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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174 <strong>The</strong> <strong>Design</strong> <strong>of</strong> <strong>Modern</strong> <strong>Steel</strong> <strong>Bridges</strong><br />
(2) For the support region:<br />
or<br />
or<br />
sa þ sa y<br />
r 2<br />
sa þ sa y<br />
r 2<br />
sE<br />
sE sa<br />
sE<br />
sE sa<br />
þ sb >j s 0 y<br />
>j ðs 0 y<br />
sa >j Rs 00<br />
y<br />
where Rs00 y is the strut strength <strong>of</strong> a strut made <strong>of</strong> material yield stress s00 y ,<br />
and s 00<br />
y ¼ s0y sb<br />
sbÞ<br />
ð6:14aÞ<br />
and R is the ratio <strong>of</strong> the strut strength to material yield stress <strong>of</strong> a strut made <strong>of</strong><br />
material yield stress s00 y .<br />
Alternatively<br />
sa<br />
Rs0 y<br />
þ sb<br />
s0 y<br />
>j 1 ð6:14bÞ<br />
Comparing equation (6.13) with this equation, it should be noted that ssu is<br />
less than Rs0 y ,asRis calculated for a strut <strong>of</strong> a lower effective material yield<br />
; this reflects the benefit <strong>of</strong> the applied bending moment not being<br />
magnified by the axial load over the support section.<br />
stress s 00<br />
y<br />
6.8 Effect <strong>of</strong> variation in the bending moment <strong>of</strong> a girder<br />
<strong>The</strong> applied axial stress in a longitudinal stiffener in a stiffened flange varies<br />
according to the shape <strong>of</strong> the bending moment diagram on the box or plate<br />
girder. Such a stiffener may be checked as a uniformly compressed strut with<br />
an equivalent applied axial load equal to that occurring at a distance 0.4L from<br />
the heavily stressed end. However, for a relatively slender strut, i.e. one with<br />
high ‘l/r’ ratio, subjected to a substantial variation in the axial loading at its<br />
two ends, such an approximate method may be too conservative. A more accurate<br />
method, in which the magnitude and location <strong>of</strong> the maximum bending<br />
moment is calculated for such a strut with initial out-<strong>of</strong>-straightness imperfection,<br />
is given in Reference [2].<br />
6.9 Transverse stiffeners in stiffened compression flanges<br />
In the design <strong>of</strong> longitudinal stiffeners, it has been assumed that the transverse<br />
stiffeners shall provide adequate support to the longitudinal stiffeners, so that