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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

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