This example is to illustrate the design of one way and two way spanning walls in a rectangular water tank. Design an open overhead tank (internal dimensions 3.5 m x 6 m x 2.5 m) supported on a reinforced concrete frame structure as shown below. Use a minimum thickness of 200 mm for walls and floor slab. slab. Over flow pipe 200 mm 2.5 m
3.5 m
Consider the following material properties in the design Density of water = 9.8 kN/m3 Density of concrete = 25 kN/m3 fcu = 35 N/mm2 f y = 460 N/mm2
effective length l x = 6000 6000 + ½ x 2 x 200 = 6200 mm effective height ly = 2500 + ½ x 200 = 2600 mm l x
6200
l y
2600
2.4
2
200 mm
2.5 m
6m
200 mm
Hence slab slab will span one way i.e. as a cantilever. cantilever.
Design of water-retaining structures
2
REF
BS 8007
2.2.2
CALCULATIONS CALCULATIONS
OUT PUT
Maximum water pressure = 9.8 x 2.5 x 1.4 = 34.3 kN/m2 0 0 Water load F = ½ x 34.3 x 2.5 x 1 5 2 = 42.875 kN/m BM at base (vertical (vertical bending) = 42.875 x [1/3 [1/3 (2.5) + 0.1] = 40.02 kNm/m
The liquid level should be taken to the working top liquid level or overflow level. Maximum water pressure = 9.8 x 1.0 x 2.3 = 22.54 kN/m 2 Water load = ½ x 22.54 x 2.3 = 25.92 kN/m Maximum vertical BM = 25.92 x [1/3 x 2.3 + 0.1] = 22.46 kNm/m Maximum shear force at Base = 25.92 kN/m kN/m
l x
= 3500 + ½ x 2 x 200 = 3700 mm = 2500 + ½ x 200 = 2600 mm
ly l x
3700
l y
2600
1.4
2
3500 2500
(Two way spanning slab)
Maximum water pressure at ULS
= 9.8 x 2.5 x 1.4 = 34.3 kN/m2
Maximum water pressure at SLS
= 9.8 x 2.3 = 22.5 kN/m 2
BM at Base (ULS) = 40.02 kNm/m SF at Base (ULS) = 42.875 kN/m
Ultimate limit state analysis of two way spanning walls Method 1 – By elastic analysis with ULS loads (approximate method) Method 2 - Plastic analysis using yield line theory ( exact method) Method 1 To carry out elastic analysis of thin walls any available method can be used. There are design charts (T 53) are available in the Reynolds’s Hand book for different boundary conditions of the wall. The curves given in Table 53 (RHB) can be used to calculate critical service bending moments on vertical and horizontal strips of unit width when the slab is fully fixed or freely supported or unsupported along the top edge. The curves are based on elastic analyses and for a value of Poisson’s ratio of 0.2. Maximum water load (ULS) = f = 34.3 kN/m 2 Using T53/RHB 0.015
For top edge unsupported wall slab l x = 3700 l z = 2600 k = l x / l z = 1.4 Mm = 0.015 x 34.3 x 2.6 2 = 3.48 kNm/m Ms = 0.055 x 34.3 x 2.6 2 = 12.75 kNm/m Mhm = 0.008 x 34.3 x 3.7 2 = 3.76 kNm/m Mhs = -0.021 x 34.3 x 3.7 2 = 9.86 kNm/m
Method 2 – Yield line analysis The ultimate moments in a wall panel subjected to triangular loading can be determined by Yield-line method. A feature of yield line method of designing two-way slabs is that the designer is free to choose the ratio between the moments in each direction and between the positive and negative units in each direction. However, in case of wall panel subjected to triangular load distribution results from the storage of liquid, it is more important to ensure that the choice of these ratios in such that the formation of cracks under service loading is minimized. This is achieved if the ratios selected correspond approximately to those given by elastic analysis. The following design procedure is thus suggested. 1. Determine the proportion of the horizontal moments at mid span Mhm and at the supports M hs, and the vertical moment at the base Ms to the vertical moment at mid span M m from the appropriate chart on T53/RHB. 2. Then if i4 = Ms / Mm , = Mhm / Mm and i1 = i3 = Mhs / Mm , determine , i1, i3 and i4 3. Calculate lyr from l yr
