr Sc
(AASHTO 5.6.3.3-1)
= (0.75)(1.6)(0.455)(288)
= 157.25 =kip-in 13.10 kip-ft
1.33Mu 1.33(5.63)
= = 7.49 kip-ft
Mcr = 13.10
Mr = 24.38 kip-ft > smaller of
φMn = =7.49 kip-ft (AASHTO 5.6.3.3)
1.33M u = 7.49
Crack Control
AASHTO Article 5.6.7 requires maximum limits of rebar spacing for crack control.
700 γ e
s ≤ − 2dc (AASHTO 5.6.7-1)
βs fss
Assuming exposure factor γe is equal to 1 (class-I exposure), and dc is equal to 2.5 in.
dc 2.5
βs = 1 + = 1+ = 1.376
0.7(h − dc ) ( 0.7 )(12 − 2.5 )
The cracked concrete section is used to calculate tensile stress in steel reinforcement
under service loads, and the moment of inertia for unit width (12 in.) of the transformed
section (based on concrete), Itr, is calculated as follows:
1.5
= (33,000)(1.0)(0.15)
= 3.6 3637 ksi
Es 29,000
=
n = = 7.97
Ec 3,637
As 0.60
=
ρ = = 0.0053
bde (12 )( 9.5 )
2
k= ( ρn ) + 2 ( ρn ) − ρn
2
= ((0.0053)(8)) + 2(0.0053)(8) − (0.0053)(8)= 0.252
k=
de =
kd e ( 0.252 )( 9.5
= ) 2.394 in.
bk 3 2
Itr = de + n As ( de − kde )
3
3
(12 )( 2.394 ) + ( 8 )( 0.60 )( 9.5 − 2.394
2
= = ) 297.26 in.
3
Tensile stress in steel reinforcement at the service limit state is calculated as:
700 γ e 700(1)
s= 12 in. ≤ − 2dc= − 2(2.5)= 58.59 in. OK
βs fss (1.376)(8)
For backwall, b = 12 in. (unit width) and backwall height h = 6.75 ft = 81 inches, the
horizontal shrinkage and temperature reinforcement per unit foot width shall satisfy the
following equations (Article 5.10.6):
1.3bh 1.3(12)(81)
As ≥ = = 0.113 in.2 (AASHTO 5.10.6-1)
2(b + h )fy 2(12 + 81)(60)
2
0.11 in.= ≤ As 0.1963 in.2 ≤ 0.6 in.2 OK
The shear design for the abutment backwall is usually based on the shear resistance of
the concrete alone. The backwall is not heavily reinforced since it is designed to break
during a seismic event. The design procedure is the same as the steam wall shown in
Section 11.1.6.7.3 and is not repeated herein.
The weights of backwall, stem wall, wing walls, shear keys, superstructure (DCsup),
wearing surface, and utilities load (DW), as well as the design truck (HL93) and the permit
truck (Permit), are vertical gravity loads applied to the stem wall. The bearing pad shear
load, prestressing load (PS), horizontal pressure by live load surcharge, horizontal active
soil pressure from the back of stem wall and backwall, and the horizontal passive soil
pressure from the fill in front of the stem wall (this passive pressure may be conservatively
ignored for short seat abutments however it is considered for tall cantilever abutments)
are horizontal loads that are considered in stem wall design.
Similar to the backwall, thirteen permanent loads are considered in the stem wall design,
which result in a very high number of possible load combinations. CTAbut is used to
identify controlling load combinations in this design example. CTAbut prints out the load
factors for controlling combinations to be used for the design of each component of the
abutment at the end of the full report. Tables 11.1.6-8 and 11.1.6-9 show the values of
load factors for governing cases for stem wall design.
