The thrust generation in a jet engine is explained. Newton's law is used to derive the thrust equation. The functions of the diffuser, compressor, burner or combustor, turbine and nozzle are explained. The turbojet, turbofan, turboprop and ramjet are explained along with the pressure-volume curves. Isentropic flow and constant pressure combustion are explained for the jet engines. The video will serve as a tutorial for jet engine propulsion for aerospace engineers.
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