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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 />

In the analysis the member forces and moments due to joint fixity should be<br />

calculated and superimposed on the global member forces. For trusses in buildings<br />

the secondary effects due to joint fixity may normally be ignored provided the<br />

slenderness, in the plane of the truss, is greater than 50 for the chord elements<br />

and 100 for most of the web members. If this condition is satisfied the<br />

members are assumed to be pin jointed in the analysis. Secondary effects due to<br />

axial deformations are usually ignored in building trusses. Local effects due to joint<br />

eccentricities and where loads are not applied at nodes should be taken into<br />

account.<br />

For bridge trusses to BS 5400: Part 3: 2000, the effects of joint rigidity are required<br />

to be taken into account. Secondary stresses due to axial deformations may be<br />

ignored at the ultimate limit state but should be considered at the serviceability limit<br />

state and for fatigue checks. As for building trusses, the local effects due to joint<br />

eccentricities and cases where loads are not applied at nodes must be considered in<br />

bridge trusses.<br />

19.6.2 Effective length of compression members<br />

Detailed design considerations for elements 553<br />

For building trusses the fixity of the joints and the rigidity of adjacent members<br />

may be taken into account for the purpose of calculating the effective length of<br />

compression members. The designer should be careful to ensure that the critical<br />

slenderness is identified. For chords, out-of-plane unrestrained lengths do not necessarily<br />

relate to the truss nodes, and effective length factors are usually unity; in-plane<br />

effective length factors may be demonstrated to be less than unity if the restraining<br />

actions of tension members and non-critical compression members are mobilized<br />

at the ends of the member. Single angle elements, for both the webs and chord,<br />

have minimum radii of gyration that do not lie either in, or normal to, the plane of<br />

the truss.<br />

For compression members in bridge trusses the effective lengths may either be<br />

obtained from Table 11 of BS 5400: Part 3: 1982 or be determined by an elastic<br />

critical buckling analysis of the truss.<br />

In the case of simply supported underslung trusses the top compression chord<br />

will be effectively restrained laterally throughout its length provided the connection<br />

between the chord and the deck is capable of resisting a uniformly distributed<br />

lateral force of 2.5% of the maximum force in the chord. The effective length in<br />

such a case is taken as zero where friction provides the restraint, or as equal to the<br />

spacing of discrete connections where these are provided.<br />

The economic advantages of underslung trusses over through or semi-through<br />

trusses is obvious in this respect, due to the dual function of the deck structure.<br />

In the case of unbraced compression chords, that is, chords with no lateral<br />

restraints, the provision of U-frames is necessary. The effective length of the compression<br />

chord is a function of the stiffness of the chord and the spacing and

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