Table 11.1.6-8 Load Factors for Strength and Construction Limit States
Stem Pad
DCSup. DCSub. DW PS LLHL93 LLPermit EHa LSh EHp Comb.
wall* shear+
Pmax 1.25 1.25 1.50 1.00 1.25 0.00 1.35 1.50 0.00 - STR2
Vmax(B) 1.25 0.90 1.50 1.00 1.25 1.75 0.00 1.50 1.75 - STR1
Mmax(B) 1.25 0.90 1.50 1.00 1.25 1.75 0.00 1.50 1.75 - STR1
Vmax(F) 0.90 1.25 0.65 1.00 -1.25 0.00 1.35 0.75 0.00 - STR2
Mmax(F) 0.90 1.25 0.65 1.00 -1.25 0.00 1.35 0.75 0.00 - STR2
*B = Back face of the stem wall in tension; F = Front face of the stem wall in tension
+Negative gamma factor for Pad shear has been applied to capture bi-directional force effects
Stem Pad
DCSup. DCSub. DW PS LLHL93 LLPermit EHa LSh EHp Comb.
wall shear
Mmax(B) 1.0 1.0 1.0 1.0 1.0 1.0 0 1.0 1.0 - SER1
Mmax(F) 1.0 1.0 1.0 1.0 -1.0 1.0 0 1.0 1.0 - SER1
All the controlling factored design loads could be calculated by using the tables above.
For example, the factored design shear for the stem wall is calculated as:
Vmax ( B=
) 1.25Vpad + 1.5H2 + 1.75LS2
Summary of factored loads effects for the stem wall design are given in Table 11.1.6-10.
Irrespective of the direction, the maximum calculated shear is used for the design of the
shear reinforcement in the stem wall. The designer should check both faces (the heel
side and the toe side) when designing the shear reinforcement if the concrete cover is
different. CTAbut reports some cases as 0.00 if the compression or tension does not
affect the section.
An axial force is not usually considered in the flexural design of the stem wall since the
effect is often minimal. The effect of the moment acting in the transverse direction (biaxial
bending) is also negligible. However, in the case of narrow abutments (i.e., single lane on
or off-ramp), Article 5.6.4.5 requirements shall be satisfied.
The design procedure for flexural, crack control, and shrinkage and temperature
reinforcement is the same as the backwall and is not repeated here. However, the detailed
steps for the shear design are shown in the next section.
The shear design for the abutment stem wall and footing follows the General Procedure
per Article 5.7.3.4.2 and its CA amendment. The flowchart of the process in CTAbut is
shown in figure 11.1.6-6, and the shear design for the stem wall follows.
d = 48 in.
β1 = 0.85
Checking Shear
Capacity
Is
Is Add shear
Add shear Continues with Vu ≤ φVn?
Vu ≤ φVn? Yes No reinforcement
reinforcement No check See 5.7.3.3
See 5.7.3.3 and recheck
and recheck For Vn
For Vn
Yes
As fy (38.4)(60)
=c = '
= 1.18
α1fc β1b (0.85)(3.6)(0.85)(751.2)
bar diameter 1
de= 48 – concrete cover – = 48 − 2 − = 45.5 in.
2 2
The minimum transverse reinforcement requirement from Article 5.7.2.5-1 is not satisfied.
a 1
dv = d e − = 45.5 − = 45.0
2 2
Per AASHTO Article 5.7.2.8: dv need not be taken to be less than the greater of
Av fy dv cot θ
Vs = (AASHTO C5.7.3.3-1)
s
Since the section contains less than the minimum transverse reinforcement as specified
in Article 5.7.2.5, equation B5.2-4 would be used to obtain the εx.
Mu
+ 0.5Nu + 0.5 Vu − Vp cot θ − Aps fpo
d
ε x = v (AASHTO B5.2-4)
Es As + E p Aps
Mu
+ 0.5Nu + 0.5 Vu cot θ
d
ε x = v (11.1.6.1-1)
Es As
Per AASHTO CB5.2, 0.5 cot θ could be assumed 1 for the first trial to limit a trial
and error process.
