| タイトル | Effects of tip clearance on overall performance of transonic fan stage with and without casing treatment |
| 本文（外部サイト） | http://hdl.handle.net/2060/19770010049 |
| 著者（英） | Moore, R. D.; Osborn, W. M. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1977-02-01 |
| 言語 | eng |
| 内容記述 | The overall performance of a transonic fan stage is presented for various tip clearances, with and without casing treatment. The stage was tested with a solid casing, and with open skewed slots and closed skewed slots in the casing over the rotor blade tips. Four nominal nonrotating rotor blade tip clearances from 0.061 to 0.178 centimeter were used. For all three casings, the pressure ratio and efficiency decreased with increasing tip clearance. The stall margin for a given casing also decreased with increasing clearance. At design speed and a given tip clearance, the highest stall margin was obtained with the open-slot casing, and the lowest stall margin was obtained with the solid casing. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 77N16992
E-8945
NASA-TM-X-3479 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/183298 |
