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Unsteady Vortex Lattice Calculation of the Flow Around a Slender Delta Wing
https://jaxa.repo.nii.ac.jp/records/31215
https://jaxa.repo.nii.ac.jp/records/3121582bcb792-1677-418e-be1f-5b9cacbaa9d7
名前 / ファイル | ライセンス | アクション |
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SA0033460.pdf (423.7 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 | ||||||
言語 | en | |||||
タイトル | Unsteady Vortex Lattice Calculation of the Flow Around a Slender Delta Wing | |||||
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 |
SAKURAI, Akira
× SAKURAI, Akira× UCHIHORI, Hiroshi |
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著者所属(英) | ||||||
en | ||||||
Department of Aeronautical Engineering, Kyushu University | ||||||
著者所属(英) | ||||||
en | ||||||
Post Graduate Course, Kyushu University | ||||||
出版者 | ||||||
出版者 | 宇宙科学研究所 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science | |||||
書誌情報 |
en : The Institute of Space and Astronautical Science report. S.P. : The Proceedings of the Symposium on Mechanics for Space Flight 1989 巻 12, p. 53-59, 発行日 1990-03 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The unsteady vortex lattice method was applied to the calculation of the unsteady flow field around a slender delta wing at a high angle of attack. The result shows that the essential feature of the flow such as the formation of the leading edge vortex can be described by this model, while the detail of the calculated flow field still depends on the practical aspects of the scheme such as the selection of the viscous core radius. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0288-433X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA10455137 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA0033460000 |