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OS-C501

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Offshore Standard DNV-<strong>OS</strong>-<strong>C501</strong>, November 2013<br />

Sec.4 Materials - laminates – Page 55<br />

3.11.3 This section is applicable for estimating the characteristic (and subsequently the design) time to failure<br />

under a specified load for a laminate exposed to static or cyclic load, provided the plot of log stress vs. log time<br />

is linear.<br />

3.11.4 If the linear relationship cannot be documented, an equivalent approach shall be used, taking the nonlinearity<br />

into account.<br />

3.11.5 Values shall be based on data that are fairly evenly distributed over the plot of log time to failure vs. log<br />

load, or log number of cycles vs. log load. Load is usually expressed as stress or strain. At least 15 data points<br />

should be used.<br />

3.11.6 To obtain the characteristic curve the mean S-N curve of the form:<br />

log σ = log σ 0 fatigue - α log N<br />

or the mean stress rupture curve of the form:<br />

log σ = log σ 0 stress rupture - β log t<br />

shall be converted to the form:<br />

log(X) mean = log(X 0 ) – k⋅logσ<br />

where X represents the time (or number of cycles) to failure under a sustained stress σ (or stress range σ). X is<br />

a function of σ and exhibits a natural variability from point to point within the material.<br />

logσ<br />

0<br />

log X =<br />

0<br />

β<br />

stress rupture<br />

k =<br />

1<br />

β<br />

or<br />

or<br />

log<br />

log =<br />

X<br />

0<br />

1<br />

k =<br />

α<br />

σ 0 fatigue<br />

α<br />

Guidance note:<br />

Usually, estimates of k and logσ 0stressrupture (or logσ 0fatigue ) can be obtained from linear regression analysis of log X<br />

on log σ.<br />

---e-n-d---of---G-u-i-d-a-n-c-e---n-o-t-e---<br />

3.11.7 When the standard deviation σ ε of the variations in log(X) about the mean is constant, i.e. when σ ε does<br />

not depend on the sustained load or stress range σ, then the characteristic value of log(X) c can be taken as:<br />

log(X) c = log(X 0 ) – k⋅logσ - x⋅σ ε<br />

in which σ ε is estimated from available tests, and x is taken from Table 4-7 depending on the number n of<br />

available data pairs (logs, log X) from tests.<br />

Table 4-7 Values of coefficient x<br />

x<br />

n (# of tests) Case 1 Case 2<br />

10<br />

15<br />

20<br />

50<br />

100<br />

Infinite<br />

3.9<br />

3.4<br />

3.1<br />

2.6<br />

2.4<br />

2.0<br />

4.7<br />

4.0<br />

3.7<br />

3.0<br />

2.6<br />

2.0<br />

3.11.8 The coefficient values marked as Case 1 are valid and can be used for sustained loads or cyclic stresses<br />

within the range of σ-values covered by available tests, i.e. whenever the available tests cover a wide enough<br />

range of σ-values. These coefficient values will be non-conservative if applied for sustained loads or stresses<br />

σ outside the range of log σ-values covered by available tests. When values for x are needed for σ-values<br />

outside this range, coefficient values marked as Case 2 can be used for extrapolation within a concentric range<br />

of logσ twice the length of the range covered by tests.<br />

3.11.9 The mean curve can be transformed back into the standard formulation of an S-N curve, or stress rupture<br />

or fatigue curve using the same equations as given above.<br />

log<br />

— Stress rupture curve: σ<br />

X<br />

1<br />

0<br />

log 0stress<br />

rupture = and β = with X 0 as time.<br />

β<br />

k<br />

log<br />

X<br />

1<br />

0<br />

— Fatigue curve: log σ 0 fatigue = and α = with X 0 as number of cycles.<br />

α<br />

k<br />

3.11.10 The characteristic mean curve can be transformed back into the standard formulation of an S-N curve<br />

or stress rupture curve using the same equations as given above.<br />

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