Leading edge erosion detection for a wind turbine blade using far-field aerodynamic noise

Leading edge erosion detection for a wind turbine blade using far-field aerodynamic noise

Zhang, Y. (TU Delft Wind Energy)
Avallone, F. (Politecnico di Torino)
Watson, S.J. (TU Delft Wind Energy)

2023-05

In this paper, the feasibility of using far-field acoustic measurements as a non-contact monitoring technique for wind turbine blade leading edge erosion is assessed. For this purpose, a DU96 W180 airfoil with several eroded leading edge configurations of different severities is experimentally investigated. The eroded leading edges are designed with pits, gouges and coating delamination scaled from a real eroded blade. To assess the feasibility of the technique in quasi-realistic configurations, experiments are carried out under clean and turbulent inflow conditions. Acoustic measurements are performed with a phased microphone array. In the absence of inflow turbulence, because of the low Reynolds number at which the experiments are carried out, the case with minor erosion severity shows similar far-field noise spectra as the clean leading-edge cases, i.e., the presence of tonal peaks caused by laminar boundary layer instability noise through a self-sustained feedback loop but with higher tonal amplitudes. Increasing the damage level (considered as moderate erosion), the spectra of the noise scattered from the suction side show that the tonal peaks shift to higher frequencies and have lower amplitudes, thus suggesting that the damage alters the flow features responsible for the acoustic feedback loop; whereas, the spectra from the pressure side show a broadband noise distribution. For heavy erosion, the far-field noise spectra show broadband features from both airfoil sides, thus suggesting that the damage has fully forced the transition to turbulent flow; in which case, an increase in the low-frequency content is observed. Conversely, in the presence of turbulent inflow, when comparing the noise scattered at the trailing edge, no difference is found. However, leading edge impingement noise decreases at medium–high frequency compared with the baseline case at a chord-length-based Strouhal number St_C~10. The experimental results also suggest that the delamination feature is the one which is the most easily detectable and the approach is valid for a wide range of angles of attack and inflow velocity.

Wind turbine blade
Leading edge erosion
Aerodynamic noise
Damage detection
Aeroacoustics

http://resolver.tudelft.nl/uuid:313ab9c7-7732-40f9-b3c4-13d6cd356057

https://doi.org/10.1016/j.apacoust.2023.109365

0003-682X

Applied Acoustics, 207 (2023)

Institutional Repository

journal article

© 2023 Y. Zhang, F. Avallone, S.J. Watson