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The Design of Modern Steel Bridges - TEDI

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Figure 5.6 Buckling <strong>of</strong> plates in compression.<br />

and<br />

where<br />

T ¼ p2 bF<br />

8a d2 m 2<br />

D ¼ flexural rigidity <strong>of</strong> the plate, equal to Et 3 /12(1 m 2 )<br />

t ¼ thickness <strong>of</strong> the plate<br />

E ¼ Young’s modulus<br />

m ¼ Poisson’s ratio.<br />

<strong>The</strong> critical value <strong>of</strong> F is thus given by<br />

Fcr ¼ sx crt ¼ p2 a 2 D<br />

m 2<br />

Rolled Beam and Plate Girder <strong>Design</strong> 111<br />

m2 n2<br />

þ<br />

a2 b2 2<br />

ð5:18Þ<br />

Another method for obtaining the critical value <strong>of</strong> F is to consider the<br />

St Venant differential equation <strong>of</strong> equilibrium <strong>of</strong> the plate given by<br />

q 4 o<br />

qx4 þ 2q4o qx2qy2 þ q4o F q<br />

¼<br />

qy4 D<br />

2 o<br />

qx2 ð5:19Þ<br />

<strong>The</strong> deflected shape given by equation (5.17) is one solution <strong>of</strong> this<br />

differential equation. Substitution <strong>of</strong> equation (5.17) into equation (5.19) leads<br />

directly to the critical value <strong>of</strong> F given by equation (5.18). <strong>The</strong> limitation <strong>of</strong><br />

this method is that closed-form expressions for the deflected shape <strong>of</strong> the plate<br />

are found only for a few types <strong>of</strong> applied stress patterns.<br />

<strong>The</strong> St Venant differential equation (5.19) for a plate in compression is<br />

equivalent to the following well-known differential equation <strong>of</strong> equilibrium <strong>of</strong><br />

a strut<br />

EI d4o dx4 ¼ P d2o dx2

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