2011 Fiscal Year Final Research Report
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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| 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 |
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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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