abutment jem ba an
TRANSCRIPT
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ABUTMENT : Bendung ….
1. Input
Dimension
+ 80.45 HT
B1
B2
B3
+ 79.00 B4
B5
B6
BT
H1
H1 max
+ 75.00 H2
H3
H4
H5
+ 74.00 H6
H10
ho
Abutment wi
+ 69.00 Support from P
Rh1
Rb1
Hw1
+ 67.40 Hw2
Slope
(in case no soi
Design Load f
Unit Weight Wheel load
Soil 1.80 t/m3 T
Soil (saturated) 2.00 t/m3 Contact widConcrete 2.40 t/m3 a
Effective width
Reaction of superstructure Thickness of pav
Normal Vn=Rd+Rl 137.96 ton
Seismic Ve=Rd 71.27 ton With Impa
He= 12.83 ton (He=2 kh Rd, for fixed bearing)
Type of bearing Movable (He=kh Rd, for movable bearing) Width of Co
(Input Fixed or Movable) Thickness of Impac
Surcharge Load 0.70 t/m2 Length of Imp
Soil depth ab
Parameters
q : surcharge load (t/m2) 0.70
q' : surcharge load (t/m2) (=0) 0.00
g : unit weight of earth (t/m3) 1.80
w : ground surface angle (degree) 0.00f : internal friction angle (degree) 30.00
d 1: friction angle between earth and wall (degree) normal 20.00 (=2/3f)
d 2: friction angle between earth and earth (degree) normal 0.00
d E1: friction angle between earth and wall (degree) seismic 15.00 (=1/2f)
d E2: friction angle between earth and earth (degree) seismic 24.20
b : wall angle (degree) 0.00
c : cohesion of soil (t/m2) (do not consider) 0.00
kh : 0.18
Uc: Uplift coefficient 1.00
f : Friction Coefficient =Tan f b = 0.60
N-SPT : 50.00
Qa : Allowable bearing capacity normal t/m2 20.83 ( max. 20.83 t/m
Qae: Allowable bearing capacity seismic t/m2 31.25 ( max. 31.25 t/m
Normal condition Seismic condition
Concrete Design Strength sc kgf/m2 175 175
Creep strain coefficient (concrete) 0.0035 0.0035
ho
H5
H6B3
B6B5B4
HT
H10
H2
H1
H4
H3
B1 B2
BT
Hw1
Hw2
Slope 1:n
Rh1
Rb1
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2. Check
2.1 Stability Analysis
Overturning e= -0.32 m e= -0.62 m
BT / 6 = 1.50 m BT / 3 = 3.00 m
(e < BT/6) OK (e < BT/3) OK
Sliding Fs =Hu / H= 2.65 Fs =Hu / H= 1.26Fs > 2.00 OK Fs > 1.25 OK
Settlement Qmax = 13.19 t/m2 Qmax = 10.56 t/m2
(bearing capacity) Qmax < Qa OK Qmax < Qa OK
Qa = 20.8 t/m2 Qae= 31.3 t/m2
2.2 Structural Analysis
(1) Body Section A-A S
Normal Seismic Normal
Bar arrangement
Back face (tensile bar) f (mm) 25 25 25
(vertical) spacing (mm) 90 90 180
As (cm2) 273 273 136
Front face (compressive bar) f (mm) 25 25 25
(vertical) spacing (mm) 180 ok 180 ok 180
( As' > 0.5 As, cm2 ) 136 >=136.4 136 >=136.4 136 >
Hoop bar (horizontal) f (mm) 16
interval (mm) 200
Max interval (mm) 300
Design dimensions
Effective width (whole width) (cm) 500 500 500
Concrete cover : d1(cm) 7.5 7.5 7.5
d2(cm) 7.5 7.5 7.5
Effective height (cm) : d-d1(cm) 172.5 172.5 109.7
Design load Mf (t m) 704.25 1210.07 144.44
Nd (t) 321.86 255.17 219.11
S (t) 118.55 240.87 42.67
Checking of minimum reinforcement bar
Required bar (cm2) 258 356 53Checking of allowable stress as rectangular beam as column as rectangular bea
Compressive stress sc kgf/cm2 33 ok 58 ok 22 o
Bending stress ss kgf/cm2 1676 ok 2212 ok 1050 o
ss' kgf/cm2 - 787 ok -
Mean shearing stress tm kgf/cm2 1.54 ok 3.03 ok 3.04 o
(2) Footing Toe side Heel side
(Normal / Seismic) Normal
Bar arrangement
Upper (tensile bar) f (mm) 25
(bridge axis) spacing (mm) 150
As1 (cm2)
(compressive bar) f (mm) 25
(bridge axis) spacing (mm) 300 ok
As2' (cm2, >0.5 As2) 16.36 >=8.18(distribution bar) f (mm) 19 19
spacing (mm) 300 ok 100 ok
Aso (cm2, > As /3) 9.45 >=5.45 28.35 >=4.50
Lower (tensile bar) f (mm) 25
(bridge axis) spacing (mm) 300
As2 (cm2) 16.36
(compressive bar) f (mm) 25
(bridge axis) spacing (mm) 300 ok
As1' (cm2, >0.5 As1) 16.36 >=4.50
(distribution bar) f (mm) 19 19
spacing (mm) 150 ok 200 ok
Aso (cm2, >As /3) 18.90 >=5.45 14.18 >=5.45
Design dimensions
Effective width (unit width) (cm) 100 100
Concrete cover : d1(cm) 7.5 7.5
d2(cm) 7.5 7.5
Effective height (cm) : d-d1(cm) 92.5 92.5
Normal condition Seismic condition
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(3) Parapet With Impact Plate Without Impact Plate With Impact Plate
Normal Normal Seismic
Bar arrangement
Back face (tensile bar) f (mm) 12 16
(vertical) spacing (mm) 250 250
As1 (cm2) 8.04
(compressive bar) f (mm) 16
(vertical) spacing (mm) 250 ok
As1 (cm2, >As3/2) 8.04 >=8.04(distribution bar) f (mm) 12 12 12
(horizontal) spacing (mm) 250 250 ok 250
As2 (cm2, >As1/3) 4.52 >=4.50 4.52 >
Front face (tensile bar) f (mm) 16
(vertical) spacing (mm) 125
As3 (cm2, >As1/2) 16.08
(compressive bar) f (mm) 12 16
(vertical) spacing (mm) 125
As3 (cm2, >As1/2) 16.08 >
(distribution bar) f (mm) 12 16 16
(horizontal) spacing (mm) 250 ok 250
As6 (cm2, >As3/3) 8.04 >=5.36 8.04 >
Design dimensions
Effective width (unit width) (cm) 100 100
Concrete cover of fronf face (cm) 7
Concrete cover of back face (cm) 10 10
Effective height (cm) 33 30
Design load Mf (t m) 5.189 1.570
Nd (t) 0.000 0.000
S (t) 0.000 1.599
Checking of minimum reinforcement bar
Required bar (cm2) 10.78 3.14
Checking of allowable stress
Compressive stress 19.04 ok 12.92 o
Bending stress 1239.88 ok 722.95 o
Mean shearing stress 0 ok 0.59 o
(4) Impact Plate and Corbel
Impact PlateUpper Lower Upper
Bar arrangement
(main bar) f (mm) 16 19 19
spacing (mm) 300 ok 150 300
As1 (cm2) 6.70 >=4.50 18.90 9.45
(distribution bar) f (mm) 16 12 12
spacing (mm) 300 ok 250 ok 250
As2 (cm2, >As1/6) 6.70 >=4.50 4.52 >=4.50 4.52 >
Design dimensions
Effective width (unit width) (cm) 100 100 100
Concrete cover (cm) 5 5 7
Effective height (cm) 25 25 23
Design load Mf (t m) 5.818 3.146
Nd (t) - -
S (t) - -Checking of minimum reinforcement bar
Required bar (cm2) 14.73 8.66
Checking of allowable stress
Compressive stress 48.88 ok 37.88 o
Bending stress 1447.22 ok 1642.35 o
Mean shearing stress - -
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DIMENSIONS OF ABUTMENT
Super structure Type T-Beam
Dimensions
HT B1 B2 B3 B4 B5 B6 BT H1 H2 H3
13.05 0.90 0.40 0.40 2.25 1.80 4.95 9.00 1.45 10.00 0.60
H1 max 1.45
Hw1 Hw2 Rh1 Rb1 Width of impact plate (Corbel)
6.60 7.60 0.73 0.45
WEIGHT OF ABUTMENT
Bo
1.45
10.00
1: 0
2.60
13.05 11.450.00 0.00
10.00
6 00 8 60 So
H5
H6B3
B6B5B4
HT
H10
H2
H1
H4
H3
B1 B2
BT
Rh1
Rb1
B1 B2
ho
H5
H6
B3HT H10
H2
H1
Bimp
1
2
1
3
4
5
10
11
12
13
15
16
1718
19
2021
22'
22
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EARTH PRESSUREqs Parameters
qs : surcharge loa
q' : surcharge loa
g : unit weight o
1.45 g sat: unit weight o
w : ground surfa
f : internal fricti
d 1: friction angle
d 2: friction angle
d E1: friction angle
11.45 d E2: friction angle
13.05 b : wall angle (d
10.00 c : cohesion of s
kh :
w : ground surfa
f : internal fricti
6.60 7.60 d 1: friction angle
0.60 d 2: friction angle
1.00 d E1: friction angle
d E2: friction angle
b : wall angle (r
a : tan-1 kh (ra
9.00 d E: internal fricti
Uc: uplift coeffic
Earth Pressure
Normal Condition Seismic Condition
Description Description
Pa : active earth pressure (t/m2/m) 56.061 Pea : active earth p
Ka 1: coefficient of active earth pressure, earth and earth 0.333 Kea1 : coefficient ofKa 2: coefficient of active earth pressure, wall and earth 0.297
y : Vertical acting point 4.406 y : Vertical actin
X: Horizontal acting point = BT 9.0 X: Horizontal a
PV : Vertical Pressure = Pa sin d 0 PV : Vertical Pres
PH : Horizontal Pressure = Pa cos d 56.061 PH : Horizontal P
qa1 = 0.333 x 0.70 = 0.233 qa1 = 0.438
qa2 = 0.333 x 5.45 x 1.80 = 3.270 qa2 = 0.438
qa3 = 0.333 x 7.60 x 2.00 = 5.067 qa3 = 0.438
qw2 = -6.600 x 1.00 = -6.600 qw2 = -6.600
qu1 = -6.60 x 1.0 = -6.60 qu1 = -6.60
qu2 = -7.60 x 1.0 = -7.60 qu2 = -7.60
Normal condition Seismic condition
No. H Y HY No.
