Superposition of AC-DBD plasma actuator outputs for three-dimensional disturbance production in shear flows

Journal Article (2023)
Author(s)

J. W. Kurelek (University of Waterloo, TU Delft - Aerodynamics)

M. Kotsonis (TU Delft - Aerodynamics)

S. Yarusevych (University of Waterloo, TU Delft - Aerodynamics)

Research Group
Aerodynamics
Copyright
© 2023 J.W. Kurelek, M. Kotsonis, S. Yarusevych
DOI related publication
https://doi.org/10.1007/s00348-023-03616-9
More Info
expand_more
Publication Year
2023
Language
English
Copyright
© 2023 J.W. Kurelek, M. Kotsonis, S. Yarusevych
Research Group
Aerodynamics
Issue number
4
Volume number
64
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Abstract

This investigation explores the utility of Alternating Current, Dielectric Barrier Discharge (AC-DBD) plasma actuators for producing three-dimensional disturbances of a desired spanwise wavelength via superposition. The technique utilizes two pairs of exposed and covered electrodes on a single dielectric layer arranged in streamwise succession. Two-dimensional forcing is achieved through operation of the upstream, spanwise uniform electrode pair, while three-dimensional forcing at a prescribed spanwise wavelength is attained by operating both electrode pairs simultaneously, with the downstream actuator spanwise modulating the upstream, two-dimensional output. The ability to produce disturbances of different spanwise wavelengths but with equal streamwise wavelength, frequency and total momentum is established through a combined characterization effort that considers quiescent and in-flow conditions. A demonstration of the technique in an exemplary wall-bounded shear flow, a laminar separation bubble, is provided, revealing spanwise wavelength dependent disturbance growth in the flow that could be exploited for performance gains in future flow control endeavours. Graphical abstract: [Figure not available: see fulltext.]