Figures 5,6,7 were not correct in the published article. See below for the correct figures.

Figure 5
Inflow setup. The y=0 plane corresponds to the rotor plane. U corresponds to the rotational velocity, while V(t) corresponds to the free-stream velocity.
Figure 5
Inflow setup. The y=0 plane corresponds to the rotor plane. U corresponds to the rotational velocity, while V(t) corresponds to the free-stream velocity.
Figure 6
Deflection corresponding to β=5 deg. (a) Raw deflection shape. (b) Airfoil trailing edge region, with thickness.
Figure 6
Deflection corresponding to β=5 deg. (a) Raw deflection shape. (b) Airfoil trailing edge region, with thickness.
Figure 7
Wind step response. Std(N) as a function of control parameter Ay.
Figure 7
Wind step response. Std(N) as a function of control parameter Ay.