Pa1 = 0.233 x 13.050 = 3.045 6.525 19.869 Pa1= 0.000
Pa2 = 3.270 x 5.450 x 0.500 = 8.911 9.417 83.910 Pa2 = 4.301
Pa2' = 3.270 x 7.600 = 24.852 3.800 94.438 Pa2' = 4.301
Pa3 = 5.067 x 7.600 x 0.500 = 19.253 2.533 48.775 Pa3 = 6.664
Total (Pa) 56.061 4.406 246.991 Total
Pw2 = -6.600 x 6.600 x 0.500 = -21.780 2.200 -47.916 Pw2 = -6.600
Total -21.780 2.200 -47.916 Total
No. V X VX No.
Pu1 = -6.600 x 9.000 x 0.500 = -29.700 3.000 -89.100 Pu1 = -6.60
Pu2 = -7.600 x 9.000 x 0.500 = -34.200 6.000 -205.200 Pu2 = -7.60Total -63.900 4.606 -294.300 Total
Description
Description
HTH10
H2
H1
H4
H3
BT
qa1
qa2 qa3qw2qu1
qu2
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STABILITY ANALYSIS
Case 1 Normal Condition
1 Moment and Acting Point
Description V Load HLoad Distance (m) Moment (t.m)
V (t) H (t) X Y Mx My
Body 330.78 3.57 4.10 1181.55 0.00
Soil Toe 6.75 0.75 1.40 5.06 0.00
Heel 580.30 7.62 8.73 4420.13 0.00
Reaction (bridge) 137.96 0.00 2.70 11.60 372.50 0.00
Earth Pressure 0.00 280.31 9.00 4.41 0.00 1234.95
Hydrostatic pressure 0.00 (108.90) 2.20 (239.58)
Uplift pressure (319.50) 4.61 (1471.50)
Surcharge Load 20.48 0.00 6.73 0.00 137.69 0.00
S 756.76 171.41 4645.43 995.37
2 Stability Analysis
2.1 Over Turnng
e<=(BT/6) e= -0.323 m BT/6 is larger than e? OK
BT/6= 1.500 m
2.2 Sliding
Friction Coefficient =Tan f b = 0.60
Shearing registance force at base
Hu=V . Tan f b 454.06 tf
Safety Rate against sliding
Fs=Hu/H 2.649 Fs is larger than 2.0 ? OK
2.3 Settlement
Allowale bearing capacity Qa 20.83 tf/m2
Reaction from the Foundation
Maximiun Fondation Reaction Q max
Q max = 13.193 tf/m2 Qmax is smaller than Qa? OK
Minimum Fondation Reaction Q max
Q min = 20.441 tf/m2
Case 2 Seismic Condition
1 Moment and Acting Point
Description V Load HLoad Distance (m) Moment (t.m)
V (t) H (t) X Y Mx My
Body 330.78 59.54 3.57 4.10 1181.5 244.12
Soil Toe 6.75 0.75 1.40 5.06 0.00
Heel 580.3 104.45 7.62 8.73 4420.1 912.2
Reaction (bridge) 71.27 12.83 2.70 12.33 192.43 158.12
Earth Pressure 142.91 317.99 9.00 4.28 1286.2 1362.3
Hydrostatic pressure (108.90) 2.20 (47.92)
Uplift pressue (319.50) 4.61 (294.30)
Surcharge Load 0.00 0.00 9.00 4.41 0.00 0.00
S 812.5 385.91 6791 2628.8
2 Stability Analysis
2.1 Over Turnng
e<=(BT/3) e= -0.623 m BT/3 is larger than e? OK
2max(min)BTBL
M6
BTBL
VQ
×
±×
=
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Bearing Capacity of soil
(1) Design Data
fB = 30.00o
cB = 0.00 t/m2
gs' =
B = 9.00 m z = 1.60 m L =
(2) Ultimate Bearing Capacity of soil, (qu)
Calculation of ultimate bearing capacity will be obtained by appliying the following
Terzaghi's formula :
qu = a c Nc + gs' z Nq + b gs' B Ng
Shape factor (Table 2.5 of KP-06)
a = 1.21 b = 0.40
Shape of footing : rectangular, B x L
Shape of footing a
1 strip 1.002 square 1.30
3 rectangular, B x L 1.21
(B < L) (= 1.09 + 0.21 B/L)
(B > L) (= 1.09 + 0.21 L/B)
4 circular, diameter = B 1.30
Bearing capacity factor (Figure 2.3 of KP-06, by Capper)
Nc = 36.0 Nq = 23.0
f Nc Nq
0 5.7 0.0
5 7.0 1.4
10 9.0 2.7
15 12.0 4.520 17.0 7.5
25 24.0 13.0
30 36.0 23.0
35 57.0 44.0
37 70.0 50.0
39 > 82.0 50.0
a c Nc = 0.000
gs' z Nq = 36.800
b gs' B Ng = 72.000
qu = 108.80 t/m2
(3) Allowable Bearing Capacity of soil, (qa)
qa = qu / 3 = 36.27 t/m2
(safety factor = 3 , no
qae = qu / 2 = 54.40 t/m2
(safety factor = 2 , se
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STRUCTURAL CALCULATION
A ABUTMENT BODY
1 Load and Bending Moment of Abutment Body
Dimensions
B1 B2 B3 B5 H1
0.90 0.40 0.40 1.80 1.45
Hw1 Hw2
5.00 6.00
Abutment Width
Bw= 5.00 m Plat Form of Impact P
1.45 Seismic Coefficient kh= 0.18
Support from Parapet hs= 0.45
A-A section
Normal Seismic
Vertical Distance Moment Horizontal
No. Load X Mx Load
t/m m tf.m/m t/m
1 1.392 0.200 0.278 0.251
10.00 2 6.048 0.450 2.722 1.089
8.60 3 0.960 0.200 0.192 0.173
5.73 4 0.192 0.133 0.026 0.035
or 5 18.576 0.450 8.359 3.344
5.00 6.00 5' 9.288 -0.300 -2.786 1.672
10 0.216 -0.550 -0.119 0.039
11 0.108 -0.500 -0.054 0.019
S 36.780 8.618 6.620
Total 183.900 43.088 33.102
Section B-B
Where Hw1' is considered, this section is same as groundwater level.
Wehre Hw1' is not considered, this section is just half of (H1 + H2).
