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- KIHARA Hisashi
- Department of Aeronautics and Astronautics, Kyushu University
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- HATANO Masaki
- Department of Aeronautics and Astronautics, Kyushu University
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- NAKIYAMA Noriyuki
- Department of Aeronautics and Astronautics, Kyushu University
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- ABE Ken-ichi
- Department of Aeronautics and Astronautics, Kyushu University
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- NISHIDA Michio
- Department of Aerospace Systems Engineering, Sojo University
この論文をさがす
抄録
Spallation particles emitted from an ablating test model mounted in a supersonic arc-heated air flow was investigated experimentally and computationally. Emission spectra of CN violet band and C2 swan band, that were attributed to spallation particles, were identified not only inside the shock layer of the ablator but also outside of it. 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 front surface of the ablator.
収録刊行物
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- TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 49 (164), 65-70, 2006
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390282679057537920
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- NII論文ID
- 10019370861
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- NII書誌ID
- AA0086707X
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- ISSN
- 21894205
- 05493811
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- NDL書誌ID
- 8018464
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- 本文言語コード
- en
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- データソース種別
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可