AE 4660 - Aerospace Propulsion I

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 either (ME 3560 or AE 3610), with a grade of “C” or better required in all prerequisites.

Credits: 3 hours

Restrictions: This course restricted to majors in aerospace engineering.