Abstract
Inspired by the water-entry head morphology of cetaceans, this study investigates a biomimetic leading-edge deformation strategy for a symmetric NACA (National Advisory Committee for Aeronautics) 0009 hydrofoil (with chord length C = 100 mm). A series of deformation configurations was constructed by systematically varying the leading-edge deformation region (x0) and nose-drop distance (d0), and their cavitation control performance was evaluated in detail. High-fidelity large-eddy simulations were conducted to analyze the cavity structure, boundary layer characteristics, and hydrodynamic responses of each configuration. The results reveal that moderate leading-edge deformations (d0 > 0.02C, x0 = 0.2C-0.4C) significantly reduce cavity size, suppress unsteady cloud cavitation, and induce strong favorable pressure gradients near the cavity closure. These changes accelerate the boundary layer and enhance near-wall momentum transport, leading to a reduction in the resolved Reynolds shear stress. As the reentrant jet weakens and the cavity becomes more stable, vortex structures remain attached to the suction surface, resulting in a more stable and orderly flow field. Meanwhile, the lift-to-drag ratio increases substantially from 14.46 for the original hydrofoil to 45.67 under typical deformation parameters (x0 = 0.3C, d0 = 0.03C). When the deformation region is fixed at x0 = 0.3C, increasing d0 to 0.04C leads to the complete elimination of cavitation on the suction surface. This biomimetic approach offers new physical insights and practical design strategies for low-cavitation applications in marine propulsion and hydraulic machinery.
| Original language | English |
|---|---|
| Article number | 101909 |
| Journal | Physics of Fluids |
| Volume | 37 |
| Issue number | 10 |
| DOIs | |
| State | Published - 1 Oct 2025 |
UN SDGs
This output contributes to the following UN Sustainable Development Goals (SDGs)
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SDG 14 Life Below Water
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