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What is Upgrading SR-30 Turbojet Exhaust Nozzle about?

The report details the design and development of a variable nozzle for the SR-30 turbojet engine, aimed at enhancing educational demonstrations in aerospace engineering. The proposed design features a converging-diverging nozzle with a fixed-area converging duct and a variable-area diverging duct, utilizing mechanical linear actuation for control. This adaptation is intended to facilitate performance studies on propulsion technologies while addressing the limitations of existing nozzle designs for small edu

Author

noticiasfleidohmun

Language

EN