Effects of Plunging Acceleration on the Passive Morphing of Avian-Inspired Flexible Foils

TL;DR

This research explores how passive wing morphing under acceleration affects aerodynamics, revealing optimal flexibility levels and the influence of wing geometry on performance, with implications for bio-inspired flight design.

Contribution

It introduces a comprehensive simulation study linking wing flexibility, geometry, and unsteady aerodynamics in accelerated plunging scenarios, highlighting optimal stiffness and flexible segment effects.

Findings

Flexible trailing-edge wings improve aerodynamic performance.

Excessive flexibility beyond an optimal point degrades lift stability.

Bio-inspired geometries show moderate lift fluctuations compared to rigid wings.

Abstract

This study investigates the dynamics of passively morphing foils under accelerated plunging, establishing mechanistic links between transient kinematics, structural compliance, and aerodynamic performance. Two-way coupled simulations are performed for three wing geometries: a symmetric NACA0012 foil and two bio-inspired geometries based on falcon and owl wing sections, across non-dimensional bending rigidity values, chordwise flexible segment extents from the trailing-edge (25%, 50%, and 75%), and transition speed parameters. The present findings reveal that flexible trailing-edge configurations exhibit improved aerodynamic performance relative to stiffer foils, and the aerodynamic benefit of trailing-edge compliance is strongly influenced by wing geometry. A geometry-specific optimal bending stiffness exists beyond which additional flexibility degrades performance. The extent of the chordwise flexible segment critically governs the aeroelastic response. Whilst a 25% flexible segment produces behaviour indistinguishable from a rigid wing, extending flexibility to 75% of the chord induces highly unsteady lift fluctuations, particularly for the NACA0012 foil, for which the root-mean-square lift coefficient increases sharply. The bio-inspired foils, in contrast, exhibit a moderate reduction in root-mean-square lift coefficient for the 50% and 75% cases, reflecting the stabilising influence of their cambered geometry. Increasing the transition speed parameter monotonically amplifies trailing-edge deflection, strengthens the leading- and trailing-edge vortices, and intensifies the coupling between structural deformation and instantaneous lift. These findings provide new physical insight into bio-inspired propulsion and manoeuvring strategies, with implications for the design of passively adaptive lifting surfaces in unsteady environments.