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The characteristics of a cylindrical probe at high subsonic speeds. Part 2. The case having inclination angles
https://doi.org/10.18999/memfenu.25.1.81
833fd52b-d96c-422b-886d-1aae5e39a472
名前 / ファイル | ライセンス | アクション | |
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Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
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公開日 | 2021-01-25 | |||||
タイトル | ||||||
タイトル | The characteristics of a cylindrical probe at high subsonic speeds. Part 2. The case having inclination angles | |||||
言語 | en | |||||
著者 |
Hashimoto, Taka-aki
× Hashimoto, Taka-aki× Otsuka, Shintaro× Futsukaichi, Sadamu |
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抄録 | ||||||
内容記述 | In measuring high subsonic internal flows which are observed in high speed turbomachines such as transonic or supersonic compressors, authors planned to use a cylindrical probe which was supported at both ends, and got satisfactory results in the case of zero inclination angle. Futhermore, the inclination characteristics of this probe were investigated experimentally and it was revealed that the yaw angle of flow could be easily obtained independently of both Mach number M∞ and inclination angle α. It was also revealed that the flow component normal to the probe axis could be obtained with a fair accuracy from the characteristics of zero inclination angle within the range of not too large inclination angles (about ± 15°). | |||||
言語 | en | |||||
内容記述タイプ | Abstract | |||||
出版者 | ||||||
出版者 | Faculty of Engineering, Nagoya University | |||||
言語 | ||||||
言語 | eng | |||||
資源タイプ | ||||||
資源 | http://purl.org/coar/resource_type/c_6501 | |||||
タイプ | departmental bulletin paper | |||||
ID登録 | ||||||
ID登録 | 10.18999/memfenu.25.1.81 | |||||
ID登録タイプ | JaLC | |||||
ISSN(print) | ||||||
収録物識別子タイプ | PISSN | |||||
収録物識別子 | 0027-7657 | |||||
書誌情報 |
Memoirs of the Faculty of Engineering, Nagoya University 巻 25, 号 1, p. 81-88, 発行日 1973-12-10 |
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著者版フラグ | ||||||
値 | publisher |