OS-C501
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Offshore Standard DNV-<strong>OS</strong>-<strong>C501</strong>, November 2013<br />
Sec.6 Failure mechanisms and design criteria – Page 114<br />
F<br />
F<br />
F<br />
F<br />
f<br />
+<br />
nn<br />
1<br />
= , if σ < 0<br />
fibre<br />
II<br />
A<br />
+<br />
n<br />
=<br />
nt<br />
1c<br />
with,<br />
A t = A c = 1.6<br />
c<br />
1<br />
=<br />
R<br />
p<br />
R<br />
σ<br />
z<br />
⊥<br />
( + )<br />
⊥Ψ<br />
A<br />
⊥Ψ<br />
p<br />
−<br />
R<br />
( + )<br />
⊥Ψ<br />
A<br />
⊥Ψ<br />
, F<br />
, F<br />
− nn<br />
=<br />
−<br />
n<br />
=<br />
R<br />
( −)<br />
⊥Ψ<br />
A<br />
⊥Ψ<br />
= 1 1<br />
, F<br />
A<br />
nl<br />
=<br />
R<br />
R⊥<br />
||<br />
⊥⊥<br />
p<br />
p<br />
R<br />
( −)<br />
⊥Ψ<br />
A<br />
⊥Ψ<br />
τ<br />
τ<br />
nl<br />
nt<br />
= tan ψ<br />
( + ) ( + )<br />
( + )<br />
p<br />
⊥Ψ<br />
p<br />
p<br />
⊥<br />
=<br />
⊥⊥<br />
||<br />
cos<br />
2<br />
ψ + sin<br />
2<br />
ψ<br />
R<br />
A A<br />
⊥Ψ<br />
R<br />
⊥⊥ R<br />
⊥||<br />
( −)<br />
p<br />
2 ⊥||<br />
cos ψ + sin<br />
R<br />
( −)<br />
( −)<br />
p<br />
⊥Ψ<br />
p<br />
⊥⊥<br />
2<br />
=<br />
A A<br />
R<br />
⊥Ψ<br />
R<br />
⊥⊥<br />
⊥||<br />
R<br />
A<br />
⊥⊥<br />
d<br />
R⊥<br />
=<br />
2(1 + p<br />
(−)<br />
⊥⊥<br />
where the shape parameters<br />
)<br />
ψ<br />
( + ) ( −)<br />
( + ) ( −)<br />
p<br />
⊥||<br />
, p<br />
⊥||<br />
,p<br />
⊥⊥<br />
,p<br />
⊥⊥<br />
should be determined experimentally.<br />
If they are not available the following default values shall be used:<br />
( + )<br />
( −)<br />
( + )<br />
p = 0.30, p = 0.30, p = 0.15, p<br />
z<br />
R ⊥<br />
= σ ∧ matrix , R<br />
d = matrix , shear ⊥ σ ∧ ⊥||<br />
= .<br />
4.3.4 The characteristic strength for each of the stress<br />
components matrix , matrix , shear<br />
2t 2c<br />
and the corresponding coefficients of variation COV n are defined<br />
as specified in Sec.4 [1.6]. The combined COV comb is defined as:<br />
COV comb = max n (COV n )<br />
4.3.5 When two or more loads are combined, each stress component σ nk in direction n can be the result of<br />
several combined loads. In that case each stress component σ nk j , which is the local load effect of the structure<br />
in direction n due to load j, shall be considered separately as an individual stress component to determine the<br />
COV.<br />
or<br />
2t<br />
σ ∧<br />
2c<br />
( −)<br />
⊥|| ⊥||<br />
⊥⊥<br />
⊥⊥<br />
=<br />
σ ∧ 12<br />
σ ∧<br />
R 12<br />
σ ∧<br />
COV<br />
comb<br />
⎛ j ⎞ ⎛<br />
= ⎜∑σ . COVn<br />
⎟ / ⎜<br />
nk ∑<br />
⎝ n<br />
⎠ ⎝ n<br />
COV comb. = max n (COV n )<br />
Guidance note:<br />
This approach is conservative compared to the approach of Tukstra’s rule as used for the fibre design criteria. This<br />
approach has been chosen for simplification. In the case of fibre failure, only the strains parallel to the fibre directions<br />
have to be considered, whereas for matrix cracking all stress directions may interact.<br />
---e-n-d---of---G-u-i-d-a-n-c-e---n-o-t-e---<br />
4.3.6 The choice of the partial safety factors shall be based on the most conservative partial safety factors<br />
obtained when treating each stress component σ nk<br />
j , which is the local load effect of the structure in direction<br />
n due to load j, as a single load.<br />
j<br />
σ<br />
nk<br />
⎟<br />
⎠<br />
⎞<br />
0.27<br />
DET NORSKE VERITAS AS