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382                                                  Part III Fatigue and Fracture


                 standards such as AWS (1997) are used in the USA. However, it should be noted that different
                 design  standards provide different procedures in the  fatigue stress determination and  S-N
                 classification, which result in large discrepancies in the predicted fatigue damages. Therefore,
                 a consistent procedure based on one design standard shall be used.
                 The safety factors for fatigue design of floating structures are given by the design standards
                 listed in Section 20.2 based on:
                    Criticality of the joint
                    Inspectability and repairability
                 The criticality of a join is determined based on its structural redundancy. A joint is critical if
                 its failure will potentially lead to the failure of the structure.
                 20.5.2  Stress Range Analysis

                 A stress range analysis is performed using the fatigue software as a precursor to the fatigue
                 damage calculation. The  FEA  unit  load,  model  geometry  and  element  stress results  are
                 interfaced into the fatigue calculation model. Loading combinations will then be defined for
                 each fatigue wave load based on the applied boundary loads.
                 Geometry and  element properties from the  space frame model  are plotted and revised for
                 accuracy. Any detected errors are corrected in the FEA input file and the FE analysis repeated.
                 The  finite  element model  of  the  specific hotspot  region  shall be  developed  based  on  the
                 procedures, finite element size requirement defined by the design standards.
                 In the FEA model, unit load results will be interfaced into the space fiame model database.
                 These unit loads are then appropriately combined based on the applied boundary loads.
                 20.5.3  Spectral Fatigue Parameters

                 Wave Environment
                 The  wave  environment  consists  of  wave  scatter  diagram  data  and  wave  directional
                 probabilities.
                 The  scatter  diagram  data  consists  of  annual  probabilities  of  occurrence  as fimctions  of
                 significant wave heights and peak periods in the structure installation site. For spectral fatigue
                 analysis, a wave spectrum (e.g. Pierson-Moskowitz) is associated with each cell of the scatter
                 diagram.
                 Directional probabilities for fatigue waves are also included in the fatigue assessment. It is
                 usually unconservative to  ignore any  non-uniform  distribution in  directional probabilities.
                 However, in lieu of such information, the wind directional probability may be used to account
                 for the non-uniformity in the wave approaching direction and to provide conservatism in the
                 fatigue damage calculation.
                 Stress Concentration Factors
                 The determination of the appropriate SCF in the fatigue analysis is a complex task. It is also
                 dependent on the S-N classification and stress analysis methods. The general rule of thumb is
                 that the stress used in the fatigue analysis should resemble the fatigue stress obtained from the
                 specimen tested when  deriving the S-N curves. The fatigue stress does not mean the most
                 accurate stress determined by the high-resolution fine mesh FEA.  It is the pertinent stress, in
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