BEAM DESIGN
DIMENSIONS:
Size of the beam =
230*375 mm
L = 4.803 m
d = 230 mm
D
= 260 mm
b = 375 mm
LOADS:
Total load on beam = 35.17 KNm
Mu = 0.125*Wu*L2
=
0.125*35.17*4.8032
Mu = 102 KNm
Vu = WL/2 = (35.17*4.803) / 2 = 70.34
KN
TENSION REINFORCEMENTS:
Mu lim
= 0.138*fck*b*d2
=
(0.138*20*375*2302)*10-6
Mu lim
= 29.2 KNm
Since Mu
< Mulim
The section is under reinforced.
Mu =
0.87*fy*Ast*d*[(1)-((Ast*fy) / (fck*b*d))]
29.2*106 = 0.87*415*Ast*150*[(1)-((Ast*415) /
(20*200*230))]
29.2*106 = 83041.5Ast
– 37.4589375Ast2
Ast = 438 mm2
Provide 2 bars of 16mm diameter (Ast= 402 mm2)
& 2 layer bars of 10 mm dia.
CHECK FOR SHEAR:
Vu = 70.34 KN
Nominal shear
stress (τv) = Vu / bd
= (70.34*103)
/ (230*375)
τv = 1.52
N/mm2
% of tensile reinforcement Pt = 100Ast / bd
= (100*402) /
(230*375)
= 1.005
From IS 456-2000, table 19.,
τc = 0.63 N/mm2
τc > τv
provide nominal shear reinforcement using 6mm dia of
two-legged stirrups at spacing of,
SPACING:
Sv = (Ast*0.87*fy)
/ (0.4*b)
=
(2*29.2*0.87*415) / (0.4*200)
= 255 mm
Sv = (0.75*d) = 0.57*200 > 150mm
Provide stirrups spacing = 150 mm
CHECK FOR DEFLECTION
CONTROL:
Pt = 1.005
Modification factor, Kt = 1.05 & by lecting the
hangerbar.
(L/d)max = (L/d)basic*Kt*Kc*Kf
=
20*1.05*1*1.05
= 22
(L/d)actual = 4803/200 = 24
Since (L/d)max = (L/d)basic
Deflection control is satisfactory.
DESIGN USING
SP-16 DESIGN TABLES:
Mu/bd2 = (29.2*106) / (200*2302)
= 2.76
Refer table sp-16,
Pt = 0.958
Ast = Pt*b*d /
100
=
(0.958*200*230) / 100
= 441 mm2
Hence Ast is the same as flat computed using theoretical
equation.
No comments:
Post a Comment