Effect of combined heaving and pitching on propulsion of single and tandem flapping foils

TL;DR

This paper investigates how combined heaving and pitching motions affect the propulsion of single and tandem flapping foils through numerical simulations, emphasizing wake interactions, pressure effects, and three-dimensional dynamics.

Contribution

It provides a systematic analysis of kinematic effects on thrust, highlighting the role of wake pressure and three-dimensional effects in flapping foil propulsion.

Findings

Propulsive performance depends on wake-foil interaction and timing.

Pressure in the wake significantly influences thrust beyond jet formation.

Three-dimensional effects are notable at large amplitude flapping.

Abstract

In this study, we present two and three-dimensional numerical investigation to understand the combined effects of the non-dimensional heave amplitude varying from 0 to 1 and the pitch amplitude ranging from 0 to 30 on the propulsive performance for a single and tandem foil system at Reynolds number 1100 and reduced frequency 0.2. We initially present a systematic analysis on the thrust generation due to the kinematic parameters for a single foil. The significance of effective angle of attack and the projected area of the foil has been emphasized in explaining the dynamics of lift and drag forces and their relationship with the propulsion. We next investigate the relation between the streamwise gap and kinematic parameters on propulsion for the tandem foil system. We show that the propulsive performance strongly depends on the upstream wake interacting with the downstream foil, and the timing of the interaction due to the gap between the foils. Through a control volume analysis, the time-averaged pressure and streamwise velocity have been investigated to explain the effect of kinematic parameters on the hydrodynamic forces. Typically in the literature, the formation of jet in the wake has been attributed to thrust generation. However, in this study, we emphasize and show the significance of the time-averaged pressure in the wake apart from the streamwise velocity (jet) for predicting the thrust forces. The study is concluded with a three-dimensional demonstration of the tandem foils to understand the possible three-dimensional effects due to the large amplitude flapping and wake-foil interaction.