Distance AB: 6.00 m B-B section
Normal Seismic
Vertical Distance Moment Horizontal
No. Load X Mx Load
t/m m tf.m/m t/m
1 1.392 -0.514 -0.715 0.251
2 6.048 0.136 0.823 1.089
3 0.960 -0.514 -0.493 0.173
4 0.192 -0.447 -0.086 0.035
5 5.616 0.136 0.764 1.011
5' 1.698 -0.405 -0.687 0.306
10 0.216 -0.864 -0.187 0.039
11 0.108 -0.814 -0.088 0.019
S 16.230 -0.669 2.921
Total 81.149 -3.347 14.607
2 Load and Bending Moment due to Super Structure Normal Seismic
Vertical Distance Moment Horizontal Distance Moment Mi=
No. Load X Mx Load Y My Mx+My
t/m m tf.m/m t/m m tf.m/m tf.m/m
Section A-A
Normal Rd + Rl 137.962 0.45 62.083 0.00 0.00 0.00 62.083
Seismic Rd 71.272 0.45 32.072 12.83 10.97 140.69 172.763
Section B-B
Normal Rd + Rl 137.962 0.45 62.083 0.00 0.00 0.00 62.083
Seismic Rd 71.272 0.45 32.072 12.83 4.97 63.72 95.790
3 Load and Bending Moment due to Earth and Water Pressure
1) Section B-B
a) Normal Condition
ho
H5
H6
B3
B5
H2
H1
B1 B2
X
0.60Lp
A A
B B
(H1+H2)/2
Hw1'
(0,0)X
Y
5'
5
4
23
1
10
11
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b) Seismic Condition
qe1= q'*Kea qe1= 0.000 tf/m
qe2= (q'+g*H)*Kea qe2= 4.301 tf/m
EeH= (qe1+qe2)*(1/2)*H*cosd EaH= 11.320 tf/m
y= [H*(2qe1+qe2)]/[3*(qe1+qe2)] y= 1.817 m
S= EeH*Bw S= 56.599 tf
My= EeH*Bw*y My= 102.822 tf.m/m
where, q' Surcharge Load (seismic) 0 tf/m2
Kea coefficient of active earth pressure 0.438
g Unit weight of soil 1.8 tf/m3
d friction angle between earth and wall 0.2618 radian
H 5.45 m
y Acting Point (m)
S Shearing Force(tf)
Bw Abutment Width 5.00 m
2) Section A-A
a) Normal Condition
Description
EaH : active earth pressure (t/m2/m) = Pa . cos d 36.210
Ka2 : coefficient of active earth pressure 0.297y : Vertical acting point y= 3.884
S=EaH*Bw S= 181.051
My=S*y My= 703.241
qa1 = 0.297 x 0.70 = 0.208
qa2 = 0.297 x 5.45 x 1.80 = 2.917
qa3 = 0.297 x 6.00 x 2.00 = 3.568
qw2 = -5.000 x 1.00 = -5.000
No. H Y HY
Pa1 = 0.208 x 11.450 = 2.383 5.725 13.64
Pa2 = 2.917 x 5.450 x 0.500 = 7.948 7.817 62.12
Pa2' = 2.917 x 6.000 = 17.500 3.000 52.50
Pa3 = 3.568 x 6.000 x 0.500 = 10.703 2.000 21.40Total (Pa),per m 38.534 3.884 149.67
Pw2 = -5.000 x 5.000 x 0.500 = -12.500 1.667 -20.83
Total, per m -12.500 -20.83
Total (per width) width = 5.00 m -62.500 1.667 -104.16
b) Seismic Condition
Description
Pea : active earth pressure (t/m2/m) = Pa . cos d 51.489
Kea : coefficient of active earth pressure 0.438
y : Vertical acting point y= 3.763
S=EaH*Bw S= 257.443
My=S*y My= 968.728
qa1 = 0.438 x 0.00 = 0.000
qa2 = 0.438 x 5.45 x 1.80 = 4.301qa3 = 0.438 x 6.00 x 2.00 = 5.261
qw2 = -5.000 x 1.00 = -5.000
No. H Y HY
Pa1= 0.000 x 11.450 = 0.000 5.725 0.00
Pa2 = 4.301 x 5.450 x 0.500 = 11.719 7.817 91.60
Pa2' = 4.301 x 6.000 = 25.804 3.000 77.41
Pa3 = 5.261 x 6.000 x 0.500 = 15.782 2.000 31.56
Total (per m) 53.305 3.763 200.58
Pw2 = -5.000 x 5.000 x 0.500 = -12.500 1.667 -20.83
Total (per m) -12.500 -20.83
Total (per width) width= 5.00 m -62.500 1.667 -104.16
4 Summary of Intersectional Force
Normal Condition Seismic Condition
Description
Description
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5 Calculation of Required Reinforcement Bar as Rectangular Beam, Normal Conditio
1) Cracking Moment Section A-A
Mc= Zc*(s'ck + N/Ac) Mc= 90516242 kgf.cm/m
= 905 tf.m/m
where, Mc Cracking Moment kgf.cm
Zc Section Modulus
Zc=1/6*b*h12
b=100 cm 2,700,000 cm3
s'ck Tensile strength of Concrete (bending)
s'ck = 0.5*sck 2/3
15.6 kgf/cm2
s ck= 175 kgf/cm2
N Axial force 321,862 kg
Ac Area of Concrete = b*h1 18000 cm2
h1 thickness of section, B5 180 cm
b 500 cm
Section A-A
1) Design Bending Moment Mf= 704 tf.m/m
2) Required Bar Area As_req= Mf / (s sa*j*d)
As_req= 258 cm2
s sa= Allowable Stress R-bar 1850 kgf/cm2
j= 1 - k/3 0.854
k= n / (n + ssa / sca) 0.438
n= Young's modulus ratio 24
sca= Allowable Stress Concrete 60 kgf/cm2
d= Effective height = h1-d1 173 cm
d1= 7.5 cm
h1= 180 cm
3) Ultimate Bending Moment Mu= As*ssy { d - 0.5*[As*ssy]/[0.85*sck*b]}
Mu= 1,297 tf.m
Mu= Ultimate Bending Moment
As= Area of Tensile Bar
ssy= Yielding point of Tensile Bar (Spec >295 N/mm2) 3000 kgf/cm2
s'ck= Design Compressive Strength of Concrete 175 kgf/cm2
b= Effective Width 500 cm
4) Checking : Single or Double Bar Arrangement M1=
M1= 1,669 tf.m
M1= Resistance moment
Cs= { 2n / ( k*j ) }1/2
12.844
j= 1 - k/3 0.854
k= n / (n + ssa / sca) 0.438
n= ssa/sca 31
ssa= 1850 kgf/cm2
sca= 60 kgf/cm2
Check : M1 > Mf ? M1= 1,669 tf.m
Mf= 704 tf.m
Mf < M l : Tensile Bar Only M f < M l : Tens
(a) Tensile Bar
Max Bar Area : 2%*b*d As max = 1,725 cm2
Min Bar Area : 4.5%*b As min = 23 cm2
Estimation of Required Bar Area : As_req= 258 cm2
Apply f :
Required Bar Nos : b/pitch= 56 nos
Bar Area : As= 273 cm2
ok
Resistance Moment by Tensile bar As2 As1= Mf / {ssa*j*d}
As1= 258 cm2
As2= 14 cm2
25 @ 90
(d/Cs)2*ssa*b
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Bar Area : As' = 0 cm2 ok
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5) Checking of Allowable Stress
(a) Tensile Bar Only
Mf= 704 tf.m
S= 119 tf
ss = Mf/(As*j*d)= 1,676 kgf/cm2 ok
sc = 2*Mf/(k*j*b*d
2
)= 33 kgf/cm2 ok tm = S/(b*j*d)= 2 kgf/cm2 ok
p= As/(b*d)= 0.003
k= {(n*p)2+2*n*p}
1/2- n*p= 0.321
j= 1-k/3= 0.893
b= 500 cm
d= 172.5 cm
n= 24
(b) Tensile Bar & Compressive Bar
Mf= 0 tf.m
S= 0 tf
sc = Mf/(b*d2*Lc)= 0 kgf/cm2 ok
ss = n*sc*(1-k)/k= 0 kgf/cm2 ok
ss' = n*sc*(k-d2/d)/k= 0 kgf/cm2 ok
tm = S/(b*j*d)= 0 kgf/cm2 ok
p= As/(b*d)= 0.003
p'= p'=As'/(b*d)= 0.000
k= {n2(p+p')
2+2n(p+p'*d2/d)}
1/2-n(p+p')= 0.321
Lc= 0.5 k (1-k/3)+(np'/k) (k-d2/d)(1-d2/d)= 0.143
j= (1-d2/d)+k 2/{2*n*p*(1-k)}*(d2/d-k/3)= 0.893
b= 500 cm
d2= 0 cmd= 172.5 cm
n= 24
h d
x=kd
b
As
d1
h d
x=kd
b
As
As'
d2
d1
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6 Calculation of Required Reinforcement Bar as Column, Seismic Condition
1) Minimum Area as Column Section A-A
Acmin = N / (0.008*ssa+sca) 2,274 cm2
ssa= Allowable stress of Reinforcement bar 2775 kgf/m2
sca= Allowable stress of Concrete 90 kgf/m2
N= Axial force 255 tf
Acdes= b*h 90,000 > Acmin ok
Minimum Reinforcement Bar
(a) As a beam 4.5% * b As min= 23 cm2
(b) As a column 0.8% * Acmin As min= 18 cm2
