| タイトル | Investigation of a nozzle instability on an F100 engine equipped with a digital electronic engine control |
| 本文（外部サイト） | http://hdl.handle.net/2060/19860015883 |
| 著者（英） | Zeller, J. R.; Burcham, F. W., Jr. |
| 著者所属（英） | NASA Dryden Flight Research Center |
| 発行日 | 1984-03-01 |
| 言語 | eng |
| 内容記述 | An instability in the nozzle of the F100 engine, equipped with a digital electronic engine control (DEEC), was observed during a flight evaluation on an F-15 aircraft. The instability occurred in the upper left hand corner (ULMC) of the flight envelope during augmentation. The instability was not predicted by stability analysis, closed-loop simulations of the the engine, or altitude testing of the engine. The instability caused stalls and augmentor blowouts. The nozzle instability and the altitude testing are described. Linear analysis and nonlinear digital simulation test results are presented. Software modifications on further flight test are discussed. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 86N25354
PAPER-12 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/566097 |
