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AE 162

Aerodynamics II

Description
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. Prerequisite:Allowed Declared Majors: Aerospace Engineering, Mechanical Engineering. ENGR 100W, MATH 133A, AE 160 or ME 111 (with a grade of 'C-' or better in each). Or Graduate Standing. Misc/Lab: Lecture 2 hours/lab 3 hours.

Grading
Normal Grade Rules

Units
3