Page 434 - Wind Energy Handbook
P. 434

408                                                     COMPONENT DESIGN


                                                    x (Down wind)



                                             ß        Ωr –y
                                y                     φ
                        (a)                                     U ∞ (l –a) –x .
                                  Plane of rotor        W
                                  rotation
                                                    F X
                                                         L

                                                    φ
                                              D        F Y
                                                             ß
                       (b)                               α
                                                        W
                                                  x
                                                     x*

                       y*
                               θ*
                           y
                       (c)
          Figure 7.16 (a) Velocity Diagram for Vibrating Blade (Looking Towards Hub); (b) Out-
          of-plane and In-plane Components of Lift and Drag Forces; (c) Directions of Vibration, x
          and y

          Here U 1 is the free stream wind speed and U 1 (1   a) the reduced wind speed at
          the rotor plane as usual. The damping coefficients per unit length for vibrations in
          the in-plane and out-of-plane directions are then given by


                                                  @F Y
                                         ^ c c Y (r) ¼                        (7:14a)
                                                    y
                                                  @ _ y
                                                  @F X
                                         ^ c c x (r) ¼                        (7:14b)
                                                    x
                                                  @ _ x
          Analagous ‘cross’ coefficients relating the in-plane force to the out-of-plane velocity
          and vice versa can also be defined as:


                                                  @F Y
                                         ^ c c YX (r) ¼                       (7:15a)
                                                    x
                                                   @ _ x
                                                  @F X
                                         ^ c c XY (r) ¼                       (7:15b)
                                                   @ _ y
                                                    y
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