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Steel Designers Manual - TheBestFriend.org

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This material is copyright - all rights reserved. Reproduced under licence from The <strong>Steel</strong> Construction Institute on 12/2/2007<br />

To buy a hardcopy version of this document call 01344 872775 or go to http://shop.steelbiz.<strong>org</strong>/<br />

<strong>Steel</strong> <strong>Designers</strong>' <strong>Manual</strong> - 6th Edition (2003)<br />

378 Local buckling and cross-section classification<br />

stress system to which the plate element under consideration is subjected. If, in addition<br />

to the moment M, an axial compression F is applied to the member, then for<br />

elastic behaviour the pattern of stress in the web is of the form shown in Fig. 13.6(a).<br />

The values of s1 and s2 are dependent on the ratio F/M with s2 approaching sy, if<br />

F is large and M is small. In this case it may be expected that the appropriate b<br />

limits will be somewhere between the values for pure compression and pure<br />

bending, approaching the former if s2 ª sy, and the latter if s2 ª-s2. A qualitative<br />

indication of this is given in Fig. 13.7, which shows Mu as a function of d /t for three<br />

different s2/s1 ratios corresponding to pure compression, s2 = 0 and pure bending.<br />

If the value of d /t is sufficiently small that the web may be classified as compact or<br />

plastic, then the stress distribution will adopt the alternative plastic arrangement of<br />

Fig. 13.6(b).<br />

For a plate element in a member which is subject to pure compression the loadcarrying<br />

capacity is not affected by the degree of deformation since the scope for a<br />

change in strain distribution as the member passes from a wholly elastic to a partially<br />

plastic state, as illustrated in Fig. 13.4 for pure bending, does not exist.<br />

The plastic and compact classifications do not therefore have any meaning; the only<br />

decision required is whether or not the member is slender, and specific values are<br />

only required for b3.<br />

stress due to compression F<br />

stress due to moment M<br />

stress due to compression F<br />

stress due to moment M<br />

(a)<br />

(b)<br />

a2 =<br />

a1 =<br />

H<br />

Fig. 13.6 Stress distributions in webs of symmetrical sections subject to combined bending<br />

and compression. (a) Semi-compact, elastic stress distribution. (b) Plastic or<br />

compact, plastic stress distribution

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