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An application of the surface-singularity method to wing-body-tail configurations
https://doi.org/10.18999/memfenu.40.2.337
https://doi.org/10.18999/memfenu.40.2.337882cc148-6bb6-4db6-9d3e-fbf4f405143e
名前 / ファイル | ライセンス | アクション |
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Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
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公開日 | 2020-10-29 | |||||
タイトル | ||||||
タイトル | An application of the surface-singularity method to wing-body-tail configurations | |||||
言語 | en | |||||
著者 |
Choi, Jang-Soo
× Choi, Jang-Soo× Chang, Keun-Shik× Sugiyama, Yoshiyuki |
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アクセス権 | ||||||
アクセス権 | open access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_abf2 | |||||
内容記述 | ||||||
内容記述 | A computer code based on the 1st order panel method is presented for solving inviscid incompressible flow fields about 3-D airplane-like bodies. A sample problem chosen for a test is solved and a comparison with other computational results shows good agreement. To increase the accuracy of the method, especially for a thin wing, the number of doublet panels on the camber surface of a wing is multiplied in the chordwise direction by a factor, which enhances the accuracy to some extent. | |||||
言語 | en | |||||
内容記述タイプ | Abstract | |||||
出版者 | ||||||
言語 | en | |||||
出版者 | Faculty of Engineering, Nagoya University | |||||
言語 | ||||||
言語 | eng | |||||
資源タイプ | ||||||
資源 | http://purl.org/coar/resource_type/c_6501 | |||||
タイプ | departmental bulletin paper | |||||
出版タイプ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
ID登録 | ||||||
ID登録 | 10.18999/memfenu.40.2.337 | |||||
ID登録タイプ | JaLC | |||||
ISSN(print) | ||||||
収録物識別子タイプ | PISSN | |||||
収録物識別子 | 0027-7657 | |||||
書誌情報 |
en : Memoirs of the Faculty of Engineering, Nagoya University 巻 40, 号 2, p. 337-350, 発行日 1989-03-31 |
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著者版フラグ | ||||||
値 | publisher |