16.121 Analytical Subsonic Aerodynamics


Class Info

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.

This class has 2.25, and 18.085 as prerequisites.

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.

You can find more information at the 16.121 LOW-SPEED AERODYNAMICS site or on the 16.121 Stellar site.

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