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Apr 24, 2024
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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.
Misc/Lab: Lecture 2 hours/lab 3 hours.
Prerequisite(s): 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. Grading: Graded
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