| タイトル | Effect of afterburner lights and inlet unstarts on a mixed compression inlet turbofan engine operating at Mach 2.5 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19750012262 |
| 著者（英） | Daniele, C. J.; Baumbick, R. J.; Batterton, P. G. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1975-04-01 |
| 言語 | eng |
| 内容記述 | Data are presented to show the response of an uncontrolled inlet to afterburner lightoff disturbances when a mixed-compression inlet is coupled to a turbofan engine. The results show a significant upstream shock excursion when the afterburner lights which is a result of the direct communication between the afterburner region and the inlet by means of the fan duct and fan stages. In addition results of a waveform analysis on the inlet pressure response to the afterburner light is presented. Inlet unstarts and their effect on operation of the propulsion system is also discussed. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 75N20334
E-8194
NASA-TM-X-3223 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/190569 |
