In this paper, a method of evaluation of the turbojet engine regulation condition in flight, based on information from its ground tests was presented. The tested engine was presented by the single comprehensive model which links input (in form of the modified signal mp4) and engine output (in form of the modified signal np2). Changes of the model parameters following during its operation can be defined using changes of the proposed simulation model parameters describing the engine operation both in flight and during ground tests.
Validity Check of the Assessment of a Jet Turbine Engine Regulation in Flight Using a Computer Simulation
2013
6 Seiten
Aufsatz/Kapitel (Buch)
Englisch
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