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三次元基本翼の広域レイノルズ数域での空力非線形性
https://jaxa.repo.nii.ac.jp/records/5429
https://jaxa.repo.nii.ac.jp/records/54291f2e37cb-9518-4660-8b50-de9c6720e47b
名前 / ファイル | ライセンス | アクション |
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64303027.pdf (3.0 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 | 三次元基本翼の広域レイノルズ数域での空力非線形性 | |||||
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 | Non-linear aerodynamic characteristics of three dimensional wings at large range of Reynolds numbers | |||||
著者 |
米本, 浩一
× 米本, 浩一× 越智, 廣志× 高藤, 圭一郎× 和田, 一輝× 佐藤, 喬也× Yonemoto, Koichiro× Ochi, Hiroshi× Takato, Keiichi× Wada, Kazuki× Sato, Takaya |
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著者所属 | ||||||
九州工業大学 | ||||||
著者所属 | ||||||
西日本工業大学 | ||||||
著者所属 | ||||||
西日本工業大学 | ||||||
著者所属 | ||||||
九州工業大学大学院 | ||||||
著者所属 | ||||||
九州工業大学大学院 | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Nishi-Nippon Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Nishi-Nippon Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
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 | Aerodynamic characteristics of three dimensional wings for a wide range of Reynolds number from 10(exp 4) to 10(exp 6) have been studied using variable-pressure wind tunnels. Rectangular wing and the delta wing with NACA0012 and flat plate cross sections were tested. The wind tunnel tests show that the aerodynamic characteristics for all the wings are almost linear at high Reynolds numbers up to the angle-of-attack of stall. The aerodynamic non-linearity appears significantly as the Reynolds number decreases especially for the thick wing that have NACA0012 cross section. But the wings that have flat plate wing sections do not have such an aerodynamic non-linearity even at low Reynolds numbers. | |||||
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: AA0064303027 | |||||
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 |