2l y (1 i1 ) 1 i3
and if the slab is supported at top edge, calculate l xr from l xr
2l x (1 i2 )
1 i4
4. Finally, with f, l x (or l xr ), l yr and i , determine M from the scale on Table 58 (RHB) if the slab is supported at top edge and from the chart T 61 otherwise. In the given example. l x = 3700 l z = 2600 k = l x / l z = 1.4
From T 53 – top edge unsupported f = 24.5 kN/m2 Mm = 0.015 x 24.5 x 2.6 2= 2.48 kNm/m Ms = 0.055 x 24.5 x 2.6 2 = 9.12 kNm/m Mhm = 0.008 x 24.5 x 3.7 2 = 2.68 kNm/m Mhs = -0.021 x 24.5 x 3.7 2 = 7.04 kNm/m
OUT PUT
Design Example 1
5
CALCULATIONS REF
OUT PUT
The most suitable values for , i1, i3 and i4 i4
i1
9.12
M m M hm
i
l yr
2.48
3.6
1.08
2.68
M m
3
l yr
l x
M s
2.48
M hs M m
7.04
2l y
(1 i1 )
1.94
1.08 x 2.48
1 i3
2.63 2 3.7
1
2.63
2
1.94
0.75
2.6
From T61 /RHB
M
flx
2
0.013
(for i4 = 3, lyr / l x = 0.8)
M = M m = 0.013 x 34.3 x 2.6 2 Ms = i4 x Mm = 3.6 x 3.01 Mhm = 1.08 x M m = 1.08 x 3.07 Mhs = 2.63 x 1.08 x 3.01
Short wall L y = 3.7 m L x = 2.6 m K = ly / l x = 1.42 < 2
OUT PUT
R2
R1
2500
3500
R3
Total water load = ½ x 34.3 x 3.5 x 2.5 R4
Assuming total load is uniformly distributed Intensity of load (w) = ½ x 34.3 = 17.15 kN/m 2 From T63 /RHB R 1 = R 3 = ½ K (1 - ¼ K) w l x2 = ½ x 1.42 (1 – 1.42/4) x 17.15 x 2.6 2 = 52.3 kN (total load carried by the shorter side)
Direct tension carried by long wall = 52.3/2.6 = 20.12 kN/m
Maximum water pressure = 22.54 kN/m 2 W = ½ x 22.54 = 11.27 kN/m 2 From T63/RHB R 1 = R 3 = ½ x 1.42 (1 – 1.42/4) x 11.27 x 2.6 2 = 34.9 kN Direct tension carried by long wall (SLS) = 34.9/2.6 = 13.41 kN/m
Mm Long wall Short 3.01 wall Short 3.48 wall
ULS Mhm Ms (KNm/m) 40.02 10.84
-
Mhs
T
Mrm
KN/m
-
3.25 8.55 Method 2 12.75 3.76 9.86 Method 1
20.12
SLS Mlm Ms (KNm/m)
-
22.46
2.39
8.38
-
Mhs
T KN/m
-
13.41
2.47 6.48
-
Design Example 1
7
CALCULATIONS
OUT PUT
REF
2.7.6
Thickness of the wall = 200 mm Cover = 40
Assume main bars to be 20 mm and distribution bars to be 12 mm. d = 200 – 40 – 12 – 20/2 = 138 mm M = 40.02 KNm/m K’ = 0.156 No. redistribution K
3.4.4.4/ BS8110
M 2
bd f cu
Z d 0.5
40.02 10 10
3
12 Ø 20 Ø
6
1382 35
0.25
40
0.06 K '
Hence no compression r/f is reqd
K
200
0.9
= 0.93 d = 0.93 x 138 = 128.3 mm As
M 0.87 f y Z
6
40.02 10
0.87 460 128.3
T = 20.12 KN/m
A s
2
779mm / m
20.12 10
3
0.87 460
There are two methods available to calculate r/f under SLS Method 1 – Based on limiting steel stress Method 2 – Based on crack width limitation
2
50.3mm /m
Design of water-retaining structures
8
CALCULATIONS
REF
OUT PUT
BS 8007
Considering the method 1 M (SLS) = 22.46 KNm/m 3
M 2
bd
T 3.1
22.46 10 3
10
1.2
Allowable steel stress f st = 130 N/mm 2 From design chart T 118 (Reynold’s HB) = 0.011 f cr = 6.5 N/mm2 (Maximum compression stress of concrete) A s bd
B2
2
138
0.011
As = 0.011 x 10 3 x 138 = 1518 mm 2 /m
Ultimate stress of concrete = 0.45 f cu = 0.45 x 35 = 15.8 N/mm2 > f cr = 6.5 N/mm 2 Hence concrete Stress is not near ultimate. Note: Method of obtaining As by calculating crack width (method 2) will be illustrated later.
