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