Erratum: “Potential Load Reduction Using Airfoils with Variable Trailing Edge Geometry” [Journal of Solar Energy Engineering, 2005, 127(4), pp. 503–516] Free

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.

Deflection corresponding to $β=5$ deg. (a) Raw deflection shape. (b) Airfoil trailing edge region, with thickness.

Wind step response. $Std(N)$ as a function of control parameter $Ay$⁠.