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Chapter 20 Spectral Fatigue Analysis and Design                       381

                  The  global motion  analysis serves as a basis  for dynamic load  development.  The  actual
                  interface  from  the  global  analysis  to  the  structural  analysis  consists  of  several  loading
                  components for each analyzed wave period and direction: the real and imaginary applied unit
                  amplitude, wave diffraction and radiation loads, the associated inertial loads and other cyclic
                  loading such as tendon dynamic reactions. The successful interface of these load components
                  is dependent on a consistent geometric and mass model between the motion and the structural
                  analyses and  is also dependent on a consistent generation of the loading components in the
                  motion analysis. Consistent modeling is obtained by interfacing the model geometry directly
                  from the motion analysis wherever possible. Consistent mass is obtained by interfacing with
                  the same weight control database for both the motions and structural analyses, when available.
                  Load combinations are formed for each wave period and direction. These combinations consist
                  of the applied wave load, the generated inertial load, and the associated cyclic loadings such as
                  tendon dynamic reactions for both  real  and  imaginary loadings of  the  floating structures.
                  These combinations form the total cyclic load condition for each wave period and direction to
                  be used in the spectral fatigue analysis.
                  Analysis and Validation
                  Hull  structural analyses are performed  using  linear finite element methods.  The reaction
                  forces  include  total  force  and  moment  reactions  and  the  analysis  results  are  verified.
                  Symmetrical  or  asymmetrical  load  conditions  are  checked  to  confirm  symmetrical  or
                  asymmetrical analysis results.

                  20.4.2  Local Structural Analysis
                  Local structural details are included as a part of the analyses for the entire hull structure.
                 The analysis of the structural details may be performed using the finite element program such
                 as ABAQUS (HKS, 2002) and other software. The FEM model is three-dimensional and linear
                 stress analysis is performed. The results from the FEA model are interfaced into the fatigue
                 model for additional model validation and subsequent spectral fatigue analysis of the local
                 structural details. The entire model is plotted and  revised for accuracy both from the FEA
                 model and after interface to the fatigue model.
                 Loading conditions for finite element analysis of local structural details should be based on the
                 hull's structural analysis since it includes all cyclic loadings of the structure.
                 The unit loading conditions are frequently applied. The resulting stresses for each unit load
                 condition are interfaced to the fatigue model for subsequent combination into fatigue design
                 loads.


                 20.5  Fatigue Analysis and Design

                 20.5.1  Overall Design
                 A  spectral fatigue assessment should be  carried out  for each individual structural detail. It
                 should be noted that  every structural detail, every welded joint and attachment or any other
                 form  of  stress  concentration  is  potentially  a  source  of  fatigue  cracking  and  should  be
                 considered individually.
                 The UK  DEn procedure or its modified versions are recommended in Europe for the fatigue
                 analysis and design of floating structures since it is the most widely accepted code. Design
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