-
12
6.0 REKA BENTUK RASUK DISOKONG MUDAH
Ref. Calculation Output
SPECIFICATION W kN/m
L h
b
Effective span, L = 8.25m
Characteristic actions :
Permanent, gk = 15 kN/m
Variable, qk = 10 kN/m
Design life = 50 years
Fire resistance = R60
Exposure classes = XC1
Materials:
Characteristic strength of concrete, fck = 20 N/mm2
(Table F.1 EN
206)
Characteristic strength of steel, fyk = 500 N/mm2
Characteristic strength of link, fyk = 500 N/mm2
Unit weight of reinforced concrete = 25 kN/m3
(Table A.1 EN
1991-1)
Assumed:
bar 1 = 20mm
bar 2 = 12mm
link = 8mm
(Excluding
selfweight)
(Table 2.1 EN 1990)
SIZE Overall depth, h = L /13 = 8250/13 = 20mm
Width, b = 0.4h = 0.4x 635 = 254mm
Use : b x h
= 250 x 650 mm
Table 4.2
Table 4.4N
4.4.1.2
4.4.1.3
4.4.1.1(2)
DURABILITY, FIRE & BOND REQUIREMENTS
Min. conc. Cover regard to bond, C min,b = 20mm
Min. conc. Cover regard to durability, C min, dur = 15mm
Min. required axis distance for R60 fire resistance,
asd = 30 + 10 = 40mm
Min. concrete cover regard to fire,
Cmin = asd - link - bar/2
= 40-8-0.5(20) = 22mm
Allowance in design for deviation, Cdev = 10 mm
Nominal cover,
Cnom = Cmin + Cdev = 20 + 10 = 30mm
Table 5.5 EN 1992-
1-2
Use :
Cnom = 35mm
-
13
Ref Calculation Output
Table A
1.2B
:EN 1990
LOADING & ANALYSIS
Beam selfweight = (0.25 x 0.65) x 25 = 4.06 kN/m
Permanent load (excluding selfweight) = 15.00 kN/m
Characteristic permanent action, gk = 19.06 kN/m
Characteristic variable action, qk = 10.00 kN/m
Design action,
Wd= 1.35gk + 1.5 qk = 1.35(19.06) + 1.5(10.00)
= 40.73 kN/m
Wd= 40.73 kN/m
L=8.25m
Shear force,
V = wd L/2
= 40.73(8.25)/2
= 168.0 kN
M
BENDINGMOMENT
M = wdL2/8
= 40.73(8.25)2/8
=346.6 kNm
MAIN REINFORCEMENT Effective Depth,
D = H Cnom - link - bar = 587mm
D = Cnom - link - bar/2 = 49mm
Design Bending Moment, Med = 346.6 Knm
K = M/Bd2fck
= 346.6x106 / (250 X 587
2 X 20)
= 0.201
Redistribution = 0% Redistribution ratio, = 1.0
Kbal = 0.454 ( - k1)/ k2 0.182( - k1)/k2]2
= 0.363 ( - k1) 0.116 ( -k1)2
= 0.167
K > Kbal Compression reinforcement is required
z = d [ 0.5 + 0.25 kbal/1.134 ]
= 0.82d
d
b
Using : EC2
K1 = 0.44
K2 = 1.25
-
14
Ref Calculation Output
= 0.82(587)
= 481.8 mm
X = (d-z)/ 0.4 = 263.1 mm
d/x = 49/263.1 = 0.19 < 0.38
: the compression steel will have yielded
fsc = 0.87 fyk
Area of compression steel
As = ( K Kbal) fckbd2
/ 0.87fyk (d - d)
= ( 0.201 0.167) x (20 x 250 x 5872)
0.87 x 500 x (587 -49)
= 250 mm2
Area of tension steel
As = kbalfckbd2 / 0.87fyk Z bal + As
= 0.167 x (20 x 250 x 5872) + 252
0.87 x 500 x 481.8
= 1623 mm2
Minimum and maximum reinforcement area,
As, min = 0.26(fctm/fyk) bd
= 0.26 (2.21/500) bd
= 0.0011 bd use= 0.0013bd
= 0.0013 x 250 x 587 = 119mm2
As,max = 0.04AC = 0.04bh
= 0.04 x 250 x 650 = 6500mm2
Use : 3H 12
(339 mm2)
