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Internal combustion engine Afterburner Turbofan Turbojet Bypass ratio Ramjet Variable cycle engine Specific thrust Thrust specific fuel consumption Jet engines Fluid dynamics Mechanical engineering		Add to Reading List Source URL: ftp.rta.nato.int Download Document from Source Website File Size: 103 B Share Document on Facebook

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	Diplomarbeit Department Fahrzeugtechnik und Flugzeugbau Assessment of Numerical Models for Thrust and Specific Fuel Consumption for Turbofan Engines DocID: 189Dy - View Document