| タイトル | Dynamics of a supersonic inlet-engine combination subjected to disturbances in fuel flow and inlet overboard bypass airflow |
| 本文（外部サイト） | http://hdl.handle.net/2060/19720016187 |
| 著者（英） | Wallhagen, R. E.; Paulovich, F. J.; Geyser, L. C. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1972-05-01 |
| 言語 | eng |
| 内容記述 | An axisymmetric mixed-compression supersonic inlet and a single-spool turbojet engine were dynamically tested at Mach 2.5. The propulsion system was subjected to sweep-frequency sinusoidal disturbances of either inlet overboard bypass airflow. The disturbances were at a logarithmic sweep rate of 1 decade per minute. Dynamic responses were taken of signals throughout the propulsion system. Selected signals were reduced relative to the prime propulsion system parameters. The experimental data are presented in Bode plots. Most of the plots are for a frequency range of 1.0 to 50 hertz. |
| NASA分類 | PROPULSION SYSTEMS |
| レポートNO | 72N23837
NASA-TM-X-2558
E-6115 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/203471 |
