Separation control using DBD plasma actuators: Designs for thrust enhancement

S. Guo, D. Burman, D. Poon, M. Mamunuru, T. Simon, D. Ernie, U. Kortshagen

Research output: Chapter in Book/Report/Conference proceedingConference contribution

4 Scopus citations

Abstract

New plasma actuators designed for enhanced flow control authority are made by increasing asymmetry of thrust during the Dielectric Barrier Discharge (DBD) actuation cycle. This is done by a change of circuitry and by adding a semi-conductive layer on top of the dielectric surface, both for effective discharging of the dielectric. Compared to the conventional sinusoidal waveform driven plasma actuators, the new designs increases the thrust by about 70% when operating at the same frequency and voltage. Measurements indicate that increases in conductivity of the semi-conductive layer lead to increasingly higher thrust.

Original languageEnglish (US)
Title of host publication39th AIAA Fluid Dynamics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781563479755
DOIs
StatePublished - Jan 1 2009

Publication series

Name39th AIAA Fluid Dynamics Conference

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