EUROCODE 2 WORKED EXAMPLES - Federbeton
EUROCODE 2 WORKED EXAMPLES - Federbeton
EUROCODE 2 WORKED EXAMPLES - Federbeton
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EC2 – worked examples 6-55<br />
6.15.4 Verification at Serviceability Limit State<br />
The verification at serviceability limit state is relative to the following conditions:<br />
− stress limitation at tensioning;<br />
− stress limitation at service;<br />
− crack widths;<br />
− deformation.<br />
Table of Content<br />
Verification at tensioning<br />
At time of tensioning, no tensile stress should be present in the extreme fibres of the slab<br />
and the maximum compressive stress should not exceed the limit value of 0.6 × fck = 21<br />
MPa. For the sake of simplicity, one reports the verification related to the four elements<br />
showed in fig ii, as subjected to the higher stress level.<br />
The external actions are calculated adopting the rare combination with only the load steps<br />
1 and 2. From FEM analysis, the value of n22 , m22 , n33 , m33 , n23 , m23 are evaluated so that<br />
it results:<br />
n22 6 m 22<br />
σyt , = σ22,<br />
t=<br />
− 2<br />
h h<br />
;<br />
n22 6 m 22<br />
σyb , = σ22,<br />
b=<br />
+ 2<br />
h h<br />
n33 6 m 33<br />
σxt , = σ33,<br />
t = − 2<br />
h h<br />
;<br />
n33 6 m 33<br />
σxb , = σ33,<br />
b=<br />
+ 2<br />
h h<br />
n23 6 m 23<br />
σxy, t = σ23,<br />
t = − 2<br />
h h<br />
; σxy, b = σ23,<br />
b<br />
n23 6 m 23<br />
= + 2<br />
h h<br />
where the subscripts t and b indicate respectively top and bottom fibre. The angles of<br />
principal directions (for which is σxy = 0) are:<br />
θ<br />
1<br />
=<br />
1<br />
2<br />
⎛ 2 σ23<br />
⎜<br />
⎝ σ − σ<br />
⎞<br />
atan ⎟ ; θ2 = θ1 + 90°<br />
22 33 ⎠<br />
and the principal stresses result:<br />
2<br />
2<br />
σ = σ cos ( θ ) + σ sin ( θ ) + σ sin(<br />
2θ<br />
)<br />
1,/ t b 22,/<br />
t b 1 33,/<br />
t b 1 23,/ t b<br />
1<br />
2<br />
2<br />
σ = σ cos ( θ ) + σ sin ( θ ) + σ sin(<br />
2θ<br />
)<br />
2,/ t b 22,/<br />
t b 2 33,/<br />
t b 2 23,/ t b<br />
2<br />
Referring to the elements marked in Fig.6.32 one obtains:<br />
Table 6.7<br />
Elem. h n 22 n 33 n 23 m 22 m 33 m 23<br />
[m] [kN/m] [kN/m] [kN/m] [kNm/m] [kNm/m] [kNm/m]<br />
648 1.5 -3091 -13159 6 -225 -2176 0<br />
93 0.963 -7806 -8526 75 743 456 -51<br />
320 1.5 -3516 -10418 1 -45 -812 0<br />
589 1.5 -4280 -10007 -67 653 1945 20<br />
Table 6.8