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Aluminium Design and Construction John Dwight

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where � 1 is again found from equation (7.5), or Figure 7.6, but now<br />

putting:<br />

(7.13)<br />

If an element has edge welds, a reduced thickness k z t is taken in each<br />

HAZ region in the same way as for uniform compression (i.e. the areas<br />

X in the figure are removed).<br />

7.3.4 Outst<strong>and</strong>s under strain gradient, general description<br />

Now we turn to outst<strong>and</strong>s, for which there are two possible cases of<br />

strain gradient (Figure 7.12):<br />

Case T peak compression is at the tip;<br />

Case R peak compression is at the root.<br />

In either case, the more heavily compressed edge is called edge 1 as<br />

before. And again we use � (=e 2 /e 1 ) to specify the degree of strain gradient.<br />

The buckling of an outst<strong>and</strong> is mainly governed by what happens at<br />

the tip. Therefore, case T is only slightly more favourable than uniform<br />

compression, since the effect of � is merely to decrease the stress in the<br />

relatively stable material close to the supported edge. But case R is<br />

clearly more favourable, because � now directly affects the tip stress<br />

which is what matters.<br />

The elastic critical stress � cr (occurring at edge 1) for a simply<br />

supported outst<strong>and</strong> under strain gradient may be found from the<br />

st<strong>and</strong>ard equation (7.2), taking a suitable value for K. Figure 7.13 shows<br />

how K varies with � for the two cases, the curves being plotted from<br />

the following empirical expressions which give a good approximation<br />

to the rigorous values:<br />

Case T K=0.41 for 1 > � > 0.5<br />

=0.50–0.18� for � < 0.5 (7.14a)<br />

Case R K=0.41+1.3(1-�) 4 (7.14b)<br />

Figure 7.12 Outst<strong>and</strong>s under strain-gradient. Cases T <strong>and</strong> R.<br />

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

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