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    Hydrodynamics and wave energy extraction in passive propulsion of a flexible foil under water surface waves

    Ming Li

    Sung Goon Park

    Fotis Sotiropoulos

    Lian Shen*

    • Department of Mechanical Engineering and Saint Anthony Falls Laboratory, University of Minnesota, Minneapolis, Minnesota 55455, USA

    • *Contact author: shen@umn.edu

    Phys. Rev. Fluids 11, 014801 – Published 8 January, 2026

    DOI: https://doi.org/10.1103/bctn-vnrj

    Abstract

    A flexible body can interact with an incident water wave passively and extract wave energy to generate a thrust force. To understand the hydrodynamic performance and the wave energy extraction mechanism in this passive propulsion, we use direct numerical simulation to investigate the two-dimensional unsteady motion of a passive flexible foil with a fixed leading edge under an incident wave superposed with a current flow at a Reynolds number of O(1000). The results of kinematics studies show that the passive flapping motion is up–down asymmetric, with the trailing-edge displacement having a larger magnitude above the fixed leading edge. The peak-to-peak trailing-edge amplitude is a strong function of the reduced frequency, and a maximum trailing-edge amplitude is observed, indicating a resonance phenomenon. Passive propulsion is achieved under the wave with a maximum cruising speed of 4.5 times of the chord length per unit time at a Reynolds number of 1000. The foil reaches a peak propulsive efficiency between the Strouhal number (St) values of 0.2 and 0.4. At low St values, the scaling relationship of the mean thrust coefficient (CT¯) and propulsion efficiency (ηe) with respect to St are similar between the passive propulsion of flexible foils under waves and the active heaving and pitching of rigid foils in free streams, and CT¯ scales with St2. At high St values, CT¯ scales with St3. When St is greater than a threshold value between 0.2 and 0.27, a passing-over leading-edge vortex is generated, which is responsible for the CT¯∼St3 scaling and the enhanced thrust force generated at high St.

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