Maximum Reinforcement Bar
(a) As a beam 2%*b*d As max = 1,725 cm2
(b) As a column 6% * Ac As max = 5,400 cm2
2) Required Reinforcement Bar
Design Bending Moment Mf= 1,210 tf.m
As_req= {[sc*(s/2)-N/(b*d)]/ssa}*b*d
As_req= 237 cm2
sc= Stress of concrete sc= 72.09 kg.cm2
Eq1= sc3
+ [3*ssa/(2*n)-3*Ms/(b*d2)]*sc
2- 6*Ms/(n*b*d
2)*ssa*sc - 3*Ms/(n
2*b*d
2)*ssa
2= 0
ssa= Allowable stress of Reinforcement Bar 2775 kg.cm2
Ms= Eccentric Moment, Ms=N(e+c) 1.42E+08 kgf.cm
e= Essentric Distance e=M/N 474.22 cm
M= Design Bending Moment 1,210 tf.m
N= Axial Force 255 tf
n= Young's Modulus Ratio 16
c= c=h/2 - d1 82.5 cm
h= Height of Section 180 cm
b= Width of section 500 cm
d1= Concrete Cover 8 cm
d= Effective Width of section d=h-d1 173 cms= n*sc/(n*sc+ssa) 0.294
[3*ssa/(2*n)-3*Ms/(b*d2)]= 232
6*Ms/(n*b*d2)*ssa= 9,936
3*Ms/(n2*b*d^2)*ssa
2= 861,643
sc (trial)= 72 sc (trial)
Eq1 (trial)= 0 ok Eq1 (trial
cross check 0 ok cross che
3) Ultimate Bending Moment
Mu= c*(h/2-0.4X)+Ts'(h/2-d2)+Ts(h/2-d1)
Mu= Ultimate Bending Moment (tf.m) Mu= 1,460 tf.m
Mu= Min (Mu1,Mu2) in case X>0 in case X<0
Mu1= 1.46E+08 1.86E+08
c= 0.68*sck*b*X 672859 -1155.34
sck= design strength of Concrete 175 kg/cm2
b= Width of section 500 cm
X= solve the equation Eq2 below 11.309 -9.709
Ts'= As'*Es*ecu*(X-d2)/X 293344 1543872
As'= Compressive Bar, As'=0.5 As 119
As= Required Reinforcement Bar (Tensile) 237
Es= Young's modulus (reinforcement bar) 2,100,000
ecu= Creep strain coefficient (concrete) 0
h= Height of Section 180 cm
d1= Concrete Cover (tensile side) 7.5 cm
d2= Concrete Cover (compressive side) 7.5 cm
Eq2 = a*X2
+ (b-Ts-N)*X-b*d2 = 0
a= 0.68*sck*b 50 59500
b= As'*Es*ecu 871013
T A * 711031
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4) Bar Arrangement
Max Bar Area : As max = 1,725 cm2
Min Bar Area : As min = 23 cm2
(a) Tensile Bar
Required Bar Area As req= 237 cm2
Apply f =
Column width b= 500 cm2
Bar Area As = 273 cm2 ok
(b) Compressive Bar
Required Bar Area As' req= 119 cm2
Apply f =
Column width b= 500 cm2
Bar Area As' = 136 cm2 ok
(c ) Hoop Bar
Minimum Diameter f' min = 12 mm
Apply f' = 16 mm
Bar Interval shall satisfy the following conditions:
d = 1725 mm
t < 12*f = 300 mm
t < 48*f '= 768 mm
then t = 200 mm ok
5) Checking of Allowable Stress, Seismic Condition
(a) Tensile Bar Only
Mf= 1,210 tf.m
S= 241 tf
ss = Mf/(As*j*d)= 2,828 kgf/cm2 check
sc = 2*Mf/(k*j*b*d2)= 66 kgf/cm2 ok
tm = S/(b*j*d)= 3 kgf/cm2 ok p= As/(b*d)= 0.00316
k= {(n*p)^2+2*n*p}^0.5 - n*p= 0.27149
j= 1-k/3= 0.90950
b= 500 cm
d= 172.5 cm
n= 16
(b) Tensile Bar & Compressive Bar
Mf= 1,210 tf.m
S= 241 tf
sc = Mf/(b*d2*Lc)= 60 kgf/cm2 ok
ss = n*sc*(1-k)/k= 2,793 kgf/cm2 check
ss' = n*sc*(k-d2/d)/k= 790 kgf/cm2 ok
tm = S/(b*j*d)= 3 kgf/cm2 ok
p= As/(b*d)= 0.003
p'= p'=As'/(b*d)= 0.002
k= {n2(p+p')
2+2n(p+p'*d2/d)}
1/2-n(p+p')= 0.254
Lc= 0.5 k (1-k/3)+(np'/k) (k-d2/d)(1-d2/d)= 0.137
j= (1-d2/d)+k 2/{2*n*p*(1-k)}*(d2/d-k/3)= 0.921
b= 500 cm
d2= 7.5 cm
d= 172.5 cm
n= 16
25 @ 90
25 @ 180
d1
d d2
h d
x=kd
b
As
d1
h d
x=kd
b
As'
d2
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7 Check for Stress of Concrete and Reinforcement bar as Column
Section A-A
Normal Seismic
Height of section h cm 180 180
Effective width b cm 500 500
Concrete cover d1 cm 7.5 7.5
d2 cm 7.5 7.5
Reinforcement bar As cm2 273 273
As' cm2 0 136
Morment Mf kgf/cm 7.04.E+07 1.21.E+08
Axcis force N kgf 321,862 255,172
Shearing force S kgf 118,551 240,874
Young's modulus ratio n 24 16
c 83 83
e 219 474
a1 386 1153
b1 23665 39405
c1 -4082130 -5105274
Neutral line x 72 51
0 0
ok ok
a2 18005 12697
b2 66 73
b3 7497 7088
b4 65 43
b5 7497 7088
b6 100 122
Stressing sc 29.04 ok 57.70 ok
ss 972.30 ok 2212.39 ok
ss' 624.33 ok 786.83 ok
tc 1.49 ok 3.03 ok
SUMMARY OF DESIGN CALCULATIONSection A-A
Description Abbr. unit
Calculation Condition Column
Princi ple Dimensions
Concrete Design Strength sc kgf/m2 175 175
Effective width of section b cm 500 500
Height of Section h cm 180 180
Concrete Cover (tensile) d1 cm 7.5 7.5
Concrete Cover (compressive) d2 cm 7.5 7.5
Effective height of Section d cm 172.5 172.5
Allowable Stress Concrete sca kgf/m2 60 90
Re-Bar ssa kgf/m2 1850 2775
Shearing ta kgf/m2 5.5 8.25
Yielding Point of Reinforcement Bar ssy kgf/cm2 3000 3000
Reinfor cement Bar
Tensile Bar Required As_req. cm2 258 237Designed As cm2 273 273
Compressive Bar Required As'_req. cm2 0 119
Designed As' cm2 0 136
Hoop Bar Designed Aso
Design L oad
Design Bending Moment Mf tf.m 704 1,210
Design Axis Force Nd tf 322 255
Shearing Force S tf 119 241
Checking of M inimum Re-Bar
Ultimate Bending Moment Mu tf.m 1,297 1,460Max Re-bar As max cm2 1,725 1,725
Min Re-bar As min cm2 23 23
Required Bar As req cm2 258 356
D25@180
D16@200
D25@90 D25@90
Normal Condition
Rectangular Beam
Seismic Condition
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B FOOTING
1 Load and Bending Moment of Footing
1) Computation Conditions
Normal Condition Toe Side
Heel Side
Seismic Condition
2) Footing
Dimensions
B4 B5 B6 B
2.25 1.80 4.95 9.Abutment Width
Bw= 5.00 m
Unit Weight of Material
Soil 1800 kgf/m
Concrete 2400 kgf/m
Surcharge Load q 700 kgf/m
q'= q seismic 0 kgf/m
Toe Side normal condition seismic condition
Area unit Vertical Distance Moment Horizontal Distance Moment
No. weight Load X Mx Load Y My
m2 tf/m3 tf/m m tf.m/m tf/m m tf.m/m
6 0.675 2.4 1.620 0.750 1.215 0.292 1.200 0.350
F1 2.250 2.4 5.400 1.125 6.075 0.972 0.500 0.486
sub-total 7.020 7.290 1.264 0.836
Distance l1 l1 (X) 1.038 m l1 (Y) 0.662 m
Heel Side normal condition seismic condition
Area unit Vertical Distance Moment Horizontal Distance Moment
No. weight Load N X Mx Load Y My
m2 tf/m3 tf/m m tf.m/m tf/m m tf.m/m
8 1.485 2.400 3.564 1.650 5.881 0.642 1.300 0.834
F3 4.950 2.400 11.880 2.475 29.403 2.138 0.500 1.069
sub-total 15.444 35.284 2.780 1.903
Distance l2 l2 (X) 2.285 m l2 (Y) 0.685 m
3) Earth Pressure, Heel Side Only
Normal Condition Seismic Conditio
Dead Load (soil) W1= 116.060 tf/m We1= 1
Distance l3 =Xo-(B4+B5) l3 = 2.379 m l3 =
Bending Moment Md Md= 276 157 tf m/m Mde= 2
BT
Q
X
BT
Q maxQ min
B4
Ra=Qmax
B6
