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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 />

Mmax<br />

Effect of moment gradient loading 519<br />

Fig. 18.8 Primary and secondary moments 1: (a) single curvature, (b) double curvature<br />

case, the point of maximum combined moment occurs near mid-height where<br />

secondary bending effects are greatest. On the other hand, for double-curvature<br />

bending the two individual maxima occur at quite different locations, and for the<br />

case illustrated, in which the secondary moments have deliberately been shown as<br />

small, the point of absolute maximum moment is at the top. Had larger secondary<br />

moments been shown, as is the case in Fig. 18.9, then the point of maximum moment<br />

moves down slightly but is still far from that of the single-curvature case.<br />

Theoretical and experimental studies of steel beam-columns constrained to<br />

respond in-plane and subject to different moment gradients, as represented by the<br />

factor of the ratio of the numerically smaller end moment to the numerically larger<br />

end moment (b), show clearly that, when all other parameters are held constant,<br />

failure loads tend to increase as b is varied from +1 (uniform single-curvature<br />

bending) to -1 (uniform double-curvature bending). Figure 18.10 illustrates the<br />

point in the form of a set of interaction curves. Clearly, if all beam-column designs<br />

were to be based upon the b =+1 case, safe but rather conservative designs would<br />

result.<br />

Figure 18.10 also shows how for high moments the curves for b π+1 tend to merge<br />

into a single line corresponding to the condition in which the more heavily stressed<br />

end of the member controls design. Reference to Figs 18.8 and 18.9 illustrates the<br />

point. The left-hand and lower parts of Fig. 18.10 correspond to situations in which<br />

Fig. 18.9 controls, while the right-hand and upper parts represent failure at one end.<br />

The two cases are sometimes referred to as ‘stability’ and ‘strength’ failure respectively.<br />

While this may offend the purists, for in both cases the limiting condition is<br />

one of exhausting the cross-sectional capacity, but at different locations within the<br />

member length, it does, nonetheless, serve to draw attention to the principal difference.<br />

Also shown in Fig. 18.10 is a line corresponding to the cross-sectional inter-<br />

(b)

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