AE 262 - Advanced Aerodynamics

3 units
Thin airfoil theory. Prandtl’s lifting-line theory. Subsonic and supersonic airfoil and wing theory. High-angle of attack aerodynamics. Boundary layer theory; Blasius and Falkner-Skan solutions, compressible boundary layers, turbulent flows, separation criteria.

Prerequisite(s): BSAE or Instructor Consent.
Grading: Graded

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