Page 293 - Wind Energy Handbook
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BLADE DYNAMIC RESPONSE                                                 267


             oscillations have largely died away after a complete revolution because of the
             relatively high levels of damping.
               The response of the Blade TR out-of-plane root bending moment to tower shadow
             combined with wind shear is shown in Figure 5.26 for a hub-height wind speed of
             12 m/s. Also plotted is the corresponding bending moment for a completely rigid
             blade. The wind shear loading is approximately sinusoidal (see Figure 5.11), and,
             consequently, the response is also. However, it is worth noting that the amplitude
             of the dominating first mode response to wind shear is the result of two effects
             working against each other – in other words the increase due to the dynamic
             magnification factor of about 9 percent is largely cancelled out by the reduction due
             to centrifugal stiffening.



             Avoidance of resonance: the Campbell diagram

             In the course of blade design, it is important to avoid the occurrence of a resonant
             condition, in which a blade natural frequency equates to the rotational frequency or
             a harmonic with a significant forcing load. This is often done with the aid of a
             Campbell diagram, in which the blade natural frequencies are plotted out against
             rotational frequency together with rays from the origin representing integer multi-
             ples of the rotational frequency. Then any intersections of the rays with a blade
             natural frequency over the turbine rotational speed operating range represent
             possible resonances. An example of a Campbell diagram is shown in Figure 5.27.
               Clearly blade periodic loading is dominated by the loading at rotational fre-
             quency from wind shear, yawed flow and shaft tilt (Section 5.7.2), gravity (Section
             5.7.3) and gust slicing (Section 5.7.5). However, the short-lived load relief resulting
             from tower shadow will be dominated by higher harmonics.

                 290

                 270

                Blade root bending moment (kNm)  230       Blade TR root bending moment:
                 250


                                                             First and second mode
                                                              combined response
                 210
                        Rotational speed = 30 r.p.m.
                          Rotor diameter = 40 m
                 190
                       Hub-height wind speed = 12 m/s
                         Wind shear exponent = 0.2
                 170
                                                    Root bending moment variation for
                                                       completely rigid blade
                 150
                   360  10  20  30  40  50  60  70  80  90  100  110  120  130  140  150  160  170  180  190  200  210  220  230  240  250  260  270  280  290  300  310  320  330  340  350  360
                                                Blade azimuth
             Figure 5.26  Blade TR Out-of-plane Root Bending Moment Dynamic Response to Tower
             Shadow and Wind Shear
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