Mathematical Model of TV3-117VM Engine

Aerospace propulsion engineering


Аuthors

Rybkin P. N.

Abstract

The article describes a mathematical model of the TV3-117VM engine used as a fragment of the mathematical model of MI-8MTV flight simulator. The model is structured according to engine automatic control. A real performance of the engine compressor has been used to compute power and fuel consumption.

Keywords:

mathematical modeling; helicopter flight simulator; gas-turbine engine performance analysis.


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