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Aluminium Design and Construction John Dwight

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One difference from the treatment of localized failure is the use of<br />

the limiting stress p o , rather than the higher value p a . For most materials,<br />

p o is taken equal to the 0.2% proof stress.<br />

The other difference is that the effective area A e now relates to the<br />

general cross-section of the member along its length, ignoring any<br />

localized weakening at the end connections or where attachments are<br />

made. For a simple extruded member, therefore, A e may be taken equal<br />

to the gross area A. Holes need only be allowed for if there is a<br />

considerable number of these along the member. Likewise, a deduction<br />

for HAZ softening is only necessary when the member contains welding<br />

on a significant proportion of its length.<br />

9.5 COLUMN BUCKLING<br />

9.5.1 Basic calculation<br />

Column (or flexural) buckling of a strut is the well-known mode of<br />

failure in which the central part of the member ‘pops out sideways’.<br />

The calculated resistance Pc is given by:<br />

Pc =Apb (9.4)<br />

where pb =column buckling stress, <strong>and</strong> A=gross section area.<br />

This equation should be employed to check for possible buckling<br />

about each principal axis of the section in turn. For a built-up member,<br />

consisting of two or more components connected together at intervals<br />

along the length, buckling should be checked not only for the section<br />

as a whole (about either axis), but also for the individual components<br />

between points of interconnection. For back-to-back angles, such that<br />

the buckling length is the same about both principal axes, accepted<br />

practice is to interconnect at third-points.<br />

9.5.2 Column buckling stress<br />

The buckling stress pb depends on the overall slenderness �. It may be<br />

read from one of the families of curves (C1, C2, C3) given in Figure 9.2,<br />

the derivation of which was explained in Chapter 5. Alternatively, it<br />

may be calculated from the relevant formula (Section 5.4.2).<br />

The appropriate family, which need not necessarily be the same for<br />

both axes of buckling, is chosen as follows:<br />

The terms ‘symmetric’ <strong>and</strong> ‘asymmetric’ refer to symmetry about the<br />

axis of buckling. A severely asymmetric section is one for which y 1<br />

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

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