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Aluminium Design and Construction John Dwight

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hole. Alternatively, it might fail in mode B or C, involving a crooked<br />

failure path with diagonal portions in it. Similarly in Figure 9.1(b). In<br />

such cases, the effective area A e must be found for each possible failure<br />

path, <strong>and</strong> the lowest value taken. In considering a crooked failure path,<br />

A e can be estimated as follows:<br />

(9.1)<br />

where A=total transverse section area, n=number of holes on the failure<br />

path, <strong>and</strong> x, y=longitudinal <strong>and</strong> transverse hole pitch, as shown. The<br />

summation is made for every diagonal portion of the failure path between<br />

pairs of holes.<br />

9.3 LOCALIZED FAILURE OF THE CROSS-SECTION<br />

The calculated resistance Pc of an axially loaded member to localized<br />

failure at a specific cross-section is found thus:<br />

Pc =AePa (9.2)<br />

where pa =limiting stress for the material (Section 5.3), <strong>and</strong> Ae =effective<br />

section area.<br />

The use of the higher limiting stress pa , rather than the usual value<br />

po , reflects the view that some limited yielding at a localized crosssection<br />

need not be regarded as representing failure of the member.<br />

The effective area Ae should be based on the most unfavourable position<br />

along the member, making suitable allowance for HAZ softening, local<br />

buckling (compression only) or holes as necessary (Section 9.2). When<br />

considering the local buckling of a very slender outst<strong>and</strong>, it is permissible<br />

to take advantage of post-buckled strength for this check (Section 7.2.5).<br />

In the case of hybrid members containing different strength materials,<br />

Pc should be found by summing the resistances of the various parts,<br />

taking an appropriate pa for each.<br />

9.4 GENERAL YIELDING ALONG THE LENGTH<br />

This is the form of failure in which the member yields all along its length,<br />

or along a substantial part thereof. It need only be checked specifically<br />

for tension members, because the column buckling check automatically<br />

covers it in the case of struts. The calculated resistance Pc is obtained thus:<br />

Pc =AePo (9.3)<br />

where po =limiting stress for the material (Section 5.3), <strong>and</strong> Ae =effective<br />

section area.<br />

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

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