Numerical framework analyzes blade icing impact on wind turbine efficiency, suggesting design improvements.
Blade icing critically constrains the efficiency and safety of wind turbines in cold and offshore regions, yet the spatial characteristics of full-blade icing under rotation, the parametric sensitivity of icing-induced aerodynamic degradation, and the mechanism of leeward icing remain insufficiently understood. This study develops a numerical framework coupling Fluent with FENSAP-ICE, in which Moving Reference Frame and dynamic-meshing techniques enable three-dimensional rotating simulations of airflow, droplet impingement, water-film migration, phase-change icing, and aerodynamic evaluation. At −10°C, rotational speed, inflow velocity, liquid water content (LWC), and median volume diameter (MVD) are varied parametrically, and response surface methodology quantifies spanwise sensitivities of icing and lift-to-drag ratio degradation. Wind velocity governs aerodynamic deterioration most strongly near the blade tip, with LWC secondary, whereas LWC dominates at mid-span, where wind velocity and droplet size show comparable secondary significance, indicating pronounced rotation-induced radial differences. Leeward icing stems mainly from windward water films transported into the leeward low-pressure separation zone by aerodynamic shear, centrifugal force, and gravity, rather than direct droplet impingement, and intensifies with larger droplets. Icing reduces the tip lift-to-drag ratio by up to 80% and shifts the optimal angle of attack, informing ice warning, zonal anti-/de-icing design, and operational control.
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Li et al. (2026) studied this question.
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