The Effect of Voltage Frequency on Thrust Production of Multi-Electrode Plasma Actuator
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- MATSUNO Takashi
- Department of Mechanical and Aerospace Engineering, Tottori University
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- FUKUDA Ai
- Department of Mechanical and Aerospace Engineering, Tottori University
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- KAWAZOE Hiromitsu
- Department of Mechanical and Aerospace Engineering, Tottori University
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- NAKAI Kumi
- Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology
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- NISHIDA Hiroyuki
- Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology
Description
<p>The impact of the AC voltage frequency and the distance between the exposed electrodes (gap length) on the thrust characteristics of the trielectrode (TED) plasma actuator have been investigated experimentally. The induced body force of the serrated TED plasma actuator is investigated on quiescent air. With the experimental results, the physical factors that affect the growth of thrust is considered by estimating the total momentum of ions from the drift velocity. As a result, we found that the characteristics of the TED plasma actuator can be predicted from two physical parameters, the rate of the AC voltage change and the drift velocity of ions, which are both affected by the gap length and the AC voltage frequency.</p>
Journal
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- TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 16 (7), 582-587, 2018
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Keywords
Details 詳細情報について
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- CRID
- 1390845713016204288
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- NII Article ID
- 130007504913
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- ISSN
- 18840485
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- Text Lang
- en
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- Data Source
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- JaLC
- Crossref
- CiNii Articles
- KAKEN
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- Abstract License Flag
- Disallowed