AE 3710 - Aerodynamics II

An introduction to compressible aerodynamics and boundary layer theory, including subsonic and supersonic flows over wings and bodies and viscous flows. Emphasis is placed on application of the basic theory for solving practical aerodynamic problems in the design of flight vehicles.

Prerequisites & Corequisites: Prerequisites: AE 3610; MATH 3740; ME 2580; with a grade of “C” or better in all prerequisites.

Credits: 3 hours

Restrictions: Restricted to majors in aerospace engineering.