Use : 6H 20
(1885 mm2)
SHEAR REINFORCEMENT
Design shear force, VEd =168.0 Kn
Concrete strut capacity
VRd, max = 0.36b wdfck ( 1- fck/250) / (cot + tan )
= (0.36 x 250 x 587 x 20 (1-20/250)
Cot +tan
=338Kn = 22 deg cot = 2.5
=486Kn = 45 deg cot = 1.0
VED < VRD,max cot = 2.5
VED < VRD, max cot = 1.0
Therefore angle < 22o
= 0.5 sin -1
[VED / 0.18bwdfck(1-fck/250)]
= 0.5 sin-1
( 168.0 x 103
)
(0.18 x 250 x 587 x 20 (1- 20/250)
-
15
Ref Calculation Output
=0.5 sin
-1 (0.35)
= 10.1o
Use: = 22.0 o tan = 0.40 cot = 2.48
9.2.2 (6)
9.2.2 (5)
Shear links
ASW/S =VED/0.78fykd cot
=168.0 x 103 /(0.78x 500x 587x 2.48)
=0.297
Try link: H8 ASW = 101 mm2
Spacing s = 101/0.30
=339 mm
Max. spacing , s max = 0.75d =0.75x 587 =440mm
Minimum links
ASW/S = 0.08fck1/2
bw/fyk
=0.08 x(20)
x 250/ 500
=0.179
Try link: H8 ASW = 101 mm2
Spacing s = 101/0.18
=562mm > 0.75d =440mm
Shear resistance of minimum links
V min = (ASW/s)( 0.78fykd cot )
=(101/425) x (0.78 x 587 x 500 x 2.5)
=134kN
Use :
H8-325
Use :
H8-425
Links arrangement 168kN
X = (16-134)/40.7
=0.83m
134kN
134kN
168kN
-
16
Ref Calculation Output
Additional longitudinal reinforcement
Additional tensile force,
F td =0.5 vEd cot
= 0.5 x 168 x 2.48
= 208 Kn
MED,max/Z = 346.6 x 106 / 481.8
= 719 kN > F td
Additional longitudinal reinforcement,
As = F td/0.87fyk
= 207.94 x 103
/ 0.87 x 500
= 478 mm2
Use : 2H 20
(628 mm2)
DEFLECTION Percentage of required tension reinforcement
= As,req/bd
= 1624 / 250 x 587
= 0.011
Reference reinforcement ratio,
o = ( fck)1/2
x 10-3
= (20)1/2
x 10-3
= 0.0045
Percentage of required compression reinforcement
= As,req / bd
= 252 / 250 x 587
= 0.002
Factor for structural system , K = 1.0
> o (use equation 2)
1/d = K [11 + 1.5 fck o/ + 3.2 fck(o/ 1)3/2
] -> (1)
1/d = K [11 + 1.5fck o/ + 1/12 fck/] ->(2)
= 1.0 (11 + 3.21 + 0.23)
=14.4
Therefore basic span-effective depth ratio, l/d =14.44
Modification factor for span greater than 7m
= 7/span = 7/8 =0.85
-
17
Ref Calculation Output
Modification factor for steel are provided,
As,prov / As,req =1885 / 1624 =1.16 < 1.5
Therefore allowable span-effective depth ratio
(i/d) allowable =14.44 x 0.85 x 1.16 =14.22
Actual span effective depth
(i/d)actual =8250 /857 =14.1 < (i/d)allowable
Table 7.1 N CRACKING
Limiting crack width, w max = 0.3mm
Steel stress,
fs = fyk/1.15 x [Gk + 0.3 Qk/(1.35Gk + 1.5 Qk)](1/)
= (500/1.15) x [19.1 + 0.3(10) / 1.35 (19.1) + 1.5
(10)](1.0)
= 236 N/mm2
Max allowable bar spacing = 150 mm
Bar spacing
s = [250-2(35)-2(8)-(20)]/2
=72 mm < 150mm
-
18
Ref Calculation Output
DETAILING
-
19
7.0 REKA BENTUK RASUK SELANJAR
Ref Calculations Output
SPECIFICATION
Dimension:
Span, L = 8.00 m
Width, B = 3.00 m
Slab thickness = 110 mm
Beam size = 225 x 500 mm
Charasteristic loads:
Finishes, etc = 1.5 kN/m2
