OS-C501
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Offshore Standard DNV-<strong>OS</strong>-<strong>C501</strong>, November 2013<br />
Sec.4 Materials - laminates – Page 68<br />
Table 4-11 Qualification against representative data (Continued)<br />
Mechanical parameter Low safety class Normal safety class High safety<br />
In-plane orthotropic<br />
elastic constants<br />
ν 13<br />
ν 23<br />
ε ∧<br />
3t<br />
ε ∧<br />
3c<br />
Poisson’s ratio normal to the fibre<br />
plane, including the fibre direction,<br />
when tensioning in the fibre direction.<br />
Poisson’s ratio normal to the fibre<br />
plane, including the direction normal<br />
to the fibres, when tensioning in the<br />
plane normal to the fibres.<br />
Tensioning strain at break, normal to<br />
the fibre plane.<br />
Compression strain at break, normal<br />
to the fibre plane.<br />
class<br />
rep × 1 rep × 1 confirm if<br />
critical for<br />
design<br />
rep × 1 rep × 1 confirm if<br />
critical for<br />
design<br />
rep × 0.9 or<br />
ε ∧<br />
= × 0.9<br />
2t<br />
rep × 0.9 or<br />
ε ∧<br />
= 2c<br />
× 0.9<br />
confirm if critical<br />
for design<br />
confirm if critical<br />
for design<br />
confirm if<br />
critical for<br />
design<br />
confirm if<br />
critical for<br />
design<br />
Tensioning strain at break normal to rep × 0.9 or<br />
ε ∧ 13<br />
the fibre plane when tensioning in the<br />
fibre direction.<br />
= ε ∧<br />
12 × 0.9<br />
confirm if critical<br />
for design<br />
confirm if<br />
critical for<br />
design<br />
ε ∧ 23<br />
Tensioning strain at break normal to rep × 0.9 or<br />
the fibre plane when tensioning in the<br />
fibre plane, normal to the fibre<br />
direction.<br />
= ε ∧<br />
12 × 0.9<br />
Tensioning stress at break normal to rep or<br />
the fibre plane.<br />
calculate<br />
σ ∧ 3t<br />
σ ∧ 3c<br />
13<br />
σ ∧ 23<br />
σ ∧<br />
Compression stress at break normal to<br />
the fibre plane.<br />
Stress at break normal to the fibre<br />
plane when tensioning in the fibre<br />
direction.<br />
Stress at break normal to the fibre<br />
plan, including the direction normal<br />
to the fibres, when tensioning normal<br />
to the fibre plane.<br />
rep or<br />
calculate<br />
rep or<br />
calculate<br />
rep or<br />
calculate<br />
confirm if critical<br />
for design<br />
calculate<br />
calculate<br />
calculate<br />
calculate<br />
confirm if<br />
critical for<br />
design<br />
calculate<br />
calculate<br />
calculate<br />
calculate<br />
Fracture Toughness<br />
Critical length In-plane rep × 0.8 confirm confirm<br />
G 1c<br />
Critical strain energy release rate in<br />
the fibre direction.<br />
rep × 0.8 confirm confirm<br />
G 2c<br />
Critical strain energy release rate in rep × 0.8 confirm confirm<br />
the fibre plane, normal to the fibre<br />
direction.<br />
Long Term Properties<br />
(see [8.6.15] and<br />
[8.6.16])<br />
Creep/Stress relaxation rep confirm if critical confirm<br />
for design<br />
Stress rupture rep confirm if critical confirm<br />
for design<br />
Static strength<br />
reduction under<br />
permanent load<br />
rep rep confirm if<br />
critical for<br />
design<br />
Change of modulus<br />
under cyclic fatigue<br />
Cycles to failure<br />
fibre dominated<br />
Cycles to failure<br />
matrix dominated<br />
Fibre dominated static<br />
strength reduction<br />
under fatigue load<br />
rep rep confirm if<br />
critical for<br />
design<br />
rep<br />
confirm if critical confirm<br />
for design<br />
rep<br />
confirm if critical confirm<br />
for design<br />
rep rep confirm if<br />
critical for<br />
design<br />
DET NORSKE VERITAS AS