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.

Credits: 3 hours

Restrictions: This course restricted to majors in aerospace engineering or aeronautical engineering.

When Offered: Spring