Variable, qk = 3.0 kN/m2
Materials:
Unit weight of concrete = 25 kN/m3
Charasteristic strength of concrete, fcl = 25 N/m2
Charasteristic strength of steel, fyk = 500 N/m2
Charasteristic strength of link, fyk = 500 N/m2
Nominal concrete cover = 30 mm
Assumed : bar 1 = 20 mm
bar 2 = 16 mm
link = 6 mm
Design beam 1a/A-D
Beam 1a/A-D
w kN/m w kN/m w kN/m
A 8.0 m B 8.0 m C 8.0 m D
-
20
Ref Calculation Output
EFFECTIVE FLANGE WIDTH
Effective flange width,
b eff = beff i +bw b
beff i= 0.2bi + 0.1lo 0.2lo
Span A-B, C-D
l =0.85l = 0.85 x 8000 = 6800 mm
b eff,1 = 960 mm
-
21
Ref. Calculation Output
Action on beam 1a/A-D : Distribution of action from slabs to
beam are as follows :
Panel 1-1a/A-D :
LY/LX = 8.00/3.00 =2.7 > 2.0, one-way slab
Shear coefficient, v = 0.50
Panel 1a-2/A_D:
LY/LX = 8.00/3.00 =2.7 > 2.0, one-way slab
Shear coefficient, v = 0.5
Characteristic permanent action:
Wo = 0.225 (0.50 0.11) x 25 = 2.19 kN/m
W1 = vnLx = 0.50 x 4.25 x 3.00 = 6.38 kN/m
W2 = vnLx = 0.50 x 4.25 x 3.00 = 6.38 kN/m
Gk = 14.95kN/m
Characteristic variable action :
W1 = vnLx = 0.50 x 3.00 x 3.00 = 4.50 kN/m
W1 = vnLx = 0.50 x 3.00 x 3.00 = 4.50 kN/m
Qk = 9.00 kN/m
Design load,
Wd = 1.35Gk + 1.5Qk
= 1.35(14.95) + 1.5(9.00) = 33.68 kN/m
ANALYSIS
Continuous beam with equal spans, uniform action and
Qk < Gk use moment and shear coefficient
From table 3.14 BS8110 Part 1
Wd kN/m Wd kN/m Wd kN/m
L m L m L m
A B C
D
0.11 FL 0.11 FL
0.09 FL 0.07 FL 0.09
FL
0.45 F 0.55 F 0.6 F
0.6 F 0.55F 0.45 F
F = WD L kn = 33.67 x 8.0 = 269 kN
Shear Force
Bending Moment
-
22
Ref. Calculation Output
9.2.1.1
MAIN REINFORCEMENT
Span A-B & C-D
Effective depth, d = h Cnom - link 0.5 bar = 454.0 mm
Bending moment,
M = 0.09 FL
= 0.09 X 269 X 8.0 = 194 kNm
Mf = 0.567 fckbhf (d - 0.5h)
= 0.567 x 25 x 2145 x 110 ( 454.0 55 )
= 1334 kNm
M < Mf neutral axis within the flange
K = M/fck bd2
= 194 x106 / (25 x 2145 x 454.0
2)
= 0.018
z = d [ 0.5 + 0.25 K/1.134)] = 0.98d
Area of tension reinforcement
As = M/0.87 fyk z
= 194.0 x 106 / (0.87 x 500 x 0.95 x 454.0)
= 1034 mm2
Minimum and maximum reinforcement area,
As min = 0.26 (fctm /fyk ) bd
= 0.26 ( 2.56 / 500) bd
= 0.0013bd use= 0.0013bd
= 0.0013 x 225 x 454.0 = 136 mm2
As max = 0.04 Ac = 0.04 bh
= 0.04 x 225 x 500 = 4500 mm2
Support B & C
Effective depth, d = h Cnom - link - bar = 444.0 mm
Bending moment,
M = 0.11 FL
= 0.11 X 269 X 8.0 =237kNm
K = M/ bd2 fck
= 237.1 x 106 / ( 225 x 444
2 x 25)
= 0.214
Redistribution = 0% redistribution ratio, = 1.0
K bal = 0.454( - k1)/k2 0.182[ - k1)/ k2]2
= 0.363 ( - k1) 0.116 ( - k1)2
= 0.167
Use : 5H 20
(1571 mm2)
Use : EC2
K1 = 0.44
K2 = 1.25
-
23
Ref. Calculation Output
K > kbal
Compression reinforcement is required
d = c + link + 0.5 bar =44mm z =d (0.5 + 0.25- kbal /1.134)
