ENGRMAE 136
Aerodynamics
Advanced potential flow, including vorticity, circulation, and the Kutta-Joukowski theorem. Incompressible flow over 2D inviscid airfoils. Prandtl lifting-line theory for finite wings. Effects of viscosity and compressibility. Elements of supersonic aerodynamics. Source and vortex panel methods.
Prerequisites & course information
Advanced potential flow, including vorticity, circulation, and the Kutta-Joukowski theorem. Incompressible flow over 2D inviscid airfoils. Prandtl lifting-line theory for finite wings. Effects of viscosity and compressibility. Elements of supersonic aerodynamics. Source and vortex panel methods.
Sources
- Course catalogue ↗2026-2027