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48                         AERODYNAMICS OF HORIZONTAL-AXIS WIND TURBINES











                                                    2a'Ωr

                                                         p D -_ 1 _    2  ρ  2
                                                              ρ(2a'Ωr)
                                                 U (1-a)
                                                  ∞
                             p D +              a'Ωr

                                          U (1-a)
                         U (1-a)            ∞
                          ∞





                                              Ωr
                           Rotor motion


                     Figure 3.5  Tangential Velocity Grows Across the Disc Thickness

          imparting the tangential velocity component to the air whereas the axial force acting
          on the ring will be responsible for the reduction in axial velocity. The whole disc
          comprises a multiplicity of annular rings and each ring is assumed to act indepen-
          dently in imparting momentum only to the air which actually passes through the
          ring.
            The torque on the ring will be equal to the rate of change of angular momentum
          of the air passing through the ring. Thus,

                  torque ¼ rate of change of angular momentum

                         ¼ mass flow rate 3 change of tangential velocity 3 radius

                     äQ ¼ räA d U 1 (1   a)2Ùa9r 2                             (3:17)

          where äA d is taken as being the area of an annular ring.
            The driving torque on the rotor shaft is also äQ and so the increment of rotor
          shaft power output is
                                          äP ¼ äQÙ

          The total power extracted from the wind by slowing it down is therefore deter-
          mined by the rate of change of axial momentum given by Equation (3.10) in Section
          3.2.2
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