Investigation of a thermodynamic cycle of a forced two-chamber turbo-jet engine
Aerospace propulsion engineering
Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
AbstractThe 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.