Course Catalog (as of Mar 2001)
Aeronautical and Astronautical Engineering
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A A E 211. Aerodynamics II, Incompressible Flow
Equations of motion for incompressible flow, both inviscid and viscous; potential flow theory, inviscid airfoil theory: two- and three-dimensional, Navier-Stokes equations, laminar boundary layer and transition to turbulence.
Prerequisite: A A E 210, C S 101, MATH 280.
3 hours.