= 0.82d =0.82 x 444 =364.4mm
X = (d-z)/0.4 =199.0mm
d/x =44/199.0 = 0.22 < 0.38
the compression steel will have have yielded
area of compression steel
As = (k- kbal) fckbd2/0.87fyk (d- d )
= (0.214-0.17)x (25 x 225 x 4442)
0.87 x 500 x (444-44)
=299mm2
Area of tension steel
As = (k- kbal) fckbd2/0.87fyk z bal + As
= 0.167x (25 x 225 x 4442)
0.87 x 500 x 364 + 299
= 1466mm2
Asmin = 0.0013 bd =136mm2
Asmax = 0.04 bh = 4500mm2
Span B-C
Effective depth , d =h-cnom link- bar =444.0 mm
Bending moment,
M =0.07FL
=0.007 X 269 X8.0 =151 kNm
Mf =0.567 fckbhr(d-0.5h)
=0.567 x 25 x 1345 x 110 (454.0-55)
=837 kNm
M < Mf neutral axis within the flange
K =m/fckbd2
=151 x 106/ (25 x1345 x454.0
2)
=0.022
Z = d(0.5+ 0.25-k/1.134) = 0.98 d
Use : 5H 20
(1571 mm2)
Use : 2H 16
(402mm2)
-
24
Ref. Calculation Output
Area of tension renforcement
As = M/0.87fyk =
= 150,9X106/(0.87 X 500 X 0.95 X 454.0)
=804mm2
Asmin =0.0013 bd =136mm2
Asmax =0.04 bh = 4500mm2
Use : 3H 20
(943mm2)
6.2.3
9.2.2 (6)
6.2.3 (7)
SHEAR REINFORCEMENT
Design shear force, VEd =168.0 Kn
Concrete strut capacity
VRd, max = 0.36b wdfck ( 1- fck/250) / (cot + tan )
= (0.36 x 250 x 587 x 20 (1-20/250)
Cot +tan
=338Kn = 22 deg cot = 2.5
=486Kn = 45 deg cot = 1.0
Support A & D
VED =0.45 F = 0.45 X 269 =121 kNm
< VRD,max cot = 2.5
< VRD, max cot = 1.0
Therefore angle < 22o
Shear link
Asw /s = ved /0.78fyk dcot
= 121.2 x 103/ (0.78 x 500 x 454 2.48)
=0.277
Try link : H6 Asw = 57mm2
Spacing, s =57/0.2777
= 204mm < 0.5d = 341 mm
Additional longitudinal reinforcement
Additional tensile force,
f td = 0.5 ved cot
= 0.5 x 121 x 2.48
= 150 kN
MEd max/z = 194.0 X 106/431.3
=450 kN > F td
As req =F td/0.87fyk =150 x 10
3 /(0.87x 500)
= 345mm2
Use :H6-200
Use :2H-200
-
25
Ref. Calculations Output
9.2.2 (6)
6.2.3 (7)
9.2.2 (6)
6.2.3 (7)
Support B & C
VEd = 0.60 F = 0.60 x 269 = 162 kN
< VRd, max cot = 2.5
< VRd, max cot = 1.0
Therefore angle < 22
Shear links
Asw / s = VEd / 0.78 fyk d cot
= 161.6 x 103 / (0.78 x 500 x 454 x 2.48)
= 0.369
Try link : H6 Asw = 57 mm2
Spacing, s = 57 / 0.369
= 153 mm < 0.75d = 341 mm
Additional longitudinal reinforcement
Additional tensile force,
Ftd = 0.5 VEd cot
= 0.5 x 162 x 2.48 = 200kN
As req = Ftd / 0.87fyk
= 200 x 103 / (0.87 x 500) = 460 mm
2
Support B & C
VEd = 0.55 F = 0.55 x 269 = 148 kN
< VRd, max cot = 2.5
< VRd, max cot = 1.0
Therefore angle < 22
Shear links
Asw / s = VEd / 0.78 fyk d cot
= 148.2 x 103 / (0.78 x 500 x 454 x 2.48)
= 0.338
Try link : H6 Asw = 57 mm2
Spacing, s = 57 / 0.338
= 167 mm < 0.75d = 341 mm
Additional longitudinal reinforcement
Additional tensile force,
Ftd = 0.5 VEd cot
= 0.5 x 148 x 2.48 = 183 kN
As req = Ftd / 0.87fyk
= 183 x 103 / (0.87 x 500) = 422 mm
2
Use : H6 150
Use : 3H 16
( 603 mm2)
Use : H6 150
