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4.2 - VSL

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The condition to be fulfilled at failure here is:<br />

(g+q) u ≥ γ<br />

(3.2.)<br />

g+q<br />

where γ=γf . γm The ultimate design loading (g+q)u divided by<br />

the service loading (g+q) must correspond to a<br />

value at least equal to the safety factor y.<br />

The simplest way of determining the ultimate<br />

design loading (g+q)u is by the kinematic<br />

method, which provides an upper boundary<br />

for the ultimate load. The mechanism to be<br />

chosen is that which leads to the lowest load.<br />

Fig. 21 and 22 illustrate mechanisms for an<br />

internal span. In flat slabs with usual column<br />

dimensions (ξ>0.06) the ultimate load can be<br />

determined to a high degree of accuracy by<br />

the line mechanisms � or � (yield lines 1-1 or<br />

2-2 respectively). Contrary to Fig. 21, the<br />

negative yield line is assumed for purposes of<br />

approximation to coincide with the line<br />

connecting the column axes (Fig. 23),<br />

although this is kinematically incompatible. In<br />

the region of the column, a portion of the<br />

internal work is thereby neglected, which leads<br />

to the result that the load calculated in this way<br />

lies very close to the ultimate load or below it.<br />

On the assumption of uniformly distributed top<br />

and bottom reinforcement, the ultimate design<br />

loads of the various mechanisms are<br />

compared in Fig. 24.<br />

In post-tensioned flat slabs, the prestressing<br />

and the ordinary reinforcement are not<br />

uniformly distributed. In the approximation,<br />

however, both are assumed as uniformly<br />

distributed over the width I1 /2 + 12 /2 (Fig. 25).<br />

The ultimate load calculation can then be<br />

carried out for a strip of unit width 1. The actual<br />

distribution of the tendons will be in<br />

accordance with chapter 5.1. The top layer<br />

ordinary reinforcement should be<br />

concentrated over the columns in accordance<br />

with Fig. 35.<br />

The load corresponding to the individual<br />

mechanisms can be obtained by the principle<br />

of virtual work. This principle states that, for a<br />

virtual displacement, the sum of the work We<br />

performed by the applied forces and of the<br />

dissipation work W, performed by the internal<br />

forces must be equal to zero.<br />

We+Wi,=0 (3.3.)<br />

If this principle is applied to mechanism �<br />

(yield lines 1-1; Fig. 23), then for a strip of<br />

width I1 /2 + 12 /2 the ultimate design load (g+q)<br />

u is obtained.<br />

internal span:<br />

Figure 21: Line mecanisms<br />

Figure 23: Line mecanisms (proposed<br />

approximation)<br />

Figure 22: Fan mecanisms<br />

Figure 24: Ultimate design load of the<br />

various mecanisms as function of column<br />

diemnsions<br />

Figure 25: Assumed distribution of the<br />

reinforcement in the approximation<br />

method<br />

(g+q)u= 8 . mu . (1+ λ) (3.7.)<br />

2<br />

l 2<br />

Edge span with cantilever:<br />

7

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