Wind tunnel controls
Educational approximation only: Lift slope is approximated as 2π per radian, with a heuristic stall loss beyond 15°. Drag uses a simple quadratic polar. Streamlines are illustrative, NOT CFD.
Lift
Drag
CL / CD
Explore a simplified aerodynamic model for a 2D airfoil.
Educational approximation only: Lift slope is approximated as 2π per radian, with a heuristic stall loss beyond 15°. Drag uses a simple quadratic polar. Streamlines are illustrative, NOT CFD.