Turboejector engine
Aerospace propulsion engineering
Аuthors
Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
Abstract
The principles of work and choice of optimum parameters of work of turboejector engines are stated. The principle possibility of using turboejector engines for an aircraft with a cruising supersonic speed is shown (М = 3,5/3,8).Download