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このアイテムのファイル:
| ファイル | 記述 | サイズ | フォーマット | |
|---|---|---|---|---|
| mfeku_20_3_163.pdf | 2.88 MB | Adobe PDF | 見る/開く |
| タイトル: | The Shock Tube as a Short Duration Wind Tunnel |
| 著者: | KAMIMOTO, Gorō SHIMIZU, Takashi AKAMATSU, Teruaki |
| 発行日: | 15-Aug-1958 |
| 出版者: | Faculty of Engineering, Kyoto University |
| 誌名: | Memoirs of the Faculty of Engineering, Kyoto University |
| 巻: | 20 |
| 号: | 3 |
| 開始ページ: | 163 |
| 終了ページ: | 181 |
| 抄録: | Descriptions of the shock tube recently constructed at Aerodynamic Laboratory and of some experimental results obtained thereby are given in this paper. The shock tube has a cross section of 156mm high and 50mm wide and is 3370mm long. By this shock tube a uniform flow field, free from turbulence, is obtained and its Mach number may freely be adjusted from zero to the supersonic range. Instantaneous photographs of the flow patterns have been taken by using the Mach-Zehnder interferometer or the schlieren method and are shown in this paper. |
| URI: | http://hdl.handle.net/2433/280414 |
| 出現コレクション: | Vol.20 Part 3 |
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