Mu
+ 0.5Nu + Vu
d
ε x = v (11.1.6.1-2)
Es As
CTAbut checks both Vumax with its associated moment and Mumax with its associated shear
for each section of the component.
Table 11.1.6.1-2 Stem Wall Back Section Loads to Calculate the Shear Reinforcement
Vumax = 672.1 kip VuM = -4356.80 kip-ft VuN = - 2148.00 kip
Mumax = -4356.80 kip-ft MuV = 672.1 kip MuN = - 2148.00 kip
In this example, the associated moment or shear is exceptionally equal to the controlling
values.
−4356.80
+ 0.5( −2148.00) + 672.1
= 3.75 0.6824 * 10−3
εx
(29000)(38.4)
1.38 1.38
=s xe s x = (3.75)(12) = 38.10 in. ≤ 80 in. OK
ag + 0.63 1 + 0.63
θ = 53.7 and β =1.66 using AASHTO Table B5.2-2 for εx ≤ 1.5 and sxe≤40.
'
=Vc 0.0316βλ f=
c bv dv 0.0316(1.66)(1.0) 3.6(751.2)(45.0)
= 3364.45 kip
φVn = φ(Vc + Vs )
Lesser of '
φ(0.25)fc bv dv
φ(0.25)fc' bv dv =
φVn = (0.9)(0.25)(3.6)(751.2)(45.0) =
27381.24 kip
φ(Vc + Vs ) =
φVn = 0.9(3364.45 + 0) =
3028.00 kip (controlled)
Vu max 672.1 kip
= = < φVn 3028.00 kip
No shear reinforcement is required for the stem wall.
The standard Class 140 piles are selected in this example, where the diameter of the pile
is 14 in. with a batter of 1 to 3. There are two rows of piles with 13 piles in each row which
brings the total number of piles to 26. One row of piles is battered. The distances to the
center of the pile from footing heel are 2 ft and 8 ft for Rows 1 and 2, respectively.
Using controlling load combinations from CTAbut output, shown in Tables 11.1.6-11 and
11.1.6-12, the factored loads for pile group design are calculated. The summary of
factored loads is shown in Table 11.1.6-13.
Table 11.1.6-11 Load Factor for Strength Limit State and Construction Combination
Pile DCSup. DCSub. DW PS Pad LLHL93 LLPermit EHa LSh EHp EVa EVp LSv Comb.
Group* shear
Pmax(C) 1.25 1.25 1.50 1.00 1.25 0 1.35 1.50 0 - 1.35 1.35 0 STR2
Pmax(T) 0 0.90 0 0 0 0 0 1.50 0 - 1.00 1.00 0 CON1
FRow(T) 0.90 0.90 0.65 1.00 1.25 1.75 0 1.50 1.75 - 1.00 1.35 0 STR1
FRow(C) 1.25 1.25 1.50 1.00 -1.25 0 1.35 0.75 0 - 1.35 1.00 0 STR2
LRow(T) - - - - - - - - - - - - - -
LRow(C) 1.25 1.25 1.50 1.00 1.25 1.75 0 1.50 1.75 - 1.00 1.35 0 STR1
*FRow: First row from Heel, LRow: Last row from Heel, T: Tension, C: Compression
Pile DCSup. DCSub. DW PS Pad LLHL93 LLPermit EHa LSh EHp EVa EVp LSv Comb.
