D: Applied Aerodynamics
This part (unit D) covers aerodynamics of 3-D airfoils and basic boundary layer models.
D-1/D-2: Aerodynamics of Wings (1) & (2) covers aerodynamics of 3-D airfoils in low-speed and high-speed (with compressibility effects).
D-3: Boundary Layer Modeling covers basic boundary layer models (laminar and turbulent).
D-4: LLT and VLM for Finite Wings demonstrates Prandtl’s Lifting Line Theory (LLT) and Vortex Lattice Method (VLM) solutions for 3-D finite wings.