Cavitation analysis of plunging hydrofoils using large eddy simulations.

This study employs numerical analysis to investigate the behavior of the National Advisory Committee for Aeronautics (NACA)66 modified (mod) hydrofoil under plunging motion, considering various cavitation numbers. The Large Eddy Simulation (LES) method is utilized to model turbulence. The hydrofoil's plunging motion leads to an increase in lift force and a decrease in drag force. Our research indicates that increasing the speed of the hydrofoil's heaving motion delays the onset of cavitation and enhances the formation of cavity clouds. Furthermore, during the peak oscillatory motion of the hydrofoil in the plunging phase, the detachment length of cavitation bubbles decreases. Additional investigations reveal that cavitation on the hydrofoil's surface accelerates the transition from a laminar to a turbulent boundary layer, strengthening the turbulent boundary layer and postponing the onset of flow separation. This research involves an in-depth investigation of the terms in the vorticity transport equation in cavitation inception, finding a correlation between vapor volume fraction and vorticity dilatation near the hydrofoil surface. This correlation proves crucial to the initial stages of the cavitation inception process. • The plunging motion of NACA66 mod hydrofoil boosts lift and cuts drag, enhancing aerodynamic efficiency. • Higher speeds in hydrofoil heaving delay cavitation onset, improving cavity cloud formation. • The study reveals a key link between vapor volume fraction and vorticity dilatation, crucial for understanding early cavitation inception. [ABSTRACT FROM AUTHOR]