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PSD (m 2 /s)<br />
10 3<br />
10 2<br />
10 1<br />
10 0<br />
10 −1<br />
10 −2<br />
Blade and Rotor Effective Wind Speed Spectra<br />
Rotor Effective Wind Speed (Entire Disk)<br />
Blade Effective Wind Speed<br />
Collective Component, u hh<br />
Shear components, Δ h , Δ v<br />
10 −2<br />
10 −1<br />
Frequency (Hz)<br />
Figure 145: Power spectra of rotating blade effective wind speed as well as collective and<br />
shear components due to three rotating blades. The rotor effective wind speed, calculated<br />
by integrating wind speeds weighted according to their contribution to power over the entire<br />
rotor disk, is shown for comparison. Spectra are generated for the IEC von Karman wind field<br />
model using the NREL 5-MW turbine at mean wind speed 13 m/s.<br />
Simley and Pao (2013a) can be extended to calculate the spectra of the collective and<br />
shear components due to three rotating blades, using Eq. (239). Using the IEC von Karman<br />
wind field and the NREL 5-MW model, the rotating blade effective wind speed and rotating<br />
collectiveandsheartermsareplottedinFig.145fortheratedrotorspeed12.1rpm(0.202Hz)<br />
and above-rated wind speed 13 m/s. The blade effective wind speed spectrum contains peaks<br />
at the 1P frequency (0.202 Hz) and its harmonics, due to the blade passing through turbulent<br />
structures once per revolution. The collective and shear component spectra contain peaks at<br />
the 3P (three times per revolution) frequency (0.606 Hz) and its harmonics because each of<br />
the three blades passes through structures once per revolution. Also shown in Fig. 145 is the<br />
rotor effective wind speed averaged across the entire rotor disk, calculated using Eq. (229),<br />
to highlight the difference between modeling rotor effective wind speed as the wind felt by<br />
the rotor disk and the wind felt by three rotating blades.<br />
Forwindturbinecontrols,itispopulartouselinearmodelsoftheturbineinthenon-rotating<br />
frame because the resulting transfer functions do not vary with azimuth angle as much as<br />
in the rotating frame. Rotating variables at each of the three blades are instead represented<br />
as a collective component y0, a vertical component yv, and a horizontal component yh. For<br />
example, the flapwise bending moment experienced by each blade can be represented as the<br />
average bendingmomentoverall blades(y0), the netbendingmomentoftherotoraroundthe<br />
y axis (yv), and the net bending moment around the vertical z axis (yh). Transfer functions<br />
are calculated in the non-rotating frame using the multiblade coordinate (MBC) transform<br />
(Bir, 2008),which is used as the basis forEqs. (237) and (239). The response of the collective<br />
component of a turbine variable is dominated by the collective wind component uhh, and the<br />
vertical and horizontal components are dominated by the vertical ∆v and horizontal ∆h shear<br />
components of the wind, respectively. Figure 146 contains the magnitude squared frequency<br />
response of the transfer functions from hub height wind speed to the collective component of<br />
flapwise blade root bending moment as well as the transfer functions from horizontal shear<br />
and vertical shear to the horizontal component and vertical component of blade root bending<br />
moment generated using FAST (Jonkman and Buhl, 2005) with the 5-MW model at the<br />
above-rated wind speed 13 m/s. These transfer functions include blade pitch and generator<br />
208 <strong>DTU</strong> Wind Energy-E-Report-0029(EN)<br />
10 0