Max thickness: 8.0% at x = 23.06% chord
Max camber: 1.8% at x = 41.73% chord
Available data sources:
JavaFoil+Calcfoil stall+Eppler ext transition
Coordinates from TraCFoil.
Commercial use of the airfoil may be restricted by the designer's copyright.
F5K-GPS Triangle (min. Cd at Cl=0.2 at Re=200k) wing root