Turboejector engine

Aerospace propulsion engineering


Аuthors

Pismenny V. L.

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).


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