Experimental study of flutter electric power generator by pulse detonation engine
| Project/Area Number |
21560823
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| Research Category |
Grant-in-Aid for Scientific Research (C)
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| Allocation Type | Single-year Grants |
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| Section | 一般 |
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| Research Field |
Aerospace engineering
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| Research Institution | Oita National College of Technology |
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Principal Investigator |
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| Project Period (FY) |
2009 – 2011
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| Project Status |
Completed (Fiscal Year 2011)
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| Budget Amount *help |
¥4,680,000 (Direct Cost: ¥3,600,000、Indirect Cost: ¥1,080,000)
Fiscal Year 2011: ¥780,000 (Direct Cost: ¥600,000、Indirect Cost: ¥180,000)
Fiscal Year 2010: ¥2,080,000 (Direct Cost: ¥1,600,000、Indirect Cost: ¥480,000)
Fiscal Year 2009: ¥1,820,000 (Direct Cost: ¥1,400,000、Indirect Cost: ¥420,000)
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| Keywords | デトネーション / PDE / 燃焼 / 熱流体計測 / Busemann翼 / インパルス / 発電 / 航空宇宙工学 / CFD |
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| Research Abstract |
We carried out the PDE experiments using a cylindrical tube, whose inner diameter and length were respectively 30 mm and 1200 mm. The impulse of cylindrical flying body is over twice as large as one of ballistic pendulum method. Also, the PDE combustor was operated at 1 Hz by magnetic valve system. To evaluate cancelation of the wave-making resistance of the double Busemann wings, we observed the shulieren photograph of the flow in supersonic flow with Mach number 2.Consequently, the elements of PDE electric power generation are successfully established.
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Report
(4 results)
Research Products
(24 results)
