Page 455 - Pipelines and Risers
P. 455

422                                                              Chapter 22















                                                              REDUCED VELOCITY
                                                              VR = U/(fnD)

           Figure 22.3 Typical amplitude response due to reduced velocity.



           22.6  Fatigue Life

           22.6.1  Estimate of Fatigue Life
           Fatigue damage from first order response due to individual seastates and from VIV generated
           by individual current profiles may be summed using the Miner’s rule. Consideration should
           be given to the distribution of fatigue damage around the riser circumference in order to avoid
           unnecessary conservatism and the damage calculated at 8 circumferential points.
           Bending  is  an  important  consideration for  fatigue.  Indeed,  the  wave  induced  bending
           moments in the splash zone are important for fatigue consideration.
           Fatigue assessment based on S-N curves shall be applied.
           Fatigue damage shall be estimated using Miner’s rule summation as given below:




           where, D is accumulated fatigue damage ratio, ni is the stress range cycle numbers in stress
           block i, Ni is the allowable stress cycle number at constant stress range, q is the allowable
           fatigue damage ratio given as:
                    0.1    no  inspection
                ‘=  { 0.3   with  inspection
           Normally, the riser should be designed without consideration of  inspection. If  inspection is
           included in fatigue evaluation, the inspection shall detect the critical cracks.
           Fracture mechanics may be applied for the estimate of fatigue life using Paris’ law. The initial
           crack size must be selected based on statistics.

           22.6.2  Effect of Inspection on Fatigue Analysis
           The effect of inspection on fatigue evaluation is included by selecting the allowable fatigue
           damage ratio q=0.3. This factor might be released a slightly by using fracture mechanics.
   450   451   452   453   454   455   456   457   458   459   460