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Distance of Landing Run and the Coefficient of Ground Friction
https://jaxa.repo.nii.ac.jp/records/35801
https://jaxa.repo.nii.ac.jp/records/358016143219e-a7d7-451e-812f-42acf1162bf5
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
SA4415994.pdf (272.4 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 | Distance of Landing Run and the Coefficient of Ground Friction | |||||||
| 言語 | en | |||||||
| 言語 | ||||||||
| 言語 | eng | |||||||
| 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 |
OGAWA, Taitiro
× OGAWA, Taitiro
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| 著者所属（英） | ||||||||
| en | ||||||||
| Member of the Institute | ||||||||
| 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 69, p. 236-243, 発行日 1930-05 |
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| 抄録（英） | ||||||||
| 内容記述タイプ | Other | |||||||
| 内容記述 | A simple formula for the distance of landing run is proposed (Chap. 1). By this formula the coefficient of ground friction of the whole landing gear μ is calculated from the observed landing distances for several aeroplanes (Chap. 2). An aeroplane with the main wing dismantled was towed by a motor-car. When a constant speed was attained the tow-wire was cut off, and from the time necessary for the aeroplane to stand still, the coefficient of wheels μ_1, and that of tail skid μ_2 were measured. Assuming that the coefficient of ground friction of wheels μ_1 remains constant for all aeroplanes, that of tail skid μ_2 was calculated for 3 aeroplanes from μ given in Chap. 2. The difference of the value μ_2 for each aeroplane can be attributed to the widely varying bearing area of the tail skids. (Chap. 3). | |||||||
| 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: SA4415994000 | |||||||
