NASA NTRS · 19780011216
Approximate dynamic model of a turbojet engine
Abstract
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.
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Artemov, O. A.. 1978-03-01. Approximate dynamic model of a turbojet engine. https://ntrs.nasa.gov/citations/19780011216
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