Max thickness: 6.0% at x = 14.30% chord
Max camber: 6.9% 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.
F1H,A Re40-60k tt30% t