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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 />

336 Beam analysis<br />

P=o -t-—<br />

tlength<br />

MAt f<br />

L<br />

(a)<br />

H<br />

MAf<br />

a1 b1<br />

C<br />

(b)<br />

(c)<br />

Fig. 10.9 Plastic failure of a fixed-end beam<br />

MB<br />

the simply-supported sagging parabolic moment diagram ACB (peak value of<br />

wL 2 /8) on the uniform moment diagram Aa 1b 1B due to the end hogging moments<br />

M A and M B. From the moment–curvature relation applied over the full length of<br />

the beam, it is readily deduced, by any one of a number of standard methods, that<br />

the rotations of the end sections at A (q A clockwise) and at B (q B anti-clockwise)<br />

and the central deflection D C are given by<br />

q A<br />

q B<br />

D C<br />

3 wL MAL MBL = - -<br />

24EI 3EI 6EI<br />

3 wL MAL MBL = - -<br />

24EI 6EI 3EI<br />

5 wL M L M L<br />

= - -<br />

384 EI 16EI 16EI<br />

4 2 2<br />

A B<br />

P=o<br />

(10.4)<br />

(10.5)<br />

(10.6)<br />

The compatibility conditions that now have to be satisfied are the directional<br />

restraint of the end sections of the beam, i.e. qA = q B = 0, giving the well-known

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