Atmospheric plasma actuators for aeroacoustic applications

Xun Huang; Sammie Chan; Xin Zhang

doi:10.1109/TPS.2007.896781

Atmospheric plasma actuators for aeroacoustic applications

Xun Huang^*, Sammie Chan, Xin Zhang

^*Corresponding author for this work

Research output: Contribution to journal › Journal Article › peer-review

32 Citations (Scopus)

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.

Original language	English
Pages (from-to)	693-695
Number of pages	3
Journal	IEEE Transactions on Plasma Science
Volume	35
Issue number	3
DOIs	https://doi.org/10.1109/TPS.2007.896781
Publication status	Published - Jun 2007
Externally published	Yes

Keywords

Aeroacoustics
Atmospheric pressure glow discharges
Flow control

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10.1109/TPS.2007.896781

Cite this

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title = "Atmospheric plasma actuators for aeroacoustic applications",

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.",

keywords = "Aeroacoustics, Atmospheric pressure glow discharges, Flow control",

author = "Xun Huang and Sammie Chan and Xin Zhang",

year = "2007",

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doi = "10.1109/TPS.2007.896781",

language = "English",

volume = "35",

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AU - Huang, Xun

AU - Chan, Sammie

AU - Zhang, Xin

PY - 2007/6

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N2 - 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.

AB - 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.

KW - Aeroacoustics

KW - Atmospheric pressure glow discharges

KW - Flow control

UR - https://www.webofscience.com/wos/woscc/full-record/WOS:000247352900024

UR - https://openalex.org/W2106133195

UR - https://www.scopus.com/pages/publications/34347370220

U2 - 10.1109/TPS.2007.896781

DO - 10.1109/TPS.2007.896781

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SP - 693

EP - 695

JO - IEEE Transactions on Plasma Science

JF - IEEE Transactions on Plasma Science

IS - 3

ER -

Atmospheric plasma actuators for aeroacoustic applications

Abstract

Keywords

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