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DESIGN OF AN INTZE TANK
COURSE CODE: CE - 4102
COURSE TITLE: STRUCTURAL ANALYSIS AND DESIGN -III SESSIONAL
Designed By:
SUMAN JYOTI
Student Id: 191125
Department of Civil Engineering
Dedicated To:
TRIBHUVAN UNIVERSITY
Kritipur, Nepal
KATHMANDU UNIVERSITY
Banepa, Nepal
DEPARTMENT OF CIVIL ENGINEERING
DHAKA UNIVERSITY OF ENGINEERING & TECHNOLOGY, GAZIPUR
Design an Intze tank from following data:
Future population = 3175
Per capita demand = 130 litre/day
Height of the cylindrical wall = 11 ft.
Concrete strength, f´c = 5030 psi
Steel strength, fy = 60 ksi = 415
Mpa
Solution:
1. GEOMETRIC DESIGN:
Total quantity of water = 3175 × 130 = 412750 lit/day = 412.75 m3
/ day
= 14564.94 ft3
/ day
Let, the diameter of the tank = D in ft.
Now, the volume of the tank = capacity of the tank
 14564.94 =
𝜋𝐷2
4
× 11ft
 D = 41.56 ft ≈ 42 ft
1.1 Dimension and Illustration of Water Tank:
Figure: Dimension Proportioning of Intz Water Tank
2. STRUCTURAL DESIGN:
2.1 Materials Property:
2.1.1 Permissible concrete stresses to resistance to cracking:
Direct tension, fc = 5√𝑓′𝑐 psi = 5√5030 psi psi = 354.61 psi = 2.445 MPa
Tension due to bending, fc = 12√𝑓′𝑐 psi = 12√5030= 851.06 psi = 5.87 MPa
Shear = √f′c psi = 2√5030 psi =141.85 psi = 0.978 MPa
Direct compression, fc = 0.25 f ′c psi = 1257.5 psi = 8.67 MPa
Compression due to bending, fc = 0.45 fc’ psi = 2263.5 psi = 15.06 MPa
Modular ratio, n =
29∗106
57000√f′c
=
29∗106
57000√5030
= 7.17
2.1.2 Allowable tensile strength of reinforcement (According to BNBC):
fs= 0.4 fy = 0.4 × 60 = 24 ksi =165.5 Mpa
2.2 Design of Top Spherical Dome:
2.2.1 Allowable tensile strength of reinforcement (According to BNBC):
Radius of top spherical dome = R
Let, r be the radius of the dome
So, h (2r-h) = R2
or, 5.25 × (2r – 5.25) = 212
or, r = 44.625 ft = 13.6 m
Now, sin θ = 21/ 44.625
θ = 28.07 º < 51.8 º (so, compression dome)
cos θ = 0.882
2.2.2 Load calculation:
Let, the thickness of dome slab = 100 mm
Self-weight = 0.1 x 25 = 2.5 kN/m2
Live load = 1.5 kN/m2
So, Total Distributed Load, w = 4 kN/m2
r
r-h
R = 21ft
h = 5.25 ft
R
2.2.3 Check for stresses:
Let, the thickness of dome
Hoop stress at any angle θ, =
𝑤𝑟
𝑡
(
cos2 θ+cosθ−1
1+𝑐𝑜𝑠θ
)
Maximum hoop stress will occur at θ = 0,
So, Hoop stress =
𝑤𝑟
𝑡
×
1
2
=
4∗1000∗13.6
0.1∗ 2
= 0.272× 106
N/m2
= 0.272 N/mm2
< 5 kN/mm2
( Ok )
Meridional stress at any angle θ, =
𝑤𝑟
𝑡
(
1
1+𝑐𝑜𝑠θ
)
Maximum meridional stress will occur at θ = 28.07 º = Ø,
So, Meridional stress =
𝑤𝑟
𝑡
×
1
1+𝑐𝑜𝑠𝜃
=
4∗1000∗13.6
0.1
×
1
1+0.882
= 0.29× 106
N/m2
= 0.29 N/mm2
< 5 kN/mm2
( Ok )
2.2.4 Area of reinforcement calculation:
Both stresses are within safe limit, hence a minimum reinforcement may be
provided.
Ast = 0.002bt
= 0.002×1000×100
= 200 mm2
per meter (both direction)
Use 8 mm dia. bar @ 200 mm c/c (both direction)
2.2.5 Detailing of reinforcements:
8 mm @ 200 mm c/c
at mid of the slab thickness
100 mm thick dome slab
2.3 Design of Top Ring Beam:
2.3.1 Load calculation:
The horizontal component of Meridional thrust, P = T Cos φ
P = 0.29 × 100 ×1000 ×(0.882) = 25578 N
Total tension tending to rupture the ring beam per meter length of its
circumference,
= P × D/2
= 25578 × (12.8/2)
= 163700 N
2.3.2 Area of reinforcement calculation:
Since steel in contact with water then fs = 165.5 N/mm2
[fs = 0.4fy ]
So, Area of reinforcement required,
Ast =
Tensile force
Allowable stress of steel
=
163700
165.5
= 990.12 mm2
Using 16 mm dia bar (as = 200.1 mm2
), required bar=
990.12
200.1
= 4.94 ≈ 5 nos.
