16.110
Flight Vehicle Aerodynamics
Aerodynamic flow modeling and representation techniques. Potential farfield approximations. Airfoil and lifting-surface theory. Laminar and turbulent boundary layers and their effects on aerodynamic flows. Nearfield and farfield force analysis. Subsonic, transonic, and supersonic compressible flows. Experimental methods and measurement techniques. Aerodynamic models for flight dynamics.
Prerequisites & course information
Prereq: 16.100 or permission of instructor G (Fall) 3-1-8 units
Sources
- Course catalogue ↗2026–2027