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AER E 411: Aerospace Vehicle Propulsion

(3-0) Cr. 3. F.S.

Prereq: AER E 311, AER E 344
Atmospheric propulsion system performance and cycle analysis. Momentum theorem, thrust and propulsive efficiency. Thermodynamics of compressible flow with heat and work addition. Components and principles of turbojet, ramjet, and turbofan aircraft engines. Introduction to rocket engines.