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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 />

The<br />

<strong>Steel</strong> Construction<br />

Institute<br />

Silwood Park, Ascot, Berks SL5 7QN<br />

Worked examples 639<br />

Subject Chapter ref.<br />

DESIGN OF CONTINUOUS<br />

COMPOSITE BEAM<br />

Design code Made by RML Sheet no.<br />

BS 5950: Parts 1 & 3 Checked by TCC<br />

Hence, the steel beam can support the loads during construction.<br />

Moment in mid-span of two-span beam after construction<br />

= 0.0703 ¥ (2.0 ¥ 3.0 + 0.6) ¥ 12 2 = 66.8 kNm<br />

Bending stress (elastic)<br />

Deflection of underside of beam after construction<br />

d o<br />

=<br />

=<br />

2. 1 ¥ ( 2. 0 ¥ 3. 0 + 0. 6) ¥ 12000<br />

384 ¥ 205 ¥ 10 ¥ 21600 ¥ 10<br />

= 16. 9 mm ( span/<br />

710)<br />

Composite condition – ultimate loading<br />

Factored loading on composite beam<br />

wu<br />

= [ ( 50 . + 10 . ) ¥ 16 . + ( 05 . + 20 . ) ¥ 14 . ]¥ 30 . + 06 . ¥ 14 .<br />

= 40. 1kN/<br />

m<br />

Design moment on composite beam<br />

Ratio of imposed load : dead load<br />

=<br />

66. 8 ¥ 10<br />

1058 ¥ 10<br />

6<br />

3<br />

=<br />

50 . + 10 .<br />

20 . + 05 . + 06 . 30 .<br />

63 N/ mm<br />

4<br />

3 4<br />

= 222 . > 2<br />

Therefore, the use of Table 21.2 is not permitted. However,<br />

calculate moments from pattern load cases as follows:<br />

2<br />

21<br />

3

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