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翼型のCzmaxとCxminの計算式
https://jaxa.repo.nii.ac.jp/records/36372
https://jaxa.repo.nii.ac.jp/records/36372fe5d5ced-7b07-4e28-9867-4d6dd2425c8e
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
SA4433020.pdf (586.7 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 | 翼型のCzmaxとCxminの計算式 | |||||||
| 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 |
糸川, 英夫
× 糸川, 英夫
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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 138, p. 84-93, 発行日 1936-02 |
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| 抄録（英） | ||||||||
| 内容記述タイプ | Other | |||||||
| 内容記述 | The most important and most ambiguous characteristics of aerofoil are maximum lift and minimum drag. Scale effect and turbulence effect make it quite difficult to obtain the actual value of the two characteristics by wind-tunnel experiments, and yet we have had no method of determinating them theoretically. The proposed method of calculating them in this paper, was gained as a simple application of the boundary layer theory, under a several assumptions which are considered to be valid in the flight conditions. By the two formulae, thus derived, the maximum lift coefficient and minimum profile drag are calculated from pressure distribution around the aerofoil, which is obtained by the potential theory. The calculated results are in good accordance with actual flight results, as examples show. | |||||||
| 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: SA4433020000 | |||||||
