| タイトル | Normal shock and restart controls for a supersonic airbreathing propulsion system |
| 著者（英） | Cole, G. L.; Neiner, G. H.; Paulovich, F. J. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1978-01-01 |
| 言語 | eng |
| 内容記述 | Results of experimental investigations to control a supersonic mixed-compression inlet coupled to a turbojet engine are presented. Special instrumentation and servoactuators were developed to have sufficiently fast dynamic response so that basic propulsion system dynamics were the main limitation to controllability. In some cases servoactuator input signals were electronically limited to simulate moderate performance flight hardware. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 78N23023 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/528180 |
