TY - GEN
T1 - Performance improvement of dielectric barrier discharge plasma actuator with two-stroke cycle operation
AU - Sato, Shintaro
AU - Enokido, Tomoki
AU - Ashikawa, Kenichiro
AU - Ohnishi, Naofumi
N1 - Publisher Copyright:
© 2021, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2021
Y1 - 2021
N2 - Electrical and mechanical characteristics of a dielectric-barrier-discharge (DBD) plasma actuator driven by two-stroke cycle operation were experimentally investigated to obtain an insight into the performance improvement of ionic wind generation. The DC-biased repetitive pulses obtained by a DC power supply and SiC-MOSFETs are applied to the DBD plasma actuator for charged particle generation. The other DC voltage is applied to a downstream exposed electrode for the charged particle acceleration. The particle image velocimetry measurement reveals that the amplitude of the DC voltage used for charged particle generation has a small impact on the wall jet generation in this study. Contrary to this, the DC voltage used for charged particle acceleration increases both the peak velocity and thickness of the wall jet. Although the increment rate of the thrust generated by the DBD plasma actuator to the amplitude of DC voltage becomes lower when the distance between the exposed electrodes becomes larger, the threshold value of the spark discharge becomes large. As a result, the maximum value of the thrust for the case of the long distance between the electrodes is larger than that of the shorter distance case.
AB - Electrical and mechanical characteristics of a dielectric-barrier-discharge (DBD) plasma actuator driven by two-stroke cycle operation were experimentally investigated to obtain an insight into the performance improvement of ionic wind generation. The DC-biased repetitive pulses obtained by a DC power supply and SiC-MOSFETs are applied to the DBD plasma actuator for charged particle generation. The other DC voltage is applied to a downstream exposed electrode for the charged particle acceleration. The particle image velocimetry measurement reveals that the amplitude of the DC voltage used for charged particle generation has a small impact on the wall jet generation in this study. Contrary to this, the DC voltage used for charged particle acceleration increases both the peak velocity and thickness of the wall jet. Although the increment rate of the thrust generated by the DBD plasma actuator to the amplitude of DC voltage becomes lower when the distance between the exposed electrodes becomes larger, the threshold value of the spark discharge becomes large. As a result, the maximum value of the thrust for the case of the long distance between the electrodes is larger than that of the shorter distance case.
UR - http://www.scopus.com/inward/record.url?scp=85099902865&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85099902865&partnerID=8YFLogxK
U2 - 10.2514/6.2021-1492
DO - 10.2514/6.2021-1492
M3 - Conference contribution
AN - SCOPUS:85099902865
SN - 9781624106095
T3 - AIAA Scitech 2021 Forum
SP - 1
EP - 7
BT - AIAA Scitech 2021 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2021
Y2 - 11 January 2021 through 15 January 2021
ER -