| Project/Area Number |
23654205
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| Research Category |
Grant-in-Aid for Challenging Exploratory Research
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| Allocation Type | Multi-year Fund |
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| Research Field |
Plasma science
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| Research Institution | Nippon Institute of Technology |
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Principal Investigator |
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| Co-Investigator(Kenkyū-buntansha) |
SATO Sugiya 日本工業大学, 工学部, 教授 (00286022)
TSUKABAYASHI Isao 日本工業大学, 工学部, 非常勤講師 (30049720)
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| Project Period (FY) |
2011 – 2013
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| Project Status |
Completed (Fiscal Year 2013)
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| Budget Amount *help |
¥3,640,000 (Direct Cost: ¥2,800,000、Indirect Cost: ¥840,000)
Fiscal Year 2013: ¥780,000 (Direct Cost: ¥600,000、Indirect Cost: ¥180,000)
Fiscal Year 2012: ¥1,040,000 (Direct Cost: ¥800,000、Indirect Cost: ¥240,000)
Fiscal Year 2011: ¥1,820,000 (Direct Cost: ¥1,400,000、Indirect Cost: ¥420,000)
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| Keywords | 大気圧プラズマ / 流体制御 / プラズマ支援燃焼 / エアロスパイク / マイクロ波 / 大気圧放電 |
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| Research Abstract |
The purpose of this study is to examine the effect by using the plasma source for the air-spike to control the heat load and the air resistance of the flight body or movable body. In addition, this plasma area is expanded to the plasma source by irradiating the micro wave. The influence of the interaction of plasma and the neutral-particle-flow to the effect of aerodynamic is examined. In this study, we developed an experimental system, and carried out the experiment separately for some themes. There is a need for further research to better understand an aerodynamics effect using a plasma air-spike.
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