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航技研突風風洞における後流測定データを利用した空力特性の推算技術
https://jaxa.repo.nii.ac.jp/records/38007
https://jaxa.repo.nii.ac.jp/records/380071c9e1c08-e5e7-4f36-8b1b-281f385709c4
名前 / ファイル | ライセンス | アクション |
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nalsp0051002.pdf (795.6 kB)
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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 | 航技研突風風洞における後流測定データを利用した空力特性の推算技術 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 突風 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アスペクト比 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 抗力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 揚力 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | gust | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | airfoil | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aspect ratio | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | drag | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | lift | |||||
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 | Estimation of aerodynamic characteristics using wake integral method at the NAL 2 m x 2 m gust wind tunnel | |||||
著者 |
上野, 真
× 上野, 真× 藤田, 敏美× 岩崎, 昭人× Ueno, Makoto× Fujita, Toshimi× Iwasaki, Akihito |
|||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所特別資料: 第64回・第65回風洞研究会議論文集 en : Special Publication of National Aerospace Laboratory: Proceedings of the 64th and 65th Workshop on Wind Tunnel Research 巻 51, p. 9-13, 発行日 2001-02 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Aerodynamic characteristics are computed from wake survey data of a rectangular wing model of aspect ratio five with an untwisted NACA0012 airfoil section. The theories of Maskell and Bets are used. Their basic approach is to rewrite the drag and lift integrals in terms of flow variables measured inside the wake region. And it furnishes separate values for the components of drag such as profile drag and induced drag, but also measures lift without the use of a balance. In addition to global data, details of the wake flow field as well as spanwise distributions of lift and drag are obtained. Wake survey data analysis is performed and the results are compared to the balance data. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0032235002 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL SP-51 |