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3次元磁場配位による磁気シールド効果への影響
https://jaxa.repo.nii.ac.jp/records/3841
https://jaxa.repo.nii.ac.jp/records/384146c93bda-c5a8-4131-9148-60ca7126d26d
名前 / ファイル | ライセンス | アクション |
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AA1530023006.pdf (7.5 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-04-28 | |||||
タイトル | ||||||
タイトル | 3次元磁場配位による磁気シールド効果への影響 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Influence of 3-Dimentional Magnetic Configuration on Electrodynamic Effect | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Incorrect title: Influence of 3-Dimentional Magnetic Configuration on Electrodynamic Effeect | |||||
著者 |
永田, 靖典
× 永田, 靖典× 山田, 和彦× 安部, 隆士× Nagata, Yasunori× Yamada, Kazuhiko× Abe, Takashi |
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著者所属 | ||||||
岡山大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Okayama University | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
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: 第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム論文集 en : JAXA Special Publication: Proceedings of the 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium 巻 JAXA-SP-14-010, p. 29-34, 発行日 2015-03-25 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム (2014年7月3日-4日. 弘前文化センター), 弘前市, 青森県 | |||||
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 | 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium (July 3-4, 2014. Hirosaki Bunka Center), Hirosaki, Aomori, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In the electrodynamic flow control, weakly-ionized plasma flow behind the strong shock wave could be controlled by the applied magnetic field around a reentry vehicle. To control the field, a very strong magnetic field is required and it could be applied by the superconducting magnet. However, the superconducting magnet system, including a superconducting magnetic coil, an electrical current source, a cooling mechanism, and refrigerant, is large and heavy for a reentry capsule such as the Hayabusa capsule. Thus, in this study, to avoid the use of the superconducting magnet, the electrodynamic effect by multiple weaker magnets such as permanent magnets is numerically investigated. According to the MHD simulation, the drag force can be also enhanced by the multiple magnets and it is clearly affected by the magnet array. Especially, the aerodynamic force part is significantly affected because the wall pressure is varied near the magnet. Therefore, the multiple magnet array might be as effective as the strong single magnet for the electrodynamic flow control. | |||||
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: AA1530023006 | |||||
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-14-010 |