Group shear
Pmax(C) 1.0 1.0 1.0 1.0 1.0 1.0 0 1.0 1.0 - 1.0 1.0 1.0 SER1
Pmax(T) 1.0 1.0 1.0 1.0 1.0 1.0 0 1.0 1.0 - 1.0 1.0 1.0 SER1
LatDC+ 1.0 1.0 1.0 1.0 1.0 1.0 0 1.0 1.0 - 1.0 1.0 1.0 SER1
FRow(T) - - - - - - - - - - - - - -
FRow(C) 1.0 1.0 1.0 1.0 -1.0 1.0 0 1.0 1.0 - 1.0 1.0 1.0 SER1
LRow(T) - - - - - - - - - - - - - -
LRow(C) 1.0 1.0 1.0 1.0 1.0 1.0 0 1.0 1.0 - 1.0 1.0 1.0 SER1
+LatDC: DC ratio of entire pile group lateral resistance capacity
Table 11.1.6-13 – Summary of Factored Load Effects for Pile Group Design
P (axial load) V ( shear) M (moment)
Pile Group
kip kip kip-ft
Pmax(C) 3366.65 690.73 2883.45
Strength Pmax(T) 984.22 474.21 1240.67
Limit FRow(T) 1836.37 822.85 4634.71
State FRow(C) 3329.01 20.58 -2893.18
LRow(C) 3012.17 822.85 4334.39
Pmax(C) 2351.11 564.85 2492.79
Service Pmax(T) 2015.16 564.85 2492.79
Limit LatDC 2015.16 564.85 2492.79
State FRow(C) 2351.11 218.41 -971.61
LRow(C) 2351.11 564.85 2492.79
The resistance of Class 140 standard piles is given in Standard Plan B2-5 as the nominal
axial structure resistance of 280 kip for the compression and the nominal axial structure
resistance of 140 kip for the tension.
The calculation of the moment of inertia of pile group, I, is shown in table 11.1.6-14.
Where np is the number of piles in each row; d is the distance from the face of footing (toe
side), and equivalent Cgpile is the center of gravity for the pile group from the footing toe.
The center of the gravity of the pile group from the toe of the footing (Cgpile) = 130/26 =
5.0 ft which is the center line of footing since the number of piles in each row are the
same.
The axial force of any vertical pile is calculated from Ppile = P/np ± Mc/I, where c is the
distance between the centerline of the pile and the center of gravity of the pile group.
As an example, the last row pile reaction (maximum that is used in the design) is
calculated as:
3012.17 4334.39 ( 5 − 2 )
PLRow (C ) = + 171.4 kip
=
26 234
Since the pile reaction force is less than factored nominal resistance in the compression
(186.0 kip), it is acceptable. This check is needed for each load combination and for each
row of the piles.
The summary of pile reactions for the strength limit state is shown in Table 11.1.6-15
(196)(3)
where: the factored vertical resistance of battered pile = = 186.0 kip .
2 2
1 +3
The permissible horizontal (lateral) load of the pile group under the service limit state shall
also be checked. The permissible horizontal load for a single pile assuming 5 feet of the
embedment and zero axial force is 27 kip, and the reduction factor for battered piles is
taken as 0.6 for this example.
2015.16 2492.79 ( 5 − 2 )
PFRow (C ) = + 109.47 kip
=
26 234
109.47
=
Horizontal reaction force of a batter pile = 36.49 kip
3
Horizontal reaction force of all battered piles, Fpile = (36.49)(13) = 474.30 kip
Total Maximum Lateral load under Service Limit State, Fx = 564.85 kip
Required horizontal load = Total maximum lateral load – horizontal reaction force of all
batter piles = 564.85 – 474.30 = 90.55 kip
The permissible horizontal load (561.6 kip) is greater than required horizontal load (90.55
kip). Therefore, it is acceptable. The designer also needs to check the Construction II
combination; however, that combination usually does not govern.
Note - This example is to show the designer the use of batter piles. The demand/capacity
for this example is extremally low, perhaps, the pile may not need to be battered for this
example.
Under the Service I Limit State, both total and the permanent support loads (calculated
as net) are reported to GD:
Total Load (net) = Maximum load under Service-I – the weight of the overburden soil
The permanent load (net) = 1851.91 - 336.0 - 38.4 = 1477.5 kip. Under the Strength Limit
State, the maximum force per support, the minimum force per support, also the maximum
compression, and the tension force per pile are reported:
There is no tension in a pile for this example. The General Foundation information to be
sent from SD to GD is shown in Table 11.1.6-16.