Use : 3H 16
( 603 mm2)
-
26
Ref. Calculation Output
9.2.2 (5)
9.2.2 (6)
6.2.4
Minimum links
Asw / s = 0.08fck1/2
b w / fyk = 0.08 x (25)
x 225 / 500
= 0.180
Try link : H6 Asw = 57 mm2
Spacing, s = 57 / 0.18
= 314 mm
< 0.75d = 0.75 x 454 = 341 mm
Shear resistance of minimum links
Vmin = (Asw / s) (0.78dfyk cot )
= (57 / 300) x (0.78 x 454 x 500 x 2.5)
= 83 kN
Link arrangement
121 148 162 83
83 162 148 121
x1 x2 x3 | | | | |
x1 = (121 83) / 33.67 = 1.14 m
x2 = (162 83) / 33.67 = 2.34 m x3 = (148 83) / 33.67 = 1.94
m
Transverse steel in the flange
The longitudinal shear stresses are the greatest over a distance
x
measured from the point of zero moment.
x = 0.5(L/2) = (L/4) = 8000 / 4 = 2000 mm
The change in moment over distance x from zero moment,
M = (wL/2) (L/4) (wL/4) (L/8) = 3wL2/32
= 3 x 33.7 x 8.02 / 32 = 202.04 kNm
The change in longitudinal force,
Fd = [ M / (d 0.5hf) ] x [ (b bw) / 2b ]
= 202.04 x 103
x
(2145 225)
(454 55) (2 x 2145)
= 227 kN
Use :
H6 - 300
-
27
Ref Calculations Output
Longitudinal shear stress
VED = FO / (hfx)
= 227 x 103 / (110 x 2000)
= 1.03 N/mm2
VED > 0.27fck = 0.27 x 2.03 = 0.55 N/mm2
Transverse shear reinforcement is required
Concrete strut capacity in the flange
vED max = 0.4fck (1-fck / 250) / (cot + tan )
= ( 0.40 x 25 ( 1- 25 / 250)
( cot + tan )
= 3.59 N/mm2 = 27 deg cot = 2.0
= 4.50 N/mm2
= 45 deg cot = 1.0
vED < vED, max cot = 2.0
vED < vED, max cot = 1.0
therefore angle < 27o
= 0.5 sin -1
[ vED / 0.2 fck(1 - fck / 250)]
= 0.5 sin -1
{ 1.03 }
{0.20 x 25 (1 25/250)}
= 0.5 sin -1
{0.23}
= 6.62o
Use : = 26.5o tan = 0.50 cot = 2.0
Transverse shear reinforcement
Asf / sf = vED hf / 0.87 fykcot
= 1.03 x 110 / (0.87 x 500 x 2.0)
= 0.13
Try : H10 Asf = 79 mm2
Spacing, sf = 79/0.13 = 605mm
-
28
Ref. Calculation Output
Minimum transverse steel area,
As,min = 0.26( fctm / fyk) bhf
= 0.26 (2.56 / 500)bhf = 0.0013 bhf Use = 0.0013bhf
= 0.0013 x 1000 x 110.0
= 147 mm2/m
Use:
H10-400
(196 mm2/m)
DEFLECTION
Check at span A-B
Percentage of required tension reinforcement,
= As,req / bd
= 1034 / 225 x 454 = 0.010
Reference reinforcement ratio,
o = (fck)1/2
x 10-3
= (25)1/2
x 10-3
= 0.005
percentage of required compression reinforcement,
= As,req / bd
= 0 /225 x 454 = 0
Factor for structural system, K = 1.3
> o use equation (2)
1/d = K [ 11 + 1.5 fck o/ + 3.2 fck(o/ 1)3/2
] (1)
1/d = K [11 + 1.5fck o / + 1/12 fck / ] (2)
= 1.3( 11 + 3.71 + 0.00)
= 19.1
Therefore basic span-effective depth ratio, 1/d = 19.12
Modification factor for steel area provided,
=As,prov/ As,req
= 1571/1034
= 1.52 > 1.50
-
29
Ref. Calculation Output
Therefore allowable span effective depth ratio,
(1/d)allowable = 19.12 x 0.88 x 1.50 = 25.23
Actual span effective depth
(1/d)actual = 8000/454.0 = 17.6 < (1/d)allowable
OK!
