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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 />

30.1.2 Design of plates fixed on four edges<br />

<strong>Steel</strong> plate floors 909<br />

The plates must be secured by continuous bolting or welding, which will achieve the<br />

fixed condition and prevent uplift which would otherwise occur at the plate corners.<br />

The bolt or weld detail should be such as to develop the strength in bending of the<br />

chosen plate thickness.<br />

(1) Uniformly distributed loading<br />

The design may be made using Pounder’s plate theory.<br />

pt<br />

w<br />

kB k k<br />

d m<br />

2<br />

=<br />

È<br />

˘<br />

1+ ( - )+ ( - )<br />

ÎÍ<br />

˚˙<br />

- kwB Ê<br />

ˆ<br />

= ¥ + ( -k)+<br />

( -k)<br />

m Et Ë<br />

¯<br />

11<br />

35 1<br />

79<br />

141 1<br />

1<br />

47<br />

1<br />

32 210 1<br />

200<br />

517 1<br />

2<br />

y<br />

2<br />

2<br />

2<br />

4<br />

2<br />

2<br />

3 g<br />

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

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

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

k =<br />

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

w = uniformly distributed load on plate (ultimate) (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 />

1<br />

= Poisson’s ratio (m = 3)<br />

m<br />

f<br />

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

gf = load factor<br />

This formula is the basis of the third load table in the Appendix Floor plate<br />

design tables.<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 />

2 067 . ppt<br />

y<br />

W =<br />

Ê 1 ˆ 2B<br />

1 + ln + b1<br />

Ë m¯<br />

pr<br />

whichever is the lesser, where<br />

or<br />

2 pt y<br />

b2<br />

2 aWB<br />

d =<br />

3<br />

g fEt<br />

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)

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