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AERO 4402 [0.5 credit] Aircraft Propulsion


Propulsion requirements, effects of Mach Number, altitude, and application; basic propeller, turboshaft, turbojet, turbofan; cycle analysis and optimization for gas turbine power plant; inter-relations between thermodynamic, aerodynamic and mechanical designs; rocket propulsion; selection of aeroengines.
Prerequisite(s): MAAE 2400, MAAE 3300 and MATH 3705.
Lectures three hours a week.