CRACKING
Limiting crack width, wmax = 0.3 mm
Steel stress,
fs = fyk / 1.15 x Gk + 0.3Qk / (1.35Gk + 1.5Qk)(1/)
= (500/1.15) x [(14.9 + (0.3 x 9.0)) / 33.7] x 1.0
= 262 N/mm2
Max allowable bar spacing = 150 mm
Bar spacing
s = [ 225 2(30) 2(6) (20)]/2
= 66.5 mm < 150mm
OK!
-
30
Ref Calculations Output
DETAILING
-
31
ANGGARAN BAHAN
Ref Calculations Output
Simply supported beam
Konkrit
Isipadu konkrit = Panjang (P) x Lebar (L) x Tinggi (H)
= 8.25 x 0.25 x 0.6
= 1.24m3
Tetulang
Panjang 1 batang tetulang = 12 m
Jenis tetulang 3H-20 (2), 3H-12
Panjang tetulang 3H-20 = 6 x 8.25
= 49.5 m
Bilangan tetulang 3H-20 = 4.125
Panjang tetulang 3H-12 = 3 x 8.25
=24.75 m
Bilangan tetulang 3H-12 = 2.06
Continuous beam
Konkrit
Isipadu konkrit = Panjang (P) x Lebar (L) x Tinggi (H)
= 24 x 0.225 x 0.45
= 2.43 m3
Tetulang
Panjang 1 batang tetulang = 12 m
Jenis tetulang 3H-20, 2H-20 (4), 2H-25 , 1H-20 (2)
Panjang tetulang 3H-20 = 3 x 8
= 24 m
Bilangan tetulang 3H-20 = 2
Panjang tetulang 2H-20 = 4 x 8 (2)
= 64 m
-
32
Bilangan tetulang 2H-20 = 5.33
Panjang tetulang 2H-25 = 2 x 8
= 16 m
Bilangan tetulang 2H-25 = 1.33
Panjang tetulang 1H-20 = 2 x 8
= 16 m
Bilangan tetulang 1H-20 = 1.33
-
33
6.0 KESIMPULAN
Kesimpulannya rasuk merupakan satu komponen dalam struktur
bangunan
yang sangat penting. Tugasnya adalah untuk menerima dan
menanggung beban dari
bumbung, lantai dan sebagainya. Penggunaan rasuk sangat la luas
seperti di dalam
pembinaan ianya digunakan untung membuat jambatan, bangunan dan
sebagainya.
Rasuk terdiri daripada pelbagai jenis antaranya ialah rasuk
sokong mudah, rasuk
julur, rasuk selanjar dan sebagainya. Dalam pembinaan rasuk
ianya haruslah di reka
bentuk terlebih dahulu mengikut spesifikasi yang telah
ditetapkan dan ianya perlu
melepasi ujian kiraan supaya tiada sebarang kegagalan
terjadi.
Terdapat pelbagai jenis sistem rasuk yang biasa ditemui dalam
bidang
kejuruteraan, antaranya adalah rasuk disokong mudah, rasuk
julur, rasuk terbina
dalam, rasuk juntaian dan rasuk berterusan. Setiap keadaan ini
mempunyai kekuatan
yang berlainan bersesuaian dengan setiap kegunaannya. Apabila
menerima bebanan,
setiap rasuk akan mengalami pesongan di mana rasuk tersebut akan
melentur
mengikut arah daya yang dikenakan. Setiap rasuk mempunyai satu
tahap di mana ia
akan melentur pada satu kedudukan yang maksimum apabila beban
dikenakan.