R. R. Burley, Adel Mansour
Abstract
Performance characteristics of auxiliary inlet ejector nozzle configurations for takeoff, transonic acceleration, and supersonic flight conditions with pressure and temperature profiles
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Performance characteristics of auxiliary inlet ejector nozzle configurations for takeoff, transonic acceleration, and supersonic flight conditions with pressure and temperature profiles
Key concepts: Injector, Nozzle, Turbojet, Generator (circuit theory), Gas generator, Inlet, Mechanical engineering, Engineering