Simulation of thrust performances ramjet engine for high supersonic velocities of flight

Aerospace propulsion engineering


Аuthors

Karasiov V. N.*, Levin V. M.*

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

*e-mail: aerospace@mai.ru

Abstract

The questions of simulation of working process in a supersonic ramjet engine working on aviation kerosene are considered. The computed examples of performances for one scheme of a supersonic ramjet engine are given.

Keywords:

flight vehicle; combined power plant; supersonic ramjet engine; mathematical simulation


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