3.1 General
3.1.1 The following assumptions are made in the fatigue assessment:
- a) A linear cumulative damage model, i.e. Palmgren-Miner’s Rule,
given in Ch 9, Sec 3, [5], has been used in connection with the
design S-N curves, given in Ch 9, Sec 3, [4].
- b) Design fatigue life, TDF, is taken not less than 25
years.
- c) Rule quasi-static wave induced loads are based on North Atlantic wave
environment. They are determined at 10-2 probability level of
exceedance by the Equivalent Design Wave (EDW) concept.
- d) Net thickness tn50 approach is used,
according to [5].
- e) Type of stress used for crack initiating at the weld toe is the hot spot
stress. Type of stress used for crack initiating at free edge of non-welded
details is local stress at free edge.
- f) Fatigue stress range ΔσFS may be calculated by simplified
stress analysis or by finite element stress analysis for details with more
complex geometry.
- g) Long term distribution of stress range of a structural detail is assumed to
follow a two-parameter Weibull distribution. Weibull shape parameter ξ is equal
to 1 and the fatigue stress range ΔσFS is given at the
reference probability level of exceedance equal to 10-2.
- h) The acceptance criteria for fatigue checking are the total
fatigue damage D to be less than 1 for the design fatigue life, as
required in Ch 9, Sec 3, [2].