Ra'
l 2
M
(0,0)
B6B5B4
H4
H3
BT
F1 F2 F3
7 86
9
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4) Reaction from Foundation
Reaction from the Foundation
Normal Q max 13.193 tf/m2
Qmin 20.441 tf/m2
Seismic Qmax 10.560 tf/m2
Qmin 25.552
X 9.000 m
Reaction from Foundation, Toe Side
Normal Condition
Rat= Q max Rat= 13.193 tf/m2 Cantilever length
Ra't= Q max-(B4/BT)*(Q max - Qmin) Ra't= 15.005 tf/m2
Seismic Condition
Reat= Q Reat= 10.560 tf/m2 Cantilever length
Rea't= Q*(X-B4)/X Reat'= 7.920 tf/m2
Reaction from Foundation, Heel Side
Normal Condition
Rah= Q min Rah= 20.441 tf/m2 Cantilever length
Ra'h= Q max-[(B4+B5)/BT]*(Q max - Qmin) Ra'h= 16.455 tf/m2
Seismic ConditionReah'= Q*(X-B4-B5)/X Rea'h= 17.306 tf/m2 Cantilever length
Reah= Qmin Reah= 25.552 tf/m2
Reah'= Q*(X-B4-B5)/X Rea'h= 5.808 tf/m2 Cantilever length
Reah= 0 Reah= 0.000 tf/m2
Reah'= Q*(X-B4-B5)/X Rea'h= 17.306 tf/m2 Cantilever length
Reah= Qmin Reah= 25.552 tf/m2
5) Intersectional Force due Reaction
Axial Force = 0 tf/m
Toe Section Heel
Description Moment Shearing Moment Shearing Moment She
M S Me Se M
(tf.m/m) (tf/m) (tf.m/m) (tf/m) (tf.m/m) (tf
Footing -7.290 -7.020 -7.290 -7.020 35.284 1Dead Load, Earth 276.157 11
Surcharge Load 8.576
Earth Pressure 42.284 1
Reaction form Foundation 34.924 31.723 24.502 20.790 -234.147 -9
Total - per m 27.634 24.703 17.212 13.770 128.153 5
Total -5 m 138.169 123.514 86.060 68.848 640.765 28
2 Calculation of Required Reinforcement Bar :
1) Design Bending Moment ( Mf )
Normal Condition M= 27.634 tf.m/m
Seismic Condition Me= 17.212 tf.m/mMax. Design Bending Moment Mf= 27.63 tf.m/m
2) Required Bar Area
As= Mf / (s sa*j*d) 11.47 cm2
s sa= Allowable Stress R-bar 1850 kgf/cm2
j= 1 - k/3 0.854
k= n / (n + ssa / sca) 0.438
n= Young's modulus ratio 24
sca= Allowable Stress Concrete 60 kgf/cm2
3) Ultimate Bending Moment
Mu=As*s sy{d-(1/2)*[As*s sy]/[0.85*s ck*b]} Mu= 5.21E+06 kgf.cm
52.07 tf.mwhere, Mu Ultimate Bending Moment
As Area of Tensile Bar
s sy Yielding point of Tensile Bar 3000 kgf/cm2 (Spec >295 N/mm2)
Normal CondiSeismic Condition Normal Condition
Toe Section
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(a) Tensile Bar
Max Bar Area : 2%*b*d = 305.00 cm2
Min Bar Area : 4.5%*b = 4.50 cm2
Required Bar Area As req= 11.47 cm2
Apply f =
Required Bar Nos Nos=b/pitch = 3.333333 nos
Bar Area As = 16.36 cm2 ok
(b) Compressive Bar, in case M1<Mf
M' = Mf - M1
M'= 0.00 tf.m
As' = M' / [ssa*(d - d2)]
Required Bar Area As'= 0.00 cm2
d= 152.5 cm
d2= 0.00 cm
ssa= 1850 kgf/cm2
Apply f =
Bar Area As' = 0.00 cm2 ok
5) Checking of Allowable Stress
(a) Tensile Bar Only
Mf= 27.63 tf.m/m
S= 24.70 tf/m
ss = Mf/(As*j*d)= 1,187.67 kgf/cm2 ok
sc = 2*Mf/(k*j*b*d2)= 12.58 kgf/cm2 ok
tm = S/(b*j*d)= 1.74 kgf/cm2 ok
p= As/(b*d)= 0.00 b= 100 cm
k= {(n*p)2+2*n*p}
1/2- n*p= 0.20 d= 152.5 cm
j= 1-k/3= 0.93 n= 24
(b) Tensile Bar & Compressive Bar
Mf= 27.63 tf.m
S= 24.70 tf
sc = Mf/(b*d2*Lc)= 12.58 kgf/cm2 ok
ss = n*sc*(1-k)/k= 1,187.67 kgf/cm2 ok
ss' = n*sc*(k-d2/d)/k= 301.84 kgf/cm2 ok
tm = S/(b*j*d)= 1.74 kgf/cm2 ok
p= As/(b*d)= 0.00
p'= p'=As'/(b*d)= 0.00 b= 100 cm
k= {n2(p+p')
2+2n(p+p'*d2/d)}
1/2-n(p+p')= 0.20 d= 152.5 cm
Lc= 0.5 k (1-k/3)+(np'/k) (k-d2/d)(1-d2/d)= 0.09 d2= 0.00 cm
j= (1-d2/d)+k 2/{2*n*p*(1-k)}*(d2/d-k/3)= 0.93 n= 24
3 Calculation of Required Reinforcement Bar : ( Normal Condition )
1) Design Bending Moment Me>0
Normal Condition M= 128.153 tf.m/m
Seismic Condition Me= 75.755 tf.m/m
Mf= 128.15 tf.m/m
2) Required Bar Area
As= Mf / (s sa*j*d) 53.18 cm2
s sa= Allowable Stress R-bar 1850 kgf/cm2
j= 1 - k/3 0.854
k= n / (n + ssa / sca) 0.438
n= Young's modulus ratio 24
sca= Allowable Stress Concrete 60 kgf/cm2
3) Ultimate Bending Moment
Mu=As*s sy{d-(1/2)*[As*s sy]/[0.85*s ck*b]} Mu= 23475776 kgf.cm
= 234 76 tf m
Heel Section
25 @ 300 d1
h d
h
d1
d
h
h
Tensile
Com ressivee
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Max Bar Area : 2%*b*d = 320.00 cm2
Min Bar Area : 4.5%*b = 4.50 cm2
Required Bar Area As req= 53.18 cm2
Apply f =
Required Bar Nos Nos=b/pitch = 6.666667 nos Pitch shall be same as that of toe
Bar Area As = 32.72 cm2 check or arrange compressive bar
(b) Compressive Bar, in case M1<Mf
M' = Mf - M1 M'= 0.00 tf.m
As' = M'/[ssa*(d - d2)] As'= 0.00 cm2
d= 152.5 cm
d2= 0.00 cm
Required Bar Area As' req= 0.00 cm2
Apply f =
Bar Area As' = 0.00 cm2 ok
5) Checking of Allowable Stress
(a) Tensile Bar Only
Mf= 128.15 tf.m/m
S= 56.47 tf/mss = Mf/(As*j*d)= 2,825.55 kgf/cm2 check check
sc = 2*Mf/(k*j*b*d2)= 44.33 kgf/cm2 ok ok
tm = S/(b*j*d)= 4.07 kgf/cm2 ok ok
p= As/(b*d)= 0.00 b= 100 cm
k= {(n*p)2+2*n*p}
1/2- n*p= 0.27 d= 152.5 cm
j= 1-k/3= 0.91 n= 24
(b) Tensile Bar & Compressive Bar
Mf= 128.15 tf.m
S= 56.47 tf
sc = Mf/(b*d2*Lc)= 44.33 kgf/cm2 ok
ss = n*sc*(1-k)/k= 2,825.55 kgf/cm2 check
ss' = n*sc*(k-d2/d)/k= 1,063.96 kgf/cm2 ok
tm = S/(b*j*d)= 4.07 kgf/cm2 ok p= As/(b*d)= 0.00
p'= p'=As'/(b*d)= 0.00
k= {n2(p+p')
2+2n(p+p'*d2/d)}
1/2-n(p+p')= 0.27 b= 100 cm
Lc= 0.5 k (1-k/3)+(np'/k) (k-d2/d)(1-d2/d)= 0.12 d= 152.5 cm
j= (1-d2/d)+k 2/{2*n*p*(1-k)}*(d2/d-k/3)= 0.91 d2= 0.00 cm
n= 24
4 Calculation of Required Reinforcement Bar : ( Seismic Condition )
1) Design Bending Moment Me>0
Normal Condition M= 128.153 tf.m/m
Seismic Condition Me= 75.755 tf.m/m
Mf= 75.76 tf.m/m
2) Required Bar Area
As= Mf / (s sa*j*d) 20.20 cm2
s sa= Allowable Stress R-bar 2775 kgf/cm2
j= 1 - k/3 0.886
k= n / (n + ssa / sca) 0.438
n= Young's modulus ratio 16
sca= Allowable Stress Concrete 90 kgf/cm2
3) Ultimate Bending Moment Mu= 9.12E+06 kgf.cm
= 91.19 tf.m
where, Mu Ultimate Bending Moment
As Area of Tensile Bar
s sy Yielding point of Tensile Bar 3000 kgf/cm2 (Spec >295 N/mm2)
Heel Section
25 @ 150
d1
h d
h
d1
d
h
h
Tensile
Com ressivee
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(a) Tensile Bar
Max Bar Area : 2%*b*d = 0.00 cm2
Min Bar Area : 4.5%*b = 4.10 cm2
Required Bar Area As req= 20.20 cm2
Apply f =Required Bar Nos Nos=b/pitch = 6.666667 nos
Bar Area As = 32.72 cm2 check or arrange compressive bar
(b) Compressive Bar, in case M1<Mf
M' = Mf - M1 M'= 0.00 tf.m
As' = M'/[ssa*(d - d2)] As'= 0.00 cm2
