Simulation of thrust performances ramjet engine for high supersonic velocities of flight
Aerospace propulsion engineering
Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
AbstractThe 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