MAE 4120

Aerospace Propulsion

Course Description

Pre-Requisite(s): MAE 3210 and MAE 2100

Aero- and thermodynamics of compressible fluids in air-breathing and rocket engines. Performance and cycle analysis of air-breathing engines, emphasizing turbojets, turbofans, turboprops, and ramjets; space propulsion including rocket dynamics, thrust chamber thermodynamics, and propulsion performance; performance of axial-flow and centrifugal compressors; turbines; and the matching of engine components.


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