pondasi-1-6
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Foundation Engineering Foundation Engineering
Lecture #05 Lecture #05
Bearing Capacity of Soils
on
Eccentrically Loaded Footings
L. Prieto-Portar, 2008
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Foundations with a One-Way Eccentricity.
In most instances, foundations are subjected to moments in addition to the vertical load
as shown below. In such cases the distribution of pressure by the foundation upon the soil
is not uniform.
Q M
B B
B X L
e
F o r e < B /6
q m in
q m a x
F o r e > B /6
q m a x
e
(b )( a )
Figure 6. An
eccentrically
loaded
footing.
The effectivewidth is now,
B’ = B - 2e
whereas the
effective length is
Still,
L’ = L
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The distribution of the nominal pressure is :
where Q is the total vertical load and M is the moment on the footing in one axis.
Figure 6b shows a force system equivalent to that in Figure 6a. The distance e is the
eccentricity of the load, or
Substituting equation 16 in equations 14 and 15 yields:
max 2
min 2
6 (14)
and
6 q (15)
Q M q BL B L
Q M
BL B L
= +
= −
M e (16)Q
=
max
min
6
1 (17 a)
6
q 1 (17 b)
Q e
q BL B
and
Q e
BL B
= +
= −
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Note that in these equations, when the eccentricity e becomes B/6, q min is zero. For e >
B/6, q min will be negative, which means that tension will develop. Because soils can sustain
very little tension, there will be a separation between the footing and the soil under it.Also note that the eccentricity tends to decrease the load bearing capacity of a
foundation. In such cases, placing foundation column off-center, as shown in Figure 7 is
probably advantageous. Doing so in effect, produces a centrally loaded foundation with a
uniformly distributed pressure.
M
e
Q
Figure 7. A footing with the column off-center to preserve a uniform pressure on the soil.
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The general bearing capacity equation is therefore modified to,
qu’ = c N c F cs F cd F ci + q N q Fqs Fqd Fqi + γ γγ γ B’ N γ γγ γ Fγ γγ γ s Fγ γγ γ d Fγ γγ γ i
and Qu = qu’ B’ L’
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Foundations with Two-way Eccentricities.
Consider a footing subject to a vertical ultimate load Qult and a moment M as shown in
Figures 8a and 8b. For this case, the components of the moment M about the x and y axis
are M x and M y respectively. This condition is equivalent to a load Q placed eccentrically
on the footing with x = e B and y = e L as shown in Figure 8d.
M
B X L
Q u lt
B(a )
Qult
B
L
Qult
My
x
y
My
Qult
Mx eL
eB
(b) (c) (d)
Figure 8. Analysis of a footing with a two-way eccentricity.
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Note that,
ult
c q
ult u
(18)
If Q is needed, it can be obtained as ' ' ,
1' cN qN B ' N (19)2
A' is the effective area B'L'
Finally Q = q (
y x B L
ult ult
ult u
u cs cd ci qs qd qi s d i
M M e and eQ Q
Q q A where
q F F F F F F F F F
and
γ γ γ
= =
=
= + +
cs qs s
A')
As before, to evaluate F , F , and F , use the effective length (L') and the effective width
(B') dimensions instead of L and B, respectively. To calculate F , ,and ,do not replaceB with B
cd qd d F F
γ
γ
'. In determining the effective area (A'), effective width (B'), and the effective (L'),
four possible cases may arise (Highter and Anders, 1985).
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B1
B
Qult
L1
Effectivearea
eL
eB
L
1 1
ffective area for the case of and .6 6
L Be e
L B≥ ≥Figure 9. Case I. The e
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1 1
1 1
1 1 and .
6 6
1The effective area for this condition is A' (20)
2
3 3where B 1.5 and L 1.5 (21 a and b)
The effective length L
L B
B L
e e
L B
B L
e e B L
B L
≥ ≥
=
= − = −
Case I :
1 1', is the larger of the two dimensions B L .
Therefore, the effective width is:
' ' (22)
'
L
or
A B
L
e
=
Case II :
1 2
1 2
1 1 and 0 . The effective area for this case is shown in Figure 10a,
2 6
1 ' ( ) (23)
2The magnitude of L and L can be det
Be
L B
A L L B
< < <
= +
1 2
1 2
ermined from Figure 10b. The effective width is,
' ' (24)
( arg )
The effective length is ' ( arg ) (25)
A B
L or L whichever is l er
L L or L whichever is l er
=
=
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0.4
0.1
For
obtaining
L2 /L
0.60
0
0.2 0.4
0 .
1 6
0.2
0.1
0.3
e L / L
0 . 1 0
eB /B =
0 . 1 2
0 . 1 4 0
. 0 6
0 . 0 8
0 . 0
4
For
obtaining
L1 /L
0.8 1.0
0 . 0
1
0 . 0
2
0 . 0 2
0 . 0 1
0.080.06
0.04
0.5
eB /B =0.167
L1 /L , L2 /L
(b)
L
(a)
Qult
L2eB
B
L1
eL
Effective
area
1 1Effective area for the case of and 0 (After Highter and Anders, 1985)
2 6
'The effective width is ' and the effective length is ' .
L Be e
L B
A B L L
L
< < <
= =
Figure 10. Case II.
L1 and L2 can be determined from the figure,
1 2
'' B
L orL
=
using in the denominator the largest
value of L, that is,
L’ = L1 or L2 whichever is larger
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1 2
1 1 and 0 . The effective area is shown in Figure 11a.
