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The Design of Modern Steel Bridges - TEDI

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Chapter 6<br />

Stiffened Compression Flanges <strong>of</strong><br />

Box and Plate Girders<br />

6.1 General features<br />

Stiffened compression flanges <strong>of</strong> box and plate girders consist <strong>of</strong> a flange plate<br />

stiffened longitudinally by either open (i.e. flat, bulb-flat, angle or tee) or closed<br />

(i.e. trough, vee) types <strong>of</strong> stiffeners spanning between transverse stiffeners<br />

which are supported by the girder webs or web stiffeners. Such compression<br />

flanges may be subjected to the following stresses:<br />

(1) Longitudinal stresses due to the bending moment (and axial force) on the<br />

main girder; these stresses may vary across the width <strong>of</strong> the flange due to<br />

shear lag, and along the length due to the variation in the bending moment;<br />

additional longitudinal stresses may be caused by restrained warping <strong>of</strong><br />

a box girder.<br />

(2) In-plane shear stresses in the flange plate due to any shear force on the<br />

girder and/or torsion in the case <strong>of</strong> a box girder.<br />

(3) Flexural stresses in the flange stiffeners due to any loading applied locally<br />

on the flange, e.g. wheel loading on a bridge deck.<br />

(4) In-plane transverse stresses in the flange plate due to bending <strong>of</strong> transverse<br />

flange stiffeners, and in the case <strong>of</strong> box girders due to distortion <strong>of</strong><br />

the box cross-section and in the vicinity <strong>of</strong> internal diaphragms over box<br />

girder supports.<br />

Typical stiffened flange details are shown in Fig. 6.1.<br />

A stiffened compression flange comprises several parallel struts each continuous<br />

over and supported at many transverse stiffener locations; it can be<br />

idealised as a series <strong>of</strong> pin-ended struts supported at transverse stiffeners. Apart<br />

from the complex stress field mentioned above, the following geometrical<br />

complexities need investigation:<br />

(1) Longitudinal continuity over transverse stiffeners.<br />

(2) Transverse continuity between parallel stiffeners.<br />

(3) Four separate buckling modes, namely local buckling <strong>of</strong> flange plating<br />

between longitudinal stiffeners, local buckling <strong>of</strong> stiffener components,<br />

159

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