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Aluminium Design and Construction John Dwight

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compression flange. This is valid when the flange, although held in<br />

position at these points, is free in terms of plan-view rotation. It is<br />

permissible to reduce the value of l when the flange is restrained against<br />

such rotation, although by just how much is a matter of some guesswork.<br />

British St<strong>and</strong>ard BS.8118 permits l=0.85L for the case of ‘partial’ rotational<br />

restraint <strong>and</strong> 0.7L for ‘full’ restraint.<br />

There are some situations where l should be taken greater than the<br />

bay length L, namely as follows:<br />

(a) Destabilizing loads<br />

For a bay that carries intermediate loading (Section 8.7.3(b)) it is important<br />

to consider at what height this loading acts. A destabilizing load is one<br />

which effectively acts at a point X located higher than the shear centre<br />

S (Figure 8.25). As the beam buckles, taking the load with it, the resulting<br />

moment about S aggravates the tendency to twist. Such a load therefore<br />

represents a more adverse condition than that of a non-destabilizing load<br />

(acting at, or below S), <strong>and</strong> must be allowed for by increasing l. Just how<br />

much depends on h (the height of X above S), a reasonable value being:<br />

(8.37)<br />

where D is the overall depth of section. When the load is applied at top<br />

flange level in a symmetrical I-beam (h=D/2), this gives l=1.2L. Equation<br />

(8.37) assumes that the compression flange is unrestrained against planview<br />

rotation at the ends of the bay. When restraint against such rotation<br />

is provided, BS.8118 permits effective lengths of L <strong>and</strong> 0.85L for the<br />

case h=D/2, corresponding to ‘partial’ <strong>and</strong> ‘full’ restraint respectively.<br />

(b) Beams without end-posts<br />

It is desirable to stabilize the top flange of a beam against out-of-plane<br />

movement over the reaction points, by fitting a properly designed end-<br />

Figure 8.25 Lateral-torsional buckling, destabilizing load.<br />

Copyright 1999 by Taylor & Francis Group. All Rights Reserved.

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