Page 95 - Wind Energy Handbook
P. 95

BLADE GEOMETRY                                                          69


             (see Equation 3.50a), giving
                                             d     1   a
                                                a ¼                               (3:57)
                                            da9      a9
             From Equations (3.48) and (3.50a) a relationship between the flow induction factors
             can be obtained. Dividing equations 3.48 and 3.50a

                                    C l
                                       tan ö   1
                                    C d             ºìa9(1   a)
                                               ¼                                  (3:58)
                                     C l         a(1   a) þ (a9ºì) 2
                                       þ tan ö
                                     C d
             The flow angle ö is given by
                                                   1   a
                                          tan ö ¼                                 (3:59)
                                                 ºì(1 þ a9)
             Substituting Equation (3.59) into Equation (3.58) gives


                                  C l  1   a
                                                1
                                  C d ºì(1 þ a9)  ¼   ºìa9(1   a)
                                         1   a                   2
                                   C l             a(1   a) þ (a9ºì)
                                     þ
                                   C d  ºì(1 þ a9)
             Simplifying,

                                C l
                                  (1   a)   ºì(1 þ a9)
                                C d                     ºìa9(1   a)
                                                   ¼
                                         C l          a(1   a) þ (a9ºì) 2
                               ºì(1 þ a9)  þ (1   a)
                                        C d

                C l                                2             C l
                  (1   a)   ºì(1 þ a9) [a(1   a) þ (a9ºì) ] ¼ ºì(1 þ a9)  þ (1   a) ºìa9(1   a)
               C d                                               C d
                                                                                  (3:60)

             At this stage the process is made easier to follow if drag is ignored, Equation (3.60)
             then reduces to

                                                   2 2
                                         a(1   a)   º ì a9 ¼ 0                   (3:60a)
             Differentiating Equation (3.60a) with respect to a9 gives

                                               d      2 2
                                       (1   2a)   a   º ì ¼ 0                     (3:61)
                                               da9

             and substituting Equation (3.57) into (3.61)
                                                      2 2
                                      (1   2a)(1   a)   º ì a9 ¼ 0                (3:62)
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