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296                        DESIGN LOADS FOR HORIZONTAL-AXIS WIND TURBINES


          exponent are compared in Figure 5.41 for two- and three-bladed rigid hub machines
          operating at 30 r.p.m. in a hub-height wind speed of 12 m=s. The ratio of moment
          ranges is still close to 2:1:5.


          5.10.3 Stochastic aerodynamic loads

          The out-of-plane blade root bending moments arising from stochastic loads on the
          rotor will result in both a fluctuating hub ‘dishing’ moment (see above) and
          fluctuating shaft bending moments. For a two-bladed, rigid hub rotor, the shaft
          moment is equal to the difference between the two out-of-plane blade root bending
          moments, or teeter moment, the standard deviation of which is given by Equation
          (5.102). Similarly, the standard deviation of the mean of these two moments (i.e.,
          the ‘dishing’ moment) is given by Equation (5.103).
            The derivation of the standard deviation of the shaft moment for a three-bladed
          machine is at first sight more complicated, as the integration has to be carried out
          over three blades instead of two. However, if the shaft moment about an axis
          parallel to one of the blades, M ZS (Figure 5.35), is chosen, the contribution of
          loading on that blade disappears, and the expression for the shaft moment standard
          deviation becomes:
                              ð  ð                     p ffiffiffi  p ffiffiffi
                             2 R   R                    3    3
                                      o
             ó  2  ¼  1 ˜Ù  dC l     k (r 1 , r 2 ,0)c(r 1 )c(r 2 )           (5:119)
              Mzs    2   dÆ     R  R  u                2  r 1  2  r 2 jr 1 jjr 2 j dr 1 dr 2
                                                                         o
          where the limits of the integrations refer to the other two blades. k (r 1 , r 2 ,0) is
                                                                         u
          given by Equation (5.51), with Ùô set equal to zero when r 1 and r 2 are radii to points
          on the same blade, and replaced by 2ð=3when r 1 and r 2 are radii to points on
          different blades. Note that, compared with the two-bladed case, the cross correla-

               50
                     Shaft bending moment: two bladed rigid hub machine
               40  Shaft bending moment: three bladed machine Rotational speed = 30 r.p.m.
              Shaft bending moment about axis perpendicular to blade 1  -10 0  0  10  20  30  40  50  60  70  80  90  100  110  120  130  plane root bending moment 220  230  240  250  260  270  280  290  300  310  320  330  340  350  360
               30
                                          Rotor diameter = 40 m
                                        Hub-height wind speed = 12 m/s
               20
                                           Shear exponent = 0.2
               10
                                           150
                                                 180
                                               170
                                             160
                                                    200
                                                      210
                                                  190
                                          140
                                            Blade 1 out-of-
               -20
               -30
               -40
               -50
                                          Azimuth of blade 1 (degrees)
                    Figure 5.41 Shaft Bending Moment Fluctuation due to Wind Shear
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