Page 121 - Wind Energy Handbook
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CALCULATED RESULTS FOR AN ACTUAL TURBINE                                95


                0.8                                   0.15



                0.6                                    0.1
               Axial flow induction factor  0.4      Tangential flow induction factor  0.05








                0.2



                 0                                      0
                  0.2          0.4           0.6        0.8         1  0.2          0.4           0.6        0.8         1
                                r/R                                    r/R
               Figure 3.43 Distribution of the Flow Induction Factors for a Range of Tip Speed Ratios


              0.6                                       8
                        dQ
                        dr                                        dF
              0.5                                                 dr
                  1
                      p  U     s  R 2
                        2

                  2                                     6   1     p  U     s  R 2
                                                                  2
              0.4                                           2
           Torque per unit span  0.3                  Blade axial force per unit span  4



              0.2


              0.1                                       2


               0                                        0
               0.2            0.4             0.6             0.8             1  0.2            0.4             0.6             0.8             1
                               r/R                                      r/R
                     Figure 3.44  Distribution of Blade Loads for a Range of Tip Speed Ratios


             the flat distribution of torque at the high tip speed ratio of 12; this is caused by the
             effect of drag which reduces torque as the square of the local speed ratio and with
             the low angle of attack at º ¼ 12 drag causes a significant loss of power.
               Although the blade axial force coefficient increases with tip speed ratio it must be
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