The Design of Modern Steel Bridges - TEDI
The Design of Modern Steel Bridges - TEDI
The Design of Modern Steel Bridges - TEDI
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Rolled Beam and Plate Girder <strong>Design</strong> 125<br />
Figure 5.18 Buckling behaviour <strong>of</strong> plates with initial out-<strong>of</strong>-plane deviations.<br />
(a) Ideally flat plate; (b) plate with initial out-<strong>of</strong>-plane deviations.<br />
quantitative effects <strong>of</strong> initial out-<strong>of</strong>-plane deviations depend on:<br />
(1) the magnitude <strong>of</strong> the deviations<br />
(2) the pattern <strong>of</strong> the deviations<br />
(3) the type <strong>of</strong> the applied stresses on the plate<br />
(4) the in-plane and out-<strong>of</strong>-plane edge conditions <strong>of</strong> the plate<br />
(5) the slenderness (i.e. the width-to-thickness ratio) <strong>of</strong> the plate and to a<br />
lesser extent its aspect ratio (i.e. the ratio <strong>of</strong> length to width).<br />
Obviously, the larger the deviations, the worse are the effects. Initial<br />
deviations in the pattern <strong>of</strong> the elastic critical buckling mode <strong>of</strong> the plate have<br />
the worst effects. For example, in a plate with an aspect ratio <strong>of</strong> 3, subjected to<br />
compression on the shorter edges, the worst pattern <strong>of</strong> initial deviations will be<br />
the one with one sine wave across the width and three sine waves in the form<br />
<strong>of</strong> ripples along the length. Plates subjected to in-plane compression along one<br />
or both directions are most affected by initial deviations; plates in shear are<br />
least affected. In-plane restraints on the edges reduce the effects <strong>of</strong> initial<br />
deviations. But the beneficial effects <strong>of</strong> out-<strong>of</strong>-plane edge fixities (i.e. clamped<br />
against rotation) are less pronounced in the case <strong>of</strong> initially curved plates than<br />
the improvement in the elastic critical buckling stress <strong>of</strong> a perfectly flat plate.<br />
Plates with low slenderness, e.g. the width–thickness ratio less than, say, 20 in<br />
the case <strong>of</strong> longitudinal in-plane compression or 50 in the case <strong>of</strong> in-plane<br />
bending or shear, are able to reach their squash loading, i.e. applied stress can<br />
be as high as the yield stress, in spite <strong>of</strong> any out-<strong>of</strong>-plane deviations. A more