Page 155 - Pipelines and Risers
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128                                                              Chapter 9


           9.4.2  Cross-flow VIV in Combined Wave and Current
           This section applies to all cross-flow loads in all types of regions (a4.5 & 0.5ca4.8 wave
           dominant and d.8 current dominant).


           Onset of Cross-flow Lock-on
           For  steady  current  dominated  flow  situations  on-set  of  cross-flow  VIV  of  significant
           amplitude occurs typically at a value of reduced velocity, VR, between 3.0 and 5.0, whereas
           maximum amplitude vibrations occur at a value between 5.0 and 7.0. For wave dominated
           flow situations, cross flow vibrations may be initiated for VR as low as between 2 and 3 and
           are in this region apparently linked to the in-line motions. For high values of VR the motion
           are again de-coupled.





                                                                              (9.9)






           (pJp)  is the specific mass to be taken as:

                                                                              (9.10)




           Thus the onset of cross-flow motion will not occur if the reduced velocity is below VR,,,,~~~.

           Stress Range
           If it is established that cross-flow VIV may occur, the span will have to be checked for fatigue
           damage.  An  important  parameter is the  stress range,  S(Un),  associated  with  the  response
           amplitude. The stress range may be approximately estimated as:
                S=2.S,   .R. f,(V,,Kc,a)                                      (9.1 1)

           where:
                Sm= stress amplitude (stress due to unit diameter mode shape deflection) to which is to
                    be estimated by a dedicated FE analysis package.
               R=  amplitude reduction factor accounting for damping and gap ratio.

           The  characteristic  (maximum)  amplitude  response  fy(VR,KC, a ) in  combined  current  and
           wave flow may be taken from Figure 9.4 (DNV, 1998).
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