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楕圓形風洞の境界の影響に關する小計算
https://jaxa.repo.nii.ac.jp/records/36475
https://jaxa.repo.nii.ac.jp/records/364758dba9d9d-f212-456b-bfb4-8353131700e9
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
SA4433763.pdf (242.4 kB)
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| Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||||
|---|---|---|---|---|---|---|---|---|
| 公開日 | 2015-03-26 | |||||||
| タイトル | ||||||||
| タイトル | 楕圓形風洞の境界の影響に關する小計算 | |||||||
| 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 | |||||||
| 著者 |
谷, 一郎
× 谷, 一郎
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| 出版者 | ||||||||
| 出版者 | 東京帝國大學航空研究所 | |||||||
| 書誌情報 |
東京帝國大學航空研究所彙報 巻 156, p. 433-437, 発行日 1937-08 |
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| 抄録（英） | ||||||||
| 内容記述タイプ | Other | |||||||
| 内容記述 | A small four-bladed wind vane was placed behind a wing model, and the rate of rotation was measured stroboscopically in order to investigate the lift distribution along the span. It was found both theoretically and experimentally that the rate of rotation was nearly proportional to dГ/dy, where Гis the circulation and y is the distance along the span, provided that the wind vane was sufficiently small and properly placed behind the model. The allowable diameter of the wind vane is estimated to be of the order of one per cent of the span. The present miniature test was made as a preliminary investigation in order to determine the applicablity of a wind vane for such a purpose. It is hoped in the near future to make the test in the larger scale. | |||||||
| 書誌レコードID | ||||||||
| 収録物識別子タイプ | NCID | |||||||
| 収録物識別子 | AN00162779 | |||||||
| 資料番号 | ||||||||
| 内容記述タイプ | Other | |||||||
| 内容記述 | 資料番号: SA4433763000 | |||||||
