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<論文>遷音速軸流圧縮機の翼列性能に関する研究(V/STOL機用エンジンに関する研究)
https://jaxa.repo.nii.ac.jp/records/31478
https://jaxa.repo.nii.ac.jp/records/31478a200f740-3e8f-49c1-bfdc-4e67d5b15909
名前 / ファイル | ライセンス | アクション |
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SA0124369.pdf (2.1 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 | <論文>遷音速軸流圧縮機の翼列性能に関する研究(V/STOL機用エンジンに関する研究) | |||||
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 | Investigation of the Performance of Blade Rows in Transonic Axial-flow Compressor | |||||
著者 |
田中, 英穂
× 田中, 英穂× 丸田, 秀雄× 網野, 一夫× TANAKA, Hideo× MARUTA, Hideo× AMINO, Kazuo |
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著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science, University of Tokyo | ||||||
出版者 | ||||||
出版者 | 東京大学宇宙航空研究所 | |||||
書誌情報 |
東京大学宇宙航空研究所報告 巻 1, 号 3_B, p. 127-163, 発行日 1965-09 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | V/STOL機用エンジンの開発に欠くことのできない段当り圧力比の高い遷音速圧縮機の設計資料に供するため,翼形としては二重円弧翼を使用しボス比0.7,軸流速度180 m/sec段当り圧力比1.6の遷音速試験翼列を試作し,遷音速圧縮機としての全体性能並びに圧縮機内部の流れの様子を調べ,動翼列および静翼列個々の翼列性能を明らかにした. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | As a component of a jet engine for V/STOL plane, a transonic axial-flow compressor with high pressure ratio per stage is hoped to be developed. At present, only a few design data for a transonic blade row are available for designers. Considering of this status quo, we made a single stage transonic axial-flow test compressor with pressure ratio of 1. 6 per stage, boss ratio of 0.7 and axial air velocity of 180 m/sec. We used double circular arc blades for both the rotating and the stationary blades. Using this test compressor, we made clear the overall performance of it and the performance of both the rotating and the stationary blade rows. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0563-8100 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00161914 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA0124369000 |