Investigation of the influence of parameters of the working process on specific parameters of a 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 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.