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Numerical Investigation on Voltage Waveform Composed of Gradual and Steep Slope for Performance Improvement of Plasma Actuator
AIAA 2018-2045
Session: Plasma Flow Control III
Published Online:7 Jan 2018https://doi.org/10.2514/6.2018-2045
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- 1 Jan 2020 | TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, Vol. 18, No. 6
- 7 Nov 2019 | Journal of Applied Physics, Vol. 126, No. 17
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8–12 January 2018
Kissimmee, Florida
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Copyright © 2018 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
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