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Lifting-Line Theory for Cascade of Blades in Subsonic Shear Flow
https://jaxa.repo.nii.ac.jp/records/34396
https://jaxa.repo.nii.ac.jp/records/34396bc8c102b-33f7-4c8e-b09a-2989f0d5375d
名前 / ファイル | ライセンス | アクション |
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SA2400561.pdf (2.8 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 | Lifting-Line Theory for Cascade of Blades in Subsonic Shear Flow | |||||
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 |
NAMBA, Masanobu
× NAMBA, Masanobu× ASANUMA, Tsuyoshi |
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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 32, 号 8, p. 133-179, 発行日 1967-08 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A theory of lifting-lines for cascade of blades in subsonic shear flow is developed by assuming that the dependence of the local lift force upon the local upstream Mach number in shear flow is same as that in two-dimensional flow. By comparing theoretical results with experimental ones, the physical validity of the present theory is discussed. The effect of compressibility upon the mean characteristics of a cascade is found to depend upon the root of harmonic mean square of upstream Mach number (M^^^-^*_<-∞>). Experimental correlation is satisfactory as far as M^^^-^*_<-∞> of the shear flow lies below a certain limit value, and this limit value corresponds to the two-dimensional Mach number beyond which the small disturbance theory for two-dimensional cascade shows poor validity. Significance of M^^^-^*_<-∞> as a criterion for the mean characteristics is also confirmed experimentally. | |||||
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: SA2400561000 |