Page 269 - Wind Energy Handbook
P. 269

BLADE LOADS DURING OPERATION                                           243




                                                             U
                                       A
                                  r
                                   radius
                                       Ωr

                               R                                B
                                       C











                                  v L A                s
                                          v T A
                                      A
                                 2  2
                               s 2  s 3
                               2r sin  Ωτ                   v L B   B
                                             2                     v r
                                        C                       B
                                                 s    Uτ
                                                 1
             Figure 5.17  Geometry for the Derivation of the Velocity Autocorrelation Function for a
             Point on a Rotating Blade

                                                                        B
             the corresponding function for velocity components (v A  and v ) in a direction
                                                                        T
                                                                T
             perpendicular to AB. s 1 is the separation of points A and B measured in the along-
             wind direction, Uô. Noting that the distance between points A and C on the rotor
             disc is 2r sin(Ùô=2), we have
                                            2 2
                                                   2
                                       2
                                                       2
                                      s ¼ U ô þ 4r sin (Ùô=2)                     (5:36)
             Hence
                                  2     "         2 #            2                   2
                             Uô               Uô            Uô          2r sin (Ùô=2)
              k u (~ s,0) ¼ k L (s)  þk T (s)1      ¼ k L (s)    þk T (s)
                 s
                              s                s             s               s
                                                                                  (5:37)

             For incompressible flow, it can also be shown (Batchelor, 1953) that

                                                     s dk L (s)
                                        k T (s) ¼ k L (s) þ                       (5:38)
                                                     2   ds
   264   265   266   267   268   269   270   271   272   273   274