2.3.3 Size of beam calculation:
Equivalent area of the composite section = A + ( n-1 ) Ast
= A + ( 7.17-1 ) × 5 × 200.1
= A + 6174
Take the allowable stress to the composite section is 1.2 kN/mm2
.
or, 1.2 =
163700
A + 6174
or, A = 130242 mm2
Let, beam width is, b = 500 mm and the depth, d = 260.48 ≈ 260 mm
2.3.4 Minimum reinforcement calculation:
Using (#3) 10 mm dia bar, then spacing, Sv =
2.5 As∗fy
b
As = 2 × 0.11 in2
( for two legs )
So, Spacing, Sv =
2.5∗78.54∗413.7
260
= 312.42 mm ≈ 300 mm c/c
2.3.5 Detailing of reinforcements:
2.4 Design of Cylindrical Wall:
2.4.1 Load Calculation:
Let, joint condition is simple joint, i.e., cylindrical wall is free to move at top
and bottom.
Maximum hoop tension at the base of the wall is,
T = γh
𝐷
2
= 10000 × 3.534 ×
12.8
2
[Using, γw = 10000 N/m3
]
T = 226176 N
2.4.2 Area of reinforcement calculation:
Area of the required reinforcement, Ast =
226176
165.5
= 1366.6 mm2
Area of reinforcement on each face = 1366.6/2 = 683.3 mm2
≈ 684 mm2
Using 16 mm dia. bar, the spacing =
1000 ∗ 201
684
= 293.86 mm ≈ 280 mm c/c
Cut 50% bar at a depth of 1.8 m below the top cylinder than base,
So, spacing is = 560 mm c/c
2.4.3 Thickness of cylindrical wall calculation:
Equivalent area of composite section = t×103
+ (7.17–1) × (
1000
280
×2×201)
= 1000t + 8858.35
Since the tension is direct then permissible direct tensile stress = 1.2 N/mm2
or, 1.2 =
226176
1000𝑡+8858.35
or, t = 179.62 mm ≈ 180 mm
Since hoop tension is smaller at the top of cylinder than base,
So, use thickness 150 mm at the top of cylindrical wall.
2.4.4 Distribution of reinforcement calculation:
Average thickness of the wall slab =
180+150
2
= 165 mm
Area of steel required is = 0.0022 × 1000 × 165 = 330 mm2
Using 12 mm bar, the spacing =
113∗1000
330
= 342.4 mm c/c ≈ 300 mm c/c
2.4.5 Detailing of reinforcement:
2.5 Design of bottom ring beam:
2.5.1 Load Calculation:
Load due to top dome = Area of slab x Meridional stress x sin φ
= 100 x 1000 x 0.29 x sin28.07º
= 13646 N /m
Load due to top ring beam = 0.26 x (0.5 - 0.15) x 25000
= 2275 N/m
Load due to cylindrical wall = 0.165 x 3.35 x 25000
= 13819 N /m
Assume, beam size, 900 mm x 500 mm
Self-weight of beam = 0.5 x (0.9 – 0.5) x 25000 = 5000 N /m
Total w1= 34740 N/ m
Horizontal thrust due to vertical load = w1 tan β
= 34740 x tan 45º = 34740 N/ m
Hoop tension due to vertical load, H1 =
34740∗12.8
2
= 222336 N
Hoop tension due to water, H2 = 10000 x 3.35 x 0.6 x 12.8/2 = 128640 N
Total hoop tension, H = 222336 + 128640 = 350976 N
2.5.2 Area of Reinforcement Calculation:
Area of the required reinforcement, Ast =
350976
165.5
= 2120.7 mm2
Using 16 mm dia bar, Nos. of bar =
2120.7
201
= 10.55 ≈ 11 Nos.
2.5.3 Check for Tensile stresses:
Maximum tensile stress =
350976
900∗500+(7.17−1)∗11∗201
= 0.0006 N/mm2
<1.2 N/mm2
( Ok )
2.5.4 Shear reinforcement calculation:
Using 10mm dia bar Spacing, Sv =
2.5 𝐴𝑠𝑣 𝑓𝑦
𝑏
=
2.5∗ 78.54∗4∗165.5
500
= 260 mm c/c ≈ 250 mm c/c
2.5.5 Detailing of reinforcements:
Fig. Detailing of bottom ring beam
2.6 Design of conical dome:
2.6.1 Load Calculation:
Average diameter of Conical dome = 10.4 m
Average depth of water = 3.35 + 2.4/2 = 4.55m
Assume, Thickness of slab 400 mm
Self-weight of slab = (π x 10.8 x 3.39) x 0.4 x 25000 = 1150203 N
Weight of water = (π x 10.8 x 4.55 x 2.4) x 10000 = 370508 N
Load from Top dome, cylindrical wall, bottom ring beam, = 34740× π×10.4
= 370508 N
Total load on Conical dome =1150203+ 370508 + 370508
= 1891219 N
Load at per meter of conical dome base =
1891219
3.1416∗4.54
= 132598 N/m
Meridional thrust, T =
132598
𝑐𝑜𝑠45
= 187522 N
Meridional stress =
187522
1000∗400
= 0.5 N/mm2 < 5.0 N/mm2
, So Safe.