Table 11.1.6-16a Information to be Provided to GD
Foundation Design Data Sheet
Note -Since this design example is for abutment design, information on bents is not shown.
Tables 11.1.6-17 and 11.1.6-18 summarize the load factors for the controlling load
combinations for the design of the pile cap.
Using the information shown in Tables 11.1.6-17 and 11.1.6-18, the factored loads for the
pile cap are calculated. The summary of factored loads shown in Table 11.1.6-19 is used
for the top and bottom reinforcement design as well as the shear design.
The pile cap is designed for shear forces and bending moments calculated on the toe and
heel sides of the stem. The shear force is conservatively calculated at the face of the
stem rather than at a distance equal to the depth of the footing. For example, the shear
force at the heel side is calculated by reducing forces of the piles that are partially located
in the free body diagram, as well as considering other factored forces:
Vheel =
(pile reaction )(number of piles )( effective fraction of pile reaction )
footing length
−
(load factor )V1 − (load factor )V3 − (load factor ) LSVertical
footing length footing length footing length
−
(load factor )W1 (heel width ) / ( footing width )
footing length
=
(165.13 )(13 )( 0.928 ) − (1.35 )( 259.1) − (1.35 )( 6.1) − ( 0 )( 38.4 ) − (1.25 )( 240 )( 2.5 ) / (10 )
64 64 64 64 64
= 24.36 kip/ft
Pile reaction forces may be fractional depending on the pile's location with respect to the
heel's face. In this case, the center line of the second row of piles is located 8 ft from the
toe edge of the footing. The fraction of the pile reaction that contributes to the shear at
the heel is approximated as:
fraction ≈
(heel width ) − ( footing width-location of pile - pile diameter/2 )
pile diameter
2.5 − (10 − 8 − 1.167 / 2 )
≈ 0.928
=
1.167
The summary of the cap design forces per linear foot at the face of the stem (the toe side
and the heel side) are shown in Table 11.1.6-20.
Table 11.1.6-20 Summary of Cap Design Forces per Liner Foot at the Face of Stem
(Toe Side and Heel Side)
Limit State Forces Top of Toe Bottom of Toe Top of Heel Bottom of Heel
Shear at face (kip/ft) 4.46 30.91 2.87 24.36
Strength
Moment at face (kip-ft/ft) 0.00 45.50 6.60 9.48
Service Moment at face (kip-ft/ft) 0.00 32.05 2.31 3.51
The steps for flexural design, shear design, crack control, and horizontal temperature
reinforcement of the pile cap are similar to the backwall or the stem wall.
Using governing load combinations and load factors reported by the CTAbut program (not
shown here), Table 11.1.6-22a and 11.1.6-22b summarize governing factored loads for
soil and structural checks, respectively of the abutment design.
The first check for Strength/Construction load combinations is a bearing stress check.
The governing load combination is used to check the soil's bearing resistance and the
footing's size. Using absolute values of the moment and the axial force, the eccentricity,
effective footing width, and effective area are calculated as:
Mu 4634.71
=e = = 2.52 ft
Pg 1836.37
=Ae (=
64 )( 4.95 ) 316.95 ft 2
The ultimate bearing stress is calculated based on a uniform stress distribution as the
footing is on soil:
1836.37
=
qg ,u = 5.79 ksf
316.95
qn = 29.02 ksf
The second check for Strength/Construction load combinations is the sliding check.
Ignoring the backfill passive resistance, the factored sliding resistance is obtained by
Article 10.6.3.4 as:
RR =
φRn = 0.8P µ
φτR τ =
where P is the total vertical force, φτ is the resistance factor for sliding between soil and
foundation (AASHTO Table 10.5.5.2.2-1), and µ = tan (φf) where φf is the internal friction
angle of drained soil.
