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.
