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Aug 14, 2024
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AE 162 - Aerodynamics II 3 unit(s) 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. Allowed Declared Majors: Aerospace Engineering, Mechanical Engineering. Grading: Letter Graded
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