TY - GEN
T1 - Inuence of voltage waveform on electrohydrodynamic force in a dielectric-barrier-discharge plasma actuator
AU - Sato, Shintaro
AU - Ohnishi, Naofumi
N1 - Funding Information:
The computations in this work were performed on Silicon Graphics International (SGI) Altix UV1000 at Advanced Fluid Information Research Center, Institute of Fluid Science, Tohoku University and FUJITSU Supercomputer PRIMEHPC FX100 at Japan Aerospace Exploration Agency (JAXA). The present work was supported in part through the Program for Leading Graduate Schools, “Inter-Graduate School Doctoral Degree Program on Global Safety” by the Ministry of Education, Culture, Sports, Science and Technology.
Publisher Copyright:
© 2017 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2017
Y1 - 2017
N2 - Two-dimensional numerical simulations of the discharge process in a dielectric-barrier-discharge (DBD) plasma actuator were carried out toward the detailed understanding of the electrohydrodynamic (EHD) force characteristics and proposal of the suitable voltage input in view of the EHD force production. In this study, the inuence of the voltage amplitude on the discharge regime and EHD force is investigated when a triangle voltage waveform is applied. The streamer discharges are obtained with high amplitude in the positive-going phase in a voltage cycle, whereas no streamer propagation is observed with low amplitude. In the negative-going phase, the frequency of the repetitive current pulses decreases with decreasing the amplitude because the voltage slope decreases with the same voltage frequency. The charge on the dielectric surface has a quite important role in the discharge inception voltage; the discharge is ignited in the negative-going phase even though the applied voltage is positive. The time-averaged EHD force increases with increasing the voltage amplitude and can be divided into two-power law regions. The increment rate of the EHD force changes sharply when the discharge regime transits to the streamer discharge. A wall jet induced by the DBD plasma actuator in quiescent air is reproduced by using the EHD force distribution obtained from the discharge simulation, which shows qualitatively agreement with experimental result.
AB - Two-dimensional numerical simulations of the discharge process in a dielectric-barrier-discharge (DBD) plasma actuator were carried out toward the detailed understanding of the electrohydrodynamic (EHD) force characteristics and proposal of the suitable voltage input in view of the EHD force production. In this study, the inuence of the voltage amplitude on the discharge regime and EHD force is investigated when a triangle voltage waveform is applied. The streamer discharges are obtained with high amplitude in the positive-going phase in a voltage cycle, whereas no streamer propagation is observed with low amplitude. In the negative-going phase, the frequency of the repetitive current pulses decreases with decreasing the amplitude because the voltage slope decreases with the same voltage frequency. The charge on the dielectric surface has a quite important role in the discharge inception voltage; the discharge is ignited in the negative-going phase even though the applied voltage is positive. The time-averaged EHD force increases with increasing the voltage amplitude and can be divided into two-power law regions. The increment rate of the EHD force changes sharply when the discharge regime transits to the streamer discharge. A wall jet induced by the DBD plasma actuator in quiescent air is reproduced by using the EHD force distribution obtained from the discharge simulation, which shows qualitatively agreement with experimental result.
UR - http://www.scopus.com/inward/record.url?scp=85017211907&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85017211907&partnerID=8YFLogxK
U2 - 10.2514/6.2017-1804
DO - 10.2514/6.2017-1804
M3 - Conference contribution
AN - SCOPUS:85017211907
T3 - AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting
BT - AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 55th AIAA Aerospace Sciences Meeting
Y2 - 9 January 2017 through 13 January 2017
ER -