| タイトル | Approximate dynamic model of a turbojet engine |
| 本文（外部サイト） | http://hdl.handle.net/2060/19780011216 |
| 著者（英） | Artemov, O. A. |
| 著者所属（英） | NASA Headquarters |
| 発行日 | 1978-03-01 |
| 言語 | eng |
| 内容記述 | An approximate dynamic nonlinear model of a turbojet engine is elaborated on as a tool in studying the aircraft control loop, with the turbojet engine treated as an actuating component. Approximate relationships linking the basic engine parameters and shaft speed are derived to simplify the problem, and to aid in constructing an approximate nonlinear dynamic model of turbojet engine performance useful for predicting aircraft motion. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 78N19159
NASA-TM-75263 |
| 権利 | No Copyright |
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