| タイトル | A theory of post-stall transients in multistage axial compression systems |
| 本文（外部サイト） | http://hdl.handle.net/2060/19850012807 |
| 著者（英） | Moore, F. K.; Greitzer, E. M. |
| 著者所属（英） | Massachusetts Inst. of Tech.|Cornell Univ. |
| 発行日 | 1985-03-01 |
| 言語 | eng |
| 内容記述 | A theory is presented for post stall transients in multistage axial compressors. The theory leads to a set of coupled first-order ordinary differential equations capable of describing the growth and possible decay of a rotating-stall cell during a compressor mass-flow transient. These changing flow features are shown to have a significant effect on the instantaneous compressor pumping characteristic during unsteady operation, and henace on the overall system behavior. It is also found from the theory that the ultimate mode of system response, stable rotating stall or surge, depends not only on the B parameter but also on other parameters, such as the compressor length-to-diameter ratio. Small values of this latter quantity tend to favor the occurrence of surge, as do large values of B. A limited parametric study is carried out to show the impact of the different system features on transient behavior. Based on analytical and numerical results, several specific topics are suggested for future research on post-stall transients. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 85N21117
NAS 1.26:3878
NASA-CR-3878 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/156991 |
