| タイトル | TF34 engine compression system computer study |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810006490 |
| 著者（英） | Hosny, W. M.; Steenken, W. G. |
| 著者所属（英） | General Electric Co. |
| 発行日 | 1979-06-01 |
| 言語 | eng |
| 内容記述 | The stability of the fan and the compressor components was examined individually using linearized and time dependent, one dimensional stability analysis techniques. The stability of the fan core integrated compression system was investigated using a two dimensional compression system model. The analytical equations on which this model was based satisfied the mass, axial momentum, radial momentum, and energy conservation equations for flow through a finite control volume. The results gave an accurate simulation of the flow through the compression system. The speed lines of the components were reproduced; the points of instability were accurately predicted; the locations where the instability was initiated in the fan and the core were indicated; and the variation of the bypass ratio during flow throttling was calculated. The validity of the analytical techniques was then established by comparing these results with test data and with results obtained from the steady state cycle deck. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 81N15005
R78AEG612
NASA-CR-159889 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/170431 |
