Atmospheric plasma actuators for aeroacoustic applications
Atmospheric plasma actuators for aeroacoustic applications
A plasma actuator operating in atmospheric air was applied to attenuate low-speed cavity flow-induced tones. It demonstrated the working effect of glow discharges for aeroacoustic applications. The details of the overall system were summarized. To improve the power efficiency, several plasma driving signals were tested on a real-time system. The corresponding results were discussed in this paper.
693-695
Huang, Xun
44c6d7c9-07ca-436c-9cbe-1ba9a2f834f9
Chan, Sammie
5d167d44-fa65-4b60-a260-e9d49a7bcf87
Zhang, Xin
3056a795-80f7-4bbd-9c75-ecbc93085421
June 2007
Huang, Xun
44c6d7c9-07ca-436c-9cbe-1ba9a2f834f9
Chan, Sammie
5d167d44-fa65-4b60-a260-e9d49a7bcf87
Zhang, Xin
3056a795-80f7-4bbd-9c75-ecbc93085421
Huang, Xun, Chan, Sammie and Zhang, Xin
(2007)
Atmospheric plasma actuators for aeroacoustic applications.
IEEE Transactions on Plasma Science, 35 (3), .
(doi:10.1109/TPS.2007.896781).
Abstract
A plasma actuator operating in atmospheric air was applied to attenuate low-speed cavity flow-induced tones. It demonstrated the working effect of glow discharges for aeroacoustic applications. The details of the overall system were summarized. To improve the power efficiency, several plasma driving signals were tested on a real-time system. The corresponding results were discussed in this paper.
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Published date: June 2007
Organisations:
Aerodynamics & Flight Mechanics
Identifiers
Local EPrints ID: 46652
URI: http://eprints.soton.ac.uk/id/eprint/46652
ISSN: 0093-3813
PURE UUID: a266bcda-b30c-4507-8f92-856b006f3197
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Date deposited: 13 Jul 2007
Last modified: 15 Mar 2024 09:25
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Author:
Xun Huang
Author:
Sammie Chan
Author:
Xin Zhang
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