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The Design of Modern Steel Bridges - TEDI

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110 <strong>The</strong> <strong>Design</strong> <strong>of</strong> <strong>Modern</strong> <strong>Steel</strong> <strong>Bridges</strong><br />

Figure 5.5 Buckling behaviour <strong>of</strong> thin plates.<br />

5.4.1 Elastic critical buckling <strong>of</strong> plates<br />

5.4.1.1 Plates under uniaxial compression<br />

Consider an ideally flat residual-stress-free rectangular plate simply supported<br />

along its four edges and subjected to a compressive load F per unit length<br />

uniformly distributed along two opposite edges, as shown in Fig. 5.6. At a<br />

certain value <strong>of</strong> F the flat form <strong>of</strong> equilibrium becomes unstable and the plate<br />

buckles; this instability is due to the fact that the energy <strong>of</strong> the plate in a buckled<br />

form is equal to or less than that if it remained flat under the same edge forces.<br />

<strong>The</strong> critical value <strong>of</strong> F may be determined by considering a deflected shape <strong>of</strong><br />

the plate consistent with its boundary conditions. One such shape is given by<br />

o ¼ d sin mpx npy<br />

sin ð5:17Þ<br />

a b<br />

where o is the out-<strong>of</strong>-plane deflection at point (x, y). In this method, the<br />

bending energy U <strong>of</strong> the plate is equated with the work done T by the applied<br />

forces due to the shortening <strong>of</strong> the plate. It can be shown[5] that<br />

U ¼ p4 abD<br />

8<br />

d 2 m2 n2<br />

þ<br />

a2 b2 2

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