Page 151 - Pipelines and Risers
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124                                                               Chapter 9


          9.2.4  Vibration Amplitude and Stress Range Analysis
          The results of the structural and environmental analysis are used as input to the calculation of
          the response of the free span to the environmental loads.
          The response may be found through the application of  static or quasi-static loads or may be
          given directly as vibration amplitudes.
          Due to the complexity of the physical processes involved, Le. the highly non-linear nature of
          the fluid-elastic interaction of  the vibrating span, the response of  the span will generally be
          determined through the application of model or full scale investigation.
          Therefore the fluid-elastic properties of the environmental and the free span will be described
          by a number of governing non-dimensional parameters which are used to retrieve the relevant
          response data (force coefficients and oscillation amplitudes).
          The response data are subsequently used to calculate:
             Stress range distribution
             Expected number of oscillations
             Fatigue damages parameter
             Maximum stress

          9.2.5  Fatigue Model
          To  calculate the relationship between  stress cycles experienced in  pipe  and  the  resulting
          fatigue damages, and thus the consumption of  fatigue life, relationship of  imperial or semi-
          empirical nature may  be  applied. This typically means a  determination of  the  number of
          cycles that lead to  failure for the  various dynamic stress range (e.g.  S-N curves) and the
          subsequently determination of  the accumulation of  the partial damages (e.g.  Palmer-Miners
          law).


          9.3  Fatigue Design Criteria


          9.3.1  Accumulated Fatigue Damage
          The fatigue damage shall be based on the accumulation law by Palmgren-Miner:



          where:
               DfaF accumulated fatigue damage
               q=  allowable damage ratio, normally to be taken as 0.1
               Ni=  number of cycles to failure at stress range S(U.)  defined by S-N curve
               ni=  number of equivalent stress cycles with stress range S(UJ  in block i


          Whcn sevcral potential vibration modes may bccomc activc simultancousl  y at givcn current
          velocity the  ode  associated with  the  largest contribution to  the  fatigue  damage  must  be
          applied. Formally, the fatigue damage criteria may be assessed numerically.
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