The efficiency of combustion chamber work in the complex with turbojet engine

Аuthors

Agul'nik A. В.^*, Onishchik I. I.^**, Htay T. M.^***

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

*e-mail: agulnik201@mail.ru
**e-mail: agulnik@mai.ru
***e-mail: tinmaunghtay377@gmail.com

Abstract

This is the calculation result of combustion efficiency and excess air coefficient at failure combustion in the combustor, working in turbojet structure. Parameters of engine working process and modes of its work were change. At calculations characteristics of compressors with various compression ratio and calculation programs of engine characteristics were used.

Keywords:

turbo-jet engine, combustion chamber, altitude and airspeed, combustion efficiency, excess air factor.