d= 152.5 cm
d2= 0.00 cm
Required Bar Area As' req= 0.00 cm2
Apply f =
Bar Area As' = 0.00 cm2 ok
5) Checking of Allowable Stress
(a) Tensile Bar Only
Mf= 75.76 tf.m/m
S= 38.67 tf/mss = Mf/(As*j*d)= 1,643.98 kgf/cm2 ok
sc = 2*Mf/(k*j*b*d2)= 30.68 kgf/cm2 ok
tm = S/(b*j*d)= 2.75 kgf/cm2 ok
p= As/(b*d)= 0.00 b= 100 cm
k= {(n*p)2+2*n*p}
1/2- n*p= 0.23 d= 152.5 cm
j= 1-k/3= 0.92 n= 16
(b) Tensile Bar & Compressive Bar
Mf= 75.76 tf.m
S= 38.67 tf
sc = Mf/(b*d2*Lc)= 30.68 kgf/cm2 ok
ss = n*sc*(1-k)/k= 1,643.98 kgf/cm2 ok
ss' = n*sc*(k-d2/d)/k= 490.93 kgf/cm2 ok
tm = S/(b*j*d)= 2.75 kgf/cm2 ok p= As/(b*d)= 0.00
p'= p'=As'/(b*d)= 0.00
k= {n2(p+p')
2+2n(p+p'*d2/d)}
1/2-n(p+p')= 0.23 b= 100 cm
Lc= 0.5 k (1-k/3)+(np'/k) (k-d2/d)(1-d2/d)= 0.11 d= 152.5 cm
j= (1-d2/d)+k 2/{2*n*p*(1-k)}*(d2/d-k/3)= 0.92 d2= 0.00 cm
n= 16
SUMMARY OF DESIGN CALCULATION, FOOTING
Description Abbr. unit
Calculation Condition Normal Normal S
Principle Dimensions
Concrete Design Strength sc kgf/m2 175 175Effective width of section b cm 100 100
Height of Section, H4 h cm 100 100
Concrete Cover (tensile) d1 cm 7.5 7.5
Concrete Cover (compressive) d2 cm 0 0
Effective height of Section d cm 92.5 92.5
Allowable Stress Concrete sca kgf/m2 60 60
Re-Bar ssa kgf/m2 1850 1850
Shearing ta kgf/m2 5.5 5.5
tma kgf/m2 14 14
Yielding Point of Reinforcement Bar ssy kgf/cm2 3000 3000
Reinforcement Bar
Tensile Bar Required As req. cm2 11.47 53.18
Designed As cm2 16.36 32.72
Compressive Bar Required As' req. cm2 0.00 0.00
Designed As' cm2 0.00 0.00
Design Load
D25@300 D25@150
Toe Side Heel Side
25 @ 150
d1
h d
h
d1
d
h
h
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C PARAPET WALL
1 Sectional Force without Impact Plate
(1) Rear Face Reinforcement Bar Mo= Mp + Me
So= Sp + Ph
where,
Mo Bending Moment at Parapet (
So Shearing Force at Platform (tf
Mp Bending Moment due T-Loa
Me Bending Moment due Earth P
Sp Shearing Force dueT-Load (tf
Ph Earth Pressure (tf/m)
1) Sectional Force due to T-Load
Mp= Ka T/1.375*{-H1+(H1+a)*ln[(a+H1)/a] 4.393 tfm
Sp= Ka T/1.375*ln[(a+H1)/a] 4.563 tf
where, Ka Coefficient of active earth pressure 0.297
T Wheel load of T-Load 10.000 tf
a contact width of T-load 0.200 m
H1 Height of Parapet 1.450 m
2) Sectional Force due to Earth Pressure
Ph= 0.5 g *Kah*H1^2 Ph= 0.554 tf
Me= (1/3)*Ph*H1 Me= 0.268 tfm
where, Kah Ka*cos d 0.293
d friction angle between the parapet wall and soil = (1/3)f 0.175 (radian)g Unit Weight of Soil 1.800 tf/m3
H1 Height of Parapet 1.450 m
3) Summary of Sectional Force
Mo= Mp + Me 4.661 tfm
So= Sp + Ph 5.117 tf
2. Sectional Force with Impact Plate
(1) Front Face Reinforcement Bar (compute under normal condition)
Rf= (1/2)*Wd*Lo Rf= 3.105 tf/m
Rp= T/1.375 Rp= 7.273 tf/m
R= Rf + Rp R= 10.378 tf/m B2= 0.40 m
Lx= (1/2)*B2+Bu Lx= 0.500 m Bu= 0.30 mMf= R*Lx Mf= 5.189 tfm/m
where Rf Reaction due self weight Wd tf
a
b
H1
gKaH1
T-Load Earth Pressure
B1 B2 Bu
Ds
Ft
R
Lx
Lo
L=0.7 Lo
w1
w2
Lo-Bu
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(2) Rear Face Reinforcement Bar (compute under seismic condition)
1) Sectional Force due to Impact Plate
Rh= 2*Rf*Kh 1.118 tf/m Lp= 0.300 m (= Bu)
Mr = Rh*Yr 1.285 tfm/m
where, Kh seismic coefficient 0.18Yr = H1-Lp = 1.150 m
2) Sectional Force due to Earth Pressure
H1 > Ds ? H1= 1.450 m
H1-Ds= 0.750 m
Peh 1= (1/2)*g*Kah*Lp^2 0.024 tf/m
Me 1= Peh*[(Lp)*(1/3)+(H1-Lp)] 0.030 tfm/m
Peh 2= (1/2)*g*Kah*he^2 0.148 tf/m
Me 2= (1/3)*Peh*he 0.037 tfm/m
then Peh =Peh 1+ Peh2 0.172 tf/m
Me =Me 1+Me2 0.067 tfm/m
3) Intersectional Force of Parapet due to Earth Pressure
Section Area Unit Weight Kh Se
(m2) Weight (tf) W
G
1 0.580 2.4 1.392 0.18
10 0.090 2.4 0.216 0.18
11 0.045 2.4 0.108 0.18
S
Note: if H1 < Dc, areas 10 & 11 w
4) Summary of Intersectional Force
Mo= Mr+Me+Mg 1.570 tfm/m
So= Rh+Reh+Gh 1.599 tf/m
3. Calculation of Required Reinforcement Bar
1) Cracking Moment
Mc= Zc*(s'ck + N/Ac) Mc= 417155 kgf.cm = 4.172 tf.m
where, Mc Cracking Moment kgf.cm
Zc Sectional Coefficient
Zc=b*B2^2/6 b=100 cm 26667 cm3
s'ck Tensile strength of Concrete (bending)s'ck = 0.5*sck^(2/3) 15.64 kgf/cm2
s ck= 175 kgf/cm2
N Axis force (=0) 0
B1 B2 Bu
Ds
FtR H
Lo
heYr
H1 H1
g K ah he
B5
B2
Lp
Lp
Lp
H1 110
11
B1
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3) Ultimate Bending Moment
Mu=As*s sy{d-(1/2)*[As*s sy]/[0.85*s ck*b]} Mu= 955213 kgf.cm = 9.552
where, Mu Ultimate Bending Moment tf.m
As Area of Tensile Bar cm2
s sy Yielding point of Tensile Bar 3000 kgf/cm2 (Spec >295 N/mm2)d Effective height = B2-cover 33 cm
cover d1= 7 cm
B2 = 40 cm
s'ck Design Compressive Strength of Concrete 175 kgf/cm2
b Effective Width 100 cm
As=Mf/(s sa*j*d) 9.951 cm2
s sa= Allowable Stress Rbar 1850 kgf/cm2
j= 1 -k/3 (=8/9 ) 0.854
or k = n/{n+s sa/s ca)
n= Young's modulus ratio 24
s ca Allowable Stress Concrete 60 kgf/cm2
Check Mu & Mc Mu = 9.552 tf.m
Mc = 4.172 tf.m Mu>Mc? ok
4) Bar Arrangement
(a) Front Face, with Impact Plate
Max Bar Area As max = 0.02*b*d = 66.0 cm2 Concrete Cover d1= 7
Min Bar Area As min = b*4.5%= 4.5 cm2 Then d= 33
Required Bar Area As req= 10.780 cm2
Apply f = 16 @ 125 mm
Bar Area As = 16.085 cm2 ok
(b) Rear Face, without Impact Plate
Max Bar Area As max = 0.02*b*d = 60.0 cm2 Concrete Cover d1= 10
Min Bar Area As min = b*4.5%= 4.5 cm2 Then d= 30
Required Bar Area As req= cm2
Apply f = 12 @ 250 mm spacing of body, tensile f 25
Bar Area As = cm2
(c) Rear Face, with Impact Plate
Max Bar Area As max = 0.02*b*d = 60.0 cm2 Concrete Cover d1= 10
Min Bar Area As min = b*4.5%= 4.5 cm2 Then d= 30
Required Bar Area As req= 3.143 cm2
Apply f = 16 @ 250 mm spacing of body, tensile f 25
Bar Area As = 8.042 cm2 ok
5) Checking of Allowable Stress
(a) Front Face, with Impact Plate
Mf (front) 5.189 tf.m Concrete Cover d1= 7
S 0.000 tf Then d= 33
ss = Mf/(As*j*d) 1239.88 kgf/cm2 check ss < ssa ? ok
sc = 2*Mf/(k*j*b*d^2) 19.04 kgf/cm2 check sc < sca ? ok
p=As/(b*d) 0.0230
k={(n*p)^2+2*n*p}^0.5 - n*p 0.6347
j= 1-k/3 0.7884
(b) Rear Face, without Impact Plate
Mf (rear) 4.661 tf.m Concrete Cover d1= 10
So 5.117 tf Then d= 30
ss = Mf/(As*j*d) kgf/cm2 check ss < ssa ?
