AE 162 - Aerodynamics II

3 units
Two-dimensional and three-dimensional, incompressible and compressible potential flow theory. Airfoil and wing theory for subsonic, supersonic, and hypersonic flows. Flow visualization in a water tunnel. Lift and drag measurements in a subsonic wind tunnel.

Lecture 2 hours/Lab 3 hours.

Prerequisite(s): C or better in ENGR 100W, MATH 33A and (AE 160 or ME 111), or graduate standing.
Grading: Letter Graded

Class Schedule | Syllabus Information | University Bookstore