2.6.2 Hoop tension calculation:
General expression for hoop tension
Diameter of conical dome at h m height from base, Dh = 8 + 2 × 2.4/2.4 × h
= 8 + 2h
Intensity of water pressure at height h from base, p
or, p = (5.76 – h) x 10000 x 1 = (57600 – 10000h) N/m
Weight of Conical dome, w1 = 0.4 x 1 x 25000 = 10000 N/m
Hoop tension at any height h, = (𝑝𝑠𝑖𝑛β+ w1 tanβ) ×
8 + 2h
2
= {(57600 – 10000h) sin45 + 10000 tan45)} ×
8 + 2h
2
Maximum Hoop tension (at h = 2.44) = 216056 N
2.6.3 Area of reinforcement calculation:
Area of Reinforcement Calculation, Ast =
216056
165.5
= 1306mm2
Area of steel on each face =
1306
2
= 653 mm2
Using 16 mm dia. bar, Spacing =
201∗1000
653
= 307.8 mm C/C ≈ 300 mm C/C
Check for maximum tensile stress-
=
216056
400∗ 1000 +(12.8 − 1)∗(
1000
100
∗201∗2)
= 0.00001 N/mm2
< 1.2 N/mm2
(Ok)
2.6.4 Distribution Reinforcement Calculation:
Assuming distribution bar as 0.18 %
Ast = 0.0018× 400 × 1000 = 720 mm2
Area of steel on each face = 720 /2 = 360 mm2
Using 12 mm bar, spacing =
113.1∗1000
360
= 314.2 mm ≈ 300 m c/c
2.6.5 Area of reinforcement for B.M.
The conical dome also acts as a slab,
Load on slab, W =
1150203 + 370508
3.1414 ∗8
= 60507.16 N/m
Load on 1m wide and 3m spanned slab, W = 60507.16 N/m
So, Maximum Bending moment =
60507.16 ∗3
12
= 15126.8 N-m
Let, main bar Ø16mm, then effective depth = 400 – 40 -16/2 = 352 mm
Ast =
15126.8∗1000
115 ∗ 352 ∗ 0.866
≈ 430 mm2
Use #5 (16mm) bar, Spacing =
201.1∗1000
430
= 467.67 mm C/C ≈ 400 mm C/C
Since flexural reinforcing bar spacing = 400 mm C/C,
Which will also act as distribution bar as well as main bar.
Use #4 (12mm) bar @ 400 mm C/C as distribution bar at the top of the slab.
2.6.6 Reinforcement Detailing
Fig. Detailing of conical dome slab
2.7 Design of bottom spherical dome:
2.7.1 Load Calculation:
Assume, slab thickness = 400 mm
Let, Radius of dome rb,
rb2 = (rb- 1.6)2 + 4.0 2
∴ rb = 5.8 m
or, sin φ =
4
5.8
= 0.6897
∴ φ = 43.60 < 51.8º So Compression dome
∴ cos φ = 0.724
Self-weight of dome = (2π rb × h) × t × γc = 2π x 5.8 x 1.6 x 0.4 x 25000
= 583080 N
Volume of water above conical dome, V = πR2
hwater – 1
3
π x h2
x (3 x rb – h)
= π × 42
× 4.55 – 1
3
π × 1.62
× (3 × 5.8 – 1.6) = 186.35 m3
Weight of water = 186.35 x 10000 = 1863508 N
Total weight = 583080 + 1863508 = 2446588 N
2.7.2 Check for stress:
Load per unit area w =
2446588
2π x 5.8 x 1.6
= 41960 N/m2
∴ Maximum Hoop stress =
wr
𝑡
×
1
2
=
41960 x 5.8
0.4
×
1
2
= 0.304 x 106
N/m2
= 0.304 N/mm2
< 5 N/mm2
∴ Maximum Meridional stress =
wr
𝑡
×
1
(1+𝑐𝑜𝑠 φ)
=
41960 x 5.8
0.4
×
1
(1+0.724)
= 0.353 x 106
N/m2
= 0.353 N/mm2
< 5 N/mm2
2.7.3 Area of reinforcement calculation:
ρ = 0.18 %
Area of the required reinforcement, Ast =
0.18
100
x 400 x 1000 = 720 mm2
Using #4 (12mm) bar, Spacing =
113.1∗1000
720
= 157.08 mm c/c ≈ 150 mm c/c
in both directions.
R = 4 m
h = 1.6 m
r-h
rb
2.7.4 Details of reinforcement:
Fig: Detailing of Bottom Spherical Dome.
2.8 Design of circular bottom beam:
2.8.1 Load Calculation:
Meridional thrust from conical dome, T = 187522 N/m
Inward thrust from conical dome = 187522× sin 45º = 132598.07 N/m
Meridional thrust from bottom spherical dome = 0.353 × 400 × 1000
= 141200 N/ m
Outward thrust from bottom spherical dome = 141200 × Cos 43.6°
= 102253 N/m
So, Net inward thrust, P = 132598.07 – 102253
= 30345 N/m (Compressive)
Hoop compressive force in Beam =
𝑃𝐷
2
=
30345∗
26.25
3.28
2
= 121380 N
Assuming, Beam size = 450 mm × 800 mm
∴ Hoop stress =
121380
450∗800
= 0.3372 N/mm2
< 5 N/mm2
Vertical load from conical dome = 132598 N/m (Computed earlier)
12 mm @ 150 mm c/c
at mid of the slab thickness
00 mm thick dome slab
Vertical load from bottom spherical dome,
= 2446588/ (π x 8) = 97346.6 N/m
Total Vertical load on beam = 132598 + 97346.6 = 229945 N/m
Self-weight of beam = 0.45 × 0.8 × 25000 = 9000 N/ m
∴ The design load for the beam, 𝜔 = 229945 + 9000 = 238945 N/m
2.8.2 Moment Calculation:
Load on per meter beam, w = 238945 N/m
It is proposed to support the beam by 6 Columns.
