AAE 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: AAE 3610; MATH 3740; ME 2580.

Credits: 3 hours