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垂直風洞によるバドミントン用シャトルコックの静的空力特性の解明
https://jaxa.repo.nii.ac.jp/records/48382
https://jaxa.repo.nii.ac.jp/records/48382ae2e364c-041d-4d1f-9e98-410cdcc7e9cd
名前 / ファイル | ライセンス | アクション |
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AA2130027009.pdf (2.0 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2022-02-14 | |||||
タイトル | ||||||
タイトル | 垂直風洞によるバドミントン用シャトルコックの静的空力特性の解明 | |||||
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 | Experimental Study on Static Aerodynamic Characteristics of Badminton Shuttlecocks with Vertical Wind Tunnel | |||||
著者 |
板倉, 嘉哉
× 板倉, 嘉哉× 遠藤, 果歩× 重田, 実穂× ITAKURA, Yoshiya× ENDO, Kaho× SHIGETA, Miho |
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著者所属 | ||||||
千葉大学 | ||||||
著者所属 | ||||||
千葉大学 | ||||||
著者所属 | ||||||
千葉大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Chiba University | ||||||
著者所属(英) | ||||||
en | ||||||
Chiba University | ||||||
著者所属(英) | ||||||
en | ||||||
Chiba 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: 第53回流体力学講演会/第39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 53rd Fluid Dynamics Conference / the 39th Aerospace Numerical Simulation Symposium 巻 JAXA-SP-21-008, p. 125-130, 発行日 2022-02-14 |
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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53回流体力学講演会/第39回航空宇宙数値シミュレーション技術シンポジウム (2021年6月30日-7月2日. 日本航空宇宙学会 : 宇宙航空研究開発機構(JAXA)オンライン会議) | |||||
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 | The 53rd Fluid Dynamics Conference / the 39th Aerospace Numerical Simulation Symposium (June 30 - July 2, 2021. The Japan Society for Aeronautical and Space Sciences : Japan Aerospace Exploration Agency (JAXA), Online meeting) | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | According to many badminton players, there are some differences in impact feeling and flight trajectory between feather and synthetic shuttlecocks. The stiffness of the structural materials must affect the impact feeling. The difference in-flight trajectory is thought to be causally related to the Reynolds number dependency. In the present study, using the vertical wind tunnel, static axial force and rolling moment acting on shuttlecocks were measured for a range of Reynolds number 10,000 less than Re less than 43,000. Typical results are as follows: (1) Axial force of the feather shuttlecock declined sharply as the Re number decreased, and differences of axial force between feather and synthetic became remarkable. (2) Contribution of wind-milling drag to the total drag was estimated. The contribution ratio of windmill drag was about 15 - 40 %. | |||||
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 | |||||
ISSNONLINE | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 2433-2232 | |||||
著者版フラグ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA2130027009 | |||||
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-21-008 |