16.121 Analytical Subsonic Aerodynamics
Analysis of external inviscid, subsonic, flow over aerodynamic thin airfoils and slender lifting bodies. Analyses formulated using singular perturbation and multiple scale methods. Linearized theory. Similarity. Rayleigh-Janzen method. Prandtl-Glauert method. Göthert similarity rule. Subsonic flow past a wave-shaped wall.
16.121 will not be offered this semester. It will be available in the Fall semester, and will be instructed by W. L. Harris.
Lecture occurs 9:30 AM to 11:00 AM on Mondays and Wednesdays in 33-422.
This class counts for a total of 6 credits.
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