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The Design of Modern Steel Bridges - TEDI

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wherefrom<br />

Ms ¼ 2<br />

3 PE P<br />

<strong>The</strong> net bending moment at mid-span <strong>of</strong> the longitudinal stiffeners is equal to<br />

P e1 þ<br />

d P2<br />

PE P<br />

2<br />

3<br />

dP 2<br />

dP 2<br />

P 2<br />

PE P ¼ P e1 1 þ 0:411<br />

PEfPE Pg<br />

since d ¼ 1.234 ðPe1=PEÞ.<br />

If a pin-ended strut, with Euler buckling load P E and subjected to an axial<br />

load P, had an initial imperfection e eff, then the maximum bending moment<br />

due to buckling would be<br />

P eeff<br />

PE<br />

PE P<br />

Hence, for checking the mid-span section <strong>of</strong> the longitudinal stiffener as a<br />

strut, we may assume the longitudinal stiffener to have an initial imperfection<br />

e eff, given by<br />

wherefrom<br />

Stiffened Compression Flanges <strong>of</strong> Box and Plate Girders 171<br />

P eeff<br />

PE<br />

P 2<br />

PE P ¼ P e1 1 þ 0:411<br />

PEfPE Pg<br />

eeff ¼ k1e1, when k1 ¼ 1<br />

P<br />

PE<br />

þ 0:411 P<br />

<strong>The</strong> direction <strong>of</strong> eeff is the same as the direction <strong>of</strong> e1, i.e. causing compression<br />

on flange plate.<br />

<strong>The</strong> support section <strong>of</strong> the longitudinal stiffener needs to be checked to<br />

ensure that yielding is not caused by the maximum fibre stress due to the axial<br />

load P and bending moment equal to<br />

P e1 Ms<br />

P 2<br />

¼ P e1 1 0:823<br />

PEfPE Pg<br />

¼ P e1 k2, when k2 ¼ 1 0:823<br />

PEfPE Pg<br />

For various ratios <strong>of</strong> P/PE, the values <strong>of</strong> k1 and k2 are tabulated below:<br />

PE<br />

P 2<br />

P/P E k 1 k 2<br />

0 1.0 1.0<br />

0.2 0.816 0.959<br />

0.4 0.666 0.781<br />

0.6 0.548 0.259<br />

0.8 0.463 1.634<br />

2

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