Investigation of a thermodynamic cycle 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
AbstractThermodynamic cycles of a perfect and practicable turbo-jet engine are considered. Their features and methods of choice of optimum parameters are analysed. The theoretical means of receiving varied specific tractions and specific spendings of fuel by two-chamber turbo-jet engines are given in this article.