Towards the noise reduction of piezoelectrical-driven synthetic jet actuators

This work details an experimental investigation aimed at reducing the noise output of piezoelectrical-driven synthetic jet actuators while minimising peak jet velocity reduction. The study considers double-chamber actuator for anti-phase noise suppression and lobed orifice as a method to enhance jet...

Full description

Bibliographic Details
Main Authors: Jabbal, Mark, Jeyalingam, Jonne
Format: Article
Published: Elsevier 2017
Subjects:
Online Access:https://eprints.nottingham.ac.uk/46743/
_version_ 1848797390047281152
author Jabbal, Mark
Jeyalingam, Jonne
author_facet Jabbal, Mark
Jeyalingam, Jonne
author_sort Jabbal, Mark
building Nottingham Research Data Repository
collection Online Access
description This work details an experimental investigation aimed at reducing the noise output of piezoelectrical-driven synthetic jet actuators while minimising peak jet velocity reduction. The study considers double-chamber actuator for anti-phase noise suppression and lobed orifice as a method to enhance jet turbulent mixing to suppress jet noise. The study involved the design, manufacture and bench test of interchangeable actuator hardware. Hot-wire anemometry and microphone recordings were employed to acquire velocity and sound pressure level measurements respectively across a range of excitation frequencies for a fixed diaphragm clamping and input voltage. The data analysis indicated a 26% noise reduction (16 dB) from operating a single-chamber, round orifice actuator to a double-chamber, lobed orifice one at the synthetic jet resonant frequency. Results also showed there was a small reduction in peak jet velocity of 7% (∼3 m/s) between these two cases based on orifices of the same discharge area. The electrical-to-fluidic power conversion efficiency of the double-chamber actuator was found to be 15% for both orifice types at the resonant frequency; approximately double the efficiency of a single-chamber actuator.
first_indexed 2025-11-14T20:03:07Z
format Article
id nottingham-46743
institution University of Nottingham Malaysia Campus
institution_category Local University
last_indexed 2025-11-14T20:03:07Z
publishDate 2017
publisher Elsevier
recordtype eprints
repository_type Digital Repository
spelling nottingham-467432020-05-04T19:12:37Z https://eprints.nottingham.ac.uk/46743/ Towards the noise reduction of piezoelectrical-driven synthetic jet actuators Jabbal, Mark Jeyalingam, Jonne This work details an experimental investigation aimed at reducing the noise output of piezoelectrical-driven synthetic jet actuators while minimising peak jet velocity reduction. The study considers double-chamber actuator for anti-phase noise suppression and lobed orifice as a method to enhance jet turbulent mixing to suppress jet noise. The study involved the design, manufacture and bench test of interchangeable actuator hardware. Hot-wire anemometry and microphone recordings were employed to acquire velocity and sound pressure level measurements respectively across a range of excitation frequencies for a fixed diaphragm clamping and input voltage. The data analysis indicated a 26% noise reduction (16 dB) from operating a single-chamber, round orifice actuator to a double-chamber, lobed orifice one at the synthetic jet resonant frequency. Results also showed there was a small reduction in peak jet velocity of 7% (∼3 m/s) between these two cases based on orifices of the same discharge area. The electrical-to-fluidic power conversion efficiency of the double-chamber actuator was found to be 15% for both orifice types at the resonant frequency; approximately double the efficiency of a single-chamber actuator. Elsevier 2017-10-15 Article PeerReviewed Jabbal, Mark and Jeyalingam, Jonne (2017) Towards the noise reduction of piezoelectrical-driven synthetic jet actuators. Sensors and Actuators A: Physical, 266 . pp. 273-284. ISSN 0924-4247 Synthetic jet actuator; Noise reduction; Dipole; Lobed orifice http://www.sciencedirect.com/science/article/pii/S0924424717301929 doi:10.1016/j.sna.2017.09.036 doi:10.1016/j.sna.2017.09.036
spellingShingle Synthetic jet actuator; Noise reduction; Dipole; Lobed orifice
Jabbal, Mark
Jeyalingam, Jonne
Towards the noise reduction of piezoelectrical-driven synthetic jet actuators
title Towards the noise reduction of piezoelectrical-driven synthetic jet actuators
title_full Towards the noise reduction of piezoelectrical-driven synthetic jet actuators
title_fullStr Towards the noise reduction of piezoelectrical-driven synthetic jet actuators
title_full_unstemmed Towards the noise reduction of piezoelectrical-driven synthetic jet actuators
title_short Towards the noise reduction of piezoelectrical-driven synthetic jet actuators
title_sort towards the noise reduction of piezoelectrical-driven synthetic jet actuators
topic Synthetic jet actuator; Noise reduction; Dipole; Lobed orifice
url https://eprints.nottingham.ac.uk/46743/
https://eprints.nottingham.ac.uk/46743/
https://eprints.nottingham.ac.uk/46743/