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アイテム
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タンブリング平板の自由落下実験
https://jaxa.repo.nii.ac.jp/records/5431
https://jaxa.repo.nii.ac.jp/records/5431b5d16e1b-e459-4b41-af34-305d76149e03
名前 / ファイル | ライセンス | アクション |
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64303029.pdf (1.1 MB)
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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 | ||||||
タイトル | タンブリング平板の自由落下実験 | |||||
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 | Free-fall experiments on a tumbling plate | |||||
著者 |
川口, 大輔
× 川口, 大輔× 山内, 一樹× 舟木, 治郎× 平田, 勝哉× Kawaguchi, Daisuke× Yamauchi, Kazuki× Funaki, Jiro× Hirata, Katsuya |
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著者所属 | ||||||
同志社大学理工学部 | ||||||
著者所属 | ||||||
同志社大学理工学部 | ||||||
著者所属 | ||||||
同志社大学理工学部 | ||||||
著者所属 | ||||||
同志社大学理工学部 | ||||||
著者所属(英) | ||||||
en | ||||||
Faculty of Science and Engineering, Doshisha University | ||||||
著者所属(英) | ||||||
en | ||||||
Faculty of Science and Engineering, Doshisha University | ||||||
著者所属(英) | ||||||
en | ||||||
Faculty of Science and Engineering, Doshisha University | ||||||
著者所属(英) | ||||||
en | ||||||
Faculty of Science and Engineering, Doshisha University | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
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40回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2008論文集 en : JAXA Special Publication: Proceedings fo 40th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2008 巻 JAXA-SP-08-009, 発行日 2009-02-27 |
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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40回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2008. 会期: 2008年6月12日-6月13日. 会場: 東北大学片平キャンパス | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this study, we deal with the tumbling, which is a rotating motion with the axis perpendicular to the falling direction. Our purpose is to reveal the fundamental aerodynamic characteristics of the tumbling, experimentally. As the test plate, we consider a prism with a rectangular cross section with a depth-to-width ratio lambda of 0.3. As a result, the reduced terminal rotating rate omega(sup *), the lift coefficient C(sub L), the drag coefficient C(sub D) and the lift-to-drag ratio C(sub L)/C(sub D) are independent of the aspect ratio AR, when AR is greater than 10. As the inertia moment ratio I(sup *) increases from zero to 50, omega(sup *), C(sub L) and C(sub D) increase. However, omega(sup *), C(sub L) and C(sub D) become almost constant, if I(sup *) is greater than 50. We propose the empirical formulae to predict them. | |||||
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 | |||||
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: AA0064303029 | |||||
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-08-009 |