6 2
1 ' ( ) (26)
2
The effective width is,
'
L Be e
L B
A B B L
B
< < <
= +
=
Case III :
1 2
' (27)
The effective length is equal to L' L (28)
The magnitudes of B and B can be determined
A
L =
22
2
fron Figure 11b.
1 1
and . The effective area is shown in Figure 12a.6 6
The ratio and thus B can be determined by using the curves that slope upward.
Similarely, the ratio
L B
L
e e
L B
B e
B L
L
L
< <Case IV :
2
2 2 2
and thus L can be determined by using the curves that slope downward.
The effective area is then,
1 ' ( )( ) (29)
2
Le
L
A L B B B L L= + + −
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00 0.2 0.4 0.6 0.8 1.0
0.1
0.2
0.3
0.4
0.5
B1 /B , B2 /B
e B / B
Effectivearea
Qult
0 . 1
6
For
obtaining
B2 /B
For
obtaining
B1 /B
0 . 1 4
eL /L =
0 . 1 2
0 . 1 0
0 . 0 8
0 . 0
6
0 . 0
4
0 . 0
2
0 . 0
1
eL
eB
B
L
eL /L =
0 . 0 2
0 . 0 1
0.167
0.10.08
0.060.04
(a)
(b)
B1
B2
Foundation with Two-way Eccentricity, Case III
1 1Effective area for the case of and 0
6 2(After Highter ans Anders, 1985).
L Be e
L B
< < <Figure 11.
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00 0.2 0.4 0.6 0.8 1.0
0.05
0.10
0.15
0.20
B2 /B , L2 /L
e B / B
Effectivearea
Qult
eL /L = 0.02
eL
eB
B
L
0.02 = eL /L
(a)
(b)
B2
For obtaining L2 /L
For obtaining B2 /B
L2
0 .0 4
0 .0 6
0 . 0
8 0 .1
0 .1 4 0.04
0.060.080.10
0 . 1
2 0 . 1
6
0 . 1
4
Foundation with Two-way Eccentricity, Case IV
1 1Effective area for the case of and
6 2
(After Highter ans Anders, 1985)
L Be e
L B< <Figure 12.
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Example 7.
A square foundation is shown in Figure 13. Assume that the one- way load eccentricity eis 0.15 m. Determine the ultimate load Qult.
Solution : With c = 0, equation 19 becomes:
γ sat =18kN/m
φ = 30°c = 0
1.5 m x 1.5 m
0.7 m
sand3
( ) ( )
1q 2
2
f
' qN B'N
and D 0.7 18 12.6 kN m
u qs qd qi s d iq F F F F F F
q
γ γ γ
γ
= +
= = =
Figure 13.
For = 30º, N q = 18.4 and N = 22.4
B’ = 1.5 – 2(0.15) = 1.2 m
L’ = 1.5 m
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( ) ( ) ( )2
B ' 1 .2 1 tan 1 tan 3 0 1 .4 6 2
' 1 .5
0 .289 0 .7 1 2 tan 1 - s in 1 1 .135
1 .5
B ' 1 .2 1 - 0 .4 1 - 0 .4 0 .68
L ' 1 .5
q s
f
q d
s
F L
DF
B
F γ
φ
φ φ
= + = + ° =
= + = + =
= = =
( ) ( ) ( ) ( ) ( ) ( ) ( ) ( ) ( )
( ) ( ) ( ) ( )
12
2
1
' 1 2 .6 1 8 .4 1 .4 6 2 1 .1 3 5 1 8 1 .2 2 2 .4 0 .6 8 1
384 .7 164 .50 549 .2 kN m
B ' ' ' 1 .2 1 .5 5 4 9 .2 9 8 8
d
u
u lt u
F
S o
q
H en ce
Q L q kN
γ =
= +
= + =
= = ≈
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Example 8.
Using the data from Example 5, and having a two-way eccentricity, for Figure 14,determine the ultimate load Qult.
1.5m
e =0.3 m
1.5m
L
e =0.15mB
2.0
5.1
3.0
L
e :SolutionL ==
1.05.1
15.0
B
e B ==
2
21
1.193m)0.315)(1.5(1.275
2
1
)LL(2
1 'A
)51.3.(FromEq
=+
=+=
Figure 14.
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1
1q 2
2
q
qs
A' 1.193From equation 24 B' 0.936
L' 1.275
From equation 25, L' L
Since c 0
' qN B'N
(0.7)(18) 12.6 kN /m
For 30 , N 18.4 and N 22.4
'F 1 tan'
u qs qd qi s d i
f
q F F F F F F
and q D
B L
γ γ γ
γ
γ
φ
= = =
=
=
= +
= = =
= ° = =
= +
s
2
qd
d
0.9361 tan 30 1.4241.275
' 0.936F 1 0.4 1 0.4 0.706
' 1.275
(0.289)(0.7)
F 1 2 tan (1 sin ) 1 1.1351.5
F 1
1 ' ' '( ' )
2
(1.193)[(12.6)
f
ult u q qs qd s d
B
L
D
B
Q A q A qN F F B N F F
γ
γ
γ γ γ
φ
φ φ
γ
= + ° =
= − = − =
= + − = + =
=
∴ = = + =
= (18.4)(1.424)(1.135) (0.5)(18)(0.936)(22.4)(0.706)(1)]
606 kN
+
=
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References:
1. J. Bowles, “Foundation Analysis and Design”, McGraw-Hill;
2. B. Das, “Principles of foundation Engineering”, Thompson;
3. Liu, Everett, “Soils and Foundations”, Prentice Hall;