A study of plasma flow field around dielectric barrier discharge plasma actuator for high velocity flow condition
| Project/Area Number |
23860077
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| Research Category |
Grant-in-Aid for Research Activity Start-up
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| Allocation Type | Single-year Grants |
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| Research Field |
Aerospace engineering
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| Research Institution | Hokkaido University (2012)
Japan Aerospace Exploration Agency (2011) |
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Principal Investigator |
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| Project Period (FY) |
2011 – 2012
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| Project Status |
Completed (Fiscal Year 2012)
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| Budget Amount *help |
¥2,860,000 (Direct Cost: ¥2,200,000、Indirect Cost: ¥660,000)
Fiscal Year 2012: ¥1,430,000 (Direct Cost: ¥1,100,000、Indirect Cost: ¥330,000)
Fiscal Year 2011: ¥1,430,000 (Direct Cost: ¥1,100,000、Indirect Cost: ¥330,000)
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| Keywords | プラズマ流 / 数値解析 / 熱化学的非平衡流 / 熱化学非平衡 |
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| Research Abstract |
Final goal of the present research is to develop a high-performance plasma actuator which is applicable for a condition of high-velocity flow. In the present study, to describe plasma flow behavior and potential drop by cathode sheath, numerical simulation models of plasma flow generated by dielectric barrier discharge plasma actuator and plasma near an electrode has been suggested and developed.
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Report
(3 results)
Research Products
(2 results)
