Max thickness: 6.1% at x = 15.61% chord
Max camber: 5.4% at x = 39.72% 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.
F1B,G models Re~40k Trip Top 30% Botom 5%