TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
Online ISSN : 1884-0485
ISSN-L : 1884-0485
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Computational Study of Discharge Process in Plasma Actuator for Enhanced Electrohydrodynamic Force Generation toward Low-Voltage Operation
Shintaro SATOHaruki FURUKAWAMasayuki TAKAHASHINaofumi OHNISHI
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2021 年 19 巻 1 号 p. 17-23

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Numerical simulations of discharge process in two types of actuator modules were conducted to obtain better understanding of the process of electrohydrodynamic (EHD) force generation toward the low-voltage operation. The charge accumulated on the dielectric surface can be absorbed by the additional downstream-side exposed electrode, which is a component of the adjacent actuator module in a multi-module plasma actuator, when positively-DC-biased negative polarity pulses are applied. The elimination of the surface charge results in EHD force enhancement. The enhanced EHD force is also obtained when a negatively-DC-biased positive polarity pulses are applied. The applied voltage affects the surface charge profile and EHD force enhancement by the downstream-side exposed electrode. Under our simulation condition, the positively-DC-biased negative pulses obtain larger enhancement of EHD force compared to that obtained by the negatively-DC-biased positive pulses.

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© 2021 The Japan Society for Aeronautical and Space Sciences
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