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MECH 481 Aerodynamics of Aircraft I

Analysis of airfoils and wings. Potential flow, thin airfoil theory, lifting line analysis of wings. Predicting viscous drag. Numerical methods for analysis and design of airfoils and wings. Use of wind tunnels for experimental study of aerodynamics.

This course is not eligible for Credit/D/Fail grading.

Credits: 3

Pre-reqs: MECH 380.

Status Section Activity Term Interval Days Start Time End Time Comments
RestrictedMECH 481 101Lecture1 Mon Wed Fri13:0014:00