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Aluminium Design and Construction John Dwight

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The parameter � depends purely on the geometry of the member.<br />

For ordinary column buckling (C) it is simply taken as effective length<br />

over radius of gyration (l/r). For the other buckling modes (T, LT) it is<br />

defined as follows:<br />

(5.8)<br />

where the ideal buckling stress p E is as given by st<strong>and</strong>ard elastic buckling<br />

theory. In other words, ? is taken in such a way that the ‘ideal’ curve<br />

(E) is always the same as the Euler curve, whatever buckling mode is<br />

considered.<br />

The stress p 1 at which the design curve intercepts the stress-axis would<br />

normally be put equal to the limiting stress p ° for the material (Section<br />

5.3). However, a reduced value must be taken if the cross-section has<br />

reduced strength, due to either local buckling or HAZ softening at welds.<br />

5.4.3 The design curves<br />

The exact shape of the curve for a given value of p 1 is controlled by two<br />

parameters: the plateau ratio � 1 /� ° <strong>and</strong> the imperfection factor c. In any<br />

buckling situation, these have to be adjusted to give the right shape of<br />

design curve. British St<strong>and</strong>ard BS.8118 rationalizes overall buckling by<br />

adopting six series of design curves, with parameter values as given in<br />

Table 5.5. These are based on research by Nethercot, Hong <strong>and</strong> others<br />

[15–17]. The curves are compared in Figure 5.7 on a non-dimensional<br />

plot. Actual design curves of p b against � appear in Chapters 8 <strong>and</strong> 9,<br />

covering a range of values of p 1.<br />

Table 5.5 Overall buckling curves—parameter values<br />

Notes. 1. This table relates to equations (5.6), (5.7).<br />

2. The resulting families of design curves are presented as follows: LT, Figure 8.22; C1, 2, 3,<br />

Figure 9.2; T1, 2 Figure 9.9.<br />

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

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