| タイトル | Impeller blade design method for centrifugal compressors |
| 本文（外部サイト） | http://hdl.handle.net/2060/19750003125 |
| 著者（英） | Kirschner, A. M.; Jansen, W. |
| 著者所属（英） | Northern Research and Engineering Corp. |
| 発行日 | 1974-01-01 |
| 言語 | eng |
| 内容記述 | The design of a centrifugal impeller with blades that are aerodynamically efficient, easy to manufacture, and mechanically sound is discussed. The blade design method described here satisfies the first two criteria and with a judicious choice of certain variables will also satisfy stress considerations. The blade shape is generated by specifying surface velocity distributions and consists of straight-line elements that connect points at hub and shroud. The method may be used to design radially elemented and backward-swept blades. The background, a brief account of the theory, and a sample design are described. |
| NASA分類 | MECHANICAL ENGINEERING |
| レポートNO | 75N11197 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/570444 |
