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シャトルコックの空力特性
https://jaxa.repo.nii.ac.jp/records/4726
https://jaxa.repo.nii.ac.jp/records/4726ab88b3b7-e10f-4dbc-9390-ccb5f22784f0
名前 / ファイル | ライセンス | アクション |
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64967019.pdf (1.4 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 | シャトルコックの空力特性 | |||||
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 | Aerodynamic Characteristics of Badminton Shuttlecocks | |||||
著者 |
板倉, 嘉哉
× 板倉, 嘉哉× 古村, 文音× Itakura, Yoshiya× Komura, Ayane |
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著者所属 | ||||||
千葉大学教育学部 | ||||||
著者所属 | ||||||
千葉大学教育学部 | ||||||
著者所属(英) | ||||||
en | ||||||
Chiba University, Faculty of Education | ||||||
著者所属(英) | ||||||
en | ||||||
Chiba University, Faculty of Education | ||||||
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42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2010 論文集 en : JAXA Special Publication: Proceedings of 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010 巻 JAXA-SP-10-012, 発行日 2011-02-28 |
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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42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2010 (2010年6月24日-25日. 米子コンベンションセンター BiG SHiP) | |||||
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 | 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010 (June 24-25, 2010. Yonago Convention Center BiG SHiP), Yonago, Tottori Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | As you know, badminton is a well-known sport that young and old can play. The reason why everyone can enjoy is in strong deceleration of the shuttlecock, however, its aerodynamic characteristics have not been elucidated well. In the present work, using a low speed wind tunnel, effects of the flow passing through the slot located at leg part of the feather on the aerodynamic characteristics are demonstrated. Aerodynamic force and moment acting on the shuttlecock and flow field structure in the shuttlecock are measured in angle of attack rage from -10 to +10 degrees. Typical two observed aerodynamic characteristics are significant reduction of the drag without the slot and nonliner lift characteristics (N shaped change) around angle of attack zero. This lift behavior is remarkable result we have never seen. | |||||
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: AA0064967019 | |||||
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-10-012 |