thin airfoil theory panel code unsteady aerodynamics

This animation has been created for course AE4135 Rotor Wake Aerodynamics at TU Delft, Aerospace Engineering MSc program. The video shows the unsteady aerodynamic respons for an oscillating airfoil at reduced frequency k=0.1 (unsteady domain). Programmed in Matlab, based on Katz & Plotkin Aerodynamics chapter 13.