Yayın: Exergetic effects of some design parameters on the small turbojet engine for unmanned air vehicle applications
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Anahtar kelimeler
Turbojet, Exergy, Gas compressor, Mach number, Thrust, Overall pressure ratio, Turbine, Aerospace engineering, Range (aeronautics), Thrust specific fuel consumption, Automotive engineering, Engineering, Environmental science, Mechanical engineering, Fuel efficiency, Process engineering