Dr MARK JABBAL Mark.Jabbal@nottingham.ac.uk
ASSOCIATE PROFESSOR
Towards the noise reduction of piezoelectrical-driven synthetic jet actuators
Jabbal, Mark; Jeyalingam, Jonne
Authors
Jonne Jeyalingam
Abstract
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.
Citation
Jabbal, M., & Jeyalingam, J. (2017). Towards the noise reduction of piezoelectrical-driven synthetic jet actuators. Sensors and Actuators A: Physical, 266, https://doi.org/10.1016/j.sna.2017.09.036
Journal Article Type | Article |
---|---|
Acceptance Date | Sep 20, 2017 |
Online Publication Date | Sep 22, 2017 |
Publication Date | Oct 15, 2017 |
Deposit Date | Sep 29, 2017 |
Publicly Available Date | Sep 23, 2018 |
Journal | Sensors and Actuators A: Physical |
Print ISSN | 0924-4247 |
Electronic ISSN | 1873-3069 |
Publisher | Elsevier |
Peer Reviewed | Peer Reviewed |
Volume | 266 |
DOI | https://doi.org/10.1016/j.sna.2017.09.036 |
Keywords | Synthetic jet actuator; Noise reduction; Dipole; Lobed orifice |
Public URL | https://nottingham-repository.worktribe.com/output/887785 |
Publisher URL | http://www.sciencedirect.com/science/article/pii/S0924424717301929 |
Contract Date | Sep 29, 2017 |
Files
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Copyright Statement
Copyright information regarding this work can be found at the following address: http://creativecommons.org/licenses/by-nc-nd/4.0
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