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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 />

Os<br />

D<br />

elastic<br />

neutral axis<br />

stress p<br />

Be/ae<br />

(a) (b)<br />

equivalent<br />

steel area<br />

example, in continuous construction, or in beams where the ductility of the shear<br />

connection is not adequate.<br />

The important properties of the section are the section modulus and the second<br />

moment of area. First it is necessary to determine the centroid (elastic neutral axis)<br />

of the transformed section by expressing the area of concrete in steel units by dividing<br />

the concrete area within the effective breadth of the slab, Be, by an appropriate<br />

modular ratio (ratio of the elastic modulus of steel to concrete).<br />

In unpropped construction, account is taken of the stresses induced in the noncomposite<br />

section as well as the stresses in the composite section. In elastic analysis,<br />

therefore, the order of loading is important. For elastic conditions to hold,<br />

extreme fibre stresses are kept below their design values, and slip at the interface<br />

between the concrete and steel should be negligible.<br />

The elastic section properties are evaluated from the transformed section as in<br />

Fig. 21.6. The term ae is the modular ratio. The area of concrete within the profile<br />

depth is ignored (this is conservative where the decking troughs lie parallel to the<br />

beam). The concrete can usually be assumed to be uncracked under positive<br />

moment.<br />

The elastic neutral axis depth, xe, below the upper surface of the slab is determined<br />

from the formula:<br />

x<br />

e<br />

D D<br />

r D s - p Ê ˆ<br />

+ a e + Ds<br />

2 Ë 2 ¯<br />

=<br />

( 1 + a r)<br />

e<br />

Analysis of composite section 607<br />

Fig. 21.6 Elastic behaviour of composite beam. (a) Elastic stress distribution.<br />

(b) Transformed section<br />

(21.1)

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