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遠心過給機の特性に及ぼす翼數の影響
https://jaxa.repo.nii.ac.jp/records/35368
https://jaxa.repo.nii.ac.jp/records/35368157dec1e-1940-471e-8fd1-dc7895835461
名前 / ファイル | ライセンス | アクション |
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SA4146563.pdf (4.2 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 | ||||||
タイトル | 遠心過給機の特性に及ぼす翼數の影響 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Influence of Number of Blades on the Performance of Centrifugal Supercharger. | |||||
著者 |
渡部, 一郎
× 渡部, 一郎× 柴田, 浩× 中川, 彌壽男× 豊澤, 道生× WATANABE, Itiro× SIBATA, Hirosi× NAKAGAWA, Yasuo× TOYOZAWA, Dosei |
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出版者 | ||||||
出版者 | 東京帝國大學航空研究所 | |||||
出版者(英) | ||||||
出版者 | Aeronautical Research Institute, Tokyo Imperial University | |||||
書誌情報 |
東京帝國大學航空研究所報告 en : Report of Aeronautical Research Institute, Tokyo Imperial University 巻 13, 号 159, p. 146-168, 発行日 1937-12 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper describes the effect of number of blades on the performance of centrifugal supercharger. Experiments were carried on eighteen, nine and six blades on model impeller, and sixteen, eight and four blades on actual impeller. The results of these experiments showed that the more the number of blades, the better the performance of the supercharger, i. e. the overall adiabatic efficiency, pressure ratio, density ratio and so on. The conclusion of this research can briefly be stated as follows. "Let the number of blades be as much as possible, so far as the suction area be properly retained." | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA00387631 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA4146563000 |