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衝撃波の生成に關する實驗
https://jaxa.repo.nii.ac.jp/records/35535
https://jaxa.repo.nii.ac.jp/records/35535dccb5d21-48a5-4d11-b29d-3a61e6330eec
名前 / ファイル | ライセンス | アクション |
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SA4148622.pdf (5.2 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 | 衝撃波の生成に關する實驗 | |||||
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 | Experimental Study on the Formation of Shock Waves. | |||||
著者 |
河田, 三治
× 河田, 三治× KAWADA, Sandi |
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出版者 | ||||||
出版者 | 東京帝國大學航空研究所 | |||||
出版者(英) | ||||||
出版者 | Aeronautical Research Institute, Tokyo Imperial University | |||||
書誌情報 |
東京帝國大學航空研究所報告 en : Report of Aeronautical Research Institute, Tokyo Imperial University 巻 18, 号 237, p. 244-264, 発行日 1942-07 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Two aerofoils of 4cm chord were tested in 16×16cm high speed wind tunnel. The upper and lower boundaries of the tunnel were removable, thus both closed- and open-type wind tunnel, were available for the experiment. Especially in the closed-type tunnel very clear photographs of the shock waves were obtained. Two different kinds of shock waves were observed. The principal shock wave is the one perpendicular to the flow and in passings this the velocity jumps from supersonic to subsonic state. The another is smaller oblique shock wave situated in front of the former. The velocity after this wave is still supersonic. | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA00387631 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA4148622000 |