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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 />

908 Floors and orthotropic decks<br />

B = breadth of plate (mm)<br />

t = thickness of plate (mm)<br />

k =<br />

py = yield stress of plate (N/mm2 )<br />

E = Young’s modulus 205 ¥ 103 (N/mm2 4<br />

Ê L ˆ<br />

Á ˜<br />

Ë 4 4<br />

L + B ¯<br />

)<br />

gf = load factor<br />

This formula, which is the basis of the first two load tables in the Appendix<br />

Floor plate design tables, assumes that there is no resistance to uplift in plate<br />

corners. Where such resistance is provided, higher design strength may be<br />

obtained by using References 1 or 2.<br />

(2) Centre point loads (concentrated over a small circle of radius r)<br />

The design may be made using formulae developed by Roark. 1<br />

NB There is a small amount of uplift (negative load) on the corners of the plate<br />

when design is made using the following formula. Fastening at each corner must<br />

be able to resist an uplift of 6% of the centre point load.<br />

pt<br />

w<br />

B<br />

m r<br />

d<br />

WB<br />

2 067 . p y<br />

=<br />

Ê 1 ˆ 2<br />

1 + ln + b<br />

Ë ¯ p<br />

2<br />

a<br />

= 3<br />

g Et<br />

f<br />

where W = concentrated load (ultimate) (N)<br />

d = maximum deflection (mm), occurring at serviceability<br />

L = length of plate (mm) (L > B)<br />

B = breadth of plate (mm)<br />

t = thickness of plate (mm)<br />

py = yield stress of plate (N/mm2 )<br />

E = Young’s modulus 205 ¥ 103 (N/mm2 )<br />

1<br />

= Poisson’s ratio (m = 3)<br />

m<br />

r = radius of contact for a load concentrated on a small area (mm)<br />

ln = natural logarithm of (2B/pr)<br />

g f = load factor<br />

Table 30.4 Values of b and a for centre point loads on simply supported plates<br />

L/B 1.0 1.2 1.4 1.6 1.8 2.0 •<br />

b 0.435 0.650 0.789 0.875 0.972 0.958 1.0<br />

a 0.1267 0.1478 0.1621 0.1715 0.1770 0.1805 0.1851

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