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Approximate dynamic model of a turbojet engineAn 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.
Document ID
19780011216
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Artemov, O. A. (NASA Headquarters Washington, DC United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1978
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-75263
Report Number: NASA-TM-75263
Accession Number
78N19159
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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