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Supersonic Flow Around Tip Sides of Wings
https://jaxa.repo.nii.ac.jp/records/31288
https://jaxa.repo.nii.ac.jp/records/31288f1fd5d4c-38b9-477a-83cd-756e328d2bcc
名前 / ファイル | ライセンス | アクション |
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SA0033549.pdf (403.7 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 | Supersonic Flow Around Tip Sides of Wings | |||||
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 |
VOSKRESENSKY, G. P.
× VOSKRESENSKY, G. P. |
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著者所属(英) | ||||||
en | ||||||
Keldysh Inst. of Applied Mathem. of the USSR Academy of Sciences Moscow | ||||||
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. : Proceedings of the Symposium on Mechanics for Space Flight 1985 巻 4, p. 217-223, 発行日 1986-03 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The problem of the supersonic flow around the tip sides of wings with swept or unswept leading edges and an attached shock wave is presented. The solution of the problem is based on the assumption that the surface of a rounded tip side of wing is conical and the flow around it is self-similar. This fact makes it possible to use the self-similar statoning principle for the solution of the problem. The realization of this principle is carried out with the help of the finite-difference second-order algorthm. The results at M∝=2,α=0゜, α=5゜are given. | |||||
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: SA0033549000 |