sc = 2*Mf/(k*j*b*d^2) kgf/cm2 check sc < sca ?
tm = S/(b*j*d) kgf/cm2 check tm < ta ?
p=As/(b*d)
k={(n*p)^2+2*n*p}^0.5 - n*p
j= 1-k/3
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4. Summary of Design Calculation
Description Abbr. unit Front Face Back Face
Provision on Impact Plate Yes No Yes
Calculation Condition Normal Normal Seismic
Principle Dimensions
Concrete Design Strength sc kgf/m2 175 175 175
Effective width of section b cm 100 100 100
Height of Parapet B2 cm 40 40 40
concrete cover (tensile) d1 cm 7 10 10
concrete cover (compressive) d2 cm 0 0 0
Effective width of Parapet d cm 33 30 30
Allowable Stress Concrete sca kgf/m2 60 60 90
Re-Bar ssa kgf/m2 1850 1850 2775
Shearing ta kgf/m2 5.5 5.5 8.25
Yielding Point of Reinforcement Bar ssy kgf/cm2 3000 3000 3000
Reinforcement Bar
Tensile Bar Required As req. cm2 10.78 3.14
Tensile Bar Designed As cm2 16.08 8.04D16@125 D16@250
Design Load
Design Bending Moment Mf tf.m 5.189 4.661 1.570
Design Axis Force Nd tf 0.000 0.000 0.000
Shearing Force S tf 0.000 5.117 1.599
Checking of Minimum Re-Bar
Cracking Moment Mc tf.m 4.172 4.172 4.172
1.7*Mf 8.821 7.924 2.669
1.7*Mf < Mc ? If no, check Mu check Mu ok
Ultimate Bending Moment Mu tf.m 9.552
Mu > Mc ? ok
Max Re-bar As max cm2 66.0 60.0 60.0
Min Re-bar As min cm2 4.5 4.5 4.5
Required Bar As req. cm2 10.780 3.143
Area of Re-bar for Design As cm2 16.085 8.042
Checking of Allowable Stress
Young's Modulus Ratio n 24 24 16
Effective height d cm 33 30 30
Compressive Stress sc kgf/cm2 19.04 12.92
Bending Tensile Stress ss kgf/cm2 1239.88 722.95
Mean Shearing Stress tm kgf/cm2 0 0.59
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ABUTMENT : Bendung ….
0.90 0.40
D16@200 D25@180
+ 80.45
D16@200
1.45
+ 79.00
0.40
0.40
D16@200
10.00
11.45
13.05
8.60
5.00
D19@100
+
0.60
2.50
1.00+
D25@300 D25@300
9.00
1.80 4.952.25
D19@150
1.00
D16@200
D16@200
D25@150
D16@200
D25@150
D16@200
D19@100
D25@90
D25@180
D25@180
D25@180
D16@200
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D IMPACT PLATE AND CORBEL
1 Design Parameters
Active load T-Load
Impact plate Length L= 3.00 m Span length Ls = 0.7*L= 2.10 mThickness h1= 0.30 m Width of corbel Lp= 0.30 m
Effective width of road B= 3.00 m Height of corbel h2= 0.30 m
Unit weight of plate gc = 2.40 tf/m3
Unit weight of soil gs = 1.80 tf/m3 Cover of R-bar
Soil depth above plate Ds= 0.05 m Impact plate d1= 5 cm
Thickness of pavement Dp= 0.05 m Corbel d3= 7 cm
2 Computation of Intersectional Force, Corbel
1) Dead Load
Impact plate 0.72 tf/m2
Soil above plate 0.09 tf/m2
Total dead load Wd= 0.81 tf/m2
2) Intersectional Force due Dead Load
Md= (1/8)*Wd*Ls^2 0.446513 tf.m
3) Intersectional Force due Live Load
wL=2*T*(1+ i)/{2.75*(a+2*d)} wL = 33.39051 tf/m2
ML={(1/4)*wL*Ls*(a+2*d)-(1/8)*wL*(a+2*d)^2}*a ML= 5.371698 tf.m
where, ML bending moment due live load
T: wheel load of T-load 10.00 tf
a contact width of T-load 0.20 m
i: impact coefficient
i=20/(50+L)= 0.377
Dp: thickness of pavement 0.05 m
a: coefficient 1.10
4) Total Intersectional Force
M=Md+ML 5.818211 tf.m
3 Corbel1) Intersectional Force due Impact Plate
M1=R*bu M1= 3.113 tf.m
where, R total reaction form corbel 10.378 tf.m/m
bu width of corbel =Lp 0.300 m
2) Intersectional Force due Corbel
M2=(1/6)*(2w1+w2)*gc*bu^2 M2= 0.032 tf.m
where, w1 0.15 m
w2 0.60 m
gc = 2.40 tf/m3
bu 0.30 m
3) Total Intersectional Force
M=M1+M2 3.146 tf.m
3 Calculation of Required Reinforcement Bar for Impact Plate1) Cracking Moment
Mc= Zc*(s'ck + N/Ac) Mc= 234650 kgf.cm = 2.346 tf.m
h M ki t k f
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2) Checking of Cracking Moment and Design Bending Moment
Design bending moment Mf 5.818 tf.m
Check Mf & Mc 1.7*Mf>Mc?, if yes check ultimate bending moment
1.7*Mf = 9.891 tf.mMc= 2.346 tf.m 1.7*Mf>Mc? Yes, check ultimate bending mome
3) Ultimate Bending Moment
Mu=As*s sy{d-(1/2)*[As*s sy]/[0.85*s ck*b]} Mu= 1039032 kgf.cm = 10.390
where, Mu ultimate bending moment tf.m
As area of tensile bar cm2
s sy yielding point of tensile bar 3000 kgf/cm2 (Spec >295 N/mm2)
d effective height = h1-cover 25 cm
cover d1= 5 cm
h1= 30 cm
s'ck design compressive strength of concrete 175 kgf/cm2
b effective width 100 cm
As=Mf/(s sa*j*d) 14.729 cm2s sa= allowable stress of reinforcement bar 1850 kgf/cm2
j= 1 -k/3 (=8/9 ) 0.854
or k = n/{n+s sa/s ca)
n= Young's modulus ratio 24
s ca allowable stress of concrete 60 kgf/cm2
Check Mu & Mc Mu = 10.390 tf.m
Mc = 2.346 tf.m Mu>Mc? ok
4) Bar Arrangement
Checking of single or double bar arrangement
M1= (d/Cs)^2*ssa*b >Mf? M1= 700936 kgf.cm = 7.009 tf.m
where, M1 resistance moment
Cs ={2m/[s*(1-s/3)]}^(1/2) 12.844
s (n*sca)/(n*sca+ssa) 0.438
m ssa/sca 30.833
ssa 1850 kgf/cm2
sca 60 kgf/cm2
n 24
Check M1 > Mf? M1= 7.009 tf.m M1>Mf : Design Tensil e Bar Onl y
Mf= 5.818 tf.m
(a) Tensile Bar
Max bar area As max = 0.02*b*d = 50.0 cm2Min bar area As min = b*4.5%= 4.5 cm2
Required bar area As req= 14.729 cm2
Apply f = 19 @ 150 mm
Bar area As = 18.902 cm2 ok
(b) Compressive Bar, in case M1<Mf
M' = Mf - M1=ssa*As'*(d - d2)
As' = M'/[ssa*(d - d2)] As'= 0.000 cm2
d= 25 cm M1= 7.009 tf.m
d2= 0 cm Mf= 5.818211 tf.m
ssa= 1850 kgf/cm2
Required bar area As' req= 0.000 cm2Apply f = 16 @ 300 mm
Bar area As' = 6.702 cm2 ok
d1
h d
h
d1
d
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5) Checking of Allowable Stress
(a) Tensile Bar Only
Mf 5.818211 tf.m
S 0 tf
ss = Mf/(As*j*d) 1447.22 kgf/cm2 check ss < ssa ? ok
sc = 2*Mf/(k*j*b*d^2) 48.88 kgf/cm2 check sc < sca ? ok
p=As/(b*d) 0.0076 b= 100 cm
k={(n*p)^2+2*n*p}^0.5 - n*p 0.4477 d= 25 cm
j= 1-k/3 0.8508 n= 24
(b) Tensile Bar & Compressive Bar
Mf 5.818211 tf.m
S 0.000 tf
sc = Mf/(b*d^2*Lc) 38.88 kgf/cm2 check sc < sca ? ok
ss = n*sc*(1-k)/k 1371.70 kgf/cm2 check ss < ssa ? ok
ss' = n*sc*(k-d2/d)/k 933.07 kgf/cm2 check ss' < ssa ? ok
p=As/(bd) 0.0076
