Aerodynamic Forces on a Wing Surfing in a Two-dimensional Vortex Wake

TL;DR

This study investigates the aerodynamic forces on a wing surfing in an unsteady 2D vortex wake, combining wind tunnel experiments and theoretical analysis to understand lift fluctuations and wake interactions.

Contribution

It provides a detailed analysis of lift response and fluctuations on a wing in a vortex wake, with validated predictions based on unsteady aerodynamics and experimental data.

Findings

Lift response aligns with flow impingement patterns.

Cycle-averaged lift fluctuations scale with flapping parameters.

Classical unsteady aerodynamics effectively predict lift fluctuations.

Abstract

Inspired by the wake-surfing nature of animals, this study aims to understand the aerodynamic force variation on a wing surfing in an unsteady 2-D wake. Wind tunnel experiments were conducted using Particle Image Velocimetry (PIV) and force measurements with a fixed wing immersed in the wake of a pitching airfoil. The comparison between force and PIV measurements shows that the lift response of the surfing wing is aligned with the impingement of flow structures, and that the dependence of the cycle-averaged lift fluctuations on the upstream flapping kinematics can be scaled as a function of the reduced amplitude and reduced frequency of the flapping motion. Good collapse of the data is found, and deviations from scaling are explained in terms of the wake characteristics. The phase-resolved lift fluctuations on the vortical wake encountering can be effectively predicted using classic unsteady aerodynamics based on measured unsteady local flow conditions (instantaneous angle of attack and speed). The theoretical predictions compare well with direct force sensor measurements.