# Variable thrust and high efficiency propulsion with oscillating foils at   high Reynolds numbers

**Authors:** Mukul Dave (1), Arianne Spaulding, Jennifer A. Franck (1) ((1), University of Wisconsin-Madison)

arXiv: 1907.01097 · 2020-09-24

## TL;DR

This study investigates the propulsion efficiency and wake dynamics of oscillating foils at high Reynolds numbers, revealing how kinematic adjustments can optimize thrust and efficiency for small to medium surface vessels.

## Contribution

It provides a detailed characterization of high Reynolds number oscillating foil propulsion, including flow regimes and vortex wake structures, using URANS simulations.

## Key findings

- Maximum thrust coefficient of 8.2 at high heave amplitude
- Propulsive efficiency reaches up to 75% at certain Strouhal numbers
- Identification of flow regimes based on vortex wake and performance

## Abstract

Bio-inspired oscillatory foil propulsion has the ability to traverse various propulsive modes by dynamically changing the foil's heave and pitch kinematics. This research characterizes the propulsion properties and wake dynamics of a symmetric oscillating foil, specifically targeting the high Reynolds number operation of small to medium surface vessels whose propulsive specifications have a broad range of loads and speeds. An unsteady Reynolds-averaged Navier-Stokes (URANS) solver with a k-$\omega$ SST turbulence model is used to sweep through pitch amplitude and frequency at two heave amplitudes of $h_0/c=1$ and $h_0/c=2$ at $Re=10^6$. At $h_0/c=2$, the maximum thrust coefficient is $C_T=8.2$ due to the large intercepted flow area of the foil, whereas at a decreased Strouhal number the thrust coefficient decreases and the maximum propulsive efficiency reaches 75%. Results illustrate the kinematics required to transition between the high-efficiency and high-thrust regimes at high Reynolds number and the resulting changes to the vortex wake structure. The unsteady vortex dynamics throughout the heave-pitch cycle strongly influence the characterization of thrust and propulsive efficiency, and are classified into flow regimes based on performance and vortex structure.

## Full text

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## Figures

47 figures with captions in the complete paper: https://tomesphere.com/paper/1907.01097/full.md

## References

37 references — full list in the complete paper: https://tomesphere.com/paper/1907.01097/full.md

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Source: https://tomesphere.com/paper/1907.01097