Max thickness: 7.0% at x = 18.42% chord
Max camber: 6.1% 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.
good for all rubber powered model, as F1B, F1G