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Aluminium Design and Construction John Dwight

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The determination of l involves a considerable degree of judgment<br />

(i.e. guesswork) by the designer—as in steel. It is found as follows:<br />

l=KL (9.7)<br />

where L=unsupported buckling length, appropriate to the direction of<br />

buckling. K may be estimated with the help of Figure 9.3.<br />

9.5.4 Column buckling of struts containing very slender outst<strong>and</strong>s<br />

For a column containing very slender outst<strong>and</strong>s (Section 7.2.5), the designer<br />

must know whether it is permissible to assume an effective section that<br />

takes account of the post-buckled strength of these. There are two possible<br />

procedures:<br />

1. Method A is effectively the same as that given in BS.8118. p 1 (expression<br />

(9.5)) is based on an effective section that ignores post-buckled strength<br />

in such elements, using expression (7.8) to obtain � o . But in finding<br />

�, it bases r on the gross section. It is further assumed that the member<br />

is under pure compression (no bending) when the applied load aligns<br />

with the centroid of the gross section.<br />

2. Method B employs an effective section which takes advantage of<br />

post-buckled strength in very slender elements, with � o found from<br />

expression (7.7). This effective section is employed for obtaining both<br />

A e <strong>and</strong> r. The member now counts as being in pure compression<br />

when the applied load acts through the centroid of the effective section.<br />

Method B thus employs a higher buckling curve (higher p 1 ), but enters<br />

it at a higher �. Method A is found to be the more favourable for the<br />

majority of cases, but method B becomes advantageous if the member<br />

is short (low �).<br />

9.6 TORSIONAL BUCKLING<br />

9.6.1 General description<br />

There are three fundamental modes of overall buckling for an axially<br />

loaded strut [27]:<br />

1. column (i.e. flexural) buckling about the minor principal axis;<br />

2. column buckling about the major axis;<br />

3. pure torsional buckling about the shear centre S.<br />

Figure 9.4 shows the mid-length deflection corresponding to each of<br />

these for a typical member. The mode with the lowest failure load is the<br />

one that the member would choose.<br />

Torsion needs to be considered for open (non-hollow) sections. Because<br />

the torsional stiffness of these is roughly proportional to thickness cubed,<br />

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

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