The mathematical model of the sound gas ejector with the cylindrical chamber of confusion in the system of the turboejector engine

Aviation technics and technology


Аuthors

Pismenny V. L.

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

Abstract

The calculation of the working line of the gas ejector in the system of the turboejector engine is given. The characteristic of the gas ejector in the system of the gas-turbo engine is illustrated. The characteristic is first defined.


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