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Considerations on Basis for Vortex-Lattice Method
https://jaxa.repo.nii.ac.jp/records/44884
https://jaxa.repo.nii.ac.jp/records/44884125c6a4b-18e2-4104-823d-e6322812e392
名前 / ファイル | ライセンス | アクション |
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naltr0629t.pdf (813.9 kB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Considerations on Basis for Vortex-Lattice Method | |||||
言語 | ||||||
言語 | eng | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
著者 |
市川, 輝雄
× 市川, 輝雄× ICHIKAWA, Teruo |
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著者所属 | ||||||
航空宇宙技術研究所機体第一部 | ||||||
著者所属(英) | ||||||
en | ||||||
First Airframe Division, National Aerospace Laboratory(NAL) | ||||||
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 |
en : Technical Report of National Aerospace Laboratory TR-629T 巻 629T, p. 11, 発行日 1980-09 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 揚力面理論の積分方程式にCauchy積分に対するStarkの数値積分公式を適用することによって,矩形翼に対するvortex lattice法の理想的な格子配置を得た。これによって,格子渦の循環と対応する局所揚力との関係を明確に定義することができ,さらにこれからの当然の帰結として誘導抵抵の翼幅方向分布を精度よく計算できることを示した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | An ideal lattice arrangement of the vortex-lattice method for rectangular wings is obtained by applying Stark’s quadrature formula for a Cauchy integral to the integral equation of the lifting-surface theory. The relation between the circulation of a lattice vortex and the corresponding local lift is thereby clearly defined, and the spanwise distribution of the induced drag is shown to be calculated accurately. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR0629000 | |||||
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 TR-629T |