Page 255 - Wind Energy Handbook
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BLADE LOADS DURING OPERATION                                           229


             permissible). These equations can be arranged to give the following expressions for
             the forces per unit length on an element perpendicular to the plane of rotation and
             in the direction of blade motion, known as the out-of-plane and in-plane forces
             respectively:

                                                                             f
                                                      1   2         2
                                                                    1
               Out-of-plane force per unit length: F X ¼ C x 2 rW c ¼ 4ðrU (1   af)a  N  r  (5:18)
                                                                             f
                                                   1   2                       2
               In-plane force per unit length:  F Y ¼ C y 2 rW c ¼ 4ðrÙU 1 (1   af)a9  r  (5:19)
                                                                            N
             The parameters in the expressions are as defined in Chapter 3 ( f is the tip loss
             factor, and N is the number of blades), while the x and y directions are as defined in
             Figure C1.
               The variation of the in-plane and out-of-plane forces with radius is shown in
             Figure 5.6 for a typical machine operating in a steady 10 m=s wind speed. The 40 m
             stall-regulated turbine considered in this example is fitted with three ‘TR’ blades as
             described in Example 5.1 and rotates at 30 r.p.m. The blade twist distribution is
             linear, and selected to produce the maximum energy yield for an annual mean
             wind speed of 7 m=s. It is evident that the out-of-plane load per unit length
             increases approximately linearly with radius, in spite of the reducing blade chord
             until the effects of tip loss are felt beyond about 75 percent of tip radius. Note that
             the form of the variation would be the same for any combination of rotational
             speed, wind speed and tip radius yielding the same tip speed ratio, because it is the
             tip speed ratio that determines the radial distribution of flow angle ö, and of the
             induction factors a and a9.
               Integration of these forces along the blade then yields in-plane and out-of-plane

                  1.8
                  1.6                        Out-of-plane force
                                               per unit length
                  1.4
                       Rotational speed = 30 rpm
                  1.2
                 Load per metre (KN)  0.8 1




                  0.6
                  0.4                             In-plane force
                                                   per unit length
                  0.2
                  0
                   0      2     4     6      8     10    12    14    16     18    20
                                                 Radius (m)
             Figure 5.6  Distribution of Blade In-plane and Out-of-plane Aerodynamic Loads during
             Operation of Typical 40 m Diameter Stall-regulated Machine in a Steady, Uniform 10 m=s
             Wind
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