=RR 0.8
= ( 984.22 ) tan(34o ) 531.1 kip
Comparing the shear force effect of the footing to the factored shear resistance:
Shear keys are not required herein to resist the sliding. In case shear keys are required,
the advantages and disadvantages of using shear keys should be considered in the
design. CTAbut provides the additional required shear force to design the shear key under
the footing in the full report only.
The first check under the Service-I load combination is to compare the net uniform bearing
stress (qn,u) to the permissible net contact stress (qpn) to limit the settlement to the
permissible level. The axial load should be used as the net when calculating the bearing
stress for the settlement check. Using absolute values of the moment and the axial force,
the eccentricity, effective footing width, and effective area are calculated as:
Mn 2492.79
=e = = 1.06 ft
Pg 2351.11
10 − 2 (1.06 ) =
B′ = 7.88 ft
=Ae (=
64 )( 7.88 ) 504.32 ft 2
2351.11
=
qg ,u = 4.66 ksf
504.32
(
qg ,u − ( AverageOG − bottom of footing ) γ SE
qn,u = )
120
qn,u = 4.66 − ( 6.5 − 0 ) * 1.00 = 3.88 ksf
1000
The permissible net contact stress qpn is calculated from Table 11.1.6-21 using B′ = 7.88
ft and interpolation between13.3 ksf and 12.2 ksf as:
The second check under the Service-I load combination is the eccentricity check. The
gross axial force is used for this check. Therefore, the eccentricity is calculated as:
Mn 2492.79
=e = = 1.24 ft
Pg 2015.16
The calculated eccentricity is less than the specified limit and is acceptable.
Note: If the footing is on the rock, the maximum eccentricity limit is Bftg/4.
Note – CTAbut reports Pgross in the soil check table. However, the settlement check
calculation must use Pnet.
Strength/Construction Mx Vy Ptotal(gross)
Limit States (kip-ft) (kip) (kip)
Mx_max 2893.18 20.58 3329.01
Mx_min 4634.71 822.85 2774.36
Bearing
Ptotal_max 2883.45 690.73 3366.65
Controlling Load 4634.71 822.85 1836.37
Vy_max 4634.71 822.85 2774.36
Vy_min 1072.58 0.00 2013.89
Sliding
Ptotal_min 1240.67 474.21 984.22
Controlling Load 1240.67 474.21 984.22
In order to calculate the internal forces of the footing, as shown in Figure 11.1.6-7, the
soil pressures, qleft (heel edge), qright (toe edge), q1 (at the face of the heel), and q2 (at the
face of the toe) are calculated. The following symbols are used:
M
P
q1 q2
qleft
Vtoe_soil = shear due to the soil pressure at the face of the toe (kip/ft)
Bftg = footing width (ft)
Wheel = heel width (ft)
Wtoe = toe length (ft)
For example, for the case shown in Table 11.1.6-22b, the “MBotHel” forces are given as:
P = 3236.19 kip, and M = 2548.73 kip-ft.
q1 =
qleft −
( )
qleft − qright Wheel
7.45 −
=
( 7.45 − 2.67 )( 2.5 ) =
6.25ksf
Wftg 10
q2 =
qright +
(
qleft − qright Wtoe )
2.67 +
=
( 7.45 − 2.67 )( 3.5 ) =
4.34 ksf
Wftg 10
=Vheelsoil
(=
qleft + q1 )Wheel ( 7.45 + 6.25 )( 2.5 )
= 17.13 kip/ft
2 2
=
M
2
q1Wheel ( q − q1 )Wheel
+ left
2
heel soil
2 3
2 2
(
=
6.25 )( 2.5 )
+
( 7.45 − 6.25 )( 2.5 )
22.03 kip-ft/ft
=
2 3
For the structure design of the footing, the forces from the overburden soil and footing
need to be subtracted from the forces caused by the soil pressure, calculated above.