p'=As'/(bd) 0.0027
k={n^2(p+p')^2+2n(p+p'*d2/d)}^05-n(p+p') 0.4048
Lc=(1/2)k(1-k/3)+(np'/k)(k-d2/d)(1-d2/d) 0.2394
b= 100 cm
d= 25 cm
d2= 0 cm
n= 24
4 Calculation of Required Reinforcement Bar for Corbel1) Cracking Moment
Mc= Zc*(s'ck + N/Ac) Mc= 234650 kgf.cm = 2.346 tf.m
where, Mc cracking moment kgf.cm
Zc section modulus
Zc=b*h2^2/6 15000 cm3
b= 100 cm
s'ck tensile strength of concrete (bending)
s'ck = 0.5*sck^(2/3) 15.643 kgf/cm2
s ck= 175 kgf/cm2
N axial force 0 tf
Ac area of concrete = b*h1 3000 cm2
h2 thickness of section, impact plate 30 cm
2) Checking of Cracking Moment and Design Bending Moment
Design bending moment Mf 3.146 tf.m
Check Mf & Mc 1.7*Mf>Mc?, if yes check ultimate bending moment
1.7*Mf = 5.348 tf.m
Mc= 2.346 tf.m 1.7*Mf>Mc? Yes, check ultimate bending momen
3) Ultimate Bending Moment
Mu=As*s sy{d-(1/2)*[As*s sy]/[0.85*s ck*b]} Mu= 574637 kgf.cm = 5.746
where, Mu ultimate bending moment tf.m
As area of tensile bar cm2
s sy yielding point of tensile bar 3000 kgf/cm2 (Spec >295 N/mm2)
d effective height = h1-cover 23 cm
cover d1= 7 cm
h2= 30 cm
s'ck design compressive strength of concrete 175 kgf/cm2 b effective width 100 cm
A Mf/( *j*d) 8 657 2
h d
b
As
d1
h d
b
As
As'
d1
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4) Bar Arrangement
Checking of single or double bar arrangement
M1= (d/Cs)^2*ssa*b >Mf? M1= 593272 kgf.cm = 5.933 tf.m
where, M1 resistance moment
Cs ={2m/[s*(1-s/3)]}^(1/2) 12.844
s (n*sca)/(n*sca+ssa) 0.438
m ssa/sca 30.833
ssa 1850 kgf/cm2
sca 60 kgf/cm2
n 24
Check M1 > Mf? M1= 5.933 tf.m M1>Mf : Design Tensil e Bar Only
Mf= 3.146 tf.m
(a) Tensile Bar
Max bar area As max = 0.02*b*d = 46.0 cm2
Min bar area As min = b*4.5%= 4.5 cm2
Required bar area As req= 8.657 cm2
Apply f = 19 @ 300 mmBar area As = 9.451 cm2 ok
5) Checking of Allowable Stress
Mf 3.146 tf.m
So 0.000 tf
ss = Mf/(As*j*d) 1642.35 kgf/cm2 check ss < ssa ? ok
sc = 2*Mf/(k*j*b*d^2) 37.88 kgf/cm2 check sc < sca ? ok
p=As/(b*d) 0.0041
k={(n*p)^2+2*n*p}^0.5 - n*p 0.3563
j= 1-k/3 0.8812
SUMMARY OF DESIGN CALCULATION
Description Abbr. unit Impact Plate Corbel
Principle Dimensions
Concrete Design Strength sc kgf/m2 175 175
Effective width of section b cm 100 100
Height of Section h cm 30 30
concrete cover (tensile) d1 cm 5 7
concrete cover (compressive) d2 cm - -
Effective height of Section d cm 25 23
Allowable Stress Concrete sca kgf/m2 60 60
Re-Bar ssa kgf/m2 1850 1850
Shearing ta kgf/m2 5.5 5.5
Yielding Point of Reinforcement Bar ssy kgf/cm2 3000 3000
Reinforcement Bar
Tensile Bar Required As req. cm2 14.73 8.66
Designed As cm2 18.90 D19@150 9.45 D19@300
Compressive Bar Required As' req. cm2 0.00
Designed As' cm2 6.70 D16@300
Design Load
Design Bending Moment Mf tf.m 5.818 3.146
Design Axis Force Nd tf - -
Shearing Force S tf - -
Checking of Minimum Re-Bar
Cracking Moment Mc tf.m 2.346 5.746
1.7*Mf 9.891 5.348
1.7*Mf<Mc? If "no" check Mu check Mu ok
Ultimate Bending Moment Mu tf.m 10.390
Mu>1.7*Mf? ok
Max Re-bar As max cm2 50.00 46.00
d1
h d
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Remarks
1 Input Data
"Input": Figure in red are input data.
2 There are two try and error calculation except input data such as dimension and condition.
To calculate them, click on the macro button at their right sides after inputting data.
(1) Sheet name "Body", G391 to K392 Button Calculate sc
(2) Sheet name "Body", H530 to N531. Button Calculate x
3 Allowable stress for "Body"
If allowable stress is "Check" for body, see Sheet "Body", calculation of stress
4 Minimum reinforcement bar
Step 1 Calculation of Md', find 1.7Md
Step 2 Comparison between Md' and Mc
if Md' > Mc go to step 3
Step 3 Calculation of Mu
Step 4 Comparison between Mu and Mc
Mu > Mc OK
5 Wing Wall
Wing Wall are not considered.
Revised
4-Nov-02 1 Bering capacity calculation was added.
Safety factor was revised as follows.
Normal condition 1.5 to 2.0
Seismic condition 1.2 to 1.25
9-Nov-02 2 Sheet " Footing"
Cell "H548" & "L548" is changed.
Figure "Mu" is not referred correctly. Therefore revised.
15-Nov-02 3 Sheet "Body"
Cell "I123" and "I150"
Water pressure calculated per m, there revised as per width.
29-Nov-02 4 All sheets
Some of inputting cells and calculation result cells have been rearranged.
Safety factors against sliding have been set at the same figures as retaining wall.
previous figure revised figure
normal condition 1.50 2.00
seismic condition 1.20 1.25
Reinforcement bar arrangements for additional bars and distribution bars have been added.
3-Dec-02 5 Modification of drawings
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4-Dec-02 6 Modification of additional bar arrangement
12-Dec-02 7 Minor change: sheets "Stability", "Body" and "Footing"
28-Dec-02 8 Minor correction: sheet "Body" (calculation results are same as revision 7)
20-Jan-03 9 Sheet "Parapet"
Cells "K65", "L65" and "M65" were added.
Cells "C63" and "H66" were corrected.
Cells "D71", "D72", "H71", "I70", "I71" and "I72" were corrected.
Figure 600 on Cell "C86" was deleted.
Cells "K127" and "D150" were corrected.
Cells "C151", "D151", "H151" and "I151" were inserted.
Cell "L287" was corrected.
Sheet "Input"
Cell "L40"was modified.
Calculation formulae in Cells "J226", "J227" and "J228" were deleted.
Calculation formulae in Cells "L230", "L231" and "L232" were corrected.
2-Feb-03 10 Sheet "Input"
Input Cell "E41"was modified to calculation cell.
Input Cell "E42" was added.
Cells "B42", "E43", "G41" and "G42" were added.
Sheet "Stability"
Calculation formula in Cell "J267" was changed.
Sheet "Body"
Calculation formula in Cell "H66" was corrected.
Sheet "Footing"
Calculation formula in Cells "K120", "L120", "M120" and "N120" were corre
26-Feb-03 11 Sheet "Input"
Cell "G128" was corrected. Top side ------>> Toe side
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ted.