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Turbulent transonic flow for NACA 0012/RAE 2822 airfoils under Baldwin-Lomax model
https://doi.org/10.18999/memfenu.37.2.203
https://doi.org/10.18999/memfenu.37.2.2031ab92fef-11ad-4b74-8b6c-19e498c610fb
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 | 2020-11-04 | |||||
タイトル | ||||||
タイトル | Turbulent transonic flow for NACA 0012/RAE 2822 airfoils under Baldwin-Lomax model | |||||
言語 | en | |||||
著者 |
Fujiwara, Toshi
× Fujiwara, Toshi× Wang, Yi-Yun× Ohmori, Yasunori |
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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 | |||||
抄録 | ||||||
内容記述 | The Beam-Warming scheme was applied to transonic flows around two-dimensional airfoils NACA 0012 and RAE 2822, taking account of the Baldwin-Lomax turbulence model. After appropriate grid generation techniques, the calculation successfully lead to steady flows containing a shock wave and flow separation, for a uniform flow Mach number 0.75, the Reynolds number 6×10[6] , and angles of attack 0 to 15 degrees. Note that periodical oscillations were observed at high angles of attack. | |||||
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.37.2.203 | |||||
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 37, 号 2, p. 203-218, 発行日 1986-03-31 |
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著者版フラグ | ||||||
値 | publisher |