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<論文>圧縮流れ中の翼のガスト応答と傾斜効果
https://jaxa.repo.nii.ac.jp/records/32613
https://jaxa.repo.nii.ac.jp/records/326135173ab0f-4cae-445f-b754-7063f6da2ce3
名前 / ファイル | ライセンス | アクション |
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SA0125949.pdf (389.4 kB)
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Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | <論文>圧縮流れ中の翼のガスト応答と傾斜効果 | |||||
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_6501 | |||||
資源タイプ | departmental bulletin paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Aerofoil Response in Oblique Gust | |||||
著者 |
長島, 利夫
× 長島, 利夫× 谷田, 好通× NAGASHIMA, Toshio× TANIDA, Yoshimichi |
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著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science, University of Tokyo | ||||||
出版者 | ||||||
出版者 | 東京大学宇宙航空研究所 | |||||
書誌情報 |
東京大学宇宙航空研究所報告 巻 17, 号 1_A, p. 23-34, 発行日 1981-02 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | Searsによる翼のガスト応答の問題を,亜音速流れ中でexp[iω(t-x/V)+iλz]と表わされる3次元的ガストに拡張し,特異点法を用いて解いた.翼の前縁に対してガスト波面が傾斜する効果が大きいことが結論された. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The Sears type lift functions (Imaginery vs. real parts of the unsteady lift coefficient) of an aerofoil operating in sinusoidal gusts of a general form: exp[iω (t-x/V) + iλz)] with a subsonic flow have been calculated. The obliqueness of the gust wave front with respect to the aerofoil leading edge is found to be very influencial upon the aerodynamic lift and moment. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0563-8100 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00161914 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA0125949000 |