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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108 <strong>The</strong> <strong>Design</strong> <strong>of</strong> <strong>Modern</strong> <strong>Steel</strong> <strong>Bridges</strong><br />
For minimum value <strong>of</strong> P, dP/dm ¼ 0. This leads to<br />
m ¼ L 1=4<br />
½k=EIcŠ<br />
p<br />
pffiffiffiffiffiffiffiffiffi<br />
Pcr ¼ 2 EIck<br />
L<br />
1=4<br />
¼ critical half-wave-length ¼ p½EIc=kŠ<br />
m<br />
<strong>The</strong> effective length <strong>of</strong> an equivalent strut with Euler buckling load equal to<br />
the above value <strong>of</strong> Pcr will be given by<br />
leading to<br />
p 2 EIc<br />
l 2 eff<br />
pffiffiffiffiffiffiffiffiffi<br />
¼ 2 EIck<br />
leff ¼ p pffiffiffi ½EIc=kŠ<br />
2<br />
1=4<br />
<strong>The</strong> above results are theoretically valid for a beam under constant bending<br />
moment, but may be conveniently and conservatively used for beams subjected<br />
to varying bending moments, using the maximum compressive flange force for<br />
comparing with the P cr-value obtained from above.<br />
If the lateral restraints are spaced at s and their flexibility, i.e. deflection due<br />
to unit force at the restraint, is d, then k s ¼ 1/d, and<br />
leff ¼ p pffiffiffi ½EIcsdŠ<br />
2<br />
1=4<br />
<strong>The</strong> lateral restraints to the compression flange may be in the form <strong>of</strong> torsional<br />
restraints, such that a is the rotation <strong>of</strong> the restraint due to unit torque applied<br />
at that restraint. <strong>The</strong>n the displacement <strong>of</strong> one flange with respect to the other<br />
due to unit forces applied at flange levels <strong>of</strong> each torsional restraint will be d 2 a,<br />
when d is the depth <strong>of</strong> the girder between the centroids <strong>of</strong> its flanges. <strong>The</strong><br />
effective length <strong>of</strong> the compressive flange can then be obtained by replacing<br />
d by d 2 a in the previous expression, i.e.<br />
leff ¼ p pffiffi ½EIcsd<br />
2<br />
2 aŠ 1=4<br />
5.3.4 Compression flange with full lateral restraints at ends and one restraint <strong>of</strong><br />
limited rigidity at midpoint<br />
Assume a single sinusoidal half-wave <strong>of</strong> buckling, i.e.<br />
y ¼ a sinðpx=LÞ<br />
<strong>The</strong> strain energy <strong>of</strong> bending <strong>of</strong> the flange ¼ p 4 EIca 2 =4L 3