A leading-edge ice mass grows with time and distorts the airfoil. With a de-icing system selected, the ice is shed periodically. Colour shows the penalty magnitude (green → orange → red).
$$P_{\text{base}} = \tfrac{1}{2}\,\rho\,A\,V^{3}\,C_{p}, \qquad A = \tfrac{\pi}{4}D^{2}$$
Rotor area A and baseline power P_base. ρ = 1.225 kg/m³, C_p = 0.45.
$$R_{ice} = 6\,\text{LWC}\,V\,|T|\quad(\text{T}\le 0)$$
Ice accretion rate R_ice (g/m/hr). LWC: liquid water content, V: hub wind speed, |T|: below-freezing temperature offset.
$$\eta_{\text{loss}} = \min(50,\;0.5\,R_{ice})\cdot m_F, \qquad E_{\text{loss}} = P_{\text{active}}\,\eta_{\text{loss}}\,t_{\text{ice}}$$
Power penalty η_loss and annual energy loss E_loss. m_F is the mitigation factor (none 1.0, anti-icing 0.3, de-icing 0.5, hot-air 0.4).