Civil Engineering Reference
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x = 1
h 0
2 M
f cm bh 01
1
= 1
1
10 6
2
×
194
×
×
565 = 113 mm
13 . 5
×
250
×
565 2
Bending moment resisted by prestressied reinforcements, Δ M ,is
A s f y h 0
x
2
Δ M = M max
565
=7 . 2
113
2
10 6
10 7 kN
= 194
×
1140
×
210
×
×
·
m
Thus,
10 7
Δ M
f py h + a p
7 . 2
×
= 435 mm 2
A p =
=
600 + 30
x
2
113
2
290
×
Choose 2 20, A p = 628 mm 2 .
e. Determine the tension control stress and calculate loss of prestress. According to Table
3.4, adopt the tension control stress as
σ con =0 . 85 f pyk =0 . 85
×
315 = 268 MPa
Calculate the loss of prestress. Two ends of the prestressed reinforcements are anchored
by welding, so σ l 1 =0.
Calculate the loss of prestress caused by friction at lower supporting points, σ 12 .Known
from Fig. 3.29, the angle between diagonal brace and longitudinal axis is 0.565 rad, assume
the friction coecient μ =0 . 25. Then substituting them into Eq. (3.43) gives
e −μθ ) = 268(1
e 0 . 25 × 0 . 565 )=35 . 3MPa
σ l 2 = σ con (1
The loss of prestress caused by stress relaxation can be obtained by Eq. (3.44).
σ l 4 =0 . 05 σ con =13 . 4MPa
Hence,
σ l = σ l 2 + σ l 4 =35 . 3+13 . 4=48 . 7MPa
f. Calculate prestress internal forces.
10 5 N
N p = σ con A p = 268
×
628 = 2 . 2
×
h
2 + a p
=2 . 2
600
2
+30 =7 . 26
10 6 ×
10 7 N
M p = N p
×
×
·
mm
g. Check the normal sectional strength of original beam according to eccentric compressive
members. External bending moment resisted by beam is
M = M max
M p = 194
72 . 6 = 121 . 4kN
·
m
10 5
e 0 = M
N
= 121 . 4
×
= 552 mm > 0 . 3 h 0
2 . 2
×
10 5
Thus,
e a =0 ,
i = e 0 + e a = 552 mm
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