Maximum (-ve) Bending moment at support = k1wR2
×
1
3
π
M1 = 0.089 × 238945 × 42
×
1
3
π = 356317 N- m
Maximum (+ve) Bending moment at mid span = k2wR2
×
1
3
π
= 0.045 × 238945 × 42
×
1
3
π = 180160 N- m
Maximum (-ve) Twisting moment (T) at 12.75º from support = k3wR2
×
1
3
π
= 0.009 × 238945 × 42
×
1
3
π = 36032 N- m
2.8.3 Shear Calculation:
Shear force at support section, V1= w ×
2𝜋𝑅
𝑁𝑜.𝑜𝑓 𝐶𝑜𝑙𝑢𝑚𝑛
×
1
2
= 238945 ×
2𝜋∗4
6
×
1
2
= 500445 N
Shear force at the point of maximum torsion,
V2 = 500445 – 500445 ×
12.75
30
= 287755.88 N ( rough, 360/6 column × 2 )
2.8.4 Design of support section (For Moment):
M = 356317 N- m, V1= 500445 N
Effective depth, d = √
Moment 𝑖𝑛 𝑁−𝑚𝑚2
0.5∗𝑓𝑐∗𝑗∗𝑘∗𝑏
deff = √
356317 ∗1000
0.5∗15.06∗0.866∗0.403∗450
= 548.9 mm
Let clear cover = 40 mm, and 2 layers of main bar
Ø of main bar = 25 mm & stirrup = 10 mm
So, Actual effective depth, d = 800 – 40 – 10 – (25 + 25/2)
= 712.5 mm > 548.9 mm, Safe (ok).
Area of Reinforcement =
356317 × 1000
165.5 × 0.866 × 712.5
= 3490 mm2
Use 20 mm Ø bar. So, Nos. of bars = 3490/314.2 = 11.10 ≈ 12 Nos.
2.8.5 Design of support section (For Shear):
Developed shear stress, 𝜏v =
𝑉
𝑏𝑑
=
500445
450 ∗712.5
∴ 𝜏v = 1.56 N/mm2
Maximum allowable shear stress, 𝜏allow = 3.4 √𝑓𝑐
′
∴ 𝜏allow = 3.4 √5030 = 241.13 psi = 1.66 N/mm2
Since 𝜏v < 𝜏allow, this section is safe for shear.,
Here, Percentage of steel ratio ρ =
12.5
30
= 0.417 %
So, allowable concrete shear stress, 𝜏c = 1.1 √𝑓𝑐
′
𝜏c = 1.1 √5030 = 78.01 psi = 0.538 N/mm2
Since 𝜏v > 𝜏c Shear reinforcement is required.
Here, Allowable concrete shear force, Vc = 𝜏c × bd
= 0.538 × 450 × 712.5 = 172496.25 N
Use #3 (10mm) bar 6-legged bar as stirrup, Spacing,
S =
𝐴𝑠𝑣∗𝑓𝑠𝑣∗𝑑
𝑉−𝑉𝑐
=
(6∗78.54) × 210 × 712.5
500445 −172496.25
= 215 mm C/C ≈ 200 mm C/C
2.8.6 Design for torsion:
The maximum torsion occurs at the point of contraflexure
Equivalent moment, Me = M + MT
At point of contraflexure M = 0
And, we know, MT =
𝑇
1.7
(1 +
𝐷
𝐵
)
=
36032∗1000
1.7
(1 +
800
450
) = 175.54 × 106
N-mm
So, the equivalent moment, Me = 58.87 × 106
N-mm
Area of Reinforcement =
58.87 × 106
165.5 x 0.866 x 712.5
= 576.55 mm2
Use 16 mm Ø bar. So, Nos. of bars = 576.55/201.1 = 2.87 ≈ 4
The number of bars at the point of contraflexure is more than the 3, So no
additional bars are required.
Equivalent shear, Ve = V +1.6
𝑇
𝑏
= 500445 + 1.6 ×
36032
450
= 500573 N
Equivalent nominal shear stress, 𝜏ve =
500573
450∗712.5
= 1.56 N/mm2
< 1.66 N/mm2
Let, 10mm Ø bar with 6 legged will be used as stirrup,
so, Asv = 6 × 78.54 = 471.2 mm2
Allowable concrete shear force, Vc = 0.538 × 450 × 712.5 = 172496.25 N
(i) Spacing considering torque and shear force at point of contraflexure
Asv =
𝑇∗𝑆𝑣
𝑏1 ∗ 𝑑1 ∗ 𝑓𝑠𝑣
+
𝑉2∗𝑆𝑣
2.5 𝑑1 ∗𝑓𝑠𝑣
471.2 =
36032∗1000∗𝑆𝑣
384 ∗ 719 ∗210
+
287755.88 ∗𝑆𝑣
2.5 ∗719 ∗ 210
∴ 𝑆v = 340 ≈ 300 mm c/c
b1 = 450 – 2×25 – 2×8
= 384 mm
d1 = 800 – 40 – 25 – 2 × 8
= 719 mm
(ii) Spacing considering equivalent shear force
𝐴vs =
(𝑉𝑒−𝑉𝑐)𝑆𝑣
𝑓𝑠𝑣∗𝑑
or, Sv =
𝐴𝑠𝑣∗𝑓𝑠𝑣∗𝑑
𝑉𝑒−𝑉𝑐
=
471.2 ∗ 210∗712.5
(500573 − 172496.25 )
= 214.9 mm c/c ≈ 200 mm c/c
Hence provide 10 mm-6-legged stirrup at 200 mm c/c from column face to
the point of contraflexure.
2.8.7 Design of mid-section:
Effective depth, d = 712.5 mm
Bending Moment = 180160 N- m
Area of Reinforcement =
180160 × 1000
165.5 × 0.866 × 712.5
= 1764.24 mm2
Use 20 mm Ø bar. So, Nos. of bars = 1764.24/314.2 = 5.62 ≈ 6
2.8.8 Detail Drawing:
Fig. Detailing of Circular Bottom Beam
Fig:-Section showing the details reinforcement in bottom circular beam, column and bracing.
