Page 163 - Wind Energy Handbook
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THE METHOD OF ACCELERATION POTENTIAL                                   137


               For the wind turbine the value of a 0 may not be small compared with 1 and so the
             above procedure will converge on values of a 0 which are too small compared with
             what the momentum theory would deliver.
               To produce more realistic results that is, results in line with Glauert’s momentum
             theory where
                                        p ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
                                 C T ¼ 4a  1   a(2 cos ª   a) ¼ 4aA G (a)        (3:105)

             or the Coleman theory, where

                                               ÷            ÷
                            C T ¼ 4a cos ª þ tan  sin ª   a sec 2  ¼ 4aA C (a)   (3:111)
                                               2            2

             Also, the wake skew angle should be used in matrix [L] instead of the yaw angle.
               The matrix [L] should then be modified to become
                                2                                       3
                                        1                     15      ÷
                                6     4A(a 0 )       0       128  ð tan  2  7
                                6                                       7
                                6                      ÷                7
                                6
                                                                        7
                           [L] ¼ 6      0          sec 2        0       7        (3:189)
                                6                      2                7
                                6                                       7
                                4    15        ÷                     ÷ 5
                                          ð tan      0      1   tan 2
                                  128A(a 0 )   2                     2
             where A(a 0 ) is chosen according to which momentum theory is to be used.
               The Pitt and Peters method does not include any determination of induced
             velocities in the plane of the rotor disc and as a consequence it is not possible to
                                                                                    m
             account for wake rotation. However, it is possible that the Kinner solutions Q (í)
                                                                                    n
                                                                                  2
             that were excluded from the analysis because they give infinite pressure at í ¼ 1,
             which lies along the axis of rotation, may give velocity distributions which provide
             for wake rotation; the momentum theory of Section 3.3 also predicts an infinite
             pressure at the axis of rotation because of wake rotation. In practice, of course, the
             rotor disc would not extend to the axis of rotation and the singularity would not
             occur.
               With or without wake rotation a flow angle ö can be determined from which a
             torque can be found. If the normal force on an element of the rotor disc is equal to
             äL cos ö then the tangential force will be äL sin ö.



             3.11.6  The general acceleration potential method

             Peters with a number of associates has developed the theory further and a reading
             of these references (Pitt and Peters, 1981, Goanker and Peters, 1988, HaQuang and
             Peters, 1988) is recommended. The acceleration potential method has been devel-
             oped specifically for wind turbines by van Bussell (1995) where a much more
             comprehensive account of the theory is given.
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