Investigation of a thermodynamic cycle of a forced 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 possibilities of the in crease of the traction of a two-chamber turbo-jet engine, because due to of the forcing of the main cycle, are cosidered. The influence of the conditions of the flight of an aircraft on the quantity of the forced cycle is analysed.


Download

mai.ru — informational site MAI

Copyright © 2000-2021 by MAI

Вход