Fig:- Details reinforcement of Intze Tank

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Intze Overhead Water Tank Design by Working Stress - IS Method.pdf

  • 1. DESIGN OF AN INTZE TANK COURSE CODE: CE - 4102 COURSE TITLE: STRUCTURAL ANALYSIS AND DESIGN -III SESSIONAL Designed By: SUMAN JYOTI Student Id: 191125 Department of Civil Engineering Dedicated To: TRIBHUVAN UNIVERSITY Kritipur, Nepal KATHMANDU UNIVERSITY Banepa, Nepal DEPARTMENT OF CIVIL ENGINEERING DHAKA UNIVERSITY OF ENGINEERING & TECHNOLOGY, GAZIPUR
  • 2. Design an Intze tank from following data: Future population = 3175 Per capita demand = 130 litre/day Height of the cylindrical wall = 11 ft. Concrete strength, f´c = 5030 psi Steel strength, fy = 60 ksi = 415 Mpa Solution: 1. GEOMETRIC DESIGN: Total quantity of water = 3175 × 130 = 412750 lit/day = 412.75 m3 / day = 14564.94 ft3 / day Let, the diameter of the tank = D in ft. Now, the volume of the tank = capacity of the tank  14564.94 = 𝜋𝐷2 4 × 11ft  D = 41.56 ft ≈ 42 ft 1.1 Dimension and Illustration of Water Tank: Figure: Dimension Proportioning of Intz Water Tank
  • 3. 2. STRUCTURAL DESIGN: 2.1 Materials Property: 2.1.1 Permissible concrete stresses to resistance to cracking: Direct tension, fc = 5√𝑓′𝑐 psi = 5√5030 psi psi = 354.61 psi = 2.445 MPa Tension due to bending, fc = 12√𝑓′𝑐 psi = 12√5030= 851.06 psi = 5.87 MPa Shear = √f′c psi = 2√5030 psi =141.85 psi = 0.978 MPa Direct compression, fc = 0.25 f ′c psi = 1257.5 psi = 8.67 MPa Compression due to bending, fc = 0.45 fc’ psi = 2263.5 psi = 15.06 MPa Modular ratio, n = 29∗106 57000√f′c = 29∗106 57000√5030 = 7.17 2.1.2 Allowable tensile strength of reinforcement (According to BNBC): fs= 0.4 fy = 0.4 × 60 = 24 ksi =165.5 Mpa 2.2 Design of Top Spherical Dome: 2.2.1 Allowable tensile strength of reinforcement (According to BNBC): Radius of top spherical dome = R Let, r be the radius of the dome So, h (2r-h) = R2 or, 5.25 × (2r – 5.25) = 212 or, r = 44.625 ft = 13.6 m Now, sin θ = 21/ 44.625 θ = 28.07 º < 51.8 º (so, compression dome) cos θ = 0.882 2.2.2 Load calculation: Let, the thickness of dome slab = 100 mm Self-weight = 0.1 x 25 = 2.5 kN/m2 Live load = 1.5 kN/m2 So, Total Distributed Load, w = 4 kN/m2 r r-h R = 21ft h = 5.25 ft R
  • 4. 2.2.3 Check for stresses: Let, the thickness of dome Hoop stress at any angle θ, = 𝑤𝑟 𝑡 ( cos2 θ+cosθ−1 1+𝑐𝑜𝑠θ ) Maximum hoop stress will occur at θ = 0, So, Hoop stress = 𝑤𝑟 𝑡 × 1 2 = 4∗1000∗13.6 0.1∗ 2 = 0.272× 106 N/m2 = 0.272 N/mm2 < 5 kN/mm2 ( Ok ) Meridional stress at any angle θ, = 𝑤𝑟 𝑡 ( 1 1+𝑐𝑜𝑠θ ) Maximum meridional stress will occur at θ = 28.07 º = Ø, So, Meridional stress = 𝑤𝑟 𝑡 × 1 1+𝑐𝑜𝑠𝜃 = 4∗1000∗13.6 0.1 × 1 1+0.882 = 0.29× 106 N/m2 = 0.29 N/mm2 < 5 kN/mm2 ( Ok ) 2.2.4 Area of reinforcement calculation: Both stresses are within safe limit, hence a minimum reinforcement may be provided. Ast = 0.002bt = 0.002×1000×100 = 200 mm2 per meter (both direction) Use 8 mm dia. bar @ 200 mm c/c (both direction) 2.2.5 Detailing of reinforcements: 8 mm @ 200 mm c/c at mid of the slab thickness 100 mm thick dome slab
  • 5. 2.3 Design of Top Ring Beam: 2.3.1 Load calculation: The horizontal component of Meridional thrust, P = T Cos φ P = 0.29 × 100 ×1000 ×(0.882) = 25578 N Total tension tending to rupture the ring beam per meter length of its circumference, = P × D/2 = 25578 × (12.8/2) = 163700 N 2.3.2 Area of reinforcement calculation: Since steel in contact with water then fs = 165.5 N/mm2 [fs = 0.4fy ] So, Area of reinforcement required, Ast = Tensile force Allowable stress of steel = 163700 165.5 = 990.12 mm2 Using 16 mm dia bar (as = 200.1 mm2 ), required bar= 990.12 200.1 = 4.94 ≈ 5 nos. 2.3.3 Size of beam calculation: Equivalent area of the composite section = A + ( n-1 ) Ast = A + ( 7.17-1 ) × 5 × 200.1 = A + 6174 Take the allowable stress to the composite section is 1.2 kN/mm2 . or, 1.2 = 163700 A + 6174 or, A = 130242 mm2 Let, beam width is, b = 500 mm and the depth, d = 260.48 ≈ 260 mm 2.3.4 Minimum reinforcement calculation: Using (#3) 10 mm dia bar, then spacing, Sv = 2.5 As∗fy b As = 2 × 0.11 in2 ( for two legs ) So, Spacing, Sv = 2.5∗78.54∗413.7 260 = 312.42 mm ≈ 300 mm c/c
