Investigation of the influence of parameters of the working process on specific parameters of a two-chamber turbo-jet engine

Aerospace propulsion engineering


Аuthors

Pismenny V. L.

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

Abstract

The range of the specific parameters change of a two-chamber turbo-jet engine is determined. The influence of flight conditions on specific parameters of a two-chamber turbo-jet engine is analysed. The comparison with a one-chamber turbo-jet engine is made.


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