Page 449 - Pipelines and Risers
P. 449

416                                                              Chaprer 22


          calculated assuming the drift motions are Rayleigh distributed. The total fatigue damage from
          each window is then calculated assuming the same drift motions apply to each seastate in the
          window. For each scatter diagram window, the mean and RMS drift offset are conservatively
          selected based on the extreme values of any of the seastates in the window.

          22.2.3  VIV Induced Fatigue
          Vortex-induced vibration  (VIV) is  probably  the  single  most  important  design  issue  for
          metallic catenary risers, particularly for high current locations. High frequency vibration of
          the riser pipe due to vortex shedding leads to high frequency cyclic stresses, which can result
          in high rates of fatigue damage.
          Vortex-induced vibration occurs anytime when a sufficiently bluff body is exposed to a fluid
          flow that produces vortex shedding at, or near, a structural natural frequency of the body (see
          Figure 22.1 & 22.2). Deepwater risers are especially susceptible to VIV because:
           1.  currents are typically higher in deepwater areas than in shallower areas;
          2.  the  increased  length  of  the  riser  lowers  its  natural  frequency  thereby  lowering  the
             magnitude of current required to excite VIV; and
          3.  deepwater platforms are usually floating platforms so that there are no structures adjacent
             to the riser to which it could be clamped.


                                                            IN-LINE
                                                            DIRECTION


                        U       3      3      3

                                 SYMMETRIC VORTEX SHEDDING,
                                 INDUCES IN-LINE VIBRATIONS
              mow
              VELOCITY

                                                            I   CROSSFLOW

                                     333


                        0 3333                                 DIRECTION

                                 NON-SYMMETRIC VORTEX SHEDDING,
                                 INDUCES CROSSFTOW VIBRATIONS
              FLOW
              VELOCITY



           Figure 22.2 Typical flow behind a cylinder.
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