T 3.1
Allowable steel stress = 130 N/mm 2 A st
T f st
13.41 103 130
103.2mm2 / m
2.6.2.3 A.2 T A.1 Fig. A.1
Minimum steel ratio in each surfaces zone is given by crit
f ct f y
A s bh'
0.0035
0.0035
h ‘ – Depth of surface zone
Design Example 1
9
CALCULATIONS
OUT PUT
REF
BS8007
h’ = h/2 (Since h 500 mm) = 100 mm As = 0.0035 x 10 3 x 100 = 350 mm 2 / m per each layer.
Fig. A.1
R/f in controlling crack spacing has to be provided according to Cl. A.3 (8007). Wmax = Smax R . . (T 1 + T 2) T 1 = 30o C T 2 = 10o C = 10 x 10-6 / oC R = 0.5 for rigid end restraints
This steel ratio has to be placed in both surface zones. As = 0.004 x 1000 x 100 = 400 mm2 / m (for each direction) Calculate r/f required for 20 mm bars as well.
200
Design of water-retaining structures
10
EF
CALCULATIONS
OUT PUT
R/f to carry ult. BM (u1) - 779 mm 2 /m (U 1) R/f to carry serv. BM (S1) - 1518 mm 2 /m (S1) R/f to shrinkage and thermal movement - 400 mm2 /m (S3) per each layer.(S3) U1 - 771 S1 - 1518
S3 - 400
( Y20 @ 200 )
S3 - 400
200
R/f to carry ult. tension - 50.3/2 per layer (U 2) R/f to carry serv. tension - 103.2/2 per layer (S 2) R/f to shrinkage and thermal movement - 400 per layer (S 3)
U2 - 50.3/2 S2 - 103.2/2 S3 - 400 ( Y12@275 )
U2 - 50.3/2 S2 - 103.2/2 S3 - 400
200
2.6.2.3
Maximum spacing – lesser of 300 mm and thickness of the member (200mm). Therefore max. spacing = 200 mm
Y12@200
Y20@200
Y12@200
Y12@200
200
Design Example 1
11
REF
OUT PUT
CALCULATIONS
BS8110
3.5.5
Ultimate Shear force at the base = 42.875 KN/m
V bd
100 A s
bd
3.4.5.4
3.12.8.3
10
3
f cu 0.8
0.8
3.4.5.2
42.875 10
1000 138
0.31 N / mm 2
138 2 35 4.73 N / mm
5 or
100 1570
3
0.8
f cu
.
Hence OK
1.14
T3.9 /BS 8110 indicates V c > v (=0.31) Hence No. shear r/f are required. Note: This is the normal situation.
Bond stress f b f bu (design ult anchorage bond stress) f b
3.12.8.4
F s .l
f bu
0.87 f y . . 2 4 .l f cu
0.217 f y l
f bu
0.5 35 0.7
T 3.28 ( BS 8110)
2.07 N / mm 2
The design ultimate anchorage bond stress for horizontal bars in sections under direct tension should not be greater than 0.7 times the values in 3.12.8.4/BS8110. f b
f bu
0.217 460 12
2.07
l l 579mm
Anchorage length for 12Ø bars = 580 mm
Design of water-retaining structures
12
REF
CALCULATIONS
Use lap length required according to (Cl. 3.12.8.9 / 3.12.8.11 / 3.12.8.13 and T 3.29) Simplified rules for curtailment given in Cl. 3.12.10.3 of BS 8110 do not apply as the wall is not subjected to a UDL. Bars should extend beyond the point at which it is no longer required for a distance equal to an anchorage length. In this particular example it is not possible to curtail the bars as it violates the maximum bar spacing requirement.
The hand book for the previous code of practical (BS 5337) states that deflection at the top of wall need not be checked for open structures.. But when the reservoir is roofed, or supported at top, the criteria has to be checked. Cl. 3.5.7 / BS 8110 , Cl 2.1/ BS 8007 give the procedure to check deflection. Example 2 explains the applications of these clauses.