2.5
(1.0)(259.1) + (1.0)(6.1) + (0)(38.4) + (1.25)(240)
17.13 −
= 10 =11.81 kip/ft
64
( LF )V1 ( MA ) + ( LF )V3 ( MA ) + ( LF ) LSVertical ( MA ) + ( LF )W1 ( MA )Wheel / Bftg
=
Mheel Mheel _ soil −
Lftg
2.5
(1.0)(259.1)(1.25) + (1.0)(6.1)(1.25) + (0)(38.4)(1.25) + (1.25)(240)(1.25)
22.03 −
= 10 =15.38 kip/ft
64
LF: Load Factor; MA: Moment Arm
After repeating the calculation for other sections of the footing a summary of the shear
and flexural footing design load effects was generated and shown in Table 11.1.6-24.
Table 11.1.6-24 Summary of the shear and flexural footing design loads
Limit State Forces Top Toe Bottom Toe Top Heel Bottom Heel
Shear at face (kip/ft) 0.00 21.93 6.69 11.81
Strength
Moment at face (kip-ft/ft) 0.00 41.20 8.98 15.38
Service Moment at face (kip-ft/ft) 0.00 28.24 3.35 6.75
The flexural and shear design steps for the footing are the same as for the pile foundation
or stem wall design. Therefore, it is not shown here.
NOTATION
Ae = effective shear area of a cross-section (ft2)
As = total area of non-prestressed tension reinforcement (in.2)
a = depth of equivalent rectangular stress block (in.)
an = effective live load distribution width at the deck elevation (ft)
B’ = effective footing width (ft)
BOF = bottom of footing elevation (ft)
Bftg = tooting width (ft)
bn = effective live load distribution width at the top of the footing (ft)
bv = effective width of a member for shear stress calculations (in.)
C = correction factor for concrete-soil interference
Cgpile = center of gravity for pile group (ft)
c = distance from the extreme compression fiber to the neutral axis (in)
DCsup = dead load from superstructure (kip)
DCsub = dead load from substructure (kip)
DW = additional dead load from superstructure (kip)
d = distance from the face of footing to center of the pile (ft)
dbd = deformed bar diameter (in.)
dbw = backwall thickness (in. or ft)
dc = thickness of concrete cover measured from extreme tension fiber to center
of closest bar (in.)
de = effective depth from extreme compression fiber to the centroid of the tensile
force in the tensile reinforcement (in.)
dftg = footing thickness (ft)
dLS = depth of live load surcharge on heel (ft)
dv = effective shear depth (in.)
EH = horizontal earth pressure (kip)
LSH = horizontal live load surcharge (kip)
Ec = modulus of elasticity of concrete (ksi)
Es = modulus of elasticity of reinforcing steel (ksi)
e = eccentricity (ft)
f´c = specified 28-day compressive strength of unconfined concrete (ksi)
fr = modulus of rupture of concrete (ksi)
REFERENCES
1. AASHTO. (2017). AASHTO LRFD Bridge Design Specifications, 8th Edition,
American Association of State Highway and Transportation Officials, Washington
DC.
2. Caltrans. (2019a). California Amendments to AASHTO LRFD Bridge Design
Specifications, 8th Edition, California Department of Transportation, Sacramento,
3. CA.Caltrans. (2019b). Caltrans Seismic Design Criteria, Version 2.0, California
Department of Transportation, Sacramento, CA.
4. Caltrans. (2019c). CTBridge Program, Version 1.8.3 California Department of
Transportation, Sacramento, CA.
5. Caltrans. (2020). Bridge Design Details, Chapter 6, California Department of
Transportation, Sacramento, CA.
6. Caltrans. (2022). CT- Abut program, Version 3.1.0, California Department of
Transportation, Sacramento, CA.
7. Zokaie, T., Malek, A., and Rahbari, A. (2015). “Live Load Distribution on Bridge
Abutments,” Western Bridge Engineers Seminar, September 9-11, Reno, NV.