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Supersonic Flow Past Pointed Bodies of Revolution at Small Angles of Attack
https://jaxa.repo.nii.ac.jp/records/34386
https://jaxa.repo.nii.ac.jp/records/3438616130b16-20f2-41dc-ae02-0e9a8b7d9fd4
名前 / ファイル | ライセンス | アクション |
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SA2400529.pdf (1.7 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 | Supersonic Flow Past Pointed Bodies of Revolution at Small Angles of Attack | |||||
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 |
KARASHIMA, Keiichi
× KARASHIMA, Keiichi× IWASAKI, Kenjiro |
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著者所属(英) | ||||||
en | ||||||
Mechanical Engineering Research Laboratory, Hitachi Ltd. | ||||||
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 31, 号 6, p. 117-141, 発行日 1966-08 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A general method of theoretical approach to supersonic flow past lifting bodies of revolution with arbitrary geometry is presented assuming that the flow behind an attached shock wave consists of a basic non-lifting field upon which is superimposed a perturbation field due to small angles of attack and is particularly applied to circularcones as a simple example. It is shown that, although the nonlinearity in fundamental equations predicting the basic field has a predominant effect on aerodynamic characteristics of the body, a linear approximation of perturbation field with respect to angle of attack still seems to be available even if the body is not so slender. Experimental results also confirm this. | |||||
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: SA2400529000 |