This is repetition of step a.1.3 (done by limiting steel stress method) To calculate crack width following procedure is necessary. (a) Calculate serviceability BM (b) Calculate depth of N.A, lever arm and steel stress by elastic theory. (c) Calculate surface strain allowing for stiffening effect of concrete. (d) Calculate the crack width. Consider long wall, h = 200 mm, M = 22.46 kNm/m
d = 138 mm
OUT PUT
Design Example 1
13
CALCULATIONS
OUT PUT
REF
(As) provided = 1570 mm 2 /m ρ
A s
bd
1570 10
3
138
(Y 20 @ 200)
0.0114
Es = 200 kN/mm 2 Ec = ½ x static modulus = ½ x 27 (T.7.2 / BS 8110) = 13.5 N/mm2 αe
Es
Ec
200
αeρ
13.5
200
13.5
0.0114 0.169
2 1 1 d αeρ 2 0.169 1 1 0.436 0.169 X = 0.436 x 138 = 59.4 mm
a C min 2 cr h x Cmin = 40 + 12 = 52 mm (acr + 10) 2 = 622 + 100 2 acr = 107.7 mm 1
w
3 107.7 0.815 10
3
107.7 52 200 59.4
1 2
0.15mm
0.2mm Hence O.K.
Note: Since the crack width is not close to the design crack width it is possible to reduce the reinforcement. Therefore by adopting this method an economical solution can be achieved.
OUT PUT
Design Example 1
15
CALCULATIONS
OUT PUT
REF
For large structures it is possible to save amount of steel required to control cracking in immature concrete, as well as to obtain a large spacing between bars so that compaction of concrete will be easier by the use of movement joints (Cl. 5.3 / 8007) Cl. 5.3.3 / 8007 gives the options available in providing movement joints. These options are explained by the following examples. Design r/f to control cracking due to shrinkage and thermal movement in immature concrete in a wall 225 mm thick. f cu = 35 N/mm2 f y = 460 N/mm2 (10 mm - type 2 deformed bars) Option (1) - Continuous construction (with no joints) A2 / 8007
crit
f ct
1.6
f y
0.0035
460
Wmax = Smax . R (T 1 + T 2) W max S max
Also
S max
1
f ct f b
W max 2 10
4
0.2 2 10
2
4
10 10 6 (30 10) 2 10
2
0.67
4
(A.3 / 8007 ) 10 2
0.67
10 2
0.00335 crit
Hence provide crit = 0.0035
A s
225 2
1000
As = 394 mm2 /m (each surface zone, each direction) Provide Y 10 @ 175 mm C/C(A s = 449 mm2)
Design of water-retaining structures
16
REF
CALCULATIONS
crit = W max S max
R (T 1
Also
T 2
S max
0.2
½ x 10 x 10-6 x (30 + 0) = 1.5 x 10-4
f ct f b
1.5 10
0.0035
)=
OUT PUT
2
0.67
10
0.67
10 2
2
4
0.0025
provide crit = 0.0035 i.e. Y10 @ 175 mm c/c .
Minimum steel ration
= 2/3 crit = 2/3 x 0.0035 = 0.00233
As given in T 5.1 (Note 2) / 8007, the minimum steel ratio is sufficient in option (3). As = 0.00233 x 1000 x 225/2 = 263 mm 2 /m provide Y 10 @ 200 mm c/c (maximum bar spacing ) Joint spacing for option 3 (a)
4.8
w
4.8
W max S max S max
R. .T 1
S max
1 2
(if Wmax isused) A.3/8007
10 10
0.2
1 2
10 10
6
6
30
1333.3mm
30
Joint spacing =
4.8 + 1.33 = 6.13 m provide complete joints at 6 m.
Joint spacing for option 3 (b) 0.5 Smax + 2.4 + W/ = 0.5 Smax + 2.4 + S max = 1.5 Smax + 2.4 = 1.5 x 1.33 + 2.4 = 4.4 m Joint spacing for option 3 (b) 4.4 m Provide alternate partial and complete joints at 4 m .
REF
Design Example 1
17
CALCULATIONS
OUT PUT
Joint spacing for option 3 (c) Smax + W/ = Smax + Smax = 2 Smax = 2 x 1.33 = 2.7 m
provide partial joints at spacing of 2.5 m.
Control of early thermal contraction and restrained shrinkage in walls and slabs can be effected by a suitable arrangement of r/f with or without joints. At one extreme control can be obtained by providing substantial amount of r/f in form of small bars preferably of high bond type at close spacing and without joints in conc. At the other extreme control can be effected by presence of minimum r/f in form of large bars together with movement joints at close spacing.
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