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Enhancing Jet Velocity and Power Conversion Efficiency of Piezoelectric Synthetic Jet Actuators

Gungordu, Baris; Jabbal, Mark; Popov, Atanas A.

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Authors

Baris Gungordu

MARK JABBAL Mark.Jabbal@nottingham.ac.uk
Associate Professor

ATANAS POPOV ATANAS.POPOV@NOTTINGHAM.AC.UK
Professor of Engineering Dynamics



Abstract

The present work discusses an experimental investigation into the effect of piezoceramic employed to drive a synthetic jet actuator into a quiescent flow. The electromechanical coupling ratio of polycrystalline piezoceramics, lead zirconate–titanate 5A/5H (PZT-5A/5H), conventionally used in synthetic jet actuators, is inherently low. Therefore, this study aims to investigate using more electromechanically efficient piezoceramics, such as single-crystal, lead magnesium niobate–lead titanate (PMN-PT). In addition, two different orifice-diaphragm configurations of synthetic jet actuators, opposite and adjacent, are tested. It is identified that PMN-PT piezoceramic promotes three times higher transverse diaphragm displacement and two times more peak jet velocity compared to the PZT-5A piezoelectric actuator for the same input diaphragm voltage. A peak exit jet velocity of 99.5  m⋅s−1 was obtained at 40 V of peak supply voltage, which can be classified as a low voltage supply compared to other studies in the literature that obtained similar exit jet velocity. Also, a power conversion efficiency of 72% was achieved, corresponding to the Helmholtz resonance frequency. A new figure-of-merit, momentum coefficient per power consumption, is defined to evaluate the potential impact for full-scale implementation. A state-of-the-art value of 0.09  MW−1 is achieved.

Journal Article Type Article
Acceptance Date Jun 22, 2023
Online Publication Date Jul 13, 2023
Publication Date 2023-10
Deposit Date Jul 18, 2023
Publicly Available Date Jul 19, 2023
Journal AIAA Journal
Print ISSN 0001-1452
Electronic ISSN 1533-385X
Publisher American Institute of Aeronautics and Astronautics
Peer Reviewed Peer Reviewed
Volume 61
Issue 10
Pages 4321–4331
DOI https://doi.org/10.2514/1.j062930
Keywords Aerospace Engineering
Public URL https://nottingham-repository.worktribe.com/output/23210959
Publisher URL https://arc.aiaa.org/doi/10.2514/1.J062930

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