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Roll Coupling Moment of Deflected Wing-Body Combination
https://jaxa.repo.nii.ac.jp/records/34466
https://jaxa.repo.nii.ac.jp/records/34466f575779f-3d51-4fc7-94ab-8c106d9f7bb1
名前 / ファイル | ライセンス | アクション |
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SA2400886.pdf (1.8 MB)
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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 | ||||||
言語 | en | |||||
タイトル | Roll Coupling Moment of Deflected Wing-Body Combination | |||||
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_6501 | |||||
資源タイプ | departmental bulletin paper | |||||
著者 |
TSUKAMOTO, Shigeki
× TSUKAMOTO, Shigeki |
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出版者 | ||||||
出版者 | 東京大学宇宙航空研究所 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Aeronautical Science,University of Tokyo | |||||
書誌情報 |
en : ISAS report/Institute of Space and Aeronautical Science,University of Tokyo 巻 37, 号 14, p. 329-368, 発行日 1972-12 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A method of analysis based on the slender-body theory has been developed to investigate the characteristics of the roll coupling moment due to the flow induced by deflected wings and cross flow. The method makes use of conformal mapping of the well-known hydrodynamics and numerical integration. Flow patterns on the wing have been obtained in the form of elliptic integrals and are shown for various values of span to body radius ratio λ. Calculatios have been performed for uniformly canted and elastically deflected wings in planar and cruciform wing-body combinations. It is shown that there exists a considerably wide region (from the root to 50∿57 percent of the wing span) where induced velocity has negative sign for the elastcially deffected wings. Roll coupling moment coefficients are also presented for wing-body combinations of various values of λ. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0372-1418 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA00675986 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA2400886000 |