| Project/Area Number |
17560702
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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 | Sojo University |
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Principal Investigator |
NISHIDA Michio Sojo University, Faculty of Engineering, Professor (10025968)
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| Co-Investigator(Kenkyū-buntansha) |
NAGAYAMA Kunihito Kyushu University, College of Engineering, Professor (20040446)
KIHARA Hisashi Kyushu University, College of Engineering, Research Associate (60243911)
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| Project Period (FY) |
2005 – 2007
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| Project Status |
Completed (Fiscal Year 2007)
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| Budget Amount *help |
¥3,600,000 (Direct Cost: ¥3,300,000、Indirect Cost: ¥300,000)
Fiscal Year 2007: ¥1,300,000 (Direct Cost: ¥1,000,000、Indirect Cost: ¥300,000)
Fiscal Year 2006: ¥800,000 (Direct Cost: ¥800,000)
Fiscal Year 2005: ¥1,500,000 (Direct Cost: ¥1,500,000)
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| Keywords | Aerospace Engineering / Spallation / Ablation / Atmospheric Entry into a Planet |
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| Research Abstract |
Spallation particles emitted from an ablating model mounted in a supersonic arc-heated air flow was investigated experimentally and computationally. Emission spectra of CN violet band and C_2 swan band, which were attributed to spallation particles, were identified not only inside the shock layer of the ablator but also outside of it.
The picture of spallation particles was tried to be taken, by using an ordinary camera. The picture captured the melted glass fiber ejected from the front surface. In addition, the picture by a high-speed camera also identified the flight of spallation particles.
Since the evidence of the presence of spallation particles was found, the trajectory of a spallation particle was simulated to reveal the conditions for the flight to the upstream of the shock layer. The simulation was made by ejecting a solid particle at various speeds from the surface of the ablator.
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