  • 6. 2.3.5 Detailing of reinforcements: 2.4 Design of Cylindrical Wall: 2.4.1 Load Calculation: Let, joint condition is simple joint, i.e., cylindrical wall is free to move at top and bottom. Maximum hoop tension at the base of the wall is, T = γh 𝐷 2 = 10000 × 3.534 × 12.8 2 [Using, γw = 10000 N/m3 ] T = 226176 N 2.4.2 Area of reinforcement calculation: Area of the required reinforcement, Ast = 226176 165.5 = 1366.6 mm2 Area of reinforcement on each face = 1366.6/2 = 683.3 mm2 ≈ 684 mm2 Using 16 mm dia. bar, the spacing = 1000 ∗ 201 684 = 293.86 mm ≈ 280 mm c/c Cut 50% bar at a depth of 1.8 m below the top cylinder than base, So, spacing is = 560 mm c/c 2.4.3 Thickness of cylindrical wall calculation: Equivalent area of composite section = t×103 + (7.17–1) × ( 1000 280 ×2×201) = 1000t + 8858.35 Since the tension is direct then permissible direct tensile stress = 1.2 N/mm2 or, 1.2 = 226176 1000𝑡+8858.35 or, t = 179.62 mm ≈ 180 mm Since hoop tension is smaller at the top of cylinder than base, So, use thickness 150 mm at the top of cylindrical wall.
  • 7. 2.4.4 Distribution of reinforcement calculation: Average thickness of the wall slab = 180+150 2 = 165 mm Area of steel required is = 0.0022 × 1000 × 165 = 330 mm2 Using 12 mm bar, the spacing = 113∗1000 330 = 342.4 mm c/c ≈ 300 mm c/c 2.4.5 Detailing of reinforcement:
  • 8. 2.5 Design of bottom ring beam: 2.5.1 Load Calculation: Load due to top dome = Area of slab x Meridional stress x sin φ = 100 x 1000 x 0.29 x sin28.07º = 13646 N /m Load due to top ring beam = 0.26 x (0.5 - 0.15) x 25000 = 2275 N/m Load due to cylindrical wall = 0.165 x 3.35 x 25000 = 13819 N /m Assume, beam size, 900 mm x 500 mm Self-weight of beam = 0.5 x (0.9 – 0.5) x 25000 = 5000 N /m Total w1= 34740 N/ m Horizontal thrust due to vertical load = w1 tan β = 34740 x tan 45º = 34740 N/ m Hoop tension due to vertical load, H1 = 34740∗12.8 2 = 222336 N Hoop tension due to water, H2 = 10000 x 3.35 x 0.6 x 12.8/2 = 128640 N Total hoop tension, H = 222336 + 128640 = 350976 N 2.5.2 Area of Reinforcement Calculation: Area of the required reinforcement, Ast = 350976 165.5 = 2120.7 mm2 Using 16 mm dia bar, Nos. of bar = 2120.7 201 = 10.55 ≈ 11 Nos. 2.5.3 Check for Tensile stresses: Maximum tensile stress = 350976 900∗500+(7.17−1)∗11∗201 = 0.0006 N/mm2 <1.2 N/mm2 ( Ok ) 2.5.4 Shear reinforcement calculation: Using 10mm dia bar Spacing, Sv = 2.5 𝐴𝑠𝑣 𝑓𝑦 𝑏 = 2.5∗ 78.54∗4∗165.5 500 = 260 mm c/c ≈ 250 mm c/c
  • 9. 2.5.5 Detailing of reinforcements: Fig. Detailing of bottom ring beam 2.6 Design of conical dome: 2.6.1 Load Calculation: Average diameter of Conical dome = 10.4 m Average depth of water = 3.35 + 2.4/2 = 4.55m Assume, Thickness of slab 400 mm Self-weight of slab = (π x 10.8 x 3.39) x 0.4 x 25000 = 1150203 N Weight of water = (π x 10.8 x 4.55 x 2.4) x 10000 = 370508 N Load from Top dome, cylindrical wall, bottom ring beam, = 34740× π×10.4 = 370508 N Total load on Conical dome =1150203+ 370508 + 370508 = 1891219 N Load at per meter of conical dome base = 1891219 3.1416∗4.54 = 132598 N/m Meridional thrust, T = 132598 𝑐𝑜𝑠45 = 187522 N Meridional stress = 187522 1000∗400 = 0.5 N/mm2 < 5.0 N/mm2 , So Safe. 2.6.2 Hoop tension calculation: General expression for hoop tension
