16.122 Analytical High Speed Aerodynamics
Analysis of external inviscid, transonic, supersonic, and hypersonic flows over thin airfoils and lifting bodies of revolution. Analyses formulated using singular perturbation and multiple scale methods and parametric differentiation. Non-linear, unsteady transonic flow. Prandtl-Meyer flow. Body of minimum wave drag. Sonic boom. Hypersonic equivalence principle. Hypersonic similarity rule (matched asymptotic expansions).
16.122 will not be offered this semester. It will be available in the Spring 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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