OS-C501
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Offshore Standard DNV-<strong>OS</strong>-<strong>C501</strong>, November 2013<br />
Sec.4 Materials - laminates – Page 45<br />
Table 4-3 Values of k m<br />
Target reliability level, Sec.2 [3.5]<br />
Number of<br />
test results<br />
A B C D<br />
Safety class low and Safety class normal<br />
brittle failure and brittle failure<br />
Safety class high and<br />
brittle failure<br />
or<br />
or<br />
Safety class low and<br />
ductile failure<br />
Safety class normal<br />
and ductile failure<br />
Safety class high and<br />
ductile failure<br />
3 3.0 3.7 5.0 7.4<br />
4 2.7 3.2 4.0 5.3<br />
5 2.5 2.9 3.5 4.4<br />
6 2.4 2.8 3.3 4.0<br />
7 2.4 2.8 3.1 3.7<br />
8 2.3 2.6 3.0 3.5<br />
10 2.3 2.5 2.8 3.2<br />
15 2.2 2.3 2.6 2.9<br />
Infinite 1.96 1.96 1.96 1.96<br />
[2.6] and Table 4-4 shall be used instead of Table 4-3 when the conditions specified in [2.6] apply. [2.7] and<br />
Table 4-5 may be used as an alternative to Table 4-3 when the conditions specified in [2.7] apply.<br />
The background for the specification of the k m - values in Table 4-3, Table 4-4 and Table 4-5 is given in App.J.<br />
2.6 k m for structures or components subjected loads with known maximum load effect.<br />
2.6.1 For structures or components subjected to loads with known maximum load effect k m shall be taken as<br />
specified in Table 4-4. Table 4-3 shall not be used. [2.7] and Table 4-5 may be used as an alternative to Table<br />
4-4 when the conditions specified in [2.7] apply.<br />
Table 4-4 Values of k m for loads with known maximum load effect<br />
Number of<br />
test results<br />
Target reliability level, Sec.2 [3.5]<br />
A B C D<br />
Safety class low and Safety class normal<br />
Safety class high and<br />
brittle failure and brittle failure<br />
brittle failure<br />
or<br />
or<br />
Safety class low and Safety class normal Safety class high and<br />
ductile failure and ductile failure ductile failure<br />
3 4.2 5.8 10.4 16.1<br />
4 3.5 4.4 6.6 9.0<br />
5 3.1 3.8 5.1 6.5<br />
6 2.9 3.5 4.5 5.5<br />
7 2.8 3.3 4.1 4.8<br />
8 2.7 3.1 3.8 4.4<br />
10 2.6 2.9 3.5 4.0<br />
15 2.4 2.7 3.1 3.4<br />
Infinite 1.96 1.96 1.96 1.96<br />
2.7 k m for well-known material combinations<br />
2.7.1 For well-known FRP material combinations an upper limit of the standard deviation of the strength can<br />
be specified that has a negligible probability of being exceeded. For such materials an alternative procedure for<br />
determining the characteristic strength may be followed, in place of [2.5]. This procedure may result in a larger<br />
characteristic strength compared to what is prescribed in [2.5].<br />
For the purpose of determining characteristic strength by the alternative method a well-known material shall<br />
as a minimum fulfil the following conditions:<br />
— Fibres shall be E-glass or PAN based carbon fibres. The commercial brand of fibres shall have been<br />
available in the market for at least five years. More recent introductions to the market shall not be<br />
considered well known.<br />
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