  • 10. Diameter of conical dome at h m height from base, Dh = 8 + 2 × 2.4/2.4 × h = 8 + 2h Intensity of water pressure at height h from base, p or, p = (5.76 – h) x 10000 x 1 = (57600 – 10000h) N/m Weight of Conical dome, w1 = 0.4 x 1 x 25000 = 10000 N/m Hoop tension at any height h, = (𝑝𝑠𝑖𝑛β+ w1 tanβ) × 8 + 2h 2 = {(57600 – 10000h) sin45 + 10000 tan45)} × 8 + 2h 2 Maximum Hoop tension (at h = 2.44) = 216056 N 2.6.3 Area of reinforcement calculation: Area of Reinforcement Calculation, Ast = 216056 165.5 = 1306mm2 Area of steel on each face = 1306 2 = 653 mm2 Using 16 mm dia. bar, Spacing = 201∗1000 653 = 307.8 mm C/C ≈ 300 mm C/C Check for maximum tensile stress- = 216056 400∗ 1000 +(12.8 − 1)∗( 1000 100 ∗201∗2) = 0.00001 N/mm2 < 1.2 N/mm2 (Ok) 2.6.4 Distribution Reinforcement Calculation: Assuming distribution bar as 0.18 % Ast = 0.0018× 400 × 1000 = 720 mm2 Area of steel on each face = 720 /2 = 360 mm2 Using 12 mm bar, spacing = 113.1∗1000 360 = 314.2 mm ≈ 300 m c/c
  • 11. 2.6.5 Area of reinforcement for B.M. The conical dome also acts as a slab, Load on slab, W = 1150203 + 370508 3.1414 ∗8 = 60507.16 N/m Load on 1m wide and 3m spanned slab, W = 60507.16 N/m So, Maximum Bending moment = 60507.16 ∗3 12 = 15126.8 N-m Let, main bar Ø16mm, then effective depth = 400 – 40 -16/2 = 352 mm Ast = 15126.8∗1000 115 ∗ 352 ∗ 0.866 ≈ 430 mm2 Use #5 (16mm) bar, Spacing = 201.1∗1000 430 = 467.67 mm C/C ≈ 400 mm C/C Since flexural reinforcing bar spacing = 400 mm C/C, Which will also act as distribution bar as well as main bar. Use #4 (12mm) bar @ 400 mm C/C as distribution bar at the top of the slab. 2.6.6 Reinforcement Detailing Fig. Detailing of conical dome slab
  • 12. 2.7 Design of bottom spherical dome: 2.7.1 Load Calculation: Assume, slab thickness = 400 mm Let, Radius of dome rb, rb2 = (rb- 1.6)2 + 4.0 2 ∴ rb = 5.8 m or, sin φ = 4 5.8 = 0.6897 ∴ φ = 43.60 < 51.8º So Compression dome ∴ cos φ = 0.724 Self-weight of dome = (2π rb × h) × t × γc = 2π x 5.8 x 1.6 x 0.4 x 25000 = 583080 N Volume of water above conical dome, V = πR2 hwater – 1 3 π x h2 x (3 x rb – h) = π × 42 × 4.55 – 1 3 π × 1.62 × (3 × 5.8 – 1.6) = 186.35 m3 Weight of water = 186.35 x 10000 = 1863508 N Total weight = 583080 + 1863508 = 2446588 N 2.7.2 Check for stress: Load per unit area w = 2446588 2π x 5.8 x 1.6 = 41960 N/m2 ∴ Maximum Hoop stress = wr 𝑡 × 1 2 = 41960 x 5.8 0.4 × 1 2 = 0.304 x 106 N/m2 = 0.304 N/mm2 < 5 N/mm2 ∴ Maximum Meridional stress = wr 𝑡 × 1 (1+𝑐𝑜𝑠 φ) = 41960 x 5.8 0.4 × 1 (1+0.724) = 0.353 x 106 N/m2 = 0.353 N/mm2 < 5 N/mm2 2.7.3 Area of reinforcement calculation: ρ = 0.18 % Area of the required reinforcement, Ast = 0.18 100 x 400 x 1000 = 720 mm2 Using #4 (12mm) bar, Spacing = 113.1∗1000 720 = 157.08 mm c/c ≈ 150 mm c/c in both directions. R = 4 m h = 1.6 m r-h rb
  • 13. 2.7.4 Details of reinforcement: Fig: Detailing of Bottom Spherical Dome. 2.8 Design of circular bottom beam: 2.8.1 Load Calculation: Meridional thrust from conical dome, T = 187522 N/m Inward thrust from conical dome = 187522× sin 45º = 132598.07 N/m Meridional thrust from bottom spherical dome = 0.353 × 400 × 1000 = 141200 N/ m Outward thrust from bottom spherical dome = 141200 × Cos 43.6° = 102253 N/m So, Net inward thrust, P = 132598.07 – 102253 = 30345 N/m (Compressive) Hoop compressive force in Beam = 𝑃𝐷 2 = 30345∗ 26.25 3.28 2 = 121380 N Assuming, Beam size = 450 mm × 800 mm ∴ Hoop stress = 121380 450∗800 = 0.3372 N/mm2 < 5 N/mm2 Vertical load from conical dome = 132598 N/m (Computed earlier) 12 mm @ 150 mm c/c at mid of the slab thickness 00 mm thick dome slab
