1.2.1 The following
symbols and definitions are applicable to this Chapter, unless otherwise
stated:
σo
|
= |
minimum
yield stress or 0,5 per cent proof stress of the material, in N/mm2 and
is not to be taken greater than 0,7σT
|
where
σT
|
= |
ultimate
tensile strength of the material, in N/mm2
|
1.2.2 The scantlings
in aluminium alloy are to be obtained by multiplying the scantlings
in mild steel, determined from this Chapter, by the following factors:
-
Plating thickness
factor = k
ta
- where
k
ta
|
= |
|
-
Section modulus and
cross sectional area factor, k
aa
- where
k
aa
|
= |
235/σya or 1,36, whichever is the greater
|
σya
|
= |
specified
minimum yield stress or 0,2 per cent proof stress of aluminium alloy
in the welded condition, in N/mm2
|