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OS-C501

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

Sec.3 Design input – Page 33<br />

S<br />

S<br />

S s<br />

S s1<br />

S s2<br />

t<br />

t<br />

S<br />

S<br />

S s1<br />

S s<br />

S s2<br />

t 1 t 2<br />

t<br />

t<br />

S<br />

S s1<br />

t<br />

S s2<br />

t 1 t 2<br />

Figure 3-2<br />

Examples of division into time intervals and definition of the sustained values S si for different load<br />

effects.<br />

9.6 The fatigue load effects<br />

9.6.1 All load effect fluctuations, e.g. stress or strain fluctuations, imposed during the entire design life, shall<br />

be taken into account when determining the long-term distribution of stress or strain ranges. All phases shall<br />

be included and both low-cycle fatigue and high-cycle fatigue shall be considered.<br />

9.6.2 Fatigue may be analysed for load effects in terms of either stress or strain. Strain is preferred for<br />

composite laminates.<br />

9.6.3 The characteristic distribution of load effect amplitudes shall be taken as the expected distribution of<br />

amplitudes determined from available data representative for all relevant loads. This is a long-term distribution<br />

with a total number of stress/strain cycles equal to the expected number of stress/strain cycles over a reference<br />

period such as the design life of the structure.<br />

9.6.4 For fatigue analysis the mean and amplitude of the stress or strain fluctuations shall be specified.<br />

Basically a table of the following form given in Table 3-3 should be established.<br />

Table 3-3 Definition of fatigue loads<br />

Number of cycles Mean load Amplitude<br />

DET NORSKE VERITAS AS

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