VU Computational Aerodynamics, 322.079
For the description of the course and registration, see TISS.
Lecture notes
Part A: Analysis
Compressible Potential Flow Over a Thin Airfoil: Asymptotic Expansion
Supersonic Potential Flow Over a Thin Airfoil at Zero Lift: D'Alembert Solution
- Subsonic Potential Flow Over a Thin Airfoil at Zero Lift: Prandtl-Glauert Mapping
- Thin Airfoil Theory: Circulation and Lift
- Boundary-Layer Theory