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Bow-Shock Instability around an Edged Ballistic Object in a Low-Gamma Gas
https://jaxa.repo.nii.ac.jp/records/4140
https://jaxa.repo.nii.ac.jp/records/414043683c27-ab9f-4085-b391-d4addd489016
名前 / ファイル | ライセンス | アクション |
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62070032.pdf (260.0 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Bow-Shock Instability around an Edged Ballistic Object in a Low-Gamma Gas | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | bow-shock instability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | discontinuous Galerkin method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ballistic range | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
著者 |
佐藤, 陽介
× 佐藤, 陽介× 保江, かな子× 菊池, 崇将× 大谷, 清伸× 大西, 直文× Sato, Yosuke× Yasue, Kanako× Kikuchi, Takamasa× Ohtani, Kiyonobu× Ohnishi, Naofumi |
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著者所属 | ||||||
東北大学大学院工学研究科航空宇宙工学専攻 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発本部(JAXA) | ||||||
著者所属 | ||||||
東北大学流体科学研究所 | ||||||
著者所属 | ||||||
東北大学流体科学研究所 | ||||||
著者所属 | ||||||
東北大学大学院工学研究科航空宇宙工学専攻 | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Aerospace Engineering, Graduate School of Engineering, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Fluid Science, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Fluid Science, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Aerospace Engineering, Graduate School of Engineering, Tohoku University | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料 en : JAXA Special Publication 巻 JAXA-SP-13-001E, p. 367-373, 発行日 2013-11-30 |
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会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 5th Symposium on Integrating CFD and Experiments in Aerodynamics (October 3-5, 2012, Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)), Chofu, Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Bow-shock instability observed in a low gamma flow was investigated by three-dimensional numerical simulation with a circular cone. We designed experiments based on the numerical results in order to validate our numerical results and demonstrate that bow shock wave is unstable in a low gamma gas with the edged body. The experimental results show that bow shock becomes unsteady and unstable in the proposed condition, and our numerical prediction was validated. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0062070032 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-13-001E |