Experimental investigation on cavitation and induced noise of two-dimensional hydrofoils with leading-edge protuberances

• Published in: Physics of Fluids
• Main Authors: Simanto, R. I. A., Hong, Ji-Woo, Kim, Ki-Seong, Ahn, Byoung-Kwon, Shin, Suyong
• Other Authors: National Research Foundation of Korea, Daewoo Shipbuilding & Marine Engineering
• Format: Article in Journal/Newspaper
• Language: English
• Published: AIP Publishing 2022
• Subjects: Humpback Whale
• Online Access: http://dx.doi.org/10.1063/5.0127170; https://pubs.aip.org/aip/pof/article-pdf/doi/10.1063/5.0127170/19815020/124115_1_online.pdf

The applicability of leading-edge protuberances as a passive flow control approach inspired by humpback whale flippers has attracted significant research attention in aquatic and aeronautic systems because of their influence on critical hydrodynamic and aerodynamic aspects. An experimental investigation is conducted in a cavitation tunnel under various flow conditions to determine the effectiveness of leading-edge protuberances in controlling the detrimental effects of cavitation and suppressing flow-induced noise. The experiments are carried out on four National Advisory Committee for Aeronautics airfoil 0012 hydrofoils at 7° attack angles and free stream velocities up to 10 m/s. One of the four hydrofoils is considered the baseline, while the other models have wavy leading-edge modifications with different sinusoidal protuberances. These geometry modifications are defined by the amplitudes (A) (2% and 4% of the mean chord length) and wavelengths (λ) (12.5% and 25% of the mean chord length) of the sinusoidal protuberances. Investigations of flow over hydrofoils from top and side views at various Reynolds numbers exhibit that cavitation first appears in the modified hydrofoils' troughs and is restricted to just behind the protuberance troughs for the entire cavitating flow range. These results contrast the baseline geometry, where cavitation inception occurs at the flat leading edge, and the sheet cavity expands spanwise with extensive cloud shedding. Image processing under certain conditions reveals that the protuberances reduce cavitation by 25%–60%. The analysis of the sound pressure level demonstrates that the leading-edge protuberances effectively decrease flow-induced noise at higher flow velocities when cavitation is the dominant noise source. Finally, the direct comparison of cavitating flow characteristics, quantitative cavitation measurements, and noise production analysis between the baseline and modified hydrofoils, and their comparison among the modified geometries, provides a significant reference ...