AAE 4660 - Aeronautical Propulsion Systems

Thermodynamics and fluid dynamics of aeronautical rotating turbomachines, including axial turbines, compressors, mixed flow, and centrifugal machines. Analytical and computational methods will be used to design and determine performance of aircraft propulsion systems.

Prerequisites & Corequisites: Prerequisites: ME 2320; and (ME 3560 or AAE 3710).

Credits: 4 hours
Lab Hours: (4 to 0)