  • 14. Vertical load from bottom spherical dome, = 2446588/ (π x 8) = 97346.6 N/m Total Vertical load on beam = 132598 + 97346.6 = 229945 N/m Self-weight of beam = 0.45 × 0.8 × 25000 = 9000 N/ m ∴ The design load for the beam, 𝜔 = 229945 + 9000 = 238945 N/m 2.8.2 Moment Calculation: Load on per meter beam, w = 238945 N/m It is proposed to support the beam by 6 Columns. Maximum (-ve) Bending moment at support = k1wR2 × 1 3 π M1 = 0.089 × 238945 × 42 × 1 3 π = 356317 N- m Maximum (+ve) Bending moment at mid span = k2wR2 × 1 3 π = 0.045 × 238945 × 42 × 1 3 π = 180160 N- m Maximum (-ve) Twisting moment (T) at 12.75º from support = k3wR2 × 1 3 π = 0.009 × 238945 × 42 × 1 3 π = 36032 N- m 2.8.3 Shear Calculation: Shear force at support section, V1= w × 2𝜋𝑅 𝑁𝑜.𝑜𝑓 𝐶𝑜𝑙𝑢𝑚𝑛 × 1 2 = 238945 × 2𝜋∗4 6 × 1 2 = 500445 N Shear force at the point of maximum torsion, V2 = 500445 – 500445 × 12.75 30 = 287755.88 N ( rough, 360/6 column × 2 )
  • 15. 2.8.4 Design of support section (For Moment): M = 356317 N- m, V1= 500445 N Effective depth, d = √ Moment 𝑖𝑛 𝑁−𝑚𝑚2 0.5∗𝑓𝑐∗𝑗∗𝑘∗𝑏 deff = √ 356317 ∗1000 0.5∗15.06∗0.866∗0.403∗450 = 548.9 mm Let clear cover = 40 mm, and 2 layers of main bar Ø of main bar = 25 mm & stirrup = 10 mm So, Actual effective depth, d = 800 – 40 – 10 – (25 + 25/2) = 712.5 mm > 548.9 mm, Safe (ok). Area of Reinforcement = 356317 × 1000 165.5 × 0.866 × 712.5 = 3490 mm2 Use 20 mm Ø bar. So, Nos. of bars = 3490/314.2 = 11.10 ≈ 12 Nos. 2.8.5 Design of support section (For Shear): Developed shear stress, 𝜏v = 𝑉 𝑏𝑑 = 500445 450 ∗712.5 ∴ 𝜏v = 1.56 N/mm2 Maximum allowable shear stress, 𝜏allow = 3.4 √𝑓𝑐 ′ ∴ 𝜏allow = 3.4 √5030 = 241.13 psi = 1.66 N/mm2 Since 𝜏v < 𝜏allow, this section is safe for shear., Here, Percentage of steel ratio ρ = 12.5 30 = 0.417 % So, allowable concrete shear stress, 𝜏c = 1.1 √𝑓𝑐 ′ 𝜏c = 1.1 √5030 = 78.01 psi = 0.538 N/mm2 Since 𝜏v > 𝜏c Shear reinforcement is required.
  • 16. Here, Allowable concrete shear force, Vc = 𝜏c × bd = 0.538 × 450 × 712.5 = 172496.25 N Use #3 (10mm) bar 6-legged bar as stirrup, Spacing, S = 𝐴𝑠𝑣∗𝑓𝑠𝑣∗𝑑 𝑉−𝑉𝑐 = (6∗78.54) × 210 × 712.5 500445 −172496.25 = 215 mm C/C ≈ 200 mm C/C 2.8.6 Design for torsion: The maximum torsion occurs at the point of contraflexure Equivalent moment, Me = M + MT At point of contraflexure M = 0 And, we know, MT = 𝑇 1.7 (1 + 𝐷 𝐵 ) = 36032∗1000 1.7 (1 + 800 450 ) = 175.54 × 106 N-mm So, the equivalent moment, Me = 58.87 × 106 N-mm Area of Reinforcement = 58.87 × 106 165.5 x 0.866 x 712.5 = 576.55 mm2 Use 16 mm Ø bar. So, Nos. of bars = 576.55/201.1 = 2.87 ≈ 4 The number of bars at the point of contraflexure is more than the 3, So no additional bars are required. Equivalent shear, Ve = V +1.6 𝑇 𝑏 = 500445 + 1.6 × 36032 450 = 500573 N Equivalent nominal shear stress, 𝜏ve = 500573 450∗712.5 = 1.56 N/mm2 < 1.66 N/mm2 Let, 10mm Ø bar with 6 legged will be used as stirrup, so, Asv = 6 × 78.54 = 471.2 mm2 Allowable concrete shear force, Vc = 0.538 × 450 × 712.5 = 172496.25 N
  • 17. (i) Spacing considering torque and shear force at point of contraflexure Asv = 𝑇∗𝑆𝑣 𝑏1 ∗ 𝑑1 ∗ 𝑓𝑠𝑣 + 𝑉2∗𝑆𝑣 2.5 𝑑1 ∗𝑓𝑠𝑣 471.2 = 36032∗1000∗𝑆𝑣 384 ∗ 719 ∗210 + 287755.88 ∗𝑆𝑣 2.5 ∗719 ∗ 210 ∴ 𝑆v = 340 ≈ 300 mm c/c b1 = 450 – 2×25 – 2×8 = 384 mm d1 = 800 – 40 – 25 – 2 × 8 = 719 mm (ii) Spacing considering equivalent shear force 𝐴vs = (𝑉𝑒−𝑉𝑐)𝑆𝑣 𝑓𝑠𝑣∗𝑑 or, Sv = 𝐴𝑠𝑣∗𝑓𝑠𝑣∗𝑑 𝑉𝑒−𝑉𝑐 = 471.2 ∗ 210∗712.5 (500573 − 172496.25 ) = 214.9 mm c/c ≈ 200 mm c/c Hence provide 10 mm-6-legged stirrup at 200 mm c/c from column face to the point of contraflexure. 2.8.7 Design of mid-section: Effective depth, d = 712.5 mm Bending Moment = 180160 N- m Area of Reinforcement = 180160 × 1000 165.5 × 0.866 × 712.5 = 1764.24 mm2 Use 20 mm Ø bar. So, Nos. of bars = 1764.24/314.2 = 5.62 ≈ 6 2.8.8 Detail Drawing: Fig. Detailing of Circular Bottom Beam
  • 18. Fig:-Section showing the details reinforcement in bottom circular beam, column and bracing.
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